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SAE Papers

Paper Number / Title
For more information, click on the Paper Number
Book Number
2008-01-2258
Destructive Evaluation of Four Aircraft Representative of the General Aging Aircraft Fleet
V117-1  
2008-01-2259
The Fatigue Behavior of Fastener Joints
V117-1  
2005-01-3195
Improving the Harrier: Projected Developments of the Pioneering V/Stol Combat Aircraft 1957–1990
 
2004-01-1800
International Intrigue, Paper Clips, and Envelope Pushing Research in the Heartland
 
2002-01-2949
A Longitudinal Slip Tire Model for Brake Control Systems: Features and Uses in Simulation, Control Synthesis and Stability Analysis
 
2002-01-2958
ATN Airborne Implementation
 
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
 
2002-01-2916
Assessment of the Dynamic Stability Characteristics of the Bell Model M427 Helicopter Using Parameter Estimation Technology
 
2002-01-2948
Asymmetric Approach in Solving Aircraft Brake Vibration
 
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 NASA's 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
 
2002-01-3001
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
 
2002-01-3006
HUD Symbology for Surface Operations: Command Guidance vs. Situation Guidance Formats
 
2002-01-3008
Highlights of NASA's Systems Approach to Crashworthiness Research
 
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 Victrex® PEEK™ 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
 
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
World's First Delta Wing Airplane Convair/Air Force XF-92A
 
975609
Milestones in Airborne Astronomy: From the 1920's 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
 
690432
A Radiation Pyrometer Designed for In-Flight Measurement of Turbine Blade Temperatures
 
690378
A Review of Operational Experience and Pilot Considerations for Aircraft Ground Operations
 
690712
A Systems Approach to Flammability Control for Aerospace Safety Application
 
690674
Advanced Technology in Airline Passenger 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
 
690399
Airport Terminal Planning for Tomorrow's Aircraft
 
690394
An Airline Looks at Area Navigation
 
690561
An Airplane Designer's View of Aircraft Ground Support
 
690614
An Integrated Aerospace Dynamic Program
 
690195
Application of Computer Graphics in Aircraft Design
 
690342
Application of Glass Reinforced Plastic Molding Compounds in the OV-10A Airplane
 
690335
Bioengineering of Impact Survival in Business Aircraft
 
690381
Booster Engines for Commercial Airliners
 
690628
Casting: A New Tool in Aircraft Structural Design
 
690320
Changing Airworthiness Requirements for Air Taxi Operators and Their Effect on Manufacturers of Small Airplanes
 
690725
Computer Planning With the Optical Image Terminal
 
690403
Control Concepts for a High Bypass Aircraft Turbofan Engine
 
690313
Conversion of Light-Weight Commercial Aircraft to Fulfill a Specific Military Mission
 
690673
Design and Testing of an Aircraft Nucleonic Fuel Quantity System
 
690706
Design of Fighter Aircraft for Combat Survivability
 
690724
Determination of the Influence of Propeller Thrust on CL and CD 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
 
690696
Development of a Digital Variable Stability System
 
690701
Developments in Soviet Aerospace Manufacturing Technologies
 
690344
Distance Measuring Equipment for the Supersonic Transport and the Corporate Twin
 
690346
Electrical Power Sources for Business Aircraft
 
690318
Electron Beam Welding in Aircraft Components
 
690630
Electron Beam Weldments for Large Complex Shapes
 
690659
Emergency Monopropellant Auxiliary Power Units for Large Commercial Aircraft
 
690553
Equipment for Forest Fertilization
 
690425
Evolution of the Pratt & Whitney Aircraft JT9D Engine Oil System
 
690316
Explosive Fabrication of Aircraft Components
 
690321
FAA CRASHWORTHINESS PROGRAM FOR LARGE AND SMALL AIRPLANES
 
690680
Fabrication Techniques — HY-140 for Flight Type Pressure Vessels
 
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
 
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
 
690406
LAMS B-52 Flight Experiments In Direct Lift Control
 
690662
Lifting Body Flight Tests and Analysis
 
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 GSE for the Next Generation 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 APU's for Executive Aircraft
 
690415
Passenger Airplane Economics and Systems Application Considerations for Airline Operations
 
690341
Potential Structural Materials and Design Concepts for Light Airplanes
 
690334
Simplified Fuel Systems for Light Aircraft
 
690371
Sonic Testing of Gray Iron Sleeve Castings to Predict Tensile Strength
 
690314
Special Operations Use of General Aviation
 
690707
Survivability Design of Forward Air Control and Light Attack Aircraft
 
690705
Survivability of Military VSTOL Transport Aircraft
 
690741
Systems Concepts in Control Design for APU Industrial and Commercial Aviation Application
 
690327
The Future of Cockpit TV-Radar
 
690375
The Pilot's Choice - Off the End or Off the Side of the Runway
 
690413
Total Airline Profit Model Program
 
690635
Trailer Design for Mobility
 
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
 
690690
VERSATILE LAUNCH VEHICLE DIGITAL AUTOPILOT
 
690693
VTOL Flight Investigation to Develop a Decelerating Instrument Approach Capability
 
680712
Performance Matching of the Propulsion System
 
680713
Some Implications of Noise Restrictions to Subsonic Transport Engine-Installation Design, Development, and Operation
 
680275
A Description of the VTOL Airline System
 
680288
Airframe-Propulsion Integration for Future Aircraft Systems
 
680285
Cost and Operational Problems of a Scheduled Helicopter Airline
 
680298
Decca/Omnitrac Experience — Seaboard World Airlines
 
680286
Integration of Inlet and Engine - An Engine Man’s Point of View
 
680287
Integration of Inlet and Engine — An Airplane Man’s Point of View
 
680277
New Generation Engines - The Military Outlook for Adaptive Propulsion Systems
 
680279
New Generation Engines — Research Problems and Outlook
 
680283
Operational Problems with Current Commercial V/STOL Aircraft
 
680294
Optimizing Exhaust — Nozzle/Airframe Thrust Minus Drag
 
680296
Performance Installation Effects for Nozzles Installed on a Twin-Jet Fighter Airplane Model
 
680274
Ports for STOL — Some Observations
 
680299
Results of the American Airlines Evaluation of the Litton LTN-51E Inertial Navigation System
 
680297
Status and Future of Aircraft Satellite Navigation
 
680272
The Role of the Small Jet in the Airline Training Syllabus
 
680290
The Significance of Advanced Structural Fabrication Techniques on Aircraft Lightning Protection
 
680326
VTOL Aircraft — Competitor or Assistant
 
680295
Variable-Geometry Exhaust Nozzles and Their Effects on Airplane Performance
 
680280
Wind Tunnel Investigations of a High Speed Stowed Rotor Aircraft
 
680206
Advantages of Some New Fastener Systems
 
680205
Airplane Vibrations Using Cantilevered Component Modes
 
680208
Combustion Heating System for Business and Utility Aircraft
 
680202
Devices for Stick Free Stability
 
680215
General Aviation Avionics Reliability
 
680203
Initial Report on Operational Experiences of General Aviation Aircraft
 
680219
Maintenance Program for the Executive Operator
 
680201
Recent Transonic Airfoil Developments and Some Business Aircraft Implications
 
680204
Unique Design Considerations for a Large “T” Tail Aircraft
 
680214
Who Needs Avionics Performance Minimums - The Government or You?
 
680209
Accuracy in Fuel Management for General Aviation
 
680330
Advancements in Structural Beryllium Technology
 
680199
Aerodynamic Development of the Cessna 177
 
680339
Air Pollution Emissions from Jet Aircraft Operating in New York Metropolitan Area
 
680312
Aircraft Auxiliary Power Supplies
 
680671
Aircraft Integrated Data Systems as a Flight Operations Tool
 
680721
Astronaut Safety Features for Apollo Lunar Surface Experiments Package
 
680311
Auxiliary Power Systems for 1975 Fighter Aircraft
 
680651
Beryllium: Brazing and Welding
 
680333
C-5A Propulsion System Installation
 
680225
Capacitance Fuel Gaging for Business Aircraft
 
680216
Constant Frequency AC Electrical System for Business Aircraft
 
680231
Contamination + Microbes = Corrosion + Malfunctions: An Equation which Yields Trouble for Aircraft Integral Fuel Tanks
 
680190
Criteria for Contamination Level in Flight Control Systems
 
680337
Design Features for Maintainability in the Pratt and Whitney Aircraft J9D Gas Turbine Engine
 
680447
Design Requirements of Small High-Temperature-Rise Combustors
 
680314
Design and Fabrication of a Pressurized Boron Composite Wing Box
 
680646
Design and Tests of Inverting Flaps and Wing Span Flaps
 
680099
Design for the Lunar Environment
 
680100
Design for the Remote Control Environment
 
680313
Designing and Fabricating Aircraft Structures with Filamentary Composites
 
680057
Designing for V/L Performance in an Aircraft Engine Fuel Pump
 
680545
Designing the Lockheed L-1011 to Meet Airline Needs Beyond 1970
 
680331
Diffusion Bonded Structures for Application to Air Transport Aircraft
 
680222
Dinade System as an Anti-Collision Device
 
680340
Effects of Dynamic Environments on Fuel Tank Flammability
 
680056
Environmental Control Accessories Test Facilities Needed for Life and Reliability on Future Projects
 
680725
Evaluation of an Air Conditioning System for a 1970 Short Haul Commercial Jet Aircraft
 
680342
Fatigue - Life Establishment and Detection
 
680670
Flight Monitoring and Analysis
 
680728
Ideas, Integrated Design and Analysis System
 
680711
Inlet and Fan Aerodynamics
 
680690
Installation features of Rolls-Royce advanced technology large transport engines
 
680709
Installation of the APU in the 747 Airplane
 
680399
Intake Valve Throttling (IVT) - A Sonic Throttling Intake Valve Engine
 
680354
Integral Weight and Balance System Applications on Cargo Aircraft
 
680644
Low-Speed Characteristics of High-Performance Lift-Engine V/STOL Aircraft
 
680317
Lubricants for Inerted Lubrication Systems in Engines for Advanced Aircraft
 
680221
Maintenance During and After Warranty
 
680374
Manned Lunar Flying Machines - Operational Characteristics
 
680733
Mechanism of Deposit Formation in Wing Tanks
 
680718
Microbiological Studies on a Water Management Subsystem for Manned Space Flight
 
680310
Modular Aircraft Engine Logistics System
 
680278
New Generation Engines — The Engine Manufacturer’s Outlook
 
680223
Noise Abatement
 
680716
On-Board Aircraft Oxygen Generating System
 
680691
POTENTIAL TECHNOLOGY IMPROVEMENTS FOR THE CF6 TURBOFAN
 
680355
Pan American Operational Experience with STAN
 
680226
Performance Characteristics of Aircraft with Turbosupercharged Engine and Cabin — 1968
 
680227
Propeller Design Consideration for Turbine Powered Aircraft
 
680744
Reliability and Maintainability Problems Confronting Environmental Control/Life Support Systems for Long Duration Space Flight
 
680666
STOL/VTOL Aircraft Characteristics, Terminal Navigation and Air Traffic Control
 
680708
Secondary Power Requirements for Large Transport Aircraft
 
680370
Short Downrange Entry
 
680346
Smoke Measurement Techniques
 
680371
Space Escape Systems - A Status Report
 
680058
Structural Requirements for Aircraft Engine Main Fuel Pumps and Controls
 
680373
Surface Mobility Systems for Lunar Exploration
 
680729
Systems Analysis Applications to the C-5
 
680648
Systems Considerations for Aerospace Beryllium Applications
 
680693
The Development of a Composite Main Rotor Blade for the Sud-Aviation SA-330 Helicopter
 
680727
The Impact of Maintainability Analysis on Aircraft Design
 
680724
The Impact of the Physiological Characteristics of Perishables on Aircraft Environmental Control Systems
 
680325
The Place of Cargo Aircraft in Total Air Transportation
 
680738
Titan III Launch Vehicle Flight Test Experience
 
680220
Trailing Vortex Hazard
 
680228
Turboprop Engine Operational Experience in STOL Aircraft Operating from Rough Fields
 
680663
VTOL Aircraft Terminal Area Operations Research
 
680309
Variable Speed Constant Frequency Power Source
 
680673
Vulnerability and Crashworthiness in the Design of Rotary Wing Vehicle Structures
 
680303
Wind Tunnel Test Considerations Unique to V/STOL Aircraft
 
670693
Applications of the ST6 Gas Turbine Engine
 
670389
A British Reusable Booster Concept
 
670254
A Category II Avionics System
 
670384
A Comparison of Fixed Wing Reusable Booster Concepts
 
670263
A Current Survey of Aircraft Fuel Gauging Systems
 
670374
A European Point of View on Recoverable and Reusable Spaceflight Systems (Aerospace Transporter)
 
670388
A French Concept for an Aerospace Transporter
 
670871
A Jet Engine Malfunction Diagnostic System using Sonic/Vibration Analysis
 
670581
A Lunar Environment Simulation Test Bed
 
670686
A Perspective Look at VTOL
 
670311
A Review of the Current Policy in the United Kingdom for the Use of Flight Simulators in Flight Crew Training and Checking
 
670566
A Unique Metal-to-Metal Seal for Separable Joints
 
670658
A-7A Aircraft Maintenance Guarantee and the Role of Training
 
670353
ADAM II Propulsion System and Internal Aerodynamics
 
670547
AGD - Concept to Configuration
 
670337
Adapting Space Vehicle Checkout Procedures and Philosophy to Near-Future Transport Aircraft
 
670244
Aerodynamic Considerations of a Medium Mach Business Aeroplane
 
670880
Aerodynamic Design Considerations of Variable Geometry Aircraft
 
670847
Aerodynamic Design Features of the C-5A
 
670846
Aerodynamic Design of the DC-9 Wing and High-Lift System
 
670243
Aerodynamics of the Cessna Tandem Twins
 
670305
Aerospace Concepts Applied to Deep Submergence Vehicle Simulation
 
670982
Airline Considerations for the SST Environmental Control System
 
670891
Airline Operation and Maintenance Requirements for Fasteners
 
670320
Airline Terminal Building Concept
 
670865
An Airline View of the SST Powerplants
 
670138
An Approach to Simpler Control Requirements
 
670027
An Ultrasonic Method of Measuring Piston Ring Bore-Contact Patterns
 
670814
Availability and Evaluation of Nonphotochemically Reactive Primers and Topcoats for Aerospace Applications
 
670574
C-5A Flight Control System
 
670312
Can Flight Training Take Lessons from our Astronaut Training Program?
 
670901
Canada's Role in the Second Decade of the Space Age — Inner Space Supersonics
 
670257
Certification of the Sabreliner Safe-Life Structure
 
670530
Comparative Evaluation of Flight Control Power Distribution Systems for Hypersonic Aircraft
 
670939
Corrosive Ring Wear - Does it Exist with Modern Lubricants and Ring Metallurgy?
 
670371
DETERMINING SST SIZE
 
670344
Design Criteria and Configuration for Long-Life Aircraft Gas Turbines
 
670579
Design Objectives for Tomorrow's Escape Systems
 
670234
Designing Business Jet Aircraft Engines for Increased Service Life
 
670363
Designing Diagnostics into Propulsion Systems
 
670617
Development of Improved Gust Load Criteria for U. S. Air Force Aircraft
 
670241
Development of the Third Level Airline Industry
 
670341
Disciplines of Organization
 
670365
Emulsified Jet Engine Fuel
 
670575
Escape System Requirements for U. S. Army Aircraft in Vietnam
 
670228
Estimating Maintenance Man-Hours Per Flight Hour for Business Turbojet Airplanes
 
670585
Evolution of the A-7A Hydraulic Tubing Permanent Joint System
 
670349
Failure Safety in V/STOL Operations
 
670888
Fastener Applications for Aircraft Gas Turbine Engines
 
670889
Fastener System Concept
 
670528
Flight Control System for The Boeing 2707 Supersonic Transport Airplane
 
670304
Flight Simulator Motion, Its Enhancement and Potential for Flight Crew Training
 
670559
Flotation Requirements for Aircraft
 
670260
Flutter Characteristics of the Slab Tail
 
670261
Flying Qualities Research Using an In-Flight Simulator
 
670326
Fuel Control System of The GE4 Engine for The Supersonic Transport
 
670370
Fuselage Configuration Studies
 
670301
Future Potential and Requirements of Digital Simulation
 
670968
Gas Turbine Engines Applied to Passenger Trains
 
670242
Gulfstream II Aerodynamic Design
 
670245
High Lift Techniques for STOL Aircraft
 
670529
Hydraulic Power Units for Supersonic Aircraft
 
670811
Impact of Rule 66 Upon Industry
 
670669
Improving Aerospace System Safety Programs Through an Inter-Company Information Exchange
 
670329
Inertial Navigation Systems for Subsonic and Supersonic Commercial Aircraft
 
670622
Long Duration Space Missions Through Use of In-Flight Maintenance
 
670883
Maintainability Considerations in Variable Geometry Aircraft
 
670835
Managing Engineering for Profit in the Aerospace Industry
 
670882
Mechanical Aspects of Variable Sweep Wings
 
670873
Mechanical Impedance Approach to Engine Vibration Transmission Into an Aircraft Fuselage
 
670295
Medical/Human Factors Aspects of Jetliner Flight in Severe Turbulence
 
670861
Metal-Matrix Composites Behavior and Aerospace Applications
 
670869
Microbes and Their Jet Fuel Environment
 
670354
Mixed Missions - Potential Improvements in Thermal Management of Hypersonic Designs
 
670302
Need for State-of-the-Art Advances in Maintenance Training Equipment
 
670339
New Advances in Nondestructive Testing Techniques
 
670327
New Flight Instrumentation for Future Transport Aircraft
 
670548
Noise Control of Aircraft Auxiliary Power Units
 
670562
OV-10A Landing Gears
 
670358
One Airline's Hits and Misses in Propulsion Systems Diagnostics
 
670325
Operating Techniques and Maintenance Considerations for Air Inlet Controls in Airline Service
 
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 Now
 
670879
Pilot Comments on Variable Geometry Aircraft
 
670267
Powerplant Pressurization for Altitude
 
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
 
670373
Proposed New Approaches to the Maintenance of the Boeing Supersonic Transport
 
670230
Quebec's Approach to the Use of Special Aircraft for Forest Fire Suppression
 
670317
RELIABILITY DEVELOPMENT ON THE GE4
 
670262
Recent Developments in Instrumentation and Fuel Systems for Turbocharged and/or Pressurized Aircraft
 
670884
Reliability of the SST Wing-Sweep Actuation System
 
670560
Results of Studies to Improve the Ground Flotation of Aircraft
 
670385
Review of European Aerospace Transporter Studies
 
670661
Risk Assessment in Complex Unattended Aerospace Systems
 
670984
SST Concorde Air Conditioning System
 
670827
Short Haul Military Requirements (1970–1980) — A Qualitative Estimate of Aircraft Criteria
 
670140
Some Aircraft Gas Turbine Environmental Challenges for the Control Designer
 
670392
Space Operations and Economics
 
670550
Space Power and the Progression of Manned Space Flight Requirements
 
670881
Structural Considerations for Variable Sweep Wings
 
670300
Survey of Flight Simulation Computation Methods
 
670578
Techniques for Space and Hypersonic Flight Escape (Paracone)
 
670269
Test Results of an All-Mechanical Flight Control System Utilizing a Cascade Toroidal Servo
 
670343
The Basic Discipline of Airline Operation
 
670561
The C-5A Landing Gear
 
670382
The Case for Ballistic Recovery of Boosters
 
670249
The Cold Starting and Service Test Evaluation of an SAE 10W30 Aircraft Engine Oil
 
670259
The Design of a Small Pressurized Aircraft Structure
 
670355
The Economics of Airline Scheduling as Frustrated by the Total System Environment
 
670338
The Future Needs and Current Advances Within the Airlines
 
670237
The General Problems in Vibration of Aircraft Powerplant Components
 
670196
The Guided-Light Display Panel
 
670531
The Hydraulic System of the Concorde
 
670631
The Impact of Maintainability Engineering Techniques on the Design of the F-111
 
670253
The Impact of Microelectronics on General Aviation Avionics
 
670306
The Influence of Piloted Flight Simulator Studies on the Design of the SST Instruments
 
670577
The LW-3B Escape System
 
670328
The Place and Capabilities of Modern Doppler Systems for Subsonic and Supersonic Aircraft
 
670405
The Place of the Aerospace Transporter in European Space Programme — Recommendations
 
670342
The Psychological Variable in Airline Safety
 
670194
The Rotating Combustion Engine - Compact, Lightweight Power for Aircraft
 
670582
The United States SST Controls Development Program
 
670297
The Urgent Need for Flight Simulators for Present and Future Aircraft
 
670333
The Use of Composite Materials in Aero Engines
 
670235
Thrust Reversers for Business Jet Aircraft
 
670250
Trends in Aircraft Direct-Current Electrical Systems
 
670238
Two-Stroke Light-Aircraft Engine Potential
 
670826
V/STOL and Short-Haul Commercial Requirements
 
670878
Variable Geometry in a Supersonic Transport Aircraft
 
670303
Visual Simulation - Where We Are - Where We Are Going
 
670571
XC-142A Control System
 
660023
A Forward Look at Tube Transportation
 
660222
A New Generation of General Aircraft Engine Mountings
 
660273
A Pilot's Summary of XB-70 Flight Test Experience
 
660205
A Practical Data Processing Approach for Achieving Effective Management Control of Aircraft Manufacture
 
660315
A Report on Stability and Control Testing of a Tilt Wing V/STOL Aircraft
 
660700
A Systematic Approach to Determining Aircraft Aerospace Ground Equipment
 
660280
ATA Direct Operating Cost Formula for Transport Aircraft
 
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
 
660194
Airline Practices in Forecasting Clear Air Turbulence
 
660219
An Evaluation of General Aviation Aircraft Flying Qualities
 
660666
Beryllium Structures for Aircraft
 
660214
Birdproofing the Sabreliner
 
660322
CANDIDATE TURBOFAN ENGINES FOR SUBSONIC AIRCRAFT OF THE 1970’s
 
660204
Cessna Aircraft Commercial Division Quality Control Program
 
660674
Changing Environment and Its Effect on Structures
 
660319
Commercial Helicopter Outlook Vertical Take-off and Landing (VTOL) Aircraft Air Traffic Control System – An Analysis of Helicopter Air Traffic Control Problems
 
660184
Correlation Between Clear Air Turbulence and Aircraft Electrical Activity
 
660207
Current and Possible Future Trends in Oxygen Equipment and Usage
 
660215
Defining the Fatigue Load Environment for Business Aircraft
 
660216
Design and Development of the Structural Integrity of a Jet Executive, D.H. 125
 
660218
Development and Flight Testing a Simplified Fixed Shaft Turboprop Flight Control System
 
660209
Development of Air Conditioning in Beech Airplanes
 
660314
Development of High-Performance Rotary-Wing VTOL Aircraft
 
660738
Development of Thrust Deflection and Vectoring - V/STOL
 
660178
Economic Aspects of Flight in Turbulence
 
660210
Economics of Business Aircraft
 
660671
Effects of Subsonic, Supersonic, Hypersonic, and Orbital Environments on Structures
 
660664
Evaluation of Proposed Hydraulic Fluids for the SST
 
660647
Experimental Titanium Crossbeam
 
660293
FAA Concept in Safety for the SST
 
660217
FAA Research, Development, and Airworthiness Compliance for General Aviation Aircraft
 
660279
Factors Affecting Utilization
 
660073
Factors Influencing Aircraft Turbine Engine Oil Drain Practices
 
660283
Flight Operations on a Circular Runway
 
660702
Ground Support for the Supersonic Transport
 
660678
Hypersonic Thermal-Structural Concept Trends
 
660737
Installation Considerations for the High Bypass Fan Engine in Subsonic Transports
 
660669
Large Cargo Airplane Structural Considerations
 
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
 
660663
Materials for Aerospace Antennas and Radomes
 
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
 
660656
New High Strength Magnesium Casting Alloys for Aerospace Applications
 
660642
New and Proposed Composites
 
660443
Next-Generation Lunar Transports
 
660701
On-Board Check-Out Systems for Aircraft
 
660646
Plasma Arc Welding for Large Titanium Aerospace Structures
 
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
 
660294
SST Operations and Maintenance Considerations
 
660296
SST Propulsion Systems - Airline Operational and Economic Goals
 
660337
Short Airfield Assisted Landing and Take-Off for Commercial Aircraft
 
660305
Some Problems the Fastener Industry Perceives in Effecting Aerospace Conversion to the Metric System
 
660673
Space Vehicle Structures — Does Man's Presence Make Any Difference?
 
660679
Structural Considerations in the Design of a Liquid Hydrogen Tank for Hypersonic Vehicles
 
660298
Supersonic Transport Propulsion Systems - Operational Growth Feasibility
 
660297
Supersonic Transports - Propulsion Systems - Application of Advanced Technology
 
660213
Support Breeds Success and Successors
 
660323
THE NEW ENGINE TECHNOLOGY AND THE SUBSONIC TRANSPORT
 
660144
Testing of Lunar Surface Vehicles under Simulated Lunar Gravity Conditions
 
660208
The Application of Vapor-Cycle Cooling Systems to Business Aircraft
 
660221
The Application of the High Bypass Turbofan for Business and Executive Aircraft
 
660150
The Correlative Advantages of Lunar and Terrestrial Vehicle and Power Train Research
 
660277
The Design Importance of Airplane Mile Costs Versus Seat Mile Costs
 
660316
The Effect of Size on the Economics of a V/STOL Transport Airplane
 
660220
The Effect of a Light Aircraft Stability Augmentation System on Pilot Performance
 
660670
The Effects of Low Level Turbulence on the Structure of a Large Logistic Aircraft
 
660223
The Jet Pump as a Fuel Pump for Today's Aircraft
 
660333
The United Aircraft Turbine Motor Train and Its Suspension System
 
660687
The “Systems” Approach to AGE Management
 
660710
Turbine Fuel Thermal Stability - from Refinery to Supersonic Transport
 
660668
V/STOL Aircraft Structural Considerations
 
660318
V/STOL Transport Aircraft for Intercity Passenger Movement
 
660275
XB-70 Ground Servicing and Safety Precautions
 
660274
XB-70A Mach 3 Design and Operating Experience
 
650844
Soft and Rough Field Landing Gears
 
650231
1953 Paper Jet Operations in Retrospect with Connotations for the Supersonic Transport
 
650364
A Five-Point Program Designed to Eliminate Contamination and Corrosion of Fuel Tanks on Aircraft Using Jet Turbine Fuel
 
650350
A Hot Gas Servocontrol System for Aerospace Applications
 
650503
A Mach 3+ Aircraft Fuel Pump
 
650265
A Method for Comparing and Selecting Propulsion Systems for V/STOL Aircraft
 
650780
A Rapid Method for Diffusion Bonding Aerospace Structures
 
650834
A Systematic Approach to Shelter Design for Lunar Exploration
 
650592
A Technique for Lunar Landing Site Selection by Earth-Based Control
 
650377
Accurate Power Checking of Production Aircraft Engines
 
650200
Advanced Propeller Developments for V/STOL Aircraft
 
650823
Aero-Acoustic Excitation of Structures
 
650247
Aeronautical Progress in the Federal Aviation Agency
 
650388
Airplane Vibration - A Practical Approach
 
650370
An Abstract of an Analysis: The Effect of the Airframe Manufacturer's Cost on the Cost of Aircraft Ownership
 
650372
An Aircraft Manufacturer Looks at Business Aircraft Operating Costs
 
650371
An Operator Looks at Business Aircraft Operating Costs
 
650580
Analysis of Toroidal Actuation Systems for Aerospace Vehicles
 
650250
Angle of Attack as an Aid to Flying
 
650101
Application of Regenerative Engines to Current and Future Aircraft
 
650249
Army Aircraft Systems Development Program
 
650269
Aviation Fuel Safety
 
650375
Aviation Spark Plug Operational Factors
 
650367
Beech Aircraft Reliability Program
 
650812
Biomedical Requirements for Manned Space Flight
 
650032
Business Aviation Department Analysis
 
650248
C-5A Cargo Transport Aircraft
 
650221
Can the Compact Jets Solve Both the Trunk and Regional Airlines Dilemma?
 
650302
Carbon-Graphites for Aerospace Seals
 
650808
Control Requirements and Control Methods for Large V/STOL Aircraft
 
650581
Control System Aspects of an Analytical Investigation into Controlling the Structural Modes of Flexible Aircraft
 
650244
Current Financial Considerations in Airline Aircraft Acquisitions
 
650235
Design Concept of a Jet Close Support Aircraft (Super COIN)
 
650349
Design Margin: Key to Lunarcraft Shock Absorber Reliability
 
650782
Design for Airfreight Development - The Next Decade
 
650227
Design of Aircraft for Safety
 
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 the Gas Turbine Engine Installation in the North American Aviation Sabreliner
 
650937
Development of the Model 727 Airplane High Lift System
 
650169
Donasonic - Turbine Tailored Silencing
 
650805
Economical Much 3+ SST Fuel Available Now
 
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
 
650055
Engineering Aspects and Mathematical Formulation of the Problem of a Computerized Aircraft Structural Analysis System
 
650226
Environmental Control System Considerations for Supersonic Cruising Aircraft
 
650597
Factors in Selecting Digital or Analog Computation for Flight Control
 
650327
Fire-Resistant High Temperature Hydraulic Fluids for the SST
 
650594
Flight Control for a Manned Orbital Space Station
 
650205
Flight Simulator Utilization for System Design and Pilot Training
 
650387
Flutter Problems of Business Airplanes
 
650297
Fuel for the Supersonic Transport
 
650598
Functional Design of the Minuteman Flight Control System
 
650755
Future Aerospace Manufacturing Educational Requirements
 
650585
Future Sensing and Information Requirements and System Ideas that Apply to Flight Control
 
650595
Gemini Flight Control System Performance during the Second Unmanned Flight
 
650368
Gulfstream Reliability
 
650803
Heat Transfer Unit Evaluates Performance of Jet Fuels for Supersonic Aircraft
 
650193
Helicopters and Propeller-Type VTOL Aircraft in the Light of Technologies
 
650115
High Temperature Hydrocarbon Fuels and Subsonic Flight Environments
 
650839
Higher Propulsive Efficiency in Subsonic Aircraft
 
650053
Historical Background
 
650809
Human Factors Challenges in Manned Space Flight
 
650575
HydroLogic Redundant Systems
 
650099
Improved Mission Capability and Economy via Regeneration
 
650241
Inertial Navigation System and Equipment Designs for Commercial Aviation
 
650198
Inlet Flow Field Studies for the Supersonic Transport
 
650828
Integrated Secondary Power System (ADS)
 
650788
Joining, The Real Challenge in Use of Advanced Structures
 
650386
Justification of Computer Use by a Small Aircraft Company
 
650831
LIFT FAN PROPULSION SYSTEMS V/STOL AIRCRAFT CONTROL
 
650201
Lift Engine Technology
 
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
 
650374
Management Ideas on the Real Value of Business Aircraft
 
650760
Metal Deformation in Macrosonic Fields
 
650384
Muffler Development for Light Aircraft and a Technique of In-Flight Data Acquisition and Analysis
 
650245
OPERATING EXPENSE FORECASTING FOR SCHEDULED AIRLINE SERVICES
 
650243
Operating Cost Objectives of V/STOL Aircraft for Commercial Airline Service
 
650214
Operating Procedures Associated with Noise Generated by the Supersonic Transport
 
650343
Operation and Maintenance Requirements for SST Hydraulic Systems
 
650251
Operational and Design Considerations of the Sweptwing Jet Transport in Turbulence
 
650383
Oxygen Usage in General Aviation
 
650389
Pressurization, Light Aircraft — Values and Controls
 
650790
Problems of Transition from Aluminum to Exotic Materials in Aerospace Structures
 
650056
Programming the System
 
650827
Progress in Constant Speed Drive Generating Systems
 
650147
Progress in Ultrasonic Metal Forming
 
650199
Propulsion Systems Sizing Criteria for the Supersonic Transport
 
650830
Reaction Control Systems for V/STOL Aircraft
 
650204
Realization of the SST Payload
 
650216
Recommended Practices for Use in the Measurement and Evaluation of Aircraft Neighborhood Noise Levels
 
650361
Redundant Damper Servoactuators for the F-111 Airplane
 
650100
Regenerators Enhance Patrol Aircraft Capability
 
650194
Research and Development of the Stowed Rotor V/STOL Concept
 
650778
Roll Diffusion Bonding, Potential Application to Aerospace Structures
 
650321
SNAP 50/SPUR Power Conversion System Objectives, Current Status, and Lunar Applications
 
650228
Safety and Reliability Through Design
 
650229
Safety and Reliability in Commercial Transport Aircraft
 
650242
Simulation Studies of the Supersonic Transport in the Air Traffic Control System
 
650784
Solution of the Airplane Minimum Time Problem by Huygens' Principle
 
650800
Some Procedures for Use in Performance Prediction of Proposed Aircraft Designs
 
650246
Some Technical Aspects of Advanced Subsonic Transport Aircraft
 
650328
Supersonic Transport Fluid Evaluation Program
 
650838
Surface Transportation Systems For Lunar Operations
 
650797
THE CHALLENGE OF THE PERFORMANCE SPECTRUM FOR MILITARY AIRCRAFT -- THE MEANING OF SPEED
 
650341
Technical Considerations in Designing a Hydraulic System for the SST
 
650366
Testing Techniques for Aircraft Reliability
 
650116
The Business Aircraft Operator in Transition to Turbine Equipment
 
650847
The Care and Feeding of All Weather Landing Systems in Airlines Service
 
650833
The Challenge of Alternate Approaches to the Achievement of Lunar Exploration and Exploitation
 
650789
The Challenge of Materials for the Supersonic Transport
 
650213
The Community Noise Characteristics of the Supersonic Transport
 
650785
The Cost/Weight Merit Function for Aerospace Hardware Design
 
650381
The Design and Development of the CJ610 Turbojet and the CF700 Turbofan Engines for Use in Business Jet Aircraft
 
650031
The Executive Operator in Transition to Turbine Powered Aircraft
 
650159
The Future of the Allison 250 Engine
 
650212
The Impact of Flight Operating Techniques Upon Engine Maintenance Costs
 
650224
The Landing Gear of the Lockheed SST
 
650835
The Manufacture of Propellants for the Support of Advanced Lunar Bases
 
650223
The Next Generation of Shorthaul Aircraft
 
650379
The Positive Displacement Supercharger and its Place in Aircraft Pressurization
 
650263
The Potential Effect of Regenerators on Army Aircraft
 
650203
The Propulsive Wing Turbofan V/STOL
 
650369
The Use of Off-the-Shelf Aircraft to Meet Army Requirements
 
650380
Turbocharging Aircraft Engine and Cabin
 
650762
Ultrasonics As Applied to Metal Forming and Assembly Processes
 
650215
United States Supersonic Transport Development Program - Sonic Boom and Noise Research
 
650054
Use of Computer Programs in Aircraft Design
 
650807
V/STOL Transport Aircraft for Air Cargo Operations
 
650087
VJ - 101 C Supersonic VTOL Program
 
650761
Vibrations — New Aid To Joining
 
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
 
640611
Aircraft Gas Turbine Engine Trend Analysis
 
640093
Aircraft Maintenance Programing
 
640488
Aircraft for Long Range and Long Endurance Missions
 
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
 
640430
COMPONENT DEVELOPMENT OF A LIQUID METAL COUPLED REGENERATOR SYSTEM FOR REGENERATOR AIRCRAFT ENGINES
 
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
 
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
 
640216
FUELS FOR THE SUPERSONIC TRANSPORT - A PROGRESS REPORT
 
640338
Flexible Wing, a Nonstop, Multiple Address, Aerial Delivery System
 
640508
Flight Testing the Boeing 727
 
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?
 
640055
Performance Requirements for Supersonic Transports
 
640818
Performance and Flying Qualities of the Double-Delta Supersonic Transport
 
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
 
640490
REQUIREMENTS FOR LONG RANGE -LONG ENDURANCE AIRCRAFT
 
640149
Recent Developments in Ultrasonic Metalworking Processes
 
640553
Results of an Airplane Reliability Program
 
640288
SST Fuels — A Major Airline Concern
 
640305
STOL Capabilities of VTOL Aircraft – Some Operating Parameters
 
640107
SYSTEMS SAFETY CONCEPTS FOR HIGH-PERFORMANCE BUSINESS AIRCRAFT
 
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
 
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
 
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
 
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
 
630036
Applications and Engineering Problems of VTOL - STOL Military Aircraft
 
630260
Breakerless High Frequency Ignition Systems for Reciprocating Aircraft Engines
 
630592
COMMERCIAL SUPERSONIC PROPULSION - MAINTAINABILITY BY DESIGN
 
630074
CONSIDERATIONS OF LIFT ENGINE INSTALLATIONS IN VTOL AIRCRAFT FROM THE VIEWPOINT OF THE AIRFRAME DESIGNER
 
630078
Characterization of Lunar Surfaces and Concepts of Manned Lunar Roving Vehicles
 
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
 
630452
Electron Beam Welding Techniques as Applied to Aerospace Structures
 
630250
Electron Beam Welding of Large Aerospace Structures with Portable Vacuum Chambers
 
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 & Whitney Aircraft J-57
 
630079
Instrumentation and Payload Design for Lunar Roving Vehicles
 
630566
LOGISTIC SUPPORT REQUIREMENTS FOR COMMERCIAL AIRLINE OPERATIONS
 
630001
LUNAR SURFACE CHARACTERISTICS
 
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
 
630456
Meteorology of the Supersonic Transport at Cruise Altitude
 
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
 
630273
SONIC BOOM & COMMUNITY RELATIONS
 
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
 
630407
Survey of Candidate Aluminum Materials for Supersonic Aircraft Applications
 
630090
THE DELIVERY SYSTEM AND PERFORMANCE REQUIREMENTS FOR A LUNAR ROVING VEHICLE
 
630243
THE EFFECTS OF SUPERSONIC TRANSPORT FLIGHT CHARACTERISTICS ON PERFORMANCE REQUIREMENTS
 
630567
TREND ANALYSIS AS APPLIED TO GAS-TURBINE ENGINES AND AIRCRAFT MECHANICAL EQUIPMENT
 
630276
The Aircraft Carrier as a Strike Warfare System
 
630483
The Application of Ultrasonic Energy to Metal Processing
 
630037
The Army VTOL Surveillance Aircraft Program
 
630396
The Cost of Landing an Airplane
 
630441
The Design and Development of a Prototype Landing Gear System for Aircraft to be Operated from Rough Unprepared Fields
 
630266
The Materials Used in Aerospace Applications for Plastics
 
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
 
620446
Aircraft Communications Electronic Signalling 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
 
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 Helicoptor 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 - (Report of Electrical Discharges Advisory Group, Aviation Fuel, Lubricant, and Equipment Research Committee of the Coordinating Research Council, Inc.)
 
620308
Extensions of the Lift/Thrust Engine Principle in V/STOL Aircraft
 
620343
Flight Control System Design for Supersonic Transport
 
620295
GMs — 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
 
620597
Introduction
 
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
Programed 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
 
620491
STRUCTURAL DYNAMICS ASPECTS OF THE MANNED LUNAR SPACE-VEHICLE LAUNCH-PHASE
 
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
 
620449
Supersonic Transports-Life in the Heat Thicket
 
620463
System Simplification Tools - An Airline Engineer's View of SST Reliability
 
620296
THE AEROELASTIC CHARACTERISTICS OF A JET-FLAP HELICOPTER ROTOR IN FORWARD FLIGHT
 
620350
THE ROLE OF NEW DEVELOPMENT IN FLUID POWER CONTROL FOR AEROSPACE SYSTEMS
 
620054
THE TREND TO TURBINES IN BUSINESS AIRCRAFT
 
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
 
620530
The Supersonic Transport - Required Characteristics of Configurations
 
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
 
610079
APPLICATIONS OF A NUCLEAR VEHICLE FOR A MANNED LUNAR LANDING
 
610005
Applications of Army-Navy Instrumentation Program to Transport Aircraft
 
610437
COOLING FOR HYPERSONIC AIRCRAFT STRUCTURES
 
610355
Contributions of Dyna-Soar To Space Flight Technology
 
610097
Effect of Inlet Normal Shock Position Control Systems on Range of Supersonic Transports
 
610165
FORECASTS FOR FLIGHT VEHICLE POWER
 
610443
HUMAN FACTORS OF THE LUNAR LOGISTICS MISSION
 
610101
Heat Transfer and Insulation Considerations for an External Expansion Ramjet with Specific Application to Mach 7 Flight
 
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
 
610478
LUNAR EXPLORATION SYSTEMS
 
610323
Lift-Thrust Turbofan Engines for VTOL and STOL Aircraft
 
610169
MECHANICAL, SONIC, ULTRASONIC, AND RADIATION STUDIES OF POLYMER-THICKENED OIL SHEAR CHARACTERISTICS
 
610016
Mach 3 Wing Structures Stiffened Skin versus Sandwich
 
610197
PAYLOAD - DENSITY - MECHANIZATION AS APPLIED TO ALL-CARGO AIRCRAFT
 
610341
Passenger Density and Accommodations as Factors in Supersonic Transport Design
 
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
 
610498
SUPERSONIC JET FUELS – QUALITY AND COST FACTORS
 
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
 
610096
Supersonic Trim Drag
 
610157
THE COMBINED TRANSONIC AXIAL AND CENTRIFUGAL STAGE COMPRESSOR
 
610482
THE COST OF LUNAR TRAVEL
 
610183
THE DEVELOPMENT OF STEEP GRADIENT AIRCRAFT FOR SHORT-HAUL TRANSPORTATION
 
610439
THERMAL RADIATION CONSIDERATIONS FOR ADVANCED FLIGHT VEHICLES
 
610158
TRANSONIC FLOW PROBLEMS IN CENTRIFUGAL COMPRESSORS
 
610311
The Air Force B-70 Valkyrie - An Example of Next Generation Aerospace Vehicles
 
610100
The Breguet Family of STOL Aircraft
 
610339
The Commercial Supersonic Transport — Some Operational Considerations
 
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
 
610250
Trends in Light Aircraft Structural Design
 
610358
Turbine Powered Transport Aircraft in the USSR
 
610010
U. S. Lunar Travel Program
 
610178
VTOL AIRCRAFT
 
600064
RADIATION EFFECTS STUDIES - for the development of radiation-resistant aircraft subsystems
 
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: PART I
 
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
 
600417
PROCESSING MISSILE FLIGHT VIBRATlOR DATA
 
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 PRESURE FUELING
 
600282
THE CANADAIR 44 - A BREAKTHROUGH CARGO AIRCRAFT
 
600371
THE PENALTIES OF NON-OPTIMUM FLIGHT OPERATIONS OF JET AIRCRAFT
 
600279
THE POTENTIAL OF NUCLEAR-POWERED AIRCRAFT FOR COMMERCIAL CARGO TRANSPORT
 
600363
THE X-15-A REACTION CONTROL AIRCRAFT
 
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
 
600045
preliminary design considerations for the Structure of a Trisonic Transport
 
590289
A PROPULSION SPECTRUM FOR VTOL AIRCRAFT
 
590301
A SYSTEMS APPROACH TO THE SUPPORT OF JET AIRCRAFT
 
590274
AIRCARFT 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
 
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
 
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
 
590012
Possibilities and Problems of Some high energy fuels for aircraft
 
590268
RADIATION SHIELDING ASPECTS OF NUCLEAR AIRCRAFT
 
590261
SOME VIEWS ON AIRCRAFT NUCLEAR PROPULSION
 
590207
SPACE TRAJECTORIES AND FLIGHT TEST OBJECTIVES
 
590177
THE AERODYNE - A NEW CONCEPT OF FLIGHT
 
590337
THE BISHOP'S BOYS: HUMAN ENGINEERING FOR THE FIRST FLIGHT
 
590290
THE EFFECT OF VERTICAL FLIGHT ON POWERPLANT DESIGN
 
590226
THE FUTURE OF AIRLINE GROUND TRANSPORTATION
 
590349
THE JT12 PRATT & WHITNEY AIRCRAFT'S 3000 LB. THRUST TURBOJET ENGINE
 
590050
The Buick Flight Pitch Dynaflow
 
590382
ULTRA HIGH SPEED AIRCRAFT AND MISSILE BALL BEARING APPLICATIONS
 
590069
design problems of VERY HIGH SPEED FLIGHT
 
590061
development of the SUPPRESSOR AND THRUST BRAKE FOR THE DC-8 AIRPLANE
 
590047
selection of Optimum Modes of Control for aircraft engines
 
590040
some thoughts on optimum combinations of Wings and Vertical Thrust Generators in VTOL Aircraft
 
590052
status of the SAE S-12 approach toVIBRATION ISOLATION of Aircraft Electronic Equipment
 
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 MACE AIRCRAFT
 
580375
CONVAIR'S NEW TRISONIC WIND TUNNEL
 
580370
DESIGN OF COMMERCIAL JET AIRCRAFT FOR SPECIFIC ROUTES
 
580169
DEVELOPMENTS IN AIRCRAFT TURBINE LUBRICANTS
 
580076
DEVELOPMENTS IN THE FIELD OF DIRECT-AIR-CICLE ARICRAFT NUCRAFT NUCLEAR PROPULSION SYSTEMS
 
580041
Designing with STEEL for Lighter Aircraft
 
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
 
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
 
580072
THE X-14 VTOL AIRPLANE - A DESIGN TOOL
 
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
 
570165
CORRELATION OF AIRFOIL ICE FORMATIONS AND THEIR AERODYNAMIC EFFECTS WITH IMPINGEMENT AND FLIGHT CONDITIONS
 
570017
Convertiplanes and Other VTOL Aircraft
 
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
 
570152
SYSTEMS ANALYSIS APPROACH TO FIREBEE FLIGHT CONTROL SYSTEMS DEVELOPMENT
 
570018
Some General Considerations Concerning VTOL Aircraft
 
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
 
570063
WHAT FUEL CHARACTERISTICS MEAN TO THE TURBINE ENGINE AIRPLANE
 
570108
WHAT OF THE (AIRCRAFT) FUTURE?
 
570009
Weld Repair of Aircraft Quality Magnesium Castings
 
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 MATER I ALS 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
 
560163
FORGINGS AND MODERN FIGHTER AIRPLANE PRODUCIBILITY
 
560090
FUEL BALANCE SYSTEM FOR SUPERSONIC AIRPLANES
 
560050
Flight Research at High Altitudes and High Speeds with Rocket-Propelled Research Airplanes
 
560293
GENERAL FUEL REQUIREMENTS FOR THE COMMERCIAL AIRCRAFT GAS TURBINE ENGINE
 
560285
HUMAN FACTORS THAT CAUSE AIRCRAFT ACCIDENTS
 
560089
HYDRAULIC AND PNEUMATIC PROBLEMS IN HIGH PERFORMANCE AIRCRAFT
 
560005
High-Temperature Problems Associated with the Use of Rubber in Aircraft
 
560096
INTEGRATED CONTROL SYSTEMS FOR AIRCRAFT
 
560281
INTEGRATED FLIGHT SYSTEMS
 
560085
NEW TOOLS TO LICK AIRCRAFT EQUIPMENT NOISE PROBLEMS
 
560266
PNEUMATIC vs. MECHANICAL POWER EXTRACTION FOR AIRCRAFT ACCESSORIES
 
560091
PROPELLERS FOR HIGH SPEED AIRCRAFT
 
560008
Pneumatic and Sonic Measurement of Combustion-Chamber Volume
 
560127
RADIOGRAPHIC INSPECTION IN AIRCRAFT STRUCTURE
 
560196
RADIOGRAPHY OF AIRCRAFT STRUCTURE FOR SAFETY AND ECONOMY
 
560075
SUPERSONIC AIR INLET CONTROLS
 
560276
SUPERSONIC BOMBER PROPULSION PROBLEMS
 
560046
Some Elevated Temperature Structural Problems of High-Speed Aircraft
 
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
ABC's of Ultrasonic Inspection
 
550179
AIR TRANSPORT DESIGN FOR THE HUMAN ELEMENT OF AIRLINE SERVICE AND MAINTENANCE PERSONNEL
 
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
 
550299
AN OIL COMPANY'S VIEWPOINT ON CIVIL AIRCRAFT TURBINE FUELS
 
550181
AUXILIARY POWER AND AIR CONDITIONING FOR THE SELF-CONTAINED AIRPLANE
 
550178
Air transport design for the human element of airline service and maintenance personnel
 
550253
Aircraft Noise Problem in Airport Vicinities
 
550255
An Airplane Manufacturer's Progress with Noise Suppression Devices
 
550247
Application of Airborne Radar to Airline Operations
 
550014
BEARINGS AND LUBRICANTS FOR AIRCRAFT TURBINE ENGINES
 
550250
Basic Facts about Noise as Related to Aviation
 
550302
ECONOMIC CONSIDERATIONS OF A JET TRANSPORT AIRPLANE
 
550188
ENVIRONMENTAL CONTROL ON A SUPERSONIC BOMBER
 
550064
EVALUATION OF THE NOISE FIELD AROUND JET-POWERED AIRCRAFT
 
550273
Effects of Operational Factors on Structural Fatigue in Fighter Aircraft
 
550268
Flight Load Measurements and Analysis
 
550066
HUMAN ENGINEERING ASPECTS OF AVIATION NOISE CONTROL
 
550168
INTEGRATION OF AIRCRAFT INSTRUMENTATION
 
550321
INTRODUCTORY TALK TO SEMINAR 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-PART I & PART II
 
550024
THE AIRCRAFT INDUSTRY IN CANADA
 
550075
THE ALLISON T56 TURBO-PROP AIRCRAFT ENGINE
 
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 FOR 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
RECTRACTABLE AIR INTLET 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
 
530163
COOLING ELECTRIC EQUIPMENT DURING SUPERSONIC FLIGHT
 
530214
Can the Airlines Use the Helicopter?
 
530148
Cold Weather Operation of Aircraft, 1953
 
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 STATUS
 
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
 
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
 
530001
THE STORY OF THE FIRST 50 YEARS OF AIRCRAFT ENGINES
 
530266
TITANIUM ALLOYS FOR AIRCRAFT ENGINE FORGINGS
 
530175
TURBO-PROPS VERSUS TURBO-JETS - AN AIRLINE VIEW
 
530223
Today’s Aluminum Aircraft Alloys
 
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
 
520038
CURRENT PLASTICS MATERIALS AND THEIR APPLICATION TO AIRCRAFT
 
520238
Characteristics of Propellers for Turboprop Airplanes
 
520117
DROP TESTING A LARGE AIRPLANE
 
520079
ECONOMICS OF NEW AIRCRAFT SELECTION
 
520073
FACILITIES AND EQUIPMENT FOR TESTING HIGH SPEED AIRCRAFT
 
520076
FLIGHT TEST AND FACILITIES FOR NAVAL AIRCRAFT
 
520110
FLIGHT TESTING OF PROTOTYPE ENGINES AS PRIMARY POWER PLANTS IN NEW AIRPLANES
 
520232
Flight Experience with Vickers Viscount Turbopropeller Airliner
 
520078
GOVERNMENT COLLABORATION IN AIRCRAFT DEVELOPMENT
 
520146
HELICOPTER AIRLINE 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
 
520148
LOWERING THE IGNORANCE FACTORS IN AIRPLANE WHEEL AND BRAKE DEVELOPMENT
 
520224
Low-Temperature Lubrication of Aircraft Engines
 
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
 
520088
STATIC-DISCHARGE PROTECTION FOR TRANSPORT AIRCRAFT
 
520229
Some Developments for Greater Crash Safety in Aircraft
 
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
 
520055
“STATISTICAL ASPECTS OF AIRLINE RESERVATIONS”
 
510094
AN INTRODUCTION TO THE AIRCRAFT TURBO-JET ENGINE
 
510074
APPLICATIONS OF CERAMIC COATINGS IN AIRCRAFT ENGINES
 
510166
Aircraft Ground Handling Characteristics As Required For Maximum Efficiency
 
510128
Aircraft Maintenance In Korea
 
510153
Airline Experience With Aircraft Engine Lubricating Oils
 
510075
CAN MAN SURVIVE PROLONGED FLIGHTS ABOVE 50,000?
 
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
 
510152
Flight Research Experience With Higher Engine Oil Temperatures
 
510146
GOVERNMENT RESPONSIBILITY IN AVIATION SAFETY
 
510131
General Design Aspects Of Turbo-Prop & Turbo-Jet Aircraft Fuel Systems
 
510004
German Aircraft Manufacturing Methods
 
510167
Local Service Aircraft And Engine Maintenance Requirements
 
510026
Observations On Flight Safety
 
510151
Operational Experience 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
 
510073
“FUTURE TRENDS IN AVIATION”
 
510170
“Flight Experience With Turbine Propeller Powered Aircraft”
 
510136
“High-Speed Pressure Refueling Of Aircraft”
 
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
 
500148
AIRPLANE WHEELS & BRAKES
 
500176
AUXILIARY GAS TURBINES for Pneumatic Power in Aircraft Applications
 
500016
Airplane Spray And Dust Application
 
500167
Compound Engine Systems for Aircraft
 
500019
Driving Aircraft Accessories Remotely From The Aircraft Engine
 
500060
FLIGHT CHARACTERISTICS AT HIGH MACH NUMBERS
 
500009
Fatigue Life Of Aircraft Engine Mounting Components
 
500151
Fuel And Lubricant Requirement 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
 
500057
INFLUENCES OF HIGH SPEED FLIGHT ON TURBO JET ENGINES
 
500127
Industrial Mobilization Planning With The Aircraft Industry
 
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 (Report of Aviation Fuels Division of Coordinating Fuel and Equipment Research Committee, CRC)
 
500058
SOME HIGH SPEED EXPERIENCE WITH FIGHTER TYPE AIRPLANES
 
500059
SOME NOTES ON HIGH SPEED FLIGHT PROBLEMS
 
500040
SUPERSONIC AND TRANSONIC AIRCRAFT PROBLEMS
 
500026
Some Developments For Safer Aircraft
 
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
 
490173
ATOMIC POWER And Aircraft Propulsion
 
490115
Aircraft Decelostat - A Device For Wheel Slide Protection
 
490067
Aircraft Evacuation On Land - Equipment, Stowage, And Procedure
 
490182
DESIGN CHARTS for Longitudinally Stiffened Wing Compression Panels
 
490206
DYNAMIC LOADS ON AIRPLANE STRUCTURES
 
490212
Design of Aircraft Structures For “Mass Production”
 
490069
Flight Testing The Wright Typhoon Turbo-Prop
 
490071
Fuel Systems And Carburetors For Personal Aircraft
 
490161
Getting the BEST out of our NEW TRANSPORTS
 
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
 
490123
ROCKET AND RAMJET SUPERSONIC POWERPLANTS
 
490019
Refuelling In Flight
 
490072
Review Of Transport Aircraft Developments During The Past Two Years And Some Predictions For The Future
 
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
 
480166
COMPLETE DESIGN PANEL - WHAT WILL BE THE POSSIBLE CHANGES IN THE CIVIL AIR REGULATIONS WHICH WILL INFLUENCE THIS 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
 
480100
Engineering Developments Required For Satisfactory Low Temperature Aircraft Engine Operations (Extract)
 
480189
FUEL INJECTION versus CARBURETION for Personal Airplane Engines
 
480049
Factors Affecting The Selection Of Propellants For Rocket Powered Aircraft
 
480222
Flight BEYOND The Earth's Atmosphere
 
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
 
480181
LONGITUDINAL CONTROL SYSTEM FOR HIGH-SPEED AIRCRAFT
 
480038
Lightning Effects On Aircraft
 
480221
PREIGNITION And Its Deleterious Effects in Aircraft Engines
 
480029
Practical Aspects Of Reverse Thrust Propellers In Airline Operation
 
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
 
480228
THE RAMJET as a Supersonic Propulsion Plant
 
480048
The Design And Development Of Rocket Engine Powerplants For Aircraft
 
480106
“The “Sleeperette” - A New Concept Of Comfort For Airline Passengers”
 
470233
AIRCRAFT DETONATION INDICATORS
 
470112
AIRCRAFT POWER PLANT PROBLEMS
 
470058
AMERICAN AIRLINES… EVALUATION OF AIRBORNE RADAR
 
470030
Aircraft Engine Starters
 
470218
Aircraft-Engine Starting Tests and Experiences in the Arctic
 
470145
An Analysis Of Composite-Powered Aircraft
 
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
 
470137
Cargo Aircraft Requirements
 
470141
Civil Aeronautics Administration Aircraft Fire Prevention Developments
 
470039
Cold Weather Operation Of Aircraft Power Plants By The United States Navy
 
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 COLLISION OF BIRDS WITH AIRCRAFT IN SCHEDULED COMMERCIAL OPERATIONS IN THE CONTINENTAL UNITED STATES
 
470159
Development of Functional Cockpits for Naval Aircraft
 
470168
ELECTRICAL POWER AND THE TRANSPORT AIRPLANE
 
470253
Effect of C. A. R. Performance Requirements on Airplane Design
 
470153
Engines For Light Aircraft
 
470117
Evaluation Of Light Aircraft Engine Lubricants
 
470229
Experiences of an Aircraft Manufacturer with Sandwich Material
 
470240
FUTURE TRENDS IN AIRCRAFT-ENGINE DESIGN
 
470189
Fuel Injection For Light Aircraft
 
470099
Future Power For The Personal Airplane
 
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
 
470053
Rocket Engines as Applied to Future Aircraft Powerplants
 
470101
SUPERCHARGING, HANDLING AND LOADING CHARACTERISTICS OF THE DC-6 AIRPLANE
 
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
 
470087
THE PILOT VERSUS SUPERSONIC SPEEDS
 
470160
The Development Of Naval Aircraft
 
470166
The Experimental Determination Of Strains In Aircraft Landing Wheels And Brakes
 
470135
The Problems Of Noise Reduction From An Airplane Design Standpoint
 
470075
The Relationship Of Aircraft Detail Design To Tooling And Manufacturing Costs
 
470130
The determination of the optimum airplane-power plant combination
 
470193
Transport Aircraft Powerplant Outlook For 1947
 
470097
WHY PNEUMATICS??? OR THE CASE FOR PNEUMATICS FOR INTERMITTENT SERVICES ON AIRCRAFT
 
470098
“Reduce Airplane Noise Through Basic Design”
 
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
 
460239
AIRCRAFT GAS TURBINES with CENTRIFUGAL COMPRESSORS
 
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
 
460199
AVIATION GAS TURBINE INSTALLATION PROBLEMS
 
460122
Aircraft Engine Induction System Deposits
 
460059
Airline Scheduling
 
460118
An NACA Flight and Wind Tunnel Investigation of Maximum Lift as Affected By Variations of Mach and Reynolds Numbers
 
460207
Application of TURBOSUPERCHARGERS to POSTWAR COMMERCIAL AIRCRAFT
 
460203
Aviation Fuels-What the Airlines WANT and EXPECT
 
460255
DESIGN AND TEST EXPERIENCE WITH MONOCOQUE MAGNESIUM WINGS
 
460151
DESIGN OF A TRANSPORT AIRPLANE ELECTRICAL SYSTEM
 
460190
DESIGN REQUIREMENTS FOR PICKUP AIRCRAFT
 
460143
DEVELOPMENT OF CHROME PLATED PISTON RINGS FOR AIRCRAFT ENGINES
 
460175
Design Trends In Aircraft Exhaust Systems
 
460217
Development and Application of HEATED WINGS
 
460260
ECONOMICS OF AIRLINE FUEL UTILIZATION
 
460013
ELECTRICAL EQUIPMENT FOR PERSONAL AIRPLANES
 
460254
Evolution of a New “Workhorse” Airplane for the Airlines
 
460107
FACTORS AFFECTING THE DESIGN OF THE AIR CONDITIONING AND PRESSURIZING SYSTEM FOR THE REPUBLIC RAINBOW AIRPLANE
 
460134
FLIGHT TESTS OF AVIATION OILS
 
460243
FUEL SENSITIVITY and ENGINE SEVERITY in Aircraft Engines
 
460205
Factors Pertaining to Installation of Inverted, In-Line AIRCOOLED AIRCRAFT ENGINES
 
460250
Factors Relative to Selected STALLING-SPEED REGULATIONS FOR TRANSPORT AIRPLANES
 
460209
Factors in AERATION and DEAERATION of AIRCRAFT-ENGINE OIL
 
460060
For Whom the Bell Tolls (Notes on Safety in Airline Operations)
 
460237
GAS TURBINES AND AIRCRAFT
 
460233
GERMAN AIRCRAFT and HYDRAULIC SYSTEMS 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
 
460181
Mechanical Design Considerations Influencing Blading Performance In Aircraft Gas Turbine Power Plants
 
460061
NACA Study of the Utilization of Exhaust Gas of Aircraft Engines
 
460252
PLANNING CABIN INTERIORS for TRANSPORT AIRCRAFT
 
460040
POSSIBILITIES OF REALLY HIGH-SPEED FLIGHT
 
460141
POSTWAR AIRCRAFT INDUSTRY CASHES IN ON WARTIME EXPERIENCE
 
460165
Passenger Aircraft Facilities - Design And Operation
 
460158
Pneumatic Tires For Modern Airplanes
 
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 VS. RANGE CHARACTERISTICS ON TRANSPORT AIRCRAFT EFFICIENCY
 
460065
SUPERSONIC INSPECTION OF MATERIALS AND PARTS
 
460156
Some Requirements of a “Feeder” Airplane
 
460257
Stability Problems With Swept Wings
 
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
 
460012
“DEVELOPMENT OF THE BEECH BONANZA LIGHT FOUR-PLACE HIGH PERFORMANCE AIRPLANE”
 
460110
“Liquid Cooled Engine Power Plants for Transport Aircraft”
 
460127
“METHOD OF OBTAINING OPTIMUM AIRCRAFT UTILIZATION - DOMESTIC AND OVERSEAS”
 
450086
A RESUME OF DESIRABLE CHARACTERISTICS FOR NON-STALLING NON-SPINNING AIRPLANES
 
450097
A report on the nature of ice formation on aircraft as related to airline operations
 
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
 
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 vs CENTRIFUGAL SUPERCHARGERS for Aircraft Engines
 
450078
Aircraft Accessories FOR 400 CYCLE MOTOR OPERATION
 
450213
Aircraft-Engine GEARS
 
450056
BOND TESTING OF SILVER PLATED AIRCRAFT ENGINE PARTS
 
450165
Basic Principles of POWER BOOST FLIGHT CONTROLS
 
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
 
450150
DISCUSSION ON “WEIGHT REDUCTION OF AIRCRAFT BRAKING SYSTEMS THROUGH THE USE OF REVERSE THRUST PROPELLERS”
 
450077
Discussion on “Defining the Market for Aircraft for Local Air Transport Service”
 
450143
ECONOMIC STATUS OF THE AIRPLANE IN THE POSTWAR MARKET
 
450022
ELECTRONIC CONTROLS IN AIRCRAFT
 
450112
ENGINEERING PROBLEMS IN THE DEVELOPMENT OF A SMALL TRANSPORT AIRPLANE DESIGN
 
450203
Electronic Analysis of Airplane Hydraulic Braking Systems
 
450003
FLIGHT ENGINEER STATION DESIGN AND REQUIREMENTS
 
450144
FLIGHT EQUIPMENT REQUIREMENTS FOR THE FEEDER AIRLINE
 
450006
FLUORESCENT LIGHTING FOR COMMERCIAL AIRPLANE INTERIORS
 
450135
FUELING A HALF FORGOTTEN BIT OF AIRCRAFT DESIGN
 
450044
FUTURE AIRCRAFT ELECTRICAL LOADS
 
450178
Fuel Injection for the Aircraft Engine
 
450076
General discussion of factors relative to selected stall speed regulations for transport airplanes
 
450237
High - Conductivity Cooling Fins for Aircraft Engines
 
450049
High Frequency Aircraft Ignition System with Low Tension, Low Frequency Distribution
 
450180
High-Altitude Factors in Flight Testing
 
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
 
450125
MODERN AIRCRAFT REFUELING
 
450090
MORE LANDING FACILITIES - THE KEY TO PRIVATE AVIATION'S GROWTH
 
450189
Military Aircraft GREASE LUBRICATION
 
450185
New Aspects of AIRLINE AIRCRAFT MAINTENANCE
 
450079
PROTECTION OF ELECTRICAL SYSTEMS ON MILITARY AIRCRAFT
 
450008
PSYCHOLOGICAL REQUIREMENTS FOR AIRCRAFT PASSENGER DESIGN
 
450151
Possibilities of AIRCRAFT STRUCTURES in Ground Vehicles
 
450091
Post-War Aviation Development and Prospects
 
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
 
450123
SOME BASIC PRINCIPLES OF AIRCRAFT MAINTENANCE ECONOMICS
 
450066
SOME OBSERVATIONS ON THE FINANCING OF AIRCRAFT FOR LOCAL AIR TRANSPORT
 
450224
Some Advantages and Limitations of CENTRIFUGAL and AXIAL AIRCRAFT COMPRESSORS
 
450014
THE APPLICATION OF HEAVY DUTY ADDITIVES TO AVIATION OILS
 
450012
THE DETECTION OF DETONATION AND OTHER OPERATING ABNORMALITIES IN AIRCRAFT ENGINES BY MEANS OF SPECIAL INSTRUMENTATION
 
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
 
450169
The FUNDAMENTALS of FLIGHT-INDUCED and FORCED COOLING
 
450149
WARTIME AIRCRAFT SERVICE PROBLEMS ------THEIR SOLUTION
 
450233
WOOD vs METAL CONSTRUCTION IN AIRCRAFT
 
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
 
450063
“FUTURE TRENDS IN INTERCONTINENTAL TRANSPORT AIRCRAFT”
 
450105
“Naval Aviation Today in the Pacific”
 
450118
“SERVICE EXPERIENCE WITH LIGHT AIRCRAFT ENGINES”
 
450092
“The Design and Development of Large Post-War Transport 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
 
440039
AIRCRAFT ENGINES IN TANKS
 
440002
AIRCRAFT ENGINES, AND THEIR ACCESSORIES
 
440090
AIRCRAFT ENVIRONMENT, THERMAL EFFECTS
 
440115
AIRCRAFT MANUFACTURING AND AIR TRANSPORT
 
440011
AIRCRAFT POWERPLANT DEVELOPMENT TESTING
 
440197
ALTITUDE VAPOR FORMATION in Aircraft Fuel Systems
 
440094
ANALYTICAL FUEL RESERVE SYSTEMS FOR LONG RANGE AIRCRAFT
 
440167
Aircraft-Engine - INLET and EXHAUST PORTING
 
440203
An Investigation of CHAFING on AIRCRAFT-ENGINE PARTS
 
440127
CARGO AIRPLANE ACCESSORIES
 
440120
COCKPIT LIGHTING OF TRANSPORT AIRCRAFT
 
440043
COLD WEATHER OPERATION OF AIRCRAFT
 
440117
CONVERTING MILITARY AIRCRAFT FOR COMMERCIAL USE
 
440099
CRUISING CONTROL OF TRANSPORT AIRCRAFT
 
440056
CURRENT TRENDS in AIRCRAFT POWER PLANTS
 
440086
Co-ordination of Flight Deck Duties on Large Airplanes
 
440154
Comparison of HYDRAULIC and ELECTRICAL ACCESSORY SYSTEMS in AIRCRAFT
 
440179
DESIGN CONSIDERATIONS of the CARGO AIRPLANE
 
440119
EFFECT OF AIRPLANE DESIGN ON AIR TRANSPORT MAINTENANCE
 
440014
EXPERIMENTAL FLIGHT TESTING FROM THE ENGINE MANUFACTURER'S VIEWPOINT
 
440150
Experience with the Use of MAGNESIUM in AIRCRAFT
 
440181
FLIGHT TESTING with a PROPELLER THRUSTMETER
 
440213
FUNDAMENTALS of AIRPLANE DESIGN
 
440171
Fundamental Requirements of POST-WAR TRANSPORT AIRPLANES
 
440100
HUMIDITY EFFECTS ON AIRPLANE EQUIPMENT PERFORMANCE
 
440153
How Will the 100-Octane Aviation Gasoline Program Affect Post-War Motor Gasoline?
 
440187
MEASUREMENT and PREDICTION of AIRCRAFT VIBRATION
 
440133
MECHANIZED HANDLING OF AIRPLANE CARGOS
 
440087
METALLURGICAL CONTROL OF AIRCRCRAFT FORGINGS
 
440061
METLBOND - A METAL ADHESIVE FOR AIRCRAFT
 
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
 
440036
PROPELLER EFFICIENCY OF A LIGHT AIRPLANE
 
440211
PROPELLER and GEAR RATIO REQUIREMENTS for Aircraft Designed for Cruising Operation
 
440101
RADIO INTERFERENCE AND THE AIRCRAFT ENGINE
 
440210
RECENT TRENDS in AIRPLANE ICE-PREVENTION TECHNIQUE
 
440136
REQUIREMENTS OF THE FEEDER LINE AIRPLANE
 
440001
SPEECH TO THE METROPOLITAN SECTION OF THE SOCIETY OF AUTOMOTIVE ENGINEERS ON 6 JANUARY 1944, SUBJECT, “DESIGN OF AIRCRAFT AND ITS RELATED ACCESSORIES FROM A MAINTENANCE VIEWPOINT”
 
440190
STRUCTURAL FLIGHT RESEARCH
 
440175
SYNTHETIC RUBBER APPLICATIONS on Aircraft Engines
 
440201
Some Aircraft-Engine PRODUCTION METHODS
 
440198
Studies of Fuels and Fuel System Phenomena Contributing to AVIATION VAPOR LOCK
 
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
 
440205
The DESIGN of SHEET for PRODUCTION METAL AIRCRAFT PARTS
 
440089
The Development and Use of Plastic Materials for Aircraft Construction
 
440207
The INTERCOOLING PROBLEM in AIRPLANE DESIGN
 
440097
The design of the DC-4/C-54 airplane
 
440034
USEFULNESS OF SAE TO THE AVIATION INDUSTRY
 
440007
“LOW-COST CYLINDER DESIGN FOR COMMERCIAL AIRPLANE ENGINES”
 
440025
“STUDY OF THE ADVANTAGES OF COMPRESSION”IGNITION ENGINE FOR AVIATION USE, AND A POSSIBLE SOLUTION.”
 
430022
A METHOD OF APPLYING PRODUCTION DESIGN TO AIRCRAFT
 
430141
AIRCRAFT ACCESSORY SYSTEM
 
430055
AIRCRAFT ELECTRIC REMOTE CONTROLS
 
430052
AIRCRAFT HYDRAULIC REMOTE CONTROLS
 
430162
AIRCRAFT OIL SYSTEMS HIGH - ALTITUDE PROBLEMS
 
430030
AIRCRAFT STRUCTURAL TESTING
 
430056
Aircraft manufacturing problems
 
430013
Aircraft service in combat areas
 
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
 
430025
CO-DESIGNING AIRCRAFT POWER PLANTS
 
430078
CONVERTING TODAY'S MILITARY AIRPLANE TRANSPORTS FOR POST WAR PASSENGER AND CARGO USE
 
430027
Chevrolet's aviation engine test plant~Its organization, development and operation
 
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 0F 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 Simulation Altitude Conditions From Sea Level to 40,000 Feet
 
430077
PHILOSOPHY OF FLIGHT TESTING
 
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
 
430024
THE EFFECT OF ENVIRONMENT ON AIRCRAFT ENGINE DESIGN AND PERFORMANCE
 
430062
THE FUTURE OF AVIATION
 
430153
The POSSIBILITIES of SHAVED GEARS for AIRCRAFT ENGINES
 
430150
The Use of PETROLEUM PRODUCTS in AIRCRAFT
 
430098
The age of cargo flight
 
430051
Training Operators for Aviation Engine Testing
 
430072
“POST WAR COMMERCIAL AVIATION”
 
430040
“STRATEGIC MATERIALS - AIRCRAFT PRODUCTION AND DESIGN”
 
420087
AIRCRAFT CARBURETOR AIRSCOOPS on FUEL-AIR and Their Effect METERING in Flight
 
420131
AIRCRAFT-ENGINE RADIO SHIELDING
 
420054
AIRPLANE DESIGN FOR CARGO TRANSPORTATION
 
420003
AVIATION POWER PLANTS
 
420073
Advantages and problems of diesel power in aircraft
 
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
 
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
 
420019
“FLOW PRODUCTION” AS APPLIED TO THE MANUFACTURING OF AIRCRAFT EXHAUST COLLECTOR SYSTEMS
 
420074
“PROPELLER CONTROL and ITS RELATION to POWER in AIRCRAFT ENGINES”
 
410002
AIRCRAFT CYLINDER FINISHES
 
410101
AIRCRAFT ELECTRICITY as the Airline Operator Sees It
 
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
 
410089
Aircraft-Engine REDUCTION GEARS and TORQUE METERS
 
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
 
410095
SUPERCHARGED Aircraft Ignition Harnesses
 
410006
Some Factors Influencing Aircraft Engine-Propeller Vibrations
 
410118
Standardization of AIRCRAFT - ENGINE COMPONENTS
 
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
 
410137
The ALLISON AIRCRAFT-ENGINE DEVELOPMENT
 
410086
The C.U.E. Cooperative Universal Engine for Aviation Single-Cylinder Research
 
400063
AIRLINE MAINTENANCE
 
400166
ALTITUDE and the Aircraft Engine
 
400110
AVAILABILITY AND CHARACTERISTICS OF AVIATION SAFETY FUELS
 
400142
Aluminum Aircraft Fuel Tanks
 
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
 
400153
EXPERIENCE in Integral Aircraft Fuel-Tank Construction
 
400152
Economic Aspects of LIGHT AIRPLANE ENGINES …
 
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
 
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
 
400145
Shortcomings of Mica Insulation for Aviation Spark Plugs
 
400150
Status of Fuel Performance Tests in Aviation Engines
 
400104
THE STANDARDIZATION PROBLEM IN THE AIRCRAFT INDUSTRY
 
400001
TRANSPORT AIRCRAFT - PAST - PRESENT AND FUTURE
 
400170
The Performance of MODERN AIRCRAFT DIESELS
 
400062
The progress of the aircraft diesel
 
400120
VOLATILITY DECREASES AND AVAILABILITY OF HIGH KNOCK RATING AVIATION FUELS
 
400112
“CERAMIC SPARK PLUGS RE-ENTER AVIATION”
 
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
 
390089
AIRPLANE BRAKE INSTALLATION and CONTROL CONSIDERATION
 
390181
Aircraft Engines and Their Lubrication
 
390121
Aircraft-Engine Lubrication
 
390136
Aircraft-Engine Valve Mechanisms
 
390155
Airline Power Control with a Torque Meter
 
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
 
390107
PROBLEMS IN AIRCRAFT ACCESSORY DRIVES
 
390160
Permissible Amplitudes of Torsional Vibration in Aircraft Engines
 
390157
Prospects for Use of “Safety Fuels” in Spark-Ignition Aircraft Engines
 
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
 
390012
TRANSPORT AIRPLANE DEVELOPMENT WITH PARTICULAR REFERENCE TO THE CURTISS-WRIGHT TWENTY
 
390149
Ten Years' Service Experience with Alclad Materials in Aircraft
 
390169
The Analysis of Leading-Edge Wing Beams
 
390134
The BMEP Parameter for Airplane Cruising-Power Control
 
390175
The Testing of Large Aircraft
 
390179
Transatlantic Airplane Design
 
390185
Vibration Characteristics of Aircraft Engine-Propeller Systems
 
390068
“ACCELERATED AIRCRAFT PRODUCTION FOR NATIONAL DEFENSE AND SOME OF ITS EFFECTS ON ORGANIZATION AND PERSONNEL.”
 
380020
A SURVEY OF MECHANICAL FAILURES OF AIRCRAFT DURING 1936-1937
 
380072
ADAPTATION OF PUMPS TO AIRCRAFT SERVICE
 
380112
AIRCRAFT FUELS
 
380029
ANALYSIS OF IMPROVEMENTS IN AVIATION SPARK PLUGS
 
380146
Airplane Performance Calculations by Means of Logarithmic Graphs
 
380111
BASIC PROBLEMS IN THE DESIGN OF HIGH-OUTPUT AIRCRAFT ENGINES
 
380018
ENGINES FOR LIGHT AIRPLANES
 
380143
Engine Installation and Related Problems in Large Aircraft
 
380124
Flight-Testing with an Engine Torque Indicator
 
380081
HIGH FLIGHT ENGINEERING
 
380046
Investigation of Vapor Lock in Aviation Fuel Systems; C.F.R. Progress Report--
 
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 - Completion of First Program and Progress on Second Program-Report of the Cooperative Fuel Research Committee
 
380017
STAINLESS STEEL FOR AIRCRAFT
 
380028
THE AIR-TRACK SYSTEM OF AIRCRAFT INSTRUMENT LANDING
 
380032
THE EFFECT OF OIL CHARACTERISTICS ON WEAR IN AVIATION ENGINES.
 
380074
THE LIGHT AIRPLANE FOR PRIVATE OWNER
 
380140
The Accessory-Drive Problem of Aircraft Engines
 
380137
The Diesel as a High-Output Engine for Aircraft
 
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
 
370021
DESIGN TRENDS IN FRENCH AIRCRAFT ENGINES AND PROPELLERS
 
370193
Design of Cowlings for Air-Cooled Aircraft Engines
 
370086
EUROPEAN AIRCRAFT PRODUCTION EQUIPMENT
 
370180
Engine and Laboratory Tests of Stability of Aviation Oils
 
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 CF TRANSPORT AIRPLANES
 
370161
Lubrication and Cooling Problems of Aircraft Engines
 
370108
PLASTICS IN THE AIRCRAFT INDUSTRY
 
370145
Plant Layout and Production Methods for Modern Aircraft Engines
 
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
 
370109
“MAINTENANCE PROBLEMS OF ARMY AIRPLANES”
 
360035
AIRCRAFT ENGINE PISTON RING AND CYLINDER WEAR
 
360132
Air-Cooled Radial Aircraft-Engine Installation
 
360121
Air-Cooled Radial Aircraft-Engine Performance Possibilities
 
360075
DESIGNING AND BUILDING FOR THE COMMERCIAL AIRCRAFT MARKET
 
360083
DESIGNING FOR THE USE OF ALUMINUM ALLOY FORGINGS AND EXTRUSIONS IN AIRCRAFT PRODUCTION
 
360129
Design of Two-Engined Aircraft
 
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 AIRPLANE SERVICE
 
360112
Rating Aviation Fuels-in Full-Scale Aircraft Engines - A report of the Cooperative Fuel Research Committee
 
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
 
360012
“CARBURETOR ICING IN AIRLINE OPERATION”
 
350100
A Designer-Manufacturer Viewpoint of Transport-Aircraft Needs
 
350045
AIRCRAFT STRUCTURAL DESIGN AND ITS INFLUENCE ON OTHER ENGINEERING DESIGN.
 
350112
Aircraft Spark-Ignition Versus Compression-Ignition Engines
 
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 & TECHNICAL PROBLEMS OF PRIVATE COMMERCIAL AIRPLANES
 
350097
The Influence of Engine Oils on Aircraft-Engine Performance
 
340070
AIRCRAFT INSTRUMENTS AND THEIR USES
 
340076
Acoustics and the Airplane
 
340081
Aerodynamics of Wing Sections for Airplanes
 
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
 
340071
THE MEASUREMENT OF LANDING SPEED AND OTHER FLIGHT TEST PROCEDURE
 
340107
The Airplane Landing-Gear Shock-Absorbing System
 
340089
The Cowling and Cooling of Radial Air-Cooled Aircraft Engines
 
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 ALLMETAL 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 NAVY1
 
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
 
190064
THE AIRPLANE AS A COMMERCIAL POSSIBILITY
 
190062
THE HORSEPOWER OF RESISTANCE IN AIRPLANE DESIGN
 
190020
THE LIBERTY AIRCRAFT ENGINE
 
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
 
180041
THE FUTURE OF THE AIRPLANE BUSINESS
 
180050
THE HISPANO-SUIZA AIRCRAFT ENGINE
 
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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