Accession Number : AD0681618

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

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Kuriat,R. I. ; Miroshnichenko,Yu. D.

Report Date : 25 JUN 1968

Pagination or Media Count : 14

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)

Descriptors :   (*GAS TURBINE BLADES, THERMAL STRESSES), GAS TURBINE NOZZLES, COOLING, NUMERICAL ANALYSIS, USSR

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE