SAE Papers

Paper Number	Paper Title	Book Number
2009-01-3247	Aerionics: An Update on this New Aero Industry for Flight Control
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	SP-2214
2008-01-2234	Active Vortex Generators Using Thrust Vectoring Plasma Actuators	V117-2008
2008-01-2275	Aerodynamic Comparison of Tilt-Rotor, -Wing and -Body Concept for Multi Task MAVs
2008-01-2267	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	V117-2008
2008-01-2233	Correlation of Hand Book Method Results with Wind Tunnel Data for a Subsonic UAV Design	V117-2008
2008-01-2268	Distributed Vehicle Concepts and Technologies	V117-2008
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	SP-2211
2008-01-2231	Hybrid Rigid/Inflatable Wings for Low Volume Wing Storage	SP-2211
2008-01-2238	Importance of Unmanned Air Vehicles	SP-2211
2008-01-2263	Jam-Free, Fail-Safe Flight Control System with Asymmetric Load Alleviation Capability	SP-2214
2008-01-2243	Nimbus Meta-plane, a New Aerodynamic Concept for Unmanned Hybrid Aerial Vehicle Application	SP-2211
2008-01-2244	Plasma Micro-thrusters for Micro Aerial Vehicles	SP-2211
2008-01-2237	Robust Control Design for a Flexible Unmanned Aerial Vehicle	SP-2211
2008-01-2269	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	V117-2008
2008-01-2255	Three-Movement Handlebar Piloting Control	SP-2214
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	V116-2007
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	V116-2007
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	V116-2007
2007-01-3858	Racecar Aerodynamic Optimization for an E-1 Class Streamliner Using Arbitrary Shape Defromation
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
2-27-8-16	Sound sound-research techniques
2007-01-3888	The 747-400 Dream Lifter - Overview & Mission	V116-2007
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 Gm-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 Modelling 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
2-24-8-40	Fine-Tuning Aerodynamics
2-24-7-13	A Developing Situation
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 Modelling of a Rotating Heat Pipe Aero-Engine Nose Cone Anti-Icing System
2003-01-3017	A Dry Aircraft Is a Safer Aircraft - Beating Condensation By Using Dry Air
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
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
2002-01-2921	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
2002-01-2948	Asymmetric Approach in Solving Aircraft Brake Vibration
2002-01-2958	Atn Airborne Implementation
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 NasaS Next-Generation Aviation Paradigm: a Summary of Research Findings
2002-01-2953	Electric Starting of Large Aircraft Engines
2002-01-2945	End Item Temperature Test--An Improved Lru-Level Screen
2002-01-2998	Enhanced Security Flight Deck Doors-Commercial Airplanes
2002-01-2941	Environmental Systems Considerations for Aircraft Cabins During Ground Operation
2002-01-2916	Estimation Technology of the Bell Model M427 Helicopter Using Parameter Assessment of the Dynamic Stability Characteristics
2002-01-3001	Fea Cyclic Symmetric Fatigue Analysis of Aircraft Wheels
2002-01-2957	Fire Resistant Composites
2002-01-2920	Flow Control Valve With Integrated Electronics for Aircraft Applications
2002-01-2931	Fuel Transfer System in the Conceptual Design Phase
2002-01-3008	Highlights of NasaS Systems Approach to Crashworthiness Research
2002-01-3006	Hud Symbology for Surface Operations: Command Guidance Versus Situation Guidance Formats
2002-01-2956	Hybrid-Ceramic Circumferential Carbon Ring Seal
2002-01-2927	Identification and Evaluation of Technologies for the Development of a Quiet Supersonic Business Jet
2002-01-2930	Impact of Configuration and Requirements on the Sonic Boom of a Quiet Supersonic Jet
2002-01-2990	Improving the Aerodynamic Efficiency of High Lift Devices By a Stiffness-Oriented Re-Design With Tailored Laminates
2002-01-3010	Incorporation of Lean Principles Through the Use of Flexible Fuel Tubing in a Large Military Transport Aircraft
2002-01-2919	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 VictrexSr PeekSt Thermoplastic to Drive New Designs, Processing Flexibility, and Cost Reduction in Aerospace Components
2002-01-3013	Utilization Life of Electronic Systems-Aging Avionics Usable Life and Wear-Out Issues
2002-01-2995	Vertical Drop Test of a Narrow-Body Transport Fuselage Section With Overhead Stowage Bins
2002-01-2997	Vertical Drop Test of a Transport Fuselage Section
2002-01-2912	Wind-Tunnel Investigation of Commercial Transport Aircraft Aerodynamics At Extreme Flight Conditions
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
2002-01-3191	Simulation of An Active Damping Device for Dc Power Networks
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
2002-01-2645	Affordable Reconfigurable Tooling
2002-01-2642	Airbus A340 Final Assembly By S.O.J.A.: Semi-Automatic Orbital Fuselage Join Up Robot
2002-01-2634	An Algorithm for Assembly Centric Design
2002-01-2640	Analysis and Modelling Reduce Development Risks for Improving Integration of Large Aircraft Components
2002-01-2629	C-17 Cargo Ramp and Door Automated Drilling and 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
2-21-10-29	737-800 Winglet Integration
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
2001-01-2566	An Investigation Into the Use of Small, Flexible, Machine Tools to Support the Lean Manufacturing Environment
2001-01-2988	Analytical and Numerical Modeling of the Turn Maneuver of Agricultural Aircraft
2001-01-2976	Assessment of the Overflow Navier Stokes Code for Various Airplane Components
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
2001-01-3025	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
2001-01-3034	Development of An Object-Oriented Vehicle Library for Automated Design Analysis
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
2001-01-2950	Distributed Maintenance Error Information, Investigation and Intervention
2001-01-2576	Drill and Drive End Effector
2001-01-3028	Dynamometer Simulation of Aircraft Tire Wear Due to Braking
2001-01-2958	Ecata and Other European Cooperative Programs
2001-01-2990	Experimental and Computational Modeling of the Aerodynamics of a Racecar
2001-01-2608	F/A-18 E/F Outer Wing Lean Production System
2001-01-2579	Flexible Automated Riveting of Fuselage Skin Panels
2001-01-2957	French Aerospace Education
2001-01-2606	Frequency Response Measurement of Cutting Tools for Aerospace Applications
2001-01-2992	Fte and Pilot Workload Comparison of Perspective Flight Guidance Displays to Conventional Flight Director Symbology in Instrument Approach Applications
2001-01-3030	German V/Stol Transport Programs in the Twentieth Century
2001-01-2567	High Accuracy Drilling and Reaming Machines Used on a 340-500/600 Final Assembly
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
2001-01-2610	Laser Forming of Aerospace Alloys
2001-01-2607	Machined Component Quality Improvements Through Manufacturing Process Simulation
2001-01-3037	Maintenance and Engineering: Keeping Airplanes in the Sky
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
2001-01-2949	On-Line Maintenance Resource Management Training: the Smart Center
2001-01-2571	Orbital Drilling of Sandwich Constructions for Space Applications
2001-01-2963	Organization of Signal Data Sets for Evaluation and Rating of Diagnostic and Prognostic Signal Analysis Techniques
2001-01-2624	Process Simulation of Superplastic Forming of Titanium Structure
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
2001-01-2573	Single-Pass Drilling of Composite/Metallic Stacks
2001-01-2995	Tdma Air-To-Air Surveillance System for Helicopter Safety
2001-01-2605	The Effect of Process Damping on Stability and Hole Form in Drilling
2-21-9-15	The Fantastic Five
2001-01-2954	The Generic Aircraft-Store Interface Framework
2001-01-2951	The Role of Standardization on the Journey to "Plug & Play" Weapons
2001-01-2578	The StresswaveSt Fatigue Life Enhancement Process
2001-01-2574	Understanding Exit Burr in the Drilling Process
2001-01-3000	Use of Probabilistics in Campaign Analysis
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	PT-71
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 Analysis 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
2000-01-5589	Methodology for Assessing Survivability Tradeoffs in the Preliminary Design Process
2000-01-5618	Methodology for the Parametric Structural Conceptual Design of Hypersonic Vehicles
2000-01-5500	Micco Mac-145b Spin Flight Test
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
2001-01-3001	Trajectory Generation Using Genetic and Sequential Quadratic Programming Methods
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
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 MoirAe 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	PilotS Control Actions During Aircraft Maneuvering Support System as a Means 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 AdministrationS 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
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
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
975542	Cristo: a Code for Integrated Synthesis and Trajectory Optimization of Commuter and Regional Aircraft
975559	Semi-Empirical Vortex Step Method for the Lift and Induced Drag Loading of 2d Or 3d Wings
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-Componnet Airfoil Employed in a Racing Car Wing
965547	Aircraft Vortex Wake Dynamics
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	Gas Dynamics and Optics of An Aircraft Condensable Wake
965567	Rds-Professional in Action: Aircraft Design on a Personal Computer
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	Aerodynamics 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 and 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	Modelling Aerodynamic Problems Using Smoothered 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 Configuration
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 Highsp Eed 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 With Computational 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
910994	The Evolution of An Airline--Piedmont Airlines 1948--1989
910992	Tvd Formulations of the 2d Navier-Stokes Equations for Airfoil Analysis
901857	Airplane: Unstructured-Mesh Applications
901866	An Application of Wing Aerodynamics 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 Measurements 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	Nonlinear Aeroelastic Predictions for Transport Aircraft
901812	Numerical Analysis of Compressible Flow Around Three-Dimensional Fin-Body Combination
901811	Numerical Solutions for Axisymmetric Bodies of Revolution in Pitching Oscillatory Motion
901932	Prospects for Drag Prediciton 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 MarylandS "Pride of Maryland" Solar Powered Vehicle
901933	The Computation of Induced Drag With Nonplanar and Deformed Wakes
901807	Visualization Research At GrummanS Computer Applications Laboratory (Cal)
901867	Wind Tunnel and Track Testing An Arca Race Car
901936	Wingtip Vortex Turbine Investigation for Vortex Energy Recovery
892322	A Nonlinear Transient Formulation of Ultra High Bypass Aeroelastic Response and Stability--Part I Theoretical Formulation
892222	In-Flight Flow Visualization Characteristics of the Nasa F-18 High Alpha Research Vehicle At High Angles of Attack
892202	Some Aerodynamic Characteristics of the Scissor Wing Configuration
891032	A Review and Update of the Nasa Aircraft Noise Prediction Program Propeller Analysis System
891040	Blade Surface Pressure Measurement on a Pusher Propeller in Flight
881386	An Overview of the Current Nasa Program on Aircraft Icing Research
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
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: BoeingS 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)
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
851979	Aerodynamic Flight Testing of the Space Shuttle Orbiter
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 An 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
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 Effect 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	Matric 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 Wind-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 Technnology 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
730914	Air Force Stol Tactical Aircraft Investigation: Evaluation of Externally Blown Flaps
730318	Applications of Advanced Aerodynamic Technology to Light Aircraft
730305	Automated Prediction of Light Aircraft Performance and Riding and Handling Qualities
730915	External Blowing Flap Technology on the Usaf/ Mcdonnell Douglas Yc-15 (Amst) Program
730330	Feasibility and Optimization of Variable-Geometry Wing for Jet Amphibian Business Aircraft
730876	New Airfoil Sections for General Aviation Aircraft
730328	Some Aspects of Stol Aircraft Aerodynamics
730298	Some Effects of Camber on Swept-Back Wings
730913	Stol Tactical Aircraft Investigation
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	Flight Control System Providing a Simple-To-Fly, Constant Attitude Aircraft
710378	Nasa Aerodynamic Research Applicable to Business Aircraft
710379	Review of the University of Kansas Light Airplane Research Program
700240	An Assessment of Performance, Stability, and Control Improvements for General Aviation Aircraft
700811	Synthesis of High Lift Systems for Future Turbofan Stol Aircraft
690305	Aerodynamic Improvements for Agricultural Aircraft
690724	Determination of the Influence of Propeller Thrust on the Coefficient of Lift and the Coefficient of Drag of An Airplane Using a Triple-Slotted Flap At Various Deflections
690662	Flight Tests and Analysis of Lifting Body Reentry Vehicles
690664	Materials Applications and Structural Concepts for Hypersonic Air-Induction Systems
680199	Aerodynamic Development of Cessna 177 Four-Place Single-Engine Cantilever-Wing Airplane
680711	Inlet and Fan Aerodynamics for Multimission Military Aircraft
680227	Propeller Design Considerations for Turbine-Powered Aircraft
670353	Adam(Air Deflection and Modulation)Is Applied to Propulsive Wing Airplane Configurations Housing Propulsion System
670244	Aerodynamic Considerations for 300-Mph Business Airplane - Handley Page Jetstream Twin Turboprop Airplane
670880	Aerodynamic Design Considerations of Variable Geometry Aircraft
670847	Aerodynamic Design Features of the C-5a Subsonic Jet Military Transport
670846	Aerodynamic Design of the Wing and High-Lift System of the Dc-9 Short-To-Medium-Range Jet Transports
670243	Aerodynamics of the Cessna Tandem Twins Business Aircraft
670845	Airfoil Analysis and Synthesis Utilizing Computer Graphics
670242	Design of Gulfstream Ii - a Low Wing Business Aircraft - of Moderate Sweep, Powered By Two Aft-Mounted Turbofan Engines
670245	High Lift Techniques for Stol Aircraft
660274	Aerodynamic Concepts and Configuration of Xb-70a Research Aircraft and Its Airborne Systems
660734	Aerodynamic Considerations for Engine Exhaust Design for Subsonic High-Bypass Fan Engines
660733	Aerodynamic Considerations for Engine Inlet Design for Subsonic High-Bypass Fan Engines
660732	Aerodynamic Installation of High-Bypass-Ratio Fan Engines on High Subsonic Aircraft
660671	Effects of Subsonic, Supersonic, Hypersonic and Orbital Environments on Structures
650937	Development of the Model 727 Airplane High Lift System
670260	Flutter Characteristics of the Slab Tail in Business Aircraft
650193	Helicopters and Propeller-Type Vtol Aircraft in the Light of Technologies
650800	Procedures for Use in the Performance Prediction of Proposed Aircraft Designs
650203	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