THERMAL STRESSES IN GAS TURBINE NOZZLE BLADES UNDER TRANSIENT THERMAL CONDITIONS

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) Edited machine trans....

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Bibliographic Details
Main Authors: Kuriat,R. I, Miroshnichenko,Yu. D
Format: Report
Language:English
Subjects:
COOLING
GAS TURBINE BLADES
GAS TURBINE NOZZLES
Jet and Gas Turbine Engines
NUMERICAL ANALYSIS
THERMAL STRESSES
TRANSLATIONS
USSR
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Summary: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) Edited machine trans. of Energomashinostroenie (USSR) v12 n10 p30-32 1966.