SG6043 (sg6043-il)
SG6043 - Selig / Giguere SG6043 wind turbine airfoil (high L/D)
| Details | Dat file | Parser | |
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(sg6043-il) SG6043 Selig / Giguere SG6043 wind turbine airfoil (high L/D) Max thickness 10% at 32.1% chord. Max camber 5.1% at 53.3% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
SG6043
1.000000 .000000
.998105 .000656
.992735 .002712
.984387 .006072
.973434 .010465
.960071 .015523
.944288 .020916
.925966 .026547
.905161 .032475
.882072 .038683
.856884 .045099
.829794 .051648
.801008 .058240
.770741 .064777
.739215 .071138
.706663 .077173
.673195 .082684
.638892 .087606
.603962 .091903
.568537 .095505
.532761 .098415
.496847 .100592
.460955 .102010
.425276 .102690
.389995 .102599
.355272 .101752
.321306 .100174
.288269 .097880
.256330 .094905
.225671 .091274
.196447 .087021
.168817 .082199
.142926 .076839
.118895 .070995
.096866 .064730
.076936 .058094
.059198 .051170
.043757 .043981
.030622 .036590
.019828 .029159
.011416 .021706
.005277 .014355
.001496 .007410
.000024 .000942
.000588 -.004677
.003930 -.008595
.010772 -.011195
.020868 -.013164
.034086 -.014302
.050504 -.014598
.070145 -.014215
.092915 -.013293
.118637 -.011970
.147117 -.010343
.178147 -.008477
.211498 -.006446
.246927 -.004303
.284172 -.002104
.322960 .000114
.363008 .002319
.404014 .004498
.445705 .006689
.487849 .008933
.530290 .011167
.572862 .013270
.615252 .015037
.657041 .016351
.697849 .017212
.737347 .017604
.775201 .017514
.811085 .016945
.844678 .015916
.875671 .014467
.903773 .012654
.928712 .010558
.950241 .008276
.968141 .005908
.982146 .003613
.992088 .001700
.998026 .000453
.999999 .000000
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Polars for SG6043 (sg6043-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| sg6043-il | 50,000 | 9 | 39.7 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6043-il | 50,000 | 5 | 37.9 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6043-il | 100,000 | 9 | 66.5 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6043-il | 100,000 | 5 | 65.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6043-il | 200,000 | 9 | 98 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6043-il | 200,000 | 5 | 94.7 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6043-il | 500,000 | 9 | 143 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6043-il | 500,000 | 5 | 129.8 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6043-il | 1,000,000 | 9 | 175.2 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6043-il | 1,000,000 | 5 | 145.2 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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