Fig. 4From: Wall pressure beneath a transitional hypersonic boundary layer over an inclined straight circular conea The temporal mean of the wall heat flux \(\bar {Q}_{w}\). Dashed lines represent two trajectories of stationary crossflow vortices V1 and V2 determined by the local maximum of \(\bar {Q}_{w}\). \(\bar {Q}_{w}\) along the two trajectories are given in b with solid and dashed lines respectively for V1 and V2Back to article page