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"Phil J" wrote in message ... OK. But why on the canards flying these days is the little wing in front of the CG, and the big wing behind it. It seems like it would be more stable in pitch if the little wing was behind the CG. Putting the little wing in front of the CG seems like it would make the airplane inherently unstable in pitch. Looking at Rutan's designs, it looks like he countered this by using a swept main wing. But that would have been unnecessary if he had put the smaller wing in back. The only reason I can think of to put the smaller wing out front would be for pilot visibility, so maybe that's the explanation? Phil The pitch and yaw stability of an aircraft have to do with the relationship of the center of gravity and the center of pressure. The farther ahead of the CP the CG is, the more stable an aircraft will be. The swept wing on rutan designs serves 2 purposes. First, it moves the center of lift (and center of pressure) aft in order to accomodate the aft CG caused by the rear mounted engine. Second, sweeping the wing places the vertical surfaces farther aft, giving them more authority. KB |
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