Hello! I’m in the process of planing the wings for a flying wing without any sweep, but all reflex airfoils I can find have a Cm of -0.05 or something like that, and since I have no tail I need a Cm close to 0, right? I don’t know, what to do now. (really sorry for my bad english)
@Designer103
4 жыл бұрын
I would recommend finding an expert on flying wings. The static margin on those things is too small for me to want to deal with them.
@jamesfinch6455
2 жыл бұрын
How would I know the position of lift force?
@joedoe4249
2 жыл бұрын
It acts at the aerodynamic center of the aircraft and is normal to the aircraft's velocity vector
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