Accession Number:

ADA265275

Title:

Theoretical Investigation of 3-D Shock Wave - Turbulent Boundary Layer Interactions

Descriptive Note:

Interim rept. 1 Mar-30 Sep 92,

Corporate Author:

RUTGERS - THE STATE UNIV NEW BRUNSWICK NJ DEPT OF MECHANICAL AND AEROSPACE ENGINEERING

Personal Author(s):

Report Date:

1992-11-01

Pagination or Media Count:

59.0

Abstract:

The research concerns the understanding of 3-D shock waveturbulent boundary-layer interactions. The research effort during the current period focused on the following areas a the 3-D double fin crossing shock interaction at Mach 8.3 for symmetric 15 deg fins, 2 the 3-D crossing shock interaction at Mach 4 for symmetric 15 deg fins, and 3 the 3-D tripe triple shock interaction at Mach 8.3 for 10 deg fins

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE