期刊
THEORETICAL AND COMPUTATIONAL FLUID DYNAMICS
卷 23, 期 2, 页码 79-107出版社
SPRINGER
DOI: 10.1007/s00162-009-0103-z
关键词
Shock boundary layer interaction; Global mode; Compressible turbulence; LES; Low-frequency unsteadiness; Separation bubble; Digital filter; Inflow turbulence
资金
- EPSRC
- Engineering and Physical Sciences Research Council [EP/G069581/1, EP/F011016/1] Funding Source: researchfish
- EPSRC [EP/F011016/1, EP/G069581/1] Funding Source: UKRI
The need for better understanding of the low-frequency unsteadiness observed in shock wave/turbulent boundary layer interactions has been driving research in this area for several decades. We present here a large-eddy simulation investigation of the interaction between an impinging oblique shock and a Mach 2.3 turbulent boundary layer. Contrary to past large-eddy simulation investigations on shock/turbulent boundary layer interactions, we have used an inflow technique which does not introduce any energetically significant low frequencies into the domain, hence avoiding possible interference with the shock/boundary layer interaction system. The large-eddy simulation has been run for much longer times than previous computational studies making a Fourier analysis of the low frequency possible. The broadband and energetic low-frequency component found in the interaction is in excellent agreement with the experimental findings. Furthermore, a linear stability analysis of the mean flow was performed and a stationary unstable global mode was found. The long-run large-eddy simulation data were analyzed and a phase change in the wall pressure fluctuations was related to the global-mode structure, leading to a possible driving mechanism for the observed low-frequency motions.
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