%0 Journal Article
%T THE TRAILING-EDGE VORTEX STRUCTURE OF A CONSTANT-RATE AIRFOIL AND MECHANISM OF DYNAMIC STALL<br>等速上仰翼型尾部流动观察及动态失速机理探讨
%A Sun Mao Wang Jialu Lian Qixiang
%A <br>孙茂
%A 王家禄
%A 连淇祥
%J 力学学报
%D 1993
%I 
%X The vortex structure shed from the trailing-dege of a constant-rate pitching airfoil was visualized using hydrogen bubble technique. Its time evolution, and the effects of pitching rate were studied. Combining the trailing-dege vortex structure with the (previously obtained) airfoil upper-surface separated vortex structure, a complete flow structure was obtained. The mechanism of dynamic stall was studied based on the flow structure and vorticity dynamics theory, and insights were provided.
%K pitching airfoil
%K trailing-edge shed vortex
%K dynamic stall<br>上仰翼型
%K 尾涡层
%K 动态失速
%U http://www.alljournals.cn/get_abstract_url.aspx?pcid=6E709DC38FA1D09A4B578DD0906875B5B44D4D294832BB8E&cid=5D344E2AD54D14F8&jid=4100DA4A1A3BA1B0CE5AD99AE1DFB420&aid=6F9821D61B201FA282958E5554FA98B6&yid=D418FDC97F7C2EBA&vid=C5154311167311FE&iid=94C357A881DFC066&sid=3EABEBD973E45554&eid=250DF325A002B9CC&journal_id=0459-1879&journal_name=力学学报&referenced_num=0&reference_num=3