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Inviscid Simulation

This tutorial consists of an external inviscid computation at Mach 9.59 for a missile type geometry, the HB-2, at 0° angle of attack.

Cone at 20deg aoa - inviscid flow-field Mach 9.59 HB-2 geometry at 0° angle-of-attack: Flowfield U-velocity in symmetry-plane slice showing bow-shock stand-off and forebody structure.