copy turbie parms to matlab

MATLAB_model/CT.txt

+V(m/s)	CT
+4.0 	0.923
+5.0 	0.919
+6.0 	0.904
+7.0 	0.858
+8.0 	0.814
+9.0 	0.814
+10.0	0.814
+11.0	0.814
+12.0	0.577
+13.0	0.419
+14.0	0.323
+15.0	0.259
+16.0	0.211
+17.0	0.175
+18.0	0.148
+19.0	0.126
+20.0	0.109
+21.0	0.095
+22.0	0.084
+23.0	0.074
+24.0	0.066
+25.0	0.059
\ No newline at end of file

MATLAB_model/main.m

@@ -12,7 +12,7 @@ global t f M C K rho Dr CT V
 
 %% Turbine parameters
 
-parameters = readvars('../turbie/turbie_parameters.txt', 'CommentStyle','%',  'NumHeaderLines',1, 'ExpectedNumVariables',14);
+parameters = readvars('./turbie_parameters.txt', 'CommentStyle','%',  'NumHeaderLines',1, 'ExpectedNumVariables',14);
 mb = parameters(1);         % Blade mass [kg]
 mn = parameters(2);         % Nacelle mass [kg]
 mh = parameters(3);         % Hub mass [kg]
@@ -83,7 +83,7 @@ table(fntar,fnu,fnd,fnerr,drtar,dr,drerr)
 %% Thrust coefficient
 
 % Load table with CT as function of mean wind speed
-temp = importdata('../CT.txt');
+temp = importdata('./CT.txt');
 Vtab = temp.data(:,1);
 CTtab = temp.data(:,2);
 

MATLAB_model/turbie_parameters.txt

+% Turbie parameters
+41e3     % mb [kg]
+446e3    % mn [kg]
+105e3    % mh [kg]
+628e3    % mt [kg]
+4.208e3  % c1 [N/(m/s)]
+1.273e4  % c2 [N/(m/s)]
+1.711e6  % k1 [N/(m/s)]
+3.278e6  % k2 [N/(m/s)]
+0.63     % fb [Hz]
+0.25     % ft [Hz]
+0.004933803235848756  % drb [-]
+0.0030239439187460114  % drt [-]
+178   % Dr [m]
+1.22  % rho [kg/m3]