Fig. 5From: Wall pressure beneath a transitional hypersonic boundary layer over an inclined straight circular coneThe instantaneous a and r.m.s. b of the fluctuating wall pressure. The dashed lines in b represent the trajectories of stationary crossflow vortices shown in Fig. 4. The markers are probe points with those upstream and downstream of the transition front labeled as Group 1 and Group 2, respectivelyBack to article page