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Commit 887a35d

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Refactoring
1 parent 0612534 commit 887a35d

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2 files changed

+6
-6
lines changed

2 files changed

+6
-6
lines changed

src/solver.jl

Lines changed: 5 additions & 5 deletions
Original file line numberDiff line numberDiff line change
@@ -26,7 +26,7 @@ Struct for storing the solution of the [solve!](@ref) function. Must contain all
2626
@with_kw mutable struct VSMSolution{P}
2727
### private vectors of solve_base!
2828
_x_airf_array::Matrix{Float64} = zeros(P, 3)
29-
y_airf_array::Matrix{Float64} = zeros(P, 3)
29+
_y_airf_array::Matrix{Float64} = zeros(P, 3)
3030
z_airf_array::Matrix{Float64} = zeros(P, 3)
3131
va_array::Matrix{Float64} = zeros(P, 3)
3232
chord_array::Vector{Float64} = zeros(P)
@@ -339,7 +339,7 @@ function solve(solver::Solver, body_aero::BodyAerodynamics, gamma_distribution=n
339339
solver.lr.v_a_array,
340340
solver.sol.chord_array,
341341
solver.sol._x_airf_array,
342-
solver.sol.y_airf_array,
342+
solver.sol._y_airf_array,
343343
solver.sol.z_airf_array,
344344
solver.sol.va_array,
345345
solver.br.va_norm_array,
@@ -369,15 +369,15 @@ function solve_base!(solver::Solver, body_aero::BodyAerodynamics, gamma_distribu
369369

370370
# Clear arrays
371371
solver.sol._x_airf_array .= 0
372-
solver.sol.y_airf_array .= 0
372+
solver.sol._y_airf_array .= 0
373373
solver.sol.z_airf_array .= 0
374374
solver.sol.va_array .= 0
375375
solver.sol.chord_array .= 0
376376

377377
# Fill arrays from panels
378378
for (i, panel) in enumerate(panels)
379379
solver.sol._x_airf_array[i, :] .= panel.x_airf
380-
solver.sol.y_airf_array[i, :] .= panel.y_airf
380+
solver.sol._y_airf_array[i, :] .= panel.y_airf
381381
solver.sol.z_airf_array[i, :] .= panel.z_airf
382382
solver.sol.va_array[i, :] .= panel.va
383383
solver.sol.chord_array[i] = panel.chord
@@ -436,7 +436,7 @@ function gamma_loop!(
436436
va_array = solver.sol.va_array
437437
chord_array = solver.sol.chord_array
438438
x_airf_array = solver.sol._x_airf_array
439-
y_airf_array = solver.sol.y_airf_array
439+
y_airf_array = solver.sol._y_airf_array
440440
z_airf_array = solver.sol.z_airf_array
441441
solver.lr.converged = false
442442
n_panels = length(body_aero.panels)

test/bench.jl

Lines changed: 1 addition & 1 deletion
Original file line numberDiff line numberDiff line change
@@ -131,7 +131,7 @@ using LinearAlgebra
131131
solver.sol.va_array .= va_array
132132
solver.sol.chord_array .= chord_array
133133
solver.sol._x_airf_array .= x_airf_array
134-
solver.sol.y_airf_array .= y_airf_array
134+
solver.sol._y_airf_array .= y_airf_array
135135
solver.sol.z_airf_array .= z_airf_array
136136
result = @benchmark gamma_loop!(
137137
$solver,

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