Aerodynamic Loads

[Tony Renshaw <renshaw@ozemail.com.au>]

Gidday,
Can anyone supply the formula/s for calculating the applied force on a
flight control, so that I may be able to do a load analysis on using teflon
sleeved hinges with the consequent reduced pin diameter. If the areas of
ailerons,rudder, and trim tabs is also known this would also be hand At the
same time if anyone knows the forum address for the Longeze/Varieze builders
I would appreciate getting it also.Thanks
Reg
Tony Renshaw
Builder No.236