With CFS1, you really don't have a choice about fixing the CoG if it is located incorrectly. My preference given a choice is to put the center (0,0,0) of the model at about 1/3 chord of the wing and slightly below the centerline of the engine on a low wing aircraft because the wing structure and landing gear shift the whole CoG down a bit.
Hi Sparks,
I joined late in this thread, but here goes: My understanding was that the Center of Lift really describes the the lift of the wing. In level flight, it would be balanced out by trim effects mostly from the horizontal stabilizer. Ideally, for most efficient flight, the center of lift should be slightly ahead of the CoG so that the h-stabilizer is also providing a slight amount of lift, but still set up in such a manner that the wing stalls before the h-stabilizer. Some aircraft are set up so that the CoG is slightly ahead of the Center of Lift and the tail has to provide downforce but this is less efficient because the wing has to also counter the tail's downforce.
Reasonable?
- Ivan.
Correct on CFS1, the FM center is the MDL center.
The wing has a center of lift and the airframe has a center of lift, which may or may not be in the same position.
In FS, we only have one CoL, which is the sum of the lift of the wing, horizontal stab and elevator.
The purpose of the elevator is to change the moment coefficient (CM), but changing CM can also be thought of as changing the postion of the CoL.
In order for an aircraft to fly level, the CoL and the CoG have to be in the same location. If they are not, you will have pitch rotation - i.e. the nose will pitch up or down. That's why the CoL and CoG are usually located close together with the plane loaded and fueled, and the elevator and trim neutral.