Nonlinear aerodynamics of two-dimensional airfoils in severe maneuver

Results are obtained for cases of both large and small amplitude motion. The analysis, which is based in part on an extension of Wagner's integral equation to the nonlinear regime, allows completely for the trailing wake's tendency to deform under local velocities. Interactive computational results are presented for a variety of imposed airfoil motions. These show examples of wake-induced lift and moment augmentation and/or delay on the order of 20-30 percent of quasistatic values as well as a variety of long-term «history» effects

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