跨声速激波边界层相互作用的被动控制

IMECH-IR > 力学所知识产出(1956-2008)

	跨声速激波边界层相互作用的被动控制
	张瑜; 李静美; 秦俭
Source Publication	力学学报
	1995
Volume	27 Issue:5 Pages:523
ISSN	0459-1879
Abstract	运用激波管风洞,在Re_∞/m=3×10~7,M_∞=0.732-0.817范围内,在厚度比为12％的圆弧翼型半模型和厚度比为14％的超临界翼型半模型上,对被动控制现象及其若干规律进行了实验研究。结果表明,不同空腔深度的开孔壁和导管连通壁均可对壁面激波与边界层的相互作用实现被动控制,使得沿以上两种模型表面的马赫数峰值、逆压力梯度和激波强度明显减小,这对于飞行器将起到减阻作用。对超、跨声速压气机内激波与边界层相互作用的控制,亦能提高其效率和工作的稳定性。
Keyword	跨声速流激波边界层相互作用被动控制
Indexed By	CSCD
Language	中文
CSCD ID	CSCD:276556
Citation statistics	Cited Times:1[CSCD] [CSCD Record]
Document Type	期刊论文
Identifier	http://dspace.imech.ac.cn/handle/311007/35312
Collection	力学所知识产出(1956-2008)
Corresponding Author	张瑜
Recommended Citation GB/T 7714	张瑜,李静美,秦俭. 跨声速激波边界层相互作用的被动控制[J]. 力学学报,1995,27,5,:523.
APA	张瑜,李静美,&秦俭.(1995).跨声速激波边界层相互作用的被动控制.力学学报,27(5),523.
MLA	张瑜,et al."跨声速激波边界层相互作用的被动控制".力学学报 27.5(1995):523.

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