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Forum: FLUENT

May 7, 2013, 10:17

Replies: 6

Simulating aircraft- my l-d values

Views: 1,464

Posted By blackmask

How could cl be correct if the lift is too low? ...

How could cl be correct if the lift is too low?
CL = lift/(1/2*rho*U^2*Area)

Forum: FLUENT

May 6, 2013, 21:03

Replies: 6

Simulating aircraft- my l-d values

Views: 1,464

Posted By blackmask

Are you sure that you have the right AoA (angle...

Are you sure that you have the right AoA (angle of attack) ? Lift or cl is much easier to predict so that the result of your simulation should not differ much from the real world if you have the same...

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