小型跨声速高雷诺数实验装置

IMECH-IR > 力学所知识产出(1956-2008)

	小型跨声速高雷诺数实验装置
	郑之初
Source Publication	力学与实践
	1984
Volume	6 Issue:2 Pages:6-8,45
ISSN	1000-0879
Abstract	<正> (一)引言近代,随着大型飞行器的出现,飞行雷诺数大大提高;C-141飞机事件的出现更使跨声速下雷诺数效应问题成为设计先进飞机和导弹的主要问题.人们迫切需要寻找一种能实现高雷诺数的试验设备.七十年代初期,美国和北大西洋公约组织都成立了专门小组从事这项研究.从雷诺数的定义Re=ρul/μ知道,提高雷诺数有三个途径:增加模型尺度l;提高气体密
Keyword	高雷诺数跨声速雷诺数效应试验设备大型飞行器先进飞机低温风洞马赫数流场
Language	中文
Document Type	期刊论文
Identifier	http://dspace.imech.ac.cn/handle/311007/37512
Collection	力学所知识产出(1956-2008)
Corresponding Author	郑之初
Recommended Citation GB/T 7714	郑之初. 小型跨声速高雷诺数实验装置[J]. 力学与实践,1984,6,2,:6-8,45.
APA	郑之初.(1984).小型跨声速高雷诺数实验装置.力学与实践,6(2),6-8,45.
MLA	郑之初."小型跨声速高雷诺数实验装置".力学与实践 6.2(1984):6-8,45.

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