Accession Number : AD0764930

Title :   Methods of Thermal-Strength Testing of the Nozzle Units of Turbines of Aviation GTE,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Grigorev,P. F. ; Meshcheryakov,M. P.

Report Date : 30 JUL 1973

Pagination or Media Count : 9

Abstract : The report describes the dynamic response of gas turbine parts exposed to repetitive high temperatures.

Descriptors :   (*GAS TURBINE NOZZLES, THERMAL ANALYSIS), TURBINE BLADES, THERMAL STRESSES, FATIGUE(MECHANICS), CRACKS, BUCKLING, USSR

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE