replace plot with PLOT

Author: ufechner7

examples/ram_air_kite.jl

@@ -10,7 +10,7 @@ end
 using CSV
 using DataFrames
 
-plot = true
+PLOT = true
 
 # Create wing geometry
 wing = KiteWing("data/ram_air_kite_body.obj", "data/ram_air_kite_foil.dat")
@@ -36,7 +36,7 @@ vel_app = [
 set_va!(body_aero, vel_app)
 
 # Plotting geometry
-plot && plot_geometry(
+PLOT && plot_geometry(
     body_aero,
     "";
     data_type=".svg",
@@ -53,7 +53,7 @@ results = solve(vsm_solver, body_aero)
 
 body_y_coordinates = [panel.aero_center[2] for panel in body_aero.panels]
 
-plot && plot_distribution(
+PLOT && plot_distribution(
     [body_y_coordinates],
     [results],
     ["VSM"];
@@ -63,7 +63,7 @@ plot && plot_distribution(
     is_show=true
 )
 
-plot && plot_polars(
+PLOT && plot_polars(
     [vsm_solver],
     [body_aero],
     [

examples/rectangular_wing.jl

@@ -2,7 +2,7 @@ using LinearAlgebra
 using ControlPlots
 using VortexStepMethod
 
-plot = true
+PLOT = true
 
 # Step 1: Define wing parameters
 n_panels = 20          # Number of panels
@@ -53,7 +53,7 @@ println("CD = $(round(results_vsm["cd"], digits=4))")
 println("Projected area = $(round(results_vsm["projected_area"], digits=4)) m²")
 
 # Step 6: Plot geometry
-plot && plot_geometry(
+PLOT && plot_geometry(
       wa,
       "Rectangular_wing_geometry";
       data_type=".pdf",
@@ -65,7 +65,7 @@ plot && plot_geometry(
 # Step 7: Plot spanwise distributions
 y_coordinates = [panel.aero_center[2] for panel in wa.panels]
 
-plot && plot_distribution(
+PLOT && plot_distribution(
     [y_coordinates, y_coordinates],
     [results_vsm, results_llt],
     ["VSM", "LLT"],
@@ -74,7 +74,7 @@ plot && plot_distribution(
 
 # Step 8: Plot polar curves
 angle_range = range(0, 20, 20)
-plot && plot_polars(
+PLOT && plot_polars(
     [llt_solver, vsm_solver],
     [wa, wa],
     ["LLT", "VSM"];