Inviscid Simulation

This tutorial consists of an external inviscid computation at Mach 6 for a blunted straight cone at 20° angle of attack. The cone nose radius is Rnose = 22.45mm and the cone half angle is 15°.

Mach 6 blunt cone at 20° angle-of-attack: Flowfield U-velocity in symmetry-plane slice showing bow-shock stand-off and forebody structure.