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Inverse heat transfer problem solution of sounding rocket using moving window optimization

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  • Adam Dąbrowski
  • Leszek Dąbrowski

Abstract

An Inverse Heat Transfer Problem is solved for a sounding rocket module given its geometry and measured temperature profile. The solution is obtained via moving window optimization, a technique for solving inverse dynamics. An analysis is performed to modify the method to avoid oscillatory behavior of the resulting heat flux profile. The method parameters are tuned in relation to characteristic phases of the flight. Results are presented and correlated with measured flight data. Conclusions are drawn for better experiments for measuring heat flux on a sounding rocket skin.

Suggested Citation

  • Adam Dąbrowski & Leszek Dąbrowski, 2019. "Inverse heat transfer problem solution of sounding rocket using moving window optimization," PLOS ONE, Public Library of Science, vol. 14(6), pages 1-24, June.
    • Handle: RePEc:plo:pone00:0218600
    DOI: 10.1371/journal.pone.0218600
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