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Main Menu > Report > Forces...
Select Forces. Under Force Vector, enter 0.9998 next to X. Enter 0.02094 next to Y. Select airfoil under Wall Zones. Click Print.
Here's is what we see in the main menu:
Code Block |
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No Format |
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Force vector: (0.99980003 0.02094 0)
pressure viscous total pressure viscous total
zone name force force force coefficient coefficient coefficient
n n n
------------------------- -------------- -------------- -------------- -------------- -------------- --------------
airfoil 3.8125084 0 3.8125084 0.0024897052 0 0.0024897052
------------------------- -------------- -------------- -------------- -------------- -------------- --------------
net 3.8125084 0 3.8125084 0.0024897052 0 0.0024897052
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Before we can make any conclusion about the accuracy of our result, we should always make validation check. The most common validation step is grid convergence check.
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