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NREL's S802 Airfoil (s802-nr)

NREL's S802 Airfoil - NREL HAWT airfoil S802 tip Not recommended


Airfoil s802-nr
Details Dat file Parser  
(s802-nr) NREL's S802 Airfoil
NREL HAWT airfoil S802 tip Not recommended
Max thickness 11.5% at 37.9% chord.
Max camber 3.8% at 47.3% chord
Source NWTC National WInd Technology Center
Source dat file
The dat file is in Selig format
NREL's S802 Airfoil
  x/c       y/c
1.00000   0.00000
0.99666   0.00105
0.98730   0.00427
0.97302   0.00923
0.95416   0.01500
0.93048   0.02120
0.90208   0.02796
0.86941   0.03531
0.83300   0.04314
0.79337   0.05129
0.75111   0.05957
0.70680   0.06774
0.66104   0.07551
0.61441   0.08255
0.56748   0.08838
0.52044   0.09240
0.47311   0.09451
0.42569   0.09504
0.37871   0.09421
0.33264   0.09212
0.28798   0.08885
0.24520   0.08451
0.20474   0.07918
0.16702   0.07297
0.13242   0.06598
0.10132   0.05833
0.07401   0.05015
0.05078   0.04156
0.03182   0.03269
0.01729   0.02369
0.00724   0.01471
0.00153   0.00605
0.00000   0.00000
0.00014  -0.00164
0.00397  -0.00754
0.01367  -0.01210
0.02895  -0.01600
0.04956  -0.01913
0.07528  -0.02152
0.10587  -0.02318
0.14099  -0.02415
0.18029  -0.02450
0.22333  -0.02431
0.26960  -0.02365
0.31857  -0.02259
0.36963  -0.02117
0.42216  -0.01945
0.47551  -0.01744
0.52901  -0.01512
0.58198  -0.01237
0.63388  -0.00891
0.68470  -0.00444
0.73467   0.00047
0.78328   0.00483
0.82950   0.00798
0.87227   0.00955
0.91038   0.00932
0.94251   0.00756
0.96777   0.00501
0.98575   0.00250
0.99646   0.00067
1.00000   0.00000
Dat file parser warnings
  • Line 2 - Invalid characters : x/c y/c
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Polars for NREL's S802 Airfoil (s802-nr)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s802-nr50,000936.7 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s802-nr50,000533.8 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   s802-nr100,000961 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s802-nr100,000560.2 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   s802-nr200,000991.3 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s802-nr200,000585.7 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   s802-nr500,0009124.3 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s802-nr500,0005113.6 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s802-nr1,000,0009149.5 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   s802-nr1,000,0005132.5 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
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