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浸入边界/大涡模拟混合方法模拟翼型绕流的转捩问题
杨晓雷; 何国威; 张星
Source Publication中国力学学会学术大会'2009论文摘要集.中国力学学会,2009,p.262
2009-08-24
Pages262
Conference Name中国力学学会学术大会'2009
Conference Date2009-08-24
Conference Place中国河南郑州
Abstract<正>以雷诺数Re=60000静止翼型SD7003和扑动翼型SD7003绕流为例,验证结合浸入边界和大涡模拟的混合方法模拟流动转捩的能力。对于静止翼型绕流算例,结合浸入边界和大涡模拟的混合方法可以很好地预测转捩点以及再附点。对于扑动翼型绕流的算例,目前方法给出
Keyword浸入边界方法 大涡模拟 流动转捩
Funding Organization中科院创新项目(KJCX-SW-L08) ; 中科院创新项目(KJCX3-SYW-S01) ; 973项目(2007CB814800) ; 自然科学基金项目(10628206,10732090,10872201)资助
Language中文
Document Type会议论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/43079
Collection非线性力学国家重点实验室
Corresponding Author杨晓雷
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杨晓雷,何国威,张星. 浸入边界/大涡模拟混合方法模拟翼型绕流的转捩问题[C]中国力学学会学术大会'2009论文摘要集.中国力学学会,2009,p.262,2009:262.
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