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I am trying to consider a design for a lightweight flapping winged aircraft, powered by an electric motor for each wing.
If you took a wing that is attached to the fuselage by some large 'hinge', then if you replaced the pin in the hinge with the rod from an electric motor (geared right down), would that be an inefficient way of driving the wing up and down?
It is hard for me to explain, but I mean, would it be better to push the wing up and down a few meters out from the hinge, so that there was not so much bad effect from leverage?
If you took a wing that is attached to the fuselage by some large 'hinge', then if you replaced the pin in the hinge with the rod from an electric motor (geared right down), would that be an inefficient way of driving the wing up and down?
It is hard for me to explain, but I mean, would it be better to push the wing up and down a few meters out from the hinge, so that there was not so much bad effect from leverage?