Accession Number:

AD0869039

Title:

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

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH

Personal Author(s):

Report Date:

1970-03-11

Pagination or Media Count:

12.0

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

Subject Categories:

  • Test Facilities, Equipment and Methods
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE