Accession Number:

AD0783927

Title:

Solutions to the Direct Problem of Heat Transfer between a Cooled Turbine Blade and Gas using the Dispersion Method,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Report Date:

1974-07-24

Pagination or Media Count:

12.0

Abstract:

The dispersion method is used to solve a differential equation of the third order describing heat exchange between gas and a cooled turbine blade.

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE