NREL's S834 Airfoil (s834-nr)
NREL's S834 Airfoil - NREL HAWT airfoil S834 tip 15.0% Dia=1 to 3 m Re=4.0E+5 Clmax(S)=1.00 Clmax(R)=1.02 High max lift coef
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(s834-nr) NREL's S834 Airfoil NREL HAWT airfoil S834 tip 15.0% Dia=1 to 3 m Re=4.0E+5 Clmax(S)=1.00 Clmax(R)=1.02 High max lift coef Max thickness 15% at 39.5% chord. Max camber 1.6% at 60% chord Source NWTC National WInd Technology Center Source dat file The dat file is in Selig format |
NREL's S834 Airfoil x/c y/c 1.000000 0.000000 0.996064 0.000606 0.984816 0.003101 0.967539 0.007914 0.945483 0.014649 0.919407 0.022470 0.889501 0.030561 0.855652 0.038699 0.818293 0.046926 0.777966 0.055030 0.735169 0.062727 0.690338 0.069726 0.643856 0.075777 0.596064 0.080708 0.547330 0.084531 0.498288 0.087141 0.449272 0.088341 0.400592 0.088199 0.352742 0.086855 0.306248 0.084371 0.261604 0.080802 0.219296 0.076196 0.179743 0.070615 0.143372 0.064126 0.110502 0.056817 0.081485 0.048795 0.056518 0.040187 0.035873 0.031189 0.019660 0.022005 0.008118 0.012967 0.001394 0.004469 0.001039 0.003754 0.000308 0.001855 0.000001 0.000091 0.000250 -0.001671 0.000632 -0.002862 0.000915 -0.003559 0.006099 -0.010998 0.016371 -0.019451 0.031347 -0.027791 0.050767 -0.035619 0.074629 -0.042738 0.102659 -0.048948 0.134765 -0.054145 0.170598 -0.058239 0.209956 -0.061194 0.252411 -0.062996 0.297656 -0.063666 0.345187 -0.063248 0.394605 -0.061807 0.445343 -0.059431 0.496925 -0.056213 0.548737 -0.052268 0.600249 -0.047696 0.650829 -0.042590 0.699974 -0.037023 0.747128 -0.031105 0.791833 -0.024939 0.833594 -0.018671 0.872254 -0.012170 0.907866 -0.006512 0.939211 -0.002526 0.965020 -0.000329 0.984215 0.000393 0.996021 0.000244 1.000000 0.000000 |
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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 S834 Airfoil (s834-nr)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| s834-nr | 50,000 | 9 | 29.8 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s834-nr | 50,000 | 5 | 26.6 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s834-nr | 100,000 | 9 | 47.4 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s834-nr | 100,000 | 5 | 44.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s834-nr | 200,000 | 9 | 70.6 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s834-nr | 200,000 | 5 | 55.5 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s834-nr | 500,000 | 9 | 81.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s834-nr | 500,000 | 5 | 74.4 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s834-nr | 1,000,000 | 9 | 102.7 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s834-nr | 1,000,000 | 5 | 83.5 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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