|March 25, 2009, 06:02||
Help! Supersonic/hypersonic flow over sharp wedge/cone, detached shock
Tan Jun Wei
Join Date: Mar 2009
Posts: 1Rep 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?
|cone, detached shock, wedge|
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