simulation of supersonic flow
I am new to CFD. I have recently started learning GAMBIT and Fluent.
My question is, I am doing a Shock wave boundary layer analysis over a micro wedge using a 6x6 wind tunnel.
I would also like to do the same in any simulation software available either (Fluent, Solidworks, etc). Please suggest me a good way to start this. I would really appreciate your help. I believe that this is the best forum where I could learn from scratch.
I feel that the question very abstract, but as I said, I dont know anything about the CFD. If there are threads which already discussed this, please point me to them. Any suggestions are welcomed.
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