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A couple of Boeing G limit question
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6th May 2014 | 23:30
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Pugilistic Animus
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Whenever you change stall speeds you change the stall limited maneuver speed (Vp). Since the maximum weight to be carried by the wing is the weight the wing carries at the stall. The relationship is Vp=Vs(n)^0.5, where n is the design limit load
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