AXIALLY SYMMETRIC, INVISCID, REAL GAS, NON-ISOENERGETIC FLOW SOLUTION BY THE METHOD OF CHARACTERISTICS

Abstract

A numerical procedure is presented for the solution of the characteristic equations for a non-isoenergetic, supersonic, real gas jet expanding into a constant pressure ambience. Included is a procedure for inserting the expansion fan and the embedded shock. Examples are given for high temperature argon jets with radiation.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1970
Accession Number
AD0699199

Entities

People

  • John H. Fox

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Abstracts
  • Air Force
  • Boundaries
  • Computer Programs
  • Computers
  • Contracts
  • Dissipation
  • Engineering
  • Equations
  • Flow
  • Flow Fields
  • High Temperature
  • Mach Number
  • Method Of Characteristics
  • Pressure Distribution
  • Radiation
  • Radiation Effects

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow