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#1 |
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New Member
ajay varma
Join Date: Dec 2015
Location: india
Posts: 7
Rep Power: 11 ![]() |
Im using fluent for analyzing flow on a 2d wing. my flow speeds are around 30m/s . solver settings are : pressure based, k-w SST, boudary conditions are
velocity inlet , pressure outlet,top(wall),bottom(wall),aerofoil (wall). i have done modeling in icem cfd with 7lakh quad mesh and i have used farfield distance for about 5 times of the chord due to computational constraints. i m having problem with increase in the angle of attack.that is pressure coeffiecient value is going higher than that of 1 when i increase my angle to 4 degree. can someone pls help me .
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#2 |
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Senior Member
Lucky
Join Date: Apr 2011
Location: Orlando, FL USA
Posts: 5,836
Rep Power: 68 ![]() ![]() ![]() |
Check your reference values. Make sure you have specified the correct reference velocity, length, etc.
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#3 |
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New Member
ajay varma
Join Date: Dec 2015
Location: india
Posts: 7
Rep Power: 11 ![]() |
how should we calculate reference values, if there is any way please kindly specify thank you
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| Tags |
| fluent 16.0, icem cfd 16.2 |
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