1.Institute of Theoretical and Applied Mechanics, Siberian Branch,Russian Academy of Sciences,Novosibirsk,Russia;2.Novosibirsk State University,Novosibirsk,Russia
Abstract:
Results of a numerical and experimental study of characteristics of disturbances in a hypersonic shock layer on a flat plate
covered by a sound-absorbing coating and aligned at an angle of attack are presented. Experiments and computations are performed
for the free-stream Mach number M∞ = 21 and Reynolds number ReL = 6 · 104. A possibility of suppressing pressure fluctuations in the shock layer at frequencies of 20–40 kHz with the use of tubular
and porous materials incorporated into the plate surface is demonstrated. Results of numerical simulations are found to be
in good agreement with experimental data.