Hi Aerohead,
Good observations. I imagine you are thinking about more than you are actually writing. For example, you mention the wheel-less Aptera/Morelli shape which (several sources agree) is a .05 -.06 shape, as is a typical bomb, torpedo, etc. But what you did not mention is that the actual CD with wheels, suspension, ground proximity and drive shafts is at least .15, and the X Prize test results suggest a little higher than that -- although I don't have an accurate frontal area.
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*Sailplanes are governed by skin friction drag
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Sailplanes are all about lift/drag, and fuselage drag is a small part of the overall drag. Induced drag is the big part. If you were writing only about the fuselage, then there is a lot more than just skin drag. It would be simple to make a sailplane with a cylinder for a fuselage, but such a shape produces, (for the fuselage alone) a Cd close to 1. So I think your statement is a little shorter than it needs to be to be valid.
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*the 1957 MG EX 181 registered Cd 0.12 on 'real' tires
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