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Receptivity of hypersonic boundary layer due to fast-slow acoustics interaction 被引量:5

Receptivity of hypersonic boundary layer due to fast-slow acoustics interaction
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摘要 The objective of receptivity is to investigate the mechanisms by which external disturbances generate unsta- ble waves. In hypersonic boundary layers, a new receptivity process is revealed, which is that fast and slow acoustics through nonlinear interaction can excite the second mode near the lower-branch of the second mode. They can generate a sum-frequency disturbance though nonlinear interaction, which can excite the second mode. This receptivity process is generated by the nonlinear interaction and the nonparal- lel nature of the boundary layer. The receptivity coefficient is sensitive to the wavenumber difference between the sumfrequency disturbance and the lower-branch second mode. When the wavenumber difference is zero, the receptivity coefficient is maximum. The receptivity coefficient decreases with the increase of the wavenumber difference. It is also found that the evolution of the sum-frequency disturbance grows linearly in the beginning. It indicates that the forced term generated by the sum-frequency disturbance resonates with the second mode. The objective of receptivity is to investigate the mechanisms by which external disturbances generate unsta- ble waves. In hypersonic boundary layers, a new receptivity process is revealed, which is that fast and slow acoustics through nonlinear interaction can excite the second mode near the lower-branch of the second mode. They can generate a sum-frequency disturbance though nonlinear interaction, which can excite the second mode. This receptivity process is generated by the nonlinear interaction and the nonparal- lel nature of the boundary layer. The receptivity coefficient is sensitive to the wavenumber difference between the sumfrequency disturbance and the lower-branch second mode. When the wavenumber difference is zero, the receptivity coefficient is maximum. The receptivity coefficient decreases with the increase of the wavenumber difference. It is also found that the evolution of the sum-frequency disturbance grows linearly in the beginning. It indicates that the forced term generated by the sum-frequency disturbance resonates with the second mode.
出处 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2015年第6期899-909,共11页 力学学报(英文版)
基金 supported by the National Natural Science Foundation of China (Grants 11332007 and 11202147) the Specialized Research Fund for the Doctoral Program of Higher Education (Grants 20120032120007)
关键词 Hypersonic boundary layer · Receptivity·Nonlinear interaction · Acoustic Hypersonic boundary layer · Receptivity·Nonlinear interaction · Acoustic
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  • 1沈清,袁湘江.三维平面超音速剪切层失稳结构和混合增强的数值模拟[C]//空气动力学前沿研究论文集,北京:中国宇航出版社,2003:397-403.
  • 2Poinsot T J,Lele S K.Boundary conditions for direct simulations of compressible viscous flows[J].Journal of Computational Physics,1992,101(1):104-129.
  • 3付德薰,马延文.计算流体力学[M].北京:高等教育出版社,2002
  • 4Fedorov, A. Transition and stability of high-speed boundary layers. Annual Review of Fluid Mechanics, 43, 79-95 (2010).
  • 5Ma, Y. B. and Zhong, X. L. Receptivity of a supersonic boundary layer over a flat plate, part 2: receptivity to free-stream sound. Journal of Fluid Mechanics, 488, 79-121 (2003).
  • 6Salwen, H. and Grosch, C. E. The continuous spectrum of the Orr-Sommerfeld equation, part 2: eigenfunction expansions. Journal of Fluid Mechanics, 104, 445-465 (1981).
  • 7Balakumar, P. and Malik, M. R. Discrete modes and continuous spectra in supersonic boundary layers. Journal of Fluid Mechanics, 239, 631-656 (1992).
  • 8Tumin, A. The biorthogonal eigenfunction system of linear stability equations: a survey of appli-cations to receptivity problems and to analysis of experimental and computational results. 41st AIAA Fluid Dynamics Conference and Exhibit, American Institute of Aeronautics and Astronau-tics, America (2011).
  • 9Fedorov, A. and Tumin, A. Initial-value problem for hypersonic boundary layer flows. AIAA Journal, 41(3), 379-389 (2003).
  • 10Tumin, A. Multimode decomposition of spatially growing perturbations in a two-dimensional boundary layer. Physics of Fluids, 15, 2525-2540 (2003).

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