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- W587046789 abstract "A linear theory of 2-D thick wing oscillating in a uniform flow is presented. The effects of the steady flow on the boundary condition on body surface are taken into account. It is assumed on the theory that the wake vorticity sheds along straight line from the trailing edge with the uniform vorticity, which greatly simplifies the problem. The distribution of unsteady pressure on the wing and the resulting hydrodynamic forces are obtained by solving the boundary integral equation with respect to velocity potential. Calculated results of the unsteady lift and moment acting on wings heaving in a steady flow are compared with those of model tests in a circulating water tank. These results show that the unsteady lift forces acting on the wing heaving in a steady flow are not much affected by the thickness and attack angle of the wing." @default.
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- W587046789 date "1988-08-25" @default.
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- W587046789 title "HYDRODYNAMIC FORCES ACTING ON A OSCILLATING WING IN UNIFORM FLOW" @default.
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