Contributions to the Development of a Power Spectral Gust Design Procedure for Civil Aircraft
Contributions to the Development of a Power Spectral Gust Design Procedure for Civil Aircraft
Preliminary Investigation of the Use of Throttles for Emergency Flight Control
Impact Data from a Transport Aircraft During a Controlled Impact Demonstration
Adaptive Wing Camber Optimization: A Periodic Perturbation Approach
Airplane Stopping Capability on Wet and Dry Runway Surfaces. (Model 707-123B and 720-023B)
Composite Impact Dynamics Research at NASA Larc: A Review
A Dynamic Simulation Study of the Sweptwing Transport Aircraft in Severe Turbulence
Simulation and Effects of Severe Turbulence on Jet Airline Pilots
GPSS/360 Computer Models to Simulate Aircraft Passenger Emergency Evacuation
Military and Commercial Aircraft Bearing Field Experience