Accession Number:

AD0630849

Title:

HEAT TRANSFER TO THE SURFACE OF GAS TURBINE BLADES,

Descriptive Note:

Corporate Author:

ARMY FOREIGN SCIENCE AND TECHNOLOGY CENTER WASHINGTON D C

Personal Author(s):

Report Date:

1966-02-01

Pagination or Media Count:

15.0

Abstract:

The article studies heat transfer to the surface of gas turbine blades on the basis of experimental data for a nonstationary blade temperature field obtained by the authors during experimental investigation of various transient regimes of an operating gas turbine engine. According to the authors the literature hitherto contained no data on the coefficients of heat transfer to blades under actual gas-turbine operating conditions. Author

Subject Categories:

  • Thermodynamics
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE