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SAE International

SAE Papers

Paper Number / Title
For more information, click on the Paper Number
Book Number
2009-01-3165
Capitalizing on the Increased Flexibility that Comes from High Power Density Electrothermal Deicing
 
2008-01-2256
A Brief Study of Conditionally Enabled Phase Compensated Rate Limiters
 
2008-01-2234
Active Vortex Generators Using Jet Vectoring Plasma Actuators
V117-1  
2008-01-2275
Aerodynamic Comparison of Tilt-Rotor, -Wing and -Body Concept for Multi Task MAVs
 
2008-01-2267
Are the New Ones Really Better? An Inquiry About Sporty Looking Airplanes of All Ages
 
2008-01-2235
CFD Analysis of the Tigerfish Retractable Float System on a DHC- Twin Otter
V117-1  
2008-01-2233
Correlation of Hand Book Method Results with Wind Tunnel Data for a Subsonic UAV Design
V117-1  
2008-01-2268
Distributed Aviation Concepts and Technologies
V117-1  
2008-01-2239
Ensuring VLJ Operational Safety: Learning to Ask the Right Questions
 
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
 
2008-01-2243
Nimbus Meta-plane, a New Aerodynamic Concept for Unmanned Hybrid Aerial Vehicle Application
 
2008-01-2244
Plasma Micro-Thrusters for Micro-Aerial Vehicles
 
2008-01-2237
Robust Control Design for a Flexible Unmanned Aerial Vehicle
 
2008-01-2269
The Pulsed Turbine Rotor Engine VTOL Propulsion Concept and Applications: Capturing the Elusive Jet-Powered Flying Car and Redesigning a Radical Variant of the V-22 Osprey
 
2008-01-2264
The Seven Parameters of Highly Effective Cable Control Systems
V117-1  
2008-01-2255
Three-Movement Handlebar Piloting Control
 
2007-01-3788
A Brief Survey of the Experimental Methods Used for Wake Vortex Investigations
 
2007-01-3925
A Software Method for Demonstrating Validation of Computer Dummy Models Used in the Evaluation of Aircraft Seating Systems
 
2007-01-3920
Active Flow and Aeroelastic Control of Lifting Surfaces Using Synthetic Jet Actuators
 
2007-01-3857
CFD Analysis of Directional Stability for the American Challenger Rocket Car
 
2007-01-3889
Columned Multi Bubble Fuselage (CMBF) for BWB
 
2007-01-3856
Computational Fluid Dynamics Development of the JCB DIESELMAX Land Speed Record Vehicle
 
2007-01-3845
Coordinated Autonomous UAVs: Applications for a Heterogeneous Urban RSTA Team
 
2007-01-3816
Guidance Concept for a Receiver Aircraft to Perform Autonomous Aerial Refueling
 
2007-01-3912
Image Exploitation System for Airborne Surveillance
 
2007-01-3817
Implementation of Automatic Airspace Avoidance in an Advanced Flight Control System
 
2007-01-3875
Methodology for Optimizing the Aerodynamic Performance of the Time Attack Series Cobb Tuning Subaru WRX 2006 Using Mesh Deformation Techniques
 
2007-01-3804
Prediction of Susceptibility of Small Aircraft to Pilot-Induced Oscillations
 
2007-01-3858
Racecar Aerodynamic Optimization for an E-1 Class Streamliner Using Arbitrary Shape Deformation
 
2007-01-3921
Robust Analysis of Active Flutter Suppression Using Multiple Control Surfaces via Second-Order Controllers
 
2007-01-3922
Safety and Certification of UAVs
 
2007-01-3888
The 747-400 Dreamlifter - Overview & Mission
 
2007-01-3787
The Effects of Humidity on the Properties of Air and the Influence of Condensation on the Pressure Distribution over an Aerofoil
 
2005-01-3435
A Collaborative Design Environment to Support Multidisciplinary Conceptual Systems Design
 
2005-01-3434
A Concept Selection Method Developed from a Probabilistic Multi-Criteria Decision Making Technique Using Utility Theory
 
2005-01-3377
A Prototype Probe For Direct Measurement of the LWC in SLD Clouds
 
2005-01-3415
Actual Accuracy in Flight Data Collection and Analysis
 
2005-01-3358
Aerodynamics In The Future
 
2005-01-3421
Analysis of Active Flutter Suppression with Leading- and Trailing-Edge Control Surfaces via μ-Method
 
2005-01-3399
Conceptual Design of Current Technology and Advanced Concepts for an Efficient Multi-Mach Aircraft
 
2005-01-3187
Continued Computational Investigation into Circulation Control for the V-22 Osprey Download Reduction
 
2005-01-3392
Design and Flight Testing of Inflatable Wings with Wing Warping
 
2005-01-3391
Development and Testing of a Wing Morphing Mechanism for the Control of a Swept Wing Tailless Aircraft
 
2005-01-3188
Download Alleviation on a V-22 Model Having a Simple Flap Used in Conjunction With Periodic Excitation, Suction and Blowing
 
2005-01-3360
Feasibility of Modeling Wake Vortices in Ground Effect in a Water Tunnel
 
2005-01-3419
Fundamentals of FBW Augmented Manual Control
 
2005-01-3375
Mechanisms for Downstream Ice Growth
 
2005-01-3418
Phase Compensated Rate Limiters for Alleviation of Pilot-Induced Oscillations Caused by Control Surface Rate Limiting
 
2005-01-3433
Program and Design Decisions in an Uncertain and Dynamic Market: Making Engineering Choices Matter
 
2005-01-3359
Relationship of Wing Drag to Entropy Production
 
2005-01-3420
Response of an Advanced Flight Control System to Microburst Encounters
 
2005-01-3398
Supersonic Business Jet Design and Requirements Exploration using Multiobjective Interactive Genetic Algorithms
 
2005-01-3393
Technology Assessment of a Supersonic Business Jet
 
2005-01-3400
Variable Cycle Optimization for Supersonic Commercial Applications
 
2004-01-3089
A New Investigation of Natural Flight Characteristics and Theory
 
2004-01-3092
Design of a Standardized Roll-On, Roll-Off Sensor Pallet System for a C-130 Aircraft
 
2004-01-3101
Experimental Investigation of the Dynamic Interactions Between Co-Rotating Wing/Flap Tip Vortices
 
2004-01-3088
How Flies the Albatross – the Flight Mechanics of Dynamic Soaring
 
2004-01-3091
Simple Adaptive Planforms For Wings
 
2004-01-3100
Simulation Study of a Commercial Transport Airplane During Stall and Post-Stall Flight
 
2004-01-3099
Velocity Profile Measurements Under the Ramp of a Lockheed Martin C-130 Aicraft
 
2004-01-3090
Wind Tunnel Testing of Micro Air Vehicles at Low Reynolds Numbers
 
2004-01-1808
A Camera Installation in a Pressurized Part 23 Aircraft
 
2004-01-1807
An Advanced Flight Control System for General Aviation Application
 
2004-01-1806
Climb Performance Analysis Using a GPS Reference Method
 
2004-01-1816
Further Application of the Mass Loss Model to the GLC-305 and MS(1)-317 Airfoils
 
2004-01-1810
Future General Aviation Piston Engines and Fuels - An Integrated Approach
 
2004-01-1809
Interacting Processes and Fatigue Life Prediction in SCONES
 
2004-01-1805
Learjet Model 45 Steep Approach Certification
 
2004-01-1804
More Electric Small Turbofan
 
2004-01-1803
Preliminary Design Considerations for Zero Greenhouse Gas Emission Airplanes
 
2004-01-1817
Thermal Modeling of a Rotating Heat Pipe Aero-Engine Nose Cone Anti-Icing System
 
2003-01-3021
A Relationship Between Wave Drag and Induced Drag
 
2003-01-3034
Aircraft Manoeuvres Simulation Steady and Unsteady Aerodynamic
 
2003-01-3033
Control of Hypersonic Vehicles by Non-Geometric Boundary Conditions
 
2003-01-3024
Correlation of Flow Visualization and Force and Moment Measurements in a Water Tunnel
 
2003-01-3022
Drag Prediction Using the Euler/Navier-Stokes Code FANSC
 
2003-01-3015
Globalization of Commercial Aircraft Manufacturing
 
2003-01-3026
Interdisciplinary Wing Design – Structural Aspects
 
2003-01-3049
Modal Parameters from a Wind Turbine Wing by Operational Modal Analysis
 
2003-01-3023
The Development of A Multi-Disciplinary Wing Design Method
 
2003-01-3032
Trajectory Simulation of Ice Shed From a Business Jet
 
2003-01-3031
Validation of a Hot-Air Anti-icing Simulation Code
 
2003-01-3017
“A Dry Aircraft is a Safer Aircraft – Beating Condensation by Using Dry Air”
 
2002-01-2949
A Longitudinal Slip Tire Model for Brake Control Systems: Features and Uses in Simulation, Control Synthesis and Stability Analysis
 
2002-01-2914
A Phenomenological Model of Dynamic Stall
 
2002-01-2958
ATN Airborne Implementation
 
2002-01-2921
Advanced Dynamometer Designed to Fully Characterize the Propulsion System for a UAV
 
2002-01-2946
Aircraft Electric Brakes - Technical Development
 
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
 
2002-01-2915
Defining Boundary Conditions at Wind Tunnel Investigations
 
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
 
2002-01-2920
Flow Control Valve With Integrated Electronics For Aircraft Applications
 
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
 
2002-01-2919
Inlet Flow Angularity Descriptors Proposed for Use With Gas Turbine Engines
 
2002-01-2913
Macro-Aerodynamics: – A Phenomenological Model of Highly Non-linear Aerodynamics
 
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
 
2002-01-2917
Updating Nonlinear Aerodynamic Models Based on Flight Test Data-Practical Approach
 
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
 
2002-01-3191
Simulation of an Active Damping Device for DC Power Networks
 
2002-01-2650
A Study of the Influence of Drilling Method and Hole quality on Static Strength and Fatigue Life of Carbon Fiber Reinforced Plastic Aircraft Material
 
2002-01-2648
Airplane Wing Structure Fatigue Life: Impact of Misaligned Lower Rivet Dies
 
2002-01-2646
Determinant Spar Assembly Cell
 
2002-01-2631
Lightweight HH503 Handheld Riveter
 
2002-01-2649
State-of-the-Art Automated Fastening and its Integration into an Existing Production Infrastructure Discussed with an Actual Example
 
2002-01-2630
Use of Electromagnetic and Vacuum Forces on Aircraft Assembly
 
2002-01-2647
Vacuum Feeding and Chip Removal
 
2002-01-2644
A Versatile Riveting System for Metal/CFC Structures
 
2002-01-2642
AIRBUS A340 Final Assembly by S.O.J.A.: Semi-Automatic Orbital Fuselage Join Up Robot
 
2002-01-2645
Affordable Reconfigurable Tooling
 
2002-01-2634
An Algorithm for Assembly Centric Design
 
2002-01-2640
Analysis & Modeling Reduce Development Risks For Improving Integration of Large Aircraft Components
 
2002-01-2629
C-17 Cargo Ramp and Door Automated Drilling & Fastening System - Project Overview
 
2002-01-2632
Drilling Cost Model
 
2002-01-2625
Floor Drilling Gantry System
 
2002-01-2627
Implementation of a Universal Drive Blind Fastening System During Transition from Manual to Automated Assembly
 
2002-01-2633
Investigation of Manual One Way Assembly on Primary Wingbox Structure
 
2002-01-2628
Mechanical and Structural Aspects of the C-17 Cargo Ramp and Cargo Door ADFS
 
2002-01-2626
ONCE (ONe-sided Cell End effector) Robotic Drilling System
 
2002-01-2639
One Pass Drilling of Precision Holes in Aircraft Structures
 
2002-01-2637
Radial and Tangential Forces, Tool Motion, and the Formation of Lobed Holes in Drilling
 
2002-01-2636
Robotic Orbital Drilling of Structures for Aerospace Applications
 
2002-01-2313
Concept of Mechanical Interfaces for Planetary Space Suit to Airlock and Rover
 
2002-01-2574
Continuous Manufacturing Improvement Using Real Time Data
 
2002-01-2575
Integrated Simulation Solutions for Manufacturing and Design
 
2002-01-2568
Optimization of CDCF Grinding of Turbine Blade
 
2002-01-2571
Piezoelectric Tool Actuator for Precision Turning of Turbine Shafts on Conventional CNC Lathes
 
2002-01-2567
The Use of Manufacturing Process Models (MPM) in Manufacturing
 
2002-01-1544
A Method for Selecting Aircraft to Meet Coast Guard System Requirements
 
2002-01-1531
Analysis of Candidate Communication Architectures for Automated Airborne Reporting of Weather Conditions
 
2002-01-1548
Assessment of Timely Lockup of Web-Sensing Restraint Retractors
 
2002-01-1518
Contending with Airframe Icing
 
2002-01-1543
Development of a Low Cost Cascade Aerodynamics Test Facility Using a Simple Flow Visualization Velocimetry Technique
 
2002-01-1511
Fuel Consumption Measurement in I.C. Reciprocating Engines Utilizing Manifold Pressure and Engine RPM
 
2002-01-1512
Functional Digital Aircraft: Designing Flight Controls
 
2002-01-1545
Future Trends for General Aviation In-Cockpit Weather Information Systems
 
2002-01-1519
Ice Accretions on a Swept GLC-305 Airfoil
 
2002-01-1528
Iced Aircraft Flight Data for Flight Simulator Validation
 
2002-01-1510
Non-Electrically Invasive Liquid Level Measurement
 
2002-01-1527
Simulation Model Development for Icing Effects Flight Training
 
2002-01-1507
The Road to Regulation
 
2002-01-1551
Toward Simplified Methodologies for Seat Design to FAR §23.562
 
2002-01-1530
Using Global Satellite Digital Audio Radio Systems for Aviation Weather Dissemination
 
2002-01-0359
The “Magic Dragon” Aircar Development Project
 
2001-01-2989
737–800 Winglet Integration
 
2001-01-3033
A Bayesian Approach to Non-Deterministic Hypersonic Vehicle Design
 
2001-01-2991
A New Airfoil Optimized For Light Aircraft Performance
 
2001-01-3027
A Paradigm for Developing Operational Decision-Making (ODM) Training
 
2001-01-3018
A Technique for Selecting Emerging Technologies for a Fleet of Commercial Aircraft to Maximize R&D Investment
 
2001-01-2945
Active Separation Control: from Basic Research to a Simplified High-lift System
 
2001-01-2955
Aerospace Education in Germany
 
2001-01-3004
Aerospace Manufacturing Cost Prediction from a Measure of Part Definition Information
 
2001-01-3015
An Improved Procedure for Prediction of Drag Polars of a Joined Wing Concept Using Physics-Based Response Surface Methodology
 
2001-01-3035
An Integrated Human Modeling Simulation Process for the International Space Station, Intra-Vehicular Activity
 
2001-01-2988
Analytical and Numerical Modelling of the Turn Maneuver of Agricultural Aircraft
 
2001-01-2976
Assessment of the OVERFLOW Navier Stokes Code for Various Airplane Components
 
2001-01-3025
Aviation Safety Plans: Content and Training
 
2001-01-2977
Calculation of Incompressible Viscous Flows by a Viscous-Inviscid Splitting Method
 
2001-01-2953
Common Launch Acceptability Region Task Group
 
2001-01-3003
Conceptual Control Law Design for Aircraft with Reduced Tail Size
 
2001-01-2946
Control of Aerodynamic Characteristics of Airfoils and Wing Systems in Subsonic Flow
 
2001-01-3014
Development of a Multi-Mission Sizing Methodology Applied to the Common Support Aircraft
 
2001-01-2952
Development of a Standardized Electrical Interface for Miniature Munitions
 
2001-01-3034
Development of an Object Oriented Vehicle Library for Automated Design Analysis
 
2001-01-2950
Distributed Maintenance Error Information, Investigation and Intervention
 
2001-01-3028
Dynamometer Simulation of Aircraft Tire Wear Due to Braking
 
2001-01-2958
ECATA and Other European Co-operative Programmes
 
2001-01-2990
Experimental and Computational Modeling of the Aerodynamics of a Racecar
 
2001-01-2992
FTE and Pilot Workload Comparison of Perspective Flight Guidance Displays to Conventional Flight Director Symbology in Instrument Approach Applications
 
2001-01-2957
French Aerospace Education
 
2001-01-3030
German V/STOL Transport Programs in the Twentieth Century
 
2001-01-3017
Identification of the Requirements Space Topology for a Rapid Response Strike System
 
2001-01-2978
Influence of Wing-tip Dihedral and Planform on Induced Drag
 
2001-01-3037
Maintenance and Engineering: Keeping Airplanes in the Sky
 
2001-01-2949
On-Line Maintenance Resource Management Training: The Smart Center
 
2001-01-2963
Organization of Signal Data Sets For Evaluation and Rating of Diagnostic and Prognostic Signal Analysis Techniques
 
2001-01-3008
Quantities, Characteristics and Reduction Potentials of Aircraft Engine Emissions
 
2001-01-2665
Reducing Human Errors in Aircraft Maintenance
 
2001-01-3026
Reviewing The Role of Cockpit Alerting Systems: Implications for Alerting System Design and Pilot Training
 
2001-01-2995
TDMA Air-to-Air Surveillance System for Helicopter Safety
 
2001-01-2954
The Generic Aircraft-Store Interface Framework
 
2001-01-2951
The Role of Standardization on the Journey to “Plug & Play” Weapons
 
2001-01-3000
Use of Probabilistics in Campaign Analysis
 
2001-01-2566
An Investigation into the Use of Small, Flexible, Machine Tools to Support the Lean Manufacturing Environment
 
2001-01-2570
Automated Alignment and Marry-Up of Aircraft Fuselage Sections with a Final Assembly Line
 
2001-01-2568
Automated Cold Working Using Split Mandrel Technology
 
2001-01-2565
Automated Drilling Systems of ARIANE 5 Structures
 
2001-01-2572
Automated Support of Manual Fastening Operations
 
2001-01-2576
Drill and Drive End Effector
 
2001-01-2608
F/A-18 E/F Outer Wing Lean Production System
 
2001-01-2579
Flexible Automated Riveting of Fuselage Skin Panels
 
2001-01-2606
Frequency Response Measurement of Cutting Tools for Aerospace Applications
 
2001-01-2567
High Accuracy Drilling and Reaming Machines Used on a 340-500/600 Final Assembly
 
2001-01-2610
Laser Forming of Aerospace Alloys
 
2001-01-2607
Machined Component Quality Improvements Through Manufacturing Process Simulation
 
2001-01-2569
Method of Accurate Countersinking and Rivet Shaving
 
2001-01-2575
New Fasteners Used on the Composite Keel Beam for the A340-500/600 Program
 
2001-01-2571
Orbital Drilling of Sandwich Constructions for Space Applications
 
2001-01-2624
Process Simulation of Superplastic Forming of Titanium Structure
 
2001-01-2573
Single-Pass Drilling of Composite/Metallic Stacks
 
2001-01-2605
The Effect of Process Damping On Stability and Hole Form in Drilling
 
2001-01-2578
The StressWaveTM Fatigue Life Enhancement Process
 
2001-01-3001
Trajectory Generation Using Genetic and Sequential Quadratic Programming Methods
 
2001-01-2574
Understanding Exit Burr in the Drilling Process
 
2001-01-2620
Virtual Extended Enterprises, Trusted Agents, Unions, Temp Agencies, Info-expeditors, and The “Bonkers” Business Environment
 
2001-01-2484
Recent Advances in Reducing Fuel Permeability and Leakage into the Environment from Automotive Fuel Systems
 
2000-01-5535
1998/1999 AIAA Foundation Graduate Team Aircraft Design Competition: Super STOL Carrier On-board Delivery Aircraft
 
2000-01-5560
A Method for Concept Exploration of Hypersonic Vehicles in the Presence of Open & Evolving Requirements
 
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
 
2000-01-5546
Aircraft Design Optimizing Operators, Environmental System and Manufacturers Requirements
 
2000-01-5544
An Applied Program of Aviation Safety Training for the Civil Aviation Flying College of China
 
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
 
2000-01-5510
An Experimental and Theoretical Study of Reynolds and Mach Number Effects at Two-Dimensional Wind Tunnel Testing
 
2000-01-5518
Augmentation for Synthetic Vision Displays – An Energy Based Approach
 
2000-01-5596
Automation Issues: Perspectives from the Flight Deck
 
2000-01-5577
Benefits of Door-to-Door Travel Time Reduction to US Economy
 
2000-01-5501
Certification Flight Test for an Extended Range Modification for the Cessna 337 Aircraft
 
2000-01-5542
Costs and Benefits of Head up Displays: An Attention Perspective and a Meta Analysis
 
2000-01-5538
Design of a High-g Unmanned Aerial Vehicle Structure
 
2000-01-5598
Developing a Pilot-Centered Autoflight Interface
 
2000-01-5585
Fasteners Modeling for MSC.Nastran Finite Element Analysis
 
2000-01-5559
Formulation, Realization, and Demonstration of a Process to Generate Aerodynamic Metamodels for Hypersonic Cruise Vehicle Design
 
2000-01-5617
How to Involve Younger Members and Non-North Americans in Standards Development - an Imperative for U.S. Business
 
2000-01-5595
Identifying Flight Deck Automation Issues
 
2000-01-5586
Impact Simulation of Simplified Structural Models of Aircraft Fuselage
 
2000-01-5561
Implementation of Parametric Anaylsis to the Aerodynamic Design of a Hypersonic Strike Fighter
 
2000-01-5573
Information Requirements for Traffic Awareness in the Free-flight Environment
 
2000-01-5521
Integration of Cockpit Displays for Surface Operations: The Final Stage of a Human-Centered Design Approach
 
2000-01-5545
Intelligent Tutoring Systems for Aviation Automation
 
2000-01-5500
MICCO Mac-145B Spin Flight Test
 
2000-01-5589
Methodology for Assessing Survivability Tradeoffs in the Preliminary Design Process
 
2000-01-5618
Methodology for the Parametric Structural Conceptual Design of Hypersonic Vehicles
 
2000-01-5505
Military Pilot Training Concepts
 
2000-01-5534
Modeling and Design of Piezoelectric Actuators for Fluid Flow Control
 
2000-01-5619
Modifications Required to Convert a U.S. Registered Aircraft for European Operations
 
2000-01-5503
Next Generation European Air System
 
2000-01-5593
Optimal and Near-Optimal Take-off Maneuvers in the Presence of Windshear
 
2000-01-5547
Regional Aircraft Family Design
 
2000-01-5549
Research Programs for Transport Aircraft in Europe
 
2000-01-5525
Scenario-Based Systems Studies for Military Aircraft
 
2000-01-5516
Specialized Anti-Armor Aircraft of the Eastern Front: 1941-1945
 
2000-01-5502
The Bombardier Flight Test Center - Meeting the Challenge
 
2000-01-5578
The C-17 Global Air Traffic Management (GATM) Application
 
2000-01-5543
The Fundamentals of Performance Based Training in Aviation
 
2000-01-5594
The Three Facets of Risk
 
2000-01-5590
Use of Flight Simulation in Early Design: Formulation and Application of the Virtual Testing and Evaluation Methodology
 
2000-01-5511
Wake Flow in an Adverse Pressure Gradient
 
2000-01-1677
The Rise and Fall of General Aviation — An Economists View with Focus on Single Engine Aircraft and the Impact of Airline Deregulation
 
1999-01-5554
A New Replaceable Contact Aircraft Power Receptacle
 
1999-01-5555
A System-of-Systems Approach to Aerospace Ground Equipment
 
1999-01-5619
Advanced Aerodynamic Control Effectors
 
1999-01-5598
Advances in Projection Moiré Interferometry Development for Large Wind Tunnel Applications
 
1999-01-5500
Aerodynamic Shape Optimization: Methods and Applications
 
1999-01-5618
CFD Modeling of 2-D Aileron Effectiveness
 
1999-01-5551
Combined Loads, Vibration, and Modal Testing of the QuikSCAT Spacecraft
 
1999-01-5550
Direct Acoustic Test of Quikscat Spacecraft
 
1999-01-5553
Direct, Near Field Acoustic Testing
 
1999-01-5578
Enabling Advanced Design Methods in an Internet-Capable Framework
 
1999-01-5659
Enhanced/Synthetic Vision Systems for Search and Rescue Operations
 
1999-01-5506
Improving AC-130H Gunship Performance Through Drag Reduction - A Wind Tunnel and Flight Test Partnership
 
1999-01-5534
Introduction to Flight Testing Using an Aerobatic Trainer
 
1999-01-5577
Low Speed Wind Tunnel Testing of a Laser Propelled Vehicle
 
1999-01-5576
Microphone Array Phased Processing System (MAPPS): Phased Array System for Acoustic Measurements in a Wind Tunnel
 
1999-01-5621
Multidisciplinary Design Optimization of a Transonic Commercial Transport with a Strut-Braced Wing
 
1999-01-5559
Numerical Study of a Trapezoidal Wing High-Lift Configuration
 
1999-01-5611
Pilot’s Control Actions During Aircraft Maneuvering Support System as a Mean of “Board Intellect” Increase
 
1999-01-5625
Starcar on the Road
 
1999-01-5622
Supersonic Business Jet Design Through Bi-Level Integrated System Synthesis
 
1999-01-5503
Survivability Benefits from the Use of Standoff Weapons by Stealth Aircraft
 
1999-01-5558
Three-Dimensional Viscous Flow Analysis for High-Lift Configurations Using a Parallel Unstructured Multigrid Solver
 
1999-01-5557
Unstructured Grid Generation for Complex 3D High-Lift Configurations
 
1999-01-5623
Viable Designs Through a Joint Probabilistic Estimation Technique
 
1999-01-5510
Visual Speech Interface: Apparatus and Algorithms
 
1999-01-2981
Human Factors Analysis of Naval Transport Aircraft Maintenance and Flight Line Related Incidents
 
1999-01-2982
Maintainer Perceptions of Naval Transport Aircraft Maintenance and Flight-Line Operations
 
1999-01-1578
Activities of the Federal Aviation Administration’s Aviation Weather Research Program
 
1999-01-1592
Aerodynamic Effects of Oversized Tires and Tall Landing Gear on a Small General Aviation Aircraft
 
1999-01-1587
Analysis Tools for DaDTA on Riveted Lap Joints
 
1999-01-1586
Analysis of Widespread Fatigue Damage in Lap Joints
 
1999-01-1585
Application of Shape Memory Alloys for Leading Edge Deicing
 
1999-01-1579
Aviation Weather Information Systems Research and Development
 
1999-01-1583
Detection of Icing and Related Loss of Control Effectiveness in Regional and Corporate Aircraft
 
1999-01-1584
Experimental Investigation of Ice Adhesion
 
1999-01-1561
Fatigue Analysis of an Aircraft Wing Spar
 
1999-01-1589
Fracture Mechanics Based Approach for Quantifying Corrosion Damage
 
1999-01-1581
Math Modeling of Propeller Geometry and Aerodynamics
 
1999-01-1576
Mathematical Models of Fastened Structural Connections
 
1999-01-1580
Newton II Aircraft Powerplant Test Cell Mount
 
1999-01-1574
Residual Strength of an Aluminum Panel with a Centric Hole and One Cracked Ligament
 
1999-01-1593
SJ30-2 High Performance Business Jet Development: A Prototype Based Approach
 
1999-01-1575
Strength of Stiffened Panels with Multiple Site Damage
 
1999-01-1604
The Effect of Age on Computer Input Device Use: Performance and Ratings of Perceived Exertion
 
983129
High Fatigue Life Bearings and Bushings
 
983128
The Advanced Split Mandrel Coldworking Process in Various Military Life Extension Applications
 
985525
A Hypersonic Cruiser Concept for the 21st Century
 
985508
AGDA: Airplane Geometry Design Assistant
 
985591
Analysis of Vortex Wake Effect on the Aircraft Model and Search for Aerodynamic Means to Compensate It
 
985500
Application of Computational Fluid Dynamics at Eglin Air Force Base
 
985597
Barrel Aircraft Engines: Historical Anomaly or Stymied Innovation?
 
985555
Evaluation of Near-Term Applications for ADS-B/CDTI Implementation
 
985539
Impacts of Structural Dynamics on Engine Inlet Flow Characteristics
 
985546
Inlet Unstart Influence on Aerodynamic Characteristics of Next Generation Supersonic Transport (SST)
 
985544
Prediction of Airfoil Performance with Leading Edge Roughness
 
985550
The Boeing 777-300/PW4098 Flying Test-Bed Program
 
985558
The Surface Operations Research and Evaluation Vehicle (SOREV): A Testbed for HSCT Taxi Issues
 
981695
Sojourner on Mars and Lessons Learned for Future Planetary Rovers
 
975559
Semi-Empirical Vortex Step Method for the Lift and Induced Drag Loading of 2D or 3D Wings
 
975542
CRISTO: A Code for Integrated Synthesis and Trajectory Optimization of Commuter and Regional Aircraft
 
975500
The Experimental Investigation of HLFC-System Use on the Swept Wing at Subsonic Velocities
 
970136
Contemplation of Nozzle Blockage in Open Jet Wind-Tunnels in View of Different ‘Q’ Determination Techniques
 
970411
Experiments and Numerical Investigation on a Multi-Component Airfoil Employed in a Racing Car Wing
 
965547
Aircraft Vortex Wake Dynamics
 
965567
An Update on RDS - Professional
 
965564
Attachment-Line Transition and Boundary-Layer Relaminarization on a High-Lift Wing in Flight
 
965546
Evolution of the Pair of Rectilinear Laminar Vortices in a Stratified Atmosphere
 
965548
Gasdynamics and Optics of an Aircraft Condensable Wake
 
965545
Simulation of Vortex Wake Impact on a General-Aviation Aircraft Model in a Wind Tunnel Using the Airfoil Lattice
 
965562
Studies on Vortex Wake Evolution and Flight Safety Problems
 
951977
Aerodynamic Influence of a Finite-Span Flap on a Simple Wing
 
952036
An Examination of Aircraft Aerodynamic Estimation Using Neural Networks
 
951432
Aerodynamic Investigation of Wing Tip Sails
 
951182
Unsteady Transonic Aerodynamics in Frequency Domain and Calculation of Flutter Characteristics of Aircraft
 
942100
Balance Accuracy and Repeatability Measured at Low Loads
 
941142
A Comparative Study of Four Algebraic Transition Models
 
941143
An Easy Way to Analyze Longitudinal and Lateral-Directional Trim Problems with AEO or OEI
 
941144
An Inviscid Aerodynamic Investigation of Wing/Winglet Geometries for RPV Applications
 
941140
Dependence of Integrated Vertical-Tail Buffet Loads For F/A-18 on Sensor Density
 
941141
Vortex Developments Over NACA 0015 Airfoil with Trailing Edge Jet
 
940061
The Latest Progress in the Computational Aerodynamic System for Practical Aircraft Configurations
 
932574
A Brief Survey of Wing Tip Devices for Drag Reduction
 
932571
ACCURATE DRAG PREDICTION - A PREREQUISITE FOR DRAG REDUCTION RESEARCH
 
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
 
932624
Civil Aircraft Propulsion Integration - Current & Future
 
932510
Compressible Navier-Stokes Calculations of the Flow Over Airfoil Sections. Comparison of 1st and 2nd Order Turbulence Models
 
932514
Computational Aerodynamic Analysis on the Open Skies Aircraft
 
932532
Computational Fluid Dynamics with Icing Effects
 
932513
Computational Study of Boundary Layer Control for Improving Airfoil Performance
 
932531
Computational Study of a Two-Slot Circulation Control Airfoil
 
932572
Low Reynolds Number Laminar Separation Bubble Control Using a Backward Facing Step
 
932512
Modeling Aerodynamic Problems Using Smoothed Particle Hydrodynamics (SPH)
 
932515
Nonlinear Analysis of Swept Wing Transitional Boundary Layers
 
932573
On the Differences Between the Effect of Acoustic Perturbation and Unsteady Bleed in Controlling Flow Separation Over a Cylinder
 
932511
Three-Dimensional Steady Flow Computations in Manifold-Type Junctions and a Comparison with Experiment
 
931384
A Design Trade Study Using CFD Modeling of Reaction Jets for Aerodynamic Control
 
931370
An Experimental Investigation of Forward-Swept Wings at Low Reynolds Numbers
 
931385
Comparative Analysis of Navier-Stokes Codes - Accuracy and Efficiency
 
931386
Hybrid Laminar Flow Over Wings Enhanced by Continuous Boundary-Layer Suction
 
931368
Primary and Secondary Vortex Structures Over Accelerated-Decelerated Airfoils at High Angles of Attack
 
931383
Some Additional Stability and Performance Characteristics of the Scissor/Pivot Wing Configurations
 
921996
A Summary of the Forebody High-Angle-of-Attack Aerodynamics Research on the F-18 and the X-29A Aircraft
 
922007
Advanced Diagnostics Research for High Speed Aerodynamic Testing
 
921985
An Assessment of Varying Mission Requirements on Fighter/Attack Aircraft Sizing
 
922009
An Overview of Doppler Global Velocimetry
 
921923
Analysis of the Effect of Heat Strips on Boundary Layer Development Over a Flat Plate
 
921924
CFD Analysis of Ejection Seat Escape Systems
 
921926
Comparative Study of MacCormack and TVD MacCormack Schemes for Three-Dimensional Separation at Wing/Body Junctions in Supersonic Flows
 
922008
Flight Testing of Pneumatic Forebody Vortex Control on the X-29 Technology Demonstrator
 
921990
Influence of Two-Dimensional Imperfections on Laminar Flow
 
921925
Investigation of the Longitudinal Stability of the T-45A withComputational Fluid Dynamics
 
921928
Numerical Analysis of Turbine Blade Tip Treatments
 
921986
Role of Micron - Sized Roughness in Swept - Wing Transition
 
922010
Stall Warning Using Contamination Detecting Aerodynamics
 
921987
Streamline - Curvature Effect in Three - Dimensional Boundary Layers
 
921991
Three-Dimensional Boundary Layer Stability and Transition
 
921937
Transonic Propulsion Aerodynamics Research at NASA Langley Research Center
 
912020
Aerodynamic Characteristics Near the Tip of a Finite Wing by a Panel Method
 
912010
Aerodynamic Development of Boundary Layer Control System for NAL QSTOL Research Aircraft ‘ASKA’
 
912044
Aerodynamic Heating in Three-Dimensional Shock Wave Turbulent Boundary Layer Interaction Induced by Sweptback Sharp Fins in Hypersonic Flows
 
912002
Applicability of Euler Analysis to Prop-Fan Aerodynamic Design
 
911990
Computational Aerodynamics in Aircraft Design: Challenges and Opportunities for Euler/Navier-Stokes Methods
 
911988
Computational Aerodynamics: The Next Generation
 
911992
Computational Fluid Dynamics Applications in Airplane Cabin Ventilation System Design
 
911981
Experimental Studies on Aerodynamic Characteristics of SSTO Vehicle at Low Subsonic Speeds
 
912004
Free Wake Analyses of a Hovering Rotor Using Panel Method
 
911991
Numerical Simulations of Separated Flows Around Oscillating Airfoil for Dynamic Stall Phenomena
 
912003
Recent Applications of the FNS Zonal Method to Complex Flow Problems
 
911974
The High Speed Challenge for Rotary Wing Aircraft
 
911989
The Impact of CFD on the Airplane Design Process: Today and Tomorrow
 
910990
A Computational Model for the Analysis of Finite Wings in Potential Flow
 
910991
A Vortex Lattice Model for Delta Wings with Bursting
 
911026
Aerodynamic Impact of Deicing/Anti-Icing Fluids on Commuter Aircraft
 
911019
Aerodynamic Performance of Wing-Body Configurations and the Flying Wing
 
911174
Numerical Simulation of Propulsion-Induced Aerodynamic Characteristics on a Wing-Afterbody Configuration with Thrust Vectoring
 
910995
Petroleum Helicopters Inc. - A Success Story
 
910992
TVD Formulations of the 2D Navier-Stokes Equations for Airfoil Analysis
 
910994
The Evolution of an Airline Piedmont Airlines 1948 - 1989
 
901857
AIRPLANE: Unstructured-Mesh Applications
 
901866
An Application of Wing Aerodynamic Principles to the Reduction of Road Vehicle Air Drag Loads
 
901988
Application of Favorable Aerodynamic Interference to Supersonic Airplane Design
 
901992
Application of Very Thick BLC Airfoils to a Flying Wing Type Transport Aircraft
 
901809
BOUNDARY-LAYER STABILITY ANALYSIS OF FLIGHT-MEASURED TRANSITION DATA
 
901935
Calculation and Measurement of Induced Drag at Low Speeds
 
901854
Computational Analysis of the External Flowfield About a Fighter Configuration
 
901855
Efficient Euler Analysis of Transonic Flow Around Advanced Turbo-Prop.
 
901869
Experimental Evaluations of the Aerodynamics of Unlimited Racing Hydroplanes Operating in and out of Ground Effect
 
901979
Flight Experiments Studying the Growth of Disturbances in the Laminar Boundary Layer
 
901978
HYBRID LAMINAR FLOW CONTROL TESTS IN THE BOEING RESEARCH WIND TUNNEL
 
901934
Induced Drag of a Simple Wing From Wake Measurements
 
901856
Internal and External Flow Simulation Using Multizone Euler/Navier-Stokes Aerodynamic Methods
 
901808
Navier-Stokes Computations of Transition to Turbulent Flow Around Airfoils
 
901852
Non-Linear Aeroelastic Predictions for Transport Aircraft
 
901812
Numerical Anaylsis of Compressible Flow Around Three-Dimensional Fin-Body Combination
 
901811
Numerical Solutions for Axisymmetric Bodies of Revolution in Pitching Oscilliatory Motion
 
901932
PROSPECTS FOR DRAG PREDICTION USING COMPUTATIONAL FLUID DYNAMICS
 
901987
Some Thoughts on the Design of Subsonic Transport Aircraft for the 21st Century
 
901993
Supersonic Aerodynamic Characteristics of a Maneuvering Canard-Controlled Missile with Fixed and Free-Rolling Tail Fins
 
901868
The Aerodynamic Development of the University of Maryland's “Pride of Maryland” Solar Powered Vehicle
 
901933
The Computation of Induced Drag with Nonplanar and Deformed Wakes
 
901807
Visualization Research at Grumman's Computer Applications Laboratory (CAL)
 
901867
Wind Tunnel and Tract Testing an ARCA Race Car
 
901936
Wingtip Vortex Turbine Investigation for Vortex Energy Recovery
 
892315
A MACH 6 External Nozzle Experiment with Argon-Freon Exhaust Simulation
 
892322
A Nonlinear Transient Formulation of UHB Aeroelastic Response and Stability: Part 1 - Theoretical Formulation
 
892287
A VSAERO Analysis of Several Canard Configured Aircraft - Part 2
 
892344
An Entropy Method for Induced Drag Minimization
 
892288
Application of Divergent Trailing-Edge Airfoil Technology to the Design of a Derivative Wing
 
892381
Computational Results for the Effects of External Disturbances on Transition Location on Bodies of Revolution from Subsonic to Supersonic Speeds and Comparisons with Experimental Data
 
892224
Effects of Turbulence Models on The Prediction of Transonic Wing Flows
 
892220
Forebody Vortex Manipulation for Aerodynamic Control of Aircraft at High Angles of Attack
 
892310
Hypersonic CFD Applications for the National Aero-Space Plane
 
892345
Hypersonic Forebody Lift-Induced Drag
 
892222
In-Flight Flow Visualization Characteristics of the NASA F-18 High Alpha Research Vehicle at High Angles of Attack
 
892341
Induced Drag - Historical Perspective
 
892312
Low-Speed Aerodynamic Characteristics of a Powered Nasp-Like Configuration in Ground Effect
 
892314
NUMERICAL SIMULATION OF FLOW THROUGH THE LANGLEY PARAMETRIC SCRAMJET ENGINE
 
892202
Some Aerodynamic Characteristiscs of the Scissor Wing Configuration
 
892313
Stability Characteristics of a Conical Aerospace Plane Concept
 
892245
The Development of Crossflow Vortices on a 45 Degree Swept Wing
 
892291
Three Dimensional Flow Calculations for a Projectile with Standard and Dome Bases
 
892379
Transition Research in the Mach 3.5 Low-Disturbance Wind Tunnel and Comparisons of Data with Theory
 
892289
Transonic Analysis of Complex Configurations Using TRANAIR Program
 
892221
VORTEX CONTROL FOR TAIL BUFFET ALLEVIATION ON A TWIN-TAIL FIGHTER CONFIGURATION
 
892346
Vortical Sources of Aerodynamic Force and Moment
 
891022
A Low Cost Stall/Spin Simulator
 
891032
A Review and Update of the NASA Aircraft Noise Prediction Program Propeller Analysis System
 
891020
An Iterative Non-Linear Lifting Line Model For Wings with Unsymmetrical Stall
 
891040
Blade Surface Pressure Measurement on a Pusher Propeller in Flight
 
891021
DEVELOPMENT OF A STALL IMPROVEMENT PACKAGE FOR THE GULFSTREAM IV
 
891019
Spanwise Distribution of Lift and Drag at High Angles of Attack
 
881452
A New Look At Wind Tunnel Flow Quality For Transonic Flows
 
881354
Aerodynamic Technology Opportunities for a High-Speed Civil Transport
 
881386
An Overview of the Current NASA Program on Aircraft Icing Research
 
881397
Design Aspects of Long Range Supersonic LFC Airplanes with Highly Swept Wings
 
881454
Emerging Technology for Transonic Wind-Tunnel-Wall Interference Assessment and Corrections
 
881393
Fifty Years of Laminar Flow Flight Testing
 
881524
Hypersonic Aerodynamics at North Carolina State University
 
881519
Hypersonic Aerodynamics at The Ohio State University
 
881521
Hypersonic Research at Stanford University
 
881520
Inviscid Flow Field Computation of Hypervelocity Projectiles
 
881449
Preliminary Test Results of NDA Cryogenic Wind Tunnel and Its System
 
881396
Studies of Friction Drag and Pressure Drag of Airfoils Using the Eppler Program
 
881522
The Hypersonics Program at SUNY/Buffalo
 
881353
What Drives Unique Configurations
 
881356
Wind-Tunnel Investigation of the Low-Speed Aerodynamics of Slender Accelerator-Type Configurations
 
880925
Some Validations by Experimental Results in Hypersonic Flow Computations
 
872308
Effect of Ground Proximity on the Aerodynamic Characteristics of the STOL Aircraft
 
872333
Propulsion/Aerodynamic Integration in ASTOVL Combat Aircraft
 
872449
Aeroelasticity Past Present and Future
 
872448
Numerical Approach of Advanced Turboprop with Three-Dimensional Euler Equations
 
872447
Unified Computation Method of Unsteady Supersonic/Hypersonic Flow Past Two Dimensional Fiat Plate and Rectangular Wings
 
871905
A General Effectiveness Methodology for Aircraft Survivability Assessments
 
871794
An Implicit Approach to the Aerodynamic Calibration of Stores of Compressed Carriage Configuration
 
871756
Design of Transonic Airfoils and Wings Using a Hybrid Design Algorithm
 
871795
Experience with Prediction Techniques for Store Installed Drag and Store Release Characteristics
 
871796
Store Separation of Nuclear Weapons
 
871347
The Experimental Aircraft Programme
 
871041
Design and Development of a Light Weight, High Pressure Ratio Aircraft Turbocharger
 
870727
Endurance Group C1 Lancia Racing Car-Definition of Rear Wing Aerodynamic Contour
 
861685
Supersonic Cruise Technology Roadmap
 
861765
A Summary of Reynolds Number Effects on Some Recent Tests in the Langley 0.3-Meter Transonic Cryogenic Tunnel
 
861767
A Summary of the Effects of Reynolds Number on Drag Divergence for Airfoils Tested in the Langley 0.3-Meter Transonic Cryogenic Tunnel
 
861815
An Introduction to Flight Simulation for the Aerodynamic Engineer
 
861645
Flow Patterns of a Pivoted Rectangular Wing Aircraft
 
861744
High Speed Wind Tunnel Tests of the PTA Aircraft
 
861719
INSTALLATION AERODYNAMICS OF WING-MOUNTED, SINGLE-ROTATION PROPFANS
 
861769
Large Eddy Breakup Devices as Low Reynolds Number Airfoils
 
861684
The Market Potential of Future Supersonic Aircraft
 
861154
Meeting the Air Cargo Challenge: Boeing's Aircraft Developments
 
860218
Aerodynamic Model for Wing-Generated Down Force on Open-Wheel-Racing-Car Configurations
 
851820
INVISCID AND VISCOUS SIMULATIONS OF HIGH ANGLE OF ATTACK FLOWS
 
851790
Reduced Navier-Stokes (RNS Relaxation Procedure for Internal Flows with Interaction)
 
851979
Aerodynamic Flight Testing of the Space Shuttle Orbiter
 
851818
A Three-Dimensional Boundary-Layer Method for Flow over Delta Wings with Leading-Edge Separation
 
851899
A Verification of Propulsion and Airplane Performance Models Generated from Flight
 
851817
Application of the Vortex-Lattice Method to High-Angle-of-Attack Subsonic Aerodynamics
 
851821
Pivotable Strakes for High Angle of Attack Control
 
851770
Swept Wing-Tip Shapes for Low-Speed Airplanes
 
851895
Wake Imaging System Applications at the Boeing Aerodynamics Laboratory
 
850896
Aerodynamics of Liquid-Cooled Aircraft Engine Installations
 
850872
Propulsive Efficiency and Aircraft Drag Determined From Steady State Flight Test Data
 
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
 
850862
Further Results of Natural Laminar Flow Flight Test Experiments
 
850865
Interdependence of Parameters important to the Design of Subsonic Canard-Configured Aircraft
 
850864
Natural Laminar Flow and Regional Aircraft
 
841480
Aerodynamic Test Results for a Wing-Mounted Turboprop Propulsion Installation
 
841477
Design and Experimental Evaluation of Propfan Inlets
 
841478
Engine Inlet Interaction with a Prop-Fan Propulsion System
 
841465
Flight Deck Displays for Managing Wind Shear Encounters
 
841539
Investigation of Transonic Inlet Drag Characteristics
 
841543
Results of a Wind Tunnel/Flight Test Program to Compare Afterbody/Nozzle Pressures on a 1/12 Scale Model and a F-15 Aircraft
 
841242
Computer Modelling of Spark Ignition Engined Cars Showing What Fuel Economy is Feasible by the Year 2000
 
841021
Summary of the Weight and Balance, and The Drag Characteristics of a Typical Ultralight Aircraft
 
830741
Airfoil Stall Prediction with 2-D Wind Tunnel and 3-D Flight Verification
 
830709
Studies of Light-Twin Wing-Body Interference
 
820729
Advanced Technology for the SAAB-Fairchild 340 Aircraft
 
820956
Applications of Advanced Upper Surface Blowing Propulsive-Lift Technology
 
821469
Flight at Supernormal Attitudes
 
821467
Low-Speed Aerodynamic Characteristics of a Generic Forward-Swept-Wing Aircraft
 
811035
Mission-Adaptive Wing Flight Demonstration Program
 
811071
Operating Flight Loads and Their Effect on Engine Performance
 
PHOTO
Photo Of Page
 
810625
Aerodynamic Design Data For a Cruise-Matched High Performance Single Engine Airplane
 
810623
Full-Scale Study of the Cooling System Aerodynamics of an Operating Piston Engine Installed in a Light Aircraft Wing Panel
 
810577
Analytical Studies on the Effects of Cooling Flows on Light Aircraft Drag
 
810599
Analytical Techniques for the Analysis of Stall/Spin Flight Test Data
 
810606
Effects of Wingtip Modifications on Handling Qualities of Agricultural Aircraft
 
810567
Free Flight Research at Lockheed-Georgia
 
810610
Matrix Load Analysis Method for Flexible Aircraft Structures
 
810586
Noise and Performance of General Aviation Aircraft: A Review of the MIT Study
 
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
 
801119
A Status Report on the Energy Efficient Engine Project
 
801155
Aerodynamic Surface Cooling for Laminar Flow Control for Hydrogen-Fueled Subsonic Aircraft
 
801137
An Experimental Evaluation of the Performance Deficit of an Aircraft Engine Starter Turbine
 
801139
Optimum Subsonic, High–Angle–of–Attack Nacelles
 
801178
Preliminary Aerodynamic Characteristics of Several Advanced VSTOL Fighter/Attack Aircraft Concepts
 
800731
Aerodynamic Development of the Engine Nacelle Combination for the Boeing 767 Airplane
 
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
 
790567
Conversion of Wing Surface Pressures Into Normalized Lift Coefficient
 
790609
Determination of Cooling Air Mass Flow for a Horizontally - Opposed Aircraft Engine Installation#
 
791082
Effects of Forebody, Wing and Wing-Body-LEX Flowfields on High Angle of Attack Aerodynamics
 
790618
Full-Scale Wind-Tunnel Investigation of an Ayres S2R-800 Thrush Agricultural Airplane
 
790582
Improving Business Jet Performance: The Mark Five Sabreliner
 
791081
MCAIR Design Philosophy for Fighter Aircraft Departure and Spin Resistance
 
790575
The Design and Selection of Optimum Propellers for General Aviation Aircraft
 
790568
The Effects of Low-Level Wind Shear on the Approach and Go-Around Performance of a Landing Jet Aircraft
 
790581
The Learjet “Longhorn” Series - The First Jets with Winglets
 
781001
An Alternating Direction Explicit Method for Computing Three-Dimensional Viscous Flow Fields in Turbomachines
 
780997
Propeller Slipstream Wing Interactions at Mach No. 0.8
 
780999
TDS - A Preliminary Design System for Turbines
 
770449
Comparison of Predicted with Measured Aerodynamic Characteristics of the ATLIT Airplane
 
770464
Evaluation of Empennage Fatigue Loads for the Beech Super King Air Using a Flight Simulator
 
770461
IN-FLIGHT MEASUREMENTS OF THE GA(W)-2 AERODYNAMIC CHARACTERISTICS
 
760916
An Analytical Study of the Effects of Turbine Variable Geometry Operation on Turbine Blade Cooling Requirements for Fixed Match Point Turbojet Application
 
760481
Reduction of Stall-Spin Entry Tendencies Through Wing Aerodynamic Design
 
760482
Reflection-Plane Tests of Spoilers on an Advanced Technology Wing
 
760471
THE MARK II LEARJET FROM CONCEPT TO CERTIFICATION
 
751091
Aircraft Pay-Offs and Requirements for a Jet Flap Propulsion System
 
751077
Fairchild Republic Advanced Fighter Technology Integrator (AFTI)-Phase 1 Program Review
 
751100
Mechanically Coupled Lift Fan Propulsion and Control for Multimission V/STOL Aircraft
 
751088
Predicting Propulsion Related Drag of Jet Aftbodies
 
751092
Propulsion Concepts for High Speed Aircraft
 
751089
The Transonic Jet Flap-A Review of Recent Results
 
740368
FLIGHT TEST RESULTS FOR AN ADVANCED TECHNOLOGY LIGHT AIRPLANE WING
 
740470
Low-Speed Aerodynamics of the Upper-Surface Blown Jet Flap
 
740482
Opportunities in Flight/Propulsion Control Coupling (FPCC)
 
740889
Simulator and Flight Tests of a Side Force Control System in the A-9A Airplane
 
730318
APPLICATIONS OF ADVANCED AERODYNAMIC TECHNOLOGY TO LIGHT AIRCRAFT
 
730914
Air Force STOL Tactical Aircraft Investigation: Evaluation of Externally Blown Flaps
 
730305
Automated Prediction of Light Aircraft Performance and Riding and Handling Qualities
 
730915
External Blowing Flap Technology on the USAF McDonnell Douglas YC-15
 
730330
Feasibility and Optimization of Variable-Geometry Wing for Jet Amphibian Business Aircraft
 
730876
New Airfoil Sections for General Aviation Aircraft
 
730913
STOL Tactical Aircraft Investigation
 
730328
Some Aspects of STOL Aircraft Aerodynamics
 
730298
Some Effects of Camber on Swept-Back Wings
 
730916
Upper Surface Blowing Technology as Applied to the YC-14 Airplane
 
720337
Consideration of Application of Currently Available Transport-Category Aerodynamic Technology in the Optimization of General Aviation Propeller-Driven Twin Design
 
720861
Fly-Off in the Wind Tunnels
 
720856
NASA Lift Fan V/STOL Transport Technology Status
 
720321
Preliminary Results of Some Experiments with a Vortex Augmented Wing
 
720320
Thick-Wing Flight Demonstrations
 
710393
A Flight Control System Providing A Simple-to-Fly, Constant Attitude Aircraft
 
710379
A Review of The University of Kansas Light Airplane Research Program
 
710378
NASA Aerodynamic Research Applicable to Business Aircraft
 
700240
An Assessment of Performance, Stability, and Control Improvements for General Aviation Aircraft
 
700811
Synthesis of Future High Lift Systems
 
690305
Aerodynamic Improvements for Agricultural Aircraft
 
690724
Determination of the Influence of Propeller Thrust on CL and CD of an Airplane Using a Triple-Slotted Flap at Various Deflections
 
690662
Lifting Body Flight Tests and Analysis
 
690664
Materials Applications and Structural Concepts for Hypersonic Air-Induction Systems
 
680199
Aerodynamic Development of the Cessna 177
 
680711
Inlet and Fan Aerodynamics
 
680227
Propeller Design Consideration for Turbine Powered Aircraft
 
670353
ADAM II Propulsion System and Internal Aerodynamics
 
670244
Aerodynamic Considerations of a Medium Mach Business Aeroplane
 
670880
Aerodynamic Design Considerations of Variable Geometry Aircraft
 
670847
Aerodynamic Design Features of the C-5A
 
670846
Aerodynamic Design of the DC-9 Wing and High-Lift System
 
670243
Aerodynamics of the Cessna Tandem Twins
 
670845
Airfoil Analysis and Synthesis Utilizing Computer Graphics
 
670260
Flutter Characteristics of the Slab Tail
 
670242
Gulfstream II Aerodynamic Design
 
670245
High Lift Techniques for STOL Aircraft
 
660734
Aerodynamic Considerations for Engine Exhaust Design for Subsonic High Bypass Fan Engines
 
660733
Aerodynamic Considerations for Engine Inlet Design for Subsonic High Bypass Fan Engines
 
660732
Aerodynamic Installation of High-Bypass-Ratio Fan Engines
 
660671
Effects of Subsonic, Supersonic, Hypersonic, and Orbital Environments on Structures
 
660274
XB-70A Mach 3 Design and Operating Experience
 
650937
Development of the Model 727 Airplane High Lift System
 
650193
Helicopters and Propeller-Type VTOL Aircraft in the Light of Technologies
 
650800
Some Procedures for Use in Performance Prediction of Proposed Aircraft Designs
 
650203
The Propulsive Wing Turbofan V/STOL
 
640789
Aerodynamics and Flying Qualities of Jet V/STOL Airplanes
 
620492
AERODYNAMIC CONTROL OF DECELERATION AND RANGE FOR THE LUNAR MISSION
 
570165
CORRELATION OF AIRFOIL ICE FORMATIONS AND THEIR AERODYNAMIC EFFECTS WITH IMPINGEMENT AND FLIGHT CONDITIONS
 
540277
THE AERODYNAMIC AND POWER PLANT HEATING PROBLEM IN HIGH SPEED AIRCRAFT
 
490204
AERODYNAMICS OF HIGH-SPEED AIRPLANES
 
340081
Aerodynamics of Wing Sections for Airplanes
 

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