Fig. 8From: Oblique-mode breakdown in hypersonic and high-enthalpy boundary layers over a blunt coneContours of the time-averaged flow: (a) the streamwise velocity \(\bar {u}/U_{\infty }\) at s=1.05m with the black lines the disturbance streamlines in the y−θ plane and (b) the wall-normal gradient \(\partial \bar {T}/(T_{\infty } \partial y)\) at the wallBack to article page