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RAJEEV October 12, 2012 02:18

AIR intake for fighter aircraft
Hi everyone, I am simulating flow through an air intake duct with pressure ratio 0.85, i specified bc's as pressure farfield for flow entering ( 0.1 MACH and pr = 101325) and outlet (-14500pa ) to set back pressure, but i am getting error mesg that flow as been reversed on outlet faces, later i reduced Courant number and tried but residuals are not converging ... so anybody please rectify this problem.

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