diff --git a/+af_tools/+utils/lednicer.m b/+af_tools/+utils/lednicer.m
new file mode 100644
index 0000000000000000000000000000000000000000..8eecbf5d7a8bea31d23c2a64cdc7f3ed544b20e0
--- /dev/null
+++ b/+af_tools/+utils/lednicer.m
@@ -0,0 +1,20 @@
+function [coord, array] = lednicer(upper, lower)
+ % Lednicer Output airofil coordinates in the Lednicer format
+ % -----
+ % (c) Copyright 2022 University of Liege
+ % Author: Thomas Lambert <t.lambert@uliege.be>
+ % ULiege - Aeroelasticity and Experimental Aerodynamics
+ % Apache 2.0 License
+ % https://gitlab.uliege.be/am-dept/matlab_airfoil_toolbox
+
+ % ----------------------------------------------------------------------------------------------
+
+ coord = [upper; lower];
+
+ nPts = size(upper, 1);
+ array = num2str([nPts, nPts; coord], '%0.7f ');
+ sep = blanks(size(array, 2));
+
+ array = [array(1:size(upper, 1), :); sep; array(size(upper, 1) + 1:end, :)];
+
+end
diff --git a/+af_tools/+utils/selig.m b/+af_tools/+utils/selig.m
new file mode 100644
index 0000000000000000000000000000000000000000..f776cbf20ee85a20ff34284116268da00b53f510
--- /dev/null
+++ b/+af_tools/+utils/selig.m
@@ -0,0 +1,15 @@
+function [coord, array] = selig(upper, lower)
+ % SELIG Output airofil coordinates in the Selig format
+ % -----
+ % (c) Copyright 2022 University of Liege
+ % Author: Thomas Lambert <t.lambert@uliege.be>
+ % ULiege - Aeroelasticity and Experimental Aerodynamics
+ % Apache 2.0 License
+ % https://gitlab.uliege.be/am-dept/matlab_airfoil_toolbox
+
+ % ----------------------------------------------------------------------------------------------
+
+ coord = [flipud(upper); lower(2:end, :)];
+ array = num2str(coord, '%0.7f ');
+
+end
diff --git a/+af_tools/formatairfoilcoord.m b/+af_tools/formatairfoilcoord.m
new file mode 100644
index 0000000000000000000000000000000000000000..8bd986fb4b1cba1f7706feeb4baa26873d3ff7dc
--- /dev/null
+++ b/+af_tools/formatairfoilcoord.m
@@ -0,0 +1,255 @@
+function Dat = formatairfoilcoord(varargin)
+ % FORMATAIRFOILCOORD Re-format airfoil coordinates.
+ % The UIUC airfoil database from the University of Illinois gathers the coordinates for more
+ % than 1600 airfoils. Two different standards are used to represent the coordinates of the
+ % airfoil:
+ % - Selig: The first line is the name of the airfoil, and each line after that is a set of
+ % coordinates. The coordinates are ordered from the trailing edge, along the
+ % upper surface to the leading edge and back around the lower surface to trailing
+ % edge. This format is the most common one.
+ % - Lednicer: The first line is the name of the airfoil, the second one is the number of
+ % points on each side and the lines after that are the coordinates. The
+ % coordinates are given separately for the upper and lower surfaces, each from
+ % the leading edge to the trailing edge.
+ %
+ % Many engineering tools or application (such as XFOIL) rely on inputs in the Selig format
+ % only. This script was therefore created to reformat original data so they can be used easily
+ % with other tools.
+ %
+ % Even though the _Selig_ format is the default option, the script allows also the user to
+ % reformat _Selig_ files in _Lednicer_ form if needed. It also comes with the option to refine
+ % the coordinates by adding points with a spline interpolation following the half-cosine rule
+ % (more points are the leading and trailing edge). If that option is selected, the airfoil
+ % will be defined using 50 points for each surface.
+ %
+ % Note:
+ % This function can be used on many files at once in order to speed-up the process.
+ %
+ % <a href="https://gitlab.uliege.be/thlamb/airfoil_toolbox">Documentation (README)</a>
+ % <a href="https://gitlab.uliege.be/thlamb/airfoil_toolbox/-/issues">Report an issue</a>
+ % -----
+ %
+ % Usage:
+ % DAT = FORMATAIRFOILCOORD prompts the user for all inputs, then converts the coordinates to
+ % the Selig format.
+ %
+ % DAT = FORMATAIRFOILCOORD(INPUTDIR) converts all dat files found in INPUTDIR.
+ %
+ % DAT = FORMATAIRFOILCOORD(INPUTDIR, INPUTFILES) converts only the polars specified by
+ % INPUTFILES found in INPUTDIR.
+ %
+ % DAT = FORMATAIRFOILCOORD(..., 'autosave', true) saves the resulting coordinates in a new
+ % dat-file.
+ %
+ % DAT = FORMATAIRFOILCOORD(..., 'overwrite', true) saves the resulting coordinates by
+ % overwriting the original dat-file. If autosave is not specified but overwrite is true, the
+ % file will be overwritten anyway. If autosave is set to false and overwrite is true, the file
+ % will not be saved at all.
+ %
+ % DAT = FORMATAIRFOILCOORD(..., 'refine', true) refines the input data by using a spline
+ % interpolation with 100 coordinates in total, spaced following the half-cosine rule.
+ % False by default.
+ %
+ % DAT = FORMATAIRFOILCOORD(..., 'outputFormat', 'Lednicer') select the output format (Selig or
+ % Lednicer). Selig by default.
+ %
+ % Inputs:
+ % inputDir : Path of the directory with the UIUC oridinal dat-files
+ % inputFiles : Files to select (ex: '*' (default), '*0012*', {'file1','file2'}, etc)
+ %
+ % Output:
+ % Dat : A structure for the results for each input file.
+ % - Dat.file : original filename
+ % - Dat.format : Format of the output coordinates
+ % - Dat.airfoil : airfoil name, parsed from the input file
+ % - Dat.nPoints : Number of coordinates
+ % - Dat.coord : whole airfoil coordinates, with 0 <= X <= 1
+ % - Dat.upper : airfoil upper surface coordinates.
+ % - Dat.lower : airfoil lower surface coordinates.
+ %
+ % Example:
+ % FORMATAIRFOILCOORD
+ % FORMATAIRFOILCOORD('test_data')
+ % FORMATAIRFOILCOORD('test_data', '*0012*')
+ % FORMATAIRFOILCOORD('test_data', {'0012_re1e5', '0012_re1e6'})
+ % FORMATAIRFOILCOORD('test_data', 'autosave', true)
+ % FORMATAIRFOILCOORD('test_data', 'overwrite', true)
+ % FORMATAIRFOILCOORD('test_data', 'refine', true)
+ % FORMATAIRFOILCOORD('test_data', 'outputFormat', 'Lednicer')
+ %
+ % See also: NACAAIRFOIL.
+ %
+ % -----
+ % UIUC Airfoil Database: https://m-selig.ae.illinois.edu/ads/coord_database.html
+ % -----
+ % (c) Copyright 2022 University of Liege
+ % Author: Thomas Lambert <t.lambert@uliege.be>
+ % ULiege - Aeroelasticity and Experimental Aerodynamics
+ % Apache 2.0 License
+ % https://gitlab.uliege.be/am-dept/matlab_airfoil_toolbox
+
+ % ----------------------------------------------------------------------------------------------
+
+ narginchk(0, 8);
+
+ % Import other functions from this package
+ import af_tools.utils.*
+
+ % Constants and defaults
+ OPTION_LIST = {'autosave', 'overwrite', 'refine', 'outputFormat'};
+ FILETYPE = '.dat';
+ REFINED_SPACING = 'halfcosine';
+ REFINED_NPOINTS = ceil((100 + 1) / 2);
+
+ % Parse inputs
+ [allFileNames, fullpath, idxOpts] = parsefileinputs(OPTION_LIST, FILETYPE, varargin{:});
+ [autosave, overwrite, refine, outputFormat] = parseoptioninputs(varargin{idxOpts:end});
+
+ % Convert filenames to string array
+ allFileNames = string(allFileNames);
+
+ % -------------------------------------------
+ % Convert all files
+
+ % Number of files found
+ nbFiles = length(allFileNames);
+
+ % Initialize structures
+ Dat = struct('file', [], 'airfoil', [], 'format', [], 'nPoints', [], 'coord', [], ...
+ 'upper', [], 'lower', []);
+
+ for i = 1:nbFiles
+
+ % Load file and start parsing
+ % No matter the file type, line 1 should always be the airfoil name
+ fileID = fopen(fullfile(fullpath, allFileNames{i}));
+ tmpAirfoil = textscan(fileID, '%s', 1, 'Delimiter', '\n:', 'HeaderLines', 0);
+ tmpCoord = cell2mat(textscan(fileID, '%f %f %*[^\n]', 'HeaderLines', 0));
+ fclose(fileID);
+ clear fileID;
+
+ % Split airfoil into its upper and lower surfaces
+ [Dat(i).upper, Dat(i).lower] = splitsurfaces(tmpCoord);
+
+ % Refines coordinates by adding points if needed
+ [Dat(i).upper, Dat(i).lower] = refinesurfaces(Dat(i).upper, Dat(i).lower, refine, ...
+ REFINED_SPACING, REFINED_NPOINTS);
+
+ % Fromats according to desired output
+ switch outputFormat
+ case 'Selig'
+ [Dat(i).coord, Dat(i).array] = selig(Dat(i).upper, Dat(i).lower);
+ case 'Lednicer'
+ [Dat(i).coord, Dat(i).array] = lednicer(Dat(i).upper, Dat(i).lower);
+ end
+
+ % Output structure
+ Dat(i).path = fullpath;
+ Dat(i).file = allFileNames{i};
+ Dat(i).airfoil = char(cellstr(tmpAirfoil{:}));
+ Dat(i).format = outputFormat;
+
+ end
+
+ % -------------------------------------------
+ % Save results automatically
+
+ if autosave
+
+ for i = 1:length(Dat)
+
+ filename = split(Dat(i).file, '.dat');
+ if ~overwrite
+ filename = [filename{1}, '-', outputFormat];
+ end
+ filename = appendextension(filename, '.dat');
+ filename = fullfile(Dat(i).path, filename);
+ header = Dat(i).airfoil;
+ savetodat(filename, header, Dat(i).array);
+ end
+ end
+
+ % Cleanup
+ Dat = rmfield(Dat, 'array');
+
+end
+
+% --------------------------------------------------------------------------------------------------
+function [autosave, overwrite, refine, outputFormat] = parseoptioninputs(varargin)
+ % PARSEOPTIONINPUTS Parses the options and checks their validity
+
+ import af_tools.utils.*
+
+ % Constants and defaults
+ DEFAULT_AUTOSAVE = false;
+ DEFAULT_OVEWRITE = false;
+ DEFAULT_REFINE = false;
+ DEFAULT_FORMAT = 'Selig';
+ ALLOWED_FORMATS = {'Selig', 'Lednicer'};
+
+ % Option validator
+ validLogical = @(x) validateattributes(x, {'logical'}, {'scalar'}, mfilename());
+ validFormat = @(x) any(validatestring(x, ALLOWED_FORMATS, mfilename()));
+
+ % Parse options
+ p = inputParser;
+ addParameter(p, 'autosave', DEFAULT_AUTOSAVE, validLogical);
+ addParameter(p, 'overwrite', DEFAULT_OVEWRITE, validLogical);
+ addParameter(p, 'refine', DEFAULT_REFINE, validLogical);
+ addParameter(p, 'outputFormat', DEFAULT_FORMAT, validFormat);
+
+ parse(p, varargin{:});
+ autosave = p.Results.autosave;
+ overwrite = p.Results.overwrite;
+ refine = p.Results.refine;
+ outputFormat = p.Results.outputFormat;
+
+end
+
+function [upper, lower] = splitsurfaces(data)
+ % SPLITSURFACES Splits the whole airfoil into its upper and lower surfaces
+
+ % Determine format
+ if data(1, 1) > 1
+ inputFormat = 'Lednicer';
+ elseif data(1, 1) == 1
+ inputFormat = 'Selig';
+ else
+ error('MATLAB:formatairfoilcoord:unknownInputFormat', ...
+ ['The second line of the data file must either be 1 (Selig format) or '...
+ 'an integer larger than 1 (Lednicer).']);
+ end
+
+ % Split lower and upper surfaces
+ switch inputFormat
+ case 'Selig'
+ idx = find(diff(data(:, 1)) < 0, 1, 'last');
+ upper = data(1:idx + 1, :);
+ upper = flipud(upper);
+ lower = data(idx + 1:end, :);
+ case 'Lednicer'
+ nCoord = data(1, 1);
+ upper = data(2:nCoord + 1, :);
+ lower = data(nCoord + 2:end, :);
+ end
+
+end
+
+function [newUpper, newLower] = refinesurfaces(upper, lower, refine, spacing, nPoints)
+ % REFINESURFACES Refines the upper and lower surfaces by adding more points
+
+ import af_tools.utils.spacedvector
+
+ if refine && size(upper, 1) < nPoints
+ xc = fliplr(spacedvector(spacing, nPoints))';
+
+ newUpper(:, 1) = xc;
+ newLower(:, 1) = xc;
+ newUpper(:, 2) = interp1(upper(:, 1), upper(:, 2), xc, 'spline');
+ newLower(:, 2) = interp1(lower(:, 1), lower(:, 2), xc, 'spline');
+ else
+ newUpper = upper;
+ newLower = lower;
+ end
+
+end
diff --git a/+af_tools/uiuccleaner.m b/+af_tools/uiuccleaner.m
deleted file mode 100644
index 804b0de5c9b7817a8e4d5f80e3c2024d9d2962a0..0000000000000000000000000000000000000000
--- a/+af_tools/uiuccleaner.m
+++ /dev/null
@@ -1,196 +0,0 @@
-function Dat = uiuccleaner(varargin)
- % UIUCCLEANER Cleans airfoil data from UIUC Airfoil Database.
- % The UIUC airfoil database from the University of Illinois gathers the coordinates for more
- % than 1600 airfoils. However, there is a few discrepancies between the format and ordering of
- % these coordinates. This script alleviates that by re-formatting any input file from the
- % original database.
- %
- % Format:
- % The output format of this script follows the "labeled coordinates" file, used originally by
- % Selig on the UIUC Airfoil Database.
- % The first line contains the name of the airfoil, and each line after that is a set of
- % coordinates. The coordinates are ordered from the trailing edge, along the upper surface to
- % the leading edge and back around the lower surface to trailing edge.
- %
- % Note:
- % This function can be used on many files at once in order to speed-up the process.
- %
- % <a href="https://gitlab.uliege.be/thlamb/airfoil_toolbox">Documentation (README)</a>
- % <a href="https://gitlab.uliege.be/thlamb/airfoil_toolbox/-/issues">Report an issue</a>
- % -----
- %
- % Usage:
- % DAT = UIUCCLEANER prompts the user for all inputs, then converts the coordinates to the
- % correct standard.
- %
- % DAT = UIUCCLEANER(INPUTDIR) converts all dat files found in INPUTDIR.
- %
- % DAT = UIUCCLEANER(INPUTDIR, INPUTFILES) converts only the polars specified by INPUTFILES
- % found in INPUTDIR.
- %
- % DAT = UIUCCLEANER(..., 'autosave', true) saves the resulting coordinates in a new dat-file.
- %
- % DAT = UIUCCLEANER(..., 'overwrite', true) saves the resulting coordinates by overwriting the
- % original dat-file. If autosave is not specified but overwrite is true, the file will be
- % overwritten anyway. If autosave is set to false and overwrite is true, the file will not be
- % saved at all.
- %
- % DAT = UIUCCLEANER(..., 'refine', true) refines the input data by using a spline
- % interpolation with 100 coordinates in total, spaced following the half-cosine rule.
- % False by default.
- %
- % Inputs:
- % inputDir : Path of the directory with the UIUC oridinal dat-files
- % inputFiles : Files to select (ex: '*' (default), '*0012*', {'file1','file2'}, etc)
- %
- % Output:
- % Dat : A structure for the results for each input file.
- % - Dat.file : original filename
- % - Dat.airfoil : airfoil name, parsed from the input file
- % - Dat.x : airfoil X coordinates, with 0 <= X <= 1
- % - Dat.y : airfoil Y coordinates.
- %
- % Example:
- % UIUCCLEANER
- % UIUCCLEANER('test_data')
- % UIUCCLEANER('test_data', '*0012*')
- % UIUCCLEANER('test_data', {'0012_re1e5', '0012_re1e6'})
- % UIUCCLEANER('test_data', 'autosave', true)
- % UIUCCLEANER('test_data', 'overwrite', true)
- % UIUCCLEANER('test_data', 'refine', true)
- %
- % See also: NACAAIRFOIL.
- %
- % -----
- % UIUC Airfoil Database: https://m-selig.ae.illinois.edu/ads/coord_database.html
- % -----
- % (c) Copyright 2022 University of Liege
- % Author: Thomas Lambert <t.lambert@uliege.be>
- % ULiege - Aeroelasticity and Experimental Aerodynamics
- % Apache 2.0 License
- % https://gitlab.uliege.be/am-dept/matlab_airfoil_toolbox
-
- % ----------------------------------------------------------------------------------------------
-
- narginchk(0, 8);
-
- % Import other functions from this package
- import af_tools.utils.*
-
- % Constants and defaults
- OPTION_LIST = {'autosave', 'overwrite', 'refine'};
- FILETYPE = '.dat';
- REFINED_SPACING = 'halfcosine';
- REFINED_NPOINTS = ceil((100 + 1) / 2);
-
- % Parse inputs
- [allFileNames, fullpath, idxOpts] = parsefileinputs(OPTION_LIST, FILETYPE, varargin{:});
- [autosave, overwrite, refine] = parseoptioninputs(varargin{idxOpts:end});
-
- % Convert filenames to string array
- allFileNames = string(allFileNames);
-
- % -------------------------------------------
- % Convert all files
-
- % Number of files found
- nbFiles = length(allFileNames);
-
- % Initialize structures
- Dat = struct('file', [], 'airfoil', [], 'x', [], 'y', []);
-
- for i = 1:nbFiles
-
- % Load file and start parsing
- % No matter the file type, line 1 should always be the airfoil name
- fileID = fopen(fullfile(fullpath, allFileNames{i}));
- tmpAirfoil = textscan(fileID, '%s', 1, 'Delimiter', '\n:', 'HeaderLines', 0);
- resultArray = cell2mat(textscan(fileID, '%f %f %*[^\n]', 'HeaderLines', 0));
- fclose(fileID);
- clear fileID;
-
- % Re-order file if it is needed
- if resultArray(1, 1) ~= 0 && resultArray(1, 1) ~= 1 && resultArray(2, 1) == 0
- % Remove first line
- resultArray = resultArray(2:end, :);
-
- % Find index at the end of the upper side (normally diff would be -1,
- % but we use -0.5 in case the LE and TE are not precisely at 0 and 1. It
- % should be the only negative diff anyway).
- idx = find(diff(resultArray) < -0.5, 1);
- upper = flipud(resultArray(1:idx, :));
- lower = resultArray(idx + 1:end, :);
- resultArray = [upper; lower(2:end, :)];
- end
-
- % Refine coordinates to add more points
- if refine && size(resultArray, 1) < 2 * REFINED_NPOINTS
- xc = fliplr(spacedvector(REFINED_SPACING, REFINED_NPOINTS))';
-
- idx = find(diff(resultArray(:, 1)) < 0, 1, 'last');
- upper = resultArray(1:idx + 1, :);
- lower = resultArray(idx + 1:end, :);
-
- refinedUpperY = interp1(upper(:, 1), upper(:, 2), xc, 'spline');
- refinedLowerY = interp1(lower(:, 1), lower(:, 2), flipud(xc), 'spline');
-
- x = [xc; flipud(xc(1:end - 1))];
- y = [refinedUpperY; refinedLowerY(2:end)];
- resultArray = [x, y];
- end
-
- % Output structure
- Dat(i).path = fullpath;
- Dat(i).file = allFileNames{i};
- Dat(i).airfoil = char(cellstr(tmpAirfoil{:}));
- Dat(i).x = resultArray(:, 1);
- Dat(i).y = resultArray(:, 2);
-
- end
-
- % -------------------------------------------
- % Save results automatically
-
- if autosave
-
- for i = 1:length(Dat)
-
- filename = split(Dat(i).file, '.dat');
- if ~overwrite
- filename = [filename{1}, '-CLEAN'];
- end
- filename = appendextension(filename, '.dat');
- filename = fullfile(Dat(i).path, filename);
- header = Dat(i).airfoil;
- savetodat(filename, header, Dat(i).x, Dat(i).y);
-
- end
- end
-
-end
-
-% --------------------------------------------------------------------------------------------------
-function [autosave, overwrite, refine] = parseoptioninputs(varargin)
- % PARSEOPTIONINPUTS Parses the options and checks their validity
-
- import af_tools.utils.*
-
- % Constants and defaults
- DEFAULT_AUTOSAVE = false;
- DEFAULT_OVEWRITE = false;
- DEFAULT_REFINE = false;
-
- % Option validator
- validLogical = @(x) validateattributes(x, {'logical'}, {'scalar'}, mfilename());
-
- % Parse options
- p = inputParser;
- addParameter(p, 'autosave', DEFAULT_AUTOSAVE, validLogical);
- addParameter(p, 'overwrite', DEFAULT_OVEWRITE, validLogical);
- addParameter(p, 'refine', DEFAULT_REFINE, validLogical);
- parse(p, varargin{:});
- autosave = p.Results.autosave;
- overwrite = p.Results.overwrite;
- refine = p.Results.refine;
-
-end
diff --git a/CHANGELOG.md b/CHANGELOG.md
index 69e56b86eed4ef903afab4f7874b737d87f4aaa8..ff3f266b97403c5479a83bc4d4179f56496981b1 100644
--- a/CHANGELOG.md
+++ b/CHANGELOG.md
@@ -15,6 +15,9 @@ and this project adheres to [Semantic Versioning](https://semver.org/spec/v2.0.0
### Changed
+- **BREAKING**: Renamed **uiuccleaner** in **formatairfoilcoord**
+- Feat: Add possibility to select output style for **formatairfoilcoord**
+- Feat: Add Selig and Lednicer utils for airfoil formatting
- Style: Adopt style from MISS_HIT
- Copyright notice: change main copyright holder to the University
- Doc: Revamp `CONTRIBUTING.md` to put emphasis on MISS_HIT and conventions
diff --git a/README.md b/README.md
index 0915c8cc4f9ef5c2b523846f6ef69319131b3489..7e181b15db0024bd1ecfa1852a6ab017b988e497 100644
--- a/README.md
+++ b/README.md
@@ -84,8 +84,8 @@ af_tools.xf2mat(args)
List of functions:
- [xf2mat](#xf2mat): Aggregates multiple XFOIL or XFLR5 polar results into a single structure.
-- [uiuccleaner](#uiuccleaner): Re-formats airfoil coordinates obtained from UIUC
- Airfoil database.
+- [formatairfoilcoord](#formatairfoilcoord): Re-format airfoil coordinates
+ datafile.
- [Airfoil generation](#airfoil-generation)
- [nacacamber](#nacacamber): Generates the coordinates of the camberline for a NACA 4 or 5 digits airfoil.
- [nacaairfoil](#nacaairfoil): Generates the full coordinates of a NACA 4 or 5 digits airfoil.
@@ -136,20 +136,34 @@ angles of attack and N is the number of input files.
| `cd` | Drag coefficient | [M x N] |
| `cm` | Moment coefficient | [M x N] |
-### uiuccleaner
-
-The [UIUC airfoil database][uiuc-af-db] from the University of Illinois gathers the
-coordinates for more than 1600 airfoils. However, there is a few
-discrepancies between the format and ordering of these coordinates. This
-scripts alleviates that by re-formatting any input file from the original
-database. The main use of this function is to make the coordinates files
-compliant with other existing tools, such as [XFOIL][xfoil].
-
-The output format of this script follows the "labeled coordinates" file, used
-originally by Selig on the UIUC Airfoil Database. The first line contains the
-name of the airfoil, and each line after that is a set of coordinates. The
-coordinates are ordered from the trailing edge, along the upper surface to the
-leading edge and back around the lower surface to trailing edge.
+### formatairfoilcoord
+
+The [UIUC airfoil database][uiuc-af-db] from the University of Illinois gathers
+the coordinates for more than 1600 airfoils. Two different standards are used
+to represent the coordinates of the airfoil:
+
+- _Selig_: The first line is the name of the airfoil, and each line after that
+ is a set of coordinates. The coordinates are ordered from the trailing edge,
+ along the upper surface to the leading edge and back around the lower surface
+ to trailing edge (_e.g._, see
+ [E205](https://m-selig.ae.illinois.edu/ads/coord/e205.dat)). This format is
+ the most common one.
+- _Lednicer_: The first line is the name of the airfoil, the second one is the
+ number of points on each side and the lines after that are the coordinates.
+ The coordinates are given separately for the upper and lower surfaces, each
+ from the leading edge to the trailing edge (_e.g._, see [Clark
+ Y](https://m-selig.ae.illinois.edu/ads/coord/clarky.dat)).
+
+Many engineering tools or application (such as [XFOIL][xfoil]) rely on inputs in
+the _Selig_ format only. This script was therefore created to reformat original
+data so they can be used easily with other tools.
+
+Even though the _Selig_ format is the default option, the script allows also the
+user to reformat _Selig_ files in _Lednicer_ form if needed. It also comes with
+the option to refine the coordinates by adding points with a spline
+interpolation following the half-cosine rule (more points are the leading and
+trailing edge). If that option is selected, the airfoil will be defined using 50
+points for each surface.
```matlab
import af_tools.xf2mat
@@ -158,14 +172,15 @@ Polar = uiuccleaner(inputDir, inputFiles, 'autosave', true)
Polar = uiuccleaner(inputDir, inputFiles, 'overwrite', true)
```
-| Input | Example | Default |
-|------------- | ---------------------------------------------- | --------|
-| `inputDir` | `'.'`, `'xf_results'` | - |
-| `inputFiles` | `'*'`, `'*0012*'`, `'{'*0012_1*', '*0012_2*'}` | `'*'` |
-| | | |
-| 'autosave' | `false`, `true` | `false` |
-| 'overwrite' | `false`, `true` | `false` |
-| 'refine' | `false`, `true` | `false` |
+| Input | Example | Default |
+|--------------- | ---------------------------------------------- | --------|
+| `inputDir` | `'.'`, `'xf_results'` | - |
+| `inputFiles` | `'*'`, `'*0012*'`, `'{'*0012_1*', '*0012_2*'}` | `'*'` |
+| | | |
+| 'autosave' | `false`, `true` | `false` |
+| 'overwrite' | `false`, `true` | `false` |
+| 'refine' | `false`, `true` | `false` |
+| 'outputFormat' | `Selig`, `Lednicer` | `Selig` |
### Airfoil generation
diff --git a/tests/test_formatairfoilcoord.m b/tests/test_formatairfoilcoord.m
new file mode 100644
index 0000000000000000000000000000000000000000..d1660f5034479c87f7288cddbb573b5f1e763f53
--- /dev/null
+++ b/tests/test_formatairfoilcoord.m
@@ -0,0 +1,222 @@
+% TEST_FORMATAIRFOILCOORD Unitary tests for the formatairfoilcoord function
+% Note:
+% Matlab package functionality is not very test-framework friendly.
+% Either the whole package has to be imported in EVERY SINGLE TEST or the
+% functions must be called as <package>.function() everytime.
+% The second option is preferred for the tests as it has the smaller scope.
+%
+% -----
+% (c) Copyright 2022 University of Liege
+% Author: Thomas Lambert <t.lambert@uliege.be>
+% ULiege - Aeroelasticity and Experimental Aerodynamics
+% Apache 2.0 License
+% https://gitlab.uliege.be/am-dept/matlab_airfoil_toolbox
+
+% --------------------------------------------------------------------------------------------------
+
+%% Main test function
+
+function tests = test_formatairfoilcoord
+
+ tests = functiontests(localfunctions);
+
+end
+
+%% Setup and teardown
+
+function setupOnce(testCase)
+
+ addpath('../.'); % Add repository to Matlab Path
+ addpath('./test_utils'); % Add utils to Matlab Path
+
+ % Set random number generator settings.
+ testCase.TestData.currentRNG = rng;
+
+end
+
+function teardownOnce(testCase)
+
+ rmpath('../.'); % Remove repository from Matlab Path
+ rmpath('./test_utils'); % Remove utils from Matlab Path
+
+ % Restore the random number generator settings.
+ s = testCase.TestData.currentRNG;
+ rng(s);
+
+end
+
+function teardown(~)
+
+ close all; % Close all figures that would have been openend
+
+end
+
+%% Arguments and errors tests
+
+function test_nargin(testCase)
+ % Error if too many arguments
+
+ dummy = (1:10)';
+
+ verifyError(testCase, ...
+ @() af_tools.formatairfoilcoord(dummy, dummy, dummy, ...
+ 'autosave', true, 'overwrite', false, 'refine', true), ...
+ 'MATLAB:narginchk:tooManyInputs');
+
+end
+
+function test_invalidInputsType(testCase)
+ % Error if base inputs are of the wrong type
+
+ empty = [];
+ scal = 0;
+ logi = true;
+ Struct = struct;
+
+ % 1. inputDir (char vector or string)
+ verifyError(testCase, @() af_tools.formatairfoilcoord(empty), 'MATLAB:parsefileinputs:invalidType');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(scal), 'MATLAB:parsefileinputs:invalidType');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(logi), 'MATLAB:parsefileinputs:invalidType');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(Struct), 'MATLAB:parsefileinputs:invalidType');
+
+ % 2. inputFile (char, string, cell of chars)
+ verifyError(testCase, @() af_tools.formatairfoilcoord(scal, empty), 'MATLAB:parsefileinputs:invalidType');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(scal, scal), 'MATLAB:parsefileinputs:invalidType');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(scal, logi), 'MATLAB:parsefileinputs:invalidType');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(scal, Struct), 'MATLAB:parsefileinputs:invalidType');
+
+end
+
+function test_invalidOptions(testCase)
+ % Error if invalid option name or missing parameter value
+
+ wrongName = 'wrongOption';
+ testdir = [pwd, '/test_utils'];
+
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, '*', wrongName), ...
+ 'MATLAB:InputParser:ParamMissingValue');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, '*', wrongName, true), ...
+ 'MATLAB:InputParser:UnmatchedParameter');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, 'autosave', true, wrongName), ...
+ 'MATLAB:InputParser:ParamMissingValue');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, 'autosave', true, wrongName, true), ...
+ 'MATLAB:InputParser:UnmatchedParameter');
+
+end
+
+function test_invalidOptionsVal(testCase)
+ % Error if valid option name but invalid value
+
+ empty = [];
+ scal = 0;
+ char = 'test';
+ Struct = struct;
+ vect = 1:10;
+
+ testdir = [pwd, '/test_utils'];
+
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, 'autosave', empty), ...
+ 'MATLAB:formatairfoilcoord:invalidType');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, 'autosave', scal), ...
+ 'MATLAB:formatairfoilcoord:invalidType');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, 'autosave', char), ...
+ 'MATLAB:formatairfoilcoord:invalidType');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, 'autosave', Struct), ...
+ 'MATLAB:formatairfoilcoord:invalidType');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, 'autosave', vect), ...
+ 'MATLAB:formatairfoilcoord:invalidType');
+
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, 'overwrite', empty), ...
+ 'MATLAB:formatairfoilcoord:invalidType');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, 'overwrite', scal), ...
+ 'MATLAB:formatairfoilcoord:invalidType');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, 'overwrite', char), ...
+ 'MATLAB:formatairfoilcoord:invalidType');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, 'overwrite', Struct), ...
+ 'MATLAB:formatairfoilcoord:invalidType');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, 'overwrite', vect), ...
+ 'MATLAB:formatairfoilcoord:invalidType');
+
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, 'refine', empty), ...
+ 'MATLAB:formatairfoilcoord:invalidType');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, 'refine', scal), ...
+ 'MATLAB:formatairfoilcoord:invalidType');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, 'refine', char), ...
+ 'MATLAB:formatairfoilcoord:invalidType');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, 'refine', Struct), ...
+ 'MATLAB:formatairfoilcoord:invalidType');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, 'refine', vect), ...
+ 'MATLAB:formatairfoilcoord:invalidType');
+
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, 'outputFormat', empty), ...
+ 'MATLAB:formatairfoilcoord:unrecognizedStringChoice');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, 'outputFormat', scal), ...
+ 'MATLAB:formatairfoilcoord:unrecognizedStringChoice');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, 'outputFormat', char), ...
+ 'MATLAB:formatairfoilcoord:unrecognizedStringChoice');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, 'outputFormat', Struct), ...
+ 'MATLAB:formatairfoilcoord:unrecognizedStringChoice');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, 'outputFormat', vect), ...
+ 'MATLAB:formatairfoilcoord:unrecognizedStringChoice');
+
+end
+
+% -------------------------------------
+function test_dirNotFound(testCase)
+ % Error if valid inputDir not found
+
+ verifyError(testCase, @() af_tools.formatairfoilcoord('missingdir'), 'MATLAB:parsefileinputs:dirNotFound');
+
+end
+
+function test_fileNotFound(testCase)
+ % Error if valid inputDir not found
+
+ testdir = [pwd, '/test_utils'];
+
+ verifyWarning(testCase, @() af_tools.formatairfoilcoord(testdir, {'clarky.dat', 'testdummy.dat'}), ...
+ 'MATLAB:parsefileinputs:FileNotFound');
+ % remove warning first warning about FileNotFound before it throws the error
+ warning('off', 'MATLAB:parsefileinputs:FileNotFound');
+ verifyError(testCase, @() af_tools.formatairfoilcoord(testdir, 'randomFile'), ...
+ 'MATLAB:parsefileinputs:noFilesFound');
+ warning on; % Reactivate warnings
+
+end
+
+%% Test if function returns expected outputs
+
+function test_correctOrder(testCase)
+ % Verify if the output starts and ends at X = 1;
+
+ testdir = [pwd, '/test_utils'];
+
+ Dat = af_tools.formatairfoilcoord(testdir, '*');
+
+ verifyEqual(testCase, Dat(1).coord(1, 1), 1);
+ verifyEqual(testCase, Dat(1).coord(end, 1), 1);
+ verifyEqual(testCase, Dat(2).coord(1, 1), 1);
+ verifyEqual(testCase, Dat(2).coord(end, 1), 1);
+
+end
+
+function test_correctRefinePoints(testCase)
+ % Verify if the output of refined solution has 101 points
+
+ testdir = [pwd, '/test_utils'];
+ nPoints = 101;
+
+ DatNoRefine = af_tools.formatairfoilcoord(testdir, '*');
+ Dat = af_tools.formatairfoilcoord(testdir, '*', 'refine', true);
+
+ for i = 1:length(Dat)
+ if length(DatNoRefine(i).coord(:, 1)) > nPoints
+ verifyEqual(testCase, Dat(i).coord(:, 1), DatNoRefine(i).coord(:, 1));
+ verifyEqual(testCase, Dat(i).coord(:, 2), DatNoRefine(i).coord(:, 2));
+ else
+ verifyEqual(testCase, length(Dat(i).coord(:, 1)), nPoints);
+ verifyEqual(testCase, length(Dat(i).coord(:, 2)), nPoints);
+ end
+ end
+
+end
diff --git a/tests/test_uiuccleaner.m b/tests/test_uiuccleaner.m
deleted file mode 100644
index 83b0534c4b54ccac915efd2b545051357392d673..0000000000000000000000000000000000000000
--- a/tests/test_uiuccleaner.m
+++ /dev/null
@@ -1,195 +0,0 @@
-% TEST_UIUCCLEANER Unitary tests for the uiuccleaner function
-% Note:
-% Matlab package functionality is not very test-framework friendly.
-% Either the whole package has to be imported in EVERY SINGLE TEST or the
-% functions must be called as <package>.function() everytime.
-% The second option is preferred for the tests as it has the smaller scope.
-%
-% -----
-% (c) Copyright 2022 University of Liege
-% Author: Thomas Lambert <t.lambert@uliege.be>
-% ULiege - Aeroelasticity and Experimental Aerodynamics
-% Apache 2.0 License
-% https://gitlab.uliege.be/am-dept/matlab_airfoil_toolbox
-
-% --------------------------------------------------------------------------------------------------
-
-%% Main test function
-
-function tests = test_uiuccleaner
-
- tests = functiontests(localfunctions);
-
-end
-
-%% Setup and teardown
-
-function setupOnce(testCase)
-
- addpath('../.'); % Add repository to Matlab Path
- addpath('./test_utils'); % Add utils to Matlab Path
-
- % Set random number generator settings.
- testCase.TestData.currentRNG = rng;
-
-end
-
-function teardownOnce(testCase)
-
- rmpath('../.'); % Remove repository from Matlab Path
- rmpath('./test_utils'); % Remove utils from Matlab Path
-
- % Restore the random number generator settings.
- s = testCase.TestData.currentRNG;
- rng(s);
-
-end
-
-function teardown(~)
-
- close all; % Close all figures that would have been openend
-
-end
-
-%% Arguments and errors tests
-
-function test_nargin(testCase)
- % Error if too many arguments
-
- dummy = (1:10)';
-
- verifyError(testCase, ...
- @() af_tools.uiuccleaner(dummy, dummy, dummy, ...
- 'autosave', true, 'overwrite', false, 'refine', true), ...
- 'MATLAB:narginchk:tooManyInputs');
-
-end
-
-function test_invalidInputsType(testCase)
- % Error if base inputs are of the wrong type
-
- empty = [];
- scal = 0;
- logi = true;
- Struct = struct;
-
- % 1. inputDir (char vector or string)
- verifyError(testCase, @() af_tools.uiuccleaner(empty), 'MATLAB:parsefileinputs:invalidType');
- verifyError(testCase, @() af_tools.uiuccleaner(scal), 'MATLAB:parsefileinputs:invalidType');
- verifyError(testCase, @() af_tools.uiuccleaner(logi), 'MATLAB:parsefileinputs:invalidType');
- verifyError(testCase, @() af_tools.uiuccleaner(Struct), 'MATLAB:parsefileinputs:invalidType');
-
- % 2. inputFile (char, string, cell of chars)
- verifyError(testCase, @() af_tools.uiuccleaner(scal, empty), 'MATLAB:parsefileinputs:invalidType');
- verifyError(testCase, @() af_tools.uiuccleaner(scal, scal), 'MATLAB:parsefileinputs:invalidType');
- verifyError(testCase, @() af_tools.uiuccleaner(scal, logi), 'MATLAB:parsefileinputs:invalidType');
- verifyError(testCase, @() af_tools.uiuccleaner(scal, Struct), 'MATLAB:parsefileinputs:invalidType');
-
-end
-
-function test_invalidOptions(testCase)
- % Error if invalid option name or missing parameter value
-
- wrongName = 'wrongOption';
- testdir = [pwd, '/test_utils'];
-
- verifyError(testCase, @() af_tools.uiuccleaner(testdir, '*', wrongName), ...
- 'MATLAB:InputParser:ParamMissingValue');
- verifyError(testCase, @() af_tools.uiuccleaner(testdir, '*', wrongName, true), ...
- 'MATLAB:InputParser:UnmatchedParameter');
- verifyError(testCase, @() af_tools.uiuccleaner(testdir, 'autosave', true, wrongName), ...
- 'MATLAB:InputParser:ParamMissingValue');
- verifyError(testCase, @() af_tools.uiuccleaner(testdir, 'autosave', true, wrongName, true), ...
- 'MATLAB:InputParser:UnmatchedParameter');
-
-end
-
-function test_invalidOptionsVal(testCase)
- % Error if valid option name but invalid value
-
- empty = [];
- scal = 0;
- char = 'test';
- Struct = struct;
- vect = 1:10;
-
- testdir = [pwd, '/test_utils'];
-
- verifyError(testCase, @() af_tools.uiuccleaner(testdir, 'autosave', empty), 'MATLAB:uiuccleaner:invalidType');
- verifyError(testCase, @() af_tools.uiuccleaner(testdir, 'autosave', scal), 'MATLAB:uiuccleaner:invalidType');
- verifyError(testCase, @() af_tools.uiuccleaner(testdir, 'autosave', char), 'MATLAB:uiuccleaner:invalidType');
- verifyError(testCase, @() af_tools.uiuccleaner(testdir, 'autosave', Struct), 'MATLAB:uiuccleaner:invalidType');
- verifyError(testCase, @() af_tools.uiuccleaner(testdir, 'autosave', vect), 'MATLAB:uiuccleaner:invalidType');
-
- verifyError(testCase, @() af_tools.uiuccleaner(testdir, 'overwrite', empty), 'MATLAB:uiuccleaner:invalidType');
- verifyError(testCase, @() af_tools.uiuccleaner(testdir, 'overwrite', scal), 'MATLAB:uiuccleaner:invalidType');
- verifyError(testCase, @() af_tools.uiuccleaner(testdir, 'overwrite', char), 'MATLAB:uiuccleaner:invalidType');
- verifyError(testCase, @() af_tools.uiuccleaner(testdir, 'overwrite', Struct), 'MATLAB:uiuccleaner:invalidType');
- verifyError(testCase, @() af_tools.uiuccleaner(testdir, 'overwrite', vect), 'MATLAB:uiuccleaner:invalidType');
-
- verifyError(testCase, @() af_tools.uiuccleaner(testdir, 'refine', empty), 'MATLAB:uiuccleaner:invalidType');
- verifyError(testCase, @() af_tools.uiuccleaner(testdir, 'refine', scal), 'MATLAB:uiuccleaner:invalidType');
- verifyError(testCase, @() af_tools.uiuccleaner(testdir, 'refine', char), 'MATLAB:uiuccleaner:invalidType');
- verifyError(testCase, @() af_tools.uiuccleaner(testdir, 'refine', Struct), 'MATLAB:uiuccleaner:invalidType');
- verifyError(testCase, @() af_tools.uiuccleaner(testdir, 'refine', vect), 'MATLAB:uiuccleaner:invalidType');
-
-end
-
-% -------------------------------------
-function test_dirNotFound(testCase)
- % Error if valid inputDir not found
-
- verifyError(testCase, @() af_tools.uiuccleaner('missingdir'), 'MATLAB:parsefileinputs:dirNotFound');
-
-end
-
-function test_fileNotFound(testCase)
- % Error if valid inputDir not found
-
- testdir = [pwd, '/test_utils'];
-
- verifyWarning(testCase, @() af_tools.uiuccleaner(testdir, {'clarky.dat', 'testdummy.dat'}), ...
- 'MATLAB:parsefileinputs:FileNotFound');
- % remove warning first warning about FileNotFound before it throws the error
- warning('off', 'MATLAB:parsefileinputs:FileNotFound');
- verifyError(testCase, @() af_tools.uiuccleaner(testdir, 'randomFile'), 'MATLAB:parsefileinputs:noFilesFound');
- warning on; % Reactivate warnings
-
-end
-
-%% Test if function returns expected outputs
-
-function test_correctOrder(testCase)
- % Verify if the output starts and ends at X = 1;
-
- testdir = [pwd, '/test_utils'];
-
- Dat = af_tools.uiuccleaner(testdir, '*');
-
- verifyEqual(testCase, Dat(1).x(1), 1);
- verifyEqual(testCase, Dat(1).x(end), 1);
- verifyEqual(testCase, Dat(2).x(end), 1);
- verifyEqual(testCase, Dat(2).x(end), 1);
-
-end
-
-function test_correctRefinePoints(testCase)
- % Verify if the output of refined solution has 101 points
-
- testdir = [pwd, '/test_utils'];
- nPoints = 101;
-
- DatNoRefine = af_tools.uiuccleaner(testdir, '*');
- Dat = af_tools.uiuccleaner(testdir, '*', 'refine', true);
-
- for i = 1:length(Dat)
- if length(DatNoRefine(i).x) > nPoints
- verifyEqual(testCase, Dat(i).x, DatNoRefine(i).x);
- verifyEqual(testCase, Dat(i).y, DatNoRefine(i).y);
- else
- verifyEqual(testCase, length(Dat(i).x), nPoints);
- verifyEqual(testCase, length(Dat(i).y), nPoints);
- end
- end
-
-end