NREL's S803 Airfoil (s803-nr)
NREL's S803 Airfoil - NREL HAWT airfoil S803 tip Not recommended
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(s803-nr) NREL's S803 Airfoil NREL HAWT airfoil S803 tip Not recommended Max thickness 11.5% at 37.5% chord. Max camber 3.7% at 46.9% chord Source NWTC National WInd Technology Center Source dat file The dat file is in Selig format |
NREL's S803 Airfoil x/c y/c 1.00000 0.00000 0.99672 0.00104 0.98752 0.00419 0.97347 0.00901 0.95487 0.01456 0.93147 0.02042 0.90331 0.02674 0.87082 0.03353 0.83447 0.04070 0.79474 0.04813 0.75218 0.05567 0.70734 0.06313 0.66079 0.07032 0.61309 0.07700 0.56482 0.08294 0.51650 0.08787 0.46867 0.09142 0.42154 0.09317 0.37507 0.09307 0.32949 0.09145 0.28530 0.08852 0.24294 0.08441 0.20288 0.07924 0.16551 0.07312 0.13124 0.06618 0.10042 0.05855 0.07336 0.05035 0.05033 0.04173 0.03153 0.03281 0.01712 0.02375 0.00715 0.01471 0.00150 0.00601 0.00000 0.00000 0.00015 -0.00171 0.00403 -0.00766 0.01376 -0.01232 0.02903 -0.01634 0.04957 -0.01961 0.07517 -0.02214 0.10557 -0.02393 0.14046 -0.02503 0.17946 -0.02547 0.22215 -0.02534 0.26803 -0.02469 0.31654 -0.02359 0.36706 -0.02207 0.41897 -0.02011 0.47161 -0.01766 0.52431 -0.01448 0.57686 -0.01011 0.62958 -0.00479 0.68219 0.00056 0.73384 0.00524 0.78358 0.00882 0.83044 0.01101 0.87344 0.01163 0.91147 0.01059 0.94336 0.00823 0.96830 0.00530 0.98600 0.00259 0.99652 0.00069 1.00000 0.00000 |
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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 S803 Airfoil (s803-nr)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| s803-nr | 50,000 | 9 | 38.6 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s803-nr | 50,000 | 5 | 37.1 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s803-nr | 100,000 | 9 | 63.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s803-nr | 100,000 | 5 | 63 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s803-nr | 200,000 | 9 | 89.5 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s803-nr | 200,000 | 5 | 83.8 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s803-nr | 500,000 | 9 | 118.4 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s803-nr | 500,000 | 5 | 108.1 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s803-nr | 1,000,000 | 9 | 140.3 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s803-nr | 1,000,000 | 5 | 124 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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