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

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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.

Author(s):
Kholshchevnikov, K. V.
Author Organization(s):
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Supplementary Note:
Edited trans. of mono. Soglasovanie Parametrov Kompressora i Turbiny v Aviatsionnykh Gazoturbinnykh Dvigatelyakh, Moscow, 1965 p1-200.
Annotation:
Matching of compressors and turbine parameters in gas turbine aircraft engines--Translation.
Pagination:
0205

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
FTD-HT-23-637-68
Project Number(s):
FTD-7230178
 Subject Terms
Communities of Interest:
Air Platforms
Descriptor(s):
(*GAS TURBINES, *AIRCRAFT ENGINES), (*TURBOJET ENGINES, *AXIAL FLOW COMPRESSORS), CORRELATION TECHNIQUES, EFFICIENCY, STRESSES, USSR
Field(s)/Group(s):
Jet and Gas Turbine Engines
Keyword(s):
TRANSLATIONS
Report Date:
1969 Dec 02