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

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.

Document Details

Document Type
Technical Report
Publication Date
Dec 02, 1969
Accession Number
AD0701978

Entities

People

  • K. V. Kholshchevnikov

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircraft Engines
  • Aircrafts
  • Centrifugal Compressors
  • Compressors
  • Engines
  • Gas Turbines
  • Jet Aircraft
  • Turbines
  • Turbojet Engines

Fields of Study

  • Engineering
  • Physics

Readers

  • Aerodynamics.
  • Aerospace Engineering