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Help! Supersonic/hypersonic flow over sharp wedge/cone, detached shock

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March 25, 2009, 06:02	Help! Supersonic/hypersonic flow over sharp wedge/cone, detached shock	#1
jwtan New Member Tan Jun Wei Join Date: Mar 2009 Posts: 1 Rep Power: 0	Hi, im doin supersonic and hypersonic flow over a 2D wedge and 3D cone. I've used symmetry and axisymmetric condition for them to save computational time. I'm interested in finding the detached shock when the wedge/cone angle exceeds the max. angle. However, i cant seem to get a converged solution and the shock cant seem to detach. Im using inviscid model, implicit, 2nd order model to run fluent. Can anyone tell me what settings i need to input to be able to get a satisfactory result?

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