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