Lift coefficient for the airfoil section located at arbitrary spanwise station Calculator
The lift coefficient (Cl) for an airfoil section located at an arbitrary spanwise station represents the dimensionless measure of the lift generated by that specific section of the airfoil. Local section lift slope (a0) in per rad Effective angle of attack at the spanwise station y₀ (αeff(y₀)) in rad Zero-lift angle of attack (αL=0) in […]