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Calculation of heat conduction in aerospace plane thermal protection system

  • Flight Vehicle Design
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Abstract

In this paper, a technique is proposed for calculating the heat conduction of heatprotection tiles in aerospace planes by using as a base the now-existing algorithms to analyze the composite material characteristics as well as thermoforce analogy. The efficiency of this technique is confirmed by the numerical calculation.

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References

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Author information

Authors and Affiliations

  1. Nanjing University of Aeronautics and Astronautics, Nanjing, China

    Zhijin Wang & Hong Ye

  2. Tupolev Kazan National Research Technical University, Kazan, Russia

    A. S. Kretov

Authors
  1. Zhijin Wang
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  2. Hong Ye
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  3. A. S. Kretov
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Additional information

Original Russian Text © Wang Zhijin, Hong, A.S. Kretov, 2013, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2013, No. 3, pp. 3–6.

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Wang, Z., Ye, H. & Kretov, A.S. Calculation of heat conduction in aerospace plane thermal protection system. Russ. Aeronaut. 56, 213–218 (2013). https://doi.org/10.3103/S106879981303001X

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  • DOI: https://doi.org/10.3103/S106879981303001X

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