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Analysis of nonstationary heating and cooling of a thermomagnetic engine gadolinium working element

  • Aircraft and Rocket Engine Design and Development
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Abstract

The paper presents the results of calculating nonstatitionary heat exchange between a heattransfer agent (water) and a gadolinium working element of the thermomagnetic engine with the use of ANSYS 13.0 certified software. Recommendations for designing the thermomagnetic engine working elements are given based on the analysis of calculation results.

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Authors and Affiliations

  1. Moscow Aviation Institute (State Technical University), Moscow, Russia

    D. A. Gabrielyan & V. V. Semenov

  2. OAO NPO Energomash named after Academician V.P. Glushko, Moscow, Russia

    D. S. Martirosov

Authors
  1. D. A. Gabrielyan
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  2. V. V. Semenov
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  3. D. S. Martirosov
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Additional information

Original Russian Text © D.A. Gabrielyan, V.V. Semenov, D.S. Martirosov, 2013, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2013, No. 3, pp. 40–45.

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Gabrielyan, D.A., Semenov, V.V. & Martirosov, D.S. Analysis of nonstationary heating and cooling of a thermomagnetic engine gadolinium working element. Russ. Aeronaut. 56, 266–273 (2013). https://doi.org/10.3103/S1068799813030082

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  • DOI: https://doi.org/10.3103/S1068799813030082

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