NREL's S813 Airfoil (s813-nr)
NREL's S813 Airfoil - NREL HAWT airfoil S813 tip
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(s813-nr) NREL's S813 Airfoil NREL HAWT airfoil S813 tip Max thickness 16% at 40.4% chord. Max camber 2.3% at 54.4% chord Source NWTC National WInd Technology Center Source dat file The dat file is in Selig format |
NREL's S813 Airfoil x/c y/c 1.00000 0.00000 0.99626 0.00057 0.98539 0.00259 0.96820 0.00644 0.94559 0.01202 0.91823 0.01890 0.88649 0.02669 0.85064 0.03527 0.81126 0.04473 0.76921 0.05491 0.72532 0.06549 0.68048 0.07589 0.63530 0.08526 0.58991 0.09277 0.54414 0.09799 0.49785 0.10089 0.45109 0.10174 0.40425 0.10092 0.35786 0.09864 0.31245 0.09505 0.26852 0.09026 0.22656 0.08441 0.18702 0.07761 0.15034 0.07001 0.11693 0.06173 0.08714 0.05294 0.06130 0.04377 0.03971 0.03441 0.02259 0.02504 0.01017 0.01587 0.00261 0.00713 0.00000 0.00000 0.00002 -0.00057 0.00355 -0.00747 0.01332 -0.01450 0.02821 -0.02162 0.04797 -0.02848 0.07237 -0.03492 0.10117 -0.04077 0.13406 -0.04595 0.17071 -0.05036 0.21075 -0.05394 0.25375 -0.05664 0.29926 -0.05843 0.34677 -0.05927 0.39578 -0.05914 0.44572 -0.05801 0.49604 -0.05580 0.54617 -0.05237 0.59573 -0.04745 0.64476 -0.04084 0.69355 -0.03305 0.74176 -0.02508 0.78848 -0.01771 0.83277 -0.01138 0.87364 -0.00638 0.91013 -0.00283 0.94134 -0.00066 0.96649 0.00032 0.98493 0.00047 0.99620 0.00019 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 S813 Airfoil (s813-nr)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| s813-nr | 50,000 | 9 | 23.5 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s813-nr | 50,000 | 5 | 20.4 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s813-nr | 100,000 | 9 | 35.2 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s813-nr | 100,000 | 5 | 34.4 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s813-nr | 200,000 | 9 | 64.8 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s813-nr | 200,000 | 5 | 65.3 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s813-nr | 500,000 | 9 | 104.6 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s813-nr | 500,000 | 5 | 96.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s813-nr | 1,000,000 | 9 | 130.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s813-nr | 1,000,000 | 5 | 115.3 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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