Accession Number:

AD0656570

Title:

AERODYNAMICS OF POWER PLANT INSTALLATION, PART II.

Descriptive Note:

Corporate Author:

ADVISORY GROUP FOR AERONAUTICAL RESEARCH AND DEVELOPMENT PARIS (FRANCE)

Personal Author(s):

Report Date:

1965-10-01

Pagination or Media Count:

376.0

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 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.

Subject Categories:

  • Transport Aircraft
  • VSTOL
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE