蜂蜡球锥的驻点烧蚀研究

IMECH-IR > 力学所知识产出(1956-2008)

	蜂蜡球锥的驻点烧蚀研究
	周正瑾
Source Publication	力学学报
	1984
Volume	16 Issue:2 Pages:192-196
ISSN	0459-1879
Abstract	<正> 1.引言飞行器再入大气层时受热情况严重,表面要发生严重的烧蚀,外形要发生显著的变化,驻点的烧蚀更为严重。这一烧蚀过程能否由蜂蜡这种低温液态层材料在高超音速风洞中再现,能否通过对蜂蜡球锥的驻点烧蚀研究为液态层材料的烧蚀图象形成机理和发展规律提供依据,为两相流问题的理论研究提供实验资料,这便是我们进行蜂蜡球锥驻点烧蚀研究的目的。
Keyword	烧蚀率驻点压力烧蚀图象球锥蜂蜡经验公式高超音速风洞大气压头部半径
Language	中文
Document Type	期刊论文
Identifier	http://dspace.imech.ac.cn/handle/311007/37506
Collection	力学所知识产出(1956-2008)
Corresponding Author	周正瑾
Recommended Citation GB/T 7714	周正瑾. 蜂蜡球锥的驻点烧蚀研究[J]. 力学学报,1984,16,2,:192-196.
APA	周正瑾.(1984).蜂蜡球锥的驻点烧蚀研究.力学学报,16(2),192-196.
MLA	周正瑾."蜂蜡球锥的驻点烧蚀研究".力学学报 16.2(1984):192-196.

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