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Old 03-07-2010, 07:33 PM
IvanK IvanK is offline
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Join Date: Oct 2007
Location: Australia
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Wether the engines are in the wings fuselage or wherever the aircraft is designed and certifed to given structual load limit. Now if you get some bending relief from weight in the wings then the designer takes that into account to allow the structure to to be certified at the specified structural design G limit.

Last edited by IvanK; 03-07-2010 at 07:39 PM.