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SAE International

SAE Papers

Paper Number Paper Title Book Number
2008-01-2258 Destructive Evaluation of Four Aircraft Representative of the General Aging Aircraft Fleet V117-2008
2008-01-2259 The Fatigue Behavior of Fastener Joints V117-2008
2005-01-3195 Improving the Harrier: Projected Developments of the Pioneering V/Stol Combat Aircraft 1957-1990
2-26-1-13 Dassault--Business Aviation Pioneer
2-24-5-29 Farnborough Preview
2004-01-1800 International Intrigue, Paper Clips, and Envelope Pushing Research in the Heartland
2-23-11-31 American Attack UavS--Part Ii
2-23-10-16 American Attack Uavs--Part 1
2-23-7-17 Prosperity in the Face of Challenge
2-23-6-13 The Growth of An Industry
2-23-5-14 Paris Air Show: the Details
2-23-3-12 The Dawn of the Jet Age: the First 10 Years
2002-01-2949 A Longitudinal Slip Tire Model for Brake Control Systems: Features and Uses in Simulation, Control Synthesis and Stability Analysis
2002-01-2963 Airline Pilots Perceptions of and Experiences in Crew Resource Management (Crm) Training
2002-01-2965 An Automated System Framework for Pre-Mission Success Evaluation of Medical Emergency Helicopters Operations-Derived Mission Capability Sub-Module
2002-01-2948 Asymmetric Approach in Solving Aircraft Brake Vibration
2002-01-2958 Atn Airborne Implementation
2002-01-2968 Designing User-Interfaces for the Cockpit: Five Common Design Errors and How to Avoid Them
2002-01-3012 Determining Optimum Redesign Plans for Avionics Based on Electronic Part Obsolescence Forecasts
2002-01-2947 Development of Reduced Catalytically Active Runway Deicer Fluids for Carbon/Carbon Composite Friction Materials
2002-01-2924 Economic Viability of NasaS Next-Generation Aviation Paradigm: a Summary of Research Findings
2002-01-2953 Electric Starting of Large Aircraft Engines
2002-01-2945 End Item Temperature Test--An Improved Lru-Level Screen
2002-01-2998 Enhanced Security Flight Deck Doors-Commercial Airplanes
2002-01-2916 Estimation Technology of the Bell Model M427 Helicopter Using Parameter Assessment of the Dynamic Stability Characteristics
2002-01-3001 Fea Cyclic Symmetric Fatigue Analysis of Aircraft Wheels
2002-01-2957 Fire Resistant Composites
2002-01-2931 Fuel Transfer System in the Conceptual Design Phase
2002-01-3008 Highlights of NasaS Systems Approach to Crashworthiness Research
2002-01-3006 Hud Symbology for Surface Operations: Command Guidance Versus Situation Guidance Formats
2002-01-2956 Hybrid-Ceramic Circumferential Carbon Ring Seal
2002-01-2927 Identification and Evaluation of Technologies for the Development of a Quiet Supersonic Business Jet
2002-01-2930 Impact of Configuration and Requirements on the Sonic Boom of a Quiet Supersonic Jet
2002-01-2990 Improving the Aerodynamic Efficiency of High Lift Devices By a Stiffness-Oriented Re-Design With Tailored Laminates
2002-01-3010 Incorporation of Lean Principles Through the Use of Flexible Fuel Tubing in a Large Military Transport Aircraft
2002-01-3004 Metastable Beta Titanium Spring Performance At Elevated Temperature
2002-01-2942 Method for Analyzing Lubricating Oil Contamination of Aircraft Systems
2002-01-2918 Model of Casing Treatment Influence on Compressor Rotor Efficiency
2002-01-2974 One-Pass Pricing Methodology
2002-01-2944 Past, Present, and Future of the Gas Turbine Engine Simulator; a Technical and Financial Analysis
2002-01-3000 Photon-Induced Positron Annihilation (Pipa)-A New, Core Technology to Improve the Nondestructive Inspection and Life Prediction for Critical Components
2002-01-3011 Plastic Ball-Grid-Arrays (Pbga): Are They Ready for Environmentally Harsh Aerospace Applications?
2002-01-2929 Quiet Supersonic Jet Engine Performance Tradeoff Analysis Using a Response Surface Methodology Approach
2002-01-2983 Recommendations for Future Avionics Hardware Development
2002-01-2922 Relative Guidance of Aircraft: Analysis and Comparison of Two Control Approaches
2002-01-2951 Reliable Bearing Wear Detection System for On-Condition Maintenance of Electric Generators
2002-01-2954 Sensorless Control of Brushless Dc Motor for More Electric Aircraft
2002-01-2985 Software Tools for the Development of Design Decision Support for Re-Configurable Unmanned Arial Vehicles
2002-01-2928 Solution of the Non-Synchronous Vibration in the As900 Engine
2002-01-3007 Tail Icing Effects on the Aerodynamic Performance of a Business Jet Aircraft
2002-01-2939 The Benefits of a Wire Integrity Program
2002-01-2970 The Efficacy of Using Synthetic Vision Terrain-Textured Images to Improve Pilot Situation Awareness
2002-01-3023 The Gp7200 Engine-Power for the Airbus A380
2002-01-2971 Use of Enhanced Vision Sensors for Approach Hazard Detection
2002-01-2923 Use of VictrexSr PeekSt Thermoplastic to Drive New Designs, Processing Flexibility, and Cost Reduction in Aerospace Components
2002-01-3013 Utilization Life of Electronic Systems-Aging Avionics Usable Life and Wear-Out Issues
2002-01-2995 Vertical Drop Test of a Narrow-Body Transport Fuselage Section With Overhead Stowage Bins
2002-01-2997 Vertical Drop Test of a Transport Fuselage Section
2002-01-2912 Wind-Tunnel Investigation of Commercial Transport Aircraft Aerodynamics At Extreme Flight Conditions
2-22-5-16 Civil and Military Technologies in Close Formation
2000-01-5514 Lessons Learned From the British Aircraft Corporation Tsr2 Project
2000-01-5516 Specialized Anti-Armor Aircraft of the Eastern Front: 1941-1945
2000-01-5517 The Clark Y Airfoil: a Historical Retrospective
2000-01-5515 WorldS First Delta Wing Airplane Convair/Air Force Xf-92a
975609 Milestones in Airborne Astronomy: From the 1920s to the Present
975652 The Origins of the Anti-Ship Guided Missile
965598 Menasco Aircraft Engines: Air Racing Paragon of the 1930s
942192 Observations and Future Opportunities Reflected Upon From Sixty Years as a Student and Participant in the Air Transport Industry
690678 Integrated Flight Test Data System With Real-Time Graphic Display
690337 A Low Cost Inertial Measurement Unit for Business Aircraft
690658 A New Concept to Provide Emergency Auxiliary Power for Aircraft
690674 Advanced Technology in Airline Passenger Food Services
690305 Aerodynamic Improvements for Agricultural Aircraft
690434 Aircraft Fuel Vent Line Sensitivity to Lightning Effects
690744 Aircraft Hydraulic Pumps for High-Speed Operation
690340 Aircraft Proximity Warning Devices
690553 Aircraft and 4-Wheel-Drive Ground Vehicles for Forest Fertilization
690561 Airplane DesignerS View of Aircraft Ground Support
690399 Airport Terminal Planning for TomorrowS Aircraft
690394 An Airline Looks At Area Navigation
690195 Application of Computer Graphics in Aircraft Design
690342 Application of Glass-Reinforced Plastic Molding Compounds in the Ov-10a Airplane
690406 B-52 Flight Experiments in Direct Lift Control Under the Load Alleviation and Mode Stabilization Advanced Development Program
690335 Bioengineering of Impact Survival in Business Aircraft
690381 Booster Engines for Commercial Airliners
690628 Cast Hardware Parts Are Being Produced for the Aircraft Industry That Are Virtually Ready for Installation
690320 Changing Airworthiness Requirements for Air Taxi Operators and Their Effect on Manufacturers of Small Airplanes
690725 Computer Planning of Aircraft Manufacturing With the Optical Image Terminal
690403 Control Concepts for a High Bypass Aircraft Turbofan Engine
690313 Conversion of Lightweight Commercial Aircraft to Fulfill a Specific Military Mission
690375 Deceleration and Control of Aircraft on the Ground When Ground Friction Has Been Lost Or Only Sliding Friction Exists
690673 Design and Testing of An Aircraft Nucleonic Fuel Quantity Gaging System
690706 Design of Fighter Aircraft for Combat Survivability
690724 Determination of the Influence of Propeller Thrust on the Coefficient of Lift and the Coefficient of Drag of An Airplane Using a Triple-Slotted Flap At Various Deflections
690675 Development Testing of the New Generation of Large Jet Aircraft
690315 Development of Army Utility Aircraft Model U-21a - An Unpressurized Version of the Beech King Air
690413 Development of Total Airline Profit Model Program to Permit Simulation and Evaluation of Total Air Cargo System
690696 Development of a Digital Variable Stability System for Evaluating Design Parameters of Vtol Fixed-Wing Aircraft
690701 Developments in Soviet Aerospace Manufacturing Technologies
690344 Distance-Measuring Equipment for the Supersonic Transport and the Corporate Aircraft
690327 Effectiveness of Aircraft Cockpit Tv-Radar in Providing Navigational, Weather and Traffic Data
690346 Electrical Power Sources for Business Aircraft
690318 Electron Beam Welding in Aircraft Components
690630 Electron Beam Weldments for Large Complex Shapes of the Type Used in the Aircraft Space Industries
690659 Emergency Monopropellant Auxiliary Power Units for Large Commercial Aircraft
690425 Evolution of the Pratt & Whitney Aircraft Jt9d Engine Oil System
690321 FAA Crashworthiness Program for Large and Small Airplanes
690680 Fabrication Techniques With Hy-140 Steel for Flight-Type Pressure Vessels
690662 Flight Tests and Analysis of Lifting Body Reentry Vehicles
690536 Fluidic Vortex Valve Servoactuators - An Advancement in Helicopter Flight Control Systems
690308 Functional Compatibility Analysis of Aircraft-Engine Fuel Systems
690379 Ge4 Supersonic Transport Engine--Development Progress and Status
690560 Ground Support and Service Features for the B-747 and Dc-10 Aircraft
690328 Human Factors Evaluation of Aircraft Engine Instrument Displays
690670 Hydraulic System State-Of-The-Art Advances on the 747 Airplane
690436 Ignition of Aircraft Fluids on High Temperature Engine Surfaces
690614 Integrated Program of Dynamic Tests and Analyses Required to Evaluate, Develop, and Qualify An Aerospace Vehicle
690414 Long-Term Trends in Airlines Economics
690424 Lubricant Evaluation and Systems Design for Aircraft Gas Turbine Engines
690667 Lubricity of Aviation Turbine Fuels
690619 Lunar Module Environmental Control Subsystem
690625 Lunar Module Thermal Control and Life Support Systems for Apollo Applications
690664 Materials Applications and Structural Concepts for Hypersonic Air-Induction Systems
690631 Mechanical Ground Support Equipment for the Next Generation of Military Aircraft
690668 Methane Fuel Systems for High Mach Number Aircraft
690402 Metropolitan Airports for V/Stol Aircraft
690423 Modern Application of Engine Oil Analysis to Airline Operation
690329 Modular Hydraulic Power Systems for General Aviation
690437 Nitrogen Inerting of Aircraft Fuel Tanks
690617 Nonuniformities of Reverberant Sound Fields and Their Implications for Sonic Test Specification
690332 On Board Gas Turbine Apus for Executive Aircraft
690415 Passenger Airplane Economics and Systems Application Considerations for Airline Operations
690341 Potential Structural Materials and Design Concepts for Light Airplanes
690432 Radiation Pyrometer Designed for In-Flight Measurement of Compressor Blades of Turbine Engine Temperatures
690378 Review of Operational Experience and Pilot Considerations for Aircraft Ground Operations--Including Handling, Take-Off, and Taxiing
690334 Simplified Fuel Systems for Light Aircraft
690371 Sonic Testing of Gray Iron Sleeve Castings to Predict Tensile Strength
690707 Survivability Design of Forward Air Control and Light Attack Aircraft
690705 Survivability of Military V/Stol Transport Aircraft
690712 Systems Approach to Flammability Control for Aerospace Safety Application
690741 Systems Concepts in Control Design for Industrial and Commercial Aviation Applications of Auxiliary Power Units
690621 Transient Thermal Performance Prediction of the Lunar Module Environmental Control System
690049 Ultrasonic Measurement and Influence of Nonmetallic Inclusions on Fatigue and Engineering Behavior of Medium and High-Strength Steels
690314 Usaf Special Operations Force Experience in the Use of General Aviation Aircraft for Reconnaissance, Liason, and Other Activities
690316 Use of Explosive Forming in the Fabrication of Aircraft Components
690690 Versatile Titan Iiic Launch Vehicle Digital Flight Control System
690693 Vtol Flight Investigation to Develop a Decelerating Instrument Approach Capability
690635 Wheeled Mobility Design for Aerospace Ground Equipment Trailers
680712 Requirements of the Propulsion Systems for Multimission Aircraft
680713 Some Implications of Noise Restrictions to Subsonic Transport Engine-Installation Design, Development, and Operation
680277 Adaptive propulsion systems for future supersonic military aircraft
680288 Airframe-propulsion integration for future military aircraft
680205 Analysis of airplane vibrations using cantilevered component modes
680294 Careful integration of exhaust nozzle airframe and engine is needed on modern high-speed aircraft
680287 Closer integration of inlet and engine can bring improvements in propulsion systems of high-speed aircraft
680208 Combustion heating system for business and utility aircraft
680285 Cost and operational problems of a scheduled helicopter airline
680204 Design requirements of C-5A military cargo aircraft
680274 Development of special airports for STOL aircraft
680202 Devices for stick free stability in light aircraft
680215 General aviation avionics equipment reliability
680203 Initial report on operational experiences of general aviation aircraft
680219 Maintenance program for the executive operator of aircraft
680275 Metropolitan and intercity transportation system of future will use helicopters and high-speed VTOL aircraft
680214 Minimum standards are needed for electronic equipment used in aircraft that participate in air traffic control system
680206 New fastener systems for aircraft include expensive use of titanium alloys, and the application of oversize or interference fit systems
680283 Operational problems with current commercial V/STOL aircraft
680296 Performance installation effects for exhaust nozzles installed on a twin-jet fighter airplane model
680286 Problems of integrating air for aircraft operation at Mach 2 and up
680201 Recent Transonic Airfoil Developments of Some Business-Aircraft Implications
680279 Research problems and outlook for the next generation of aircraft engines
680299 Results of the American Airlines evaluation of the Litton LTN-51E inertial navigation system
680272 Role of the small jet in the airline training syllabus
680298 Seaboard World Airlines experience with Decca Omnitac equipment for determining aircraft position
680290 Significance of Adhesively Bonded Construction on Aircraft Lightning Protection
680297 Status and future of aircraft satellite navigation
680326 VTOL aircraft will assist airlines in solving problem of over crowded airport facilities
680295 Variable-geometry exhaust nozzles and their effects on airplane performance
680280 Wind tunnel investigations of a high-speed stowed rotor aircraft
680199 Aerodynamic Development of Cessna 177 Four-Place Single-Engine Cantilever-Wing Airplane
680339 Air Pollution Emissions From Jet Aircraft Operating in New York Metropolitan Area
680671 Aircraft Integrated Data Systems as a Flight Operations Tool
680221 Aircraft Maintenance During and After Warranty
680223 Aircraft Noise Abatement Through Legislation
680721 Astronaut Safety Features for Apollo Lunar Surface Experiments Package
680311 Auxiliary Power Systems for 1975 Fighter Aircraft
680651 Brazing and Welding Beryllium Assemblies for Aerospace and Nuclear Structures
680216 Constant-Frequency A-C Electrical System for Business Aircraft
680231 Contamination and Microbes Cause Corrosion and Malfunctions in Aircraft Integral Fuel Tanks
680190 Criteria for Contamination Level in Flight Control Systems
680447 Design Requirements of Small High-Temperature-Rise Combustors for Turbine Engines Designed for Vtol Aircraft
680314 Design and Fabrication of a Pressurized Boron Composite Wing Box
680646 Design and Testing of Inverted Flaps and Wing Span Flaps
680337 Design of Pratt and Whitney Aircraft Jt9d Turbofan Engine for Maintainability
680099 Design of Vehicles for the Lunar Environment
680057 Designing An Aircraft Engine Fuel Pump to Meet Specified Vapor-To-Liquid Ratios
680313 Designing and Fabricating Aircraft Structures With Filamentary Composites
680545 Designing the Lockheed L-1011 Jet Transport to Meet Airline Needs Beyond 1970
680693 Development of a Composite Main Rotor Blade for Sud-Aviation Sa-330 Helicopter
680331 Diffusion Bonded Structures of Titanium Alloy for Application to Air Transport Aircraft
680222 Dinade System as An Aircraft Anti-Collision Device
680340 Effect of Dynamic Environments on Aircraft Fuel Tank Flammability
680056 Environmental Control Accessories Test Facilities Needed to Provide Life and Increased Reliability of Future Aircraft
680725 Evaluation of An Air Conditioning System for a 1970 Short Haul Commercial Jet Aircraft
680342 Fatigue-Life Establishment and Detection in the Field of Aircraft Maintenance
680670 Flight Monitoring and Analysis
680333 Four Turbofan Engines Power C-5a Military Logistics Aircraft of 712,000 Lb Design Gross Weight and 5500-Nautical-Mile Range
680209 Fuel Flow Measured With Turbine Meter in New Fuel Measurement System for Medium-Priced Aircraft
680728 Ideas, Integrated Design and Analysis System Aids Sizing and Analysis of Aircraft Primary Structure
680727 Impact of Maintainability Analysis on Aircraft Design
680724 Impact of the Physiological Characteristics of Perishables on Aircraft Environmental Control Systems
680711 Inlet and Fan Aerodynamics for Multimission Military Aircraft
680690 Installation Features of Rolls-Royce Three-Shaft Turbofan Engines for Large Subsonic Transport Aircraft
680709 Installation of Boeing Auxiliary Power Unit in 747 Aircraft
680354 Integral Weight and Balance System Applications on Cargo Aircraft
680225 Low-Cost Capacitance Fuel Gaging System for Business Aircraft
680644 Low-Speed Characteristics of High-Performance Lift-Engine V/Stol Aircraft
680317 Lubricants for Inerted Lubrication Systems in Engines for Advanced Aircraft
680373 Manned and Unmanned Roving Vehicles for Lunar Exploration
680733 Mechanism of Deposit Formation in Wing Tanks
680718 Microbiological Studies on a Water Management Subsystem for Manned Space Flight
680310 Modular Accessory Concept for Turbine Engines in Military Aircraft
680716 On-Board Aircraft Oxygen Generating System
680374 Operational Characteristics of Manned Lunar Flying Machines
680355 Pan American Operational Experience With Stan--An On-Board Aircraft Weight and Balance System
680226 Performance Characteristics of Aircraft With Turbosupercharged Engine and Cabin--1968
680325 Place of Cargo Aircraft in Total Air Transportation
680278 Potential Characteristics of Powerplants for a Aircraft of the 1980s
680691 Potential Technology Improvements for the Dual-Rotor High Bypass Ratio Cf6 Turbofan Engine Designed for Use in Trijet Aircraft
680227 Propeller Design Considerations for Turbine-Powered Aircraft
680744 Reliability and Maintainability Problems Confronting Environmental Control/Life Support Systems for Long Duration Space Flight
680100 Remote Control of Both Lunar Based and Earth Bound Vehicles
680708 Secondary Power Requirements for Large Transport Aircraft
680370 Short Downrange Entry Performance of Spacecraft Having Maximum Hypersonic Lift to Drag Ratio of 2.2
680399 Sonic Throttling Intake Valves Allow Spark-Ignition Engine to Operate With Extremely Lean Mixtures
680666 Stol/Vtol Aircraft Characteristics, Terminal Navigation, and Air Traffic Control
680058 Structural Requirements for Aircraft Engine Main Fuel Pumps and Controls
680371 Study of Orbital Space Flight Emergency Shows Reentry Escape Systems Are Best
680729 Systems Analysis Applications to the C-5 Troop/Cargo Military Aircraft
680648 Systems Considerations for Aerospace Beryllium Applications
680346 Techniques for Measuring Smoke From Aircraft Jet Engines
680738 Titan Iii Launch Vehicle Flight Test Experience
680228 Turboprop Engine Operational Experience in Stol Aircraft Operating From Rough Fields
680330 Use of Beryllium for Aircraft Structural Components
680312 Use of Pneumatic Power System to Supply Aircraft System Power Remote From Propulsive Engines
680309 Variable-Speed Constant-Frequency Power Source for Aircraft
680663 Vtol Aircraft Terminal Area Operations Research
680673 Vulnerability and Crashworthiness in the Design of Rotary Wing Vehicle Structures
680220 Ways for Light Plane Pilot to Avoid Trailing Vortex Hazard, Or the Wake Turbulence of Heavy Aircraft
680303 Wind Tunnel Test Considerations Unique to V/Stol Aircraft
670693 United Aircraft 550-shp ST6 turboshaft engine has many marine and industrial applications
670353 Adam(Air Deflection and Modulation)Is Applied to Propulsive Wing Airplane Configurations Housing Propulsion System
670337 Adopting Space Vehicle Checkout Procedures and Philosophy to Near-Future Transport Aircraft
670244 Aerodynamic Considerations for 300-Mph Business Airplane - Handley Page Jetstream Twin Turboprop Airplane
670880 Aerodynamic Design Considerations of Variable Geometry Aircraft
670847 Aerodynamic Design Features of the C-5a Subsonic Jet Military Transport
670846 Aerodynamic Design of the Wing and High-Lift System of the Dc-9 Short-To-Medium-Range Jet Transports
670243 Aerodynamics of the Cessna Tandem Twins Business Aircraft
670984 Air Conditioning System of Concorde Supersonic Transport Is Bootstrap Air Cycle, With Fuel and Ram Air Cooling in Intercooler Loop
670811 Aircraft Companies Face Many Problems in Meeting Rule 66, Which Controls Emission of Organic Solvents in Los Angeles County
670370 Aircraft Fuselage Configuration Studies Point to Use of Multideck Fuselages
670982 Airline Considerations for the Supersonic Transport Environmental Control System
670891 Airline Operation and Maintenance Requirements for Fasteners
670865 Airline View of Supersonic Transport Powerplants
670622 Apollo Applications Program Is Determining Feasibility of Long-Duration Space Missions Through Use of In-Flight Maintenance
670888 Application of Fasteners to Large Aircraft Gas Turbine Engines
670230 Approach By Quebec to the Use of Special Aircraft for Forest Fire Suppression
670814 Availability and Evaluation of Nonphotochemically Reactive Primers and Topcoats for Aerospace Applications
670547 Axial-Gear Differential Constant-Speed Drives for Driving Constant-Frequency A-C Generators on Aircraft
670382 Ballistic Versus Lifting-Body and Winged Recovery Techniques for Space Launch Vehicles With Small Payload
670566 Bobbin Metal-To-Metal Seal for Separable Joints Should Overcome Problem of Leaking Joints in Missile, Aerospace, Or Aircraft Systems
670249 Cold Starting and Service Test Evaluation of SAE 10w-30 Aircraft Engine Oil
670530 Comparative Evaluation of Flight Control Power Distribution Systems for Hypersonic Aircraft
670138 Control System Requirements for Advanced Direct-Lift Engine Designed for Mach 2 Fighter Aircraft
670939 Corrosive Piston-Ring Wear Is Much Less With Chrome-Faced and Molybdenum-Filled Rings Than With Cast-Iron Wings
670344 Design Criteria and Configuration for Long-Life Aircraft Turbine Engines
670579 Design Objectives for Aircraft Escape Systems of Tomorrow
670242 Design of Gulfstream Ii - a Low Wing Business Aircraft - of Moderate Sweep, Powered By Two Aft-Mounted Turbofan Engines
670582 Design of Integrated Flight Control/Hydraulic System for Boeing 2707 Supersonic Transport Aircraft
670234 Designing Business Jet Aircraft Engines for Increased Service Life
670371 Determining the Size of the Supersonic Transport
670617 Development of Improved Gust Load Criteria for U.S. Air Force Aircraft
670241 Development of the Third Level Airline (Air Taxi) Industry
670341 Discipline in Airline Organization Helps Provide Safe, Economical Transportation
670355 Economics of Airline Scheduling as Frustrated By the Total System Environment
670363 Eight Diagnostic Devices Being Considered for the Supersonic Engine
670365 Emulsified Jet Engine Fuel Helps Reduce Possibility of In-Flight Or Post Crash Fires
670575 Escape System Requirements for U.S. Army Aircraft in Vietnam
670228 Estimating Maintenance Man-Hours Per Flight Hour for Business Turbojet Airplanes
670374 European Point of View on Recoverable and Reusable Spaceflight Systems (Aerospace Transporter)
670349 Failure Safety in Rotary Wing Operations
670384 Fixed Wing Reusable Booster Concepts Compared on the Basis of Weight, Cost, Technical Difficulty and Availability Date
670574 Flight Control System for C-54 Military Transport Aircraft
670528 Flight Control System for the Boeing 2707 Supersonic Transport Airplane
670571 Flight Control and Stability Augmentation Systems for Xc-142a V/Stol Aircraft
670869 Fuel Distribution Facilities Account for Large Part of Microbial Contamination in Fuel Found in Jet Aircraft Fuel Tanks
670338 Future Needs and Current Advances in Aircraft Maintenance
670686 Future of Vtol Aircraft Depends on Recognition of Need to Select Proper Type for Each Specific Role
670237 General Problems in Vibration of Aircraft Powerplant Components
670559 Ground Flotation Requirements for Military Aircraft
670196 Guided-Light Concept of Internal Light Distribution Is Applicable to Aerospace Control Console Panels and Indicating Instruments
670245 High Lift Techniques for Stol Aircraft
670562 High-Flotation Landing Gear for Ov-10a Small Multipurpose Military Aircraft
670561 High-Flotation Landing Gear for the C-5a Military Transport Aircraft
670529 Hydraulic Power Units for Supersonic Aircraft
670343 If Airline Operations Are to Grow, Its People Must Pay Attention and Make Use of All the Facilities Available
670631 Impact of Maintainability Engineering Techniques on the Design of the F-111 Aircraft
670253 Impact of Microelectronics on General Aviation Avionics
670669 Improving Aerospace System Safety Programs Through An Inter-Company Information Exchange
670329 Inertial Navigation Systems for Subsonic and Supersonic Commercial Aircraft
670254 Instrument Landing System for Business Jet Aircraft Operating in Category Ii Weather Minima
670871 Jet Engine Malfunction Diagnostic System Using Sonic/Vibration Analysis
670581 Lunar Environment Simulation Test Bed
670577 Lw-3b Escape System for Low and Medium Performace V/Stol Aircraft
670835 Managing Engineering for Profit in the Aerospace Industry
670882 Mechanical Aspects of Variable Sweep Wings, as Used on F-111 Aircraft
670873 Mechanical Impedance Approach to Jet Engine Vibration Transmission Into An Aircraft Fuselage
670861 Metal-Matrix Composites Show Promise for Aerospace Applications
670389 Multimodule Reusable Booster Concept Emerges From Study of Hypersonic Vehicles
670658 Navy A-7a (Corsair Ii) Aircraft Maintenance Guarantee and the Role of Training
670339 New Advances in Nondestructive Testing Techniques for Turbojet Engines and Aircraft
670548 Noise Control of Aircraft Auxiliary Power Units
670394 Operational Experience of the X-15 Airplane as a Reusable Vehicle System
670217 Packaging of Electronic Signal Conditioning Equipment for the Project Apollo Lunar Module
670665 Parametric Relationships of Factors Affecting Maintainability of Long Duration Manned Space Flights
670031 Peak to Valley Surface Roughness Control Is Being Used on Aerospace Production Hardness
670879 Pilot Comments on Variable Geometry Aircraft
670328 Place and Capabilities of Modern Doppler Systems for Subsonic and Supersonic Aircraft
670354 Potential Improvements in Thermal Management of Hypersonic Aircraft for Mixed Missions
670246 Preliminary Studies of a Supersonic Business Jet
670248 Present Day Lubricants for Utility Aircraft Engines
670239 Professional Growth of Engineers With Business Aircraft Manufacturers
670348 Progress on All-Weather Operations for V/Stol Aircraft
670373 Proposed New Approaches to the Maintenance of the Boeing Supersonic Transport
670342 Psychological Variable in Airline Safety
670827 Qualitative Estimate of Aircraft Criteria to Meet Military Short-Haul Requirements for 1970-1980
670405 Recommendations Regarding the Place of the Aerospace Transporter in European Space Program
670884 Reliability of the Boeing Sst Wing-Sweep Actuation System
670560 Results of Studies to Improve the Ground Flotation of Military Aircraft
670385 Review of European Aerospace Transporter Studies
670661 Risk Assessment in Complex Unattended Aerospace Systems
670194 Rotating Combustion Engine Can Provide Compact, Lightweight Power for Aircraft
670140 Some Aircraft Gas Turbine Environmental Challenges for the Fuel Control Designer
670392 Space Flight Operations and Economics
670550 Space Power and the Progression of Manned Space Flight Requirements
670531 Special Problems Encountered in the Design of the Hydraulic System for the Concorde Supersonic Transport
670881 Structural Considerations for Variable Sweep Wings of Fighter Aircraft
670578 Techniques for Space and Hypersonic Flight Escape (Paracone)
670901 The Role of Canada in the Second Decade of the Space Age - Inner Space Supersonics
670235 Thrust Reversers for Business Jet Aircraft
670250 Trends in Aircraft Direct-Current Electrical Systems
670358 Turbine Engine Diagnostics Helps Airlines Avoid In-Flight Engine Failures
670388 Two- Or Three-Stage Horizontal Aerospace Transporter Is Studied
670238 Two-Stroke Light-Aircraft Engine Potential
670027 Ultrasonic Method of Measuring Piston Ring Bore-Contact Patterns
670968 United Aircraft Turbotrain Has Free Turbine Engine, Lightweight Structure and Banking Suspension to Allow High Speed Operation
670333 Use of Glass Fiber Reinforced Plastics in Aircraft Engines
670585 Use of Induction Brazing Method to Form Permanent Joints in Hydraulic Tubing for the A-74 Corsair Ii Aircraft
670826 V/Stol Aircraft for Short-Haul Commercial Transportation
670878 Variable Geometry Features of Boeing Supersonic Transport Aircraft
670883 Variable Geometry Wing Is Used in Boeing Supersonic Aircraft
670889 Wide Range of Threaded Fasteners Is Available for Aerospace Industry
660274 Aerodynamic Concepts and Configuration of Xb-70a Research Aircraft and Its Airborne Systems
660734 Aerodynamic Considerations for Engine Exhaust Design for Subsonic High-Bypass Fan Engines
660733 Aerodynamic Considerations for Engine Inlet Design for Subsonic High-Bypass Fan Engines
660732 Aerodynamic Installation of High-Bypass-Ratio Fan Engines on High Subsonic Aircraft
660280 Air Transport Association Direct Operating Cost Formula for Transport Aircraft
660296 Airline Operational and Economic Goals of the Supersonic Transport Propulsion Systems
660194 Airline Practices in Forecasting Clear Air Turbulence
660277 Airplane Design Factors That Affect Direct Operating Costs
660323 Application of 5-7 Bypass Ratio Engines to Subsonic Transport Will Reduce Fuel Consumption and Increase Thrust-Weight Ratio
660208 Application of Vapor-Cycle Cooling Systems to Business Aircraft
660221 Application of the High Bypass Turbofan Engine for Business and Executive Aircraft
660337 Assisted Landing and Takeoff for Short Field Commercial Aircraft
660666 Beryllium Structures for Aircraft
660214 Birdproofing the Cockpit of the North American Sabreliner -- a High Performance Aircraft
660204 Cessna Aircraft Commercial Division Quality Control Program
660674 Changing Environment and Its Effect on Aircraft Structures
660319 Commercial Helicopter Outlook of Vertical Take-Off and Landing Aircraft Air Traffic Control System
660150 Corollary Advantages of Lunar and Terrestrial Vehicle and Power Train Research
660184 Correlation Between Clear Air Turbulence and Aircraft Electrical Activity
660207 Current and Possible Future Trends in Oxygen Equipment and Usage for Aircraft
660215 Defining the Fatigue Load Environment for Business Aircraft
660216 Design and Development of the Structural Integrity of a Jet Executive Aircraft, D.H. 125
660647 Design and Fabrication of Large Experimental Titanium Crossbeam for Aerospace Applications
660218 Development and Flight Testing a Simplified Fixed Shaft Turboprop Flight Control System
660209 Development of Air Conditioning in Beech Executive Airplanes
660314 Development of High-Performance Rotary-Wing Vtol Aircraft for the Army
660738 Development of Thrust Deflection and Vectoring in European V/Stol Aircraft
660178 Economic Aspects of Flight in Turbulence
660210 Economics of Business Aircraft
660316 Effect of Size on the Economics of a V/Stol Transport Airplane
660220 Effect of a Light Aircraft Stability Augmentation System on Pilot Performance
660670 Effects of Low Level Turbulence on the Structure of a Large Logistic Aircraft
660671 Effects of Subsonic, Supersonic, Hypersonic and Orbital Environments on Structures
660219 Evaluation of General Aviation Aircraft Flying Qualities
660664 Evaluation of Proposed Hydraulic Fluids for the Supersonic Transport
660293 FAA Concept in Safety for the Supersonic Transport
660217 FAA Research, Development, and Airworthiness Compliance for General Aviation Aircraft
660279 Factors Affecting Aircraft Utilization
660073 Factors Influencing Aircraft Turbine Engine Oil Drain Practices
660283 Flight Operations on a Circular Runway
660273 Flight Testing the Xb-70 Research Aircraft in Both Low-Speed and High Mach Number Regimes
660443 Future-Generation Spacecraft for Advanced Lunar Missions
660702 Ground Support for the Supersonic Transport
660663 Heat-Resistant Materials for Aerospace Antennas and Radomes
660322 High Bypass Ratio Turbofan Engines for Subsonic Aircraft of the 1970s
660656 High Strength Magnesium Casting Alloys for Aerospace Applications
660678 Hypersonic Aircraft Thermal-Structural Concept Trends
660737 Installation Considerations for the High Bypass Fan Engine in Subsonic Transports
660223 Jet Pump as a Fuel Pump for Aircraft of Today
660149 Locomotion Energy Requirements for Lunar Surface Vehicles
660146 Lunar Mobile Laboratory -- Design Characteristics
660449 Lunar Scientific Missions
660206 Manufacturing Methods Suitable for High Subsonic Speed Aircraft
660287 Maximizing Aircraft Production for Industrial Readiness Programs
660074 Means of Assessing Aviation Turbine Lubricant Quality
660195 Minimizing the Effects of Mountain Waves and Shear Generated Clear Air Turbulence in Airline Operations
660222 New Generation of General Aircraft Engine Mountings
660023 Novel Tube Transportation System, Under Study At Rensselaer Polytechnic Institute, Is Capable of Supersonic Speeds
660701 On-Board Checkout Systems for Aircraft
660646 Plasma Arc Welding of Titanium Up to 5/16 In. Thick--For Aerospace Structures
660205 Practical Data Processing Approach for Achieving Effective Management Control of Aircraft Manufacture
660147 Preliminary Mobility Tests of a Scale Model Lunar Roving Vehicle
660686 Problems in Management of Aerospace Ground Equipment
660310 Protective Coatings for Extended Life of Aircraft Jet Engine Parts
660634 Recent Advances in Forging Beryllium for Aerospace Applications
660213 Service and Support Are Important Functions of the Manufacturer of Business Aircraft
660305 Some Problems the Fastener Industry Perceives in Effecting Aerospace Conversion to the Metric System
660315 Stability and Control Testing of a Tilt Wing V/Stol Aircraft
660679 Structural Considerations in the Design of a Liquid Hydrogen Tank for Hypersonic Vehicles
660669 Structural Considerations of C-141a -- a Large Cargo Airplane
660673 Study of Mariner Iv and Lunar Excursion Module
660294 Supersonic Transport Operations and Maintenance Considerations
660298 Supersonic Transport Propulsion Systems--Operational Growth Feasibility
660297 Supersonic Transports--Propulsion Systems--Application of Advanced Technology
660700 Systematic Approach to Determining Aircraft Aerospace Ground Equipment
660687 Systems Approach to Aerospace Ground Equipment Management
660144 Testing of Lunar Surface Vehicles Under Simulated Lunar Gravity Conditions
660710 Turbine Fuel Thermal Stability -- From Refinery to Supersonic Transport
660333 United Aircraft Corp. Turbine Powered Train, With Emphasis on Its Suspension System
660642 Use of Reinforced Plastic Composites in Commercial Aircraft Can Bring Savings in Weight
660668 V/Stol Aircraft Structural Considerations
660318 V/Stol Transport Aircraft for Intercity Passenger Movement
660275 Xb-70 Research Aircraft Ground Servicing and Safety Precautions
650844 Military aircraft require landing gears capable of operating on soft and rough fields
650231 1953 Paper Jet Operations in Retrospect, With Connotations for the Supersonic Transport
650388 A Practical Approach to Airplane Vibration
650377 Accurate Power Checking of Production Aircraft Engines
650200 Advanced Propeller Developments for V/Stol Aircraft
650247 Aeronautical Progress in the Federal Aviation Agency
670305 Aerospace Concepts Applied to Deep Submergence Vehicle Simulation
670267 Aircraft Cabin Pressurization By Means of Turbocharger Driven By Exhaust Gases From Powerplant
650372 Aircraft Manufacturer Looks At Business Aircraft Operating Costs
650580 Analysis of Toroidal Actuation Systems for Aerospace Vehicles
650101 Application of Advanced Regenerative Powerplants to Present and Future Aircraft
650249 Army Aircraft Systems Development Program
650375 Aviation Spark-Plug Operational Factors
650367 Beech Aircraft Reliability Program
650812 Biomedical Requirements for Manned Space Flight
650269 Brief Report on Safe Handling and Usage of Aviation Gasolines and Turbine Fuels
650116 Business Aircraft Operator in Transition to Turbine Equipment
650032 Business Aviation Department Analysis
650248 C-5a Cargo Transport Aircraft
650302 Carbon-Graphites for Aerospace Seals
670257 Certification of the Sabreliner Twin Jet Executive Airplane, With Special Emphasis on Fatigue Evaluation of Structure
650833 Challenge of Alternate Approaches to the Achievement of Lunar Exploration and Exloitation
650797 Challenge of Performance Spectrum for Military Aircraft--The Meaning of Speed
650201 Choosing Lift Engines for Vtol Aircraft
650213 Community Noise Characteristics of the Supersonic Transport
650221 Compact Jets Can Solve Both the Trunk and Regional Airlines Dilemma
650263 Comparison of Regenerative and Nonregenerative Turbine Engines on Army Utility Helicopters and Medium Fixed Wing Transport Aircraft
650055 Computerized Static and Dynamic Aircraft Structural Analysis System--Engineering Aspects and Mathematical Formulation of the Problem
650053 Computerized Static and Dynamic Aircraft Structural Analysis System--Historical Background
650056 Computerized Static and Dynamic Aircraft Structural Analysis System--Programming the System
650054 Computerized Static and Dynamic Aircraft Structural Analysis System--Use of Computer Programs in Aircraft Design
650808 Control Requirements and Control Methods for Large V/Tol Aircraft
650581 Control System Aspects of An Analytical Investigation Into Controlling the Structural Modes of Flexible Aircraft
650785 Cost/Weight Merit Function for Aerospace Hardware Design
650244 Current Financial Considerations in Airline Aircraft Acquisitions
670263 Current Survey of Aircraft Fuel Gaging Systems
650235 Design Concept of a Jet Close Support Aircraft for Counterinsurgency Operations
650349 Design Margin Is Key to Lunarcraft Shock Absorber Reliability
650381 Design and Development of Cj610 Turbojet and the Cf700 Turbofan Engines for Use in Business Jet Aircraft
650227 Design of Air Force Aircraft for Safety
670259 Design of Pressurized Cabins for Business Aircraft
650013 Determination of Breguet 941 Stol Aircraft Transition Velocities With Various Flap Deflections
650264 Development and Flight Test Results of the Tri-Service X-19 V/Stol Aircraft
650573 Development of Failure-Correcting Flight Control System
650307 Development of Fluid Power Techniques for Lunar Environments
650363 Development of Gas Turbine Engine Installation in North American Aviation Sabreliner
650937 Development of the Model 727 Airplane High Lift System
650169 Donasonic Intake Silencer for Small Turbines
650805 Economical Mach 3 and Over Supersonic Transport Fuels Are Available Now
650370 Effect of Airframe Manufacturing Cost on Cost of Aircraft Ownership
650799 Effect on Airplane and Flexible Pavement Design of Varying Design Tire Pressure From 60 to 360 Psi
650225 Engine Air Inlet Compatibility for the Supersonic Transport
650226 Environmental Control System Considerations for Supersonic Cruising Aircraft
650031 Executive Operator in Transition to Turbine-Powered Aircraft
650597 Factors in Selecting Digital Or Analog Computation for Flight Control
650327 Fire-Resistant High-Temperature Hydraulic Fluids for Supersonic Transport
650364 Five-Point Program Designed to Eliminate Contamination and Corrosion of Fuel Tanks on Aircraft Using Jet Turbine Fuel
650594 Flight Control for a Manned Orbital Space Station
670304 Flight Simulator Motion, Its Enhancement and Potential for Flight Crew Training
650205 Flight Simulator Utilization for System Design and Pilot Training
670312 Flight Training Can Take Lessons From Our Astronaut Training Program
670260 Flutter Characteristics of the Slab Tail in Business Aircraft
650387 Flutter Problems of Business Airplanes
670261 Flying Qualities Research Using a Variable Stability Airplane as An In-Flight Simulator
670326 Fuel Control System of General Electric Ge4 Engine for the Boeing 2707 Supersonic Transport
650503 Fuel Pump for Mach 3 Plus Aircraft
650297 Fuel for the Supersonic Transport
650598 Functional Design of the Minuteman Flight Control System
650755 Future Aerospace Manufacturing Educational Requirements
670301 Future Potential and Requirements of Digital Computer Simulation for Flight and Space Trainers
650585 Future Sensing and Information Requirements and System Ideas That Apply to Flight Control
650159 Future of Allison 250 Small Aircraft Turbine Engine in Fixed-Wing Commercial Aircraft
650595 Gemini Flight Control System Performance During the Second Unmanned Flight
650803 Heat Transfer Unit Evaluates Performance of Jet Fuels for Supersonic Aircraft
650193 Helicopters and Propeller-Type Vtol Aircraft in the Light of Technologies
650839 Higher Propulsive Efficiency in Subsonic Aircraft
650350 Hot Gas Servocontrol System for Aerospace Applications
650368 How Reliability Was Attained in Grumman Gulfstream Airplane
650809 Human Factors Challenges in Manned Space Flight
650575 Hydrologic Redundant Systems for Overall Flight Control
650212 Impact of Flight Operating Techniques Upon Engine Maintenance Costs
650241 Inertial Navigation System and Equipment Designs for Commercial Aviation
670306 Influence of Piloted Flight Simulator Studies on the Design of Sst Instruments
650198 Inlet Flow Field Studies for the Supersonic Transport
650788 Joining Methods Being Used for Advanced Aircraft Structures
650386 Justification of Computer Use By a Small Aircraft Company
670320 Kansas City, Missouri, Airline Terminal Building Concept
650224 Landing Gear of the Lockheed Model L-2000 Supersonic Transport
650831 Lift Fan Propulsion Systems -- V/Stol Aircraft Control
650233 Light Armed Reconnaissance Aircraft Operational Concept
650044 Lunar Surface Vehicle Computer Evaluation Program
650017 Machining Methods Most Adaptable to Aerospace Materials
650222 Maintenance and Reliability Requirements for Future Generation Aircraft
650847 Maintenance of All-Weather Landing Systems in Airline Service
650374 Management Ideas on the Real Value of Business Aircraft
650835 Manufacture of Propellant Oxygen for the Support of Advanced Lunar Bases
670295 Medical-Human Factors Aspects of Jetliner Flight in Severe Turbulence
650760 Metal Deformation in Macrosonic Fields
650265 Method for Comparing and Selecting Propulsion Systems for V/Stol Aircraft
650384 Muffler Development for Light Aircraft and Technique of In-Flight Data Acquisition and Analysis
650250 Navy Angle of Attack System for Controlling Airplane Approach and Landing Speeds
670302 Need for State-Of-The-Art Advances in Aircraft Maintenance Training Equipment
670327 New Flight Instrumentation for Improving Approaches and Landings of Future Transport Aircraft
650223 Next Generation of Short Haul Aircraft
650215 Objective of United States Supersonic Transport Program Is to Provide Minimum Sonic Boom and Engine Noise Levels
650243 Operating Cost Objectives of V/Stol Aircraft for Commercial Airline Services
650245 Operating Expense Forecasting for Scheduled Airline Services
650214 Operating Procedures Associated With Noise Generated By Supersonic Transport
670325 Operating Techniques and Maintenance Considerations for Air Inlet Controls in Airline Service
650343 Operation and Maintenance Requirements for Supersonic Transport Hydraulic Systems
650251 Operational and Design Considerations of Swept Wing Transports in Turbulence
650371 Operator Looks At Business Aircraft Operating Costs
650383 Oxygen Usage in General Aviation
650379 Positive Displacement Supercharger and Its Place in Aircraft Pressurization
650389 Pressurization of Light Aircraft -- Values and Controls
650790 Problems of Transition From Aluminum to Exotic Materials in Aerospace Structures
650800 Procedures for Use in the Performance Prediction of Proposed Aircraft Designs
650827 Progress in Constant-Speed-Drive Generating Systems for Aircraft
650204 Proper Interior Arrangement Helps Attain Maximum Payload-Range-Economy Capability in Supersonic Transport
650199 Propulsion Systems Sizing Criteria for the Supersonic Transport
650203 Propulsive Wing Turbofan V/Stol
650780 Rapid Method for Diffusion Bonding Aerospace Structures Made From Refractory Metals of Despersion-Hardened Metals
650830 Reaction Control Systems for V/Stol Aircraft
670262 Recent Developments in Instrumentation and Fuel Systems for Turbocharged And/Or Pressurized Aircraft
650216 Recommended Practices for Use in the Measurement and Evaluation of Aircraft Neighborhood Noise Levels
650361 Redundant Damper Servoactuators for the F-111 Airplane
650099 Regeneration Gives Improved Mission Capability and Economy to Turbine Powered Aircraft
650100 Regenerators Enhance Patrol Aircraft Capability
670317 Reliability Development on the Ge4 Augmented Turbojet Engine for the Supersonic Transport
650194 Research and Development of the Stowed Rotor Concept for High-Speed V/Stol Aircraft
670311 Review of Current Policy in the United Kingdom for the Use of Flight Simulators in Flight Crew Training and Checking
650778 Roll Diffusion Bonding, Potential Application to Aerospace Structures
650229 Safety and Reliability in Commercial Transport Aircraft
650228 Safety and Reliability of General Aviation Aircraft Through Design
650242 Simulation Studies of the Supersonic Transport in the Air Traffic Control System
650321 Snap 50/Spur Power Conversion System Objectives, Current Status, and Lunar Applications
650784 Solution of the Airplane Minimum Time Problem By the Huygens Principle
650246 Some Technical Aspects of Advanced Subsonic Transport Aircraft
650328 Supersonic Transport Fluid Evaluation Program
650838 Surface Transportation Systems for Lunar Operations
670300 Survey of Flight Simulation Computation Methods
650834 Systematic Approach to Shelter Design for Lunar Exploration
650341 Technical Considerations in Designing a Hydraulic System for Supersonic Transport
650592 Technique for Lunar Landing Site Selection By Earth-Based Control
670269 Test Results of An All-Mechanical Flight Control System Utilizing a Cascade Toroidal Servo
650366 Testing Techniques Assist in Attaining Aircraft Reliability
650782 The Quick-Change Convertible Cargo-Passenger Aircraft Will Aid Air Freight Development in the Next Decade
650828 Three Arrangements of Secondary Power Systems for Supersonic Transports and Vtol Aircraft
650789 Titanium Alloys Are Selected as Basic Structural Material for the Supersonic Transport
650380 Turbocharging Aircraft Engine and Cabin
650823 Turbulent Boundary Layers and Jets of Turbine Engines and Rockets Cause Random Excitation of Aerospace Structures
650761 Ultrasonic Welding and Soldering Can Be Applied to a Wide Variety of Metal Combinatons
650147 Ultrasonics Is Being Used for Wire Drawing and Material Extrusion, Forming Sheet Metal, and Forging
650762 Ultrasonics as Applied to Metal Forming and Assembly Processes
670297 Urgent Need for Flight Simulators for Present and Future Aircraft
650115 Use of High-Temperature Hydrocarbon Fuels in Subsonic Flight Environment
650369 Use of Off-The-Shelf Aircraft to Meet Army Requirements
650807 V/Stol Transport Aircraft for Air Cargo Operations
670303 Visual Presentation for Flight Simulation - Where We Are - Where We Are Going
650087 Vj 101 Supersonic Vtol Is a High-Speed Research Aircraft
640423 A lightweight universal fuel control for aircraft turbine engines
640826 A new look at the aircraft noise problem
640096 A rational method for selecting business aircraft
640614 A review of progress in the areas of aeronautical and aerospace spares management
640232 A spacecraft for ion thrustor flight tests
640240 A spot of land~The place of V/STOL aircraft in inter- and intra-city transport
640209 Adaptation of Army engine inspection techniques by computer for aircraft applications
640789 Aerodynamics and flying qualities of jet V/STOL airplanes
640308 Aircraft corrosion
640197 Aircraft fire detection~The problem and the solution
640488 Aircraft for long range and long endurance missions
640611 Aircraft gas turbine engine trend analysis
640093 Aircraft maintenance programming
640607 Airline flight testing for reliability and maintainability
640525 American Airlines lower minimum program
640200 An airline approach to reliability
640236 An approach to the evaluation of propulsion systems in V/STOL aircraft
640436 An approach to the isolation and control of vibration in light business aircraft
640343 Analysis of propulsion systems for V/STOL aircraft
640389 Bendix flameout sensor for turbine engine aircraft
640539 Cargo density as it affects aircraft design
640438 Centerline thrust for twin engine aircraft
640157 Collins 3-D flight director system and peripheral command indicator~Status report
640430 Component development of a liquid metal coupled regenerator system for regenerator aircraft engines
640489 Consideration of the high bypass ratio tip turbine cruise fan for long range and long endurance aircraft
640020 Control and flight characteristics of commercial supersonic transport aircraft
640593 Control for maintainability in aerospace fluid power systems
640336 Corrosion balance between launch complex and flight vehicle in an underground silo
640316 Crash safety tests of two transport aircraft
640248 Data for fail-safe design of the supersonic transport pressure cabin
640109 Delivery of clean, dry, thermally stable jet fuel to supersonic aircraft by in-field catalytic filtration
640058 Design considerations for a supersonic transport
640295 Design for in-flight maintenance for manned space missions
640441 Determination of installed versus dynamometer horsepower for utility-type aircraft
640034 Experience with reinforced plastic primary aircraft structures
640338 Flexible wing, a nonstop, multiple address, aerial delivery system
640508 Flight testing the Boeing 727
640216 Fuels for the supersonic transport~A progress report
640009 General considerations in the design of combustion chambers for aircraft and industrial gas turbines
640072 Hawker Siddeley P.1127 V/STOL strike reconnaissance aircraft
640391 High efficiency can be achieved in small size transonic compressor rotors
640501 High-temperature cobalt-tungsten alloys for aerospace applications
640519 Hydraulic fluid performance standards for present and future commercial jet aircraft
640327 Hydraulic fluid temperature control on aircraft requiring long endurance at supersonic speeds
640152 Improved reliability in transport aircraft hydraulic systems
640296 In flight checkout of the LEM environmental control system
640605 Indispensable role of the field test program in the realization of manned aerospace system reliability
640346 Initial flight experience with lift fan propulsion
640214 Kerosene fuels for supersonic transport
640227 LEM flight control~A statement of the problem
640608 Man's reliability in the X-15 aerospace system
640606 Manufacturer's flight testing for reliability and maintainability
640224 Mechanical analysis for cylindrical fuel elements of a fast reactor for use in a lunar powerplant
640049 Mechanics of locomotion and lunar surface vehicle concepts
640344 Needed research and development on V/STOL powerplants for Navy aircraft
640059 New test procedures for aircraft piston engine oils
640095 Operating business aircraft as a tool of industry
640440 Operation and maintenance of the flat opposed reciprocating aircraft engine as related to service problems
640331 Operational experience with the Trident aircraft
640597 Operational safety practices~Polaris flight test
640094 Optimization of business aircraft maintenance philosophy~Fact or fancy
640818 Performance and flying qualities of the double-delta supersonic transport
640055 Performance requirements for supersonic transports
640521 Personnel seating research for Air Force aerospace vehicles
640495 Planning for the introduction of a new aircraft into an airline fleet
640036 Predicted behavior of lunar vehicles with metalastic wheels
640159 Predicting reliability of supersonic propulsion systems
640437 Pressurization systems for executive aircraft
640332 Progress of the 727 jet in airline service
640149 Recent developments in ultrasonic metalworking processes
640490 Requirements for long range~Long endurance aircraft
640553 Results of an airplane reliability program
640288 SST fuels~A major airline concern
640305 STOL capabilities of VTOL aircraft~Some operating parameters
640598 Safety engineering for piloted aircraft
640527 Scheduling the supersonic transport
640300 Some flight deck design considerations for supersonic transports
640301 Status report on the Boeing model 733~Supersonic transport
640215 Super fuels for supersonic transports~An airline viewpoint
640107 Systems safety concepts for high-performance business aircraft
640633 Technical development status of the project Apollo lunar excursion module
640429 Test of a Regenerative Turboprop Aircraft Engine
640805 The Aircraft Regenerative Turbine Engine-Where Now
640074 The Army XV-5A lift fan flight research airplane
640831 The assessment of supersonic transport operating costs
640235 The effect of propulsion system parameters on vertical take-off and landing performance of a transport aircraft
640640 The lunar prospect
640630 The manned lunar landing mission
640801 The role of numerical control in machining of aerospace materials
640005 The theory, practice, and economics of ultrasonic cleaning of small mechanical subassemblies
640341 The value of limited random vibration flight data
640444 V/STOL aircraft trade-offs
640249 Variable sweep~Application to the supersonic transport
640439 What can be gained with additive oils in utility aircraft engines
640510 X-ray~A necessary tool for detecting incipient structural failures in service aircraft
630240 A linear approach in sonic fatigue analysis and calculations
630207 A new look at supersonic aircraft hydraulic requirements
630574 Advanced maintainability techniques for aircraft systems
630408 Air pumping system for a laminar flow control aircraft
630220 Air traffic control problems associated with aircraft carrier operations
630268 Aircraft arresting systems for military and commercial aviation
630395 Aircraft economies~Fact or fiction
630409 Airline management of overhaul processes with critical path methods
630401 Airplane design for reliability
630039 Altitude performance with turbosupercharged light aircraft engines
630274 An international airline looks at the supersonic transport
630371 An investigation of structural concepts for a mach 3+ supersonic transport wing
630577 Application of reliability models to the choice of a booster for lunar missions
630369 Application of self-adaptive control techniques to the flexible supersonic transport
630036 Applications and engineering problems of VTOL-STOL military aircraft
630260 Breakerless high frequency ignition systems for reciprocating aircraft engines
630078 Characterization of lunar surfaces and concepts of manned lunar roving vehicles
630592 Commercial supersonic propulsion~Maintainability by design
630074 Considerations of lift engine installations in VTOL aircraft from the viewpoint of the airframe designer
630224 Design considerations for the supersonic transport electric power system
630398 Development of a high temperature (1500 F) nuclear radiation resistant pneumatic power system for flight vehicles
630250 Electron beam welding of large aerospace structures with portable vacuum chambers
630452 Electron beam welding techniques as applied to aerospace structures
630269 Equipment and procedures utilized in rearming naval and marine aircraft
630492 Evaluation and test of a liquid metal coupled regenerator system for aircraft turboshaft engines
630247 Evaluation of dynamic response characteristics of a supersonic transport landing gear system
630222 Expandable balloon-type drag devices for mach 10 flight regime
630202 Ground support equipment for aircraft carriers
630246 Heat intercept cooling system for the supersonic transport
630089 Human performance in the environment of a lunar vehicle
630370 In-flight applied rain repellents for aircraft windshields
630066 Industrial application of the Pratt and Whitney Aircraft J-57
630079 Instrumentation and payload design for lunar roving vehicles
630566 Logistic support requirements for commercial airline oeprations
630001 Lunar surface characteristics
630456 Meteorology of the supersonic transport at cruise altitude
630520 Method of allocating reliability goals to aircraft subsystems and components
630571 Minuteman flight control system~The approach to and the results of a formal reliability program
630265 Observations of flight safety
630244 Performance safety requirements for civil supersonic transports
630223 Pneumatics for supersonic transport
630081 Powerplant System for V/Stol Aircraft
630267 Precise electrical power requirements for support of naval aircraft
630342 Preparation for lunar environment with a means of varying gravitational environment
630263 Recent French experience in the field of V/STOL aircraft
630264 Requirements for the flight control system of a supersonic transport
630239 Research on techniques of establishing random type fatigue curves for broad band sonic loading
630469 Retreading and repairing of high performance aircraft tires
630377 Simulation approach to development of the XV-5A Lift-fan V/STOL aircraft
630272 Some radiation problems in the supersonic environment
630422 Sonic Boom Problems and Noise From High Performance Propulsion Systems
630273 Sonic boom and community relations
630407 Survey of candidate aluminum materials for supersonic aircraft applications
630037 The Army VTOL surveillance aircraft program
630276 The aircraft carrier as a strike warfare system
630483 The application of ultrasonic energy to metal processing
630396 The cost of landing an airplane
630090 The delivery system and performance requirements for a lunar roving vehicle
630441 The design and development of a prototype landing gear system for aircraft to be operated from rough unprepared fields
630243 The effects of supersonic transport flight characteristics on performance requirements
630266 The materials used in aerospace applications for plastics
630567 Trend analysis as applied to gas-turbine engines and aircraft mechanical equipment
620445 A new maintenance tool for aircraft
620539 A terminal control landing system~Theory, system integration concepts, and flight test results
620458 Advanced design features in Canada's supersonic wind tunnel
620492 Aerodynamic control of deceleration and range for the lunar mission
620296 Aeroelastic characteristics for a jet-flap helicopter rotor in forward flight
620446 Aircraft communications electronic signaling system
620373 Aircraft instrumentation and display system~Adaptation of tactile link
620058 Airline experience~Jet aircraft tires
620481 All mechanical primary flight control system for VTOL/STOL aircraft
620026 Arresting large jet transport aircraft
620597 Aviation gas turbine controls introduction
620436 Canadair 44 mechanized loading system in operation with Seaboard World Airlines
620356 Commercial jets~Hydraulic system contamination versus airline maintenance
620034 Commercial supersonic transport development
620552 Considerations in selection of wing and fuselage sheet materials for trisonic transports
620468 Design and operation of V/STOL commercial aircraft
620482 Design and test experience with high-speed mechanical drive systems for helicopter and VTOL aircraft
620327 Development of the variable geometry inlet for the B-58 airplane
620342 Direct sink environmental systems for supersonic transports
620523 Distortion control during heat treatment of aircraft and missile components
620325 Dynamometer evaluation of aircraft wheel microinspection techniques
620474 Economic and safety aspects of short haul V/STOL aircraft on high density routes
620344 Effective application of supersonic transports to airline operations
620357 Effects of fuel contamination on corrosion of aircraft fuel systems
620305 Electrostatic discharges in aircraft fuel systems
620308 Extensions of the lift/thrust engine principle in V/STOL aircraft
620343 Flight control system design for supersonic transport
620295 GEMs~Aircraft, seacraft, or groundcraft
620057 Gas turbines and the business aircraft
620341 High temperature electrical system development applicable to supersonic transports
620485 High-voltage electron beam welding of aerospace components
620104 Immersed ultrasonic testing and recording
620301 Importance of air induction system design to supersonic aircraft
620300 Inlet duct~Engine airflow match and compatibility for supersonic aircraft
620331 Insulation~Radiation temperature control of inflatable hypersonic vehicles
620486 Nuclear auxiliary power unit for lunar exploration
620477 Optical tooling as applied to aircraft/missile fixtures and machine alignment
620312 Preparation of a guide for customer flight crew transition training by airframe manufacturers
620379 Programmed reliability in design for a V/STOL airplane
620313 Proposed standard index and format for manuals covering civil aircraft ground support equipment
620302 Propulsion systems for supersonic transports
620338 Recuperators for long duration aircraft engines
620336 Rigidizable expandable aerospace structures
620448 Safety, reliability and economic considerations for supersonic transports
620059 Satisfying the jet age challenge in aircraft tires
620456 Setting the structural design criteria for space debris effects in cislunar and outer space travel
620515 Some effects of runway slush and water on the operation of airplanes, with particular reference to jet transports
620491 Structural dynamics aspects of the manned lunar space vehicle launch phase
620449 Supersonic transports~Life in the heat thicket
620463 System simplification tools~An airline engineer's view of SST reliability
620489 Terminal weather problems of supersonic transport
620345 Test and training central for antisubmarine warfare patrol aircraft
620155 The development of aircraft crash-resistant fuel cells, safety valves, and breakaway accessories
620346 The role of a prototype in the development of an ASW airplane
620350 The role of new development in fluid power control for aerospace systems
620530 The supersonic transport~Required characteristics of configurations
620054 The trend to turbines in business aircraft
620074 Ultrasonic metal joining and machining
620103 Ultrasonic pickling and cleaning
610342 A consideration of powerplants for supersonic transport aircraft
610118 A parametric study of the take-off performance of Getol aircraft
610444 A transportation system to establish a manned lunar outpost
610005 Applications of Army-Navy instrumentation program to transport aircraft
610079 Applications of a nuclear vehicle for a manned lunar landing
610355 Contributions of dyna-soar to space flight technology
610437 Cooling for hypersonic aircraft structures
610097 Effect of inlet normal shock position control systems on range of supersonic transports
610165 Forecasts for flight vehicle power
610101 Heat transfer and insulation considerations for an external expansion ramjet with specific application to Mach 7 flight
610443 Human factors of the lunar logistics mission
610367 Industrial power requirements and the aircraft gas turbine engine
610370 Integration of gust alleviators in flight control systems
610314 Jet fuel anti-icing additives~A new concept in safety of flight
610323 Lift-thrust turbofan engines for VTOL and STOL aircraft
610478 Lunar exploration systems
610016 Mach 3 wing structures stiffened skin versus sandwich
610169 Mechanical, sonic, ultrasonic, and radiation studies of polymer-thickened oil shear characteristics
610341 Passenger density and accommodations as factors in supersonic transport design
610197 Payload-density-mechanization as applied to all-cargo aircraft
610351 Productioneering in the aerospace age planning~The fundamental technique
610315 Radiation fuel gage applications to transport aircraft
610085 Reacting flight loads at forging temperatures
610378 Selected methods for atmosphere control in manned space flights
610372 Significant environmental differences between powerplants for aerospace and underwater missiles
610104 Some aspects of supersonic transport propulsion
610379 Sonic proof testing B-58 weapons system
610251 Special aspects of structural design for safety of light aircraft
610099 Spontaneous ignition and supersonic flight
610498 Supersonic jet fuels~Quality and cost factors
610096 Supersonic trim drag
610311 The Air Force B-70 Valkyrie~An example of next generation aerospace vehicles
610100 The Breguet family of STOL aircraft
610157 The combined transonic axial and centrifugal stage compressor
610339 The commercial supersonic transport~Some operational considerations
610482 The cost of lunar travel
610183 The development of steep gradient aircraft for short-haul transportation
610088 The exploitation of the maximum capabilities of the human body to withstand maneuvering loads in manned aerospace vehicle design
610344 The implications of producing aerospace weapons at planned low rates
610098 The operator's viewpoint on the supersonic transport
610076 The performance of a hypersonic ramjet using detonative combustion
610340 The supersonic transport~Pilot views on operational goals, handling characteristics, and related subjects
610095 The world-wide search and retrieval problem~Factors involved in the selection of a rescue/retrieval aircraft
610439 Thermal radiation considerations for advanced flight vehicles
610158 Transonic flow problems in centrifugal compressors
610250 Trends in light aircraft structural design
610358 Turbine powered transport aircraft in the USSR
610010 U.S. lunar travel program
610178 VTOL Aircraft
600264 A high energy absorption landing gear for VTOL aircraft
600286 A new design approach for supersonic transports
600345 A small company uses airplanes
600272 Adaptive control considerations for re-entry flight
600186 Aeroflot~Soviet civil aviation
600427 An evaluation of the relationship between reliability, overhaul periodicity, and economics in the case of aircraft engines
600298 Applications and limitations of metal removal techniques in aircraft and missile manufacturing
600290 Choice of engine type for nuclear powered multi-purpose aircraft
600382 Community psychoacoustics~Key to aircraft noise design and operation
600418 Correction and statistical analysis of missile flight vibration data
600381 Development of in-flight modulating type thrust reverser for single engine aircraft
600260 Discussion of some design problems associated with artificial feel systems of airplanes with irreversible powered flight controls
600384 Economics of the supersonic transport
600369 Electronic computer for optimum flight plan determination
600378 Flight characteristics of the DC-8
600280 Flight reliability in nuclear aircraft
600379 Flight testing the Convair 880
600346 General aviation during the soaring sixties
600395 Loctracs~An all aircraft surveillance system
600385 Low cost cargo aircraft~Turboprop or turbofan
600284 Minimum flyable handling qualities of airplanes
600045 Preliminary design considerations for the structure of a trisonic transport
600417 Processing missile flight vibration data
600064 Radiation effects studies for the development of radiation-resistant aircraft subsystems
600058 Refractory nonmetals for use in hypersonic aircraft
600373 Review of aircraft instrument problems
600311 Scheduling and dispatching of airline aircraft
600287 Shock wave noise of supersonic aircraft
600291 Some practical methods for fabricating shields for nuclear-powered aircraft
600383 Sound suppressor and jet reverser effects on aircraft performance
600288 Supersonic air transports~An airline talks back
600077 Surge characteristics of aircraft underwing fueling~A by-product of pressure fueling
600282 The Canadair 44~A breakthrough cargo aircraft
600363 The X-15~A reaction control aircraft
600371 The penalties of non-optimum flight operations of jet aircraft
600279 The potential of nuclear-powered aircraft for commercial cargo transport
600226 Towing tractors for heavy jet aircraft
600265 Trends in VTOL aircraft propulsion system requirements
600051 Turbine fuel thermal stability CFR coker and flight evaluations
590289 A propulsion spectrum for VTOL aircraft
590301 A systems approach to the support of jet aircraft
590274 Aircraft Accident Investigation Techniques
590270 Airline ground equipment~Functional requirements and design
590155 Can we define aircraft turbine fuel cleanliness requirements
590248 Comparative cost and effectiveness of manned aircraft and guided missiles in air defense
590254 Considerations in the application of evaporative cooling systems to hypersonic vehicles
590406 Design of aircraft for commercial use
590069 Design problems of very high speed flight
590061 Development of the suppressor and thrust brake for the DC-8 airplane
590297 Doppler-inertial navigation for high performance aircraft
590230 Electrical ground power for commercial jet aircraft
590351 Elevated temperature testing of flight vehicle materials
590295 Ground support and handling of jet aircraft
590153 Handling the commercial jet airplane on the ground
590253 High performance hydrocarbon fuels for supersonic propulsion
590360 Increased reliability of aviation and missile electronics by use of damped structures
590380 Needle bearings for present and future aircraft
590012 Possibilities and problems of some high energy fuels for aircraft
590294 Prediction of aircraft wing gust fatigue damage by means of power spectral analysis and constant life curves
590233 Present status and future potential of VTOL aircraft
590252 Pyrophorics for Aircraft Propulsion-Their Promise and Problems
590268 Radiation shielding aspects of nuclear aircraft
590047 Selection of Optimum Modes of Control for Aircraft Engines
590261 Some views on aircraft nuclear propulsion
590207 Space trajectories and flight test objectives
590052 Status of the SAE S-12 approach to vibration isolation of aircraft electronic equipment
590177 The Aerodyne~A new concept of flight
590337 The Bishop's boys~Human engineering for the first flight
590050 The Buick Flight Pitch Dynaflow
590349 The JT12 Pratt and Whitney Aircraft's 3000 lb. thrust turbojet engine
590290 The effect of vertical flight on powerplant design
590226 The future of airline ground transportation
590382 Ultra high speed aircraft and missile ball bearing applications
590040 Wings and vertical thrust generators in VTOL aircraft
580162 A collision avoidance system for aircraft
580066 Adaptation of constant speed drives to long range manned aircraft of the immediate future
580152 Aero-thermodynamic aspects of high speed flight
580285 Aircraft pneumatic systems
580179 Basic fuel injection for business aircraft
580045 Behavior of aircraft structures under thermal stress
580068 Constant speed drives for high mach aircraft
580375 Convair's new trisonic wind tunnel
580370 Design of commercial jet aircraft for specific routes
580041 Designing with steel for lighter aircraft
580169 Developments in aircraft turbine lubricants
580076 Developments in the field of direct-air-cycle aircraft nuclear propulsion systems
580270 Environmental factors affecting bearings for aircraft motor applications
580070 Jet engine control and attitude control in vertical attitude VTOL aircraft
580365 Lockheed arc-heated hypersonic tunnel
580362 Low level escape in naval aircraft
580231 Management's role in meeting the future of the aircraft industry
580280 Mechanical Factors Involved in Bearing Design for Aircraft Electric Motors
580120 New fuels for piston-engine aircraft
580077 Nuclear powered aircraft
580140 Performance and control of variable geometry aircraft inlets
580153 Physiologic effects of high speed, high altitude flight
580263 Potential application of niobium to aviation gas turbines
580163 Powerplants for supersonic transports
580176 Primary creep in aircraft design
580016 Problems in the application of high-strength steel alloys in the design of supersonic aircraft
580170 Relation of fuels to aircraft turbine engines
580289 Self-contained turbomachine systems for aircraft and vehicular air conditioning
580136 Some of the needs of modern general aircraft and some of the possible answers
580190 Techniques involved in aircraft accident investigation
580072 The X-14 VTOL airplane~A design tool
580146 The application of operations research and computer techniques to airline operations
580165 The future of aircraft fuels
580147 The integration of navigational flight information for jet interceptor aircraft
580075 The radiation effects testing of aircraft systems
580069 The turbonator~An integrated air turbine generator for high mach aircraft
580257 Two methods of aircraft skid control
580221 Use of adhesives in the aircraft industry
570161 A digital system for collecting and processing flight test data
570233 A discussion of some recent developments in aircraft engine oil filtration
570158 A progress report on the development of landing gear for use by STOL aircraft operating from rough unprepared fields
570160 An application of a digital computer to aircraft route analyses
570112 An integrated aircraft air conditioning system for transport aircraft
570002 Application of ultrasonic inspection to detection of seams in steel products
570020 Compressor stall problems in gas-turbine-type aircraft engines
570219 Concept, design, and manufacture of supersonic aircraft
570232 Contaminants and their effects on aircraft engines
570017 Convertiplanes and other VTOL aircraft
570165 Correlation of airfoil ice formations and their aerodynamic effects with impingement and flight conditions
570218 Cruise control instrumentation for turbojet aircraft
570159 Describing the aircraft as a vibration source
570200 Developments in aircraft turbine lubricants
570065 Discussion~Grades of commercial aviation fuels
570256 Flight testing and flying techniques of high altitude supersonic aircraft
570171 Fuel system testing of high performance aircraft
570163 High speed aircraft design for good spin characteristics
570208 Human factors in the design of high performance aircraft
570255 Integration of the F-100 airplane into Air Force squadron service
570124 Latest developments in VTOL aircraft
570191 Molybdenum for aircraft applications
570195 Overrun safety arrestment of commercial jet aircraft
570190 Potential advancements in the field of small aircraft engines
570213 Pre-flight development of modern aircraft
570008 Preignition in aircraft reciprocating engines
570018 Some general considerations concerning VTOL aircraft
570152 Systems analysis approach to firebee flight control systems development
570146 The application of nuclear power to logistic aircraft systems
570263 The development of business transport aircraft
570206 The ramjet-turbojet propulsion system for supersonic flight
570156 The role of high strength weldments in aircraft structure
570357 The tilt-wing VTOL aircraft as a commercial air transport
570204 Thrust reversers for jet aircraft
570214 Trends in modern aircraft structural design
570199 Turbine-powered aircraft demand new fuel handling techniques
570009 Weld repair of aircraft quality magnesium castings
570063 What fuel characteristics mean to the turbine engine airplane
570108 What of the (aircraft) future
570174 X-ray inspection techniques in airline operation
560191 Accelerated service testing of turbo-prop engines in USAF test bed aircraft
560086 Air-conditioning and pressurization equipment requirements for high performance flight
560278 An appraisal of VTOL aircraft
560188 Anti-friction bearing materials for aircraft powerplants
560035 Application of high-temperature materials to aircraft powerplants in the temperature range 1200-2400 F
560002 Application of metallic materials for aircraft structures in the temperature range 600 to 1100 F
560282 Development of a cabin pressure control system for transport type aircraft
560171 Dynamic seals for aircraft gas turbine engines
560092 Electric equipment problems in supersonic vehicles
560270 Engine inlet air diffuser controls for supersonic aircraft
560050 Flight research at high altitudes and high speeds with rocket-propelled research airplanes
560163 Forgings and modern fighter airplane producibility
560090 Fuel balance system for supersonic airplanes
560293 General fuel requirements for the commercial aircraft gas turbine engine
560005 High-temperature problems associated with the use of rubber in aircraft
560285 Human factors that cause aircraft accidents
560089 Hydraulic and pneumatic problems in high performance aircraft
560096 Integrated control systems for aircraft
560281 Integrated flight systems
560085 New tools to lick aircraft equipment noise problems
560008 Pneumatic and sonic measurement of combustion-chamber volume
560266 Pneumatic versus mechanical power extraction for aircraft accessories
560091 Propellers for High Speed Aircraft
560127 Radiographic inspection in aircraft structure
560196 Radiography of aircraft structure for safety and economy
560046 Some elevated temperature structural problems of high-speed aircraft
560075 Supersonic air inlet controls
560276 Supersonic bomber propulsion problems
560158 The economics of large aircraft
560103 The effect of high frequency impact loads on airplane landing gears
560097 The synthesis of aircraft hydraulic servos
560087 The transport airplane from the pilot's viewpoint
560012 Wing-lift augmentation methods for the improvement of low-speed performance of high-speed aircraft
550186 A propeller synchrophaser for aircraft noise control
550243 AbcS of Ultrasonic Inspection
550178 Air transport design for the human element of airline service and maintenance personnel
550253 Aircraft noise problem in airport vicinities
550077 Aircraft powerplants~Present and future
550297 An airframe manufacturer's viewpoint on civil aircraft turbine fuel
550300 An airline's viewpoint of the status of the turbine era
550255 An airplane manufacturer's progress with noise suppression devices
550299 An oil company's viewpoint on civil aircraft turbine fuels
550247 Application of airborne radar to airline operations
550181 Auxiliary power and air conditioning for the self-contained airplane
550250 Basic facts about noise as related to aviation
550014 Bearings and lubricants for aircraft turbine engines
550302 Economic Considerations of a Jet Transport Airplane
550273 Effects of operational factors on structural fatigue in fighter aircraft
550188 Environmental control on a supersonic bomber
550064 Evaluation of the noise field around jet-powered aircraft
550268 Flight load measurements and analysis
550066 Human engineering aspects of aviation noise control
550168 Integration of aircraft instrumentation
550321 Introductory talk on environmental testing of aircraft and missiles
550083 Marine Corps assault aircraft transports
550239 Napier Nomad aircraft diesel engine
550303 Planning for the best airplanes
550076 Safety considerations in aircraft design
550074 Small turbojet engines~A big factor in aviation
550189 Stability and control of piloted aircraft at high altitudes
550223 Structural design and static testing of utility aircraft
550179 Supersonic rain erosion testing techniques (unclassified)
550075 The Allison T56 Turbo-Prop Aircraft Engine
550024 The aircraft industry in Canada
550019 The convertible aircraft art
550190 The design and development of high-pressure high-temperature pneumatic ducting systems for aircraft
550177 The influence of propeller synchrophasing on aircraft cabin noise
550048 The next twenty-five years in the aviation industry
550137 The role of testing in modern military aircraft design
550078 Turbojet engines for pilotless aircraft~Present and future
550193 Turboprop airplane control problems associated with engine failure considerations
550084 USAF experience to date with turbo-prop aircraft
550251 Why do airplanes make noise
540140 A comparison of experimental and analytical flutter characteristics for a swept wing jet bomber
540200 A general production system for production of aircraft
540236 A new concept of explosion testing of aircraft equipment
540155 A plan of attack on aircraft fatigue
540077 A realistic approach to the testing of aircraft air conditioning equipment
540199 A systematic series of engines for utility aircraft
540163 Aircraft environment and airborne electronic equipment packaging
540079 Airline requirements of air conditioning a jet transport
540231 Airplane configurations for high-speed flight
540158 Capabilities and operating costs of possible future transport airplanes
540284 Ceramic and metal coatings for high temperature aircraft materials
540148 Clear design thinking using the aircraft growth factor
540166 Design of light-weight, high-performance military aircraft
540154 Experience with synthetic lubricants in aircraft power plants
540141 Factors affecting the design of thin wings
540144 Fragility rating for aircraft equipment~Potential aid to package cushion design
540105 Helicopter flight experience with the Continental XT-51 fixed shaft turbine
540085 Inlet protection for aircraft gas turbine engines
540024 Light aircraft turbo-propeller installations
540080 OSP and the revival of the French aircraft industry
540160 Problems of high speed flight
540196 Propeller design for high performance utility aircraft
540197 Radio communication and navigation equipment for utility aircraft
540084 Retractable air inlet screens for aircraft gas turbines
540151 Selection of aircraft construction materials
540027 Simulated altitude tests of large aircraft engine exhaust systems
540153 Small turbojet for trainer aircraft
540212 Suppression of explosion and fire in aircraft
540277 The aerodynamic and power plant heating problem in high speed aircraft
540198 The growing importance of the businessman's aircraft
540015 The modern executive airplane as a medium of transportation
540278 Thermal limitations of common aircraft materials
540025 Tooling and planning problems related to modern transport aircraft
540146 Turbo prop installation in large water based aircraft
540253 Turbojet-engine design problems for supersonic flight
540162 Unsymmetrical flight loads problems in supersonic aircraft
530020 A designer's view of combat aircraft reliability
530145 A rationalised fuel reserve policy for medium range airline operations
530177 Aircraft gas turbines
530071 Aircraft instrument integral lighting
530013 Aircraft turbine engine synthetic lubricants and their lubricating properties
530264 Aviation fuel economy and quality~Brothers under the aircraft skin
530214 Can the airlines use the helicopter
530148 Cold weather operation of aircraft
530163 Cooling electric equipment during supersonic flight
530158 Delta wing design analysis
530079 Design and development of aircraft hydraulic components for increased reliability
530153 Design considerations for maneuverability of high speed airplanes
530274 Design considerations in the use of ultra high strength alloy steels in aircraft
530087 Design for increased reliability of aircraft hydraulic systems
530080 Designing hydraulic systems to increase dependability of tomorrow's airplanes
530028 Effect of engine weight, drag, and fuel consumption on direct operating cost of a commercial airplane
530077 Factors Influencing Airplane Costs
530162 Flight test instrumentation statues
530078 High-temperature problems associated with aircraft hydraulic systems
530258 Instrumentation for aircraft gas turbine development
530157 Landing gear design as applied to modern aircraft
530159 Pressurizing and air conditioning a fighter airplane~Design problems and compromises
530010 Protective design in forward and rearward facing seats in transport aircraft
530174 Shot peening applications and techniques in the aircraft industry
530074 Simulated flight for engines at AEDC
530147 Small turbines~The heart of modern aircraft accessory power systems
530144 Some trends in gust loads for transport airplane operations
530150 Tanker aircraft refueling systems
530001 The Story of the First 50 Years of Aircraft Engines
530114 The aircraft economic parameter and its use in the comparative evaluation of all-cargo type aircraft
530100 The airplane and the Arctic pack
530151 The armed services-industry cooperative study of aircraft fuel rating methods
530165 The creation of an aviation engine industry in Canada
530006 The dawn of aviation's new era
530149 The effect of temperature on aircraft structural design
530266 Titanium alloys for aircraft engine forgings
530223 Today's aluminum aircraft alloys
530175 Turbo-props versus turbo-jets~An airline view
530096 What happens to the dissolved water in aviation fuels
520087 A system of reducing flight test data to standard conditions applicable to all subsonic speeds and large angles of climb and glide also simplified position error functions
520016 Accident survival~Airplane and passenger car
520201 Aircraft cost reduction
520051 An engineering comparison using straight, swept, and delta wings
520269 Application of titanium to aircraft engines
520018 Aviation spark plug fouling~Its cause and control
520123 Chan-o-seal for modern aircraft
520206 Characteristics and limitations of expansion turbines for auxiliary power purposes in turbine-propelled aircraft
520238 Characteristics of propellers for turboprop airplanes
520038 Current plastics materials and their application to aircraft
520117 Drop testing a large airplane
520079 Economics of new aircraft selection
520073 Facilities and equipment for testing high speed aircraft
520110 Flight Testing of Prototype Engines as Primary Power Plants in New Airplanes
520232 Flight experience with Vickers Viscount turbopropeller airliner
520076 Flight test and facilities for naval aircraft
520078 Government collaboration in aircraft development
520146 Helicopter airlines operation in New England
520053 High pressure pneumatics in a modern fighter aircraft
520118 High-speed water-based aircraft
520019 Hydraulic drives for aircraft
520074 Improved passenger comfort through the application of airline experience to air conditioning system design
520077 Introduction of new transport aircraft
520224 Low-temperature lubrication of aircraft engines
520148 Lowering the ignorance factors in airplane wheel and brake development
520200 New design requirement learned from Korean war aircraft
520152 New transparent plastics for aircraft enclosures
520112 Operational experiences with flying test bed airplanes
520040 Plastic tooling in aircraft manufacture
520161 Precipitation hardening steels show advantages in aircraft
520113 Radome optical system problems on supersonic aircraft
520229 Some developments for greater crash safety in aircraft
520088 Static-discharge protection for transport aircraft part I~Protection from discharges to aircraft antennae
520055 Statistical aspects of airline reservations
520149 The case for turbines in small aircraft
520196 The development of rust preventive lubricating oils for reciprocating aircraft engines
520080 The impact of turbines on airlines
520048 The importance of Europe in the cooperation of the Atlantic countries with respect to aviation
520164 Timing and phasing of flight testing in the development of engines
520162 Use of high tensile steels in aircraft
510166 Aircraft ground handling characteristics as required for maximum efficiency
510128 Aircraft maintenance in Korea
510153 Airline experience with aircraft engine lubricating oils
510094 An introduction to the aircraft turbo-jet engine
510074 Applications of ceramic coatings in aircraft engines
510075 Can man survive prolonged flights above 50,000 feet
510193 Comparison of some turboprop cycles for subsonic speeds
510154 First use of turbosuperchargers in commercial aviation
510150 Flight characteristics of the Boeing B-47 stratojet
510170 Flight experience with turbine propeller powered aircraft
510152 Flight research experience with higher engine oil temperatures
510073 Future trends in aviation
510131 General design aspects of turbo-prop and turbo-jet aircraft fuel systems
510004 German aircraft manufacturing methods
510146 Government responsibililty in aviation safety
510136 High-speed pressure refueling of aircraft
510167 Local service aircraft and engines maintenance requirements
510026 Observations on flight safety
510151 Operational experiences with multi-engine jet aircraft
510183 Research and development to promote safety in aviation
510002 The development of the aircraft gas turbine in Great Britain and its influence on petroleum requirements
510085 The evolution of civil aviation
510163 Wanted~A new airplane
510027 Working for air defense~A warning against making Germany's mistakes on wartime aircraft production
500140 A concrete phase in the development of the load detachability principle in aircraft
500071 A review of a year's operation of the Curtiss-Wright Dehmel flight simulator
500016 Airplane spray and dust application
500148 Airplane wheels and brakes
500176 Auxiliary gas turbines for pneumatic power in aircraft applications
500167 Compound engine systems for aircraft
500019 Driving aircraft accessories remotely from the aircraft engine
500009 Fatigue life of aircraft engine mounting components
500060 Flight characteristics at high mach numbers
500151 Fuel and lubricant requirements of personal plane aircraft engines
500079 Fundamentals of airlines scheduling and flight equipment routing after 1955
500020 Ground and flight evaluation of the performance of jet powerplant installations and some installation factors affecting output
500080 Ground operational problems with jet powered aircraft
500195 High-altitude aircraft oil systems
500127 Industrial mobilization planning with the aircraft industry
500057 Influences of high speed flight on turbo jet engines
500072 Investigation of reversing propeller pitch on a multi-engine aircraft in- flight
500153 Light aircraft engine tests~Fuels and operating variables
500013 Needed~A new agricultural airplane
500077 Passenger markets for future airplanes
500152 Recommendations for fuel system design for personal aircraft with regard to vapor lock
500026 Some developments for safer aircraft
500058 Some high speed experience with fighter type airplanes
500059 Some notes on high speed flight problems
500040 Supersonic and transonic aircraft problems
500161 The development of assault transport and troop carrier aircraft
490230 A completely nonflammable aircraft hydraulic fluid
490070 A method of evaluating power plants for use in subsonic transport airplanes
490204 Aerodynamics of high-speed airplanes
490115 Aircraft decelostat~A device for wheel slide protection
490067 Aircraft evacuation on land~Equipment, stowage, and procedure
490173 Atomic power and aircraft propulsion
490182 Design charts for longitudinally stiffened wing compression panels
490212 Design of aircraft structures for "mass production"
490206 Dynamic loads on airplane structures
490069 Flight testing the Wright typhoon turbo-prop
490071 Fuel systems and carburetors for personal aircraft
490161 Heating, ventilating, pressurizing and air conditioning of civil transport aircraft
490164 Hydraulic equipment on modern aircraft
490168 Improved utilization of fuels and lubricants in transport airplanes
490017 Interior treatment of aircraft
490232 Lubrication, friction and wear studies with high-output aircraft engines
490028 Must airlines lose money
490023 Personal aircraft~Problems and progress
490222 Problems of aircraft life evaluation
490019 Refuelling in flight
490072 Review of transport aircraft developments during the past two years and some predictions for the future
490123 Rocket and ramjet supersonic powerplants
490117 Sand and dust erosion in aircraft gas turbines
490172 The airlines' viewpoint
490169 The airplane as a whole
490020 The design of airplane interiors
490179 Traffic control requirements for jet transport aircraft
480142 A method of evaluating aircraft engine oils by piston ring sticking tests
480169 An approach to the analytical design of aircraft
480204 Calculation of heat required for wing thermal ice prevention in specified icing conditions
480001 Development of aircraft windshields to resist impact with birds in flight part II~Investigation of windshield materials and methods of windshield mounting
480195 Engine installation problems in the XP-84 airplane
480100 Engineering developments required for satisfactory low temperature aircraft engine operations
480049 Factors affecting the selection of propellants for rocket powered aircraft
480222 Flight beyond the earth's atmosphere
480189 Fuel injection versus carburetion for personal airplane engines
480226 Full-scale engine performance characteristics of aviation safety-type fuels
480179 Instrumentation for development of aircraft powerplant components involving fluid flow
480230 Jet aircraft cabin temperature control
480103 Light aircraft vapor-lock problems
480038 Lightning effects on aircraft
480166 Long-range overseas transport plane of 1955~What will be the possible changes in the civil air regulations which will influence this aircraft
480181 Longitudinal control system for high-speed aircraft
480029 Practical aspects of reverse thrust propellers in airline operation
480221 Preignition and its deleterious effects in aircraft engines
480191 Research on aircraft hydraulic packings
480047 Simplicity as a goal in the design of aircraft systems
480183 Some factors influencing operating cost analyses of transport aircraft
480130 Structural aspects of high speed airplanes
480106 The "sleeperette"'~A new concept of comfort for airline passengers
480048 The design and development of rocket engine powerplants for aircraft
480228 The ramjet as a supersonic propulsion plant
470233 Aircraft detonation indicators
470030 Aircraft engine starters
470112 Aircraft power plant problems
470218 Aircraft-engine starting tests and experiences in the Arctic
470058 American Airlines' evaluation of airborne radar
470145 An analysis of composite-powered aircraft
470137 Cargo aircraft requirements
470141 Civil Aeronautics Administration aircraft fire prevention developments
470039 Cold weather operation of aircraft power plants by the U.S. Navy
470150 Comparison of use of mixed structural materials and fabric covering to all-metal construction for personal aircraft from a manufacturing viewpoint
470222 Cost aspects of airline policies and procedures
470016 Design trends in turbo-jet and turbo-prop aircraft engines
470048 Development of aircraft windshields to resist impact with birds in flight~Part I
470159 Development of functional cockpits for naval aircraft
470253 Effect of C.A.R. performance requirements on airplane design
470168 Electrical power and the transport airplane
470153 Engines for light aircraft
470117 Evaluation of light aircraft engine lubricants
470229 Experiences of an aircraft manufacturer with sandwich material
470189 Fuel injection for light aircraft
470099 Future power for the personal airplane
470240 Future trends in aircraft-engine design
470155 Hermetically sealing aircraft instruments and control components
470156 Installation engineering of aircraft turbo-jet engines
470216 Light aircraft service experience with all-purpose fuel
470214 Mutual adaptation of aircraft fuels and engines
470054 Power plant requirements for personal aircraft
470239 Predicted effects of the atmosphere on turbine-type aircraft engines
470041 Propeller requirements for light aircraft
470134 Proposed air traffic control and controlled handling systems for high speed aircraft
470098 Reduce airplane noise through basic design
470053 Rocket engines as applied to future aircraft powerplants
470029 Slant mechanism~Its fundamentals and application to diesels for aircraft and other low weight fields
470158 Some applications of hydraulics to high speed, rotary drives for aircraft accessories
470064 Some problems in compressible flows for airplanes
470180 Study of fuel systems for jet aircraft
470101 Supercharging, handling and loading characteristics of the DC-6 airplane
470130 The determination of the optimum airplane-power plant combination
470160 The development of naval aircraft
470166 The experimental determination of strains in aircraft landing wheels and brakes
470087 The pilot versus supersonic speeds
470135 The problems of noise reduction from an airplane design standpoint
470075 The relationship of aircraft detail design to tooling and manufacturing costs
470193 Transport aircraft powerplant outlook for 1947
470097 Why pneumatics or the case for pneumatics for intermittent services on aircraft
460147 A new approach to the flight problem
460195 A petroleum engineer looks at aircraft fuels
460003 A report on the German commercial airline~The Deutsche Luft-Hansa
460108 A summary of design and test experience with monocoque magnesium wings
460150 Air conditioning of turbine-propelled military aircraft
460122 Aircraft engine induction system deposits
460239 Aircraft gas turbines with centrifugal compressors
460059 Airline scheduling
460118 An NACA flight and wind tunnel investigation of maximum lift as affected by variations of Mach and Reynolds numbers
460149 Analysis of transport aircraft cabin air conditioning requirements with special reference to air freshness, temperature, and humidity control
460120 Application of jet assistance to transport aircraft
460207 Application of turbosuperchargers to postwar commercial aircraft
460203 Aviation fuels~What the airlines want and expect
460199 Aviation gas turbine installation problems
460255 Design and test experience with monocoque magnesium wings
460151 Design of a transport airplane electrical system
460190 Design requirements for pickup aircraft
460175 Design trends in aircraft exhaust systems
460217 Development and application of heated wings
460143 Development of chrome plated piston rings for aircraft engines
460012 Development of the Beech Bonanza light four-place high performance airplane
460260 Economics of airline fuel utilization
460013 Electrical equipment for personal airplanes
460254 Evolution of a new "workhorse" airplane for airline use
460107 Factors affecting the design of the air conditioning and pressurizing system for the Republic rainbow airplane
460209 Factors in aeration and deaeration of aircraft-engine oil
460205 Factors pertaining to installation of inverted, in-line aircooled aircraft engines
460250 Factors relative to selected stalling-speed regulations for transport airplanes
460134 Flight tests of aviation oils
460060 For whom the bell tolls~Notes on safety in airline operations
460243 Fuel sensitivity and engine severity in aircraft engines
460237 Gas turbines and aircraft
460233 German aircraft hydraulic systems and their components
460030 German rocket aircraft and their power plants
460247 Heat recovery applied to heating and anti-icing of aircraft
460111 High altitude performance of aircraft electrical equipment
460035 Investigation of an opposed piston light aircraft engine
460163 Landing and launching of transport aircraft from moving land vehicles
460110 Liquid Cooled Engine Power Plants for Transport Aircraft
460181 Mechanical design considerations influencing blading performance in aircraft gas turbine power plants
460127 Method of obtaining optimum aircraft utilization~Domestic and overseas
460061 NACA study of the utilization of exhaust gas of aircraft engines
460165 Passenger aircraft facilities~Design and operation
460252 Planning cabin interiors for transport aircraft
460158 Pneumatic tires for modern airplanes
460040 Possibilities of really high-speed flight
460141 Postwar aircraft industry cashes in on wartime experience
460200 Refrigeration for air conditioning pressurized transport aircraft
460253 Safety in airline operation
460031 Selection of aircraft accessory equipment
460144 Simplified structures for low cost airplanes
460241 Simplifying the airplane for the private owner
460027 Some effects of payload versus range characteristics on transport aircraft efficiency
460156 Some requirements of a "feeder" airplane
460257 Stability problems with swept wings
460065 Supersonic inspection of materials and parts
460245 The airplane icing problem and its alleviation through research
460161 The development of magnesium alloys as aircraft materials
460157 The planning of cabin interiors for transport aircraft
460121 The two cycle engine in aircraft~The crankcase scavenge target engine
460022 Trends in aircraft structures
460259 Utilization of exhaust gas of aircraft engines
460221 Wartime refinery operations and their effect upon motor and aviation fuels
460192 Water injection for aircraft engines
460201 Weight reduction of aircraft braking systems through use of reverse- thrust propellers
450097 A report on the nature of ice formation on aircraft as related to airline operations
450086 A resume of desirable characteristics for non-stalling non-spinning airplanes
450078 Aircraft accessories for 400 cycle motor operation
450175 Aircraft bevel gears
450004 Aircraft fuels of the future~Suppliers' viewpoint
450007 Aircraft interiors from the airline viewpoint
450020 Aircraft lighting
450116 Aircraft riveting and equipment
450115 Aircraft spotwelding at Willow Run
450213 Aircraft-engine gears
450005 Airports as affected by aircraft performance and weight
450082 An analysis of the fundamental training problems created within an airline by a transition from two-engine to four-engine equipment
450042 Application of "T" category licensing test information to airline operations
450085 Auxiliary power systems for aircraft
450121 Aviation lubricating oils
450236 Axial versus centrifugal superchargers for aircraft engines
450165 Basic principles of power boost flight controls
450056 Bond testing of silver plated aircraft engine parts
450055 Control decks for long range aircraft
450172 Cost planning the post-war small airplane
450229 Detection of detonation and other operating abnormalities in aircraft engines by means of special instrumentation
450191 Detonation in flight~Its effect on fuel consumption and engine life
450084 Development of an airline training program for flight personnel involving four-engine equipment
450155 Difficulties with engines installed in civil aircraft
450077 Discussion on defining the market for aircraft for local air transport service
450143 Economic status of the airplane in the postwar market
450203 Electronic analysis of airplane hydraulic braking systems
450022 Electronic controls in aircraft
450112 Engineering problems in the development of a small transport airplane design
450003 Flight engineer station design and requirements
450144 Flight equipment requirements for the Feeder Airline
450006 Fluorescent lighting commercial airplane interiors
450178 Fuel injection for the aircraft engine
450135 Fueling a half forgotten bit of aircraft design
450044 Future aircraft electrical loads
450063 Future trends in intercontinental transport aircraft
450076 General discussion of factors relative to selected stall speed regulations for transport airplanes
450049 High frequency aircraft ignition system with low tension, low frequency distribution
450180 High-altitude factors in flight testing
450237 High-conductivity cooling fins for aircraft engines
450040 Indoctrination period for operation of new type airline aircraft
450058 Jet propulsion and gas turbines in aviation
450163 Late Developments of the Allison Aircraft Engine
450158 Lessons from aircraft engines applied to heavy-duty ground vehicle engines
450189 Military aircraft grease lubrication
450125 Modern aircraft refueling
450090 More landing facilities~The key to private aviation's growth
450105 Naval aviation today in the Pacific
450185 New aspects of airline aircraft maintenance
450151 Possibilities of aircraft structures in ground vehicles
450091 Post-war aviation development and prospects
450079 Protection of electrical systems on military aircraft
450008 Psychological requirements for aircraft passenger design
450074 Reduction of vulnerability of aircraft hydraulic systems
450138 Research and development of aircraft accumulators
450174 Research and tomorrow's aircraft undercarriage
450139 S-S system of lubrication for aircraft engines
450118 Service experience with light aircraft engines
450224 Some advantages and limitations of centrifugal and axial aircraft compressors
450123 Some basic principles of aircraft maintenance economics
450066 Some observations on the financing of aircraft for local air transport
450014 The application of heavy duty additives to aviation oils
450092 The design and development of large post-war transport aircraft
450012 The detection of detonation and other operating abnormalities in aircraft engines by means of special instrumentation
450169 The fundamentals of flight-induced and forced cooling
450080 The mechanics of the manufacture of aviation gasoline
450119 The operating costs of personal airplanes
450241 The place of the gas turbine in aviation
450043 Training of personnel for the operation of the Mars aircraft
450073 Turbosuperchargers for transport airplanes
450149 Wartime aircraft service problems~Their solution
450150 Weight reduction of aircraft braking systems through the use of reverse thrust propellers
450064 What about the age of flight~A realistic appraisal of air transportation in the 5 years to follow the war as seen by United Air Lines
450233 Wood versus metal construction in aircraft
440103 A current outlook on the effects of dynamic loads on aircraft
440158 A new laboratory method of evaluating ring-sticking tendencies of aircraft oils
440135 A study on the efficiencies of cargo airplane designs
440076 Air cargo~A problem of cooperation and coordination between carriers on the ground and in flight
440032 Aircraft engine carburetors and their acceptance testing
440002 Aircraft engines and their accessories
440039 Aircraft engines in tanks
440090 Aircraft environment, thermal effects
440115 Aircraft manufacturing and air transport
440011 Aircraft powerplant development testing
440167 Aircraft-engine~Inlet and exhaust porting
440197 Altitude vapor formation in aircraft fuel systems
440203 An investigation of chafing on aircraft-engine parts
440094 Analytical fuel reserve systems for long range aircraft
440127 Cargo airplane accessories
440086 Co-ordination of flight deck duties on large airplanes
440120 Cockpit lighting of transport aircraft
440043 Cold weather operation of aircraft
440154 Comparison of hydraulic and electrical accessory systems in aircraft
440117 Converting military aircraft for commercial use
440099 Cruising control of transport aircraft
440056 Current trends in aircraft power plants
440179 Design considerations of the cargo airplane
440001 Design of aircraft and its related accessories from a maintenance viewpoint
440119 Effect of airplane design on air transport maintenance
440150 Experience with the use of magnesium in aircraft
440014 Experimental flight testing from the engine manufacturer's viewpoint
440181 Flight testing with a propeller thrustmeter
440171 Fundamental requirements of post-war transport airplanes
440213 Fundamentals of airplane design
440153 How will the 100-octane aviation gasoline program affect post-war motor gasoline
440100 Humidity effects on airplane equipment performance
440007 Low-cost cylinder design for commercial airplane engines
440187 Measurement and prediction of aircraft vibration
440133 Mechanized handling of airplane cargos
440061 Metalbond~A metal adhesive for aircraft
440087 Metallurgical control of aircraft forgings
440110 New light weight power plants for post-war airplanes
440146 Operating temperatures and stresses of aluminum aircraft-engine parts
440095 Passenger comfort in commercial aviation
440058 Pilot line tooling for an experimental airplane
440016 Production design changes of the C-47 airplane
440211 Propeller and gear ratio requirements for aircraft designed for cruising operation
440036 Propeller efficiency of a light airplane
440101 Radio interference and the aircraft engine
440210 Recent trends in airplane ice-prevention technique
440136 Requirements of the feeder line airplane
440201 Some aircraft-engine production methods
440190 Structural flight research
440198 Studies of fuels and fuel system phenomena contributing to aviation vapor lock
440025 Study of the advantages of compression-ignition engine for aviation use, and a possible solution
440175 Synthetic rubber applications on aircraft engines
440205 The design for production of sheet metal aircraft parts
440097 The design of the DC-4\mfC-54 airplane
440089 The development and use of plastic materials for aircraft construction
440207 The intercooling problem in airplane design
440116 The operation of Consairway by Convair has influenced post-war aircraft design
440010 The postwar private airplane
440128 Transport operation experience with cargo airplanes
440034 Usefulness of SAE to the aviation industry
430022 A method of applying production design to aircraft
430141 Aircraft accessory system
430055 Aircraft electric remote controls
430052 Aircraft hydraulic remote controls
430056 Aircraft manufacturing problems
430162 Aircraft oil systems~High-altitude problems
430013 Aircraft service in combat areas
430030 Aircraft structural testing
430156 An aircraft double windshield~Its development and use
430142 Cabin supercharging in scheduled airline operation
430149 Carburetion for the aircraft engine
430116 Chemicals that aid in aircraft production
430027 Chevrolet's aviation engine test plant~Its organization, development and operation
430025 Co-Designing Aircraft Power Plants
430078 Converting today's military airplane transports for post war passenger and cargo use
430100 Corrosion preventive oil and aircraft engine preservation
430167 Deficiencies of converted passenger airplanes for cargo transport and operating requirements
430010 Design and development of the North American aviation trainer series
430023 Field maintenance and repair of fighting airplanes
430131 Flight-testing equipment for large aircraft
430104 General aspects of aircraft power plant installation
430165 Impact extrusion and cold pressing of airplane parts
430047 Influence of new materials on the structural design of airplanes
430154 Intake systems for aircraft engines
430045 Large cargo airplanes
430133 New materials for aircraft engines
430163 Notes on the selection and installation of aircraft propellers
430026 Operating characteristics of lubrication system for an aircraft power plant installation under simulated altitude conditions from sea level to 40,000 feet
430077 Philosophy of flight testing
430072 Post war commercial aviation
430069 Practical application of stress strain theory in fabrication of aircraft parts
430064 Probable trend of post-war aircraft powerplant installation design
430159 Problems in wood aircraft
430130 Re-refining of aircraft-engine oils
430118 Requirements for carburetor air filters for aircraft engines
430011 Scheduling of changes in aircraft production
430014 Servicing military aircraft in overseas theatres
430005 Some economic aspects of the commercial use of converted military aircraft
430085 Some tactical considerations in aircraft design
430040 Strategic materials~Aircraft production and design
430153 The Possibilities of Shaved Gears for Aircraft Engines
430098 The age of cargo flight
430024 The effect of environment on aircraft engine design and performance
430062 The future of aviation
430150 The use of petroleum products in aircraft
430051 Training Operators for Aviation Engine Testing
420019 "Flow production" as applied to the manufacturing of aircraft exhaust collector systems
420073 Advantages and problems of diesel power in aircraft
420087 Aircraft carburetor airscoops and their effect on fuel-air metering in flight
420131 Aircraft-engine radio shielding
420054 Airplane design for cargo transportation
420003 Aviation power plants
420049 Controllable pitch propellers for light airplanes
420077 Cooling characteristics of submerged light aircraft engines
420092 Current problems in light airplane engines
420018 Design aspects of aircraft exhaust system
420123 Design features of the Junkers 211B aircraft engine
420015 Electrolytic etching in aircraft tooling
420008 Engineering styling applied to aircraft interiors
420124 Fuel consumption from the airline's viewpoint
420101 Ground versus flight tests of airplane engine installations
420081 Icing problems in aircraft induction systems
420126 Limiting factors of overhaul periods for aircraft engines
420059 New applications of Panelyte in the aircraft industry
420074 Propeller control and its relation to power in aircraft engines
420057 Requirements for aircraft oil servicing equipment for the war effort
420007 Salvage practices in aircraft manufacture
420055 Structural materials for the cargo airplane
420043 The growth and development of aircraft hydraulic systems and equipment
420062 The place and use of spot welding in design and production of aircraft
420023 The war production effort in aircraft
420021 Tooling for plastic bonded aircraft
420045 Wood-plastics in mass production of aircraft
410002 Aircraft cylinder finishes
410101 Aircraft electricity as the airline operator sees it
410089 Aircraft-engine reduction gears and torque meters
410064 Airplane quality control
410112 Altitude conditioning of aircraft cabins
410099 Altitude performance of high-output aircraft engines
410063 Aviation vapor lock investigation cooperative fuel research committee report
410078 Considerations on the design of aircraft propellers
410138 Design of airscoops for aircraft carburetors
410140 Development of the Ercoupe~An airplane for simplified private flying
410130 Icing problems in operation of transport aircraft
410091 Magnesium alloys in the aircraft industry
410131 Mercedes-Benz DB-601A aircraft engine~Design features and performance characteristics
410001 Modern aircraft engine testing
410007 More aircraft engines for national defense
410113 New high-altitude fuel system for aircraft
410109 Report of CFR committee on aviation vapor-lock investigation
410006 Some factors influencing aircraft engine-propeller vibrations
410118 Standardization of aircraft-engine components
410095 Supercharged aircraft ignition harnesses
410137 The Allison Aircraft-Engine Development
410086 The C.U.E. cooperative universal engine for aviation single-cylinder research
410051 The development of aircraft spotwelding
410023 The du Pont rivet~A new blind fastener for the aircraft industry
410065 The small airplane and its power plant
400063 Airline maintenance
400166 Altitude and the aircraft engine
400142 Aluminum aircraft fuel tanks
400110 Availability and characteristics of aviation safety fuels
400112 Ceramic spark plugs re-enter aviation
400114 Correlation of wind tunnel and flight test results
400099 Criterion of vertical fin area for modern airplanes
400126 Design problems in the quantity production of aircraft engines
400152 Economic aspects of light airplane engines
400153 Experience in integral aircraft fuel-tank construction
400154 Geared engines for light airplanes
400133 High-Output Aircraft Engines
400072 Maintenance development in light aircraft
400169 Modern aircraft materials and their testing
400136 Modern aircraft valves
400159 Passenger comfort in commercial aviation
400137 Performance of aircraft spark-ignition engines with fuel injection
400157 Production of magnesium-alloy aircraft parts
400147 Progress in light aircraft engines
400149 Rudder control problems on four-engined airplanes
400145 Shortcomings of mica insulation for aviation spark plugs
400090 Some economic aspects of aviation fuel volatility
400076 Some simple methods of speeding up airplane production
400118 Some uses of stainless steel in aircraft
400041 Special problems in the production of aircraft engines
400038 Stainless steel in aircraft
400075 Standardization as applied to aircraft design
400150 Status of fuel performance tests in aviation engines
400170 The performance of modern aircraft diesels
400062 The progress of the aircraft diesel
400104 The standardization problem in the aircraft industry
400001 Transport aircraft~Past, present and future
400120 Volatility decreases and availability of high knock rating aviation fuels
400029 War wings
390019 A low-density material for aircraft structures
390018 A new laboratory method for rating aviation fuels of high octane number
390166 A non-icing fully maneuverable aircraft carburetor
390106 A report of studies and tests to decrease aircraft fire hazards
390055 A simplified method for development of prototype airplanes as applied to consolidated model 31 long range patrol boat
390068 Accelerated aircraft production for national defense and some of its effects on organization and personnel
390181 Aircraft engines and their lubrication
390121 Aircraft-engine lubrication
390136 Aircraft-engine valve mechanisms
390155 Airline power control with a torque meter
390089 Airplane brake installation and control consideration
390170 Aviation fuels and engines~Some observations on their present and future development
390098 Composite aircraft
390132 Coordinating aircraft-engine design and production
390171 DC-4 flight tests~Their relation to large air-transport designs
390050 Dynafocal suspension for radial aircraft engines
390145 Dynamic suspension~A method of aircraft-engine mounting
390088 Engineering experimental aircraft
390168 Feathering propellers in airline transport operation
390151 Fuel-economy possibilities of Otto-cycle aircraft engines
390025 Interchangeability in modern aircraft production
390143 Loss prevention in non-scheduled civil aviation
390011 Military value of commercial aviation
390112 Performance and development trends in military aircraft and accessories
390160 Permissible amplitudes of torsional vibration in aircraft engines
390107 Problems in aircraft accessory drives
390157 Prospects for use of "safety fuels" in spark-ignition aircraft engines
390149 Ten years' service experience with alclad materials in aircraft
390134 The BMEP parameter for airplane cruising-power control
390169 The analysis of leading-edge wing beams
390108 The application of electrical equipment to aircraft
390072 The effects of rivets and surface roughness on wing drag
390090 The final assembly of aircraft
390175 The testing of large aircraft
390179 Transatlantic airplane design
390012 Transport airplane development with particular reference to the Curtiss- Wright twenty
390185 Vibration characteristics of aircraft engine-propeller systems
380020 A survey of mechanical failures of aircraft during 1936-1937
380072 Adaptation of pumps to aircraft service
380112 Aircraft fuels
380146 Airplane performance calculations by means of logarithmic graphs
380029 Analysis of improvements in aviation spark plugs
380111 Basic problems in the design of high-output aircraft engines
380143 Engine installation and related problems in large aircraft
380018 Engines for light airplanes
380124 Flight-testing with an engine torque indicator
380081 High flight engineering
380046 Investigation of vapor lock in aviation fuel systems
380053 Plotted transport flight plan
380152 Propeller factors tending to limit aircraft-engine powers
380151 Propeller problems imposed by substratosphere flight
380119 Quality control of aluminum-alloy aircraft castings
380177 Rating aviation fuels in full-scale aircraft engines
380017 Stainless steel for aircraft
380140 The accessory-drive problem of aircraft engines
380028 The air-track system of aircraft instrument landing
380137 The diesel as a high-output engine for aircraft
380032 The effect of oil characteristics on wear in aviation engines
380074 The light airplane for private owner
380161 The single sleeve as a valve mechanism for the aircraft engine
380159 Torsional vibration of in-line aircraft engines
370035 Aircraft engine maintenance
370177 Aircraft powerplant trends
370135 Aircraft spotwelding efforts benefit many industries
370153 Aircraft-engine installation vibration problems
370142 Aircraft-engine materials
370063 Bringing the private owners airplane up to date
370103 Carburetion of engines for long range flight
370193 Design of cowlings for air-cooled aircraft engines
370021 Design trends in French aircraft engines and propellers
370180 Engine and laboratory tests of stability of aviation oils
370086 European aircraft production equipment
370179 Features of the in-line air-cooled aircraft engine
370133 Gust loads on airplanes
370150 High output in aircraft engines
370102 Interior finish and arrangement of transport airplanes
370161 Lubrication and cooling problems of aircraft engines
370109 Maintenance problems of army airplanes
370145 Plant layout and production methods for modern aircraft engines
370108 Plastics in the aircraft industry
370132 Problems in design and construction of large aircraft
370129 Selections of oils for high-output aircraft engines
370157 The aircraft trend in body design from the aircraft viewpoint
370131 The aircraft trend in body structural design
370171 The determination of ratings for transport aircraft engines
370188 The problem of ring-sticking in aviation engines
370167 The vibration problem in aircraft-propeller designing
370175 Vibration measurement in flight
360132 Air-cooled radial aircraft-engine installation
360121 Air-cooled radial aircraft-engine performance possibilities
360035 Aircraft engine piston ring and cylinder wear
360012 Carburetor icing in airline operation
360129 Design of two-engined aircraft
360075 Designing and building for the commercial aircraft market
360083 Designing for the use of aluminum alloy forgings and extrusions in aircraft production
360105 Eliminating crankshaft torsional vibration in radial aircraft engines
360111 Engine nacelles and propellers and airplane performance
360113 Everyman's airplane~A move toward simpler flying
360149 Flight in the sub-stratosphere
360127 Future possibilities of 100-octane aircraft-engine fuel
360078 Maintenance and overhaul of naval aircraft
360138 Manufacturing phases of metal-aircraft construction
360070 Naval aircraft engines
360081 Problems in testing of airplanes for airline service
360112 Rating aviation fuels in full-scale aircraft engines
360010 Smart airplanes for dumb pilots
360049 Some recent developments in aircraft engines
360143 Stressed-skin structures for aircraft
360041 The government's interest in commercial aviation
360077 Tooling a medium sized airplane factory
360053 Trans-Atlantic flight
350100 A designer-manufacturer viewpoint of transport-aircraft needs
350112 Aircraft spark-ignition versus compression-ignition engines
350045 Aircraft structural design and its influence on other engineering design
350119 An analysis of critical stresses in aircraft-engine parts
350006 Are we giving the average private operator the airplane most suitable to his needs
350083 Current problems in airline engines
350086 Fuel injection as applied to aircraft engines
350113 Further progress in controlled cooling of radial aircraft engines
350076 Modern aircraft engine developments
350010 Operating requirements for transport airplanes
350022 Progress report of CFR aviation gasoline detonation subcommittee
350007 Sales and technical problems of private commercial airplanes
350097 The influence of engine oils on aircraft-engine performance
340076 Acoustics and the airplane
340081 Aerodynamics of wing sections for airplanes
340070 Aircraft instruments and their uses
340105 Aircraft-propeller development and testing summarized
340096 Altitude performance of aircraft engines equipped with gear-driven superchargers
340019 Correlation of knock-rating of aviation gasolines
340018 Design limitations of aircraft engines
340116 Ice formation in aircraft-engine carburetors
340030 New airline advancements~Maintenance and operations
340085 Rotating-wing aircraft compared to conventional airplanes
340032 Some aspects of commercial aviation
340107 The airplane landing-gear shock-absorbing system
340089 The cowling and cooling of radial air-cooled aircraft engines
340071 The measurement of landing speed and other flight test procedure
330066 Aircraft maintenance on scheduled service
330004 Airplane flight testing for maximum speed
330030 Airplane vibrations and flutter controllable by design
330003 Commercial flight tests improved by new equipment and methods
330054 Detonation rating of aviation fuels
320069 Bending moments in the master rod of a radial aircraft engine
320043 Flight control by air visualization
320012 Indicators as a means of improving aircraft-engine performance
320011 Late developments in airplane stress-analysis methods and their effect on airplane structures
320037 Magnesium alloys in aircraft-engine construction
320066 Relation of design to airplane maintenance
320014 The economic aspects of transport-airplane design
320044 The rational specification of airplane load factors
320027 The rationalization of load factors for airplanes in flight
320010 Vibration of instrument-boards and airplane structures
310036 A study of airplane and instrument-board vibration
310029 Airplane fuel-line temperatures
310040 Bearing-load analysis and permissible loads as affected by lubrication in aircraft engines
300037 Aircraft-engine installation
300030 Development of a safe airplane~The Curtiss Tanager
300033 Flight-test instruments
300024 Fuel requirements of the gasoline aircraft-engine
300036 Gaging airplane-engine performance
300023 Gasoline requirements of commercial aircraft engines
300027 Knock values of aviation fuels
300038 Suppressing ignition-interference on radio-equipped aircraft
300034 The Packard diesel aircraft-engine
300028 The effect of airplane fuel-line design on vapor lock
300032 The operator's airplane and engine requirements
300026 The vapor-locking tendency of aviation gasolines
300025 Volatility requirements of aircraft fuels
290059 Aircraft propellers
290067 Airplane lighting requirements
290050 Airplane spins and wing slots
290057 Diesel engines for aircraft
290040 Fluidity and other properties of aviation-engine oils
290062 Gearing of aircraft propellers
290063 Modern light alloys and their application to aircraft-engine design
290051 Possible improvement of present-day aircraft
290066 Prevention of corrosion in duralumin airplane structures
290049 Spinning characteristics of airplanes
280030 Duralumin all-metal airplane construction
280066 Fabrication of the Lockheed Vega airplane-fuselage
280029 Methods of building metal airplane structures
280065 Naval air-tactics and aircraft design
280028 Single-engine versus multi-engine airplanes
280064 The Packard X 24-cylinder 1500-Hp water-cooled aircraft engine
270070 Airplanes for commercial aviation
270073 Application of non-military aircraft to naval purposes
270066 Metal construction of aircraft
270072 Modern Naval Aircraft
270069 Problems in Transport-Airplane Design
270027 Recent development in aircraft powerplants
270063 Recent developments in aircraft ignition-systems
270065 Selection of materials for aircraft structures
270068 Service aviation, aeronautical engineering and commercial aviation
270071 Trends in military airplanes
260064 A roots-type aircraft-engine supercharger
260060 Air-cooled engines in naval aircraft
260025 Economic spheres of airplane and airship
260065 Economical production of all-metal airplanes and seaplanes
260063 Progress in aircraft-engine design
260061 The development of the Wright whirlwind type J-5 aircraft-engine
250027 Recent developments in aircraft engines
250066 Some aspects of aircraft-engine development
250069 Some aspects of airplane inspection
250067 The evolution of the modern racing airplane
240028 Airplane-engine designing for reliability
240033 Exhaust-valves and guides for aircraft engines
230011 Aircraft-engine practice as applied to passenger-cars
230028 Recent developments in aircraft engines in the navy
230029 The design of commercial airplanes
220064 Airplane performance formulas
220030 Recent aircraft engine developments
220065 Recent airplane design and performance improvements
220031 The trend of aviation development
210024 Commercial aviation in the eastern hemisphere
210019 Compression-ratio and thermal efficiency of airplane engines
210015 Recent progress in military aviation
210009 Some experiments on thick wings with flaps
200026 Design factors for airplane radiators
200025 Engine shape as affecting airplane operation
200045 Factors involved in high airplane speed at great altitudes
200027 Flying an airplane engine on the ground
200024 Landing run and get-away for standard airplanes
200023 Maintaining airplane engine power at great altitudes
200048 Recent advances in aviation
200022 The heat-treating of brazed fittings for aircraft
190028 Aircraft radiators
190018 Airplane and seaplane engineering
190026 Commercial future of airplanes from an engineer's standpoint
190021 Making the airplane a utility
190019 Operations of naval aircraft
190017 Problems of the naval aircraft factory during the war
190056 Progress in naval aircraft
190020 The Liberty aircraft engine
190064 The airplane as a commercial possibility
190062 The horsepower of resistance in airplane design
180049 Airplane development and naval policy
180033 Airplane types
180038 Exhaust headers and mufflers for airplane engines
180031 International aircraft standards
180047 Navy airplane development
180002 Reasons behind the liberty aviation engine
180050 The Hispano-Suiza aircraft engine
180041 The future of the airplane business
180001 Types of military airplanes
170042 Aviation engine development
170011 Evolution of airplane wing-trussing
170009 Some notes on high-pressure aviation engines
170001 Some problems in airplane construction
170010 Suggestions for standard tests of airplanes

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