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Commit df91b611 authored by Jenni Rinker's avatar Jenni Rinker
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copy turbie parms to matlab

parent 6116fc48
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1 merge request!3Adding in exercises, Turbie
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
......@@ -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);
......
% 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]
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