Arnold rule; Mike Arnold's aerodynamic ideas

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Aesquire

Well-Known Member
Joined
Jul 28, 2014
Messages
3,346
Location
Rochester, NY, USA
Hypothetical example, a high wing swept wing with moderate taper, flying wing, ( use the platform of an Atos say, ) with a Swift like pod, pusher or puller, trike gear....

Could the optimum fuselage cross section be determined by applying a smooth curve & the wing cross section, "reverse engineering" the shape?
 
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