Thermostressed state in turbine rotor blades with thermal barrier coating at transient conditions of air breathing jet engine operation |
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| Authors: | V A Trushin |
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| Institution: | 1. Ufa State Aviation Technical University, Ufa, Russia
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| Abstract: | The finite-difference method acceptable for on-board computers is applied to analyze the thermo-stressed state for the thermal-barrier coating of a perforated turbine blade and its wall at transient and stationary conditions of air-breathing jet engine operation during a flight. |
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