Update V3_kite.jl

Author: ufechner7

examples/V3_kite.jl

@@ -2,8 +2,10 @@ using LinearAlgebra
 using VortexStepMethod
 
 PLOT = true
+SAVE_ALL = false
 USE_TEX = false
 DEFORM = false
+OUTPUT_DIR = joinpath(dirname(@__DIR__), "output")
 
 project_dir = dirname(@__DIR__)
 literature_paths = [
@@ -118,8 +120,8 @@ PLOT && plot_polars(
     side_slip=sideslip_deg,
     v_a=wind_speed,
     title="$(wing.n_panels)_panels_$(wing.spanwise_distribution)_from_yaml_settings",
-    data_type=".pdf",
-    is_save=false,
+    save_path=OUTPUT_DIR,
+    is_save=false || SAVE_ALL,
     is_show=true,
     use_tex=USE_TEX,
     show_moments=true
@@ -128,10 +130,10 @@ PLOT && plot_polars(
 # Plotting geometry
 PLOT && plot_geometry(
     body_aero,
-    "";
-    data_type=".svg",
-    save_path="",
-    is_save=false,
+    "V3 kite geometry";
+    data_type=".pdf",
+    save_path=OUTPUT_DIR,
+    is_save=false || SAVE_ALL,
     is_show=true,
     view_elevation=15,
     view_azimuth=-120,
@@ -147,8 +149,8 @@ PLOT && plot_distribution(
     [results],
     ["VSM"];
     title="CAD_spanwise_distributions_alpha_$(round(angle_of_attack_deg, digits=1))_delta_$(round(sideslip_deg, digits=1))_yaw_$(round(yaw_rate, digits=1))_v_a_$(round(wind_speed, digits=1))",
-    data_type=".pdf",
-    is_save=false,
+    save_path=OUTPUT_DIR,
+    is_save=false || SAVE_ALL,
     is_show=true,
     use_tex=USE_TEX
 )
@@ -193,7 +195,8 @@ PLOT && plot_polars(
     v_a=wind_speed,
     title="LOOP solver",
     show_moments=true,
-    is_save=false,
+    save_path=OUTPUT_DIR,
+    is_save=false || SAVE_ALL,
     is_show=true,
     use_tex=USE_TEX
 )
@@ -211,7 +214,8 @@ PLOT && plot_polars(
     v_a=wind_speed,
     title="beta sweep",
     show_moments=true,
-    is_save=false,
+    save_path=OUTPUT_DIR,
+    is_save=false || SAVE_ALL,
     is_show=true,
     use_tex=USE_TEX
 )