THERMAL STRESSES IN GAS TURBINE NOZZLE BLADES UNDER TRANSIENT THERMAL CONDITIONS,

Abstract

Results are given of rough estimate of thermal stresses appearing in gas turbine nozzle blades (solid and hollow cooled) during tests under conditions close to real. Calculations were produced on the BESM-2M computer. Deformation of blade elements was assumed elastic. (Author)

Document Details

• Document Type: Technical Report
• Publication Date: Jun 25, 1968
• Accession Number: AD0681618

Entities

People

• R. I. Kuriat.
• Yu. D. Miroshnichenko

Organizations

• National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

• Computers
• Energy Generators
• Energy Systems
• Gas Turbine Nozzles
• Gas Turbines
• Generators
• Mechanical Equipment
• Nozzles
• Stresses
• Thermal Stresses
• Turbine Components
• Turbines
• Turbomachinery

Fields of Study

• Physics

Readers

• Aerodynamics.
• Fluid Dynamics.
• Structural Dynamics.