Accession Number:

AD0657160

Title:

ROCKET TUNNEL GAS PROPERTIES,

Descriptive Note:

Corporate Author:

JOHNS HOPKINS UNIV SILVER SPRING MD APPLIED PHYSICS LAB

Personal Author(s):

Report Date:

1957-09-12

Pagination or Media Count:

20.0

Abstract:

An analysis was made of the specific heat, wind tunnel expansion processes, and shock wave properties of gas mixtures in a solid propellant rocket driven supersonic wind tunnel.

Subject Categories:

  • Aerodynamics
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE