ヘリコプタ形態へのCFD解析の適用

書誌事項

タイトル別名
  • CFD application to helicopter configuration

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抄録

The in-house rotor CFD code has been further developed to apply for aerodynamic issues on realistic helicopter configuration. The code solves the unsteady Euler equations for flowfield around helicopter in forward flight with rotor blades in cyclic motions. A preliminary result for the case of analysis on rotor-fuselage aerodynamic interaction is shown and the feasibility of the present code has been demonstrated.

資料番号: AA0045948053

レポート番号: NAL SP-57

収録刊行物

詳細情報 詳細情報について

  • CRID
    1050574036209471616
  • NII論文ID
    120006838978
  • NII書誌ID
    AN10097345
  • ISSN
    0289260X
  • Web Site
    http://id.nii.ac.jp/1696/00038268/
  • 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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