|August 15, 2007, 03:34||
computation of whole aicraft...
I am simulating whole MAV (micro aerial vehicle): duct, propeller, wing and tail.
The simulation purpose is to get the static stability derivatives (CLalpha, CDalpha and CMalpha) of the whole aircraft and for each component.
I think doing the simulation separately for each component will be easier, but I don't know how to integrate the results since I have to take into account the interference effects.
Anybody done this before or have any idea?
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