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S8055 (12%) (s8055-il)

S8055 (12%) - Selig S8055 (12%) low Reynolds number airfoil


Airfoil s8055-il
Details Dat file Parser  
(s8055-il) S8055 (12%)
Selig S8055 (12%) low Reynolds number airfoil
Max thickness 12% at 33.9% chord.
Max camber 1.6% at 44.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
S8055 (12%) 
       1.00000      .00000
        .99796      .00016
        .99197      .00081
        .98231      .00211
        .96923      .00407
        .95291      .00666
        .93354      .00991
        .91134      .01383
        .88661      .01841
        .85963      .02358
        .83070      .02924
        .80014      .03529
        .76823      .04155
        .73528      .04781
        .70158      .05372
        .66703      .05899
        .63153      .06368
        .59535      .06781
        .55865      .07137
        .52163      .07437
        .48451      .07677
        .44749      .07856
        .41079      .07974
        .37459      .08026
        .33907      .08016
        .30446      .07945
        .27093      .07812
        .23870      .07622
        .20796      .07375
        .17888      .07072
        .15166      .06715
        .12643      .06303
        .10331      .05840
        .08246      .05320
        .06388      .04745
        .04757      .04130
        .03364      .03479
        .02208      .02803
        .01306      .02119
        .00649      .01419
        .00215      .00725
        .00003      .00086
        .00075     -.00429
        .00499     -.00859
        .01260     -.01287
        .02322     -.01701
        .03674     -.02091
        .05304     -.02451
        .07204     -.02777
        .09363     -.03066
        .11770     -.03316
        .14412     -.03527
        .17273     -.03697
        .20339     -.03829
        .23590     -.03921
        .27007     -.03977
        .30570     -.03996
        .34256     -.03982
        .38042     -.03936
        .41905     -.03858
        .45818     -.03753
        .49755     -.03619
        .53692     -.03458
        .57599     -.03267
        .61458     -.03039
        .65253     -.02777
        .68967     -.02481
        .72588     -.02162
        .76098     -.01832
        .79475     -.01508
        .82692     -.01207
        .85715     -.00939
        .88513     -.00708
        .91058     -.00516
        .93322     -.00362
        .95281     -.00242
        .96917     -.00144
        .98224     -.00065
        .99193     -.00014
        .99795      .00002
       1.00000      .00000
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Polars for S8055 (12%) (s8055-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s8055-il50,000932.2 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   s8055-il50,000532.7 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   s8055-il100,000950.8 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s8055-il100,000548.3 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   s8055-il200,000971 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s8055-il200,000562.3 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   s8055-il500,000986.2 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s8055-il500,000574.9 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   s8055-il1,000,000995 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   s8055-il1,000,000588.7 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
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