succesful plotting of stall model

Author: 1-Bart-1

examples/testing_stall_model.jl

@@ -99,24 +99,24 @@ path_cfd_lebesque = joinpath(
     "V3_CL_CD_RANS_Lebesque_2024_Rey_300e4.csv"
 )
 
-# plot_polars(
-#     [VSM, VSM_with_stall_correction],
-#     [wing_aero_CAD_19ribs, wing_aero_CAD_19ribs],
-#     [
-#         "VSM CAD 19ribs",
-#         "VSM CAD 19ribs , with stall correction",
-#         "CFD_Lebesque Rey 30e5"
-#     ];
-#     literature_path_list=[path_cfd_lebesque],
-#     angle_range=range(0, 25, length=25),
-#     angle_type="angle_of_attack",
-#     angle_of_attack=0,
-#     side_slip=0,
-#     yaw_rate=0,
-#     Umag=10,
-#     title="tutorial_testing_stall_model_n_panels_$(n_panels)_distribution_$(spanwise_panel_distribution)",
-#     data_type=".pdf",
-#     save_path=joinpath(save_folder, "polars"),
-#     is_save=true,
-#     is_show=true
-# )
+plot_polars(
+    [VSM, VSM_with_stall_correction],
+    [wing_aero_CAD_19ribs, wing_aero_CAD_19ribs],
+    [
+        "VSM CAD 19ribs",
+        "VSM CAD 19ribs , with stall correction",
+        "CFD_Lebesque Rey 30e5"
+    ];
+    literature_path_list=[path_cfd_lebesque],
+    angle_range=range(0, 25, length=25),
+    angle_type="angle_of_attack",
+    angle_of_attack=0,
+    side_slip=0,
+    yaw_rate=0,
+    Umag=10,
+    title="tutorial_testing_stall_model_n_panels_$(n_panels)_distribution_$(spanwise_panel_distribution)",
+    data_type=".pdf",
+    save_path=joinpath(save_folder, "polars"),
+    is_save=true,
+    is_show=true
+)

results/TUDELFT_V3_LEI_KITE/polars/$C_L$ vs $C_D$.pdf

@@ -557,8 +557,9 @@ function plot_polars(
             # Read all data first
             data = readdlm(path, ',')
             # Skip the header row by taking data from row 2 onwards
+            @show data[1, :]
             data = data[2:end, :]
-            push!(polar_data_list, [data[:,3], data[:,1], data[:,2]])
+            push!(polar_data_list, [data[:,3], data[:,1], data[:,2], zeros(length(data[:,1]))])
         end
     end