hello people,
I'm designing my firs UAV for aerial photography and FPV purpose from recommendations in this forum i did the wing and plane body analysis using XFLR5 the results of the analysis are in the pics,The angle of attack varies from 0 to 20 degrees over here with max cl at 16degrees according to the airfoil polars obtained...the analysis is a fixed speed analysis...in a nutshellI just needed to to know if the parameters are right and if my UAV is simply gonna fly or not and if anyone has ny links from where i can learn the stability analysis in XFLR5 please share... the airfoil that i have used is CLARK-Y smoothed
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