Fix tests

Author: ufechner7

test/bench.jl

@@ -44,7 +44,8 @@ using LinearAlgebra
     set_va!(body_aero, vel_app)
 
     # Initialize solvers for both LLT and VSM methods
-    solver = Solver()
+    P = length(body_aero.panels)
+    solver = Solver{P}()
 
     # Pre-allocate arrays
     gamma = rand(n_panels)
@@ -112,8 +113,9 @@ using LinearAlgebra
                     aero_model,
                     aero_data)
                 body_aero = BodyAerodynamics([wing])
-
-                solver = Solver(
+                
+                P = length(body_aero.panels)
+                solver = Solver{P}(
                     aerodynamic_model_type=model
                 )
                 result = @benchmark gamma_loop(

test/test_body_aerodynamics.jl

@@ -145,7 +145,8 @@ end
     set_va!(body_aero, v_a)
 
     # Run analysis
-    solver_object = Solver(
+    P = length(body_aero.panels)
+    solver_object = Solver{P}(
         aerodynamic_model_type=model, 
         core_radius_fraction=core_radius_fraction
     )

test/test_plotting.jl

@@ -63,8 +63,9 @@ plt.ioff()
         rm("/tmp/Rectangular_wing_geometry_top_view.pdf")
 
         # Step 5: Initialize the solvers
-        vsm_solver = Solver(aerodynamic_model_type=VSM)
-        llt_solver = Solver(aerodynamic_model_type=LLT)
+        P = length(body_aero.panels)
+        vsm_solver = Solver{P}(aerodynamic_model_type=VSM)
+        llt_solver = Solver{P}(aerodynamic_model_type=LLT)
 
         # Step 6: Solve the VSM and LLT
         results_vsm = solve(vsm_solver, body_aero)