Joined May 2015
Sorry to write here but I didn’t find an other option.
First of all I have some questions about the design program XFLR5.
I created a Matlab program in wich you can generate an archive .dat with as coordenates of the airfoil´s points through the Kutta Joukovski equations. The problem is that, when I opened my archive with XFLR5 , the program draw the airfoil but say that the value of the thickness , camber, etc are CERO. Therefore, when I start the Batch analysis it doesn´t converge, and don’t do anything.
I compared my archive with one which I downloaded, and they looks similar.
In fact, I tried to load a NACA airfoil and then edit their coordinates, but the result is exatly the same, don’t do nothing.
If someone can help me I could be in contact with him/her. I will be very gratefully.
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