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Forum: FLUENT August 8, 2014, 14:18

Replies: 7 NACA 0012 validation Drag problems Views: 2,163 Posted By ARUN.AVIATOR90 Result intrepretetion wat fluent gives is body force tat is CA-cd and CN-cl for zero AOA only(axial and normal force coeff).SO Cl=CN*cos(aoa)-CA*sin(aoa) CD=CA*cos(aoa)+CN*sin(aoa)

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