Analysis of Three-Dimensional Inviscid Supersonic Flow Between a Body and an Outer Wall (with Application to a Jet Stretcher System)

Abstract

The three-dimensional inviscid supersonic flow equations are solved for the flow over a body located within a duct. Numerical solutions are obtained by use of the reference plane method of characteristics technique. Results of the analysis are compared with experimental test body pressure distributions obtained with an off-design jet stretcher system. The analysis is sufficiently general so that a variety of internal flows may be predicted. A computer program listing and an example problem are presented.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1976
Accession Number
ADA029123

Entities

People

  • R. C. Bauer
  • W. C. Armstrong

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Computer Programs
  • Computers
  • Cooperation
  • Equations
  • Flow
  • Mathematics
  • Method Of Characteristics
  • Pressure Distribution
  • Stretchers
  • Supersonic Flow
  • Three Dimensional

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow