refactor(nacacamber): use spacedvector

+af_tools/nacacamber.m

@@ -107,12 +107,14 @@ function [xc, yc, gradY] = camber4digits(digits, nPoints, spacing)
 %   P  = Position of the max camber divided by 10
 %   XX = Maximum thickness divided by 100
 
+import af_tools.utils.spacedvector;
+
 % Airfoil parameters
 m = str2double(digits(1)) /100;
 p = str2double(digits(2)) /10;
 
 % Camberline
-xc = getxc(spacing, nPoints);
+xc = spacedvector(spacing, nPoints);
 yc = zeros(size(xc));
 gradY = zeros(size(xc));
 
@@ -139,13 +141,15 @@ function [xc, yc, gradY] = camber5digits(digits, nPoints, spacing)
 %   Q = Camber line (0=standard, 1=reflex)
 %   XX = Maximum thickness divided by 100
 
+import af_tools.utils.spacedvector;
+
 % Airfoil parameters
 cld = str2double(digits(1)) *3/20;
 p = str2double(digits(2)) /20;
 q = str2double(digits(3));
 
 % Camberline
-xc = getxc(spacing, nPoints);
+xc = spacedvector(spacing, nPoints);
 yc = zeros(size(xc));
 gradY = zeros(size(xc));
 
@@ -177,24 +181,6 @@ yc = (cld/0.3) * yc;
 end
 
 
-% ------------------------------------------------------------------------------
-function xc = getxc(spacing, nPoints)
-% GETXC Returns xc vector based on chosen spacing and number of points
-
-switch spacing
-    case 'linear'
-        xc = linspace(0, 1, (nPoints));
-    case 'halfcosine'
-        beta = linspace(0, pi, (nPoints));
-        xc = (1-cos(beta))/2;
-    case 'cosine'
-        beta = linspace(0, pi/2, (nPoints));
-        xc = 1-cos(beta);
-end
-
-end
-
-
 % ------------------------------------------------------------------------------
 function [r,k1,k2k1] = getcoeffs5digits(q, p)
 % GETCOEFFS5DIGITS Outputs the value of the various coefficients used in the NACA 5digits formula.

CHANGELOG.md

@@ -19,23 +19,39 @@ and this project adheres to [Semantic Versioning](https://semver.org/spec/v2.0.0
 
 ### Security
 
+## [1.2.0] - 2022-04-10
+
+### Added
+
+- **uiuccleaner**: Add `refine` option to allow the refining of the  original
+  datafile (spline interpolation to add more points).
+
+### Changed
+
+- Refactor of spacing function (**nacacamber**, **uiuccleaner**).
+
+### Fixed
+
+- **utils.parsefileinputs**: minor fix in case inputFiles is a cell array
+
 ## [1.1.0] - 2022-04-10
 
 ### Added
 
-- Added `savedat` option for _nacaairfoil_
-- **Added uiuccleaner function**
+- **nacaairfoil**: Added `savedat` option
+- **Added uiuccleaner function**.
 
 ### Changed
 
-- Coordinates outputted by _nacaairfoil_ now start at TE, go along upper side to
-  LE, then go along lower side back to TE
-- Refactor input parsing for xf2mat
+- **nacaairfoil**: Coordinates outputted now start at TE, go along upper side to
+  LE, then go along lower side back to TE.
+- **xf2mat**: Refactor input parsing.
 
 ## [1.0.0] - 2022-04-08
 
 - Initial release
 
 [Unreleased]: https://gitlab.uliege.be/am-dept/matlab_airfoil_toolbox/-/compare/v1.0.0...master
+[1.2.0]: https://gitlab.uliege.be/am-dept/matlab_airfoil_toolbox/-/compare/v1.1.0...v1.2.0
 [1.1.0]: https://gitlab.uliege.be/am-dept/matlab_airfoil_toolbox/-/compare/v1.0.0...v1.1.0
 [1.0.0]: https://gitlab.uliege.be/am-dept/matlab_airfoil_toolbox/-/releases/v1.0.0