Proceedings of a Workshop on V/STOL Aircraft Aerodynamics. Volume 2. Held At Naval Postgraduate School Monterey, California, May 16-18, 1979

Contents: Propulsion System/Airframe Interactions--Recent Applications of Theoretical Analysis to V/STOL Inlet Design, Inlet Operating Characteristics at High Angles of Attack, Low Speed Development of the Supersonic XFV-12A V/STOL Inlet, Subsonic VTOL Inlet Experimental Results, Inlet Ram Forces and Moments and V/STOL Aircraft, Theoretical Fan Velocity Distortions Due to Inlets and Nozzles, Aerodynamics of a Tilt-Nacelle V/STOL Propulsion System, Isolated Deflector Nozzle Static Tests for V/STOL Aircraft; V/STOL Aircraft Configurational Considerations and Developments--High Angle of Attack Aerodynamics at DTNSRDC, Development of High Lift Devices for Application to Advanced Navy Aircraft, YC-14 Low Speed Test Techniques, Vectored-Engine-Over- Wing Concept Development, Wind Tunnel Investigation of a Highly Maneuverable Supersonic V/STOL Fighter, Transition Characteristics of the External-Augmentor V/STOL Aircraft Concept, Calculation of Forces and Moments Acting on an Augmentor Wing for a VTOL Fighter in Hover or Transition Flight, Aerodynamics of an Advanced Jet Flap and an Ultra-STOL Application, and High Speed Aerodynamic Technology for V/STOL Fighter Attack Aircraft.