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S4062-095-87 (s4062-il)

S4062-095-87 - Selig S4062 low Reynolds number airfoil


Airfoil s4062-il
Details Dat file Parser  
(s4062-il) S4062-095-87
Selig S4062 low Reynolds number airfoil
Max thickness 9.5% at 31.7% chord.
Max camber 4% at 50.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
S4062-095-87
1.00000 0.00000
0.99671 0.00041
0.98696 0.00178
0.97107 0.00438
0.94954 0.00836
0.92297 0.01374
0.89200 0.02036
0.85727 0.02799
0.81936 0.03628
0.77881 0.04487
0.73609 0.05339
0.69165 0.06147
0.64586 0.06881
0.59909 0.07513
0.55168 0.08024
0.50397 0.08399
0.45626 0.08630
0.40887 0.08717
0.36217 0.08673
0.31661 0.08510
0.27271 0.08239
0.23092 0.07864
0.19171 0.07393
0.15550 0.06828
0.12259 0.06173
0.09326 0.05435
0.06769 0.04627
0.04604 0.03765
0.02843 0.02876
0.01499 0.01986
0.00578 0.01124
0.00081 0.00339
0.00061 -.00262
0.00608 -.00725
0.01719 -.01145
0.03342 -.01482
0.05470 -.01716
0.08097 -.01844
0.11211 -.01868
0.14793 -.01800
0.18813 -.01659
0.23229 -.01462
0.27993 -.01224
0.33049 -.00965
0.38336 -.00700
0.43788 -.00441
0.49336 -.00199
0.54909 0.00015
0.60436 0.00196
0.65845 0.00337
0.71066 0.00437
0.76031 0.00495
0.80673 0.00511
0.84932 0.00491
0.88751 0.00439
0.92078 0.00364
0.94869 0.00273
0.97086 0.00178
0.98695 0.00090
0.99673 0.00025
1.00000 0.00000
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Polars for S4062-095-87 (s4062-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s4062-il50,000938.7 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   s4062-il50,000538.4 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   s4062-il100,000962.7 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   s4062-il100,000561.9 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   s4062-il200,000990.5 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   s4062-il200,000586.3 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   s4062-il500,0009128.5 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s4062-il500,0005114.5 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   s4062-il1,000,0009155 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s4062-il1,000,0005131 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
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