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Development of second-mode instability in a Mach 6 flat plate boundary layer with two-dimensional roughness
Tang, Qing ; Zhu, Yiding ; Chen, Xi ; Lee, Cunbiao
刊名PHYSICS OF FLUIDS
2015
关键词SMALL-AMPLITUDE DISTURBANCES IMPINGING SHOCK-WAVE NUMERICAL INVESTIGATIONS RAYLEIGH-SCATTERING TRANSITION STABILITY FLOW SIMULATION MA=4.8
DOI10.1063/1.4922389
英文摘要Particle image velocimetry, PCB pressure sensors, and planar Rayleigh scattering are combined to study the development of second-mode instability in a Mach 6 flow over a flat plate with two-dimensional roughness. To the best of the authors' knowledge, this is the first time that the instantaneous velocity fields and flow structures of the second-mode instability waves passing through the roughness are shown experimentally. A two-dimensional transverse wall blowing is used to generate second-mode instability in the boundary layer and seeding tracer particles. The two-dimensional roughness is located upstream of the synchronization point between mode S and mode F. The experimental results showed that the amplitude of the second-mode instability will be greatly increased upstream of the roughness. Then it damps and recovers quickly in the vicinity downstream of the roughness. Further downstream, it acts as no-roughness case, which confirms Fong's numerical results [K. D. Fong, X. W. Wang, and X. L. Zhong, "Numerical simulation of roughness effect on the stability of a hypersonic boundary layer," Comput. Fluids 96, 350 (2014)]. It also has been observed that the strength of the amplification and damping effect depends on the height of the roughness. (C) 2015 Author(s). All article content, except where otherwise noted, is licensed under a Creative Commons Attribution 3.0 Unported License.; National Natural Science Funds of China for Distinguished Young Scholar group [10921202, 11221061]; SCI(E); EI; ARTICLE; cblee@mech.pku.edu.cn; 6; 27
语种英语
内容类型期刊论文
源URL[http://ir.pku.edu.cn/handle/20.500.11897/419632]  
专题工学院
推荐引用方式
GB/T 7714
Tang, Qing,Zhu, Yiding,Chen, Xi,et al. Development of second-mode instability in a Mach 6 flat plate boundary layer with two-dimensional roughness[J]. PHYSICS OF FLUIDS,2015.
APA Tang, Qing,Zhu, Yiding,Chen, Xi,&Lee, Cunbiao.(2015).Development of second-mode instability in a Mach 6 flat plate boundary layer with two-dimensional roughness.PHYSICS OF FLUIDS.
MLA Tang, Qing,et al."Development of second-mode instability in a Mach 6 flat plate boundary layer with two-dimensional roughness".PHYSICS OF FLUIDS (2015).
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