Accession Number : AD0759234

Title :   Stand for High-Altitude Velocity Tests of Units and External Systems of Gas-Turbine Engines,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Dzheneev,E. A. ; Martynov,N. V. ; Perstnev,P. V. ; Sutyrina,T. M.

Report Date : 04 APR 1973

Pagination or Media Count : 6

Abstract : The report discusses the design of a gas turbine engine test stand whereby altitude flight may be simulated.

Descriptors :   (*TEST FACILITIES, *GAS TURBINES), EXHAUST DIFFUSERS, MANIFOLDS(ENGINES), EXHAUST NOZZLES, CAPTIVE TESTS, PATENTS, USSR

Subject Categories : Test Facilities, Equipment and Methods
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE