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computation of whole aicraft...

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August 15, 2007, 03:34	computation of whole aicraft...	#1
ST Guest Posts: n/a	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

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