Turbine blades durability forecast by method of assemblies equivalent tests

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Method of program formation and methodology for equivalent tests of turbine blades under laboratory conditions are proposed. The program and equivalent test results of turbine stage 1 blade for one of a hightemperature g aircraft gas turbine engine are given.

Equivalent tests, loading cycle, thermocyclic durability, multi - factor non - isothermal loading

Короткий адрес: https://sciup.org/148200504

IDR: 148200504

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