Molecular kinetic approach to acoustic waves in a compressible boundary layer flow

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Tsukamoto M.,Sakurai A.,Iwatsu R.

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Reference8 articles.

1. Molecular kinetic approach to the problem of compressible turbulence

2. M. Tsukamoto and A. Sakurai, Molecular-Kinetic approach to gas-flow problems, Aeroacoustics, 12, Num5 &6 (2013), pp507–519.

3. A. Sakurai, M. Tsukamoto and H. Honma, A molecular kinetic model reacting gas flows, Proc. 25th Int Symp Rarefied Gas Dynamics(2006), pp929–934.

4. M.M. kuznetsov, I. ILipatov and V.S. Nicol’sky, Asymptotical Analysis of translational Non-equilibrium in the hypersonic flow near the flat plate with the sharp leading edge, Proc. 25th Int Symp Rarefied Gas Dynamics (2006), pp1319–1324.

5. F. Guillaume, S Mohamed, C. Amer. F. Yann and T. Christain, DNS of the interaction between an oblique shock wave and a boundary layer developing along a flat plate, Proc 30th Int Symp Shock Wave(2015), pp495–497

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