Accession Number : AD0656570

Title :   AERODYNAMICS OF POWER PLANT INSTALLATION, PART II.

Corporate Author : ADVISORY GROUP FOR AERONAUTICAL RESEARCH AND DEVELOPMENT PARIS (FRANCE)

Report Date : OCT 1965

Pagination or Media Count : 376

Abstract : Contents: An investigation of splitter plates for supersonic twin inlets; Boundary-layer interaction effects in intakes with particular reference to those designed for dual subsonic and supersonic performance; Possibilites actuelles d' etude theorique d' une tuyere supersonique a double-flux; Methods of measuring aerodynamic efficiency and thrust vectors of engine exhaust systems; Propulsion system integration in wings; A fully integrated propulsion system for a supersonic transport aircraft; Jet VTOL power plant experience during flight test of X-14A VTOL research vehicle; Jet lift intakes; Techniques for the simulation of jet-lift engines in wind-tunnel models of V/STOL aircraft; Aerodynamic interference effects with jet lift schemes on V/STOL aircraft at forward speeds; Lift-fan V/STOL propulsion and airframe integration; NASA research on the aerodynamics of jet VTOL engine installations; Experimental studies of VTOL fan-in-wing inlets.

Descriptors :   (*AIRCRAFT ENGINES, AERODYNAMICS), AIRCRAFT ENGINE DUCTS, BOUNDARY LAYER, SUPERSONIC FLOW, WINGS, PROPULSION SYSTEMS, TRANSPORT AIRCRAFT, SUPERSONIC AIRCRAFT, VERTICAL TAKEOFF AIRCRAFT, LIFT, WIND TUNNEL MODELS, SHORT TAKEOFF AIRCRAFT, SYMPOSIA

Subject Categories : Transport Aircraft
      V/STOL
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE