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

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)

Document Details

Document Type
Technical Report
Publication Date
Mar 11, 1970
Accession Number
AD0869039

Entities

People

  • Walerian Kordzinski

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Altitude
  • Engines
  • Gas Turbine Regenerators
  • Gas Turbines
  • High Altitude
  • Jet Engines
  • Simulations
  • Test Stands
  • Turbine Components
  • Turbines
  • Turbojet Engines
  • Turboprop Engines

Fields of Study

  • Engineering
  • Physics

Readers

  • Aerospace Engineering