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SAE International

SAE Papers

Paper Number Paper Title Book Number
2009-01-3127 A Flexible Wing Unmanned Aerial Research System
2009-01-3221 A Simulation Environment for Evaluating Image Processing Techniques for UAV Applications
2009-01-3100 A UAV Pilot's Associate
2009-01-3249 Acoustic Vector Sensors Increasing UAVs Situational Awareness
2009-01-3097 Constrained Control of UAVs Using Adaptive Anti-Windup Compensation and Reference Governors
2009-01-3126 Control and Simulation of a Ducted Fan VTOL UAV
2009-01-3166 Design and Experimental Investigation of a Small UAV
2009-01-3272 Design of Adaptive Airfoil Control for Unmanned Aerial Vehicles using Smart Materials
2009-01-3098 Intelligent Combat Maneuvers for Unmanned Combat Air Vehicles
2009-01-3209 Model-Based Design and Automatic Production Code Generation for Safety-Critical Software Development
2009-01-3125 Monitoring the Spread of a Plant Pathogen in the Lower Atmosphere Using Unmanned Aerial Vehicles and a Buoyancy-Controlled Weather Balloon
2009-01-3167 Stability of Highly Flexible Unmanned Aerial Vehicles
2009-01-3099 Standardized Interfaces for the Next Generation of Weapons for Unmanned Systems: Miniature Munition Store Interface vs. Interface for Micro Munitions
2009-01-3128 Structural and Aerodynamics Analysis on Different Architectures for the Elettra Twin Flyer Prototype
2009-01-3196 Structural and Manufacturing Considerations for a Research Unmanned Aerial Vehicle
2009-01-3250 The Joint Architecture for Unmanned Systems, A Set of SAE Interoperability Standards
2009-01-3129 UAV Operation, Crash Analysis and Measurement of Particle Concentrations above a Forest and Surrounding Farmland
2008-01-2234 Active Vortex Generators Using Thrust Vectoring Plasma Actuators V117-2008
2008-01-2275 Aerodynamic Comparison of Tilt-Rotor, -Wing and -Body Concept for Multi Task MAVs
2008-01-2253 Aircraft Performance Prediction: Comparison of Classical Handbook Methods to Detailed Time Integration Computer-Aided Methods V117-2008
2008-01-2254 Cost Benefits of Aerodynamic Data Generation Techniques for Aircraft Stability and Control Analysis Using the J2 Universal Tool-Kit V117-2008
2008-01-2271 Dynamic Taxonomies Usage in the Context of Aeronautical Maintenance Processes to Increase Effectiveness and the Efficiency of the Operations SP-2212
2008-01-2272 Finite Element Modeling Strategies for Dynamic Aircraft Seats SP-2212
2008-01-2225 Going Green: What's In It For General Aviation?
2008-01-2265 Having 5000 Destinations in the Modern U.S. Airways System
2008-01-2242 Hybrid Propulsion System Design of a VTOL Tailsitter UAV SP-2211
2008-01-2231 Hybrid Rigid/Inflatable Wings for Low Volume Wing Storage SP-2211
2008-01-2238 Importance of Unmanned Air Vehicles SP-2211
2008-01-2263 Jam-Free, Fail-Safe Flight Control System with Asymmetric Load Alleviation Capability SP-2214
2008-01-2262 Keys to Success with Knowledge-based Techniques SP-2212
2008-01-2230 Model-Driven Architecture for Platform and Store Design SP-2212
2008-01-2270 Modern Solutions for Ground Vibration Testing of Small, Medium and Large Aircraft V117-2008
2008-01-2243 Nimbus Meta-plane, a New Aerodynamic Concept for Unmanned Hybrid Aerial Vehicle Application SP-2211
2008-01-2232 Operational Loads Monitoring of a Fleet of Beech 1900D Aircraft V117-2008
2008-01-2266 Outsourcing Aircraft Maintenance
2008-01-2244 Plasma Micro-thrusters for Micro Aerial Vehicles SP-2211
2008-01-2237 Robust Control Design for a Flexible Unmanned Aerial Vehicle SP-2211
2008-01-2264 The Seven Parameters of Highly Effective Cable Control Systems V117-2008
2-28-6-28 Going green to stay in the black
2-28-5-26 From concept in mind to product in hand
2-28-1-36 Light material brings heavy challenges
2-27-10-20 Older-older vs. newer-older: room for both
2-27-9-20 Global collaboration is in the air
2-27-9-12 Let's get digital
2007-01-3908 A New Simulation Technique Using a Holistic Approach and Methodology to Assess Productivity of a New Plant for Manufacturing the Boeing 787 V116-2007
2007-01-3925 A Software Method for Demonstrating Validation of Computer Dummy Models Used in the Evaluation of Aircraft Seating Systems V116-2007
2007-01-3847 Aerionics - A New Aero Industry for Flight Control
2007-01-3910 Balloon Launched UAV with Nested Wing for Near Space Applications
2007-01-3845 Coordinated Autonomous UAVs: Applications for a Heterogeneous Urban RSTA Team
2007-01-3930 Development of a Small Long Endurance Hybrid PEM Fuel Cell Powered UAV
2007-01-3926 Developments in Hole-to-Hole Assembly V116-2007
2007-01-3844 Dynamic Target State Estimation for Autonomous Aerial Vehicles using a Monocular Camera System
2007-01-3911 Expanding the Small UAV Design Space with Inflatable Wings
2007-01-3907 Identify/Utilize Process Capability Information to Predict Variation in Aircraft Early Design
2007-01-3912 Image Exploitation System for Airborne Surveillance
2007-01-3810 Literature Data and Corrosion Testing of Hard Anodized and Duplex Sealed 7075-T7351 and 7050-T7451 Wrought Aluminum Alloy Plates after Cyclic Loading
2007-01-3846 Mission Planning for UAV Sensing Tasks in Close Proximity Environments
2007-01-3809 Re-Engineering, Austempering, and Selective Laser Hardening of a 4340 Latch Body used in the Cargo Hook of a CH-47 Military Helicopter
2007-01-3927 Reducing Design Time, Part Cost, and Manufacturing Risk on New Airplane Projects Using Intelligent Software Solutions
2007-01-3929 Robust Control Design for a Flexible Unmanned Aerial Vehicle
2007-01-3922 Safety and Certification of UAVs
2007-01-3928 The Selection and Qualification of a Parachute Recovery System for Your UAV
2-27-2-12 Management promotes sharing
2-27-1-16 On-wing designs
2005-01-3148 Aircraft Airfoil Assembly and Method
2005-01-3166 Development of a Radio-Controlled Ornicopter: a Single Rotor Helicopter Without Reaction Torque
2005-01-3168 Inclusion of the Rotor Speed Degree of Freedom for Substantial Increases In Advanced Rotorcraft Performance and Safety
2005-01-3185 Springtail Efv/Dragonfly Umr
2005-01-3184 The Operational Potential of Manned, Ducted-Fan VTOL Vehicles
2005-01-3153 Unsteady Fuselage Loads on Rotorcraft in Ground Effect
2-25-2-17 Collaboration Off the Shelf
2-25-1-29 A Rounded View of Fibers
2-25-10-16 All Things to All Operators
2-26-6-30 Better seen, not heard
2-26-4-26 Breaking records via fuel management
2-26-2-20 Collaborating on Takeoff
2-26-1-13 Dassault--Business Aviation Pioneer
2-25-6-14 Designing High-Bypass Nacelle Inlets
2-26-7-18 Getting it right through test flight
2-25-7-14 Global Technologies
2-26-4-14 Materials mature
2-26-6-13 Planning for the future
2-26-7-13 Planning for the future
2-26-5-24 Polar satellite tries to weather storm
2-26-5-14 Simulating real-time safety
2-25-5-25 Space Goes Commercial
2-25-7-28 Taking Research to the Bank
2-25-7-31 Testing Toward Perfection
2-25-6-19 Virtually Eliminating Prototypes
2004-01-3095 A Distributed Environment for Analysis of Events Related to Range Safety
2004-01-3094 A Distributed Environment for Spaceports
2004-01-3120 A Prototype Augmented-Reality Flight-Deck Airflow Hazard Visualization System
2004-01-3122 Agent Architecture for Aviation Data Integration System
2004-01-3116 Autonomous Flight Control Development on the Active Aeroelastic Wing Aircraft
2004-01-3117 Binary Optimization By Hopfield Neural Networks
2-24-10-24 Distributed Simulation
2004-01-3131 Free Vibration Analysis of Micro-Satellite Structure
2004-01-3134 Impact of Sampling Technique Selection on the Creation of Response Surface Models
2004-01-3083 Integration of Dynamic Models in Range Operations
2004-01-3082 Internet-Based Simulations of Debris Dispersion of Shuttle Launch
2004-01-3121 Knowledge Navigation for Virtual Vehicles
2004-01-3133 Neural Networks Contribution to Modelling for Flight Control
2004-01-3115 Performance Evaluation of An Integrated Retrofit Failure Detection, Identification and Reconfiguration (Fdir) System Using High-Fidelity and Piloted Simulations
2004-01-3132 Proposed Real-Time Performance Evaluation of Two Types of Adaptive Neural Network Controllers
2004-01-3098 Sensitivity Analysis of the C-130 Sensor Deployment System Arm Using Finite Element Methods
2004-01-3093 Strategy for Modelling of Large A/C Fluid Systems
2004-01-3144 Technology Portfolio Assessments Using a Multi-Objective Genetic Algorithm
2004-01-3143 Using a Fuzzy Expert System to Represent Risk: Foras
2-24-10-17 Wiring Uavs
2-24-8-30 A View From the Factory
2-24-8-40 Fine-Tuning Aerodynamics
2-24-8-37 Reverse Engineering
2-24-7-13 A Developing Situation
2-24-7-20 Remotely Testing
2-24-7-26 Technology Integration
2-27-7-26 Technology integration
2-24-5-44 A Fluid Approach
2-24-5-35 Seats Under Crash Loading
2-24-5-15 Showing How ItS Done
2-24-3-14 Controlling Uavs
2-24-3-19 Supporting Aircraft Evolutions
2-24-3-28 Time Equals Money
2-24-2-13 Planning for the Future
2-24-1-31 Simulating Safety
2-23-11-28 Supporting Aerospace Design
2-23-9-21 Laser-Welding Aluminum
2-23-9-16 Military Engines: Cost and Capability
2003-01-3012 A Multi-Objective Optimization Approach to Aircraft Preliminary Design
2003-01-3056 A Probabilistic Evaluation of Turbofan Engine Cycle Parameters for a Mach 1.8 Interceptor Aircraft
2003-01-3051 A Technique for Use of Gaussian Processes in Advanced Meta-Modeling
2003-01-3058 Aerospace Systems Design: Economics as a New Way of Thinking?
2003-01-3060 Bi-Level Integrated System Synthesis: a Proposed Application to Aeroelastic Constraint Analysis in a Conceptual Design Environment
2003-01-3007 Distributed Aircraft Analysis Using Web Service Technology
2003-01-3053 Formulation of An Integrating Framework for Conceptual Object-Oriented Systems Design
2003-01-3055 Implementation of a Physics-Based Decision-Making Framework for Evaluation of the Multidisciplinary Aircraft Uncertainty
2003-01-3052 Parametric Modeling Techniques in Industrial Conceptual Transport Aircraft Design
2003-01-3059 Response Surface Utilization in the Exploration of a Supersonic Business Jet Concept With Application of Emerging Technologies
2003-01-3014 Simulation Based Optimisation for Aircraft Systems
2003-01-3035 Simulation of Ac Arc Faults in Aircraft Electrical Networks - Critical Loads - Critical Ignition Energies
2003-01-3054 Using Optimization as a Tool in Fuel System Conceptual Design
2003-01-3065 Voice Recognition and Speech Synthesis in An Atc Simulation Environment
2-23-8-37 Wing Design Opens the Envelope
2-23-7-24 A New Trip Down Memory Lane
2-23-7-29 An Eye on Uavs
2-23-7-13 Technology and Development in Europe
2-23-6-25 Fire-Resistant Composites for Engine Nacelles
2-23-6-20 Portable Test System
2-23-5-19 Horizontal Vision and Strategy
2-23-5-14 Paris Air Show: the Details
2-23-4-19 Virtual Prototyping Helps Bombardier
2-23-3-18 Airflow Simulation for Winglets
2-23-3-12 The Dawn of the Jet Age: the First 10 Years
2002-01-2949 A Longitudinal Slip Tire Model for Brake Control Systems: Features and Uses in Simulation, Control Synthesis and Stability Analysis
2002-01-2921 Advanced Dynamometer Designed to Fully Characterize the Propulsion System for a Uav
2002-01-2963 Airline Pilots Perceptions of and Experiences in Crew Resource Management (Crm) Training
2002-01-2965 An Automated System Framework for Pre-Mission Success Evaluation of Medical Emergency Helicopters Operations-Derived Mission Capability Sub-Module
2002-01-2948 Asymmetric Approach in Solving Aircraft Brake Vibration
2002-01-2958 Atn Airborne Implementation
2002-01-2968 Designing User-Interfaces for the Cockpit: Five Common Design Errors and How to Avoid Them
2002-01-3012 Determining Optimum Redesign Plans for Avionics Based on Electronic Part Obsolescence Forecasts
2002-01-2925 Development and Application of a Real-Time Bleed Air Contamination Monitor
2002-01-2947 Development of Reduced Catalytically Active Runway Deicer Fluids for Carbon/Carbon Composite Friction Materials
2002-01-2924 Economic Viability of NasaS Next-Generation Aviation Paradigm: a Summary of Research Findings
2002-01-2953 Electric Starting of Large Aircraft Engines
2002-01-2945 End Item Temperature Test--An Improved Lru-Level Screen
2002-01-2998 Enhanced Security Flight Deck Doors-Commercial Airplanes
2002-01-2941 Environmental Systems Considerations for Aircraft Cabins During Ground Operation
2002-01-2916 Estimation Technology of the Bell Model M427 Helicopter Using Parameter Assessment of the Dynamic Stability Characteristics
2002-01-3001 Fea Cyclic Symmetric Fatigue Analysis of Aircraft Wheels
2002-01-2957 Fire Resistant Composites
2002-01-2931 Fuel Transfer System in the Conceptual Design Phase
2002-01-3008 Highlights of NasaS Systems Approach to Crashworthiness Research
2002-01-3006 Hud Symbology for Surface Operations: Command Guidance Versus Situation Guidance Formats
2002-01-2956 Hybrid-Ceramic Circumferential Carbon Ring Seal
2002-01-2927 Identification and Evaluation of Technologies for the Development of a Quiet Supersonic Business Jet
2002-01-2930 Impact of Configuration and Requirements on the Sonic Boom of a Quiet Supersonic Jet
2002-01-2990 Improving the Aerodynamic Efficiency of High Lift Devices By a Stiffness-Oriented Re-Design With Tailored Laminates
2002-01-3010 Incorporation of Lean Principles Through the Use of Flexible Fuel Tubing in a Large Military Transport Aircraft
2002-01-3004 Metastable Beta Titanium Spring Performance At Elevated Temperature
2002-01-2942 Method for Analyzing Lubricating Oil Contamination of Aircraft Systems
2002-01-2918 Model of Casing Treatment Influence on Compressor Rotor Efficiency
2002-01-2974 One-Pass Pricing Methodology
2002-01-2944 Past, Present, and Future of the Gas Turbine Engine Simulator; a Technical and Financial Analysis
2002-01-3000 Photon-Induced Positron Annihilation (Pipa)-A New, Core Technology to Improve the Nondestructive Inspection and Life Prediction for Critical Components
2002-01-3011 Plastic Ball-Grid-Arrays (Pbga): Are They Ready for Environmentally Harsh Aerospace Applications?
2002-01-2926 Propulsion Education for General Aviation Aircraft
2002-01-2929 Quiet Supersonic Jet Engine Performance Tradeoff Analysis Using a Response Surface Methodology Approach
2002-01-2967 Rear Projection for Multi-Function Displays
2002-01-2983 Recommendations for Future Avionics Hardware Development
2002-01-2922 Relative Guidance of Aircraft: Analysis and Comparison of Two Control Approaches
2002-01-2951 Reliable Bearing Wear Detection System for On-Condition Maintenance of Electric Generators
2002-01-2954 Sensorless Control of Brushless Dc Motor for More Electric Aircraft
2002-01-2985 Software Tools for the Development of Design Decision Support for Re-Configurable Unmanned Arial Vehicles
2002-01-2928 Solution of the Non-Synchronous Vibration in the As900 Engine
2002-01-3007 Tail Icing Effects on the Aerodynamic Performance of a Business Jet Aircraft
2002-01-2939 The Benefits of a Wire Integrity Program
2002-01-2970 The Efficacy of Using Synthetic Vision Terrain-Textured Images to Improve Pilot Situation Awareness
2002-01-3023 The Gp7200 Engine-Power for the Airbus A380
2002-01-2971 Use of Enhanced Vision Sensors for Approach Hazard Detection
2002-01-2923 Use of VictrexSr PeekSt Thermoplastic to Drive New Designs, Processing Flexibility, and Cost Reduction in Aerospace Components
2002-01-3013 Utilization Life of Electronic Systems-Aging Avionics Usable Life and Wear-Out Issues
2002-01-2995 Vertical Drop Test of a Narrow-Body Transport Fuselage Section With Overhead Stowage Bins
2002-01-2997 Vertical Drop Test of a Transport Fuselage Section
2002-01-2912 Wind-Tunnel Investigation of Commercial Transport Aircraft Aerodynamics At Extreme Flight Conditions
2-22-9-16 Launching Technology
2-22-8-14 Eads Aerospace Technology
2002-01-1508 On Overview of the Sino Swearingen Sj30-2 Program
2002-01-1540 The Problem: Estimating a Complex Project Duration
2002-01-1509 User Survey of Barriers to the Utility of General Aviation
2-22-2-31 Collaborating via the Web
2001-01-2985 Airplane Technologies to Reduce Jet Fuel Use
2001-01-3036 Future Combat Aircraft Capacities Offered By Advanced Technologies
2001-01-3008 Quantities, Characteristics and Reduction Potentials of Aircraft Engine Emissions
2001-01-3920 Development of a Radio-Controlled Airship
2001-01-3927 Truss Optimization in Aerospace Structures
2000-01-5535 1998/1999 Aiaa Foundation Graduate Team Aircraft Design Competition: Super Stol Carrier On-Board Delivery Aircraft
2000-01-5562 A Generalized Model for Vehicle Thermodynamic Loss Management and Technology Concept Evaluation
2000-01-5563 A Method for Technology Selection Based on Benefit, Available Schedule and Budget Resources
2000-01-5564 A Parametric Design Environment for Including Signatures Analysis in Conceptual Design
2000-01-5536 A Student Developed Sizing Methodology for Electric Powered Aircraft Applied to Small UavS
2000-01-5565 An Automated Robust Process for Physics Based Aerodynamic Prediction
2000-01-5527 An Exergy-Based Methodology for Decision-Based Design of Integrated Aircraft Thermal Systems
2000-01-5577 Benefits of Door-To-Door Travel Time Reduction to Us Economy
2000-01-5538 Design of a High-G Unmanned Aerial Vehicle Structure
2000-01-5612 Framework for the Assessment of Capacity and Throughput Technologies
2000-01-5610 Integration of Configuration Design and Multidisciplinary Analysis of Aircraft
2000-01-5589 Methodology for Assessing Survivability Tradeoffs in the Preliminary Design Process
2000-01-5552 Redesign of the C-17 Globemaster Iii Auxiliary Power Unit (Apu) Exhaust System
2000-01-5525 Scenario-Based Systems Studies for Military Aircraft
2000-01-5579 Solution of An Engine Inlet Compatibility Problem During C-17 Low-Cost N/Eat Nacelle Thrust Reverser Development
2000-01-5578 The C-17 Global Air Traffic Management (Gatm) Application
2000-01-5609 The Role of Constraints in the Mdo of a Cantilever and Strut-Braced Wing Transonic Commercial Transport Aircraft
2000-01-5590 Use of Flight Simulation in Early Design: Formulation and Application of the Virtual Testing and Evaluation Methodology
1999-01-5556 21st Century Aircraft Potable Water Systems
1999-01-5600 3d Piv in Wind Tunnel Applications: Measurements of a Truck Wake
1999-01-5569 A High Efficiency Fuselage Propeller ("Fusefan") for Subsonic Aircraft
1999-01-5657 A History of Manned Powered Flying Wing Development: 1922- 1999
1999-01-5515 Airbreathing Hypersonic Vision-Operational-Vehicles Design Matrix
1999-01-5641 An Improved Process for the Generation of Drag Polars for Use in Conceptual/Preliminary Design
1999-01-5532 Assessment of a Lethal Uninhabited Air Vehicle
1999-01-5518 Characterization of Large Thin-Film Membrane Dynamic Behavior With Uai- Nastran Finite Element Solver
1999-01-5654 Compound Tilting Wing for Stol Configurations
1999-01-5530 Design of Medium Military Transport Aircraft
1999-01-5521 Economics of Landing Fear System Design for Very Large Aircraft
1999-01-5638 Elements of An Emerging Virtual Stochastic Life Cycle Design Environment
1999-01-5631 Forecasting Technology Uncertainty in Preliminary Aircraft Design
1999-01-5533 International Teaming in Aircraft Design Education
1999-01-5599 Investigation of Measurement Errors in Doppler Global Velocimetry
1999-01-5523 Landing Gear Design in the Conceptual Design Phase
1999-01-5606 Lessons Learned From Test Flight of Military Hmds: Possible Application to Civilian Rotorcraft Operation
1999-01-5517 Next Generation Space Telescope (Ngst) Pathfinder Experiment Inflatable Sunshield in Space (Isis)
1999-01-5570 Predicting the Implications of New Technologies on Aircraft Structural Mass
1999-01-5524 Preliminary Project of the Autonomous Landing System for Unmanned Aircraft
1999-01-5520 Revolutionary Design Concepts for Inflatable Space Structures
1999-01-5632 Selection of Technologies for Future Aircraft Family Concepts
1999-01-5514 Sharp Leading Edge Hypersonic Vehicles in the Air and Beyond
1999-01-5608 Spatially Integrated Data Presentation for Tiltrotors: How to Benefit From the Concepts Developed for Fixed-Wing Aircraft?
1999-01-5596 System Integration Based on Reverse Engineering Processes and Digital Mockup for Upgrades of Military Aircrafts
1999-01-5612 The Application of Neural Networks for Spin Avoidance and Recovery
1999-01-5639 The Implementation of a Conceptual Aerospace Systems Design and Analysis Toolkit
1999-01-2640 25-Ah Li-Ion Cell for the Mars 2001 Lander
1999-01-2590 90 Ah Dependent Pressure Vessel (Dpv) Nickel Hydrogen Battery Qualification Test Results
1999-01-2615 A 50 Wh Open Core High-Speed Flywheel
1999-01-2672 A Comparison of the Entropy of Thermal Radiation to That of Heat Conduction
1999-01-2597 A Generalized Large/Small Signal Average Pwm Converter Model
1999-01-2711 A Grand Design of Future Electric Vehicle With Fuel Economy More Than 100 Km/Liter
1999-01-2494 A High-Breakdown Voltage NU+-Gaas/Gd(PU+)-Gainp/N-Gaas Heterojunction Camel-Gate Transistor for Power System Applications
1999-01-2493 A High-Breakdown and Low-Offset Voltage Ingap/Gaas Heterostructure Bipolar Transistor for Power System Applications PT-82
1999-01-2448 A Modular, Peak Power Tracking Solar Array Regulator
1999-01-2556 A Natural-Artificial, Power-Industrial System Based on Wave Energy Conversion
1999-01-2567 A New High Efficiency Segmented Thermoelectric Unicouple
1999-01-2445 A Novel Battery Charger-Discharger of the Regulated-Peak- Power-Tracking System
1999-01-2570 A Review of Fuel Processor-Based Pemfc Electrical System Development for Commercial and Military Applications
1999-01-2601 A Solar Dynamic Power Option for Space Solar Power
1999-01-2695 A Space Experiment to Measure the Atomic Oxygen Erosion of Polymers and Demonstrate a Technique to Identify Sources of Silicone Contamination
1999-01-2724 A Study on Effective Utilization of Solar Energy-Solar Hydrogen Generation By Water Electrolysis
1999-01-2506 A Study on Temperature Distribution of Stirling Engine Regenerator
1999-01-2495 A Triangular-Barrier Optoelectronic Switch With Light- Controllable Performances
1999-01-2521 Acceptability of Premixed Hydrogen in Hydrogen Diesel Engine PT-95
1999-01-2463 Advanced Lithium-Ion Solid Polymer Electrolyte Battery Development
1999-01-2524 Advanced Thermal Hydrogen Compression
1999-01-2637 Advancing Lithium-Ion Technology for Aerospace Applications
1999-01-2655 Amtec Cell Optimization for Advanced Radioisotope Power System (Arps) Design
1999-01-2660 Amtec Internal Self-Heat Pipe
1999-01-2715 An Assessment of Landfill Gas Energy Technologies and Issues
1999-01-2694 Analyses of Contaminated Solar Array Handrail Samples Retrieved From Mir
1999-01-2431 Analysis of Direct Solar Illumination on the Backside of Space Station Solar Cells
1999-01-2526 Analysis of Heat and Fluid Flow in Blast-Furnace Hearth as a Means to Increase Productivity
1999-01-2464 Analysis of the Irreversible Capacity Loss on Carbons for Li- Ion Batteries
1999-01-2689 Analysis, Simulation and Testing of the Gp-Clc Resonant Converter
1999-01-2650 Analytical Calculation of Pressure Distribution on a Residential Roof
1999-01-2681 Basic Research on Solar Stirling Power Technology for Future Space Applications
1999-01-2467 Battery State-Of-Charge Meters for High-Performance Batteries Based on Fuzzy Logic Methodology
1999-01-2548 Benefits Assessment of More Electric Aircraft Generation Ii Technologies
1999-01-2488 Bipolar Nickel-Metal Hydride Batteries for Aerospace Applications
1999-01-2514 Bipolar Nickel-Metal Hydride for Terrestrial Applications
1999-01-2436 Centralized Power Supply as Basis of New Philosophy of Space Power Engineering
1999-01-2538 Characterization and Leo Life Testing of Nickel-Hydrogen Cells for Space in Sisp
1999-01-2470 Combined Production of Power and Alternative Fuels in Connection With Pulp Mills
1999-01-2713 Combustion Noise From a Diesel Engine Operating With High Concentrations of Intake Carbon Dioxide
1999-01-2522 Combustion Synthesis of Hydrogen Storage Alloy
1999-01-2688 Composite Lithium Electrolytes Based on Aluminum Carboxylates
1999-01-2686 Continuing Challenges in Lithium Battery Development
1999-01-2718 Convection in a Rectangular Duct With a Corrugated Surface
1999-01-2460 Cylindrical Inverted Thermionic Converter for Solar Power and Propulsion Systems
1999-01-2594 Dependence of Positive Plate Design and Temperature on the Performance of Nickel-Hydrogen Cells
1999-01-2674 Design and Analysis Code for Radiators of Stirling Power Systems With General Purpose (Gphs) Heat Sources
1999-01-2633 Design and Development of the Timed Spacecraft Solar Array
1999-01-2642 Design of a Microprocessor-Based Controller for Robotics Manipulator
1999-01-2654 Design of the Epx-1 Amtec Cell for the Advanced Radioisotope Power System
1999-01-2588 Design, Fabrication, and Testing of a 10 Kw-Hr HD2-OD2 Pem Fuel Cell Power System for High-Altitude Balloon Applications
1999-01-2572 Development of Anti-Freeze Pefc Stack for Automobile Applications
1999-01-2616 Development of Vanadium Redox Flow Battery System
1999-01-2698 Development of a Simple Homogeneous Flow Model of a Two-Phase Ejector
1999-01-2575 Diagnosis of Fuel-Cell Deterioration Using Fuel-Cell, Current- Voltage Characteristics
1999-01-2561 Dish/Stirling Hybrid-Receiver, Sub-Scale Tests and Full-Scale Design
1999-01-2707 Driving Schedules Influence Electric and Hybrid Vehicle Efficiency
1999-01-2653 Effect of Cold Flow Additives on Aviation Fuel Fluidity and Tank Hold-Up
1999-01-2604 Effect of Pressure and Velocity Distribution on Propane and Air Mixing Under Reacting and Non-Reacting Conditions
1999-01-2432 Effects of Solar Array Shadowing on the Power Capability of the Interim Control Module
1999-01-2577 Electrical Energy Storage Systems for the Energy Networks With Dispersed Generators
1999-01-2458 Electrical Output of Efficient Cylindrical Thermionic Energy Converters as a Function of Interelectrode Spacing and Emitter Work Function in Vacuum
1999-01-2645 Electrical System Architectures for Future Aircraft
1999-01-2685 Electrochemical Behavior of Microscopic Secondary Batteries
1999-01-2634 Electrostatic Discharge Measurements on Solar Cell Coupons in a Simulated Geo Environment
1999-01-2697 Energy Analysis of a High-Temperature Chemical Heat Pump
1999-01-2667 Energy Balance of Low-Energy House With Ground Source Heat Pump in Hokkaido
1999-01-2582 Eos-Am Solar Array Arc Mitigation Design
1999-01-2595 Evaluation and Life Testing of Lithium-Ion Batteries for Geosynchronous Satellites
1999-01-2479 Evaluation of Aerogel Materials for High-Temperature Batteries
1999-01-2516 Evaluation of Energy Use Performance of An Induction Motor Power Conditioner
1999-01-2513 Evaluation of Plasma-Sprayed, Thin-Film Pyrite Cathodes for Thermal Batteries
1999-01-2456 Evaluation of Six Different Correlations for the Flow Friction Factor of Stirling Engine Regenerators
1999-01-2459 Evaluation of Two Types of Oxygen-Dispensing Collectors for Thermionics
1999-01-2598 Exact Simulation of Conducted Emi in Switched Mode Power Supplies
1999-01-2550 Example of a Prototype Lightweight Solar Array and the Three Promising Technologies It Incorporates: Copper Indium Diselenide (Cis) Thin-Film Photovoltaics, Smart Mechanisms Employing Shape Memory, and Multifunctional Structures
1999-01-2509 Experimental Study of a Novel Thermosyphonic Mhd Electric Generator
1999-01-2486 F-16 Battery/Charger Evaluation
1999-01-2627 Flight Testing of a Cryogenic Capillary Pumped Loop
1999-01-2477 Flight Verification of a Nitrogen Triple-Point Cryogenic Thermal Storage Unit (Ctsu)
1999-01-2589 Flywheel Energy Storage for Spacecraft Power Systems
1999-01-2473 Fuel Economy Improvement By Vehicle Control Optimization
1999-01-2587 Ground-Engineering Study on Solar Hp/Tes Receiver for Future Iss-Jem Experiment Program
1999-01-2492 High Breakdown-Voltage and High-Linearity Camel-Gate Field- Effect Transistor With Multiple Modulation-Doped Channels PT-82
1999-01-2600 High-Energy Density Regenerative Fuel Cell Systems for Terrestrial Applications
1999-01-2546 High-Power Density Converters for More Electric Aircraft Applications
1999-01-2649 High-Temperature Gasification of Solid Fuels
1999-01-2581 High-Temperature Solar Cell for Space/Terrestrial Applications
1999-01-2557 Hydrogen Permeation Issue for Gas-Fired Amtec Systems
1999-01-2578 Impact of Lightning Strikes on Nuclear Power Generating Stations
1999-01-2573 Impact of Reactant Condensation on a Cu/Zno/AlD2oD3 Catalyst Bed During Methanol-Steam Reforming for Fuel Cell Hydrogen Production
1999-01-2706 Impedance Measurements of Px-Series Amtec Cells
1999-01-2511 Improved Cycle Life Performance of the HorizonSr CU2m Battery
1999-01-2665 Improved Modeling of Urban Warming in Tokyo and Numerical Projection to 2030
1999-01-2444 Inductor Current Sensing Peak-Power-Tracking Solar Array Regulator
1999-01-2551 Inflatable Solar Arrays: Revolutionary Technology?
1999-01-2617 Influence of Ultrasonic Vibration on Freezing Temperature of Hydrate
1999-01-2483 Inner Planets Sample Return Missions: the Challenge for Power Systems
1999-01-2599 Input Series-Output Parallel Connected Converter for High- Voltage Power Conversion Applications Employing Charge Control
1999-01-2499 Integrated Energy Management System for Uninhabited Combat Air Vehicles (Ucavs)
1999-01-2434 International Space Station U.S. Major Element Laboratory Power Quality Test
1999-01-2592 Joint Dod/Nasa Lithium Ion Battery Development Program
1999-01-2554 Kinetic and Electrical Energy Storage Device on Base of the Hybrid System Mmsuperconductor-SuperflywheelMh (Sc-Sfw)
1999-01-2440 Laser Power Transmission as a Terrestrial Expedition Power Supply Under Normal Conditions and as a Rescue System in Case of An Emergency
1999-01-2704 Lifetimes of Amtec Electrodes: Rhodium-Tungsten and Titanium Nitride
1999-01-2614 Lightweight and Corrosion Resistant Metal Bipolar Plates for Pem Fuel Cells
1999-01-2517 Liquid Nitrogen as a Non-Polluting Vehicle Fuel
1999-01-2591 Lithium-Ion Performance Testing and Ac Impedance Characterization
1999-01-2515 Long-Life and High-Energy-Density Batteries as a Backup Power Supply
1999-01-2585 Long-Term Inert Processing of Rtgs
1999-01-2530 Loop Heat Pipes-Recent Developments, Test Results and Applications
1999-01-2543 Low Temperature Performance Evaluation of Battery Management Technologies
1999-01-2553 Low-Cost and Lightweight Amorphous Silicon Alloy Solar Array for Space Application
1999-01-2462 Low-Temperature Electrical Performance Characteristics of Li- Ion Cells
1999-01-2447 Mars Rover 2003 Battery Charger
1999-01-2720 Mathematical Simulation of Transient Thermal Process of Aircraft Cabins
1999-01-2608 Mechanical Testing Studies on Niobium-1%Zirconium in Association With Its Application as Cell Wall Material in An Amtec-Based Radioisotope Space Power System
1999-01-2569 Miniaturized Thermoelectric Power Sources
1999-01-2703 Model for Grain Growth in Amtec Electrodes
1999-01-2540 Modeling Double-Layer Capacitors Using Ac Impedance Measurements
1999-01-2719 Modeling and Assessment of Ice Storage for Air Conditioning
1999-01-2690 Modeling of Spacecraft Propellant Gauging System
1999-01-2670 Multi-Step Water Splitting With Mn-Ferrite/Sodium Carbonate System
1999-01-2485 Near-Earth Asteroid Rendezvous Spacecraft Power System Flight Performance
1999-01-2468 New Energy Management Technology Gives Hybrid Cars Long Battery Life PT-85
1999-01-2619 New Frequency Control Technique for Useful Utilization of Stand-Alone, Wind-Turbine-System-Generated Power
1999-01-2512 Nickel-Zinc Batteries for Commercial Applications PT-85
1999-01-2545 On the Concept of Negative Impedance Instability in the More Electric Aircraft Power Systems With Constant Power Loads
1999-01-2620 On the Development of a Wind Energy-Based Efficient Irrigation System
1999-01-2708 On the Optimum Sustainable Energy Mix
1999-01-2679 Optical Evaluation of a Refractive Secondary Concentrator
1999-01-2687 Optimization of Cobalt-Doped Chromium Oxide as Cathode Material for Secondary Lithium Batteries
1999-01-2714 Optimization of Energy Recovery From Biomass
1999-01-2453 Optimized Design of Stirling-Driven, Vapor-Compression System
1999-01-2564 Optimized Thermal Design of Small Gdt Thermoelectric Generators
1999-01-2728 Optimum Compression Ratio Variation of a 4-Stroke, Direct- Injection Diesel Engine for Maximum Brake Power and Torque and Minimum Soot and NoDx Emissions
1999-01-2519 Optimum Compression Ratio Variation of a 4-Stroke, Direct- Injection Diesel Engine for Minimum Bsfc
1999-01-2727 PEM Fuel Cell System Evaluation for Navy Surface Ship Applications
1999-01-2552 Paraboloidal Thin-Film Inflatable Concentrators and Their Use for Power Applications
1999-01-2613 Pem Energy Storage for Solar Aircraft
1999-01-2639 Performance Characteristics of Lithium-Ion Cells for Mars Sample Return Athena Rover
1999-01-2638 Performance Characteristics of Lithium-Ion Cells for NasaS Mars 2001 Lander Application
1999-01-2583 Performance Evaluation of the First Ac Bipv Installation in Canada
1999-01-2700 Performance Modeling of 5th-Generation, Heat-Assisted Stirling Heat Pump (E-3)
1999-01-2632 Performance of the Mir Cooperative Solar Array After 2.5 Years in Orbit
1999-01-2631 Photovoltaic Approaches for Near-Sun Missions
1999-01-2702 Potassium Amtec Cell Performance
1999-01-2496 Power Control of Converters Using Novel Resonant Techniques With Applications
1999-01-2443 Power Electronics Building Blocks (Pebb) in Aerospace Power Electronic Systems
1999-01-2531 Power Generation and Storage Technology Selection for An Optimal Spacecraft System Design
1999-01-2442 Power Management and Distribution Concept for Microsatellites and Nanosatellites
1999-01-2547 Power Management and Distribution System for a More-Electric Aircraft (Madmel) - Program Status
1999-01-2484 Power System Performance of the Soho Spacecraft During the 1998 Attitude Recovery
1999-01-2625 Practical Constraints in Using High Thermal Conductivity Composite Materials in Spacecraft Application
1999-01-2571 Prediction of Levels of Co Contamination in Methanol-Steam Reformate Gas for Pem Fuel Cell Power Systems
1999-01-2549 Preliminary Design Results for the Switched Reluctance Cycloconverter
1999-01-2465 Pressure-Indicating Films for Battery Manufacture and Test
1999-01-2574 Pressurized and Atmospheric Pressure Gasoline-Fueled Polymer Electrolyte Fuel Cell System Performance
1999-01-2537 Progress in the Development of Lightweight Nickel Electrode for Nickel-Hydrogen Cell
1999-01-2502 Proposal and Basic Experiments of Super Stirling Engines
1999-01-2683 Proposals for New-Types Solar Heat Engine Systems
1999-01-2433 Protection of Space Hardware During Ground Testing
1999-01-2566 Prototype Nighttime Solar CellSt-Electrical Energy Production From the Night Sky
1999-01-2696 Radiation Effects on Dc-Dc Converters
1999-01-2461 Raman Spectroscopy of the Plasma in An Open Research Thermionic Converter
1999-01-2534 Recent Advances in Power System Design At Gsfc
1999-01-2603 Recirculating Plug Flow Reactor
1999-01-2678 Refractive Secondary Concentrators for Solar Thermal Applications
1999-01-2611 Regenerative Micro-Fuel Cells and Electrolyzers
1999-01-2487 Results of a Real-Time Life Test of Aerospace Ni-Cd Battery Cells for 26,000 Cycles With and Without Scheduled Reconditioning
1999-01-2471 Revisiting Thermodynamic Analysis and Design of Power Cycles With An Intelligent Instruction Software
1999-01-2596 Rolled Barium Titanate (Bt) Film Capacitor for Pulsed Power Application
1999-01-2725 Scientific Basis for Low-Energy Nuclear Reactions (Lenrs) for Nuclear Waste Amelioration
1999-01-2497 Secondary Power System Evaluations for An Unmanned Air Vehicle Configuration
1999-01-2676 Significance of Landsat-7 Spacecraft Level Thermal Balance and Thermal Vacuum Test for Etm+ Instrument
1999-01-2501 Skin as Radiator-Passive Thermal Management for High-Altitude, Long-Endurance Uavs
1999-01-2705 Slow Reversible and Quasi-Reversible Performance Changes in Amtec Electrodes and Electrolytes
1999-01-2646 Smart Material Actuator Driven By Networked Rectenna Array
1999-01-2532 Software Validation of the Jason 1 Electrical Power Subsystem
1999-01-2482 Solar Electric Power System Analyses for Mars Surface Missions
1999-01-2671 Solar Furnace System Using Tower-Reflector With Ellipsoidal Mirror
1999-01-2449 Solar Power System Analyses for Electric Propulsion Missions
1999-01-2669 Solar Two Performance Evaluation
1999-01-2677 Solution for Direct Solar Impingement Problem on Landsat-7 Etm+ Cooler Door During Cooler Outgas in Flight
1999-01-2451 Space Solar Bimodal Brayton Power System
1999-01-2544 Steady-State Operation of a High-Voltage, Multi-Resonant Converter in a High-Temperature Environment
1999-01-2441 Sun Tower Pmad Architecture
1999-01-2491 Surface Recombination Effect in Gaas-Based Heterostructure- Emitter and Heterostructure-Base Transistors (Hehbts)
1999-01-2454 Technology Development for a Stirling Radioisotope Power System for Deep Space Missions
1999-01-2435 Testing of the Engineering Model Electrical Power Control Unit for the Fluids and Combustion Facility
1999-01-2555 The Circulation Hydraulic Contour on MeissnerS Effect
1999-01-2586 The Design of a Nuclear Power Supply With a 50-Year Life Expectancy: the Jpl VoyagerS Sige Mhw Rtg
1999-01-2643 The Effect of Reference-Environment Models on the Accuracy of Exergy Analyses of Aerospace Engines
1999-01-2664 The Effect of a Multiple Spark Discharge Ignition System and Spark Plug Electrode Configuration on Cold Starting of a Dedicated E85-Fueled Vehicle
1999-01-2606 The Emitter Tri-Layer: a Key Component of the Conductively Coupled Multi-Cell Thermionic Fuel Element
1999-01-2644 The Influence of Passive Elements on Statcom Performance
1999-01-2710 The Influence of a Particulate Trap on the in Vitro Lung Toxicity Response to Continuous Exposure to Diesel Exhaust Emissions
1999-01-2668 The Potential for Low-Cost Electricity From Concentrating Solar Power Systems
1999-01-2503 The Second Stirling Techno Rally Contest of Model and Manned Stirling Engine Cars
1999-01-2624 The Substantiation of a Wind WheelS Design With Gyrating Sailing Vanes At Low-Speed Conditions of Winds
1999-01-2628 Thermal Assessment of Landsat-7 Etm+ Radiative Cooler in Instrument and Spacecraft Thermal Vacuum Tests and in Flight
1999-01-2723 Thermal Management and Control in Testing Packaged Integrated Circuit (Ic) Devices
1999-01-2480 Thermal Management of Microelectronics By Axial Jet Impingement
1999-01-2717 Thermodynamic Analysis of a System With Open-Cycle Gas Turbine for Combined Refrigeration and Heating Purposes
1999-01-2558 Thermodynamic Design and Optimization of a 20 Kw Vuilleumier Heat Pump
1999-01-2716 Thermodynamic Remarks on An Air-Cycle Microclimate Cooling Device
1999-01-2529 Thin Copper-Water Heat Pipe Plate for Electronic Cooling
1999-01-2475 Transient Heat Transfer Experiment in Subcooled Liquid Nitrogen
1999-01-2680 Transient Thermal Analysis of a Refractive Secondary Solar Concentrator
1999-01-2474 Twa800 Fuel Tank Thermal Management Issues
1999-01-2726 Us Army Small Fuel Cell Development Program
1999-01-2469 Us Epa 1998 Certification Label Mpg Correlated With Consumers Union Fuel Economy Tests of 114 Vehicles
1999-01-2621 Using Qfd to Ensure a Holistic Integration of Renewable Energies
1999-01-2518 Utilization of Ethanol and Gas-Oil-Blended Fuels for Diesel Engine (Addition of Decanol and Isoamyl Ether)
1999-01-2629 Validation of Landsat-7 Etm+ Mem Thermal Improvement in Thermal Vacuum Tests and in Flight Due to Lower Louver Set Points
1999-01-2626 Validation of Modified Wine-Rack Thermal Design for Nickel- Hydrogen Batteries in Landsat-7 Spacecraft Thermal Vacuum Test and in Flight
1999-01-2630 Validation of the Scarlet Advanced Array on Ds1
1999-01-2498 Variable Frequency Use in Aerospace Electrical Power Systems
1999-01-2622 Weibull Distribution and Rmc Speed for Sizing Wind Energy Potential
1999-01-2542 Wide Temperature Core Loss Characteristics of Transverse Magnetically Annealed Amorphous Tapes for High-Frequency Aerospace Magnetics
1999-01-2541 Wide Temperature Magnetization Characteristics of Transverse Magnetically Annealed Amorphous Tapes for High-Frequency Aerospace Magnetics
1999-01-2430 Zarya Energy Balance Analysis: the Effect of Spacecraft Shadowing on Solar Array Performance
985512 Progress on Starcar 4
985584 Structural Integrity Assessment Through Eigensolution
975509 "Web-Acsynt": Conceptual-Level Aircraft Systems Analysis on the Internet
975537 A Methodology for Preliminary Design of Mechanical Aircraft Systems
975560 A New Look At Optimum Propeller Performance--Going From the Prandtl F Factor to a Vortex-Induced Downwash Analysis
975575 A Part-Time MasterS Course Incorporating Aircraft Design, Build and Flight Test
975582 A Practical Flying Car
975541 A Technique for Testing and Evaluation of Aircraft Flight Performance During Early Design Phases
975595 Adapting Civil Aircraft Conceptual Design Methods to Account for Broader-Based Constraints
975572 Aerothermodynamic Design of Supersonic Channel Airfoils for Drag Reduction
975510 Airplane Configuration Layout Design Using Object-Oriented Methods
975567 Airplane Criteria Process
975598 Calculation of Jet Aircraft Parameters Under Design Requirements
975644 Civil Certification of Avionics Modifications in Military Transport Category Aircraft
975587 Cost-Integration Strategies for More Affordable Aerospace Designs
975542 Cristo: a Code for Integrated Synthesis and Trajectory Optimization of Commuter and Regional Aircraft
975585 Demonstration of a Probabilistic Technique for the Determination of Aircraft Economic Viability
975566 Design Studies for a 200-Seat Transport Aircraft Using Multivarite Optimization
975513 Designing Ranged Sets of Top-Level Design Specifications for a Family of Aircraft: An Application of Design Capability Indices
975545 Economic Optimization of An Advanced Subsonic Transport
975577 Evolution and Future Development of Airplane Gust Loads Design Requirements
975589 Expanding the Role of the Wind-Driven Manipulator
975515 Experience and Potential of Multidisciplinary Optimization Tools on Supersonic Aircraft
975520 Flight Testing a Modern Flight Control System
975549 Full-Scale Test Transport Aircraft Thrust Vectoring System
975565 H-1 Upgrade Program: a Team Approach to System Safety
975574 Integrating Multidisciplinary Design in An Undergraduate Engineering Curriculum
975506 Load-By-WireSt Advanced Cargo Handling System
975547 Multidisciplinary Design and Prototype Development of a Very Small Remotely Piloted Reconnaissance Airplane
975568 Oblique All-Wing Airliner Sizing and Cabin Integration
975643 Proposed Display Arrangement and Contents for Synthetic Vision System
975551 Results of the J-5 Marco Dynamic Similar Model Flight Tests Program
975525 Review of High-Speed Civil Transport (Hsct) Flight Deck Design and Integration Issues
975610 Sofia Aircraft Design
975611 Sofia Aircraft Operations
975636 Student Evolution of An Unconventional Flying Wing Configuration
975591 The Aspect-Ratio Equivalence of Conventional Aircraft With Configurations Featuring Outboard Horizontal Stabilizers
975594 The Economic Assessment of Passenger Cabin Space
975569 The Investigation of Supersonic Commercial Transport Performance Issues Using Multivariate Optimization
972486 Design Development of An Inflatable Module for a Lunar/Martian Base
972469 Thermal Design of the Lunar Exploring Spacecraft
972201 Applications and Development of Eb Welding on the F-22
971246 Design and Performance of a 140 Kva, 3-Phase 230 Vac, Variable Frequency, Solid-State Power Controller
971247 Integrated Power Systems for Future Transport Aircraft
971245 Rationale Behind In-Process Changes to Constant and Variable Frequency Power Quality Standards
971241 Thermal Optimization of the Ecs on An Advanced Aircraft With An Emphasis on System Efficiency and Design Methodology
971474 Aircraft Design Tools for PcS
971458 Alternative Designs of Energy-Absorbing Seat Legs for Certification of Commuter Aircraft Seats
971473 General Aviation Airplane Design Tools for Pcs
971501 General Aviation Preliminary Structural Design in a Personal Computer Environment
970989 Influence on Materials Flow in Deep Drawing Using Individual Controllable Draw Pins and Smooth Blankholder Design
962288 WorldS First Vtol Airplane Convair/Navy Xfy-1 Pogo
965631 "Electric Aircraft" Pioneer the Focke-Wulf Fw 190
965519 A Generic Model Concept for Optimization in Preliminary Design
965568 Acsynt: Commercialization Success
965609 Aircraft Design Optimization on a Personal Computer
965612 An Assessments of a Reaction Driven Stopped Rotor/Wing Using Circulation Control in Forward Flight
965527 An Integrated Computer-Aided Engineering Tool for Aircraft Transparency Design Analytical Design Package--Adp
965517 Conceptual Airplane Design With Automatic Surface Generation
965528 Data Schemas to Support the Architecture of An Aerospace Design Representation Programming Interface
965581 Design Automation: Aerospace Structures and Tooling
965515 Design to Price in Business Aviation
965540 Designing for Stealth in Fighter Aircraft (Stealth From the Aircraft DesignerS Viewpoint)
965529 Development of An Interactive Computerized Aircraft Design System
965621 Flying Automobiles--Are They for Real?
965591 Formulation of An Ippd Methodology for the Design of a Supersonic Business Jet
965520 General Aviation Aircraft Design Methodology in a Pc Environment
965524 Heat Transfer Model of a Jet Pump Cowl Anti-Ice System
965597 How Design Goals of a Long-Range Business Jet Produce An Excellent Military Mission Platform
965501 New Approaches to Multidisciplinary Synthesis: An Aero-Structures-Control Application Using Statistical Techniques
965589 Prelimianry Sizing of a Supersonic Commercial Transport Between Mach 2.0 and 2.4
965567 Rds-Professional in Action: Aircraft Design on a Personal Computer
961885 The Design of a Flexible Fixture for Aircraft Assembly
965539 The Development and Application of Aircraft Radar Cross Section Prediction Methodology
965538 The Have Blue Technology Demonstrator and Radar Cross Section Reduction
965565 The Military Transatmospheric Aerospace Plane
961535 Conceptual Design of Solar-Powered Heat Pump for Lunar Base Thermal Control Systems
961464 Conceptual Design of a Crater Lunar Base
961431 Design Evolution of the Capillary Pumped Loop (Capl 2) Flight Experiment
961433 Design and Ambient Testing of the Flight Starter Pump Cold Plate
961445 Human Requirements for Extended Space Flights--First Mars Outpost Architectural Study I
961327 Computer Aided Engineering for the Design of Flight Control and Hydraulic Systems
961299 Demonstration of An Electrically Actuated Brake With Torque Feedback
961317 Math Modeling of Airfoil Geometry
960008 Cost Awareness in Design--The Role of Data Commonality
952281 Emb-145--50-Seat Regional Airliner
951986 Design of the Electronic Checklist on the Boeing 777 Flight Deck
951997 Designing the Conceptual Flight Deck for a Short Haul Civil Transport/Civil Tiltrotor
952052 Development of the Mcdonnell Douglas Md-90
952031 Forecasting Engine and Airframe Development Cost
952038 Project Design Studies on Aircraft Employing Natural & Assisted Laminar Flow Technologies
952021 Structural Integrity of Landing Gears
952053 The Preliminary Design Analysis of a Unique Semi-Tailless Aircraft Configuration
952051 The Programming Interface Mechanisms Required to Realize An Aerospace Design Representation Programming Interface
951901 Development of a Liquid-Cooled V-8 Reciprocating Engine for Aviation Applications
951533 Conceptual Design Methodology for Celss in a Lunar Base
951522 Interface Design Issues of the Ranger Telerobotics Flight Experiment
951474 Nutrient Delivery Testbed-1: Design of a Flight Experiment for Assessing Nutrient Delivery System Effectiveness Under Gm- Gravity Conditions
951452 A Global Range Hypersonic Cruiser
951161 Advanced Aircraft Analysis: a Powerful, User Friendly Framework for Airplane Preliminary Design and Analysis
951431 Analysis Method for the Design of Compensated Pitot-Static Probes for Use on General Aviation Aircraft
951185 Design Optimization and Sensitivity Analysis of An Aircraft Wing Using Astros
951158 G.A.-Cad, a Personal Computer Aided Design System for General Aviation Aircraft Configurations
951159 Overview of Acsynt for Light Aircraft Design
951171 Preliminary Design of a Ducted Fan Propulsion System for General Aviation Aircraft
951160 Rds-Professional: Aircraft Design on a Personal Computer
951173 The 3x Jet Engine Configuration
951148 Engineering Design for Rework of Lightning--Protection Plating on Carbon-Composite Military Airplane Parts
950503 Charles M. Manly: An Early American Innovator in Aircraft Engines
950694 Deep Drawing of Rectangular Pans From Aluminum Alloy 2008-T4
950086 Fuel Jet Models for Multidimensional Diesel Combustion Calculations: An Update
942554 A Millimeter Wave, Wireless, Lan for Use Inside An Aircraft
941950 Geometry of the Fuel Cloud Created By Impingement of a Diesel Jet Onto a Small Heated Target
942107 Integration of Design, Materials, and Processes for Airplane Interiors
942108 State of the Art Aircraft Interior Designs
942189 The Impact of New Software Engineering Technology on a New Aircraft Design Methodology
941370 Aeroshell Compared Design and Analysis for Mars Penetrators
941474 Design and Performance of the Cryogenic Two Phase Flight Experiment (Cryotp)
941288 Development of Experiment Kits for Processing Biological Samples Inflight on Sls-2
941515 Eureca Postflight Investigation
941379 Experience Acquired During Biobox Design, First Operative Flight and Refurbishment Activities
941556 Good Use of Flight Crew Time--A Guiding Principle for Eva System Design
941573 Some Evaluation Methods and Measures for Overcoming the Thermal Non-Design Conditions During the Spacecraft Flight
941503 Stand Alone Major Constituents Analyzer Flight Design
941171 An Integrated Thermal Energy Management Assessment Methodology for Advanced Hypersonic Aircraft
941185 Loop Heat Pipes: Design, Investigation, Prospects of Use in Aerospace Technics
941159 More-Electric Aircraft Integrated Power Unit Designed for Dual-Use
941231 The Usaf Aging Aircraft Program--A Short History and Status
940571 Glenn H. Curtiss: An Early American Innovator in Aviation and Motorcycle Engines
940061 The Latest Progress in the Computational Aerodynamic System for Practical Aircraft Configurations
931603 A.C.H. Support of Aircraft Conception; a Step in the Direction of Simultaneous Engineering.
931654 The Cim Philosophy and the Mobility Technology.
932574 A Brief Survey of Wing Tip Devices for Drag Reduction
932544 Advances in the Application of Laser Cutting, Drilling, and Welding Aerospace Parts
932534 Aerodynamic Tailoring of the Learjet Model 60 Wing
932632 Aerodynamic-Performance Planform and Camber Optimization of a Supersonic Transport Wing
932530 Aircraft Aerodynamic Analysis on a Personal Computer (Using the Rds Aircraft Design Software)
932533 Application of Artificial Neural Networks in Nonlinear Aerodynamics and Aircraft Design
932601 Carnard--A New Roadable Aircraft Concept
932604 Design Methodology and Infrastructures for Flying Automobiles
932605 Design and Analysis of a Telescopic Wing
932603 Design and Styling of An Advanced Flying Automobile
932623 Engine/Airframe Installation Cfd for Commercial Transport--An Engine Manufacturers Perspective
932602 Engineering Design of Starcar 3
932517 Flying Qualities Development and Flight Simulation Evaluation of the Tw-68 Tilt-Wing Vtol Aircraft
932527 Human Factors Issues in Aircraft Cabin Design
932577 Integrated Thermal Energy Management (I-Tem)--An Evaluation Tool for Aircraft
932586 New Sensor Technology for Aircraft Hydraulic System Diagnostics
932087 Design of a Water Electrolysis Flight Experiment
932085 Global Research, Global Power, a Goal Denied?
932055 Integrated Aircraft Thermal Management and Power Generation
932108 Space Station Freedom Carbon Dioxide Removal Flight Design
932059 The Active Control of Sound in Aircraft
932057 Whats Next in Commercial Aircraft Environmental Control Systems
931224 A Tool for Airframe Shaping--Idea and Application
931241 Lightning Protection Technology for Small General Aviation Composite Material Aircraft
931253 Preliminary Design of a Single Engine Business Jet
931219 Rapid Prototyping of Composite Aircraft Structures
931256 Should Large Business Jets Have Four Under the Wing
931255 Zen and the Art of Airplane Sizing
931388 A Detailed Power Inverter Design for a 250 Kw Switched Reluctance Aircraft Engine Starter/Generator
931382 A Subsystem Integration Technology Concept
931393 An Educational Introduction to Transonic Compressor Stage Design Principles
931598 Changing the Utility Subsystem Paradigm
931389 Detailed Design of a 250-Kw Switched Reluctance Starter/Generator for An Aircraft Engine
931591 Development Methodology for Contemporary Avionics Systems
931145 Ram Air Heat Exchangers for Very High-Altitude Subsonic Aircraft
931381 Suit: the Integration of Aircraft Utility Subsystems
931599 The Space Avionics Architecture Standard Tailored to the Common Lunar Lander Conceptual Design
930485 Charles Norvin Rinek: An Early American Pioneer in Advanced Aviation Engines
921514 Aircraft System Simulation Environment
921471 Analysis and Design of Microstrip Antennas for Aircraft Applications
921455 Cockpits: Design and Development
921445 Finite Element Method on Cba 123 Design and Certification
921985 An Assessment of Varying Mission Requirements on Fighter/Attack Aircraft Sizing
921938 Application of Advanced Technologies to Very Large Subsonic Transports
922036 Bidirectional Stringer-Stiffened Panel Buckling Procedures and Application to Optimum Aircraft Structures
922049 Data, Decisions, and Cockpit Technology
921947 Design Improvements in Air Turbine Start Systems
921919 Etops and Service Ready Standards and Processes
921946 Full-Range Pawl-And-Ratchet Clutch
921950 Ground Simulation of High Agility Flight
921955 Gyroscopic Test for the T800-Lht-800 Turboshaft Engine
922404 Integration of a Path Generation Algorithm Into Off-Line Programming of Airbus Panels
921925 Investigation of the Longitudinal Stability of the T-45a With Computational Fluid Dynamics
921984 Maneuvering Technology for Advanced Fighter Aircraft
921994 Overview of Supersonic Laminar Flow Control Research on the F-16xl Ships 1 and 2
922006 Subsystem Integration Technology Assessment Methodology
921911 The Tilt Wing Advantage - for High Speed Vstol Aircraft
921954 V-22 Osprey Tiltrotor Blade-Fold/Wing-Stow System Design and Testing
921570 Design Concepts and Market Opportunities for "Flying Automobiles"
929484 Modular Dips, 2.5-Kwe Modules for Lunar/Mars Surface Applications, Design Point Selection Summary
929447 Sp-100 Early Flight Mission Designs
921567 The Aerocar--Its Past and Future
921566 The Convair Flying Automobile
921185 A Thermal/Structural Analysis Process Incorporating Concurrent Engineering
921223 Applications of Ir Imagery to Thermal Evaluations
921405 Design and Development of a Two-Phase Reservoir for the Capillary Pumped Loop (Capl) Flight Experiment
921112 Space Station Water Processor: Current Flight Design
921131 The Effect of Geometric Field of View and Tunnel Design for Perspective Flight-Path Displays
921180 The Integral Vapor Compression and Liquid Coolant Refrigeration System
921017 Fighter Agility: Impact on Design, Performance and Flying Qualities
921041 Hud Guidance for the Aska Experimental Stol Aircraft Using Radar Position Information
921040 Limit Cycle in the Longitudinal Motion of the Usb Stol Aska--Control System Functional Mockup and Actual Aircraft
920989 Low-Cost Approaches to Proving of High-Risk Fast Vtol Designs
921009 SAE Aero Design 92
920967 The Integral Starter/Generator Development Progress
921015 Thrust Vectoring Fighter Aircraft Agility Research Using Remotely Piloted Vehicles
912183 270 Vdc/Hybrid 115 Vac Electric Power Generating System Technology Demonstrator Evolution to a Dual-Channel, More-Electric Aircraft Technology Development Testbed
912081 A Design of Strongly Stabilizing Controller
912186 Advanced Power Generation Systems for More Electric Aircraft
912216 Advances in Aircraft Component Superplastic Forming/Diffusion Bonding Technology
912021 Aero-Structural Integrated Design of Forward Swept Wing
911994 An Acrobatic Airship "Acrostat"
912008 An Economic Approach to Accurate Wing Design
912113 Analysis for the Application of Hybrid Laminar Flow Control to a Long-Range Subsonic Transport Aircraft
912115 Application of Laminar Flow Control to the High Speed Civil Transport--The Nasa Supersonic Laminar Flow Control Program
912116 Application of Linear Stability Theory in Supersonic Laminar Flow Design
912225 British Airways Airbus A320 Pilots Autothrust Survey
912177 Challenging Power Density Requirements for Future Fighter Apus
911990 Computational Aerodynamics in Aircraft Design: Challenges and Opportunities for Euler/Navier-Stokes Methods
911992 Computational Fluid Dynamics Applications in Airplane Cabin Ventilation System Design
912162 Concorde Airframe Design and Development
912184 Condor: An All Electric Airplane
912232 Configuration Design and Recovery Considerations for a Staged Sst
912118 Development of a Viable Hydraulic Circuit Breaker
911995 Ducted Fan Vtol for Working Platform
912215 Engineering Status of the Mcdonnell Douglas Hsct Program
912204 Enhanced Vision System Option on Future Aircraft
912056 Experimental and Numerical Study of Aerodynamic Characteristics for Second Generation Sst
912185 High Speed Civil Transport Electrical Power System Technology Requirements
912058 Integrated Wiring System
912112 Integrating An Els Into An Existing Aircraft Design
912126 Nonlinear Induced Drag Study of Generically Cambered Closely Coupled Dual Wings
912174 Quantification of Aircraft Carbon Brake Wear Using Regression Analysis and Periodic Wave Forms
912003 Recent Applications of the Fns Zonal Method to Complex Flow Problems
912129 Some Practical Aspects of Viscous Drag Reduction Concepts
912133 The Boeing 747-400 Upper Rudder Control System With Triple Tandem Valve
911967 The C-17: Modern Airlift Technology
911984 The Fatigue Scatter Factors and Reduction Factors in the Design of Aircraft and HelicopterS Structural Lives
911989 The Impact of Cfd on the Airplane Design Process: Today and Tomorrow
911969 The National Aero-Space Plane Program a Revolutionary Concept
912173 The Use of High Voltage Direct Current in Aircraft Electrical Systems--A Navy Perspective
912140 Training for Advanced Technology Aircraft--A PilotS Perspective
911993 Wind Tunnel Investigation of An Improved Upper Surface Blown-Flap Transport Semi-Span Model
911395 Analysis of An Initial Lunar Outpost Life Support System Preliminary Design
911325 Conceptual Designs for Lunar Base Life Support Systems
911366 Shuttle Orbiter Active Thermal Control Subsystem Design and Flight Experience
910990 A Computational Model for the Analysis of Finite Wings in Potential Flow
911172 Advanced Propulsion Technology Influence on Multi-Role Fighter System Requirements
911001 Astm Activities Related to Future Fuels for General Aviation
911015 Composite Prototype Aircraft Development a Method for Design, Fabrication and Test Training
911021 Conceptual Design of a Starcar
911022 Design Developments for Advanced General Aviation Aircraft
911180 Design-Integration Decision Making: What Should Be Taught
911003 Development and Certification Flight Test on the Piaggio P.180 "Avanit" Aircraft: a General Overview
911105 Gn&C for the PegasusSr Air-Launched Space Booster: Design and First Flight Results
911208 Methods for Evaluating Weight Perfection Index for Aircraft
911023 On the Feasibility of Small, Transcontinental Commuter Aircraft
910997 Propeller Technologies for Regional Aircraft
911030 Pusher Turboprop Installation Technology for the Embraer Cba-123 Vector
911171 The Development and Progress of Enhanced Fighter Maneuverability on the X-31
911178 The Role of Design in Aerospace Engineering Education
911176 Using Prototypes and Flight Validation in Teaching Aerospace Systems Design
902004 A Concurrent Design/Analysis Tool for Aircraft Hydraulic Systems
902016 A Thinner Flight Control Actuator
901986 Advanced Materials and the Pivoting Door Reverser
901972 Altitude Measurement Capability as Related to Altitude Measurement Performance
901988 Application of Favorable Aerodynamic Interference to Supersonic Airplane Design
901897 Apu Pod Design Concept for F-14 Aircraft
901806 Comparison of Dc-10 and Md-11 Designs
901983 Design Considerations of Material and Process Selection for Commercial Aircraft Engine Nacelles
901974 Developing Aircraft Altitude Measurement Standards Through Operational Flight Testing and Statistical Risk Analysis
901985 Development of Sonic Design Data for Engineering Plastics Used for Strut and Nacelle Applications
902003 Dynamic Hydrulic System Simulation--An Integrated Approach
901822 Electroluminescent Displays (El) for General Aviation Cockpits
901788 Electronic Chassis/Pwb Structures--Vibration Response Level Nonlinearities in Reliability Development Growth Testing
901875 Filter Line Wiring Designs in Aircraft
901890 Future Supersonic Transport Studies At Aerospatiale
901925 High-Speed Civil Transport Reseach and Technology Needs
901831 Hud Potential for Narrow-Bodied Air Carrier Aircarft
901829 Improving Situational Awareness Through the Use of Intuitive Pictorial Displays
901814 Minicomputer Part-Task Simulation for Helicopter Development--An Economical Approach
901923 NasaS High-Speed Research Program--An Introduction and Status Report
902005 Propulsion Technology for National Aero-Space Plane
901650 Quasi-Static Mobility Analysis Tool for the Design of Lunar/Martian Rovers and Construction Vehicles
901987 Some Thoughts on the Design of Subsonic Transport Aircraft for the 21st Century
901790 Thermal Design, Analysis, and Testing of the Crew and Equipment Translation Aid (Ceta) Space Shuttle Flight Experiment
901960 Vapor Cycle Compressors for Aerospace Vehicle Thermal Management
901936 Wingtip Vortex Turbine Investigation for Vortex Energy Recovery
901278 Conceptual Design for a Lunar-Base Celss
901219 Use of Ecs-Conditioned Air for Flir Avionics Thermal Control--Fighter Aircraft
901221 X-29 Ecs High-Alpha Modifications
901002 Air-To-Ground Attack Fighter Improvements Through Multi-Function Nozzles
901001 An Analysis of the Su-27 Flight Demonstration At the 1989 Paris Airshow
901031 Assessment of a Post 2000 Stovl Fighter
892239 A320 and B757 on the Liner--A Line PilotS Perspective
892357 An Interfacing Solution for Real-Time Avionics Development
892288 Application of Divergent Trailing-Edge Airfoil Technology to the Design of a Derivative Wing
892226 Considerations for Successful Application of Integrated Drive Generators to Aircraft
892375 Design Principles for Commercial Transport Aircraft--A PilotS Perspective
892210 Design and Certification of the All-Composite Airframe
892206 Douglas Aging Aircraft Programs
892238 Initial Service Experience With the Fokker 100
892234 Propulsion Integration for Military Aircraft
892326 Software Maintenance on the Airbus Family
892383 Unusual Statistics of Heart Period Add to Its Capability as An Index of Pilot Workload
892327 Use of Onboard Data Loaders
892237 Whats Going on After Concorde
891642 Future Civil Aircraft and Technologies
891565 Conceptual Design of a Liquid Droplet Radiator Space-Flight Experiment
891022 A Low Cost Stall/Spin Simulator
891072 Automated Aircraft Configuration Design and Analysis
891082 Beech Starship Interior Noise Experimental Studies
891052 Design Philosophy for a General Aviation Tcas Display
891046 Design and Development of the Garrett F109 Turbofan Engine
891079 Design for Maintainability
891075 Designing the V-22 "Osprey" Tiltrotor V/Stol Aircraft for Maintenance and Serviceability
891078 Enhanced Combat Damage Tolerance/Supportability for Improved Combat Sustainability
891081 Finite Element Calculations of the Interior Noise of the Saab 340 Aircraft
891060 Influence of Joint Fixity on the Structural Static and Dynamic Response of a Joined Wing Aircraft--Part I Static Response
891080 Interior Noise Control of the Saab 340 Aircraft
891039 Investigations of Modifications to Improve the Spin Resistance of a High-Wing, Single Engine, Light Airplane
891034 Propeller Development for the Rutan Voyager
891076 The Electronic Military Perspective
891084 Thermal Analysis of the Space Shuttle Wheel and Carbon Brake
891024 Virtual Prototype--The Key to Quality and Productivity
881354 Aerodynamic Technology Opportunities for a High-Speed Civil Transport
881483 Application of Ktran Transonic Small Disturbance Code to the Challenger Business Jet Configuration With Winglets
881431 Conceptual Design of a Stovl Fighter/Attack Aircraft
881432 Control Authority Considerations for Stovl Propulsion System Sizing
881397 Design Aspects of Long Range Supersonic Lfc Airplanes With Highly Swept Wings
881366 Design of Crew Rest Quarters
881412 Electrical Power System Architectures for Future Aerospace Vehicles
881500 Emergency Power Combined With An Auxiliary Power Unit
881393 Fifty Years of Laminar Flow Flight Testing
881475 Human Factors Engineering Workstation for Model-Based Cockpit Design
881524 Hypersonic Aerodynamics At North Carolina State University
881434 Locking Actuators Today and Beyond
881422 Low-Speed Vortical Flow Over a 5-Degree Cone With Tip Geometry Variations
881376 Measurement of Dynamic Reactions in Passenger Seat Legs
881410 Parallel Operation of Vscf Electrical Power Generators
881473 Rapidly Reconfigurable Crewstation Program
881472 Reconfigurable Cockpit Development
881471 Requirements for Rapid Prototyping of Crew Station Displays
881498 Secondary Power--Benefits of Digital Control and Vehicle Management System Integration
881447 Supportability Design Requirements for Army Aircraft and Equipment
881407 The All Electric Airplane Revisited
881484 Theoretical Investigation for the Effects of Sweep, Leading-Edge Geometry, and Spanwise Pressure Gradients on the Transition and Wave Drag At Transonic, and Supersonic Speed With Experimental Correlations
881353 What Drives Unique Configurations
881356 Wind-Tunnel Investigation of the Low-Speed Aerodynamics of Slender Accelerator-Type Configurations
881504 X-29a Subsystems Integration--An Example for Future Aircraft
881142 Assuring Safety and Quality in Future Advanced Aircraft
881181 Honeycomb Transportation Applications
881164 Nasa Advanced Turboprop Research and Concept Validation Program
881025 Concepts for Crew Experiment Interaction-Future Space Flights--Workstation Design and Requirements
881086 Design of a Two-Phase Capillary Pumped Flight Experiment
880998 Development of An Advanced High Altitude Flight Suit
880977 Concept of a "Flexible" Combi Aircraft
880973 Optimization of Lower Deck Cargo Systems
872463 Aerospace Co-Operative Engineering
872451 Comparision of Effects of the F-By-F Load Spectrum and the Block Load Spectrum on Fatigue Life Scatter
872437 F/A-18 as a Force Multipler Based on Designed-In Reliability and Multi-Mission Flexibility
872395 From Kitty Hawk to the Year 2000
872410 Gas Turbine Engine Development Partnerships
872445 Health and Usage Monitoring the Integrated Appproach
872436 Introduction of the Hornet--A Success Story
872443 Maintenance and Airline Safety
872411 Propulsion-Airframe Integration for Commercial and Military Aircraft
872428 Surveillance--High Technology Fit-Out for the Nomad Aircraft
872405 The Boeing 7j7--The Evolution of Technology and Design
871158 Australian Initiatives in Traffic Management and Energy--Vehicle Parameters and Interactions
880924 Preliminary Design Concepts for the Active Thermal Control of a European Spaceplane
880945 The Winning Edge
880110 High Performance Composites Research At Nasa-Langley
880251 Influence of Test-Section Length and Collector Area on Measurements in 3/4-Open-Jet Automotive Wind Tunnels
872382 A Supersonic Design With V/Stol Capability
872358 Aeroacoustics of Advanced Stovl Aircraft Plumes
872365 An Overview of the Us/Uk Astovl Collaboration
872381 Applying Vectored Thrust V/Stol Experience in Supersonic Designs
872379 Configuration E-7 Supersonic Stovl Fighter/Attack Technology Program
872347 Lift Engines-Applied History
872307 Propulsion-Induced Effects Caused By Out-Of-Ground Effects
872333 Propulsion/Aerodynamic Integration in Astovl Combat Aircraft
872349 Stovl Rcs Effects on Propulsion System Design
872335 The Application of Circulation Control Pneumatic Technology to Powered-Lift Stol Aircraft
872371 The Rsra/X-Wing Experiment: a Status Report
872331 The Vaac Vstol Flight Control Research Project
872338 Vstol Design Implications for Tactical Transports
872529 The National Aerospace Plane: a Political Overview
871883 A Close-Coupled Canard, Technology Demonstration Aircraft for General Aviation Applications
871730 Air 1900 Guide to Temperature Monitoring in Aircraft Gas Turbine Engines
871816 Application of Criteria of Aircraft Tow Tractors
871847 Canard Certification Loads--A Review of FAA Concerns
871844 Certification Issues for Electrical And/Or Electronic Engine Controls
871848 Certification of Natural Laminar Flow Technology
871809 Design of An Inlet Air Cleaner for the Black Hawk Helicopter Auxiliary Power Unit (Apu)
871756 Design of Transonic Airfoils and Wings Using a Hybrid Design Algorithm
871846 Design/Certification Considerations in Civil Composite Aircraft Structure
871882 Development of Wing and Tail Configurations for Low Altitude Unmanned Research Aircraft (Laura)
871886 Fault-Tolerant Electrical Power System
871823 Flight Deck Automation Today: Where Do We Go From Here
871761 Fly-By-Wire Sidestick Controller Evaluation
871799 On Simulation Techniques for the Separation of Stores From Internal Installations
871885 Power Quality of Aircraft Electric Systems
871807 Scale Effects on Inertial Particle Separator Efficiency
871908 Shuttle and Elv Flight Planning Using the Flight Design System
871868 Static Mechanical Properties of 30 X 11.5 - 14.5, Type Vii, Aircraft Tires of Bias-Ply and Radial-Belted Design
871781 Student Prospects in the SAE Radio Controlled Cargo Aircraft Competition
871763 The Design Eye Reference Point
871780 Utilities Management System on the Eap Demonstrator--Aircraft Power Systems Integration
871354 The First U.S. Afterburner Development
871019 Wind-Tunnel Investigation of a General Aviation Airplane Equipped With a High Aspect-Ratio, Natural-Laminar-Flow Wing
871438 Design of a Plant Growth Unit for Celss Flight Experiments
871350 Flight Research With the Mit Deadalus Prototype
871344 Hotol -- An Advanced European Space Transporter
871347 The Experimental Aircraft Programme
871346 X -- 31a
871031 Acoustic Experimental Investigation of Counterrotating Propeller Configurations
871055 Advanced Allison Small Turboprop Engines
871041 Design and Development of a Light Weight, High Pressure Ratio Aircraft Turbocharger
871042 Design and Development of the Voyager 200/300 Liquid Cooled Aircraft Engine
871046 Design of a Small Airship
871053 Evolution of Light Gas Turbine Engine During the Last 30 Years
871044 Flight Test Investigations of a Wing Designed for Natural Laminar Flow
871036 Human Factors Associated With Glass Cockpit Design
871051 Impacts of Regulations on Engine Airworthiness
871049 Optimization of Aircraft Structures Using Starstruc
871029 Potential Performance Gains for Light Aircraft By the Application of a Stator Behind the Propeller
871021 Spin Resistance Evaluation of a Light Airplane
871047 Structural Optimization of Landing Gears Using Starstruc
871025 Structures Technology of Modern General Aviation Aircraft
871040 The Merlyn Diesel Concept for Propulsion
872525 Advanced Technology Cockpit Design and the Management of Human Error
861726 Integrated Flight/Propulsion Control for Next Generation Military Aircraft
872507 U.S. Army Human-Error-Related Data Bases
861617 Aircraft Fire Safety Overview
861686 Higher Cruise Speed Commercial Aircraft Evolution
861650 A Cooperative Launch Optimization Technique Using the Flight Design System
861631 A Parametric Approach to Hover Balance Analysis of Two Stovl Fighter Concepts
861814 A University Flight Simulation Laboratory
861673 Application of Advanced Composites in Civil Aircraft
861152 Cargo Airlift -- Whats Old, Whats New
861727 Design Verification and Engine Test of An Advanced Fuel Management System for Aircraft Gas Turbine Engines
861714 Development of a Hot Gas Vane Motor for Aircraft Starting Systems
861645 Flow Patterns of a Pivoted Rectangular Wing Aircraft
861719 Installation Aerodynamics of Wing-Mounted, Single-Rotation Propfans
861675 Lessons Learned From the Dc-10 Carbon-Epoxy Rudder Program
861690 Military Aircraft System Engineering
861852 Pitch Axis Control System Design for Qf-4 Full-Scale Aircraft Target
861846 Reynolds Number Extrapolation of Transonic Wing Pressure Data Affected By Shock-Induced Separation
861388 Structural Design Considerations for Ultralight Aircraft
861697 Summary of Windshear Accidents and Views About Prevention
861637 Tactical Jet V/Stol -- Its Future in a Ctol World
861630 Takeoff Predictions for Powered-Lift Aircraft
861632 The Av-8b Goes Aboard -- Tacair Operations From the Lhd 1
861684 The Market Potential of Future Supersonic Aircraft
861825 The Use of Skewed Inertial Sensors in Flight Control Systems
861642 X-29 Flight Test Program Including Wind Tunnel and Computational Support
861153 "Flexible" Cargo Handling Systems for Standard-Body Airplanes
861154 Meeting the Air Cargo Challenge: BoeingS Aircraft Developments
861161 Obco -- on Board Cargo Operation System
860937 Giotto -- In-Flight Thermal Performance
860928 Habitation Module for the Space Station
861003 Shuttle Waste Management System Design Improvements and Flight Evaluation
860913 X-29 Fuel/Auxiliary Oil Systems Thermal Management
860819 A Review of Crash-Related Analyses Conducted At NasaS Langley Research Center
851886 Antimisting Fuel Technology for Transport Category Aircraft
851982 A European Experience on International Collaborations
851753 A System Look At Actuation Concepts and Alternatives for Primary Flight Control
851754 Advanced Flight Control Actuation Systems and Their Interface With Digital Commands
851766 Alpha Jet Training System Single Aircraft Concept
851903 Application of the Optimal Control Model to the Design of Flight Simulation Experiments
851851 Avionics System Architecture for Beechcraft Starship 1
851884 Controlled Impact Demonstration Review
851793 Engineering Applications of An Advanced Low-Order Panel Method
851901 Engineering Flight Simulation--A Revolution of Change
851940 European Aircraft Steering Systems
851887 FAA Structural Crash Dynamics Program Update--Transport Category Aircraft
851865 Flight Planning With the Nasa Flight Design System
851768 Hawk: the British Fighting Trainer
851816 Leading-Edge Design for Improved Spin Resistance of Wings Incorporating Conventional and Advanced Airfoils
851885 Nasa Experiments Onboard the Controlled Impact Demonstration
851806 Pilot Executive Project--Pilex
851836 Pilot Interface With Fly-By-Wire Control Systems
851759 Preliminary Design of Electromechanical Servosystems
851961 Product Support--A Technical Life Line
851752 Reducing Complexity in Fly-By-Wire Flight Control Actuators
851813 Retrofitting Avionics: Closing the Performance "Generation Gap"
851977 Sr-71 Digital Automatic Flight and Inlet Control System
851950 Techniques for Sortie Generation Analysis
851767 The Casa C-101 Advanced Trainer/Light Ground Attack Aircraft for Today and the Future
851774 The Development and Evaluation of Color Systems for Airborne Applications--Fundamental Visual, Perceptual, and Display Systems Considerations
851769 The Emb-312 Tucano--A Brazilian Trainer
851841 The Impact of Technology on Fighter Aircraft Requirements
851900 The Role of Flight Simulation in Helicopter Crew Station Design
851888 Transport Aircraft Crashworthiness Requirements--An Industry View
851518 Design of a Two-Stroke Cycle Spark Ignition Engine Employing a Scotch-Yoke Crankshaft Mechanism
851316 Digital Control for Engine Bleed Air
851318 Environmental Control System Simulation Using Easy5, as Applied to the F-14
850891 Design and Fabrication of Marvel Ii Wings
850872 Propulsive Efficiency and Aircraft Drag Determined From Steady State Flight Test Data
850912 A Full-Time Yaw Damper for the Starship Flying Scale Prototype
850900 Advanced Systems for the Gulfstream Iv
850861 An Experimental Study of a General Aviation Single-Engine Aircraft Utilizing a Natural Laminar Flow Wing
850859 An Investigation of the Effects of the Propeller Slipstream on a Laminar Wing Boundary Layer
850866 Analytical Study of Three-Surface Lifting Systems
850855 Crashworthy Design Considerations for General Aviation Seats
850890 Design Data and Buckling of Laminated Composite Triangular Plates
850888 Design and Certification of a Composite Control Surface
850893 Design and Use of KevlarSr in Aircraft Structures
850876 Flight Investigation of Cabin Noise Control Treatments for a Light Turboprop Aircraft
850902 Head-Up Displays for General Aviation
850865 Interdependence of Parameters Important to the Design of Subsonic Canard-Configured Aircraft
850879 Mechanisms of Transmission and Control of Low-Frequency Sound in Aircraft Interiors
850864 Natural Laminar Flow and Regional Aircraft
850878 Noise Transmission Characteristics of Aircraft-Type Composite Panels
850894 Single-Engine Propulsion Improvement Through Intercooling
850881 Sport Aircraft Design Trends: Shaping the Future of General Aviation
850892 Stress Concentration At a Rectangular Cutout in a Buffer Strip Laminate
850889 Stress Concentrations Study on Composites Using Photo-Stress Methods
850917 The Structural Dynamics of Electro-Impulse De-Icing on the Lear Fan Kevlar Composite Leading Edge
850915 Usaf Damage Tolerance Methods Applied to General Aviation Aircraft Design and Analysis
856122 Application of Fluidics Technology to the Development of Antilock Brakes for Motorcycles
841509 Air Turbine Starter Sizing for a Proper Bleed Source Match
841605 Airplane Mounted Accessory Gearbox Design
841508 Computer-Aided Start-System Design and Verification
841555 Estimation of Hot Gas Reingestion for a Vtol Aircraft At the Conceptual Design Stage
841472 Flight Deck Design Methodology Using Computerized Anthropometric Models
841465 Flight Deck Displays for Managing Wind Shear Encounters
841513 Low-Density Aluminum Alloy Development
841436 Machinability of Advanced Aerospace Materials
841627 Opportunities and Challenges for Electric-Drive Systems on Aircraft
841510 Peak Transient Torques in Pneumatic Starter-Engine Systems
841498 Recent Developments in Ejector Design for V/Stol Aircraft
841638 Situation Versus Command
841018 An Overview of the Nasa Rotary Engine Research Program
841021 Summary of the Weight and Balance, and the Drag Characteristics of a Typical Ultralight Aircraft
840943 Improvements in the Vapor Cycle Capability of the Advanced Environmental Control System Computer Program
840950 Monogrove Heat Pipe Radiator Shuttle Flight Experiment: Design, Analysis, and Testing
840028 "Phoenix--"A Polyester-Film Inflatable Man-Powered Aircraft
840027 Five Years Experience With Minimum Induced Loss Propellers--Part Ii: Applications
831482 A Design Approach to Integrated Flight and Propulsion Control
831556 Commercial Transport Technology Advances
831550 Design of An Advanced Composite Outer Duct for the F404 Engine
831465 Flight Management--The Real Man Machine Interface
831516 How Aerospace International Standards Will Impact New Design - Fluid Systems, Iso/Tc20/Sc 10
831513 How Aerospace Iso Standards Will Impact New Designs Sc-1 Electrical Requirements
831426 Multi-Functional Nozzle for Advanced Weapon Systems
831492 Nacelle Design for Grumman Design 698 V/Stol
831406 The Effect of Regulation 25.1309 on Aircraft Design and Maintenance
831515 The Impact of Iso/Tc20/Sc9, Air Cargo and Ground Equipment Standards on New Aircraft Design
831536 The Joint Services Advanced Vertical Lift Aircraft (Jvx) Propulsion System
831118 The Shuttle Orbiter Thermal Protection System Materials, Designs, and Flight Performance Overview
830759 A New Sensor Approach to An Attitude/Heading Reference System
830713 Aircraft Night Lighting Systems
830692 Compact, High Efficiency Plasma Spray Guns for Jet Engine Coatings
830712 Design Consideration for Lighting Modern Commercial Aircraft
830755 Design of the Low Vibration Turboprop Powerplant Suspension System for the Dash 7 Aircraft
830770 Development of Wing Leading Edge Vortex Generators for a Single Engine General Aviation Airplane
830734 Evaluation of the Acoustic Intensity Approach to Identify Transmission Paths in Aircraft Structures
830707 Final Evaluation of Multi-Viscosity Oils Designed for Aircraft Reciprocating Engines
830717 Flight Investigation of Natural Laminar Flow on the Bellanca Skyrocket Ii
830763 Handling Qualities of Canards, Tandem Wings, and Other Unconventional Configurations
830724 Protection Against the Direct Effects of Lightning Strikes for a Carbon Fiber Composite Aircraft
830771 Small, Versatile Remote Controlled Circuit Breaker Design Complements Next Generation Aircraft System Requirements
830735 Structureborne Contribution to Interior Noise of Propeller Aircraft
830709 Studies of Light-Twin Wing-Body Interference
830728 The Microprocessor and the Airplane: the Evolution of An Intelligent Trim System
830756 The Tfe731-5: Evolution of a Decade of Business Jet Service
830710 Unconventional Commuter Configurations: a Design Investigation
830720 Wing Modification for Increased Spin Resistance
821559 747 Freighter Service: Developments of Success
820716 A Review of Commuter Propulsion Technology
821345 Advanced Aluminum Alloy for Transport Aircraft--Why and What Are the Benefits
820720 Advanced Propeller Technology for New Commuter Aircraft
820731 Advanced Technology for Future Regional Transport Aircraft
821552 American Airlines Hub Plane Operation
820956 Applications of Advanced Upper Surface Blowing Propulsive-Lift Technology
821360 Cabin Noise Weight Penalty Requirements for a High-Speed Propfan-Powered Aircraft--A Progress Report
821558 Derivative Air Freighters Are Winners
821436 Design Aspects of Systems in All-Electric Aircraft
820722 Design Considerations for Ease of Maintenance in Commuter Aircraft
821426 Design and Flight Test of One-Man Operability in the F/A-18
821346 Design of An Aerobatic Aircraft Wing Using Advanced Composite Materials
820732 Design of Unconventional Commuter Configurations
820877 Evaluating Scroll Refrigerant Compressors for Reducing Size and Weight of Military Aircraft Ecs
821469 Flight At Supernormal Attitudes
821508 Future Rotorcraft Technologies
821415 How the Air Force Plans and Executes Composites Roadmaps
821340 Human Factors Approach in Certification Flight Test
821391 Impact Protection in Air Transport Passenger Seat Design
821359 Inlet Design for High-Speed Propfans
820961 Interior Noise of General Aviation Aircraft
821555 Interoperability of Military and Civil Air-Cargo Systems
821468 Optimal Turning Climb-Out and Descent of Commercial Jet Aircraft
821442 Re-Engining the 737
821375 Supersonic Stovl Research Aircraft
821556 Systems Analysis of Preliminary Aircraft Designs for Commercial Cargo Service
820955 Technology Status for An Advanced Supersonic Transport
821434 The All Electric Airplane--Benefits and Challenges
820730 The Cac-100 - Design Features
820728 The Dash 8-Design Considerations
820871 Thermal Design of Integrated Avionic Racks for Aircraft
820878 Thermal Design of Standard Avionic Enclosures
821504 U.S. Army Helicopter Icing Developments
821384 Utilization of the B.Ae. Advanced Flight Deck
821421 Validation of the Kc-10 Refueling Boom Digital Control System
820104 Voice Interface for Transport Aircraft Cockpits
811039 Airworthiness Considerations in the Design of Commercial Transport Aircraft
811081 Design Considerations of Dc-Link Aircraft Generation Systems
811055 Design Technology for Improved Performance Retention in Turbofan Engines
811038 Designing for Continued Airworthiness--General Aviation
811096 Fighter Issues - 2000
811099 Future Strike Fighter Options ... Concepts and Technologies
811066 Integration of Energy Management Concepts Into the Flight Deck
811035 Mission-Adaptive Wing Flight Demonstration Program
811097 Quality, Quantity, and Technology--A Perspective on Fighter Development
811072 Restoration of Performance, Models 727, 737, and 747
811098 Tactical Air-To-Surface Requirements for the 1990s
811100 Technology for Quality and Quantity in a New Fighter
811036 The Anatomy of a Technology Test Bed - Integrated Flight/Fire Control - I (Iffc I)
811085 The Impact of the Microprocessor on Aircraft Electric System Control Philosophy
811091 The Use of "Kapton" Polyimide Film in Aerospace Applications
810846 757/767 Flight Crew Interface
810853 Aircraft Noise Control Practices Related to Ground Transport Vehicles
810625 Aerodynamic Design Data for a Cruise-Matched High Performance Single-Engine Airplane
810630 An Assessment of Advanced Technologies for Application to General Aviation
810618 Avco LycomingS Alf 502 High Bypass Fan Engine
810628 Binocular Camera for Cockpit Visibility of General Aviation Aircraft
810637 Design Allowable Factors in Composite Materials
810640 Fibre Reinforced Composite Applications At De Havilland
810623 Full-Scale Study of the Cooling System Aerodynamics of An Operating Piston Engine Installed in a Light Aircraft Wing Panel
810617 Human Factors Aspects of Emergency Egress From a Business Jet
810622 Small Turbofan Engines: Their Impact on General Aviation Aircraft
810629 Summary of High-Lift and Control Surface Research on Nasa General Aviation Airfoils
810615 Us Army Crashworthiness Program
810604 A Prediction Procedure for Propeller Aircraft Flyover Noise Based on Empirical Data
810569 Aircraft Multi-Bus Electrical System Using a Hall-Effect Sensing Device
810614 Aircraft Subfloor Response to Crash Loadings
810577 Analytical Studies on the Effect of Cooling Flows on Light Aircraft Drag
810613 Crashworthy Design Concepts for Airframe Structures of Light Aircraft
810606 Effects of Wingtip Modifications on Handling Qualities of Agricultural Aircraft
810572 Evaluation of Multi-Viscosity Oils Designed for Aircraft Reciprocating Engines
810566 Integration of Propeller Slipstreams Into the Aerodynamic Analyses of Bodies
810608 Leading Edge High Lift Devices for Agricultural Aircraft
810561 Noise Transmission and Attenuation for Business Aircraft
810607 Predicting Aerially Applied Particle Deposition By Computer
810609 Structural Design--The Mother of Invention
810564 Studies of Hingeline Gap, Trailing Edge Treatment, Lower Surface Deflector on Spoiler Characteristics and Flow
810565 Transonic Wing Design Using Potential-Flow Codes--Successes and Failures
810605 Vortex Drag Reduction By Diffusing Vanes: Design for the "Thrush" Agricultural Aircraft
810575 Wind-Tunnel Measurements of Wing-Canard Interference and a Comparison With Various Theories
801169 757/767 Flight Management System
801180 Ad-1 Oblique Wing Aircraft Program
801209 Adhesive Bonding of Aircraft Primary Structures
801212 Advanced Graphite Composites in the 757/767
801155 Aerodynamic Surface Cooling for Laminar Flow Control for Hydrogen-Fueled Subsonic Aircraft
801132 Air Transport Flight Parameter Measurements Program--Concepts and Benefits
801065 Airbus IndustrieS Approach to the Wide-Body Freighter Aircraft Concept
801241 An Affordable Means of Increasing Sea-Based Air Power
801168 Application of Crt Displays to the Cockpit of Tomorrow
801125 Applications of Structural Dynamics Modification
801228 Av-8b Operational Features for Rapid Deployment
801138 Composite Wall Concept for High-Temperature Turbine Shrouds--Heat Transfer Analysis
801176 Feasibility of Forward-Swept Wing Technology for V/Stol Aircraft
801064 Flatbed -- a Unique and Versatile Transport Airplane
801175 Himat Systems Development Results and Projections
801165 History of SAE Committee S-7, Flight Deck and Handling Qualities Standards for Transport Category Aircraft
801173 Inspection of Turbine Blades Using Computer Aided Laser Technology
801210 Integrated Active Controls Impact on Supersonic Cruise Vehicle Structural Design
801170 Integrated Cad/Cam for the 1980s
801052 Joint Civil/Military Cargo Aircraft: Prospects and Current Perceptions
801059 Joint Civil/Military Transport Studies -- An Overview
801226 Multi Service Applications for Advancing Blade Concept Aircraft
801216 National and International Drawing Standards: Moving Toward Better Alignment With Y14.5
801227 Nuclear Hardness Assurance for Aeronautical Systems
801218 Overview of Arp 1587 Aircraft Gas Turbine Engine Monitoring System Guide
801178 Preliminary Aerodynamic Characteristics of Several Advanced Vstol Fighter/Attack Aircraft Concepts
801153 Status of the Program to Develop LhD2 for Aircraft
801208 The CadamSr System for Aircraft Structural Design
801145 The Evolution of Fiber Optics in Avionics
801148 The High Performance Auxiliary Power Unit Technology Demonstrator Program
801215 The Impact of Engineering Drawing Standards on Product Quality
801179 V/Stol Capability By Modifying Ctol Aircraft
800602 A New High Bypass Fan for General Aviation
800610 Advanced Materials for Agricultural Aircraft
800743 Aircraft of the Future
800601 Business Aircraft Turbofan Technology Progress in the 1970S, Challenges in the 1980S
800621 Evolutions in Business Jet Fuel Systems as Seen in the Falcon Jet Series
800630 Experimental Investigations to Fully Map the Flow Field Around a Wind Tunnel Model of a Transport Airplane
800605 Forward Swept Wings and Business Airplanes
800609 Lear Fan Propulsion System
800733 Propfan Propulsion for Commercial Air Transports
800756 Prospects for Hydrogen Aircraft
800755 The Future of Short-Haul Transport Aircraft
800754 The Growing Age of Specialization in Air Transportation
791057 "Quiet Please"
790603 A New Light Twin Using Bonded Metal Construction
790602 Canadair Challenger Flight Test Status
790578 Composite Applications At Bell Helicopter
790146 Composite Applications to Aircraft Structures Now and in the Future
790147 Composite Horizontal Stabilizer for the B-1--Design, Fabrication, and Test
790605 Concepts for Reducing Exhaust Emissions and Fuel Consumption of the Aircraft Piston Engine
791067 Constant Speed 400 Hz Aircraft Electric Generation System
790580 Design Description of a Four-Place Business Jet Using Two Wr-19 Engines
790631 Designing With Damping Materials to Reduce Noise and Structural Fatigue
791069 Development and Flight Test of a Two-Place Night/Adverse Weather A-10 for the Close-Air Support and Battlefield Attack Mission
790617 Development of the Beechcraft Model 77
791082 Effects of Forebody, Wing and Wind-Body-Lex Flowfields on High Angle of Attack Aerodynamics
790564 Effects of a Spin Chute Installation on Spin Characteristics
791054 Energy Conservation With Variable Displacement Pumps and Motors
791108 Fighter Options for Tactical Air Defense
791097 Future Multi-Mission Transport Aircraft: Requirements and Design Possibilities
790614 General Aviation Aircraft Design for Performance Using Small Computers
791085 High-Angle-Of-Attack Flying Qualities--An Overview of Current Design Considerations
791056 High-Efficiency Hydraulic Power Transfer Units for Multisystem Aircraft
790582 Improving Business Jet Performance: the Mark Five Sabreliner
791081 Mcair Design Philosophy for Fighter Aircraft Departure and Spin Resistance
791089 Multi Rotor Options for Heavy Lift
791096 Multirole Cargo Aircraft Options and Configurations
790613 New Technologies for General Aviation Aircraft
790585 Practical Design of Minimum Induced Loss Propellers
791071 Production Eagle and Its Potential
790598 Proper Aircraft Tire Size Selection--Optimum Performance With Minimum Maintenance
791111 Quantitative Evaluation of Deficiencies (Qed) and Deficiency Analysis Ranking Technique (Dart)
790616 Recent Results Obtained With a New Method for Measuring Aircraft Power and Drag in Flight
791109 Reliability and Maintainability Design Standards From Readiness-Related Goals
790620 Rolls-Royce Rb.401-07 Turbofan Engine for Business Aircraft in the 1980S
790590 Seat/Occupant Crash Dynamic Analysis Verification Test Program
791087 Single Rotor Options for Heavy Lift and Potential of Multi Lift
790604 Some Theoretical Considerations of a Stall Proof Airplane
790565 Spin Flight Research Summary
790575 The Design and Selection of Optimum Propellers for General Aviation Aircraft
790593 The Impact of Noise Regulations on Propeller Design
791093 The Kc-135--A Successful Multirole Transport Aircraft
790581 The Learjet "Longhorn" Series--The First Jets With Winglets
791105 The Role of Technology in Future Air-To-Surface Systems
790573 Wind Tunnel Performance of Four Energy Efficient Propellers Designed for Mach 0.8 Cruise
781030 Applying Design-To-Life Cycle Cost Methods During Engine Advanced Development
781021 Damage-Tolerance Practices Applied to Transport Aircraft Structures
781010 Environmental Factors Affecting the Installation and Operation of Gas Turbine Engines in Agricultural Aircraft
780874 Future Large Cargo Aircraft
780548 Piloted Aircraft Simulation - Advantages, Disadvantages, and Practical Problems
780997 Propeller Slipstream/Wing Interactions At Mach No. 0.8
781019 Recognition of Damage - Tolerance in Civil Airworthiness Standards
781017 Strike Drone--A Defense Suppression Concept Using Unmanned Cruise/Loiter/Attack Vehicle
780078 The Design and Development of the Upper-Pivoted Sonic Carburetor
780554 The Need and Impact of Long-Term Advances in Aircraft Technology: the Airlines Point of View
780551 The Promise of Advanced Technology for Future Air Transports
781050 Use of Radio Controlled Models in the Conceptual Development of V/Stol Aircraft
781038 V/Stol Aircraft Engine and Mechanical Drive Component Integration
770459 A Prediction Method for Spoiler Performance
770468 A Study of Simplified Methods for Longitudinal Control Decoupling
770966 Advanced Concepts for Sea Control
770455 Aeroelastically Tailored Propellers
770479 An Approach to Subsonic, Turbulent Flow Airfoil Design Using Mini-Computers
770440 Application of Numerical Optimization to the Design of Supercritical Airfoils Without Drag-Creep
770952 Army Uttas Program
770999 Design and Analysis of Propellers for Low Reynolds Number Application to Mini-RpvS
770355 Design of a Plasma Jet Ignition System for Automotive Application
770441 Flight Test Data for Light Aircraft Spoiler Roll Control Systems
770965 Land-Based Aircraft Options for Naval Missions
770446 Noise Effects on Passenger Communication in Light Aircraft
770453 Optimal Design of Composite-Material Panels for Business Aircraft
771008 Preliminary Qcsee Program Test Results
770460 Recent Conceptual Design Studies of Single Turbofan Engine Aircraft
770280 Some Uk Progress in Sodium Sulphur Technology
770474 The Controlwing Aircraft
770985 The Impact of Emerging Technologies on Tactical V/Stol Airplane Design and Utility
770454 The Influence of Curriculum on Aerospace Design Decisions
770444 The Influence of Design Parameters on Light Propeller Aircraft Noise
770481 Use of Simplified Flow Separation Criteria for Slotted Flap Preliminary Design
760439 Air Freighting in Middle East Industrial Development: the Role of the Wide-Body Aircraft
760462 A Data Acquisition System for In-Flight Airfoil Evaluation
760922 A Modern Technology, Open-Ocean Seaplane Design
760500 A Systems Approach to Aviation Safety: FAA Comments on Design for Regulatory Compliance--A Safety System
760503 A Worldwide System to Ensure a Satisfactory Level of Safety
760509 Air Transport Propulsion Improvement Opportunities With Advanced Controls
760494 Aircraft Crashworthiness: a Blight Or Panacea and Mr. Engineer--Are You Responsible
760538 Aircraft Propulsion, a Key to Fuel Conservation, An Aircraft ManufacturerS View
760477 Airfoil Section Drag Reduction At Transonic Speeds By Numerical Optimization
760929 Airframe Technology for Energy Efficient Transport Aircraft
760896 Boundary Layer Considerations for Optimization of Acoustic Liners for Aircraft Engine Ducts
760501 Design for Regulatory Compliance--A DesignerS Viewpoint
760468 Design, Development and Flight Test of the Cessna Citation Thrust Reverser
760508 Economic Benefits of Digital Electronic Propulsion Controls for Advanced Commercial Aircraft
760510 Factors to Be Considered in Applying New Technology in the Airline Environment
760478 Feasibility Study of Propeller Design for General Aviation By Numerical Optimization
760476 General Aviation Design Synthesis Utilizing Interactive Computer Graphics
760491 High Altitude Applications of the Gates Learjet
760937 Interactive Graphics in the F-18 Design
760473 Laminar Flow Rethink-Using Composite Structure
760486 Lightning Protection of Aircraft Fuel Caps
760512 Management of Service Deficiencies--A Component Manufacturers View
760514 Managing Service Deficiencies--A Pilot Perspective
760459 Parametric Analysis of Advanced Technology Applied to a Single Engine Trainer
760521 Powered Wheels for Aircraft
760481 Reduction of Stall-Spin Entry Tendencies Through Wing Aerodynamic Design
760482 Reflection-Plane Tests of Spoilers on An Advanced Technology Wing
760483 Review of the General Aviation Drag Reduction Workshop
760589 Sailplanes: the State-Of-The-Art
760480 Statistical Analysis of General Aviation Stall Spin Accidents
760540 Status Review--Yc-15 Advanced Medium Stol Prototype
760920 The Development and Flight Testing of the Xc-8a Air Cushion Landing System (Acls)
760905 The F-15 Multi-Mission Aircraft Program Status
760935 The Impact of Effectiveness Considerations on Design Synthesis
760909 The Impact of Emission Standards on the Design of Aircraft Gas Turbine Engine Combustors
760507 The Influence of Microcomputer Technology on Propulsion Management System Design
760471 The Mark Ii Learjet From Concept to Certification
760590 The Pazmany Pl-2 and Pl-4 Airplanes
760539 Yc-14 Status Report
750546 "Melmoth"--An Experimental Private Aircraft
751063 A Design Study of the Application of a Simplified Aircraft Fuel Control Method to Automotive Gas Turbines
750536 A Second Generation Turbo-Prop Power Plant
750617 Advanced Supersonic Transport
751091 Aircraft Pay-Offs and Requirements for a Jet Flap Propulsion System
750631 Ast Propulsion Comparisons
750586 Challenges of Short-Haul Air Transportation
751114 Component Performance and System Payoff for Advanced Internal Power Generation Unit
750537 Crashworthiness Investigation of General Aviation Accidents
751044 Design Freedom Offered By Fly-By-Wire
750619 Design of Jet Engine Rotors for Long Life
750524 Design of Low-Speed Airfoils By Numerical Optimization
750587 Design of Short Haul Aircraft for Fuel Conservation
750628 Engine Design Considerations for 2nd Generation Supersonic Transports
801244 Factors Affecting the Future of Commercial Aviation
750529 Flight Mechanics and Pilot Evaluation of Conventional Landings
751046 Fly-By-Wire Flight Control System Design Considerations for Fighter Aircraft
750615 Future Hydrogen Fueled Commercial Transports
750618 Future Lighter-Than-Air Concepts
750548 Handling and Performance Characteristics of Swept-Forward Flying Wing Aircraft
751051 Impact of Active Controls on Future Transport Design, Performance, and Operation
750620 Improving Performance Retention of High Bypass Engines
751120 Powerplants--Past, Present and Future
751088 Predicting Propulsion Related Drag of Jet Aftbodies
751092 Propulsion Concepts for High Speed Aircraft
750605 Quiet Clean Short-Haul Experimental Engine (Qcsee) Design Rationale
751109 Remotely Piloted Vehicle Technology Development Using the Xqm-103 Research Test Vehicle
751113 Rpv Autoland
750547 Some Ideas of Vortex Lift
750502 Summary of Systems Design Studies of Turbofan Powered Light Aircraft
751110 Teleplane and Mini Rpv Technology
750514 The B-1 Structural Integrity Program
750633 The Perceived Needs of the Short-Haul Air Carrier
750616 The Spanloader Advanced Transport Concept
750510 The Use of Plastic Foam in Metal Sailplane Construction
750543 Tri-Gull Amphibian Development
751079 Vectored Lift Advanced Fighter Technology Integrator
751103 Vertical Attitude Takeoff and Landing Remotely Piloted Demonstration Vehicle
750523 Wind Tunnel and Flight Development of Spoilers for General Aviation Aircraft
740365 A Fowler Flap System for a High-Performance General Aviation Airfoil
740359 A Quiet Propeller for Commuter and General Aviation Aircraft
740044 A Systems Engineering Evaluation of Passive Restraint Systems for Crash-Impact Attenuation in Air Transport Aircraft
740452 Acls for a Commercial Transport
740870 Advanced Composite Design Concepts for the Amst
740453 Advanced Controls for Commercial Transport Aircraft
740860 Afti Ti-1 Program
740399 Aircraft Applications for Electroless Nickel Plate
740891 Airline Tow Tractor--Baggage/Cargo Factors for Design Consideration
740395 Amphibian Aircraft Design
740488 Amphibian Stol and Its Facilities
740884 An Engine Project EngineerS View of Advanced Secondary Power Systems
740451 Application of Hydrogen to Commercial Transports
740277 Consolidated Presentation of Fatigue Data for Design Applications
740843 Design, Integration, and Testing of the F-15
740360 Evaluation of Aircraft Internal Noise
740842 F-14a Status Report: Operational Capabilities, Program Accomplishments, and Cost
740885 F-15 Secondary Power Systems
740861 F-4/Ccv-Flight Tests of Advanced Technology
740489 FAA Aircraft Retrofit Feasibility Program
740368 Flight Test Results for An Advanced Technology Light Airplane Wing
740859 Himat -- a New Approach to the Design of Highly Maneuverable Aircraft
740495 Impact of Increasing Secondary Power Requirements on Engine and Accessory System Design
740815 Improved Vibration Design and Test Procedure for Aircraft
740481 Integrated Flight/Propulsion Control Design Techniques Starting With the Engine
740467 Investigation of Noise From Full-Scale High Bypass Engine and Blown Flap System
740832 J58/Yf-12 Ejector Nozzle Performance
740470 Low-Speed Aerodynamics of the Upper-Surface Blown Jet Flap
740352 Nasa General Aviation Research Overview
740398 Potential Use of Work Hardening Aluminum Alloy X5090 Sheet in Civil Aircraft
740502 Powered Lift for Longer Field Lengths and Longer Missions?
740471 Propulsion Integration for a Hybrid Propulsive-Lift System
740455 Propulsion System Sizing for Powered Lift and Mechanical Flap Quiet Aircraft
740490 Reduction of Jt8d Powered Aircraft Noise By Engine Refanning
740465 Secondary Power Systems
740385 Semimonocoque Beam Analysis: a Displacement Formulation
740458 Sonic Inlet Technology Development and Application to Stol Propulsion
740354 Stall/Spin Research Status Report
740370 T-Tail Aerodynamics of the Super King Air
740393 The Aerocar "Flying Automobile"
740361 The Background to Propeller Airplane Noise Regulations
740376 The Design of Crashworthy General Aviation Aircraft
740485 The Experimental Clean Combustor Program--Description and Status
740392 The M. I. T. Man-Powered Aircraft
730936 An Integrated Approach to Structural Weight Estimation
730891 Application of Advances in Structures and Materials to the Design of the Yf-17 Airplane
730332 Computer Aided Parametric Analysis for General Aviation Aircraft
730934 Computer-Aided Design and Drafting (Cadd): An Advanced DesignerS Tool
730303 Control-Configured General Aviation Aircraft
730378 Design Studies of Low-Noise Propulsive-Lift Airplanes
730319 Development of Airframe Design Technology for Crashworthiness
730948 Development of Requirements For, and Evaluation Of, Manufacturer Advanced Design Aircraft
730353 Development of the A300b Wide-Body Twin
730959 Effect of Exhaust Deflectors on the Design of Lift Plus Lift/Cruise V/Stol Aircraft
730945 Evaluation of Advanced Air Vehicle Designs in the Usaf
730947 Evaluation of V/Stol Research Aircraft Designs
730330 Feasibility and Optimization of Variable-Geometry Wing for Jet Amphibian Business Aircraft
730354 Key Factors in Developing a Future Wide-Bodied Twin-Jet Transport
730881 Maintainability Concepts Used in the Design and Operation of Douglas Commercial Jet Aircraft
730317 Nasa in General Aviation Research -- Past -- Present -- Future
730304 Separate Surfaces for Automatic Flight Controls
730308 Stepped Aluminum Extrusions -- Designing for Business Aircraft
730913 Stol Tactical Aircraft Investigation
730325 The Development of Reciprocating Engine Installation Data for General Aviation Aircraft
730890 The Influence of Design to Cost and Prototyping on the A-10 Aircraft
730933 Use of Simulators in the Design and Development of Flight Control Systems
720337 Consideration of Application of Currently Available Transport-Category Aerodynamic Technology in the Optimization of General Aviation Propeller-Driven Twin Design
720712 Design and Development of a Small Highly Loaded, Two-Stage, Transonic Axial Compressor
720322 Energy-Absorbing Seat Design for Light Aircraft
720323 Methods of Crashworthiness Testing for Aircraft Design
720319 Nasa Advanced Transport Technology Program
710401 Analytical Simulation of Landing Gear Dynamics for Aircraft Design and Analysis
710465 Comparison of Stol Design Criteria for Commercial and Military Transport Aircraft
710750 Crystal Ball Focuses on the Next Generation of Transport Aircraft
710759 Design Comparison of Quiet M=0.80 Stol Transports
710444 Design Criteria for Selection of Aircraft Electric Power Generation and Distribution Systems
710447 Design Integration - the Key to Effective Aircraft Engine Condition Monitoring
710747 Designing Aircraft for Producibility: Design-Influenced Production Cost Program
710755 Development Status of the L-1011 Tristar
710426 Development of the Lockheed L-1011S Flying Stabilizer
710423 Economics of Subsonic Transport Airplane Design, Evaluation and Operation
710431 FAA Appraisal of Aircraft Design for Maintainability
710393 Flight Control System Providing a Simple-To-Fly, Constant Attitude Aircraft
710749 Future Trends in Aircraft Design
710462 High-Temperature Aircraft Turbine Engine Design Considerations
710388 Influence of Bobweights and Downsprings on Flying Qualities
710777 Influence of Powerplant Design of Airplane Operational Effectiveness - the OperatorS Point of View
710762 Installation and Integration of Transonic Transport Propulsion Systems
710406 Occupant Impact Injury Tolerances for Aircraft Crashworthiness Design
710411 Role of Military Aviation Greases in Subsonic Commercial Airplane Design
700240 An Assessment of Performance, Stability, and Control Improvements for General Aviation Aircraft
700241 Cessna Citation Design Factors and Philosophy
700202 Computer Utilization for Aircraft Contour Determination
700772 Cost/Design Performance Management During System-Definition Phase of Large, Complex Aerospace Programs
700539 Design Considerations in Selecting Alloys for Aircraft Structures
700805 Design of Engine Pods for Lockheed L-1011 Trijet for Minimum Noise
700231 Design of General Aviation Airports and Heliports
700837 Designing the Ov-10a Forward Air Control and Light Attack Aircraft
700242 Development of American Aviation CorporationsS Yankee
700925 Effects of Lightning Attachment Phenomena on Aircraft Design
700789 Future Airplane Hydraulic Distribution System Design Developments and Testing Criteria
700045 Grounding the Aircraft Gas Turbine - the Design Conversion From Air to Surface Use
700234 Human Factors in Aircraft Interior Design
700806 Impact of Noise on Subsonic Transport Design
700233 Importance of Styling and the Use of Materials in Aircraft Interiors
700289 Influence of Airline Experience on Cf6 Engine Design
700916 Lightning and Static Hazards Relative to Airworthiness
700807 Noise Considerations in the Design of Advanced Subsonic Transport Turbofan Engines
700586 S-65-200 Commercial Compound Aircraft Design for Maintenance
700232 Styling and Interior Developments in General Aviation Aircraft
700023 Traction Drive System Design Considerations for a Lunar Roving Vehicle
690561 Airplane DesignerS View of Aircraft Ground Support
690195 Application of Computer Graphics in Aircraft Design
690673 Design and Testing of An Aircraft Nucleonic Fuel Quantity Gaging System
690706 Design of Fighter Aircraft for Combat Survivability
690696 Development of a Digital Variable Stability System for Evaluating Design Parameters of Vtol Fixed-Wing Aircraft
690389 Developmental Testing of Boeing 747 Nacelle for P&W Jt9d Engine
690424 Lubricant Evaluation and Systems Design for Aircraft Gas Turbine Engines
690341 Potential Structural Materials and Design Concepts for Light Airplanes
690634 Problems of Ground Support Equipment Standardization
690432 Radiation Pyrometer Designed for In-Flight Measurement of Compressor Blades of Turbine Engine Temperatures
690707 Survivability Design of Forward Air Control and Light Attack Aircraft
690741 Systems Concepts in Control Design for Industrial and Commercial Aviation Applications of Auxiliary Power Units
690316 Use of Explosive Forming in the Fabrication of Aircraft Components
690635 Wheeled Mobility Design for Aerospace Ground Equipment Trailers
680713 Some Implications of Noise Restrictions to Subsonic Transport Engine-Installation Design, Development, and Operation
680204 Design requirements of C-5A military cargo aircraft
680202 Devices for stick free stability in light aircraft
680201 Recent Transonic Airfoil Developments of Some Business-Aircraft Implications
680199 Aerodynamic Development of Cessna 177 Four-Place Single-Engine Cantilever-Wing Airplane
680447 Design Requirements of Small High-Temperature-Rise Combustors for Turbine Engines Designed for Vtol Aircraft
680314 Design and Fabrication of a Pressurized Boron Composite Wing Box
680646 Design and Testing of Inverted Flaps and Wing Span Flaps
680337 Design of Pratt and Whitney Aircraft Jt9d Turbofan Engine for Maintainability
680099 Design of Vehicles for the Lunar Environment
680057 Designing An Aircraft Engine Fuel Pump to Meet Specified Vapor-To-Liquid Ratios
680313 Designing and Fabricating Aircraft Structures With Filamentary Composites
680545 Designing the Lockheed L-1011 Jet Transport to Meet Airline Needs Beyond 1970
680688 Development of Requirement, Configuration, and Design for Lockheed 1011 Jet Transport
680689 European Airbus (A-300) Is Beneficiary of Concorde Experience
680333 Four Turbofan Engines Power C-5a Military Logistics Aircraft of 712,000 Lb Design Gross Weight and 5500-Nautical-Mile Range
680728 Ideas, Integrated Design and Analysis System Aids Sizing and Analysis of Aircraft Primary Structure
680727 Impact of Maintainability Analysis on Aircraft Design
680354 Integral Weight and Balance System Applications on Cargo Aircraft
680696 Lockheed C-5 Troop and Cargo Handling Requirements
680697 Lockheed C-5 Troop/Cargo Handling Subsystems
680691 Potential Technology Improvements for the Dual-Rotor High Bypass Ratio Cf6 Turbofan Engine Designed for Use in Trijet Aircraft
680227 Propeller Design Considerations for Turbine-Powered Aircraft
680353 Proposed Sst Weight and Balance System
680673 Vulnerability and Crashworthiness in the Design of Rotary Wing Vehicle Structures
670244 Aerodynamic Considerations for 300-Mph Business Airplane - Handley Page Jetstream Twin Turboprop Airplane
670880 Aerodynamic Design Considerations of Variable Geometry Aircraft
670847 Aerodynamic Design Features of the C-5a Subsonic Jet Military Transport
670846 Aerodynamic Design of the Wing and High-Lift System of the Dc-9 Short-To-Medium-Range Jet Transports
670370 Aircraft Fuselage Configuration Studies Point to Use of Multideck Fuselages
670138 Control System Requirements for Advanced Direct-Lift Engine Designed for Mach 2 Fighter Aircraft
670344 Design Criteria and Configuration for Long-Life Aircraft Turbine Engines
670579 Design Objectives for Aircraft Escape Systems of Tomorrow
670242 Design of Gulfstream Ii - a Low Wing Business Aircraft - of Moderate Sweep, Powered By Two Aft-Mounted Turbofan Engines
670582 Design of Integrated Flight Control/Hydraulic System for Boeing 2707 Supersonic Transport Aircraft
670234 Designing Business Jet Aircraft Engines for Increased Service Life
670631 Impact of Maintainability Engineering Techniques on the Design of the F-111 Aircraft
670140 Some Aircraft Gas Turbine Environmental Challenges for the Fuel Control Designer
670531 Special Problems Encountered in the Design of the Hydraulic System for the Concorde Supersonic Transport
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
660277 Airplane Design Factors That Affect Direct Operating Costs
660323 Application of 5-7 Bypass Ratio Engines to Subsonic Transport Will Reduce Fuel Consumption and Increase Thrust-Weight Ratio
660216 Design and Development of the Structural Integrity of a Jet Executive Aircraft, D.H. 125
660647 Design and Fabrication of Large Experimental Titanium Crossbeam for Aerospace Applications
660670 Effects of Low Level Turbulence on the Structure of a Large Logistic Aircraft
660217 FAA Research, Development, and Airworthiness Compliance for General Aviation Aircraft
660146 Lunar Mobile Laboratory -- Design Characteristics
660679 Structural Considerations in the Design of a Liquid Hydrogen Tank for Hypersonic Vehicles
660642 Use of Reinforced Plastic Composites in Commercial Aircraft Can Bring Savings in Weight
650054 Computerized Static and Dynamic Aircraft Structural Analysis System--Use of Computer Programs in Aircraft Design
650785 Cost/Weight Merit Function for Aerospace Hardware Design
650235 Design Concept of a Jet Close Support Aircraft for Counterinsurgency Operations
650349 Design Margin Is Key to Lunarcraft Shock Absorber Reliability
650381 Design and Development of Cj610 Turbojet and the Cf700 Turbofan Engines for Use in Business Jet Aircraft
650227 Design of Air Force Aircraft for Safety
670259 Design of Pressurized Cabins for Business Aircraft
650937 Development of the Model 727 Airplane High Lift System
650799 Effect on Airplane and Flexible Pavement Design of Varying Design Tire Pressure From 60 to 360 Psi
650364 Five-Point Program Designed to Eliminate Contamination and Corrosion of Fuel Tanks on Aircraft Using Jet Turbine Fuel
650205 Flight Simulator Utilization for System Design and Pilot Training
670260 Flutter Characteristics of the Slab Tail in Business Aircraft
650387 Flutter Problems of Business Airplanes
650598 Functional Design of the Minuteman Flight Control System
650241 Inertial Navigation System and Equipment Designs for Commercial Aviation
670306 Influence of Piloted Flight Simulator Studies on the Design of Sst Instruments
650386 Justification of Computer Use By a Small Aircraft Company
650251 Operational and Design Considerations of Swept Wing Transports in Turbulence
650657 Past and Future of X-15--A High Performance, Manned Research Vehicle
650800 Procedures for Use in the Performance Prediction of Proposed Aircraft Designs
650204 Proper Interior Arrangement Helps Attain Maximum Payload-Range-Economy Capability in Supersonic Transport
650228 Safety and Reliability of General Aviation Aircraft Through Design
650834 Systematic Approach to Shelter Design for Lunar Exploration
650341 Technical Considerations in Designing a Hydraulic System for Supersonic Transport
640539 Cargo density as it affects aircraft design
640322 DC-9 operational design features
640248 Data for fail-safe design of the supersonic transport pressure cabin
640058 Design considerations for a supersonic transport
640494 Design for economy
640295 Design for in-flight maintenance for manned space missions
640009 General considerations in the design of combustion chambers for aircraft and industrial gas turbines
640331 Operational experience with the Trident aircraft
640300 Some flight deck design considerations for supersonic transports
640509 Some technical aspects of Concord
640075 The hummingbird program
630401 Airplane design for reliability
630592 Commercial supersonic propulsion~Maintainability by design
630074 Considerations of lift engine installations in VTOL aircraft from the viewpoint of the airframe designer
630224 Design considerations for the supersonic transport electric power system
630079 Instrumentation and payload design for lunar roving vehicles
630263 Recent French experience in the field of V/STOL aircraft
630262 Some development aspects of the Hawker P1127 jet V/STOL light tactical fighter
630188 The Cessna skymaster
630441 The design and development of a prototype landing gear system for aircraft to be operated from rough unprepared fields
620458 Advanced design features in Canada's supersonic wind tunnel
620468 Design and operation of V/STOL commercial aircraft
620482 Design and test experience with high-speed mechanical drive systems for helicopter and VTOL aircraft
620343 Flight control system design for supersonic transport
620056 Further developments of the JetStar program
620301 Importance of air induction system design to supersonic aircraft
620379 Programmed reliability in design for a V/STOL airplane
620456 Setting the structural design criteria for space debris effects in cislunar and outer space travel
620467 Specialized design for the short haul jet transport role
620465 The de Havilland Trident
620346 The role of a prototype in the development of an ASW airplane
610341 Passenger density and accommodations as factors in supersonic transport design
610251 Special aspects of structural design for safety of light aircraft
610100 The Breguet family of STOL aircraft
610225 The Lockheed JetStar
610088 The exploitation of the maximum capabilities of the human body to withstand maneuvering loads in manned aerospace vehicle design
610250 Trends in light aircraft structural design
600286 A new design approach for supersonic transports
600382 Community psychoacoustics~Key to aircraft noise design and operation
600260 Discussion of some design problems associated with artificial feel systems of airplanes with irreversible powered flight controls
600378 Flight characteristics of the DC-8
600085 Matching a constant speed drive to a specific application
600045 Preliminary design considerations for the structure of a trisonic transport
590270 Airline ground equipment~Functional requirements and design
590406 Design of aircraft for commercial use
590069 Design problems of very high speed flight
590077 Fairchild F-27 turbine transport progress report
590404 Progress Report~Convair 880 and Convair 600 turbojet transport
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
580370 Design of commercial jet aircraft for specific routes
580041 Designing with steel for lighter aircraft
580280 Mechanical Factors Involved in Bearing Design for Aircraft Electric Motors
580176 Primary creep in aircraft design
580016 Problems in the application of high-strength steel alloys in the design of supersonic aircraft
580072 The X-14 VTOL airplane~A design tool
570219 Concept, design, and manufacture of supersonic aircraft
570163 High speed aircraft design for good spin characteristics
570208 Human factors in the design of high performance aircraft
570214 Trends in modern aircraft structural design
560273 The Allison Power Package for the Lockheed Electra
550178 Air transport design for the human element of airline service and maintenance personnel
550303 Planning for the best airplanes
550076 Safety considerations in aircraft design
550223 Structural design and static testing of utility aircraft
550058 The Vickers' Viscount on Trans-Canada Air Lines' routes
550019 The convertible aircraft art
550190 The design and development of high-pressure high-temperature pneumatic ducting systems for aircraft
550048 The next twenty-five years in the aviation industry
550137 The role of testing in modern military aircraft design
540148 Clear design thinking using the aircraft growth factor
540137 Design considerations of the Boeing model 707
540195 Design features of the Douglas A3D Skywarrior
540166 Design of light-weight, high-performance military aircraft
540204 Development of the Piper twin engine Apache
540141 Factors affecting the design of thin wings
540144 Fragility rating for aircraft equipment~Potential aid to package cushion design
540196 Propeller design for high performance utility aircraft
540253 Turbojet-engine design problems for supersonic flight
530020 A designer's view of combat aircraft reliability
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
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
530149 The effect of temperature on aircraft structural design
520022 Commercial turbine powered transport outlook
520232 Flight experience with Vickers Viscount turbopropeller airliner
520078 Government collaboration in aircraft development
520074 Improved passenger comfort through the application of airline experience to air conditioning system design
520200 New design requirement learned from Korean war aircraft
510131 General design aspects of turbo-prop and turbo-jet aircraft fuel systems
510186 The Avro C-102 jetliner
510162 Treatise on experience~Review of some detail design experiences
510171 Wright brothers as aeronautical engineers
500140 A concrete phase in the development of the load detachability principle in aircraft
500002 Lockheed Constitution development story
500013 Needed~A new agricultural airplane
500152 Recommendations for fuel system design for personal aircraft with regard to vapor lock
500161 The development of assault transport and troop carrier aircraft
490160 A new appraisal of the 1955 air transport
490204 Aerodynamics of high-speed airplanes
490182 Design charts for longitudinally stiffened wing compression panels
490212 Design of aircraft structures for "mass production"
490023 Personal aircraft~Problems and progress
490020 The design of airplane interiors
480169 An approach to the analytical design of aircraft
480165 Long-range overseas transport plane of 1955~What are the departures from conventional arrangements to get the required performance
480167 Long-range overseas transport plane of 1955~What does the 1955 transport look like
480047 Simplicity as a goal in the design of aircraft systems
480048 The design and development of rocket engine powerplants for aircraft
470016 Design trends in turbo-jet and turbo-prop aircraft engines
470253 Effect of C.A.R. performance requirements on airplane design
470240 Future trends in aircraft-engine design
470098 Reduce airplane noise through basic design
470093 The designer and manufacturing costs
470135 The problems of noise reduction from an airplane design standpoint
470075 The relationship of aircraft detail design to tooling and manufacturing costs
460108 A summary of design and test experience with monocoque magnesium wings
460222 Aircraft approach to automobile body design
460207 Application of turbosuperchargers to postwar commercial aircraft
460255 Design and test experience with monocoque magnesium wings
460151 Design of a transport airplane electrical system
460190 Design requirements for pickup aircraft
460175 Design trends in aircraft exhaust systems
460012 Development of the Beech Bonanza light four-place high performance airplane
460107 Factors affecting the design of the air conditioning and pressurizing system for the Republic rainbow airplane
460181 Mechanical design considerations influencing blading performance in aircraft gas turbine power plants
460165 Passenger aircraft facilities~Design and operation
460031 Selection of aircraft accessory equipment
460156 Some requirements of a "feeder" airplane
450215 Basic factors of helicopter design
450112 Engineering problems in the development of a small transport airplane design
450003 Flight engineer station design and requirements
450135 Fueling a half forgotten bit of aircraft design
450098 Helicopter design problems
450008 Psychological requirements for aircraft passenger design
450092 The design and development of large post-war transport aircraft
450054 The helicopter~A very significant aeronautical development
440135 A study on the efficiencies of cargo airplane designs
440179 Design considerations of the cargo airplane
440001 Design of aircraft and its related accessories from a maintenance viewpoint
440119 Effect of airplane design on air transport maintenance
440171 Fundamental requirements of post-war transport airplanes
440213 Fundamentals of airplane design
440007 Low-cost cylinder design for commercial airplane engines
440016 Production design changes of the C-47 airplane
440211 Propeller and gear ratio requirements for aircraft designed for cruising operation
440205 The design for production of sheet metal aircraft parts
440097 The design of the DC-4\mfC-54 airplane
440207 The intercooling problem in airplane design
440116 The operation of Consairway by Convair has influenced post-war aircraft design
430022 A method of applying production design to aircraft
430025 Co-Designing Aircraft Power Plants
430010 Design and development of the North American aviation trainer series
430104 General aspects of aircraft power plant installation
430047 Influence of new materials on the structural design of airplanes
430064 Probable trend of post-war aircraft powerplant installation design
430085 Some tactical considerations in aircraft design
430040 Strategic materials~Aircraft production and design
430024 The effect of environment on aircraft engine design and performance
430062 The future of aviation
420013 Aeronautical engineering~Our trump card
420054 Airplane design for cargo transportation
420018 Design aspects of aircraft exhaust system
420123 Design features of the Junkers 211B aircraft engine
420059 New applications of Panelyte in the aircraft industry
420070 Part I~Organization
420062 The place and use of spot welding in design and production of aircraft
410078 Considerations on the design of aircraft propellers
410138 Design of airscoops for aircraft carburetors
410131 Mercedes-Benz DB-601A aircraft engine~Design features and performance characteristics
400126 Design problems in the quantity production of aircraft engines
400075 Standardization as applied to aircraft design
390055 A simplified method for development of prototype airplanes as applied to consolidated model 31 long range patrol boat
390132 Coordinating aircraft-engine design and production
390171 DC-4 flight tests~Their relation to large air-transport designs
390140 Manly, the engineer
390179 Transatlantic airplane design
380111 Basic problems in the design of high-output aircraft engines
370063 Bringing the private owners airplane up to date
370079 Constant speed propellers
370193 Design of cowlings for air-cooled aircraft engines
370021 Design trends in French aircraft engines and propellers
370082 Engine maintenance from the operators' viewpoint
370132 Problems in design and construction of large aircraft
370157 The aircraft trend in body design from the aircraft viewpoint
370131 The aircraft trend in body structural design
370167 The vibration problem in aircraft-propeller designing
370176 Trend of air-cooled aero engines~The next five years
360012 Carburetor icing in airline operation
360129 Design of two-engined aircraft
360075 Designing and building for the commercial aircraft market
360083 Designing for the use of aluminum alloy forgings and extrusions in aircraft production
360010 Smart airplanes for dumb pilots
350100 A designer-manufacturer viewpoint of transport-aircraft needs
350045 Aircraft structural design and its influence on other engineering design
350006 Are we giving the average private operator the airplane most suitable to his needs
350102 Design problems and methods for large flying boats
350077 Small plane power plant developments of Universal Engine and Propeller Company
340018 Design limitations of aircraft engines
330030 Airplane vibrations and flutter controllable by design
320066 Relation of design to airplane maintenance
320014 The economic aspects of transport-airplane design
300028 The effect of airplane fuel-line design on vapor lock
290063 Modern light alloys and their application to aircraft-engine design
280065 Naval air-tactics and aircraft design
270069 Problems in Transport-Airplane Design
270068 Service aviation, aeronautical engineering and commercial aviation
270071 Trends in military airplanes
260063 Progress in aircraft-engine design
250027 Recent developments in aircraft engines
250067 The evolution of the modern racing airplane
240028 Airplane-engine designing for reliability
230029 The design of commercial airplanes
220065 Recent airplane design and performance improvements
210060 Requirements of aeronautic powerplant development
200026 Design factors for airplane radiators
200048 Recent advances in aviation
190065 Airships and their commercial possibilities
190026 Commercial future of airplanes from an engineer's standpoint
190056 Progress in naval aircraft
190062 The horsepower of resistance in airplane design
180033 Airplane types
180001 Types of military airplanes
170026 Design and production of air-craft in time of war

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