| I just started to use Profili software, for airfoil tempaltes drawings, so I could make the frame and finalize the blades from it.
But, when I downloaded the program, and start the "Draw interpolated wing ribs" solution within it, it only asked me the beginning ( root) and ending ( tip ) chords, as well as airfoil shape. I choose NACA 4412, and some chords, but I can not find where to choose wing length ( it's software for airplane wing design).
I am planning to experiment with the bladeclac in cooperation with Profili, so I'll take blade angle from Bladecalc, and airfoils / sections from Profili, and try to produce something good.
Yes, I know it is not the best way to do, but I have some time, and think that there must be a good combo.
Just need info about how to decide the wing(blade) length, if possible. That's because I do not know section dimension. Yes, I can put three airfoils on the table, put all leading edges on one line, and when the trailing edge of the one in the middle touches the line that connect the first and the second, that's it. |
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