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Curtis C-72 (curtisc72-il)

Curtis C-72 - Curtis C-72 airfoil


Airfoil curtisc72-il
Details Dat file Parser  
(curtisc72-il) Curtis C-72
Curtis C-72 airfoil
Max thickness 11.7% at 30% chord.
Max camber 3.8% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
Curtis C-72
1.0000     0.0010
0.9500     0.0152
0.9000     0.0280
0.8000     0.0523
0.7000     0.0736
0.6000     0.0915
0.5000     0.1053
0.4000     0.1141
0.3000     0.1173
0.2000     0.1136
0.1500     0.1069
0.1000     0.0960
0.0750     0.0885
0.0500     0.0789
0.0250     0.0651
0.0125     0.0555
0.0000     0.0349
0.0125     0.0192
0.0250     0.0147
0.0500     0.0093
0.0750     0.0064
0.1000     0.0043
0.1500     0.0016
0.2000     0.0003
0.3000     0.0000
0.4000     0.0021
0.5000     0.0059
0.6000     0.0085
0.7000     0.0091
0.8000     0.0072
0.9000     0.0040
0.9500     0.0021
1.0000     0.0000
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Selig format dat file

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Polars for Curtis C-72 (curtisc72-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   curtisc72-il50,000929.9 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   curtisc72-il50,000537.8 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   curtisc72-il100,000954.7 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   curtisc72-il100,000556.5 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   curtisc72-il200,000976.3 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   curtisc72-il200,000573.3 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   curtisc72-il500,0009103.4 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   curtisc72-il500,000595.5 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   curtisc72-il1,000,0009121 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   curtisc72-il1,000,0005114.4 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
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