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

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)

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1977
Accession Number
ADA043118

Entities

People

  • D. J. Shippy
  • F. J. Rizzo

Organizations

  • University of Kentucky

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Computer Programs
  • Computers
  • Equations
  • Gas Turbines
  • Geometry
  • Heat Transfer
  • Integral Equations
  • Kernel Functions
  • Mechanics
  • Shape
  • Stress Analysis
  • Stress Concentration
  • Stresses
  • Three Dimensional
  • Turbine Blades
  • Turbines

Readers

  • Calculus or Mathematical Analysis
  • Combustion and Flow Dynamics.
  • Powder metallurgy of Titanium alloys.