Re-post from the Gallery
Originally Posted by mikegarrison,Jan 24 2008, 12:26 PM
"Wing root bending moment"
Look it up....
Look it up....
The spanwise aerodynamic loading of wings having minimum induced drag is derived for prescribed lift and root-bending moment. THis problem is an alternative to Prandtl's solution for the case that the lift and its moment of inertia about the longitudinal axis of the aircraft are given.
It's broke.
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Originally Posted by INTJ,Jan 24 2008, 09:37 AM
Note to self: Stop using cardboard wings.
Originally Posted by INTJ,Jan 24 2008, 09:37 AM
Note to self: Stop using cardboard wings.
Originally Posted by INTJ,Jan 24 2008, 09:37 AM
Note to self: Stop using cardboard wings.






