Numerical Lifting Line Wing Analysis Tool

Summary

This code uses a numerical lifting line method to determine the lift and drag of an un-swept subsonic wing.  The main use case of this code is to determine optimal washout distributions for a given optimal lift distribution.  The code can create an optimal washout distribution for an elliptic distribution or a Prandtl bell distribution.  It also outputs the bending moment on the wing as a function of span.   It can accept an arbitrary planform shape and any section airfoil properties that can be determined using a vortex panel method such as THIS ONE, or xfoil.

Some sample outputs of the code are shown below.  Detailed writeup of this code will be added soon!