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Experimental data comprising unsteady lift, pitching moment and rolling moments are presented for a set of three finite wing planforms immersed in two-dimensional oscillating gusts which are incident at oblique angles of up to 20 deg from the wing centerline. The effects of the resultant asymmetric lift distribution on the two wing halves are identified in the results with particular reference to the amplitudes and phases of rolling moment that are generated.
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M.H. Patel (1982) studied this question.
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