Online documentation – work in progress
Presentation documents used in the demonstration videos
Project files used in the demonstration videos
XFoil Theory document: M. Drela, XFoil: An Analysis and Design System for Low Reynolds Number Airfoils
XFoil program and documentation: https://web.mit.edu/drela/Public/web/xfoil/
Non-linear lifting line theory: J.C. Sivells, R. H. Neely, Method for calculating wing characteristics by lifting-line theory using non-linear section lift data, NACA TN1269, April 1947.
Quad panel method: B. Maskew, Program VSAERO Theory Document, Naca Report 4023,
Viscous loop for panel analyses: E. Ting, D. Chaparro, N. Nguyen, Computationally Efficient Transonic and Viscous Potential Flow Aero-Structural Method for Rapid Multidisciplinary Design Optimization of Aeroelastic Wing Shaping Control, June 2017.