Aerodynamic optimization of supersonic transport wing using unstructured adjoint method

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作者
Kim, H.-J. [1 ]
Sasaki, D. [1 ]
Obayashi, S. [1 ]
Nakahashi, K. [1 ]
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[1] Turbomachinery Research Department, Korea Aerospace Research Institute, Taejun 305-600, Korea, Republic of
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| 1600年 / American Inst. Aeronautics and Astronautics Inc.卷 / 39期
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25
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