Hi all,
I want to do a simulation about 2D airfoil, but I have tried so many times but I got a failure. Can somebody help me?
In addition, can someone tell me how to calc the lift, drag and moment coefficients?
Thanks very much!
2D_AIRFOIL TESTCASE
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Luciano Garelli
- Posts: 284
- Joined: Fri Dec 04, 2015 1:42 pm
Re: 2D_AIRFOIL TESTCASE
Hello,
I think that you forget to specify the velocity direction at inlet BC, maybe this is the problem.
Always search in the forum your keywords ("lift, drag, etc") in order to know if someone has ask the same question, I leave here a link
http://code-saturne.org/forum/viewtopi ... =2&t=2059
Also, you can check the file cs_user_extra_operations-global_efforts.f90 at SRC/EXAMPLE directory
Regards,
Luciano
I think that you forget to specify the velocity direction at inlet BC, maybe this is the problem.
Always search in the forum your keywords ("lift, drag, etc") in order to know if someone has ask the same question, I leave here a link
http://code-saturne.org/forum/viewtopi ... =2&t=2059
Also, you can check the file cs_user_extra_operations-global_efforts.f90 at SRC/EXAMPLE directory
Regards,
Luciano