NREL's S807 Airfoil (s807-nr)
NREL's S807 Airfoil - NREL HAWT airfoil S807 root
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(s807-nr) NREL's S807 Airfoil NREL HAWT airfoil S807 root Max thickness 18% at 28.7% chord. Max camber 1.9% at 78.3% chord Source NWTC National WInd Technology Center Source dat file The dat file is in Selig format |
NREL's S807 Airfoil x/c y/c 1.00000 0.00000 0.99646 0.00082 0.98629 0.00351 0.97045 0.00810 0.94987 0.01410 0.92503 0.02067 0.89590 0.02712 0.86227 0.03329 0.82433 0.03941 0.78256 0.04554 0.73751 0.05167 0.68974 0.05777 0.63986 0.06376 0.58850 0.06958 0.53634 0.07514 0.48405 0.08033 0.43231 0.08503 0.38181 0.08909 0.33324 0.09233 0.28733 0.09444 0.24461 0.09497 0.20533 0.09343 0.16944 0.08940 0.13650 0.08294 0.10642 0.07466 0.07953 0.06509 0.05614 0.05453 0.03650 0.04332 0.02084 0.03177 0.00939 0.02024 0.00237 0.00909 0.00000 0.00000 0.00003 -0.00105 0.00364 -0.01032 0.01334 -0.01969 0.02802 -0.02928 0.04736 -0.03877 0.07102 -0.04800 0.09863 -0.05674 0.12982 -0.06479 0.16418 -0.07192 0.20129 -0.07791 0.24069 -0.08252 0.28191 -0.08547 0.32444 -0.08628 0.36824 -0.08429 0.41366 -0.07933 0.46091 -0.07162 0.51026 -0.06166 0.56158 -0.05048 0.61419 -0.03902 0.66725 -0.02798 0.71982 -0.01798 0.77085 -0.00950 0.81926 -0.00289 0.86392 0.00170 0.90376 0.00427 0.93778 0.00500 0.96509 0.00420 0.98477 0.00238 0.99628 0.00066 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 S807 Airfoil (s807-nr)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| s807-nr | 50,000 | 9 | 20.3 at α=1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s807-nr | 50,000 | 5 | 22 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s807-nr | 100,000 | 9 | 33.4 at α=12.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s807-nr | 100,000 | 5 | 40.3 at α=10.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s807-nr | 200,000 | 9 | 56.4 at α=11.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s807-nr | 200,000 | 5 | 59.4 at α=10.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s807-nr | 500,000 | 9 | 84.9 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s807-nr | 500,000 | 5 | 83.9 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s807-nr | 1,000,000 | 9 | 106.7 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s807-nr | 1,000,000 | 5 | 101.7 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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