尖前缘翼干扰区的壁面压力和热流率分布

IMECH-IR > 力学所知识产出(1956-2008)

	尖前缘翼干扰区的壁面压力和热流率分布
	王世芬; 王宇
Source Publication	空气动力学学报
	1995
Volume	13 Issue:4 Pages:447
ISSN	0258-1825
Abstract	给出M_∞=7.8和6.72,Re_∞×10~7/m和5.4×10~7/m气流绕迎角为20°、30°和35°尖前缘翼运动时,平板锥型干扰区的壁面压力和热流率分布。结果表明: (1)平板锥型干扰区的特征几何尺度与无粘激波角β_0和翼迎角α相关,而壁面压力和热流率的峰值与法向马赫数M_n相关。(2)翼面压力和热流率分布由于受拐角涡影响,前者在翼根部呈波谷状,而后者呈波峰状,影响尺度与翼前缘处来流边界层厚度有关。
Keyword	高超声速分离流激波和湍流边界层干扰尖前缘翼壁面压力分布热流率分布
Indexed By	CSCD
Language	中文
CSCD ID	CSCD:275983
Citation statistics	Cited Times:2[CSCD] [CSCD Record]
Document Type	期刊论文
Identifier	http://dspace.imech.ac.cn/handle/311007/35274
Collection	力学所知识产出(1956-2008)
Corresponding Author	王世芬
Recommended Citation GB/T 7714	王世芬,王宇. 尖前缘翼干扰区的壁面压力和热流率分布[J]. 空气动力学学报,1995,13,4,:447.
APA	王世芬,&王宇.(1995).尖前缘翼干扰区的壁面压力和热流率分布.空气动力学学报,13(4),447.
MLA	王世芬,et al."尖前缘翼干扰区的壁面压力和热流率分布".空气动力学学报 13.4(1995):447.

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