AN IBM 7090 PROGRAM FOR COMPUTING TWO-DIMENSION AL AND AXIALLY-SYMMETRIC SUPERSONIC FLOW OF AN IDEAL GAS

Abstract

An IBM 7090 electronic computer program is given, by which it is possible to compute the axially-symmetric or two-dimensional Mach net for supersonic flows over pointed bodies with attached shocks, through channels consisting of two rigid walls, and through nozzles with an axis of symmetry. The computation of flows with free streamline boundaries is also possible, if no shocks occur within the flow.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1962
Accession Number
AD0404715

Entities

People

  • F. E. Ehlers

Organizations

  • Boeing

Tags

Communities of Interest

  • C4I

DTIC Thesaurus Topics

  • Computations
  • Computer Programming
  • Computer Programs
  • Computers
  • Digital Computers
  • Equations
  • Flow
  • Free Stream
  • Instructions
  • Mach Number
  • Method Of Characteristics
  • Nozzles
  • Procedures (Computers)
  • Scientific Research
  • Shock Waves
  • Supersonic Flow
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Calculus or Mathematical Analysis
  • Computer Science.
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Microelectronics