Multi-objective aerodynamic optimization of supercritical wing with substantial pressure constraints - 飞机研究与设计实验室(AEROlab) | LabXing

array(2) { ["lab"]=> string(2) "67" ["publication"]=> string(3) "863" } Multi-objective aerodynamic optimization of supercritical wing with substantial pressure constraints - 飞机研究与设计实验室(AEROlab) | LabXing

飞机研究与设计实验室(AEROlab)

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Multi-objective aerodynamic optimization of supercritical wing with substantial pressure constraints

2015

会议 53rd AIAA Aerospace Sciences Meeting

作者 Zhao Tong · Yufei Zhang · Haixin Chen

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American Institute of Aeronautics and Astronautics
ISBN: 9781624103438
DOI: 10.2514/6.2015-0763

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