On Mon, 16 May 2005 at 19:08:12 in message
.com, george
wrote:

Me too. This should be interesting. Different parts of the same a/c
accelerating at different speeds.
Hey look the wing's formating with us .............

Depends what you are doing. A steady roll rate at positive 'g' overall
will reduce the AoA of one wing and increase that of the other. Thus
reducing the load on one wing and increasing it on the other. If the
aircraft as whole is flying at zero 'g' then the wing loads will be
substantially the same but in different directions relative to the wing
section

However if you have a roll acceleration (Degrees per second per second)
then there will be a different 'g' acceleration at the wing tips from
the roots..

However just noting the 'g' in that case is not a good guide to finding
the forces on the structure.

Cross posting reduced to rec.aviation.piloting,rec.aviation.student
--
David CL Francis