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)
this video is fucking pure gold
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)
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.
How would I know the position of lift force?
It acts at the aerodynamic center of the aircraft and is normal to the aircraft's velocity vector
Hello me again, how do i get the air density?
initially u have to determine the altitude