Accession Number : AD0701978

Title :   MATCHING OF COMPRESSORS AND TURBINE PARAMETERS IN GAS TURBINE AIRCRAFT ENGINES,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Kholshchevnikov,K. V.

Report Date : 02 DEC 1969

Pagination or Media Count : 205

Abstract : Contents: Turbojet engine with a single-spool axial compressor; Turbojet engine with a axial twin-spool compressor; Turbojet engine with centrifugal compressor; Bypass turbojet engine; The turbo-prop engine; and Closed-circuit gas-turbine plants.

Descriptors :   (*GAS TURBINES, *AIRCRAFT ENGINES), (*TURBOJET ENGINES, *AXIAL FLOW COMPRESSORS), CORRELATION TECHNIQUES, EFFICIENCY, STRESSES, USSR

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE