AERODYNAMICS OF POWER PLANT INSTALLATION, PART II.
ADVISORY GROUP FOR AERONAUTICAL RESEARCH AND DEVELOPMENT PARIS (FRANCE)
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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 VSTOL aircraft Aerodynamic interference effects with jet lift schemes on VSTOL aircraft at forward speeds Lift-fan VSTOL propulsion and airframe integration NASA research on the aerodynamics of jet VTOL engine installations Experimental studies of VTOL fan-in-wing inlets.
- Transport Aircraft
- Jet and Gas Turbine Engines