Mikko Brummer
Senior Member
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- May 16, 2006
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Erwan, I thought the main difference between airplanes & sailboats was that the first one flies in the air and the second floats in the water ;-). The classical paper by RT Jones tells us that when root moment constrained, the downwash distribution (not the span loading) should be linearly decreasing, which leads to a bell-like span loading. For an elliptical span loading, the downwash would be constant.
For sailboats, it was shown in the 70'ies that for best performance in heavy air, the loading should go negative in the top of the sails, the top part supporting against heeling with a long "lever arm", despite the obvious extra drag associated. This leads to a negative camber in the head - look at the top battens of these Star boats sailing in a breeze - heavily overcanvassed, they could not handle a breeze like this in heavy air, without recurring to this special trim.
For sailboats, it was shown in the 70'ies that for best performance in heavy air, the loading should go negative in the top of the sails, the top part supporting against heeling with a long "lever arm", despite the obvious extra drag associated. This leads to a negative camber in the head - look at the top battens of these Star boats sailing in a breeze - heavily overcanvassed, they could not handle a breeze like this in heavy air, without recurring to this special trim.
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