低レイノルズ数条件下での改良型石井翼型の流体計算と性能評価

機関リポジトリ

書誌事項

タイトル別名
  • Numerical flow simulations around an improved Ishii airfoil under low Reynolds number flow conditions

説明

第49回流体力学講演会/第35回航空宇宙数値シミュレーション技術シンポジウム (2017年6月28日-30日. 国立オリンピック記念青少年総合センター), 渋谷区, 東京

49th Fluid Dynamics Conference /the 35th Aerospace Numerical Simulation Symposium (June 28-30, 2017. National Olympics Memorial Youth Center), Shibuya-ku, Tokyo, Japan

This paper conducts two-dimensional numerical flow simulations around an improved Ishii airfoil under low Reynolds number flow conditions. The improved Ishii airfoil is proposed in previous efforts and demonstrated better aerodynamic performance in comparison with those of an original Ishii airfoil. At first, numerical results in the cases of angles of attack ranging from -6 degrees to 9 degrees and a chord-based Reynolds number of 20,000 are compared with the experimental data. Results show a fair agreement with the experimental data. Then, Reynolds number effects are studied for the angles of attack at 3 degrees and 6 degrees, respectively. Numerical results present similar trend to that observed in the experiments. Furthermore, it seems that the change of Reynolds number has certain impact on the aerodynamic coefficients when the laminar separation bubble is not observed over the airfoil.

形態: カラー図版あり

Physical characteristics: Original contains color illustrations

資料番号: AA1730011018

レポート番号: JAXA-SP-17-004

収録刊行物

詳細情報 詳細情報について

  • CRID
    1050855511216214912
  • NII論文ID
    120006827418
  • ISSN
    24332232
  • Web Site
    http://id.nii.ac.jp/1696/00003246/
  • 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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