Refactoring

Author: ufechner7

src/solver.jl

@@ -27,7 +27,7 @@ Struct for storing the solution of the [solve!](@ref) function. Must contain all
     ### private vectors of solve_base!
     _x_airf_array::Matrix{Float64} = zeros(P, 3)
     _y_airf_array::Matrix{Float64} = zeros(P, 3)
-    z_airf_array::Matrix{Float64} = zeros(P, 3)
+    _z_airf_array::Matrix{Float64} = zeros(P, 3)
     va_array::Matrix{Float64} = zeros(P, 3)
     chord_array::Vector{Float64} = zeros(P)
     ###
@@ -210,7 +210,7 @@ function solve!(solver::Solver, body_aero::BodyAerodynamics, gamma_distribution=
             body_aero,
             gamma_new,
             solver.core_radius_fraction,
-            solver.sol.z_airf_array,
+            solver.sol._z_airf_array,
             solver.sol._x_airf_array,
             solver.sol.va_array,
             solver.br.va_norm_array,
@@ -340,7 +340,7 @@ function solve(solver::Solver, body_aero::BodyAerodynamics, gamma_distribution=n
         solver.sol.chord_array,
         solver.sol._x_airf_array,
         solver.sol._y_airf_array,
-        solver.sol.z_airf_array,
+        solver.sol._z_airf_array,
         solver.sol.va_array,
         solver.br.va_norm_array,
         solver.br.va_unit_array,
@@ -370,15 +370,15 @@ function solve_base!(solver::Solver, body_aero::BodyAerodynamics, gamma_distribu
     # Clear arrays
     solver.sol._x_airf_array .= 0
     solver.sol._y_airf_array .= 0
-    solver.sol.z_airf_array .= 0
+    solver.sol._z_airf_array .= 0
     solver.sol.va_array .= 0
     solver.sol.chord_array .= 0
 
     # Fill arrays from panels
     for (i, panel) in enumerate(panels)
         solver.sol._x_airf_array[i, :] .= panel.x_airf
         solver.sol._y_airf_array[i, :] .= panel.y_airf
-        solver.sol.z_airf_array[i, :] .= panel.z_airf
+        solver.sol._z_airf_array[i, :] .= panel.z_airf
         solver.sol.va_array[i, :] .= panel.va
         solver.sol.chord_array[i] = panel.chord
     end
@@ -437,7 +437,7 @@ function gamma_loop!(
     chord_array = solver.sol.chord_array
     x_airf_array = solver.sol._x_airf_array
     y_airf_array = solver.sol._y_airf_array
-    z_airf_array = solver.sol.z_airf_array
+    z_airf_array = solver.sol._z_airf_array
     solver.lr.converged   = false
     n_panels    = length(body_aero.panels)
     solver.lr.alpha_array .= body_aero.alpha_array

test/bench.jl

@@ -132,7 +132,7 @@ using LinearAlgebra
                 solver.sol.chord_array .= chord_array
                 solver.sol._x_airf_array .= x_airf_array
                 solver.sol._y_airf_array .= y_airf_array
-                solver.sol.z_airf_array .= z_airf_array
+                solver.sol._z_airf_array .= z_airf_array
                 result = @benchmark gamma_loop!(
                     $solver,
                     $body_aero,