NREL's S804 Airfoil (s804-nr)
NREL's S804 Airfoil - NREL HAWT airfoil S804 root Not recommended
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(s804-nr) NREL's S804 Airfoil NREL HAWT airfoil S804 root Not recommended Max thickness 17.9% at 26.7% chord. Max camber 4.2% at 39.6% chord Source NWTC National WInd Technology Center Source dat file The dat file is in Selig format |
NREL's S804 Airfoil x/c y/c 1.00000 0.00000 0.99659 0.00112 0.98671 0.00456 0.97177 0.00986 0.95200 0.01602 0.92709 0.02265 0.89711 0.02997 0.86356 0.03804 0.82396 0.04680 0.78189 0.05614 0.73698 0.06590 0.68988 0.07589 0.64123 0.08586 0.59168 0.09554 0.54185 0.10464 0.49232 0.11286 0.44364 0.11989 0.39631 0.12544 0.35078 0.12924 0.30747 0.13100 0.26675 0.13039 0.22859 0.12692 0.19259 0.12071 0.15872 0.11238 0.12736 0.10239 0.09883 0.09108 0.07346 0.07874 0.05152 0.06568 0.03324 0.05216 0.01884 0.03851 0.00844 0.02501 0.00214 0.01202 0.00000 0.00000 0.00211 -0.01023 0.00979 -0.01840 0.02369 -0.02532 0.04296 -0.03149 0.06722 -0.03684 0.09612 -0.04128 0.12932 -0.04477 0.16642 -0.04726 0.20699 -0.04872 0.25053 -0.04910 0.29650 -0.04831 0.34431 -0.04611 0.39371 -0.04204 0.44492 -0.03606 0.49798 -0.02873 0.55244 -0.02079 0.60763 -0.01281 0.66280 -0.00532 0.71708 0.00121 0.76952 0.00635 0.81912 0.00982 0.86483 0.01136 0.90540 0.01186 0.93949 0.00867 0.96615 0.00568 0.98507 0.00280 0.99629 0.00075 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 S804 Airfoil (s804-nr)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| s804-nr | 50,000 | 9 | 4.8 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s804-nr | 50,000 | 5 | 22.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s804-nr | 100,000 | 9 | 28.6 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s804-nr | 100,000 | 5 | 45.2 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s804-nr | 200,000 | 9 | 58.2 at α=11.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s804-nr | 200,000 | 5 | 67.9 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s804-nr | 500,000 | 9 | 98.1 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s804-nr | 500,000 | 5 | 98.6 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s804-nr | 1,000,000 | 9 | 128 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s804-nr | 1,000,000 | 5 | 125.5 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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