Online documentation – work in progress
Presentation documents used in the demonstration videos
Project files used in the tutorials
Project files referenced in the online documentation
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.
Vortex Particle Wake: An unsteady, accelerated, high order panel method with vortex particle wakes, D. J. Willis, M.I.T. 2006
Numerical integration over triangle panels:
“Explicit expressions for 3D boundary integrals in potential theory“, S. Nintcheu Fata 2008.
“Potential integrals on triangles”, M. Carley 2012.