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SG6050 (sg6050-il)

SG6050 - Selig / Giguere SG6050 wind turbine airfoil


Airfoil sg6050-il
Details Dat file Parser  
(sg6050-il) SG6050
Selig / Giguere SG6050 wind turbine airfoil
Max thickness 16% at 31.5% chord.
Max camber 3.1% at 48.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
SG6050
       1.00000      .00500
        .99776      .00537
        .99140      .00676
        .98154      .00926
        .96862      .01259
        .95269      .01647
        .93376      .02088
        .91202      .02588
        .88771      .03145
        .86107      .03753
        .83238      .04406
        .80189      .05095
        .76990      .05810
        .73669      .06537
        .70255      .07260
        .66777      .07960
        .63248      .08606
        .59676      .09188
        .56085      .09699
        .52482      .10124
        .48875      .10465
        .45288      .10717
        .41735      .10875
        .38234      .10944
        .34802      .10919
        .31453      .10799
        .28208      .10588
        .25080      .10283
        .22077      .09891
        .19219      .09414
        .16515      .08856
        .13976      .08230
        .11615      .07543
        .09444      .06803
        .07476      .06021
        .05720      .05205
        .04182      .04366
        .02873      .03517
        .01798      .02669
        .00963      .01842
        .00379      .01050
        .00049      .00319
        .00048     -.00309
        .00410     -.00909
        .01067     -.01542
        .01982     -.02164
        .03139     -.02736
        .04566     -.03227
        .06289     -.03656
        .08289     -.04048
        .10541     -.04399
        .13028     -.04708
        .15727     -.04970
        .18616     -.05179
        .21672     -.05320
        .24887     -.05376
        .28257     -.05342
        .31773     -.05203
        .35454     -.04962
        .39318     -.04660
        .43322     -.04364
        .47392     -.04093
        .51485     -.03820
        .55578     -.03543
        .59645     -.03264
        .63657     -.02986
        .67587     -.02715
        .71406     -.02454
        .75081     -.02210
        .78578     -.01978
        .81865     -.01740
        .84949     -.01489
        .87833     -.01247
        .90477     -.01041
        .92847     -.00874
        .94910     -.00744
        .96643     -.00638
        .98044     -.00548
        .99101     -.00494
        .99770     -.00489
       1.00000     -.00500
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Selig format dat file

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Polars for SG6050 (sg6050-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   sg6050-il50,00098.2 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6050-il50,000525.6 at α=9.75°Mach=0 Ncrit=5Xfoil predictionDetails
   sg6050-il100,000950 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6050-il100,000552.4 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   sg6050-il200,000974.7 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6050-il200,000573.2 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   sg6050-il500,0009105.1 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6050-il500,000597.3 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   sg6050-il1,000,0009126.5 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6050-il1,000,0005113 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
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