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S3016-095-87 (s3016-il)

S3016-095-87 - Selig S3016 low Reynolds number airfoil


Airfoil s3016-il
Details Dat file Parser  
(s3016-il) S3016-095-87
Selig S3016 low Reynolds number airfoil
Max thickness 9.5% at 28.9% chord.
Max camber 1.8% at 43.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
S3016-095-87
1.00000 0.00000
0.99664 0.00017
0.98669 0.00085
0.97048 0.00233
0.94843 0.00476
0.92107 0.00821
0.88898 0.01266
0.85274 0.01798
0.81299 0.02400
0.77035 0.03047
0.72541 0.03706
0.67865 0.04337
0.63040 0.04917
0.58106 0.05437
0.53112 0.05885
0.48109 0.06252 
0.43144 0.06528
0.38265 0.06707 
0.33517 0.06783
0.28946 0.06755
0.24593 0.06624
0.20504 0.06396
0.16726 0.06066
0.13288 0.05631
0.10216 0.05092
0.07529 0.04459
0.05240 0.03743
0.03358 0.02964
0.01892 0.02146
0.00839 0.01321
0.00203 0.00544
0.00007 -.00095
0.00391 -.00606
0.01386 -.01088
0.02891 -.01543
0.04888 -.01941
0.07362 -.02271
0.10296 -.02526
0.13666 -.02705
0.17444 -.02807
0.21598 -.02839
0.26085 -.02810
0.30857 -.02729
0.35862 -.02604
0.41044 -.02442
0.46345 -.02251
0.51705 -.02040
0.57061 -.01816
0.62352 -.01588
0.67514 -.01363
0.72484 -.01147
0.77202 -.00946
0.81607 -.00763
0.85645 -.00602
0.89264 -.00462
0.92414 -.00344
0.95055 -.00242
0.97154 -.00148
0.98700 -.00063
0.99668 -.00012
1.00000 0.00000
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Polars for S3016-095-87 (s3016-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s3016-il50,000931.8 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s3016-il50,000534.9 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s3016-il100,000949.2 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s3016-il100,000548.5 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   s3016-il200,000965.7 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s3016-il200,000561 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   s3016-il500,000985.5 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   s3016-il500,000578.8 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   s3016-il1,000,000999.1 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s3016-il1,000,000593.3 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
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