Figure 3
From: Investigations on the complex flows induced by dual-swept/dual-ramp wedges in supersonic flows
Shock polar analysis and numerical results of two intersecting wedges at (a,b) θ1 = θ2 = 5°, λ1 = λ2 = 0°, M0 = 3, (c,d) θ1 = θ2 = 5°, λ1 = λ2 = 30°, M0 = 3, (e,f) θ1 = θ2 = 5°, λ1 = λ2 = 30°, M0 = 6. Note: 0-wall, 1-incident shock, 2-reflected shock, 3-internal bridge-shaped shock, 4-slip line, 5-compressional waves.
