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March 8, 2012, 04:18
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Aerodynamic coefficients
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#1 |
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New Member
Mark
Join Date: Mar 2012
Posts: 20
Rep Power: 14  |
Hello,
I am new in CFD, and i am using Numeca Software (Numeca Fine and CFVIew), i am simulating a NACA airfoil. I want to calculate some aerodynamic coefficients (for example, Cn, Cd, Cm) but I don't know how to do it...can anybody help me? Best Regards, Mark |
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April 5, 2012, 22:00
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#2 |
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Member
CJ
Join Date: Apr 2010
Location: Malaysia
Posts: 69
Rep Power: 16   |
Hi Daxterss,
Good day. I am sorry to see and reply your message late. Well, for external flow, please do activate in your finehexa or fineopen > computational control > Outputs, then define your flow as external with lift direction, drag direction and etc. Once this option activated, a '.wall' file will be saved after your computation and you may look at this file in your computation folder. I hope this help.
__________________
Regards CJ NUMIT Enterprise, Malaysia +6 017 656 3436 http://maccom-numit.blogspot.com http://www.numit.com.my Email : seiko.q@numit.com.my |
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April 10, 2012, 03:20
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#3 |
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New Member
Mark
Join Date: Mar 2012
Posts: 20
Rep Power: 14 |
I had already discovered but thanks anyway!
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