Numerical Simulation of a Flat-Plate Hypersonic Shock Layer Perturbed by External Acoustic Waves

Author:

Kudryavtsev A.N.,Mironov S.G.,Poplavskaya T.V.,Tsyryulnikov I.S.

Publisher

Springer Berlin Heidelberg

Reference6 articles.

1. Ma Y., Zhong, X.: Receptivity of a supersonic boundary layer over a fflat plate. Part 2. Receptivity to free-stream sound. J. Fluid Mech., 488, 79-121 (2003)

2. Egorov, I.V., Sudakov, V.G., Fedorov, A.V.: Numerical simulation of supersonic boundary-layer receptivity to acoustic disturbances. Izvestiya RAN, Mech. Zhidk. i Gaza, 2, 43-52 (2006)

3. Suresh, A., Huynh , S.T.: Accurate monotonicity-preserving schemes with Runge-Kutta stepping. J. Comput. Phys., 136, 83-99 (1997)

4. Kudryavtsev, A.N., Mironov, S.G., Poplavskaya, T.V., Tsyryulnikov, I.S.: Experimental investigation and direct numerical simulation of evolution disturbances in viscous shock layer on a flat plate. J. Appl. Mech. Tech. Phys., 5, 43-52(2006)

5. McKenzie, J.F., Westphal , K.O.: Interaction of linear waves with oblique shock waves. Phys. Fluids, 11, 2350-2362(1968)

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