再入飞行器和模型转换雷诺数计算

IMECH-IR > 力学所知识产出(1956-2008)

	再入飞行器和模型转换雷诺数计算
	周正瑾
Source Publication	空气动力学学报
	1989
Volume	7 Issue:2 Pages:171-177
ISSN	0258-1825
Abstract	本文采用近似的激波关系、球锥体压力分布、平衡气体状态方程、边界层厚度计算公式及转捩准则等,按照流管法计算了4种再入飞行器的外流转捩雷诺数和转捩距离,并给出了高硅氧、碳石英、碳碳球锥模型的转捩雷诺数范围,对再入飞行器和模型的计算结果作了分析和比较。
Keyword	转捩雷诺数再入飞行器模型烧蚀
Language	中文
Document Type	期刊论文
Identifier	http://dspace.imech.ac.cn/handle/311007/36470
Collection	力学所知识产出(1956-2008)
Corresponding Author	周正瑾
Recommended Citation GB/T 7714	周正瑾. 再入飞行器和模型转换雷诺数计算[J]. 空气动力学学报,1989,7,2,:171-177.
APA	周正瑾.(1989).再入飞行器和模型转换雷诺数计算.空气动力学学报,7(2),171-177.
MLA	周正瑾."再入飞行器和模型转换雷诺数计算".空气动力学学报 7.2(1989):171-177.

Related Services

Bookmark

Lanfanshu

Similar articles in Bing Scholar

Terms of Use

No data!

Social Bookmark/Share

File name:	Paper0446.pdf
Format:	Adobe PDF

This file does not support browsing at this time

All comments (0)

No comment.

The comment function is only available to registered usersLog In

If you have any objections to this item, please fill out the form below and the administrator will contact you as soon as possible.
Content:
Email：	*
Institution:
Verification Code:	Refresh

Any comments and suggestions are welcomed.
Title:	*
Content:
Email：	*
Verification Code:	Refresh

中国科学院力学研究所机构知识库