Accession Number:

ADA043118

Title:

Thermo-Mechanical Stress Analysis of Advanced Turbine Blade Cooling Configuration.

Descriptive Note:

Interim scientific rept. 1 May 76-30 Jun 77,

Corporate Author:

KENTUCKY UNIV LEXINGTON DEPT OF ENGINEERING MECHANICS

Personal Author(s):

Report Date:

1977-07-01

Pagination or Media Count:

40.0

Abstract:

Program improvement features in a Boundary Integral Equation Analysis Capability for thermomechanical problems are described. A number of solved problems are presented along with a progress report on the research directed toward a thermomechanical stress analysis in the vicinity of a cooling hole in a film-cooled turbine blade. Author

Subject Categories:

  • Mechanics
  • Thermodynamics
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE