Thermo-Mechanical Stress Analysis of Advanced Turbine Blade Cooling Configuration.
Interim scientific rept. 1 May 76-30 Jun 77,
KENTUCKY UNIV LEXINGTON DEPT OF ENGINEERING MECHANICS
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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
- Jet and Gas Turbine Engines