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S3010-103-84 (s3010-il)

S3010-103-84 - Selig S3010 low Reynolds number airfoil


Airfoil s3010-il
Details Dat file Parser  
(s3010-il) S3010-103-84
Selig S3010 low Reynolds number airfoil
Max thickness 10.3% at 25% chord.
Max camber 2.3% at 43.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
S3010-103-84
1.00000 0.00000
0.99674 0.00027
0.98706 0.00118
0.97122 0.00293
0.94959 0.00564
0.92264 0.00936
0.89090 0.01405
0.85493 0.01960
0.81531 0.02585
0.77261 0.03259
0.72739 0.03958
0.68021 0.04658
0.63158 0.05337
0.58203 0.05971
0.53204 0.06541
0.48213 0.07029
0.43275 0.07422
0.38438 0.07706
0.33750 0.07870
0.29250 0.07902
0.24970 0.07796
0.20944 0.07556
0.17206 0.07184
0.13785 0.06689
0.10706 0.06076
0.07990 0.05360
0.05655 0.04556
0.03713 0.03683
0.02173 0.02766
0.01042 0.01835
0.00319 0.00927
0.00005 0.00100
0.00181 -.00543
0.00932 -.01048
0.02239 -.01506
0.04061 -.01894
0.06381 -.02203
0.09180 -.02427
0.12435 -.02567
0.16119 -.02625
0.20200 -.02610
0.24635 -.02531
0.29376 -.02399
0.34371 -.02221
0.39565 -.02009
0.44899 -.01769
0.50312 -.01514
0.55743 -.01252
0.61127 -.00994
0.66399 -.00749
0.71495 -.00526
0.76350 -.00332
0.80901 -.00172
0.85087 -.00051
0.88851 0.00031
0.92140 0.00075
0.94905 0.00086
0.97104 0.00072
0.98703 0.00042
0.99674 0.00013
1.00000 0.00000
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Polars for S3010-103-84 (s3010-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s3010-il50,000928.5 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   s3010-il50,000536.2 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   s3010-il100,000950.2 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s3010-il100,000552.8 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   s3010-il200,000970 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s3010-il200,000568.8 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   s3010-il500,000995.8 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s3010-il500,000589.2 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   s3010-il1,000,0009113.5 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s3010-il1,000,0005104.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
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