Learning Forum

[manisha k]

i wanted to know the values of Cd and Cl of the airfoil, the reports in the solution is created is the value of the cl and cd the value found in the report when given compute or is it found in the result section. if it is in result where to find it and how to check the values?

[Rob]

As they're coefficients you need to check you're using the correct reference values. There are NACA tutorials/references on Learning and in the solver Help for further information.