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Search: Posts Made By: aamer
Forum: Main CFD Forum December 21, 2010, 00:23
Replies: 9
Views: 5,007
Posted By aamer
Dear Pano... thanks for...

Dear Pano...
thanks for enlightening me on the subject with very relevant technical details. Most of the things that you have asked me to try have already been done, like , change...
Forum: Main CFD Forum December 13, 2010, 02:29
Replies: 9
Views: 5,007
Posted By aamer
Dear Pano..... i am...

Dear Pano.....
i am getting correct Cd values for almost all angles of attack but i am getting slightly higher Cl than the experimental values . For example at 5 degree angle...
Forum: Main CFD Forum December 12, 2010, 12:37
Replies: 9
Views: 5,007
Posted By aamer
Dear Pano... your comments on...

Dear Pano...
your comments on the subject were very helpful. i am actually validating experimental results of corrugated airfoil at reynolds number of 34000. my case is inherently...
Forum: Main CFD Forum December 11, 2010, 05:07
Replies: 9
Views: 5,007
Posted By aamer
Hi pano..... thanks for the...

Hi pano.....
thanks for the reply...... your suggestions regarding the use of excel or matlab seems valid.
but i didn't understand how can i get these values from a steady...
Forum: Main CFD Forum December 10, 2010, 09:21
Replies: 9
Views: 5,007
Posted By aamer
Question how to calculate mean value of lift and drag

Hello all....
if i am running unsteady simulation, i will get values of lift and drag that will show time periodic curve when the solution is converged. How can i precisely get the...
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