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Showing results 1 to 1 of 1 Search took 0.00 seconds. Search: Posts Made By: NonStopEagle

Forum: FLUENT January 12, 2020, 06:29

Replies: 9 What should be the reference area for a 2d Airfoil Analysis Views: 16,061 Posted By NonStopEagle Alright so, for an airfoil (i.e a 2-d section of... Alright so, for an airfoil (i.e a 2-d section of a wing), the formula for cl is, cl = lift/(0.5)*rho*(v^2)*c where c is the chord length. Since there is no depth in a 2-d simulation, the depth...

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