add lift and drag f(aoa) plots

aenarete · Aug 13, 2024 · 0efc96e · 0efc96e
1 parent 574cc00
commit 0efc96e
Showing 1 changed file with 11 additions and 3 deletions.
diff --git a/examples/plots.jl b/examples/plots.jl
@@ -201,9 +201,17 @@ function plot_aerodynamics(plot_lift_drag = false)
     sl    = log.syslog
 
     if plot_lift_drag
-        display(plotx(sl.time, sl.var_08, sl.var_13, sl.var_14, sl.var_15, sl.var_16; 
-        ylabels=["LoD [-]", L"\alpha_2~[°]", "Lift [N]",  "Drag [N]"],
-        fig="aerodynamics"))
+        display(plotx(sl.time, sl.var_08, sl.var_13, sl.var_15, sl.var_16; 
+                      ylabels=["LoD [-]", L"\alpha_2~[°]", "Lift [N]",  "Drag [N]"],
+                      fig="aerodynamics"))
+        display(plotxy(sl.var_13[2:end], sl.var_15[2:end]; 
+                      xlabel="AoA [°]",
+                      ylabel="Lift [N]",
+                      fig="Lift as function of AoA"))
+        display(plotxy(sl.var_13[2:end], sl.var_16[2:end]; 
+                      xlabel="AoA [°]",
+                      ylabel="Drag [N]",
+                      fig="Drag as function of AoA"))
     else
         display(plotx(sl.time, sl.var_08, sl.var_13, sl.var_14, sl.var_15, sl.var_16; 
                     ylabels=["LoD [-]", L"\alpha_2~[°]", L"\alpha_{3b}~[°]", L"\alpha_{4b}~[°]"],