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SELIG 3002-099-83 (s3002-il)

SELIG 3002-099-83 - Selig S3002 low Reynolds number airfoil


Airfoil s3002-il
Details Dat file Parser  
(s3002-il) SELIG 3002-099-83
Selig S3002 low Reynolds number airfoil
Max thickness 9.9% at 30.6% chord.
Max camber 2.3% at 49.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
 SELIG 3002-099-83
1.00000 0.00000
0.99676 0.00048
0.98723 0.00205
0.97191 0.00483
0.95131 0.00867
0.92576 0.01330
0.89553 0.01862
0.86104 0.02463
0.82286 0.03124
0.78161 0.03825
0.73787 0.04538
0.69214 0.05226
0.64481 0.05868
0.59634 0.06441
0.54711 0.06930
0.49758 0.07328
0.44820 0.07627
0.39944 0.07823
0.35178 0.07915
0.30572 0.07900
0.26173 0.07776
0.22026 0.07537
0.18165 0.07181
0.14619 0.06711
0.11417 0.06135
0.08583 0.05460
0.06135 0.04701
0.04087 0.03873
0.02450 0.03000
0.01234 0.02105
0.00440 0.01211
0.00048 0.00360
0.00051 -.00333
0.00602 -.00831
0.01778 -.01223
0.03507 -.01544
0.05763 -.01796
0.08522 -.01976
0.11761 -.02087
0.15449 -.02145
0.19537 -.02159
0.23976 -.02136
0.28711 -.02078
0.33684 -.01988
0.38835 -.01869
0.44102 -.01717
0.49424 -.01527
0.54750 -.01294
0.60027 -.01020
0.65199 -.00697
0.70250 -.00311
0.75186 0.00081
0.79932 0.00382
0.84366 0.00550
0.88373 0.00590
0.91863 0.00527
0.94770 0.00402
0.97052 0.00257
0.98688 0.00125
0.99672 0.00033
1.00000 0.00000
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Polars for SELIG 3002-099-83 (s3002-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s3002-il50,000935.3 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s3002-il50,000539.2 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   s3002-il100,000956.3 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s3002-il100,000555.8 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   s3002-il200,000976.6 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s3002-il200,000570.8 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s3002-il500,000999.8 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   s3002-il500,000589.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s3002-il1,000,0009112.5 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s3002-il1,000,0005100.1 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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