CFD
SU2
A reference pack and input adapter for SU2 configuration and mesh files. Tasks cannot run SU2.
No verified recipe for this solver is installed. The pack below is reference guidance and an input adapter. On an installation with the open workbench the assistant can set up and run cases itself with the solvers the workbench holds; such a result is marked verified against theory when it agrees with a named theoretical value, and otherwise converged and checked, not independently verified.
This describes the pack, not what a task can execute.
v8.4.0LGPL-2.1-onlysimpilot-solver-su2
- external aerodynamics and coefficient tracking
- compressible, incompressible, RANS, Euler, and elasticity application routing
- marker-driven boundary-condition generation from typed patch roles
- benchmark-oriented validation using local SU2 tutorial and test-case resources
- Verify the mesh file exists and marker tags match every boundary-condition declaration.
- Confirm the solver family and turbulence model match the frozen flow regime and fidelity target.
- Start new cases with conservative CFL and restart only from a mesh-consistent snapshot.
- Ensure history output captures the force coefficients and convergence channels required by the V&V plan.
5 knowledge packs3 field declarations2 figure bindings
- su2
- gmsh
- pyvista
- cadquery
- freecad
- su2/pressure-coefficient
- su2/mach-number
- su2/eddy-viscosity
- su2.pressure-coefficient.wing
- su2.mach-slice.midspan
SU2 ONERA M6 transonic wing RANS benchmark