Inlets and Nozzles for Aerospace Engines

Abstract

;Contents: Engine-airplane interference representation in wind tunnel testing; Thrust vectoring and control; V/stol inlets and nozzles; Supersonic inlets, nozzles, and applications; Subsonic and transonic aeropropulsion.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1971
Accession Number
AD0736310

Entities

Organizations

  • AGARD

Tags

Communities of Interest

  • Air Platforms
  • Ground and Sea Platforms
  • Human Systems
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircraft Equipment
  • Aircraft Industry
  • Aircrafts
  • Airframes
  • Boundary Layer
  • Computational Fluid Dynamics
  • Fighter Aircraft
  • Flow Visualization
  • Fluid Dynamics
  • Fluid Flow
  • Heat Transfer
  • Hydrodynamics
  • Pressure Distribution
  • Pressure Measurement
  • Short Takeoff Aircraft
  • Supersonic Aircraft
  • Turbulent Mixing

Fields of Study

  • Physics

Readers

  • Aerospace Engineering

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow
  • Space
  • Space - Hall-Effect Thruster