Abstract:
Nonlinear evolution of high-amplitude periodic disturbances in a boundary layer on a flat plate for Mach number M=2 is studied. An anomalous downstream evolution of the disturbances is found, quasi-two-dimensional disturbances being most unstable. The obtained phase velocities of the waves are 30 – 40% greater than the phase velocities of the Tollmien–Schlichting waves. The nonlinear evolution of vortex waves is accompanied by an increase in steady disturbances from the source of controlled vibrations. High-frequency disturbances decay, and a periodic wave train degenerates downstream into a quasiharmonic wave train.
Citation:
A. D. Kosinov, Yu. G. Ermolaev, N. V. Semenov, ““Anomalous” nonlinear wave phenomena in a supersonic boundary layer”, Prikl. Mekh. Tekh. Fiz., 40:5 (1999), 91–98; J. Appl. Mech. Tech. Phys., 40:5 (1999), 858–864
This publication is cited in the following 4 articles:
V. I. Lysenko, B. V. Smorodsky, Yu. G. Yermolaev, S. N. Tagaev, A. D. Kosinov, “Experimental study of the influence of supersonic boundary-layer suction on its stability to controlled disturbances”, Thermophys. Aeromech., 31:3 (2024), 437
V. I. Lysenko, S. A. Gaponov, B. V. Smorodsky, Y. G. Yermolaev, A. D. Kosinov, “Influence of distributed heavy-gas injection on stability and transition of supersonic boundary-layer flow”, Physics of Fluids, 31:10 (2019)
V. I. Lysenko, S. A. Gaponov, B. V. Smorodsky, Yu. G. Yermolaev, A. D. Kosinov, N. V. Semionov, “Combined influence of coating permeability and roughness on supersonic boundary layer stability and transition”, J. Fluid Mech., 798 (2016), 751
S. A. Gaponov, B. V. Smorodskii, “Linear stability of three-dimensional boundary layers”, J. Appl. Mech. Tech. Phys., 49:2 (2008), 157–166