高超声速压缩拐角再附峰值热流率

IMECH-IR > 力学所知识产出(1956-2008)

	高超声速压缩拐角再附峰值热流率
	王世芬; 徐朝仪
Source Publication	流体力学实验与测量
	1997
Volume	11 Issue:3 Pages:23-27
ISSN	1007-3124
Abstract	给出三维和二维压缩拐角诱导激波与高超声速层流和湍流边界层相互作用的流场结构和前向压缩表面的热流率分布。实验气流M数为7．8，单位长度Re数为3．5×107／m。结果表明：激波与边界层相互作用能促进边界层转捩。只有基于再附峰值热流率位置长度的参考温度条件下的雷诺数足够低，相互作用过程才能是纯层流的。在全再附高超声速分离流中，再附峰值热流率可用Simeonides通用相关式进行估算。
Keyword	高超声速流分离流激波与边界层相互作用再附峰值热流率压缩拐角
Language	中文
Document Type	期刊论文
Identifier	http://dspace.imech.ac.cn/handle/311007/35184
Collection	力学所知识产出(1956-2008)
Corresponding Author	王世芬
Recommended Citation GB/T 7714	王世芬,徐朝仪. 高超声速压缩拐角再附峰值热流率[J]. 流体力学实验与测量,1997,11,3,:23-27.
APA	王世芬,&徐朝仪.(1997).高超声速压缩拐角再附峰值热流率.流体力学实验与测量,11(3),23-27.
MLA	王世芬,et al."高超声速压缩拐角再附峰值热流率".流体力学实验与测量 11.3(1997):23-27.

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