Refactoring

Author: ufechner7

src/solver.jl

@@ -400,7 +400,6 @@ function solve_base(solver::Solver, body_aero::BodyAerodynamics, gamma_distribut
     gamma_loop!(
         solver,
         body_aero,
-        solver.sol.chord_array,
         solver.sol.x_airf_array,
         solver.sol.y_airf_array,
         solver.sol.z_airf_array,
@@ -415,7 +414,6 @@ function solve_base(solver::Solver, body_aero::BodyAerodynamics, gamma_distribut
         gamma_loop!(
             solver,
             body_aero,
-            solver.sol.chord_array,
             solver.sol.x_airf_array,
             solver.sol.y_airf_array,
             solver.sol.z_airf_array,
@@ -451,7 +449,6 @@ Main iteration loop for calculating circulation distribution.
 function gamma_loop!(
     solver::Solver,
     body_aero::BodyAerodynamics,
-    chord_array::Vector{Float64},
     x_airf_array::Matrix{Float64},
     y_airf_array::Matrix{Float64},
     z_airf_array::Matrix{Float64},
@@ -460,6 +457,7 @@ function gamma_loop!(
     log::Bool = true
 )
     va_array = solver.sol.va_array
+    chord_array = solver.sol.chord_array
     solver.lr.converged   = false
     n_panels    = length(body_aero.panels)
     solver.lr.alpha_array .= body_aero.alpha_array

test/bench.jl

@@ -119,10 +119,10 @@ using LinearAlgebra
                     aerodynamic_model_type=model
                 )
                 solver.sol.va_array .= va_array
+                solver.sol.chord_array .= chord_array
                 result = @benchmark gamma_loop!(
                     $solver,
                     $body_aero,
-                    $chord_array,
                     $x_airf_array,
                     $y_airf_array,
                     $z_airf_array,