TOWARD THE CALCULATION OF TEMPERATURE STRESS IN COOLED BLADE OF A GAS TURBINE,

Abstract

In the article a formula is derived for calculation of stresses caused by temperature drop through the thickness of the wall of a blade of arbitrary profile with internal cooling. (Author)

Document Details

Document Type
Technical Report
Publication Date
Mar 05, 1964
Accession Number
AD0602567

Entities

People

  • V. I. Rozenblyum

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Energy Generators
  • Energy Systems
  • Engines
  • Gas Turbines
  • Generators
  • Geometry
  • Heat Engines
  • Heat Transfer Devices
  • Internal Combustion Engines
  • Mathematics
  • Mechanical Equipment
  • Thickness
  • Turbines

Fields of Study

  • Engineering
  • Physics

Readers

  • Aerodynamics.
  • Combustion and Flow Dynamics.
  • Structural Dynamics.