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Anthony Correa
2010-04-17 12:00:00 -05:00
commit ecb6c5bb6b
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*/.DS_Store
*/Thumbs.db
XFLR Outputs/Trade Study planform/Thumbs.db
Planforms/Temp/Thumbs.db
Matlab code/strut/Thumbs.db
Matlab code/Excel Files/Thumbs.db

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73
Airfoils/CB600175b.dat Executable file
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73
Airfoils/CB600185b.dat Executable file
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73
Airfoils/CB600185c.dat Executable file
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73
Airfoils/CB600185d.dat Executable file
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73
Airfoils/CB60019c.dat Executable file
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75
Airfoils/SAX.dat Executable file
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59
Airfoils/SAX2.dat Executable file
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59
Airfoils/SAX3.dat Executable file
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Airfoils/SAX4.dat Executable file
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1 0

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Airfoils/SAX4A.dat Executable file
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0.9973 0.0053

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Airfoils/dsma523a.dat Executable file
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Airfoils/n0011sc.dat Executable file
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1 0
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33
Airfoils/n0012.dat Executable file
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33
Airfoils/n001264.dat Executable file
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73
Airfoils/n00155sc.dat Executable file
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Airfoils/n00165sc.dat Executable file
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73
Airfoils/n00175sc.dat Executable file
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73
Airfoils/n00185sc.dat Executable file
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35
Airfoils/n2410.dat Executable file
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103
Airfoils/n2612.dat Executable file
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103
Airfoils/n2616.dat Executable file
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Airfoils/nasasc0714.dat Executable file
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97
Airfoils/nasasc0716.dat Executable file
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0 85 0 CB600155a.dat
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80 5 89 nasasc0714.dat

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Excel Files/FDR013.txt Executable file
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wingspan 160
M_cruise 0.8
M_landing 0.2
cLalpha_cruise 0.0567
cL0 0.1422
cMalpha_cruise -0.06
cM0 -0.1919
efficiency 0.8872
alt_cruise 35000
weight_cruise 160000
cd_correction 0
c_f 0.003

14
Excel Files/FDR013b.txt Executable file
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QFLR5 v0.04 Beta
Wing name : sFD R013
Wing polar name : T1- 105.0 ft/ s-VLM2- 0. 00ft-Invisc id
Freestream speed : 104 .990 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
0 0.197841 0.002619 0 0.002619 0 -0.267136 0 0 0 32.001 0.1217
1 0.254737 0.00402 0 0.00402 0 -0.327464 0 0 0 32.001 0.1159
2 0.311422 0.005817 0 0.005817 0 -0.387557 0 0 0 32.001 0.1123
3 0.367837 0.008003 0 0.008003 0 -0.447341 0 0 0 32.001 0.1098
4 0.423924 0.010575 0 0.010575 0 -0.506744 0 0 0 32.001 0.108
5 0.479626 0.013523 0 0.013523 0 -0.565693 0 0 0 32.001 0.1067

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28.98 20 45 nasasc0718.dat
34.77 15 50 nasasc0714.dat
80 5 89 nasasc0714.dat

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