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  • FLUENT - Flow over an Airfoil- Step 7

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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
 No Format
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
 





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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