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JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A  2013, Vol. 39 Issue (3): 320-324    DOI:
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Wing geometric twist design method based on lifting-line theory
Qiao Yuhang1, Ma Dongli1, Deng Xiaogang2
1. School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;
2. State Key Laboratory of Aerodynamics, China Aerodynamics Research & Development Center, Mianyang 621000, China
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