IMECH-IR  > 力学所知识产出(1956-2008)
马赫数对后掠激波和湍流边界层干扰特性的影响
王宇; 王世芬
Source Publication空气动力学学报
1994-09-28
Issue03Pages:313-319
ISSN0258-1825
Abstract本文介绍了尖前缘翼诱导激波和湍流边界层干扰流场壁面特性;着重强调马赫数影响。给出2.0≤M_∞≤8.2、α≤35°分离流场中;锥型干扰区内主分离线和再附线位置与无粘激波角β和迎角α的相关式;证实无粘条件是控制锥型区尺度的主要因素。而高超声速与超声速干扰流中二次分离随激波强度的不同发展;表明干扰流场的细致结构与可压缩性有关。
Keyword高超声速流 分离流 激波与边界层干扰 流动显示 尖前缘翼
Indexed ByCSCD
Language中文
Funding Organization国家自然科学基金
CSCD IDCSCD:243403
Citation statistics
Cited Times:1[CSCD]   [CSCD Record]
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/72292
Collection力学所知识产出(1956-2008)
Recommended Citation
GB/T 7714
王宇,王世芬. 马赫数对后掠激波和湍流边界层干扰特性的影响[J]. 空气动力学学报,1994(03):313-319.
APA 王宇,&王世芬.(1994).马赫数对后掠激波和湍流边界层干扰特性的影响.空气动力学学报(03),313-319.
MLA 王宇,et al."马赫数对后掠激波和湍流边界层干扰特性的影响".空气动力学学报 .03(1994):313-319.
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