TABLES OF SOME SUPERSONIC FLOW FUNCTIONS FOR PROPANE.

Abstract

Tables are presented of some supersonic flow functions for propane (Gamma = 1.13) in the Mach number range 1 - 10. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1966
Accession Number
AD0640517

Entities

People

  • I. D. Elliott

Organizations

  • Royal Aircraft Establishment

Tags

DTIC Thesaurus Topics

  • Flow
  • Fluid Flow
  • Mach Number
  • Supersonic Flow

Fields of Study

  • Physics

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow