NREL's S808 Airfoil (s808-nr)
NREL's S808 Airfoil - NREL HAWT airfoil S808 root
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(s808-nr) NREL's S808 Airfoil NREL HAWT airfoil S808 root Max thickness 21% at 24.4% chord. Max camber 2.4% at 72.9% chord Source NWTC National WInd Technology Center Source dat file The dat file is in Selig format |
NREL's S808 Airfoil x/c y/c 1.00000 0.00000 0.99633 0.00084 0.98573 0.00362 0.96918 0.00846 0.94763 0.01493 0.92165 0.02226 0.89127 0.02978 0.85638 0.03736 0.81729 0.04519 0.77460 0.05331 0.72894 0.06161 0.68096 0.06992 0.63130 0.07806 0.58062 0.08579 0.52953 0.09289 0.47862 0.09910 0.42844 0.10417 0.37948 0.10789 0.33221 0.11006 0.28703 0.11052 0.24429 0.10916 0.20429 0.10593 0.16731 0.10081 0.13357 0.09387 0.10327 0.08522 0.07657 0.07503 0.05363 0.06354 0.03461 0.05102 0.01961 0.03773 0.00869 0.02407 0.00201 0.01058 0.00000 0.00000 0.00007 -0.00200 0.00384 -0.01426 0.01303 -0.02715 0.02656 -0.04024 0.04411 -0.05308 0.06534 -0.06531 0.08991 -0.07653 0.11748 -0.08631 0.14770 -0.09408 0.18060 -0.09915 0.21648 -0.10128 0.25536 -0.10051 0.29732 -0.09686 0.34238 -0.09071 0.39026 -0.08249 0.44063 -0.07262 0.49310 -0.06161 0.54712 -0.05000 0.60208 -0.03836 0.65719 -0.02729 0.71158 -0.01731 0.76425 -0.00887 0.81414 -0.00231 0.86013 0.00219 0.90112 0.00465 0.93608 0.00525 0.96412 0.00432 0.98431 0.00244 0.99616 0.00068 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 S808 Airfoil (s808-nr)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| s808-nr | 50,000 | 9 | 8.2 at α=0° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s808-nr | 50,000 | 5 | 24.6 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s808-nr | 100,000 | 9 | 36.5 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s808-nr | 100,000 | 5 | 41.4 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s808-nr | 200,000 | 9 | 55.1 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s808-nr | 200,000 | 5 | 56 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s808-nr | 500,000 | 9 | 78.9 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s808-nr | 500,000 | 5 | 76.6 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s808-nr | 1,000,000 | 9 | 98.5 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s808-nr | 1,000,000 | 5 | 92.8 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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