Clmax is called the maximum lift coefficient of a wing. For two wings with similar wing area and airfoil thickness, the wing with higher coefficient of lift will have higher lift for any given angle of attack. The comparision is drawn using a straight wing with same parameters with a swept wing. As the sweep back angle of wing rises the coefficient of lift varies by cosine of the sweep angle. At zero sweep, it is one and at 90* it is zero.Sir what is CImax
And How is the Mirage 2000 so successful
LCA was inspired by Mirage 2000