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Stall Mitigation and Lift Enhancement of NACA 0012 with Triangle-Shaped Surface Protrusion at a Reynolds Number of 105

IF 0.3 Q4 ENGINEERING, AEROSPACE
SAE International Journal of Aerospace Pub Date : 2019-11-21 DOI:10.4271/01-12-02-0007
A. Bodavula, R. Yadav, U. Guven
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引用次数: 3
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雷诺数为105时具有三角形表面突起的NACA 0012的失速缓解和升力增强
本文章由计算机程序翻译，如有差异，请以英文原文为准。
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来源期刊
SAE International Journal of Aerospace
SAE International Journal of Aerospace ENGINEERING, AEROSPACE-
CiteScore
0.70
自引率
0.00%
发文量
22
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