Fig. 8From: Wall pressure beneath a transitional hypersonic boundary layer over an inclined straight circular coneThe distribution of the r.m.s. (shaded contour) of the low- (10-50 kHz, I) and high-frequency (300-600 kHz, II) wall pressure and the wall heat flux (dashed lines) in the neighbourhood of stationary crossflow vortex trajectories V1 a and V2 b. Trajectories V1 and V2 are colored in blackBack to article page