Numerical simulation of transonic flow over porous airfoils

Chung-Lung Chen, Chuen Yen Chow, Terry L. Holst, William R. Van Dalsem

研究成果: Paper同行評審

9 引文 斯高帕斯(Scopus)


A numerical study is made to examine the effect of a porous surface on transonic airfoil performance. By making the surface below a normal shock porous, a strong normal shock is replaced by a weakened shock preceded by an oblique shock at the upstream end of the porous surface, where air is blown out of the cavity into the supersonic outer flow. According to the present analysis, the result of this is that » porous airfoil has a smaller drag and higher lift than a solid airfoil. The present results are in good agreement with experimental pressure distributions and predict the observed lambda-shock structure.

出版狀態Published - 1 1月 1985
事件3rd Applied Aerodynamics Conference, 1985 - Colorado Springs, United States
持續時間: 14 10月 198516 10月 1985


Conference3rd Applied Aerodynamics Conference, 1985
國家/地區United States
城市Colorado Springs


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