Fig. 9From: Oblique-mode breakdown in hypersonic and high-enthalpy boundary layers over a blunt coneContours of the instantaneous flow: (a) the streamwise velocity u/U∞ at y=1.4mm in the s−θ plane and (b) the wall-normal gradient of the density ∂ρ/(ρ∞∂y) in the s−y planeBack to article page