TABLES OF SOME SUPERSONIC GAS FLOW FUNCTIONS.

Abstract

Tables were prepared of some supersonic gas flow functions in the Mach number range of 1 to 10 for a gamma ranging from 1.05 to 1.6. (Author)

Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1968
Accession Number
AD0685452

Entities

People

  • Rebecca L. Walton

Organizations

  • Royal Aircraft Establishment

Tags

DTIC Thesaurus Topics

  • Flow
  • Fluid Flow
  • Gas Flow
  • Mach Number

Fields of Study

  • Physics

Technology Areas

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