IMECH-IR  > 力学所知识产出(1956-2008)
跨音速翼型上的激波/边界层干扰自适应控制计算
马侠; 蒋金贵; 张绵纯; 肖林奎
Source Publication应用力学学报
1994-03-30
Issue01Pages:60-65+122
ISSN1000-4939
Abstract在激波区使用自适应壁对跨音速翼型上的激波/边界层的相互作用(干扰)进行控制;可改变机翼的气动性能。这种被动控制可通过在翼型的激波区开一凹腔;其上覆盖一弹性橡胶膜柔壁来实现。本文给出用Navier-Stokes(N-S)方程数值模拟这一自适应控制翼型的跨音速粘性绕流;提出了一个适用于本特殊情况(物面边界局部地区在求解过程中有变化)的处理办法。并探讨了自适应柔壁对当代跨音速翼型绕流的影响。
Keyword激波/边界层干扰 被动控制 翼型 跨音速流
Indexed ByEI ; CSCD
Language中文
CSCD IDCSCD:251807
Citation statistics
Cited Times:1[CSCD]   [CSCD Record]
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/72333
Collection力学所知识产出(1956-2008)
Recommended Citation
GB/T 7714
马侠,蒋金贵,张绵纯,等. 跨音速翼型上的激波/边界层干扰自适应控制计算[J]. 应用力学学报,1994(01):60-65+122.
APA 马侠,蒋金贵,张绵纯,&肖林奎.(1994).跨音速翼型上的激波/边界层干扰自适应控制计算.应用力学学报(01),60-65+122.
MLA 马侠,et al."跨音速翼型上的激波/边界层干扰自适应控制计算".应用力学学报 .01(1994):60-65+122.
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