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  • FLUENT - Flow over an Airfoil- Step 7

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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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titleForce Convention

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This is an inviscid model, we are expecting a drag coefficient of zero, and yet there is a small drag coefficient that present. We should investigate more into this.

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