01
Geometry & flow
2 ELEMENTSSpeed / U∞
012≥3
⟶ U∞ 4.00°
02
Cp vs x/crefPressure distribution
03
Boundary-layer development
04
Solution Status
Boundary residual ‖Vn‖∞: —No-penetration equation error
ReadyLinear vortex panel baseline
Methods attempted
Computing flow field…
Build mesh, then Check grid. The harmonic comparison tests the SLOR target, including on an unsmoothed mesh.
Independent check details
The reference solves harmonic coordinates on the same fixed polygonal boundaries using a separate quadrilateral discretization, refined 1×, 2× and 4×. Limits: 0.05 local intervals for coordinate mismatch; 0.01 for the last reference change. These checks do not validate boundary placement, velocity continuity across dividing cuts or Euler/BL accuracy.