From 5ef8c9ed6f0dbd698dd31af82edf5dae92d3c186 Mon Sep 17 00:00:00 2001
From: Thomas Lambert <t.lambert@uliege.be>
Date: Tue, 6 Sep 2022 11:11:22 +0200
Subject: [PATCH] refact(Polar): make all properties SetAccess private
---
+af_tools/@Polar/Polar.m | 4 +---
1 file changed, 1 insertion(+), 3 deletions(-)
diff --git a/+af_tools/@Polar/Polar.m b/+af_tools/@Polar/Polar.m
index 0bb533c..8f47b38 100644
--- a/+af_tools/@Polar/Polar.m
+++ b/+af_tools/@Polar/Polar.m
@@ -68,7 +68,7 @@ classdef Polar
% Issues: https://gitlab.uliege.be/am-dept/matlab_airfoil_toolbox/-/issues
% ----------------------------------------------------------------------------------------------
- properties
+ properties (SetAccess = private)
reynolds (1, :) double {mustBeNonnegative} % Rynolds number, [-]
mach (1, :) double {mustBeNonnegative} % Mach number, [-]
nCrit (1, :) double {mustBeNonnegative} % nCrit number, [-]
@@ -76,9 +76,7 @@ classdef Polar
cl (:, :) double {mustBeReal} % Lift coefficient, [-]
cd (:, :) double {mustBeReal} % Drag coefficient, [-]
cm (:, :) double {mustBeReal} % Moment coefficient, [-]
- end
- properties (SetAccess = private)
Ext = struct('aoa', [], 'cl', [], 'cd', [], 'cm', []) % Extended polar data
Stall = struct('aoa', [], 'cl', [], 'cd', []) % Stall point data
Zero = struct('aoa', [], 'cd', []) % Zero-lift point data
--
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