Fig. 18From: Wall pressure beneath a transitional hypersonic boundary layer over an inclined straight circular coneCpp(ÎΞ,0,Ît) for high-frequency wall pressure at probe points in Group 2. Solid and dashed contours for 0.5 and -0.5 respectively. Solid lines represent ÎΞ/Ît=0.85qâBack to article page