Inverse Design of a Thick Supercritical Airfoil

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概要

• 論文の詳細を見る

• 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.

• 社団法人 日本航空宇宙学会の論文
• 2000-08-04

著者

• NAKAHASHI Kazuhiro

  Department of Aeronautics and Space Engineering, Tohoku University

• Pambagjo T

  Tohoku Univ. Sendai Jpn

• Pambagjo Tjoetjoek

  Department Of Aeronautics And Space Engineering Tohoku University

• OBAYASHI Shigeru

  Department of Aeronautics and Space Engineering,Tohoku University

• Nakahashi Kazuhiro

  Department Of Aeronautics And Space Engineering Tohoku University

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