Evolution of artificial disturbances in separation area of laminar boundary layer for M = 1.43
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Publisher
AIP Publishing
Link
http://aip.scitation.org/doi/pdf/10.1063/5.0052009
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3. The influence of the laminar–turbulent transition on the interaction between the shock wave and boundary layer at a low supersonic Mach number
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1. Evolution of artificial disturbances in a shear layer at M=1.43;Journal of Physics: Conference Series;2021-10-01
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