@@ -99,24 +99,24 @@ path_cfd_lebesque = joinpath(
9999 " V3_CL_CD_RANS_Lebesque_2024_Rey_300e4.csv"
100100)
101101
102- plot_polars (
103- [VSM, VSM_with_stall_correction],
104- [wing_aero_CAD_19ribs, wing_aero_CAD_19ribs],
105- [
106- " VSM CAD 19ribs" ,
107- " VSM CAD 19ribs , with stall correction" ,
108- " CFD_Lebesque Rey 30e5"
109- ];
110- literature_path_list= [path_cfd_lebesque],
111- angle_range= range (0 , 25 , length= 25 ),
112- angle_type= " angle_of_attack" ,
113- angle_of_attack= 0 ,
114- side_slip= 0 ,
115- yaw_rate= 0 ,
116- Umag= 10 ,
117- title= " tutorial_testing_stall_model_n_panels_$(n_panels) _distribution_$(spanwise_panel_distribution) " ,
118- data_type= " .pdf" ,
119- save_path= joinpath (save_folder, " polars" ),
120- is_save= true ,
121- is_show= true
122- )
102+ # plot_polars(
103+ # [VSM, VSM_with_stall_correction],
104+ # [wing_aero_CAD_19ribs, wing_aero_CAD_19ribs],
105+ # [
106+ # "VSM CAD 19ribs",
107+ # "VSM CAD 19ribs , with stall correction",
108+ # "CFD_Lebesque Rey 30e5"
109+ # ];
110+ # literature_path_list=[path_cfd_lebesque],
111+ # angle_range=range(0, 25, length=25),
112+ # angle_type="angle_of_attack",
113+ # angle_of_attack=0,
114+ # side_slip=0,
115+ # yaw_rate=0,
116+ # Umag=10,
117+ # title="tutorial_testing_stall_model_n_panels_$(n_panels)_distribution_$(spanwise_panel_distribution)",
118+ # data_type=".pdf",
119+ # save_path=joinpath(save_folder, "polars"),
120+ # is_save=true,
121+ # is_show=true
122+ # )
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