S1014 (s1014-il)
S1014 - Selig S1014 HPV airfoil
| Details | Dat file | Parser | |
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(s1014-il) S1014 Selig S1014 HPV airfoil Max thickness 16.5% at 42.2% chord. Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
S1014
1.00000 0.00000
0.99610 0.00022
0.98465 0.00119
0.96622 0.00341
0.94151 0.00710
0.91119 0.01238
0.87604 0.01936
0.83705 0.02802
0.79532 0.03806
0.75202 0.04895
0.70829 0.05951
0.66413 0.06797
0.61835 0.07380
0.57065 0.07784
0.52167 0.08056
0.47199 0.08210
0.42222 0.08254
0.37293 0.08195
0.32472 0.08040
0.27812 0.07791
0.23370 0.07455
0.19197 0.07037
0.15346 0.06540
0.11862 0.05966
0.08788 0.05315
0.06153 0.04581
0.03978 0.03765
0.02271 0.02873
0.01032 0.01922
0.00265 0.00944
0.00000 0.00000
0.00265 -0.00944
0.01032 -0.01922
0.02271 -0.02873
0.03978 -0.03765
0.06153 -0.04581
0.08788 -0.05315
0.11862 -0.05966
0.15346 -0.06540
0.19197 -0.07037
0.23370 -0.07455
0.27812 -0.07791
0.32472 -0.08040
0.37293 -0.08195
0.42222 -0.08254
0.47199 -0.08210
0.52167 -0.08056
0.57065 -0.07784
0.61835 -0.07380
0.66413 -0.06797
0.70829 -0.05951
0.75202 -0.04895
0.79532 -0.03806
0.83705 -0.02802
0.87604 -0.01936
0.91119 -0.01238
0.94151 -0.00710
0.96622 -0.00341
0.98465 -0.00119
0.99610 -0.00022
1.00000 0.00000
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Polars for S1014 (s1014-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| s1014-il | 50,000 | 9 | 27 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s1014-il | 50,000 | 5 | 20.3 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s1014-il | 100,000 | 9 | 38.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s1014-il | 100,000 | 5 | 23.2 at α=10.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s1014-il | 200,000 | 9 | 33.7 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s1014-il | 200,000 | 5 | 30.3 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s1014-il | 500,000 | 9 | 45.8 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s1014-il | 500,000 | 5 | 42 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s1014-il | 1,000,000 | 9 | 54.9 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s1014-il | 1,000,000 | 5 | 52.6 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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