Mach number distribution for subsonic flow over a bump.

Mach number distribution for subsonic flow over a bump.

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Flow instabilities and impact of ramp–isolator junction on shock–boundary-layer interactions in a supersonic intake, Journal of Fluid Mechanics

Horizontal velocity components; a) Measured and b) calculated values

Supersonic flow over rounded contour bumps with vortex generators or passive longitudinal jets - ScienceDirect

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Survey of control techniques to alleviate repercussions of shock-wave and boundary-layer interactions, Advances in Aerodynamics

Experimental and numerical investigation on a supersonic inlet with large bleed window, The Aeronautical Journal

Snapshot of the argon bubble (d = 0.5 mm) distribution in the symmetry

Energies, Free Full-Text

Laminar buffet and flow control - V Brion, J Dandois, R Mayer, P Reijasse, T Lutz, L Jacquin, 2020

of radiative and convective heat transfer per unit length of radiant