M_∞=1及其附近翼型绕流的计算结果

IMECH-IR > 力学所知识产出(1956-2008)

	M_∞=1及其附近翼型绕流的计算结果
	何龙德
Source Publication	空气动力学学报
	1989
Volume	7 Issue:2 Pages:255-257
ISSN	0258-1825
Abstract	本文全速势方程的有限差分数值计算结果,给出了0°和2°攻角下NACA0012翼型当地马赫数分布冻结时的自由流马赫数范围,以及M_∞稍大于1变至1.30时前方脱体激波的变化位置。
Keyword	跨音速流音速流马赫数冻结
Indexed By	CSCD
Language	中文
Citation statistics
Document Type	期刊论文
Identifier	http://dspace.imech.ac.cn/handle/311007/36474
Collection	力学所知识产出(1956-2008)
Corresponding Author	何龙德
Recommended Citation GB/T 7714	何龙德. M_∞=1及其附近翼型绕流的计算结果[J]. 空气动力学学报,1989,7,2,:255-257.
APA	何龙德.(1989).M_∞=1及其附近翼型绕流的计算结果.空气动力学学报,7(2),255-257.
MLA	何龙德."M_∞=1及其附近翼型绕流的计算结果".空气动力学学报 7.2(1989):255-257.

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