New file precompile.jl

Author: ufechner7

src/VortexStepMethod.jl

@@ -254,46 +254,7 @@ include("panel.jl")
 include("body_aerodynamics.jl")
 include("wake.jl")
 include("solver.jl")
+include("precompile.jl")
 
-@setup_workload begin
-    # Putting some things in `@setup_workload` instead of `@compile_workload` can reduce the size of the
-    # precompile file and potentially make loading faster.
-    # list = [OtherType("hello"), OtherType("world!")]
-    path = dirname(pathof(@__MODULE__))
-
-    @compile_workload begin
-        # all calls in this block will be precompiled, regardless of whether
-        # they belong to your package or not (on Julia 1.8 and higher)
-        # Step 1: Define wing parameters
-        n_panels = 20          # Number of panels
-        span = 20.0            # Wing span [m]
-        chord = 1.0            # Chord length [m]
-        v_a = 20.0             # Magnitude of inflow velocity [m/s]
-        density = 1.225        # Air density [kg/m³]
-        alpha_deg = 30.0       # Angle of attack [degrees]
-        alpha = deg2rad(alpha_deg)
-
-        # Step 2: Create wing geometry with linear panel distribution
-        wing = Wing(n_panels, spanwise_panel_distribution=LINEAR)
-
-        # Add wing sections - defining only tip sections with inviscid airfoil model
-        add_section!(wing, 
-            [0.0, span/2, 0.0],    # Left tip LE 
-            [chord, span/2, 0.0],  # Left tip TE
-            INVISCID)
-        add_section!(wing, 
-            [0.0, -span/2, 0.0],   # Right tip LE
-            [chord, -span/2, 0.0], # Right tip TE
-            INVISCID)
-
-        # Step 3: Initialize aerodynamics
-        body_aero::BodyAerodynamics = BodyAerodynamics([wing])
-
-        gamma_initial = zeros(length(body_aero.panels))
-        calculate_circulation_distribution_elliptical_wing(gamma_initial, body_aero)
-
-        nothing
-    end
-end
 
 end # module

src/precompile.jl

@@ -0,0 +1,40 @@
+@setup_workload begin
+    # Putting some things in `@setup_workload` instead of `@compile_workload` can reduce the size of the
+    # precompile file and potentially make loading faster.
+    # list = [OtherType("hello"), OtherType("world!")]
+    path = dirname(pathof(@__MODULE__))
+
+    @compile_workload begin
+        # all calls in this block will be precompiled, regardless of whether
+        # they belong to your package or not (on Julia 1.8 and higher)
+        # Step 1: Define wing parameters
+        n_panels = 20          # Number of panels
+        span = 20.0            # Wing span [m]
+        chord = 1.0            # Chord length [m]
+        v_a = 20.0             # Magnitude of inflow velocity [m/s]
+        density = 1.225        # Air density [kg/m³]
+        alpha_deg = 30.0       # Angle of attack [degrees]
+        alpha = deg2rad(alpha_deg)
+
+        # Step 2: Create wing geometry with linear panel distribution
+        wing = Wing(n_panels, spanwise_panel_distribution=LINEAR)
+
+        # Add wing sections - defining only tip sections with inviscid airfoil model
+        add_section!(wing, 
+            [0.0, span/2, 0.0],    # Left tip LE 
+            [chord, span/2, 0.0],  # Left tip TE
+            INVISCID)
+        add_section!(wing, 
+            [0.0, -span/2, 0.0],   # Right tip LE
+            [chord, -span/2, 0.0], # Right tip TE
+            INVISCID)
+
+        # Step 3: Initialize aerodynamics
+        body_aero::BodyAerodynamics = BodyAerodynamics([wing])
+
+        gamma_initial = zeros(length(body_aero.panels))
+        calculate_circulation_distribution_elliptical_wing(gamma_initial, body_aero)
+
+        nothing
+    end
+end