Accession Number:

AD0402588

Title:

CALCULATING THERMAL BOUNDARY LAYER IN A FLOW OF COMPRESSIBLE GAS

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH

Personal Author(s):

Report Date:

1963-04-03

Pagination or Media Count:

13.0

Abstract:

Discussion of method for calculating laminary, transient and turbulent zones of thermal boundary layer when a flow of compressible gas is directed around a surface translation of Russian article.

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE