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Calculation of low cycle fatigue life for gas-turbine engine critical parts

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Abstract

The paper presents a technique of calculating the life for gas turbine engine parts in a low cycle area based on the influence coefficients taking into account analytical and operational factors. A statistical method is used to determine the influence coefficients.

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Correspondence to S. A. Bukatyi.

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Original Russian Text© A.V. Pakhomenkov, R.A. Azimov, S.A. Bykatyi, 2017, published in Izvestiya Vysshikh Uchebnykh Zavedenii. Aviatsionnaya Tekhnika, 2017, No. 3, pp. 95–100.

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Pakhomenkov, A.V., Azimov, R.A. & Bukatyi, S.A. Calculation of low cycle fatigue life for gas-turbine engine critical parts. Russ. Aeronaut. 60, 421–427 (2017). https://doi.org/10.3103/S106879981703014X

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  • DOI: https://doi.org/10.3103/S106879981703014X

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