NREL's S805A Airfoil (s805a-nr)
NREL's S805A Airfoil - NREL HAWT airfoil S805A primary
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(s805a-nr) NREL's S805A Airfoil NREL HAWT airfoil S805A primary Max thickness 13.5% at 40% chord. Max camber 2.1% at 35% chord Source NWTC National WInd Technology Center Source dat file The dat file is in Selig format |
NREL's S805A Airfoil x/c y/c 1.00000 0.00000 0.98999 0.00155 0.97999 0.00344 0.97000 0.00551 0.95000 0.00984 0.93001 0.01414 0.90001 0.02014 0.85000 0.02918 0.80000 0.03779 0.75000 0.04626 0.70000 0.05461 0.65001 0.06273 0.60001 0.07048 0.55002 0.07756 0.50002 0.08340 0.45001 0.08732 0.40000 0.08893 0.35000 0.08831 0.30000 0.08579 0.24999 0.08144 0.19998 0.07514 0.14998 0.06657 0.11997 0.06007 0.09995 0.05500 0.07997 0.04920 0.05998 0.04241 0.04991 0.03849 0.03998 0.03416 0.02988 0.02914 0.01992 0.02331 0.00998 0.01581 0.00269 0.00731 0.00000 0.00000 0.00001 -0.00031 0.00296 -0.00619 0.00997 -0.01061 0.01994 -0.01432 0.02998 -0.01737 0.03995 -0.01976 0.05000 -0.02178 0.05998 -0.02359 0.07999 -0.02675 0.09999 -0.02942 0.11999 -0.03175 0.14999 -0.03475 0.19999 -0.03876 0.25000 -0.04180 0.30000 -0.04401 0.35000 -0.04547 0.40000 -0.04620 0.45000 -0.04600 0.50000 -0.04546 0.55000 -0.04384 0.60001 -0.04108 0.65001 -0.03696 0.70001 -0.03156 0.75000 -0.02519 0.80000 -0.01816 0.84999 -0.01111 0.89999 -0.00499 0.92999 -0.00212 0.95000 -0.00069 0.97000 0.00021 0.98000 0.00040 0.99000 0.00036 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 S805A Airfoil (s805a-nr)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| s805a-nr | 50,000 | 9 | 30.1 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s805a-nr | 50,000 | 5 | 27.1 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s805a-nr | 100,000 | 9 | 50.9 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s805a-nr | 100,000 | 5 | 50.6 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s805a-nr | 200,000 | 9 | 75.6 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s805a-nr | 200,000 | 5 | 67 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s805a-nr | 500,000 | 9 | 96.9 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s805a-nr | 500,000 | 5 | 89.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s805a-nr | 1,000,000 | 9 | 117.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s805a-nr | 1,000,000 | 5 | 103.3 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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