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S3025 9.38% (s3025-il)

S3025 9.38% - Selig S3025 low Reynolds number airfoil


Airfoil s3025-il
Details Dat file Parser  
(s3025-il) S3025 9.38%
Selig S3025 low Reynolds number airfoil
Max thickness 9.4% at 30.9% chord.
Max camber 3% at 44.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
S3025 9.38%    
 1.00000  0.0    
 0.99665  0.00052
 0.98690  0.00223
 0.97140  0.00529
 0.95078  0.00949
 0.92545  0.01444
 0.89560  0.01985
 0.86145  0.02571
 0.82348  0.03199
 0.78221  0.03861
 0.73820  0.04543
 0.69203  0.05228
 0.64430  0.05897
 0.59562  0.06525
 0.54650  0.07083
 0.49741  0.07546
 0.44874  0.07893
 0.40085  0.08112
 0.35411  0.08199
 0.30891  0.08150
 0.26559  0.07972
 0.22456  0.07671
 0.18621  0.07252
 0.15085  0.06718
 0.11876  0.06079
 0.09017  0.05351
 0.06529  0.04547
 0.04428  0.03688
 0.02725  0.02796
 0.01428  0.01901
 0.00535  0.01041
 0.00053  0.00282
 0.00072 -0.00273
 0.00682 -0.00678
 0.01868 -0.01030
 0.03593 -0.01310
 0.05838 -0.01510
 0.08590 -0.01630
 0.11824 -0.01676
 0.15511 -0.01654
 0.19615 -0.01576
 0.24094 -0.01454
 0.28898 -0.01301
 0.33970 -0.01129
 0.39248 -0.00950
 0.44667 -0.00773
 0.50160 -0.00605
 0.55659 -0.00449
 0.61096 -0.00312
 0.66404 -0.00195
 0.71516 -0.00100
 0.76370 -0.00026
 0.80906  0.00027
 0.85068  0.00061
 0.88803  0.00077
 0.92062  0.00084
 0.94812  0.00088
 0.97024  0.00081
 0.98655  0.00056
 0.99661  0.00019
 1.00001  0.00000
Dat file parser warnings
  • Line 62 - X value too large but included: 1.00001 0.00000
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Polars for S3025 9.38% (s3025-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s3025-il50,000933.9 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s3025-il50,000539.2 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   s3025-il100,000957 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   s3025-il100,000558.7 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   s3025-il200,000980 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   s3025-il200,000577.1 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   s3025-il500,0009109.7 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   s3025-il500,000599.4 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   s3025-il1,000,0009130.2 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s3025-il1,000,0005114.3 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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