Inverse Design of a Thick Supercritical Airfoil.

• PAMBAGJO Tjoetjoek Eko

  Department of Aeronautics and Space Engineering, Tohoku University

• NAKAHASHI Kazuhiro

  Department of Aeronautics and Space Engineering, Tohoku University

• OBAYASHI Shigeru

  Department of Aeronautics and Space Engineering, Tohoku University

抄録

In this paper, a study on designing a thick supercritical airfoil by utilizing Takanashi’s inverse design method is discussed. One of the problems to design a thick supercritical airfoil by Takanashi’s method is that an oscillation of the geometry may occur during the iteration process. To reduce the oscillation, an airfoil parameterization method is utilized as the smoothing procedure. A guideline to determine the target pressure distribution to realize the thick airfoil is also discussed.

収録刊行物

• TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

  TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 43 (140), 61-66, 2000

  一般社団法人 日本航空宇宙学会

キーワード

• Inverse Design
• Supercritical Airfoil

詳細情報

• CRID: 1390282679055408128
• NII論文ID: 10004532937
• NII書誌ID: AA0086707X
• DOI: 10.2322/tjsass.43.61
• ISSN: 21894205
• ISSN: 05493811
• NDL書誌ID: 5485796
• Web Site: https://ndlsearch.ndl.go.jp/books/R000000004-I5485796
• Web Site: https://www.jstage.jst.go.jp/article/tjsass/43/140/43_140_61/_pdf
• 本文言語コード: en
• データソース種別:
  • JaLC
  • NDL
  • Crossref
  • CiNii Articles
• 抄録ライセンスフラグ: 使用不可