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This repository has been archived by the owner on Jan 11, 2022. It is now read-only.
TriPan is the product of decades of research into high-speed aerodynamics and boundary element methods. We would be amiss to acknowledge the incredible contributions made by countless women and men who have contributed to this field since Ludwig Prandtl first started delving into the world of supersonic flow. Truly, we stand on the shoulders of giants. Since TriPan builds on a long legacy of linear panel methods, we here present a number of relevant sources which will give the user insight into the workings of panel methods.
Erickson, L., "Panel Methods: An Introduction," NASA Technical Paper 2995, 1990.
The following sources deal specifically with the development of TriPan itself:
Goates, C. and Hunsaker, D., "Development of a Subsonic-Supersonic, Unstructured Panel Method," AIAA SciTech Conference, San Diego, CA, 2022.