用短周期风洞进行涡轮叶片传热实验的初探

IMECH-IR > 力学所知识产出(1956-2008)

	用短周期风洞进行涡轮叶片传热实验的初探
	李静美; 赵润民; 王吉南
Source Publication	航空动力学报
	1987
Volume	2 Issue:1 Pages:18-22,89
ISSN	1000-8055
Abstract	本文介绍了短周期激波叶栅风洞的结构,原理和实验模型,以及在来流条件为Ma_(入口)=0.21和0.15,Re_∞/L=1×10~7,T_O/T_W=2.2时,进行涡轮叶片测压和传热实验的初步结果。结果表明10毫秒的实验时间是足够的,目前的实验方案完全可行。
Keyword	短周期风洞传热实验涡轮叶片热流率分布叶片表面马赫数叶背叶栅风洞半无限体
Language	中文
Document Type	期刊论文
Identifier	http://dspace.imech.ac.cn/handle/311007/36848
Collection	力学所知识产出(1956-2008)
Corresponding Author	李静美
Recommended Citation GB/T 7714	李静美,赵润民,王吉南. 用短周期风洞进行涡轮叶片传热实验的初探[J]. 航空动力学报,1987,2,1,:18-22,89.
APA	李静美,赵润民,&王吉南.(1987).用短周期风洞进行涡轮叶片传热实验的初探.航空动力学报,2(1),18-22,89.
MLA	李静美,et al."用短周期风洞进行涡轮叶片传热实验的初探".航空动力学报 2.1(1987):18-22,89.

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