Examples of incompressible and compressible CFD simulations with the SU2 solver.
Computational aerodynamics
Analysis of fixed-wing aircraft, wind turbines or rotors with computational fluid dynamic codes (Stanford Univeristy Unstructured, SU2 and OpenFOAM) or panel method codes (Aviumtechnologies Panel Method, APM). Full derivation of stability derivatives and hybrid flight-mechanic models (CFD + BEM). Design of fixed-wing aircraft.
CFD solvers | SU2, OpenFOAM |
BEM solvers | APM* |
*More information about the Aviumtechnologies Panel Method (APM) is available at https://apm.aviumtechnologies.com/