Accession Number:

ADA046666

Title:

Heat Exchange in Cooled Flow Area of the Turbine,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Report Date:

1977-05-20

Pagination or Media Count:

30.0

Abstract:

In the investigated range of a change of the parameters mu characteristic for turbines of GTD, the intensity of heat exchange in air-cooled blades, measured during tests at static installations and in turbine stages under conditions of rotation, remains constant. The experimental data, obtained at static installations, can be common for work conditions of blades under turbines, which substantially simplifies the procedure of experiment and the construction of test benches.

Subject Categories:

  • Thermodynamics
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE