再突入物体背面への輻射熱伝達の推算

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書誌事項

タイトル別名
  • Evaluation of radiative heat transfer on the back surface of reentry body

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抄録

The convective and radiative heat transfer rates are calculated over a super-orbital-velocity reentry body which resembles the MUSES-C reentry capsule at an altitude 60 km and at a flight speed 12 km/sec. Thermally and chemically nonequilibrium 11-species air is considered, using the Park two-temperature model and the Yos formula for transport coefficients. Chemical species number densities and temperature distributions are obtained, solving Navier-Stokes equations and the vibrational-electronic energy conservation equation, where a Harten-Yee-type second-order upwind TVD scheme is used.

資料番号: AA0047427018

レポート番号: JAXA-SP-03-002

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詳細情報 詳細情報について

  • CRID
    1050292561218527616
  • NII論文ID
    120006829767
  • NII書誌ID
    AA11984031
  • ISSN
    1349113X
  • Web Site
    http://id.nii.ac.jp/1696/00006613/
  • 本文言語コード
    ja
  • 資料種別
    conference paper
  • データソース種別
    • IRDB
    • CiNii Articles

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