CFD simulations show that the leading-edge suction parameter correlates with lift for a stationary NACA0012 airfoil in separated flow at high angles of attack, instantaneously in laminar regime and time-averaged in turbulent regime.
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Lift and leading-edge suction parameter of separated flows over an NACA0012 at high angles of attack
CFD simulations show that the leading-edge suction parameter correlates with lift for a stationary NACA0012 airfoil in separated flow at high angles of attack, instantaneously in laminar regime and time-averaged in turbulent regime.