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.


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    Title :

    Aerodynamics of Power Plant Installation, Part II


    Publication date :

    1965


    Size :

    376 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English