Accession Number : AD0869039

Title :   On the Possibilities of Simulating the Flight Operating Conditions of Turbine Engines on a Test Stand,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH

Personal Author(s) : Kordzinski, Walerian

Report Date : 11 MAR 1970

Pagination or Media Count : 12

Abstract : A discussion is presented of the possibilities for test-stand simulation of arbitrary in-flight operating conditions for single-shaft turbojet engines, single- and twin-spool engines with a two- stage compressor, and turboprop engines with and without a free turbine. Test-stand simulation of high-altitude conditions for engine start and acceleration regimes is examined. (Author)

Descriptors :   (*GAS TURBINES, TEST METHODS), SIMULATION, TURBOJET ENGINES, TURBOPROP ENGINES, ENVIRONMENTAL TESTS, HIGH ALTITUDE, STARTING, ACCELERATION, CAPTIVE TESTS, POLAND.

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

Distribution Statement : APPROVED FOR PUBLIC RELEASE