AERODYNAMICS OF POWER PLANT INSTALLATION, PART II.

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.

Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1965
Accession Number
AD0656570

Entities

Organizations

  • AGARD

Tags

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Boundary Layer
  • Exhaust Systems
  • Lift Fans
  • Propulsion Systems
  • Short Takeoff Aircraft
  • Simulations
  • Supersonic Transport Aircraft
  • Transport Aircraft
  • Vehicles
  • Wind Tunnel Models
  • Wind Tunnels
  • Wing Inlets

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Aerospace Engineering
  • Small Business Innovation Research Program (SBIR) EDI Research and Innovation.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow