diff --git a/processall.m b/processall.m
index 0356a4bf6793327f463167dc055b9fa64ef78201..5e20280f64467cf77d64c0611941a6356168ba94 100644
--- a/processall.m
+++ b/processall.m
@@ -62,6 +62,14 @@ function ExpData = processall(idFile)
 
         if ~isempty(ExpData(iTest).arduFile) % Not for static tests (no ardu data)
             [arduShort, ~] = loadardu(ExpData(iTest).arduFile);
+
+            % DEBUG
+            figure;
+            hold on;
+            plot(tunnelData(:, 1));
+            plot(tunnelData(:, 3));
+            grid on;
+
             [arduShort, tunnelData, ExpData(iTest).arduStart, ExpData(iTest).tunnelStart] = ...
                 syncdata(arduShort, tunnelData);
 
diff --git a/utils/analysis/plotcf.m b/utils/analysis/plotcf.m
index e3571c3a0df7994a893ff232d457749ea37167ca..2e6d6630841fd11f4c4f55835f918ba70aad17f4 100644
--- a/utils/analysis/plotcf.m
+++ b/utils/analysis/plotcf.m
@@ -14,10 +14,14 @@ function plotcf(ResData)
     % One figure per dx
     % Plot airspeeds in different colors
 
+    set(0, 'defaulttextinterpreter', 'latex');
+
     ONLY_ERR_BARS = true;
+    ERR_CAPSIZE = 3;
     OFFSET_STEPS = 20;
-
+    CHORD = 0.05;
     INTERESTING_PLOTS = [
+                         0.03, 2, 7.7
                          0.03, 2, 7.7
                          0.03, 3, 2.5
                          0.03, 3, 4.6
@@ -25,7 +29,7 @@ function plotcf(ResData)
                          0.03, 3.5, 4.6
                          0.03, 3.5, 7.7
 
-                         0.05, 1.25, 4.6
+                         % 0.05, 1.25, 4.6 % DRIFT ON INERTIA
                          0.05, 2, 7.7
                          0.05, 3, 7.7
                          0.05, 3.5, 2.5
@@ -38,14 +42,22 @@ function plotcf(ResData)
                          0.10, 3.5, 7.7
                         ];
 
+    SAVE_TIKZ_PARAM = [0, 0, 0]; % Points to save ([0,0,0] to make sur nothing is save)
+
     for i = 1:size(ResData, 1)
         for j = 1:size(ResData, 2)
 
             if isinteresting(ResData(i, j), INTERESTING_PLOTS)
-                expParam = sprintf('d = %0.2f, f = %0.2f, V = %0.1f', ...
+
+                trueF = ResData(i, j).Front.trueFreq;
+
+                redFreq = redfreq(trueF, CHORD, ResData(i, j).Testcase.airspeed);
+
+                expParam = sprintf('d = %0.2f, f = %0.2f, V = %0.1f (k = %0.02f)', ...
                                    ResData(i, j).Testcase.dx, ...
                                    ResData(i, j).Testcase.freq, ...
-                                   ResData(i, j).Testcase.airspeed);
+                                   ResData(i, j).Testcase.airspeed, ...
+                                   redFreq);
 
                 offsets = ResData(i, j).AllPhases.offsets;
                 cleanOffsets = -175:OFFSET_STEPS:175;
@@ -72,40 +84,170 @@ function plotcf(ResData)
                 xpos = cleanOffsets - meanOffset + stdOffset;
 
                 figure('Name', 'myfig');
-                subplot(211);
+                ax1 = subplot(211);
+                setcolormap();
                 hold on;
                 if ~ONLY_ERR_BARS
                     plot(ResData(i, j).AllPhases.offsets, ...
                          ResData(i, j).AllPhases.Front.cF(:, [1, 3]), 'o');
                 end
-                errorbar(cleanOffsets, meanF(:, 1), ynegF(:, 1), yposF(:, 1), xneg, xpos, 'o');
-                errorbar(cleanOffsets, meanF(:, 3), ynegF(:, 3), yposF(:, 3), xneg, xpos, 'o');
+                errorbar(cleanOffsets, meanF(:, 3), yposF(:, 3), 'o', 'Capsize', ERR_CAPSIZE);
+                errorbar(cleanOffsets, meanF(:, 1), yposF(:, 1), 'o', 'Capsize', ERR_CAPSIZE);
                 hold off;
-                title(['Front module -- ', expParam]);
-
-                setgca();
-
-                subplot(212);
+                setgca('XTickLabel', [], ...
+                       'XLabel', []);
+                legend({'\cl', '\cd'}, 'Location', 'SouthWest');
+                legend('boxoff');
+                ax1.Position(3) = 1.25 * ax1.Position(3);
+                title('Front');
+
+                ax2 = subplot(212);
+                setcolormap();
                 hold on;
                 if ~ONLY_ERR_BARS
                     plot(ResData(i, j).AllPhases.offsets, ...
                          ResData(i, j).AllPhases.Aft.cF(:, [1, 3]), 'o');
                 end
-                errorbar(cleanOffsets, meanA(:, 1), ynegA(:, 1), yposA(:, 1), xneg, xpos, 'o');
-                errorbar(cleanOffsets, meanA(:, 3), ynegA(:, 3), yposA(:, 3), xneg, xpos, 'o');
+                errorbar(cleanOffsets, meanA(:, 3), yposA(:, 3), 'o', 'Capsize', ERR_CAPSIZE);
+                errorbar(cleanOffsets, meanA(:, 1), yposA(:, 1), 'o', 'Capsize', ERR_CAPSIZE);
                 hold off;
-                title(['Aft module -- ', expParam]);
+                title(ax2, 'Aft');
+
                 setgca();
-                legend('Location', 'bestoutside', 'orientation', 'horizontal', 'Fx', 'Fz');
+                linkaxes([ax1 ax2], 'xy');
+                ax2.Position(3) = ax1.Position(3);
+                title('Aft');
+
+                if isinteresting(ResData(i, j), SAVE_TIKZ_PARAM)
+                    figdir = 'figures/results/';
+                    filename = sprintf('flapWindOn-Dx%0.2f_F%0.2f_V%0.1f.tex', ...
+                                       ResData(i, j).Testcase.dx, ...
+                                       ResData(i, j).Testcase.freq, ...
+                                       ResData(i, j).Testcase.airspeed);
+                    save2tikz([figdir, filename], '\small');
+                end
+                % Update titles after having saved
+                title(ax1, ['Front - ', expParam]);
+                title(ax2, ['Aft - ', expParam]);
+
+                % Save interesting stuff for other types of plots
+                Tmp(i, j).cleanOffsets = cleanOffsets;
+                Tmp(i, j).meanF = meanF;
+                Tmp(i, j).stdF = stdF;
+                Tmp(i, j).meanA = meanA;
+                Tmp(i, j).stdA = stdA;
 
             end
         end
     end
 
+    % Plot aft wings only for different spacing conditions
+    for j = 26
+
+        figure('Name', 'Dx');
+        ax1 = subplot(211);
+        setcolormap();
+        hold on;
+        errorbar(Tmp(2, j).cleanOffsets, Tmp(2, j).meanA(:, 3), Tmp(2, j).stdA(:, 3), 'o', ...
+                 'Capsize', ERR_CAPSIZE);
+        errorbar(Tmp(2, j).cleanOffsets, Tmp(2, j).meanA(:, 1), Tmp(2, j).stdA(:, 1), 'o', ...
+                 'Capsize', ERR_CAPSIZE);
+        hold off;
+        setgca('XTickLabel', [], ...
+               'XLabel', []);
+        title('$\dx = 0.03 \unit{\m}$');
+        legend({'\cl', '\cd'}, 'Location', 'NorthEast');
+        legend('boxoff');
+        ax1.Position(3) = 1.25 * ax1.Position(3);
+
+        ax2 = subplot(212);
+        setcolormap();
+        hold on;
+        errorbar(Tmp(1, j).cleanOffsets, Tmp(1, j).meanA(:, 3), Tmp(1, j).stdA(:, 3), 'o', ...
+                 'Capsize', ERR_CAPSIZE);
+        errorbar(Tmp(1, j).cleanOffsets, Tmp(1, j).meanA(:, 1), Tmp(1, j).stdA(:, 1), 'o', ...
+                 'Capsize', ERR_CAPSIZE);
+        hold off;
+        setgca();
+        title('$\dx = 0.10 \unit{\m}$');
+        linkaxes([ax1 ax2], 'xy');
+        ax2.Position(3) = ax1.Position(3);
+
+        figdir = 'figures/results/';
+        filename = sprintf('flapWindOn-DxCompa-F%0.2f_V%0.1f.tex', ...
+                           ResData(i, j).Testcase.freq, ...
+                           ResData(i, j).Testcase.airspeed);
+        save2tikz([figdir, filename], '\small');
+
+    end
+
+    % Plot aft wings only for diff frequencies
+    j = 20;
+    figure('Name', 'K');
+    ax1 = subplot(211);
+    setcolormap();
+    hold on;
+    errorbar(Tmp(1, j).cleanOffsets, Tmp(1, j).meanA(:, 3), Tmp(1, j).stdA(:, 3), 'o', ...
+             'Capsize', ERR_CAPSIZE);
+    errorbar(Tmp(1, j).cleanOffsets, Tmp(1, j).meanA(:, 1), Tmp(1, j).stdA(:, 1), 'o', ...
+             'Capsize', ERR_CAPSIZE);
+    hold off;
+    setgca('XTickLabel', [], ...
+           'XLabel', []);
+    title('$\redFreq = 0.05$');
+    legend({'\cl', '\cd'}, 'Location', 'NorthEast');
+    legend('boxoff');
+    ax1.Position(3) = 1.25 * ax1.Position(3);
+
+    j = 28;
+    ax2 = subplot(212);
+    setcolormap();
+    hold on;
+    errorbar(Tmp(1, j).cleanOffsets, Tmp(1, j).meanA(:, 3), Tmp(1, j).stdA(:, 3), 'o', ...
+             'Capsize', ERR_CAPSIZE);
+    errorbar(Tmp(1, j).cleanOffsets, Tmp(1, j).meanA(:, 1), Tmp(1, j).stdA(:, 1), 'o', ...
+             'Capsize', ERR_CAPSIZE);
+    hold off;
+    setgca();
+    title('$\redFreq = 0.07$');
+    linkaxes([ax1 ax2], 'x');
+    ax2.Position(3) = ax1.Position(3);
+
+    figdir = 'figures/results/';
+    filename = sprintf('flapWindOn-kCompa-Dx%0.2f_V%0.1f.tex', ...
+                       ResData(i, j).Testcase.dx, ...
+                       ResData(i, j).Testcase.airspeed);
+    save2tikz([figdir, filename], '\small');
+
 end
 
-function setgca()
-    % SETGCA Sets the axes parameters
+function setgca(varargin)
+
     xlim([-180, 180]);
-    grid on;
+
+    xlabel('Phase offset [deg]');
+    ylabel('\cl and \cd [-]');
+    xticks([-180:90:180]);
+
+    set(gca, ...
+        'Box', 'off', ...
+        'TickDir', 'out', ...
+        'TickLength', [.02 .02], ...
+        'XMinorTick', 'off', ...
+        'YMinorTick', 'off', ...
+        'YGrid', 'on', ...
+        'XGrid', 'on', ...
+        'XColor', 'k', ...
+        'YColor', 'k', ...
+        'GridLineStyle', ':', ...
+        'GridColor', 'k', ...
+        'GridAlpha', 0.25, ...
+        'LineWidth', 1, ...
+        'FontName', 'Helvetica', ...
+        'Fontsize', 14);
+
+    if nargin > 0
+        set(gca, varargin{:});
+    end
+
 end
diff --git a/utils/redfreq.m b/utils/redfreq.m
new file mode 100644
index 0000000000000000000000000000000000000000..b32168418ee163909bff237adcd369cdada09e5e
--- /dev/null
+++ b/utils/redfreq.m
@@ -0,0 +1,13 @@
+function redFreq = redfreq(freq, chord, speed)
+    % REFREQ Calculate the reduced frequency
+    %   Todo
+
+    % ----------------------------------------------------------------------------------------------
+    % (c) Copyright 2022 University of Liege
+    % Author: Thomas Lambert <t.lambert@uliege.be>
+    % ULiege - Aeroelasticity and Experimental Aerodynamics
+    % MIT License
+    %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+    redFreq = pi * freq * chord / speed;
+end
diff --git a/utils/syncdata.m b/utils/syncdata.m
index 05dccc01a29b372bd84d074347b83e1bcd47c716..9003ff9164f2e30ade66ee4d0cb0e0e56e81b3e2 100644
--- a/utils/syncdata.m
+++ b/utils/syncdata.m
@@ -71,7 +71,7 @@ function [arduSynced, tunnelSynced, arduStartTime, tunnelStartTime] = ...
 end
 
 function [startIdx, startTime] = getstartardu(arduData)
-    % GETSTARTARDU Get the starting point for the arduino dataset and the flapping direction at
+    % GETSTARTARDU Get the starting po  int for the arduino dataset and the flapping direction at
     % start
 
     ANGLE_IDX = [2, 3]; % Indexes of the front and aft angles in arduData file