Wing Analysis Program

This Java application computes the lift and Cl distribution over a wing with sweep and twist.
To increase the angle of attack, click near the upper part of the plot; to reduce alpha, click in the lower area.

The analysis is a discrete vortex Weissinger computation. Pitching moment is based on the mean geometric chord and is measured about the root quarter chord point. The twist is assumed linear and is taken to be positive for washout (tip incidence less than root incidence).