cfd-convergencelisted
Install: claude install-skill ashfordeOU/aero-agent-skills
# CFD Convergence Checks (aerodynamics/cfd/cfd-convergence)
Use when the task is judging computational fluid dynamics
convergence: residual behavior, Courant number stability, and mesh
refinement stability of the answer.
## Domain quick reference
- A converged run has residuals below tolerance and still
decreasing; oscillating or flat residuals mean the run is not
converged.
- The Courant number must respect the scheme stability limit:
about 1 for explicit schemes, higher for implicit schemes.
- Mesh refinement convergence compares the answer across mesh
levels; small change means the discretization error is bounded.
- Validation against classic data (NACA Report 824) anchors the
converged answer for airfoil cases.
## Workflow
1. Collect the residual history from the solver log.
2. Check convergence with residual_converged.
3. Confirm the Courant number with cfl_ok.
4. Compare mesh levels with mesh_refinement_ok.
5. Decide whether to trust the run.
## Pitfalls
- Calling a run converged on a flat residual plateau.
- Running explicit schemes at Courant numbers above the limit.
- Reporting an answer that changed on the next mesh level.
## Behavior contract (gate 3)
The residual, CFL, and mesh logic is exercised by the gate 3
contract test: scripts/test_cfd_convergence.py against
scripts/cfd_convergence_logic.py (stdlib unittest, offline). Run:
python3 scripts/test_cfd_convergence.py
## Compliance
- NACA Report 824 is US government work (public domain); summa