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Dynamic behavior of the gas turbine engine regenerator with complanar channels

  • Aircraft and Rocket Engine Theory
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Abstract

This paper expounds a technique for calculating unsteady gas temperatures, air and heat transfer elements of the corrugated plate of a recuperative heat exchanger with complanar channels for start and shut-off modes of the regenerative turbine engine. Under consideration are the distribution of thermal stresses in the plate, heat exchanger service life under stationary conditions, and the allowable number of dynamic “start–shut-off” cycles.

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References

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Authors and Affiliations

  1. Ufa State Aviation Technical University, ul. Karla Marksa 12, Ufa, 450008 Bashkortostan, Russia

    V.A. Trushin

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  1. V.A. Trushin
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Correspondence to V.A. Trushin.

Additional information

Original Russian Text© V.A. Trushin 2017, published in Izvestiya Vysshikh Uchebnykh Zavedenii. Aviatsionnaya Tekhnika, 2017, No. 2, pp. 136–140.

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Trushin, V. Dynamic behavior of the gas turbine engine regenerator with complanar channels. Russ. Aeronaut. 60, 312–316 (2017). https://doi.org/10.3103/S1068799817020246

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  • DOI: https://doi.org/10.3103/S1068799817020246

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