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Forum: FLUENT

June 17, 2013, 14:39

Replies: 14

3-D wing analysis problem

Views: 3,427

Posted By bikalpa10

thanks kumar but actually i figured out where...

thanks kumar
but actually i figured out where i was going wrong
i choose boundary condition for wind tunnel wall as velocity inlet and that worked out for me.
thanks anyways

Forum: FLUENT

June 15, 2013, 14:01

Replies: 14

3-D wing analysis problem

Views: 3,427

Posted By bikalpa10

uneven flow at aoa

i am doing a similar type of simulation
but whet i set inlet velocity at positive angle of attack
i get the flow accumulated at upper surface of wind tunnel
giving uneven flow throughout the wind...

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