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Movement of a Wing with a Small Aspect Ratio Near the Interface of Fluids with Different Densities

Abstract : The problem of the movement of a wing with a small aspect ratio below a free fluid surface has been studied. The integral equation for a wing with a small aspect ratio moving above the interface of fluids with different densities was obtained in a similar manner. But these studies did not determine the distribution of the load over the wing chord. This report will solve the problem which makes it possible to find the load distribution over the wing chord when condition lambda F r squared approaches zero, is satisfied, the Froude number being calculated for the wing span.