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SG6051 (sg6051-il)

SG6051 - Selig / Giguere SG6051 wind turbine airfoil


Airfoil sg6051-il
Details Dat file Parser  
(sg6051-il) SG6051
Selig / Giguere SG6051 wind turbine airfoil
Max thickness 12% at 35.7% chord.
Max camber 3.1% at 49.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
SG6051
       1.00000      .00500
        .99790      .00527
        .99187      .00631
        .98234      .00826
        .96969      .01097
        .95403      .01425
        .93543      .01810
        .91410      .02256
        .89031      .02759
        .86430      .03312
        .83636      .03906
        .80674      .04530
        .77574      .05168
        .74358      .05795
        .71038      .06395
        .67633      .06962
        .64160      .07477
        .60629      .07931
        .57064      .08320
        .53475      .08631
        .49871      .08866
        .46275      .09019
        .42700      .09088
        .39160      .09080
        .35675      .08992
        .32259      .08828
        .28931      .08595
        .25709      .08295
        .22611      .07934
        .19655      .07516
        .16857      .07045
        .14233      .06527
        .11797      .05967
        .09560      .05370
        .07537      .04745
        .05737      .04097
        .04167      .03436
        .02838      .02770
        .01756      .02109
        .00931      .01469
        .00369      .00848
        .00058      .00263
        .00042     -.00220
        .00365     -.00654
        .00985     -.01097
        .01874     -.01489
        .03064     -.01812
        .04567     -.02084
        .06366     -.02323
        .08447     -.02531
        .10794     -.02708
        .13392     -.02857
        .16222     -.02979
        .19263     -.03075
        .22493     -.03144
        .25883     -.03183
        .29407     -.03182
        .33051     -.03112
        .36831     -.02972
        .40753     -.02795
        .44777     -.02626
        .48846     -.02473
        .52924     -.02320
        .56988     -.02165
        .61011     -.02008
        .64967     -.01854
        .68829     -.01704
        .72569     -.01560
        .76161     -.01423
        .79579     -.01293
        .82796     -.01165
        .85800     -.01039
        .88576     -.00922
        .91097     -.00824
        .93337     -.00744
        .95273     -.00678
        .96889     -.00613
        .98190     -.00546
        .99169     -.00501
        .99787     -.00493
       1.00000     -.00500
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Polars for SG6051 (sg6051-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   sg6051-il50,000935.8 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6051-il50,000534.3 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   sg6051-il100,000958.1 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6051-il100,000557.1 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   sg6051-il200,000982.2 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6051-il200,000578.4 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   sg6051-il500,0009113 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6051-il500,0005102.3 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   sg6051-il1,000,0009133.6 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6051-il1,000,0005115.8 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
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