transonic flows over wings and can limit the flight envelope of aircraft. Based on the
boundary layer characteristics at the shock foot, buffet has been classified as laminar or
turbulent and the mechanisms underlying the two have been proposed to be different
(Dandois et al., J. Fluid Mech., vol. 18, 2018, pp. 156–178). The effect of various flow
parameters (freestream Mach and Reynolds numbers and sweep and incidence angles) on …