I have an 8' Senior Telemaster because of its High Lift Capability.
And one argument I have is with the way common RC flyer's Balance the Telemaster's CG before flight.
I seek a solution for calculating the CG that provides input for the lifting tail of the Telemaster. Because such a solution would allow the airframe to share lifting duties between the main wing and the lifting tail.
The "experienced flyers" at my airfield insist on balancing the plane as you would a non-lifting tail RC plane. I feel they are not taking into account the lifting tail of the Telemaster. Where CG balancing between the lift capability of the main wing and tail is achieved.
I believe that when balancing the CG on the Telemaster it should be tail heavy when balancing the "traditional" way.
Can anyone help me with this. I believe it would increase the actual lift capability of the plane.