Accession Number:

AD0780337

Title:

Experimental Investigation of a Turbulent Boundary Layer on a Greatly Elongated Body of Revolution in a Supersonic Flow,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• Kovalenko,V. M.
• Nesterovich,N. I.
• Shulemovich,V. M.

Report Date:

1974-05-24

Pagination or Media Count:

12.0

Abstract:

Descriptors:

• *Sounding rockets
• *Turbulent boundary layer
• Supersonic flow
• Bodies of revolution
• Wind tunnel models
• Translations
• USSR

Subject Categories:

• Rockets
• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE