Lift and Moment Prediction For an Oscillating Airfoil With a Moving Separation Point
1974 ◽
Vol 96
(4)
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pp. 372-378
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An analytical method for predicting the perturbed aerodynamic reactions of a harmonically oscillating flat plate airfoil with time dependent point of separation is presented. It is shown that this method in conjunction with an empirical knowledge of the time history of the separation point can predict stall-flutter. Numerical results are presented and compared with existing theoretical and experimental results with special emphasis on torsional mode of oscillation.
2013 ◽
Vol 549
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pp. 397-404
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2011 ◽
Vol 243-249
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pp. 2259-2265
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1977 ◽
Vol 99
(3)
◽
pp. 365-368
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