Fig. 4
From: A sharp-interface immersed boundary method for simulating high-speed compressible inviscid flows
Convergence of numerical error versus grid step for supersonic oblique shock
Fig. 4 | Advances in Aerodynamics
From: A sharp-interface immersed boundary method for simulating high-speed compressible inviscid flows
Convergence of numerical error versus grid step for supersonic oblique shock