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plz help:supersonic flow in shear driven cavity

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March 8, 2011, 02:50	plz help:supersonic flow in shear driven cavity	#1
rajaero86 New Member rajesh Join Date: Mar 2011 Posts: 1 Rep Power: 0	hi...i am working on supersonic flow over a shear driven cavity in FLUENT..I am struck with boundary conditions at inlet and outlet.i am working at mach no of 1.5...when i am using pressure farfield for inlet and pressure outlet bc, i am getting error as "DIVERGENCE DETECTED".when i am using pressure inlet or vel inlet i am not able to find any shock wave at lip of cavity...plz help me in this regard

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