超音速来流中侧向喷流干扰流场的数值模拟

IMECH-IR > 力学所知识产出(1956-2008)

	超音速来流中侧向喷流干扰流场的数值模拟
Alternative Title	Numerialc Simulation of Lateral Jet Interaction in Supersonic Flow
	周维; 刘宏; 刘嘉; 王发民
Source Publication	航空学报
	2004
Volume	25 Issue:2 Pages:108-112
ISSN	1000-6893
Abstract	通过求解三维可压缩N-S方程组，对尖锥／圆柱组合体模型在超音速绕流中的侧向喷流干扰流场进行了模拟，数值方法采用有限体积法，差分格式采用NND格式。分析了干扰流场的结构，研究了干扰效应对气动性能的影响，得到来流Ma。。=3．3和4．5时力放大因子和干扰力矩系数随攻角变化的规律，计算结果与实验一致。
Keyword	侧向喷流
Subject Area	力学
Indexed By	CSCD ; EI
Language	中文
CSCD ID	CSCD:1642656
Citation statistics
Document Type	期刊论文
Identifier	http://dspace.imech.ac.cn/handle/311007/15985
Collection	力学所知识产出(1956-2008)
Recommended Citation GB/T 7714	周维,刘宏,刘嘉,等. 超音速来流中侧向喷流干扰流场的数值模拟[J]. 航空学报,2004,25,2,:108-112.
APA	周维,刘宏,刘嘉,&王发民.(2004).超音速来流中侧向喷流干扰流场的数值模拟.航空学报,25(2),108-112.
MLA	周维,et al."超音速来流中侧向喷流干扰流场的数值模拟".航空学报 25.2(2004):108-112.

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