Steady VLM correction exemplar

This dataset includes an example MATLAB script that implements corrections to steady Vortex Lattice Method (VLM) results. Corrections include: Viscous lift curve slope. Lifting surface viscous drag (including lift-dependent viscous drag). Fuselage profile drag. Fuselage contribution to pitching moment. Tailplane contribution to pitching moment. The example includes experimental wind tunnel data from a model of an English Electric Canberra, along with software models of this aircraft in three popular steady VLM solvers: AVL, XFLR5 and OpenVSP/VSPAERO.