Influence of Aspect Ratio on Dynamic Stall of a Finite Wing
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چکیده
منابع مشابه
Flutter Analysis of a Low Aspect Ratio Swept- Back Trapezoidal Wing at Low Subsonic Flow
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ژورنال
عنوان ژورنال: AIAA Journal
سال: 2019
ISSN: 0001-1452,1533-385X
DOI: 10.2514/1.j057792