Preliminary Investigation of the Use of Throttles for Emergency Flight Control
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
Adaptive Wing Camber Optimization: A Periodic Perturbation Approach
Impact Data from a Transport Aircraft During a Controlled Impact Demonstration
Airplane Stopping Capability on Wet and Dry Runway Surfaces. (Model 707-123B and 720-023B)