Accession Number:

AD0780376

Title:

Characteristics of Diffusers in Shock Tube,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• Anufriev,V. M.
• Kozlov,G. I.
• Roitenburg,D. K.

Report Date:

1974-04-23

Pagination or Media Count:

14.0

Abstract:

A study was done on diffuser starting in a shock tube at M8 at variable Re numbers, and the throttling characteristics were recorded.

Descriptors:

• *Diffusers
• Shock tubes
• Gas flow
• Nozzle area ratio
• Translations
• USSR

Subject Categories:

• Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE