Accession Number:

AD0262842

Title:

Mach Tables for Real Gas Equilibrium Flow of Air In Hypervelocity Test Facilities with Total Temperatures to 10,000 deg K

Descriptive Note:

Corporate Author:

SANDIA CORP ALBUQUERQUE NM

Personal Author(s):

Report Date:

1961-03-01

Pagination or Media Count:

82.0

Abstract:

Aerodynamic flow parameters for isentropic expansions and flow through normal shocks, including real gas effects, have been calculated for total temperatures of 4000 to 10,000 deg K and for total pressures of 100 to 4000 atmospheres. Calculations assume equilibrium flow. Results indicate real gas effects vary from a few percent to more than two orders of magnitude.

Subject Categories:

  • Aerodynamics
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE