Fig. 11From: Reconstruction of skin friction topology in complex separated flowsTime-averaged surface pressure fields normalized by one atmospheric pressure at Mach 2.5 in incident SWBLI generated by a 13.5° cylindrical cone. From the top plot to bottom plot, the Reynolds numbers \(({Re}_{D})\) are 5, 4, 3, 2 and 1.5 million, respectively. Flow is from left to right. From Liu et al. [32]Back to article page