IMECH-IR  > 力学所知识产出(1956-2008)
Adaptive optimal control of the incompressible flow around an airfoil with smart surface
Wu CJ; Wang L; Wu, CJ (reprint author), Chinese Acad Sci, LNM, Inst Mech, Beijing 100080, Peoples R China.
会议录名称RECENT ADVANCES IN FLUID MECHANICS
2004
会议名称4th International Conference on Fluid Mechanics
会议日期JUL 20-30, 2004
会议地点Dalian, PEOPLES R CHINA
摘要In this paper, using the moving boundary CFD method, we developed a new real-time optimal control method which can adaptively change the shapes of body surface to obtain the unsteady optimal airfoil. The results show that the aerodynamics properties of airfoil with the new method can be improved remarkably, and the aerodynamics characteristics of the final optimal airfoil at different angles of attack are all superior than the original airfoil NACA0012.
WOS记录号WOS:000225709300161
ISBN号7-302-08817-9
收录类别CPCI-S
语种英语
引用统计
文献类型会议论文
条目标识符http://dspace.imech.ac.cn/handle/311007/58921
专题力学所知识产出(1956-2008)
通讯作者Wu, CJ (reprint author), Chinese Acad Sci, LNM, Inst Mech, Beijing 100080, Peoples R China.
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GB/T 7714
Wu CJ,Wang L,Wu, CJ . Adaptive optimal control of the incompressible flow around an airfoil with smart surface[C]RECENT ADVANCES IN FLUID MECHANICS,2004.
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