Eduardo Fadul
Well-Known Member
Hi everyone
I am working with a plane that owns a tail like the RANS s12, however I do not have any kind of chart for those "airfoils" made of bended tube.
Does any one have or knows how to calculate de CL and CM Vs Alpha charts for those "airfoils"?
Best regards
I am working with a plane that owns a tail like the RANS s12, however I do not have any kind of chart for those "airfoils" made of bended tube.
Does any one have or knows how to calculate de CL and CM Vs Alpha charts for those "airfoils"?
Best regards