mf92
Guest
Hello, everyone.
I must, for an examination, design a wing of a strictly structural glider, in practice all aerodynamic parameters including profiles must be credible but I do not care particularly!
I said that I looked for some profiles to be able to use, I found a project of a glider using profiles du (delft university) 80-176. This profile I have as a series of 42 percentage points (support of rope)
How do I import it into the cat?
of course if you have suggestions on some Naca profile used in gliders opto for that without problems. I don't care what I said!
I must, for an examination, design a wing of a strictly structural glider, in practice all aerodynamic parameters including profiles must be credible but I do not care particularly!
I said that I looked for some profiles to be able to use, I found a project of a glider using profiles du (delft university) 80-176. This profile I have as a series of 42 percentage points (support of rope)
How do I import it into the cat?
of course if you have suggestions on some Naca profile used in gliders opto for that without problems. I don't care what I said!