Question: Need help 6. The glider is to be modified into a powered plane, and as the result of a forward mounted propeller and an enlarged
Need help

6. The glider is to be modified into a powered plane, and as the result of a forward mounted propeller and an enlarged fuselage, the neutral point wi be shifted forward by 7% of the wing chord (AXnp = -0.07). How far forward (from the current location) should we shift the CG in order to achieve a SM of 10%)? 7. Recall that static margin SM = XNP - Xcc, prove the following: Cma SM = - CLa,veh 8. Prove the following: acm SM = - aCLveh
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