Accession Number:

ADA951865

Title:

Interaction Region in the Boundary Layer of a Shock Tube.

Descriptive Note:

Scientific interim rept.,

Corporate Author:

CASE INST OF TECH CLEVELAND OHIO FLUID THERMAL AND AEROSPACE SCIENCES

Personal Author(s):

Report Date:

1967-06-01

Pagination or Media Count:

146.0

Abstract:

Subject Categories:

  • Numerical Mathematics
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE