fix/ improve comments

Author: ufechner7

src/kite_geometry.jl

@@ -204,7 +204,9 @@ mutable struct KiteWing <: AbstractWing
     te_interp::Extrapolation
     area_interp::Extrapolation
 
-    function KiteWing(obj_path, dat_path; alpha=0.0, n_sections=20, crease_frac=0.75, wind_vel=10., mass=1.0, n_panels=54, spanwise_panel_distribution=:linear, spanwise_direction=[0.0, 1.0, 0.0])
+    function KiteWing(obj_path, dat_path; alpha=0.0, n_sections=20, crease_frac=0.75, wind_vel=10., mass=1.0, 
+        n_panels=54, spanwise_panel_distribution=:linear, spanwise_direction=[0.0, 1.0, 0.0])
+        
         !isapprox(spanwise_direction, [0.0, 1.0, 0.0]) && @error "Spanwise direction has to be [0.0, 1.0, 0.0]"
 
         # Load or create polars

src/panel.jl

@@ -414,14 +414,16 @@ Calculate the velocity induced by a vortex ring at a control point.
 end
 
 """
-    calculate_velocity_induced_bound_2D!(panel::Panel, evaluation_point::Vector{Float64})
+    calculate_velocity_induced_bound_2D!(U2D, panel::Panel, evaluation_point, work_vectors)
 
 Calculate velocity induced by bound vortex filaments at the control point.
 Only needed for VSM, as LLT bound and filament align, thus no induced velocity.
 
 # Arguments
+- U_2D: unclear
 - `panel::Panel`: Panel object
-- `evaluation_point::Vector{Float64}`: Point where induced velocity is evaluated
+- `evaluation_point`: Point where induced velocity is evaluated
+- work_vectors: unclear
 
 # Returns
 - `Vector{Float64}`: Induced velocity at the control point