computation of whole aicraft...
 

Hi,

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?

Best Regards,

ST