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    Chapter and Conference Paper

    Numerical and experimental investigation of viscous shock layer receptivity and instability

    A hypersonic viscous shock layer over a flat plate at the free-stream Mach number M∞ = 21 is investigated both numerically and experimentally. The shock layer is excited by either external acoustic field or bl...

    A. Kudryavtsev, S. Mironov, T. Poplavskaya, I. Tsyryulnikov in Shock Waves (2009)