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Old 30th March 2007 | 15:18
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chornedsnorkack
 
Joined: Aug 2005
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From: Estonia
Indeed. Logically, the centre of lift, centre of pressure and aerodynamic centre ought to apply to the whole airframe - "main wing" together with all other surfaces, whether tailplane, canards, tandem wings, fuselage/lifting body or whatever.
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