AeroWing version 1.20

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Correct the assumption made on the chord line considered as the zero lift chord in the AeroWing version 1.1.
Add the thickness distribution of the finite wing mesh.
Add more choice of reinforcement form for the case of composite wing.
Another interest of this program is that it is FREE of charge. Unfortunately, this program woks only with MATLAB. Our efforts are also focused to make this AeroWing program working with Matlab clones (like OCTAVE or SciLab) that are completely FREE too.
Check the program in MAC platform.