Accession Number:

AD0713041

Title:

STAND FOR TESTING A GAS-TURBINE ENGINE,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Report Date:

1970-08-08

Pagination or Media Count:

4.0

Abstract:

The proposed stand differs from those known in that the line contains a gas-intake duct with a baffle plate to select a portion of the hot gas, which permits regulation of the flow parameters at the inlet to the tested engine. Author

Subject Categories:

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

Distribution Statement:

APPROVED FOR PUBLIC RELEASE