Accession Number:

AD0640517

Title:

TABLES OF SOME SUPERSONIC FLOW FUNCTIONS FOR PROPANE.

Descriptive Note:

Technical rept.,

Corporate Author:

ROYAL AIRCRAFT ESTABLISHMENT FARNBOROUGH (UNITED KINGDOM)

Personal Author(s):

Report Date:

1966-06-01

Pagination or Media Count:

33.0

Abstract:

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

Subject Categories:

  • Fluid Mechanics
  • Fuels

Distribution Statement:

APPROVED FOR PUBLIC RELEASE