Figure 4
From: Investigations on the complex flows induced by dual-swept/dual-ramp wedges in supersonic flows
Theoretical results of zones in two intersecting wedges of large sweep angle at θ = 5°, λ = 0°,30°, M0 = 1~8. (a) Mach numbers behind the Mach stem, (b) Mach numbers behind incident wave and reflected wave, (c) static pressure, (d) total pressure recovery coefficient.
