NREL's S810 Airfoil (s810-nr)
NREL's S810 Airfoil - NREL HAWT airfoil S810 tip
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(s810-nr) NREL's S810 Airfoil NREL HAWT airfoil S810 tip Max thickness 18% at 44.2% chord. Max camber 0.9% at 10.9% chord Source NWTC National WInd Technology Center Source dat file The dat file is in Selig format |
NREL's S810 Airfoil x/c y/c 1.00000 0.00000 0.99626 0.00044 0.98531 0.00205 0.96786 0.00522 0.94473 0.00994 0.91657 0.01593 0.88380 0.02289 0.84676 0.03078 0.80612 0.03971 0.76278 0.04960 0.71769 0.06015 0.67191 0.07091 0.62652 0.08079 0.58155 0.08816 0.53586 0.09249 0.48909 0.09466 0.44186 0.09515 0.39470 0.09415 0.34815 0.09179 0.30273 0.08820 0.25895 0.08349 0.21727 0.07777 0.17816 0.07118 0.14205 0.06384 0.10934 0.05589 0.08038 0.04747 0.05550 0.03874 0.03497 0.02989 0.01903 0.02110 0.00786 0.01261 0.00163 0.00470 0.00000 0.00000 0.00031 -0.00183 0.00573 -0.00687 0.01878 -0.01197 0.03790 -0.01805 0.06237 -0.02507 0.09136 -0.03299 0.12403 -0.04145 0.15989 -0.04991 0.19860 -0.05809 0.23960 -0.06584 0.28221 -0.07277 0.32604 -0.07833 0.37090 -0.08224 0.41642 -0.08442 0.46207 -0.08459 0.50762 -0.08229 0.55310 -0.07728 0.59877 -0.06938 0.64530 -0.05915 0.69265 -0.04792 0.74000 -0.03683 0.78635 -0.02660 0.83065 -0.01778 0.87180 -0.01070 0.90873 -0.00550 0.94044 -0.00213 0.96603 -0.00036 0.98478 0.00022 0.99618 0.00013 1.00000 0.00000 |
Dat file parser warnings
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Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file |
Similar airfoils
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Polars for NREL's S810 Airfoil (s810-nr)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| s810-nr | 50,000 | 9 | 20.7 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s810-nr | 50,000 | 5 | 16.5 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s810-nr | 100,000 | 9 | 24.9 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s810-nr | 100,000 | 5 | 27.1 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s810-nr | 200,000 | 9 | 50 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s810-nr | 200,000 | 5 | 52.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s810-nr | 500,000 | 9 | 83.2 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s810-nr | 500,000 | 5 | 77.2 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s810-nr | 1,000,000 | 9 | 105.4 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s810-nr | 1,000,000 | 5 | 92.5 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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