Anomalous Heating Profile over Entry Capsule with Ablation and Its Relation to Earlier Turbulent Transition

この論文をさがす

説明

Effect of earlier turbulent transition and enhancement of turbulence intensity in the boundary layer due to ablation product gas is discussed in terms of anomalous heating profile over the surface of an entry capsule. First, a numerical approach that utilizes Park's injection induced turbulence model is described and some of the numerical results for code validation study are shown. Second, calculated results of trajectory-based aerodynamic heating environment for Pioneer-Venus entry capsules are shown. Finally, a numerical prediction of trajectory-based aerodynamic heating environment for MUSES-C is made and the possible effect of earlier turbulent transition is discussed.

資料番号: SA0200019000

収録刊行物

詳細情報 詳細情報について

  • CRID
    1050848249892145664
  • NII論文ID
    120006834551
  • NII書誌ID
    AA10455137
  • ISSN
    0288433X
  • Web Site
    http://id.nii.ac.jp/1696/00033240/
  • 本文言語コード
    en
  • 資料種別
    departmental bulletin paper
  • データソース種別
    • IRDB
    • CiNii Articles

問題の指摘

ページトップへ