Accession Number : AD0780376

Title :   Characteristics of Diffusers in Shock Tube,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Anufriev,V. M. ; Kozlov,G. I. ; Roitenburg,D. K.

Report Date : 23 APR 1974

Pagination or Media Count : 14

Abstract : A study was done on diffuser starting in a shock tube at M=8 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