SDPM is an open-source C++/Python, unsteady compressible source and doublet panel method, developed at the University of Liège by Adrien Crovato and Grigorios Dimitriadis, during the academic years 2022-2024. SDPM is currently capable of rapidly solving steady or unsteady compressible subsonic flows on isolated or multiple wings, as well as calculating the aerodynamic forces gradients. Furthermore, the code is interfaced with OpenMDAO so that aeroelastic computations and optimization can be easily carried out.
This wiki contains the following documentation:
Additionally, the documentation for developers can be built using doxygen. The mathematical and numerical formulations of SDPM can be found in this technical note.