Fig. 5From: A sharp-interface immersed boundary method for simulating high-speed compressible inviscid flowsPressure contours (1) and (3), Mach number contours (2) and (4), with different flows Ma = 0.8, α = 1.25∘ (1–2) and Ma = 0.85, α = 1∘ (3–4)Back to article page