Hey Folks,
I am working on a design for an aircraft and I have a dilema. I want to design a tapered wing, and I have the airfoil coordinates, but they are in the natural coordinates with the chord going from 0 to 1. To get the actual airfoil size, all I would need to do is multiply by the real chord length and get a full-sized airfoil. However, I would like to do this internal to ProE if possible. My thinking was, if possible, name a parameter the chord length. Then, use a relation to somehow multiply each row of the tabulated data to get the actual coordinates of the full-length airfoil. Is this possible, and how would I do it? Thanks!
-Chris
I am working on a design for an aircraft and I have a dilema. I want to design a tapered wing, and I have the airfoil coordinates, but they are in the natural coordinates with the chord going from 0 to 1. To get the actual airfoil size, all I would need to do is multiply by the real chord length and get a full-sized airfoil. However, I would like to do this internal to ProE if possible. My thinking was, if possible, name a parameter the chord length. Then, use a relation to somehow multiply each row of the tabulated data to get the actual coordinates of the full-length airfoil. Is this possible, and how would I do it? Thanks!
-Chris