|October 31, 2007, 09:08||
cg in Fluent
I want to obtain the roll, pitching, and yaw moment coefficient for the whole airplane (fuselage, wing and tail).
I need to set the cg (center of gravity) to get these values, but I don't know how. Anybody knows about this?
Another question. When we simulate a wing and set the aerodynamics center in report --> force. This moment is calculated relative to cp (center of pressure)? Does Fluent calculate the cp automatically based on the pressure distribution?
Thanks in advance.
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