From 3daf9f7e271fd7caa98673b122aeac2b6c23ab23 Mon Sep 17 00:00:00 2001
From: Thomas Lambert <dev@tlambert.be>
Date: Wed, 15 Mar 2023 13:44:20 +0100
Subject: [PATCH] doc(nacacamber): fix output details
---
+af_tools/nacacamber.m | 16 ++++++++--------
1 file changed, 8 insertions(+), 8 deletions(-)
diff --git a/+af_tools/nacacamber.m b/+af_tools/nacacamber.m
index 94ec3b8..ab13a45 100644
--- a/+af_tools/nacacamber.m
+++ b/+af_tools/nacacamber.m
@@ -6,13 +6,13 @@ function [coord, gradY] = nacacamber(varargin)
% -----
%
% Usage:
- % [X, Y] = NACACAMBER prompts the user for the airfoil digits, then calculates the coordinates
- % of the camberline using 100 points spaced with the half-cosine rule.
+ % [coord, gradY] = NACACAMBER prompts the user for the airfoil digits, then calculates the
+ % coordinates of the camberline using 100 points spaced with the half-cosine rule.
%
- % [X, Y] = NACACAMBER(DIGITS) calculates the coordinates of the camberline for the NACA
- % airfoil specified by DIGITS, without further input.
+ % [coord, gradY] = NACACAMBER(DIGITS) calculates the coordinates of the camberline for the
+ % NACA airfoil specified by DIGITS, without further input.
%
- % [X, Y] = NACACAMBER(DIGITS, NPOINTS) calculates the coordinates of the NACA airfoil
+ % [coord, gradY] = NACACAMBER(DIGITS, NPOINTS) calculates the coordinates of the NACA airfoil
% specified by DIGITS, using NPOINTS points spaced with the half-cosine rule.
%
% [...] = NACACAMBER(..., 'spacing', SP) uses the defined spacing rule to determine to
@@ -20,14 +20,14 @@ function [coord, gradY] = nacacamber(varargin)
% 'linear' - linear
% 'halfcosine' - (default) finer at leading and trailing edges
% 'cosine' - finer at leading edge, coarser at the trailing edge
+ % 'sine' - finer at trailing edge, coarser at the leading edge
%
% Inputs:
% digits : Character vector representing the NACA airfoil (ex: '0012', '24120', '24012')
% nPoints : Number of output coordinates
%
% Output:
- % xc : Camberline X coordinates (0 <= X <= 1)
- % yc : Camberline Y coordinates
+ % coord : Camberline coordinates [nPts x 2]
% gradY : Gradient of Y (required to get the whole airfoil coordinates)
%
% Example:
@@ -41,7 +41,7 @@ function [coord, gradY] = nacacamber(varargin)
% <a href="https://gitlab.uliege.be/am-dept/matlab_airfoil_toolbox">Documentation (online)</a>
% -------------------------------------------
- % (c) Copyright 2022 University of Liege
+ % (c) Copyright 2022-2023 University of Liege
% Author: Thomas Lambert <t.lambert@uliege.be>
% ULiege - Aeroelasticity and Experimental Aerodynamics
% MIT License
--
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