Computational fluid dynamics study of three-dimensional dynamic stall of various planform shapes

被引：0
|
作者：
Spentzos, A. [1 ,3 ]
Barakos, G.N. [1 ,3 ,4 ]
Badcock, K.J. [1 ,3 ]
Richards, B.E. [1 ,3 ]
Coton, F.N. [1 ,5 ]
Galbraith, R. A. McD [1 ,5 ]
Berton, E. [2 ]
Favier, D. [2 ]
机构：
[1] University of Glasgow, Glasgow, G12 8QQ, United Kingdom
[2] Laboratoire d'Aeárodynamique et de Biomeáchanique du Mouvement, 13288 Marseille Cedex 9, France
[3] CFD Laboratory, Department of Aerospace Engineering, United Kingdom
[4] Department of Engineering, University of Liverpool, Liverpool, L69 3GH, United Kingdom
[5] Low Speed Aerodynamics Group, Department of Aerospace Engineering
来源：
Journal of Aircraft | 1600年 / 44卷 / 04期
关键词：
Numerical simulation of 3-D dynamic stall has been undertaken using computational fluid dynamics. As a first step; validation calculations have been performed for cases in which experimental data were available. Although the amount and quality of the experimental data available for 3-D dynamic stall does not match what is available for 2-D cases; the computational fluid dynamics was found capable of predicting this complex 3-D flow with good accuracy. Once confidence on the computational fluid dynamics method was established; further calculations were conducted for several wing planforms. The calculations revealed the detailed structure of the 3-D dynamic stall vortex and its interaction with the tip vortex. Remarkably; strong similarities in the flow topology were identified for wings of very different planforms;
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摘要：
Conference article (CA)
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页码：1118 / 1128
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