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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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60
archive/Jacobi/Airfoils/CB30015.dat Executable file
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Centerbody 3
0.927434 0.030867
0.885738 0.037894
0.832426 0.044544
0.770708 0.050733
0.703824 0.054767
0.634967 0.057296
0.567289 0.058793
0.503215 0.059528
0.443412 0.059717
0.388348 0.059516
0.338469 0.059099
0.294235 0.058631
0.256072 0.058263
0.223760 0.058026
0.196178 0.057792
0.172167 0.057433
0.150558 0.056791
0.130182 0.055719
0.109959 0.054041
0.089801 0.051717
0.070408 0.048804
0.052499 0.045333
0.036815 0.041386
0.024065 0.037043
0.014845 0.032427
0.008795 0.027556
0.005152 0.022433
0.003127 0.017031
0.001941 0.011266
0.000833 0.004850
0.000868 -0.006228
0.002777 -0.014501
0.006960 -0.024027
0.014590 -0.033727
0.026905 -0.043466
0.045147 -0.053006
0.070516 -0.061993
0.104060 -0.070058
0.145165 -0.076927
0.192399 -0.082424
0.244294 -0.086545
0.299425 -0.089280
0.356322 -0.090523
0.413532 -0.090135
0.469635 -0.087990
0.523580 -0.084127
0.574750 -0.078781
0.622524 -0.072162
0.666283 -0.064484
0.705419 -0.055972
0.739322 -0.046855
0.767373 -0.037351
0.789853 -0.027657
0.808793 -0.017830
0.826372 -0.007917
0.844831 0.002026
0.866348 0.011975
0.893151 0.021929
0.927426 0.031964

1
archive/Jacobi/Planforms/AirData.dat Executable file
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0 0.610000000000000 0 n0011sc.dat

BIN
archive/Jacobi/Planforms/AirData.mat Executable file
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7
archive/Jacobi/Planforms/FDR001.avl Executable file
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0 85 0 n0012.dat
2.32 82.73 2.27 n0012.dat
6.38 73.67 11.33 n0012.dat
14.2 52.13 30.6 n0012.dat
28.98 20 55 nasasc2-0714.dat
34.77 15 60 nasasc2-0714.dat
70 7.5 803 nasasc2-0714.dat

7
archive/Jacobi/Planforms/olddater.dat Executable file
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0, 0.607142857, 0, 'CB50015.dat'
0.016571429, 0.590928571, 0.02, 'CB50015.dat'
0.045571429, 0.526214286, 0.08, 'CB50015.dat'
0.101428571, 0.371428571, 0.22, 'CB50015.dat'
0.207, 0.142857143, 0.39, 'nasasc-718.dat'
0.248357143, 0.107142857, 0.43, 'nasasc2-714.dat'
0.5, 0.053571429, 0.54, 'nasasc2-714.dat'

54
archive/Jacobi/WhettedArea.m Executable file
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%function Area = WhettedArea( fileName, wingSpan )
function WhettedArea(fileName,wingSpan, n)
% fileName = 'AirData.mat';
% wingSpan = 1;
% n = 50;
Area = 0;
pranformArea = 0;
PlanData1 = load(fileName);
PlanData = PlanData1.(fileName(1:end-4));
Chords = findChords(n, PlanData);
for i = 1:(size(PlanData,1)-1)
for j = 1:n
dist = wingSpan*(PlanData{i+1,1}-PlanData{i,1})./n;
Area = Area+findPerim( PlanData{i,4}, Chords(i,j), wingSpan).*dist;
% fprintf('Chord: %f Perimiter: %f Area: %f\n', Chords(i,j), findPerim( PlanData{i,4}, Chords(i,j), wingSpan), Area)
end
end
for i = 1:(size(PlanData,1)-1)
for j = 1:n
dist = wingSpan*(PlanData{i+1,1}-PlanData{i,1})./n;
pranformArea = pranformArea+Chords(i,j).*dist;
% fprintf('Chord: %f pranformArea: %f \n', Chords(i,j), pranformArea)
end
end
WetArea = Area *2;
pranformArea = pranformArea*2;
fprintf('Planform Area: %f, Wetted Area: %f \n', pranformArea, WetArea)
end
function Chords = findChords( n, PlanData )
Chord = cell2mat(PlanData(:,2));
X = cell2mat(PlanData(:,1));
for( i = 1:(length(Chord)-1) )
Xtemp = linspace(X(i),X(i+1),n);
Chords(i,:) = (Chord(i+1)-Chord(i))./(X(i+1)-X(i)).*(Xtemp-X(i))+Chord(i);
end
end
function peri = findPerim( airFile, chord, span)
peri = 0;
Airfoil = load(airFile);
Airfoil = Airfoil*chord*span;
for i = 1:(size(Airfoil,1)-1)
peri = peri + sqrt((Airfoil(i+1,1)-Airfoil(i,1))^2+(Airfoil(i+1,2)-Airfoil(i,2))^2);
end
end

60
archive/Jacobi/WhettedAreaflubbed.m Executable file
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%function Area = WhettedArea( fileName, wingSpan )
function WhettedAreaflubbed(fileName,wingSpan, n)
% fileName = 'AirData.mat';
% wingSpan = 1;
% n = 50;
engineArea=600;
Area = 0;
pranformArea = 0;
cd('\\ad.uiuc.edu\ae\correa2\Desktop\AE441\Matlab code\Jacobi\Planforms')
[spans, chords, offsets, airfoil]=textread(fileName, '%f %f %f %s');
Chords = findChords(n, chords, spans);
cd('\\ad.uiuc.edu\ae\correa2\Desktop\AE441\Matlab code\Jacobi\Airfoils')
for i = 1:(size(chords)-1)
for j = 1:n
Chords(i,j);
dist = wingSpan*(spans(i+1)-spans(i))./n;
Area = Area+findPerim( airfoil{i}, Chords(i,j), wingSpan).*dist;
end
end
for i = 1:(size(chords)-1)
for j = 1:n
dist = wingSpan*(spans(i+1)-spans(i))./n;
pranformArea = pranformArea+Chords(i,j).*dist;
% fprintf('Chord: %f pranformArea: %f \n', Chords(i,j), pranformArea)
end
end
Area = Area *2+engineArea;
WetArea = Area;
pranformArea = pranformArea*2;
fprintf('Planform Area: %f, Wetted Area: %f \n', pranformArea, WetArea)
cd('\\ad.uiuc.edu\ae\correa2\Desktop\AE441\Matlab code\Jacobi\')
end
function Chords = findChords( n, Chord, X )
% Chord = PlanData(:,2);
% X = PlanData(:,1);
for( i = 1:(length(Chord)-1) )
Xtemp = linspace(X(i),X(i+1),n);
Chords(i,:) = (Chord(i+1)-Chord(i))./(X(i+1)-X(i)).*(Xtemp-X(i))+Chord(i);
end
end
function peri = findPerim( airFile, chord, span)
peri = 0;
Airfoil = load(airFile);
Airfoil = Airfoil*chord*span;
for i = 1:(size(Airfoil,1)-1)
peri = peri + sqrt((Airfoil(i+1,1)-Airfoil(i,1))^2+(Airfoil(i+1,2)-Airfoil(i,2))^2);
end
end