coeffiecnt of lift and drag for naca0012
 

hey
i am pretty new to this ansys and fluent
i am trying to calculate coefficient of lift and drag for different angles of attack. Is it possible that i can import a table/ matrix from excel and ask ansys to calculate for each value of angle of attack?
or do i have to do it manually for each angle of attack which is quite monotonous and boring?

i am quite new to ANSYS FLUENT. so could you explain in detail?