I have never used solidworks before so dont judge me too harshly i know its probably a very obvious question, but for my final year project i am designing  a wing to test in wind tunnel and my supervisor thought it would be good if i learned how to use solidworks but im not getting anywhere fast. I am basing the wing on 1:5 ratio of a cessna 172 aircraft wing so i downloaded coordinates for NACA 2412 airfoil and appropriately modified 2 sets of coordinates to match the root chord and tip chord length of the wing but i dont know how to seperate the two curves by 1000mm (wing span). Would massively appreciate some help!