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Aerodynamic optimization of supersonic wing-nacelle configuration using an adjoint method with the unstructured-grid approach

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Kim, Hyoung-Jin, 大林, 茂, 中橋, 和博, Obayashi, Shigeru, Nakahashi, Kazuhiro航空宇宙技術研究所2000-12航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory49Tp.121-129

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Subject Heading...shape function elliptic equation method sequential quadratic programm...
Note (General)...ation, and the elliptic equation method is employed for the interior ...

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