List plot_section_polars under Added in the changelog

Co-Authored-By: Claude Opus 5 <noreply@anthropic.com>

Author: 1-Bort-1

CHANGELOG.md

@@ -8,16 +8,16 @@
   doi:10.1088/1742-6596/2767/2/022068): each section gets a drag increment and a force
   along its span from the flow across it, in `solve!`, `solve` and `linearize`. Opt-in
   via `is_with_viscous_drag_correction` (default `false`) on the solver settings.
+- `plot_section_polars(body_aero; panels, alphas, delta)` draws cl, cd and cm against α
+  per panel through `calculate_cl`/`calculate_cd`/`calculate_cm`, for every aero model
+  and at flap deflection `delta`, in one figure instead of one coefficient per call.
 
 ### Changed
 
 - Requires Julia 1.12 or 1.13; 1.10 and 1.11 keep resolving v5.1.1.
 - The Makie `plot!` methods for a `Panel` or a `BodyAerodynamics` return a
   `Vector{Makie.AbstractPlot}` instead of a `Vector{Any}`; for a `BodyAerodynamics`
   drawn as flat panels it is one flat list rather than a list per panel.
-- BREAKING - `plot_section_polars(body_aero; panels, alphas, delta)` draws cl, cd and cm
-  against α per panel through `calculate_cl`/`calculate_cd`/`calculate_cm`, for every
-  aero model and at flap deflection `delta`; the `coefficient` argument is removed.
 
 ### Fixed