improve examples

Author: ufechner7

examples/ram_air_kite.jl

@@ -2,8 +2,9 @@ using VortexStepMethod
 using LinearAlgebra
 using Pkg
 
-if ! ("CSV" ∈ keys(Pkg.project().dependencies))
-    using TestEnv; TestEnv.activate()
+if !("CSV" ∈ keys(Pkg.project().dependencies))
+    using TestEnv
+    TestEnv.activate()
 end
 using CSV
 using DataFrames
@@ -50,7 +51,7 @@ plot && plot_geometry(
 )
 
 # Solving and plotting distributions
-@time results = solve(VSM, body_aero)
+results = solve(VSM, body_aero)
 @time results = solve(VSM, body_aero)
 
 CAD_y_coordinates = [panel.aerodynamic_center[2] for panel in body_aero.panels]

examples/rectangular_wing.jl

@@ -8,7 +8,7 @@ plot = true
 n_panels = 20          # Number of panels
 span = 20.0            # Wing span [m]
 chord = 1.0            # Chord length [m]
-v_a = 20.0            # Magnitude of inflow velocity [m/s]
+v_a = 20.0             # Magnitude of inflow velocity [m/s]
 density = 1.225        # Air density [kg/m³]
 alpha_deg = 30.0       # Angle of attack [degrees]
 alpha = deg2rad(alpha_deg)