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SAE Papers

Paper Number / Title
For more information, click on the Paper Number
Book Number
2008-01-2256
A Brief Study of Conditionally Enabled Phase Compensated Rate Limiters
 
2008-01-2253
Aircraft Performance Prediction: Comparison of Classical Handbook Methods to Detailed Time Integration Computer-Aided Methods
V117-1  
2008-01-2254
Cost Benefits of Aerodynamic Data Generation Techniques for Aircraft Stability and Control Analysis using the J2 Universal Tool-Kit
V117-1  
2008-01-2271
Dynamic Taxonomies Usage in the Context of Aeronautical Maintenance Processes to Increase the Effectiveness and the Efficiency of the Operations
 
2008-01-2272
Finite Element Modeling Strategies for Dynamic Aircraft Seats
 
2008-01-2265
Having 5000 Destinations in the Modern U.S. Airways System
 
2008-01-2263
Jam-Free, Fail-Safe Flight Control System with Asymmetric Load Alleviation Capability
 
2008-01-2262
Keys to Success with Knowledge-based Techniques
 
2008-01-2230
Model-Driven Architecture for Platform and Store Design
 
2008-01-2270
Modern Solutions for Ground Vibration Testing of Small, Medium and Large Aircraft
V117-1  
2008-01-2232
Operational Loads Monitoring of a Fleet of Beech 1900D Aircraft
V117-1  
2008-01-2266
Outsourcing Aircraft Maintenance Designed Around Safety, Diversification, and Performance
 
2008-01-2264
The Seven Parameters of Highly Effective Cable Control Systems
V117-1  
2008-01-2255
Three-Movement Handlebar Piloting Control
 
892205
The Effect of Solidity on Propeller Normal Force
 
880928
Aerothermodynamics—The Required Tools
 
871881
AFTI/F-111 Performance Flight Test Summary
 
871858
Boundary-Layer Instability Mechanisms on a Swept-Leading Edge at Mach 3.5
 
871859
Boundary-Layer Stability Analysis of NLF and LFC Experimental Data at Subsonic and Transonic Speeds
 
871792
IFM Applications to Trajectory Predictions–Past, Present and Future
 
871757
Theoretical and Experimental Analysis of the Siotted-Wall Flow Field in a Transonic Wind Tunnel
 
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
 
851771
The X-29 - a Unique and Innovative Aerodynamic Concept
 
851816
Leading-Edge Design for improved Spin Resistance of Wings Incorporating Conventional and Advanced Airfoils
 
851898
Status of Wind Tunnel Magnetic Suspension Research
 
851897
The NCSU Low Speed Boundary Layer Wind Tunnel
 
851895
Wake Imaging System Applications at the Boeing Aerodynamics Laboratory
 
841477
Design and Experimental Evaluation of Propfan Inlets
 
841478
Engine Inlet Interaction with a Prop-Fan Propulsion System
 
841539
Investigation of Transonic Inlet Drag Characteristics
 
831427
Propulsion Simulation Test Technique for V/STOL Configurations
 
770983
Comparison of Non-Axisymmetric & Axisymmetric Nozzles Installed on a V/STOL Fighter Model
 
720861
Fly-Off in the Wind Tunnels
 
690677
Some Recent Innovations in Wind Tunnel Testing Techniques
 
650197
Experimental Investigation of Inlet-to-Inlet Shock Interference
 
650202
High Bypass Lift/Cruise Fan The State Of The Art
 
650194
Research and Development of the Stowed Rotor V/STOL Concept
 

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