Accession Number:

ADA007407

Title:

Experimental Study of Heat Transfer in a Critical Point of Sphere in Hypersonic Low-Density Flow,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1975-01-24

Pagination or Media Count:

16.0

Abstract:

In an experimental study of heat transfer at the critical point of a sphere the possibility is confirmed of using underexpanded nozzles in hypersonic wind tunnels for radiation of the flow about the models over a wide range of Reynolds numbers. Experiments were carried out in a hypersonic shock tube with numbers M 32.

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE