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SAE International

SAE Papers

Paper Number / Title
For more information, click on the Paper Number
Book Number
2011-01-2626
Aerodynamic Design of a Micro Air Vehicle: Study of Propeller-Engine Performance
 
2011-01-2787
Passive Attitude Control for Discoid Aerial Vehicles
 
2011-01-2723
Rotary Friction Welding Thermal Prediction Model
 
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 UAV's 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 Jet Vectoring Plasma Actuators
 
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
 
2008-01-2254
Cost Benefits of Aerodynamic Data Generation Techniques for Aircraft Stability and Control Analysis using the J2 Universal Tool-Kit
 
2008-01-2271
Dynamic Taxonomies Usage in the Context of Aeronautical Maintenance Processes to Increase the Effectiveness and the Efficiency of the Operations
 
2008-01-2272
Finite Element Modeling Strategies for Dynamic Aircraft Seats
 
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
 
2008-01-2231
Hybrid Rigid/Inflatable Wings for Low Volume Wing Storage
 
2008-01-2238
Importance of Unmanned Air Vehicles
 
2008-01-2263
Jam-Free, Fail-Safe Flight Control System with Asymmetric Load Alleviation Capability
 
2008-01-2262
Keys to Success with Knowledge-based Techniques
 
2008-01-2230
Model-Driven Architecture for Platform and Store Design
 
2008-01-2270
Modern Solutions for Ground Vibration Testing of Small, Medium and Large Aircraft
 
2008-01-2243
Nimbus Meta-plane, a New Aerodynamic Concept for Unmanned Hybrid Aerial Vehicle Application
 
2008-01-2232
Operational Loads Monitoring of a Fleet of Beech 1900D Aircraft
 
2008-01-2266
Outsourcing Aircraft Maintenance Designed Around Safety, Diversification, and Performance
 
2008-01-2244
Plasma Micro-Thrusters for Micro-Aerial Vehicles
 
2008-01-2237
Robust Control Design for a Flexible Unmanned Aerial Vehicle
 
2008-01-2264
The Seven Parameters of Highly Effective Cable Control Systems
 
2007-01-3908
A New Simulation Technique Using a Holistic Approach and Methodology to Assess Productivity of the New Plant for Manufacturing the Boeing 787
 
2007-01-3925
A Software Method for Demonstrating Validation of Computer Dummy Models Used in the Evaluation of Aircraft Seating Systems
 
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
 
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
 
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
 
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 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
 
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 Modeling 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
PT-137  
2004-01-3098
Sensitivity Analysis of the C-130 Sensor Deployment System Arm Using Finite Element Methods
 
2004-01-3093
Strategy For Modeling 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
 
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
 
2002-01-2949
A Longitudinal Slip Tire Model for Brake Control Systems: Features and Uses in Simulation, Control Synthesis and Stability Analysis
 
2002-01-2958
ATN Airborne Implementation
 
2002-01-2921
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
 
2002-01-2916
Assessment of the Dynamic Stability Characteristics of the Bell Model M427 Helicopter Using Parameter Estimation Technology
 
2002-01-2948
Asymmetric Approach in Solving Aircraft Brake Vibration
 
2002-01-2968
Designing User-Interfaces for the Cockpit: Five Common Design Errors and How to Avoid Them
 
2002-01-3012
Determining Optimum Redesign Plans for Avionics Based on Electronic Part Obsolescence Forecasts
 
2002-01-2925
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 NASA's Next-Generation Aviation Paradigm: A Summary of Research Findings
 
2002-01-2953
Electric Starting of Large Aircraft Engines
 
2002-01-2945
End Item Temperature Test -- An Improved LRU-Level Screen
 
2002-01-2998
Enhanced Security Flight Deck Doors-Commercial Airplanes
 
2002-01-2941
Environmental Systems Considerations for Aircraft Cabins During Ground Operation
 
2002-01-3001
FEA Cyclic Symmetric Fatigue Analysis of Aircraft Wheels
 
2002-01-2957
Fire Resistant Composites
 
2002-01-2931
Fuel Transfer System in the Conceptual Design Phase
 
2002-01-3006
HUD Symbology for Surface Operations: Command Guidance vs. Situation Guidance Formats
 
2002-01-3008
Highlights of NASA's Systems Approach to Crashworthiness Research
 
2002-01-2956
Hybrid-Ceramic Circumferential Carbon Ring Seal
 
2002-01-2927
Identification and Evaluation of Technologies for the Development of a Quiet Supersonic Business Jet
 
2002-01-2930
Impact of Configuration and Requirements on the Sonic Boom of a Quiet Supersonic Jet
 
2002-01-2990
Improving the Aerodynamic Efficiency of High Lift Devices by a Stiffness Oriented Re-design with Tailored Laminates
 
2002-01-3010
Incorporation of Lean Principles through the use of Flexible Fuel Tubing in a Large Military Transport Aircraft
 
2002-01-3004
Metastable Beta Titanium Spring Performance at Elevated Temperature
 
2002-01-2942
Method for Analyzing Lubricating Oil Contamination of Aircraft Systems
 
2002-01-2918
Model of Casing Treatment Influence on Compressor Rotor Efficiency
 
2002-01-2974
One-Pass Pricing Methodology
 
2002-01-2944
Past, Present, and Future of the Gas Turbine Engine Simulator; A Technical and Financial Analysis
 
2002-01-3000
Photon Induced Positron Annihilation (PIPA)—A New, Core Technology to Improve the Nondestructive Inspection and Life Prediction for Critical Components
 
2002-01-3011
Plastic Ball-Grid-Arrays (PBGA): Are they ready for environmentally harsh Aerospace applications?
 
2002-01-2926
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 Victrex® PEEK™ Thermoplastic to Drive New Designs, Processing Flexibility, and Cost Reduction in Aerospace Components
 
2002-01-3013
Utilization Life of Electronic Systems - Aging Avionics Usable Life and Wear-Out Issues
 
2002-01-2995
Vertical Drop Test of a Narrow-Body Transport Fuselage Section with Overhead Stowage Bins
 
2002-01-2997
Vertical Drop Test of a Transport Fuselage Section
 
2002-01-2912
Wind-Tunnel Investigation of Commercial Transport Aircraft Aerodynamics at Extreme Flight Conditions
 
2002-01-1508
An 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
 
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 Techologies
 
2000-01-5610
Integration of Configuration Design and 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-B raced 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 Gear 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 Strucutures
 
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
 
1999-01-2430
Zarya Energy Balance Analysis: The Effect of Spacecraft Shadowing on Solar Array Performance
 
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 n+-GaAs/δ (p+)-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
 
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 Chrager-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
 
1999-01-2655
AMTEC Cell Optimization for Advanced Radioisotope Power System (ARPS) Design
 
1999-01-2660
AMTEC Internal Self-Heat Pipe
 
1999-01-2521
Acceptability of Premixed Hydrogen in Hydrogen Diesel Engine
 
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
 
1999-01-2715
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 π-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
 
1999-01-2514
Bipolar Nickel Metal Hydride for Terrestrial Applications
 
1999-01-2488
Bipolar Nickel-Metal Hydride Batteries for Aerospace 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 H2-O2 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
 
1999-01-2582
EOS-AM Solar Array Arc Mitigation Design
 
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
 
1999-01-2595
Evaluation and Life Testing of Lithium-Ion Batteries for Geosynchronous Satellites
 
1999-01-2456
Evaluation of 6 Different Correlations for the Flow Friction Factor of Stirling Engine Regenerators
 
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
 
1999-01-2459
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
 
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/Al2O3 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 Horizon® C2M 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 «Superconductor-Superflywheel» (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
 
1999-01-2585
Long Term Inert Processing of RTGs
 
1999-01-2515
Long-Life and High-Energy-Density Batteries as a Backup Power Supply
 
1999-01-2530
Loop Heat Pipes - Recent Developments, Test Results and Applications
 
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
 
1999-01-2543
Low Temperature Performance Evaluation of Battery Management Technologies
 
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 ΔT 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 NOx Emissions
 
1999-01-2519
Optimum Compression Ratio Variation of a 4-Stroke, Direct Injection Diesel Engine for Minimum bsfc
 
1999-01-2613
PEM Energy Storage for Solar Aircraft
 
1999-01-2727
PEM Fuel Cell System Evaluation for Navy Surface Ship Applications
 
1999-01-2502
PROPOSAL AND BASIC EXPERIMENTS OF SUPER STIRLING ENGINES
 
1999-01-2552
Paraboloidal Thin Film Inflatable Concentrators and their Use for Power Applications
 
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 NASA’s 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
 
1999-01-2683
Proposals for New Types of Solar Heat-Engine Systems
 
1999-01-2433
Protection of Space Hardware During Ground Testing
 
1999-01-2566
Prototype Nighttime Solar Cell™ 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 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 (HEHBT’s)
 
1999-01-2435
TESTING of the ENGINEERING MODEL ELECTRICAL POWER CONTROL UNIT for the FLUIDS and COMBUSTION FACILITY
 
1999-01-2503
THE SECOND STIRLING TECHNO RALLY CONTEST OF MODEL AND MANNED STIRLING ENGINE CARS
 
1999-01-2474
TWA800 Fuel Tank Thermal Management Issues
 
1999-01-2454
Technology Development for a Stirling Radioisotope Power System for Deep Space Missions
 
1999-01-2555
The Circulation Hydraulic Contour on Meissner’s Effect
 
1999-01-2586
The Design of a Nuclear Power Supply with a 50 Year Life Expectancy: The JPL Voyager’s 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
 
1999-01-2624
The Substantiation of a Wind Wheel’s 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
 
1999-01-2726
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
 
985512
Progress on Starcar 4
 
985584
Structural Integrity Assessment Through Eigensolution
 
975560
A New Look at Optimum Propeller Performance - Going from the Prandtl F Factor to a Vortex-Induced Downwash Analysis
 
975577
Evolution and Future Development of Airplane Gust Loads Design Requirements
 
975537
A Methodology for Preliminary Design of Mechanical Aircraft Systems
 
975575
A Part-Time Master's 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
 
975542
CRISTO: A Code for Integrated Synthesis and Trajectory Optimization of Commuter and Regional Aircraft
 
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
 
975585
Demonstration of a Probabilistic Technique for the Determination of Aircraft Economic Viability
 
975566
Design Studies for a 200 Seat Transport Aircraft Using Multivariate Optimisation
 
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
 
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 of a 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-Wire™ 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
 
975509
“Web-ACSYNT”: Conceptual-Level Aircraft Systems Analysis on the Internet
 
972486
DESIGN DEVELOPMENT OF AN INFLATABLE MODULE FOR A LUNAR/MARTIAN BASE
 
972469
Thermal Design of the Lunar Exploring Spacecraft
 
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
 
972201
Applications and Development of EB Welding on the F-22
 
971474
Aircraft Design Tools for PC's
 
971458
Alternative Designs of Energy-Absorbing Seat Legs for Certification of Commuter Aircraft Seats
 
971473
General Aviation Airplane Design Tools for PC's
 
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
World's First VTOL Airplane Convair/Navy XFY-1 Pogo
 
965519
A Generic Model Concept for Optimisation in Preliminary Design
 
965568
ACSYNT: Commercialization Success
 
965609
Aircraft Design Optimization on a Personal Computer
 
965612
An Assessment 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
 
965567
An Update on RDS - Professional
 
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 Designer's 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
Preliminary Sizing of a Supersonic Commercial Transport Between Mach 2.0 and 2.4
 
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
 
965631
“Electric Aircraft” Pioneer The Focke-Wulf Fw 190
 
961464
Conceptual Design of a Crater Lunar Base
 
961535
Conceptual Design of a Solar Powered Heat Pump for Lunar Base Thermal Control System
 
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 and 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 μ-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 Calculation: 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 In-Flight 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 Transports: An Engine Manufacturer's 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 Reach, 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
What's 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 CBA123 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
 
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 withComputational 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
 
929484
Modular DIPS, 2.5-kWe Modules for Lunar/Mars Surface Applications, Design Point Selection Summary
 
929447
SP-100 Early Flight Mission Designs
 
921570
Design Concepts and Market Opportunities for “Flying Automobiles”
 
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 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
Non Linear 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 Helicopter's 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 Pilot's 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 ADVANCED MULTI-MISSION 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 Avanti Aircraft: A General Overview
 
911105
GN&C for Pegasus® 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
 
901897
APU Pod Concept for F-14 Aircraft
 
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
 
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 Hydraulic System Simulation-An Integrated Approach
 
901822
Electroluminescent Displays (EL) for General Aviation Cockpits
 
901788
Electronic Chassis/PWB Structures: Vibration Response Level Nonlinearities in Reliability Growth Testing
 
901875
Filter Line Wiring Designs in Aircraft
 
901890
Future Supersonic Transport Studies at Aerospatiale
 
901831
HUD Potential for Narrow-Bodied Air Carrier Aircraft
 
901925
High-Speed Civil Transport Research and Technology Needs
 
901829
Improving Situational Awareness Through the Use of Intuitive Pictorial Displays
 
901814
Minicomputer Part-Task Simulation for Helicopter Development-An Economical Approach
 
901923
NASA's 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 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
 
901031
ASSESSMENT OF A POST 2000 STOVL FIGHTER
 
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
 
892239
A320 and B757 on the Liner: A Line Pilot's 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 Pilot's 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
What's 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 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
Considerations of Control Authority Requirements in 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 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
 
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 ¾-Open-Jet Automotive Wind Tunnels
 
872382
A Supersonic Design with V/STOL Capability
 
872358
Aeroacoustics of Advanced STOVL Aircraft Plumes
 
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
 
872365
Overview of the US/UK ASTOVL Program
 
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
 
872463
Aerospace Co-Operative Engineering
 
872451
Comparssion 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 Approach
 
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
 
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
 
871756
Design of Transonic Airfoils and Wings Using a Hybrid Design Algorithm
 
871809
Design of an Inlet Air Cleaner for the Black Hawk Helicopter Auxiliary Power Unit (APU)
 
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 × 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 Daedalus Prototype
 
871344
HOTOL: An Advanced European Space Transporter
 
871347
The Experimental Aircraft Programme
 
871346
X—31A
 
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
 
871031
The Acoustic Experimental Investigation of Counterrotating Propeller Configurations
 
871040
The Merlyn Diesel Concept for Propulsion
 
872525
Advanced Technology Cockpit Design and the Management of Human Error
 
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 What’s Old? What’s 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
 
861726
Integrated Flight/Propulsion Control for Next Generation Military Aircraft
 
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
 
861154
Meeting the Air Cargo Challenge: Boeing's Aircraft Developments
 
861161
O B C O - A Cargo Loading management Ground Equipment for More Cargo Aircraft Flexibility
 
861153
“Flexible” Cargo Handling Systems for Standard-Body Airplanes
 
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 NASA's Langley Research Center
 
851886
Antimisting Fuel Technology for Transport Category Aircraft
 
851806
Pilot Executive Project-PILEX
 
851836
Pilot Interface with Fly-By-Wire Control Systems
 
851977
SR-71 Digital Automatic Flight and Inlet Control System
 
851774
The Development and Evaluation of Color Systems for Airborne Applications--Fundamental Visual, Perceptual, and Display Systems Considerations
 
851982
A European Experience on International Collaborations
 
851753
A System Look at Actuation Concepts and Alternatives for Primary Flight Control
 
851851
AVIONICS SYSTEM ARCHITECTURE FOR BEECHCRAFT STARSHIP 1
 
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
 
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
 
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”
 
851950
Techniques for Sortie Generation Analysis
 
851767
The CASA C-101 Advanced Trainer/Light Ground Attack Aircraft for Today and the Future
 
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 Crash worthiness 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 KEVLAR® 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
 
840027
Five Years Experience with Minimum Induced Loss Propellers-Part II: Applications
 
840028
“Phoenix”- A Polyester-Film Inflatable Man-Powered Aircraft
 
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
 
831513
How Aerospace ISO Standards Will Impact New Designs SC-1 Electrical Requirements
 
831516
How Aerospace International Standards Will Impact New Design - Fluid Systems, ISO/TC20/SC10
 
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 Gunsfor 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
 
820732
Design of Unconventional Commuter Configurations
 
821346
Design of an Aerobatic Aircraft Wing Using Advanced Composite Materials
 
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
 
811036
THE ANATOMY OF A TECHNOLOGY TEST BED - INTEGRATED FLIGHT/FIRE CONTROL-I (IFFCI)
 
811098
Tactical Air-to-Surface Requirements for the 1990s
 
811100
Technology for Quality and Quantity in a New Fighter
 
811091
The Use of “Kapton” Polyimide Film in Aerospace Applications
 
811085
“The Impact Of The Microprocessor On Aircraft Electric System Control Philosophy”
 
810846
757/767 Flight Crew Interface
 
810853
Aircraft Noise Control Practices Related to Ground Transport Vehicles
 
810630
AN ASSESSMENT OF ADVANCED TECHNOLOGIES FOR APPLICATION TO GENERAL AVIATION
 
810625
Aerodynamic Design Data For a Cruise-Matched High Performance Single Engine Airplane
 
810618
Avco Lycoming's 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 Effects 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
 
801228
AV-8B Operational Features for Rapid Deployment
 
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 Industrie's 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
 
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 LH2 for Aircraft
 
801208
The CADAM® 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
 
800743
AIRCRAFT OF THE FUTURE
 
800610
Advanced Materials for Agricultural Aircraft
 
800601
Business Aircraft Turbofan Technology Progress in the 1970’s, Challenges in the 1980’s
 
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
Profan 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
 
801244
Factors Affecting the Future of Commercial Aviation
 
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 Wing-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 1980's
 
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
 
780554
THE NEED AND IMPACT OF LONG-TERM ADVANCES IN AIRCRAFT TECHNOLOGY: THE AIRLINES' POINT OF VIEW
 
780078
The Design and Development of the Upper-Pivoted Sonic Carburetor
 
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-RPV's
 
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 Complianec-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 Manufacturer's 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 Designer's 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 Manufacturer's 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
 
760905
THE F-15 MULTI-MISSION AIRCRAFT PROGRAM STATUS
 
760471
THE MARK II LEARJET FROM CONCEPT TO CERTIFICATION
 
760920
The Development and Flight Testing of the XC-8A Air Cushion Landing System (ACLS)
 
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
 
760590
The Pazmany PL-2 and PL-4 Airplanes
 
760539
YC-14 STATUS REPORT
 
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
 
750631
AST Propulsion Comparisons
 
750617
Advanced Supersonic Transport
 
751091
Aircraft Pay-Offs and Requirements for a Jet Flap Propulsion System
 
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
 
750587
Design Of Short Haul Aircraft For Fuel Conservation
 
750619
Design of Jet Engine Rotors for Long Life
 
750524
Design of Low-Speed Airfoils by Numerical Optimization
 
750628
Engine Design Considerations for 2nd Generation Supersonic Transports
 
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
 
751113
RPV Autoland
 
751109
Remotely Piloted Vehicle Technology Development Using the XQM-103 Research Test Vehicle
 
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-I 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
 
750546
“Melmoth”-An Experimental Private 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
 
740860
AFTI TI-1 Program
 
740870
Advanced Composite Design Concepts for the AMST
 
740453
Advanced Controls For Commercial Transport Aircraft
 
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 Engineer's 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
 
740467
INVESTIGATION OF NOISE FROM FULL-SCALE HIGH BYPASS ENGINE AND BLOWN FLAP SYSTEM
 
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
 
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
 
740485
THE EXPERIMENTAL CLEAN COMBUSTOR PROGRAM - DESCRIPTION AND STATUS
 
740393
The Aerocar “Flying Automobile”
 
740361
The Background to Propeller Airplane Noise Regulations
 
740376
The Design of Crashworthy General Aviation Aircraft
 
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 Designer's 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 Design
 
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
 
730913
STOL Tactical Aircraft Investigation
 
730304
Separate Surfaces for Automatic Flight Controls
 
730308
Stepped Aluminum Extrusions - Designing for Business Aircraft
 
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
 
720322
An Energy-Absorbing Seat Design for Light Aircraft
 
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
 
720323
Methods of Crashworthiness Testing for Aircraft Design
 
720319
The NASA Advanced Transport Technology Program
 
710393
A Flight Control System Providing A Simple-to-Fly, Constant Attitude Aircraft
 
710401
Analytical Simulation of Landing Gear Dynamics for Aircraft Design and Analysis
 
710465
Comparison of STOL Design Criteria for Commercial and Military 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 Engine Condition Monitoring
 
710747
Designing for Producibility: Design-Influenced Production Cost Program
 
710755
Development Status of the L-1011 TriStar
 
710426
Development of The Lockheed L-1011's Flying Stabilizer
 
710431
FAA Appraisal of Aircraft Design for Maintainability
 
710749
Future Trends in Aircraft Design
 
710462
High Temperature Turbine Design Considerations
 
710777
Influence of Powerplant Design on Airplane Operational Effectiveness-The Operator's Point of View
 
710762
Installation and Integration of Transonic Transport Propulsion Systems
 
710406
Occupant Impact Injury Tolerances for Aircraft Crashworthiness Design
 
710750
The Crystal Ball Focuses on the Next Generation of Transport Aircraft
 
710423
The Economics of Subsonic Transport Airplane Design, Evaluation and Operation
 
710388
The Influence of Bobweights and Downsprings on Flying Qualities
 
710411
The 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
 
700539
Design Considerations in Selecting Alloys for Aircraft Structures
 
700231
Design of General Aviation Airports and Heliports
 
700837
Designing The OV-10A Forward Air Control and Light Attack Aircraft
 
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
 
700289
Influence of Airline Experience on CF6 Engine Design
 
700916
Lightning and Static Hazards Relative to Airworthiness
 
700805
Minimum Noise Pod Design
 
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
 
700242
The Development of American Aviation Corporation's Yankee
 
700233
The Importance of Styling and the Use of Materials in Aircraft Interiors
 
700023
Traction Drive System Design Considerations for A Lunar Roving Vehicle
 
690389
747 Propulsion Pod FIRST YEAR OF OPERATION
 
690432
A Radiation Pyrometer Designed for In-Flight Measurement of Turbine Blade Temperatures
 
690561
An Airplane Designer's View of Aircraft Ground Support
 
690195
Application of Computer Graphics in Aircraft Design
 
690673
Design and Testing of an Aircraft Nucleonic Fuel Quantity System
 
690706
Design of Fighter Aircraft for Combat Survivability
 
690696
Development of a Digital Variable Stability System
 
690316
Explosive Fabrication of Aircraft Components
 
690424
Lubricant Evaluation and Systems Design for Aircraft Gas Turbine Engines
 
690341
Potential Structural Materials and Design Concepts for Light Airplanes
 
690634
Problems of GSE Standardization
 
690707
Survivability Design of Forward Air Control and Light Attack Aircraft
 
690741
Systems Concepts in Control Design for APU Industrial and Commercial Aviation Application
 
690635
Trailer Design for Mobility
 
680713
Some Implications of Noise Restrictions to Subsonic Transport Engine-Installation Design, Development, and Operation
 
680202
Devices for Stick Free Stability
 
680201
Recent Transonic Airfoil Developments and Some Business Aircraft Implications
 
680204
Unique Design Considerations for a Large “T” Tail Aircraft
 
680689
A-300 — A Beneficiary of Concorde Experience
 
680199
Aerodynamic Development of the Cessna 177
 
680697
C-5 Troop/Cargo Handling Subsystems
 
680333
C-5A Propulsion System Installation
 
680337
Design Features for Maintainability in the Pratt and Whitney Aircraft J9D Gas Turbine Engine
 
680447
Design Requirements of Small High-Temperature-Rise Combustors
 
680314
Design and Fabrication of a Pressurized Boron Composite Wing Box
 
680646
Design and Tests of Inverting Flaps and Wing Span Flaps
 
680099
Design for the Lunar Environment
 
680313
Designing and Fabricating Aircraft Structures with Filamentary Composites
 
680057
Designing for V/L Performance in an Aircraft Engine Fuel Pump
 
680545
Designing the Lockheed L-1011 to Meet Airline Needs Beyond 1970
 
680688
Development of Requirement, Configuration and Design for the Lockheed 1011 Jet Transport
 
680728
Ideas, Integrated Design and Analysis System
 
680354
Integral Weight and Balance System Applications on Cargo Aircraft
 
680691
POTENTIAL TECHNOLOGY IMPROVEMENTS FOR THE CF6 TURBOFAN
 
680227
Propeller Design Consideration for Turbine Powered Aircraft
 
680353
Proposed SST Weight and Balance System
 
680696
The C-5 Troop and Cargo Handling Requirements
 
680727
The Impact of Maintainability Analysis on Aircraft Design
 
680673
Vulnerability and Crashworthiness in the Design of Rotary Wing Vehicle Structures
 
670244
Aerodynamic Considerations of a Medium Mach Business Aeroplane
 
670880
Aerodynamic Design Considerations of Variable Geometry Aircraft
 
670847
Aerodynamic Design Features of the C-5A
 
670846
Aerodynamic Design of the DC-9 Wing and High-Lift System
 
670138
An Approach to Simpler Control Requirements
 
670344
Design Criteria and Configuration for Long-Life Aircraft Gas Turbines
 
670579
Design Objectives for Tomorrow's Escape Systems
 
670234
Designing Business Jet Aircraft Engines for Increased Service Life
 
670260
Flutter Characteristics of the Slab Tail
 
670370
Fuselage Configuration Studies
 
670242
Gulfstream II Aerodynamic Design
 
670140
Some Aircraft Gas Turbine Environmental Challenges for the Control Designer
 
670259
The Design of a Small Pressurized Aircraft Structure
 
670531
The Hydraulic System of the Concorde
 
670631
The Impact of Maintainability Engineering Techniques on the Design of the F-111
 
670306
The Influence of Piloted Flight Simulator Studies on the Design of the SST Instruments
 
670582
The United States SST Controls Development Program
 
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
 
660216
Design and Development of the Structural Integrity of a Jet Executive, D.H. 125
 
660647
Experimental Titanium Crossbeam
 
660217
FAA Research, Development, and Airworthiness Compliance for General Aviation Aircraft
 
660146
Lunar Mobile Laboratory - Design Characteristics
 
660642
New and Proposed Composites
 
660679
Structural Considerations in the Design of a Liquid Hydrogen Tank for Hypersonic Vehicles
 
660323
THE NEW ENGINE TECHNOLOGY AND THE SUBSONIC TRANSPORT
 
660277
The Design Importance of Airplane Mile Costs Versus Seat Mile Costs
 
660670
The Effects of Low Level Turbulence on the Structure of a Large Logistic Aircraft
 
650364
A Five-Point Program Designed to Eliminate Contamination and Corrosion of Fuel Tanks on Aircraft Using Jet Turbine Fuel
 
650834
A Systematic Approach to Shelter Design for Lunar Exploration
 
650235
Design Concept of a Jet Close Support Aircraft (Super COIN)
 
650349
Design Margin: Key to Lunarcraft Shock Absorber Reliability
 
650227
Design of Aircraft for Safety
 
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
 
650205
Flight Simulator Utilization for System Design and Pilot Training
 
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
 
650386
Justification of Computer Use by a Small Aircraft Company
 
650251
Operational and Design Considerations of the Sweptwing Jet Transport in Turbulence
 
650204
Realization of the SST Payload
 
650228
Safety and Reliability Through Design
 
650800
Some Procedures for Use in Performance Prediction of Proposed Aircraft Designs
 
650341
Technical Considerations in Designing a Hydraulic System for the SST
 
650785
The Cost/Weight Merit Function for Aerospace Hardware Design
 
650381
The Design and Development of the CJ610 Turbojet and the CF700 Turbofan Engines for Use in Business Jet Aircraft
 
650054
Use of Computer Programs in Aircraft Design
 
650657
X-15: Past and Future
 
640539
Cargo Density as It Affects Aircraft Design
 
640322
DC-9 OPERATIONAL DESIGN FEATURES
 
640494
DESIGN FOR ECONOMY
 
640248
Data for Fail-Safe Design of the Supersonic Transport Pressure Cabin
 
640058
Design Considerations for a Supersonic Transport
 
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 Helicoptor 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
Programed 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
 
620346
The Role of a Prototype in the Development of an ASW Airplane
 
620465
The de Havilland Trident
 
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
 
610088
The Exploitation of the Maximum Capabilities of the Human Body to Withstand Maneuvering Loads in Manned Aerospace Vehicle Design
 
610225
The Lockheed JetStar
 
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
 
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
 
590069
design problems of VERY HIGH SPEED FLIGHT
 
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-PART I & PART II
 
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
 
550058
THE VECKERS' VISCOUNT ON TRANS-CANADA AIR LINES' ROUTES
 
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 & 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 (Report of Aviation Fuels Division of Coordinating Fuel and Equipment Research Committee, CRC)
 
500161
THE DEVELOPMENT OF ASSAULT TRANSPORT AND TROOP CARRIER AIRCRAFT
 
490160
A New Appraisal Of The 1955 Air Transport - A Panel Discussion
 
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
COMPLETE DESIGN PANEL WHAT ARE THE DEPARTURES FROM CONVENTIONAL ARRANGEMENTS TO GET THE REQUIRED PERFORMANCE
 
480167
COMPLETE DESIGN PANEL 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
 
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
 
470098
“Reduce Airplane Noise Through Basic Design”
 
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
 
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
 
460012
“DEVELOPMENT OF THE BEECH BONANZA LIGHT FOUR-PLACE HIGH PERFORMANCE 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
 
450054
The Helicopter: A Very Significant Aeronautical Development
 
450092
“The Design and Development of Large Post-War Transport Aircraft”
 
440135
A STUDY ON THE EFFICIENCIES OF CARGO AIRPLANE DESIGNS.
 
440179
DESIGN CONSIDERATIONS of the CARGO AIRPLANE
 
440119
EFFECT OF AIRPLANE DESIGN ON AIR TRANSPORT MAINTENANCE
 
440213
FUNDAMENTALS of AIRPLANE DESIGN
 
440171
Fundamental Requirements of POST-WAR TRANSPORT AIRPLANES
 
440016
PRODUCTION DESIGN CHANGES OF THE C-47 AIRPLANE
 
440211
PROPELLER and GEAR RATIO REQUIREMENTS for Aircraft Designed for Cruising Operation
 
440001
SPEECH TO THE METROPOLITAN SECTION OF THE SOCIETY OF AUTOMOTIVE ENGINEERS ON 6 JANUARY 1944, SUBJECT, “DESIGN OF AIRCRAFT AND ITS RELATED ACCESSORIES FROM A MAINTENANCE VIEWPOINT”
 
440116
THE OPERATION OF CONSAIRWAY BY CONVAIR HAS INFLUENCED POST-WAR AIRCRAFT DESIGN
 
440205
The DESIGN of SHEET for PRODUCTION METAL AIRCRAFT PARTS
 
440207
The INTERCOOLING PROBLEM in AIRPLANE DESIGN
 
440097
The design of the DC-4/C-54 airplane
 
440007
“LOW-COST CYLINDER DESIGN FOR COMMERCIAL AIRPLANE ENGINES”
 
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 0F AIRPLANES
 
430064
PROBABLE TREND OF POST-WAR AIRCRAFT POWERPLANT INSTALLATION DESIGN
 
430085
Some tactical considerations in aircraft design
 
430024
THE EFFECT OF ENVIRONMENT ON AIRCRAFT ENGINE DESIGN AND PERFORMANCE
 
430062
THE FUTURE OF AVIATION
 
430040
“STRATEGIC MATERIALS - AIRCRAFT PRODUCTION AND DESIGN”
 
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
 
370021
DESIGN TRENDS IN FRENCH AIRCRAFT ENGINES AND PROPELLERS
 
370193
Design of Cowlings for Air-Cooled Aircraft Engines
 
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
 
370079
“CONSTANT SPEED PROPELLERS”
 
360075
DESIGNING AND BUILDING FOR THE COMMERCIAL AIRCRAFT MARKET
 
360083
DESIGNING FOR THE USE OF ALUMINUM ALLOY FORGINGS AND EXTRUSIONS IN AIRCRAFT PRODUCTION
 
360129
Design of Two-Engined Aircraft
 
360010
SMART AIRPLANES FOR DUMB PILOTS
 
360012
“CARBURETOR ICING IN AIRLINE OPERATION”
 
350100
A Designer-Manufacturer Viewpoint of Transport-Aircraft Needs
 
350045
AIRCRAFT STRUCTURAL DESIGN AND ITS INFLUENCE ON OTHER ENGINEERING DESIGN.
 
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 & 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 AIRCRAFT IN TIME OF WAR
 

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