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
Volume27Issue:5Pages:523
ISSN0459-1879
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 ByCSCD
Language中文
CSCD IDCSCD:276556
Citation statistics
Cited Times:1[CSCD]   [CSCD Record]
Document Type期刊论文
Identifierhttp://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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