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This LS-DYNA simulation shows a simple 2D CESE input deck with a diffraction moving normal shock wave around a 90 degree corner. The Mach number is 1.2 and the moving normal shock wave relations are used in order to determine the inlet parameters.

References :

[1] : O. I. K . Takayama, Shock wave diffraction over a 90 degree sharp corner, Posters presented at 18 th ISSW, (1991).