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Forum: Main CFD Forum October 8, 2012, 00:53

Replies: 0 Inviscid Flow Views: 1,165 Posted By cfd seeker Inviscid Flow For the case of inviscid and incompressible flow over a wing at Mach. No=0.1 and Reynold's No=2000 how far should be the flow boundaries? I know for viscous flow the upstream its at least 7 times...

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