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reorganize file structure

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This commit is contained in:
Anthony Correa
2010-04-17 12:00:00 -05:00
parent 0da2092d89
commit 5bacd30bad
515 changed files with 2257 additions and 37 deletions
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airfoil/Airfoils/.DS_Store vendored Normal file
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airfoil/Airfoils/CB3.dat Executable file
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73
airfoil/Airfoils/CB600175b.dat Executable file
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73
airfoil/Airfoils/CB600185b.dat Executable file
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73
airfoil/Airfoils/CB600185c.dat Executable file
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73
airfoil/Airfoils/CB600185d.dat Executable file
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airfoil/Airfoils/CB60019c.dat Executable file
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75
airfoil/Airfoils/SAX.dat Executable file
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airfoil/Airfoils/SAX2.dat Executable file
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airfoil/Airfoils/SAX3.dat Executable file
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airfoil/Airfoils/SAX4.dat Executable file
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1
airfoil/Airfoils/SAX4A.dat Executable file
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airfoil/Airfoils/dsma523a.dat Executable file
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airfoil/Airfoils/n0011sc.dat Executable file
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33
airfoil/Airfoils/n0012.dat Executable file
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33
airfoil/Airfoils/n001264.dat Executable file
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73
airfoil/Airfoils/n00155sc.dat Executable file
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73
airfoil/Airfoils/n00165sc.dat Executable file
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73
airfoil/Airfoils/n00175sc.dat Executable file
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73
airfoil/Airfoils/n00185sc.dat Executable file
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35
airfoil/Airfoils/n2410.dat Executable file
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103
airfoil/Airfoils/n2612.dat Executable file
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103
airfoil/Airfoils/n2616.dat Executable file
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airfoil/Airfoils/nasasc0714.dat Executable file
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airfoil/Airfoils/nasasc0716.dat Executable file
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0.999994 -0.016734

97
airfoil/Airfoils/nasasc0718.dat Executable file
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1.000012 -0.009544
0.990013 -0.006143
0.980014 -0.002885
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97
airfoil/Airfoils/nasasc0721.dat Executable file
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1.000021 -0.008911
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98
airfoil/Airfoils/transairfoilsc714cb175a.dat Executable file
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transaifoil1755asc714
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1.00000 -0.00815

24
airfoil/airfoil.m Executable file
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%ASCorrea
function airfoil(airfoilfilename)
rootLOCATION='\\ad.uiuc.edu\ae\correa2\Desktop\AE441\AE441 - Home Edition\Matlab code\';
airfoilLOCATION='\\ad.uiuc.edu\ae\correa2\Desktop\AE441\AE441 - Home Edition\Airfoils';
% airfoilfilename=input('Input airfoil dat file: \nNote: You must delete the header before using \n:','s');
% airfoilfilename='flatplate.dat'
cd(airfoilLOCATION)
data=load(airfoilfilename);
plottitle=regexprep(airfoilfilename, '.dat', '');
dataX=data(:,1);
dataY=data(:,2);
plot(dataX, dataY, 'k', 'LineWidth', 2)
axis equal
axis off
title(['Airfoil ' , plottitle])
print ('-dtiff', plottitle)
cd(rootLOCATION)
end