S8036 (16%) (s8036-il)
S8036 (16%) - Selig S8036 low Reynolds number airfoil
| Details | Dat file | Parser | |
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(s8036-il) S8036 (16%) Selig S8036 low Reynolds number airfoil Max thickness 16% at 36.8% chord. Max camber 1.3% at 40.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
S8036 (16%)
1.00000 0.00000
0.99759 0.00046
0.99095 0.00217
0.98105 0.00501
0.96827 0.00843
0.95247 0.01204
0.93354 0.01594
0.91163 0.02027
0.88697 0.02505
0.85984 0.03027
0.83047 0.03590
0.79916 0.04189
0.76618 0.04816
0.73183 0.05463
0.69641 0.06119
0.66022 0.06771
0.62357 0.07402
0.58668 0.07986
0.54969 0.08509
0.51279 0.08963
0.47611 0.09328
0.43972 0.09598
0.40381 0.09776
0.36848 0.09853
0.33380 0.09838
0.29999 0.09735
0.26722 0.09547
0.23564 0.09280
0.20545 0.08939
0.17681 0.08528
0.14988 0.08053
0.12484 0.07520
0.10184 0.06934
0.08104 0.06296
0.06251 0.05610
0.04638 0.04885
0.03271 0.04115
0.02141 0.03305
0.01256 0.02483
0.00612 0.01649
0.00193 0.00823
0.00001 0.00054
0.00098 -0.00588
0.00548 -0.01153
0.01338 -0.01720
0.02433 -0.02273
0.03811 -0.02804
0.05468 -0.03304
0.07395 -0.03773
0.09576 -0.04208
0.11999 -0.04605
0.14648 -0.04964
0.17504 -0.05283
0.20549 -0.05558
0.23760 -0.05786
0.27120 -0.05962
0.30609 -0.06084
0.34204 -0.06146
0.37887 -0.06147
0.41638 -0.06087
0.45435 -0.05959
0.49265 -0.05765
0.53099 -0.05502
0.56937 -0.05165
0.60778 -0.04772
0.64594 -0.04348
0.68359 -0.03907
0.72043 -0.03464
0.75616 -0.03028
0.79048 -0.02609
0.82309 -0.02215
0.85370 -0.01852
0.88202 -0.01523
0.90775 -0.01230
0.93064 -0.00970
0.95044 -0.00739
0.96698 -0.00519
0.98037 -0.00302
0.99070 -0.00120
0.99754 -0.00020
1.00000 0.00000
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Polars for S8036 (16%) (s8036-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| s8036-il | 50,000 | 9 | 26.6 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s8036-il | 50,000 | 5 | 25.7 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s8036-il | 100,000 | 9 | 48.2 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s8036-il | 100,000 | 5 | 48 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s8036-il | 200,000 | 9 | 70.2 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s8036-il | 200,000 | 5 | 61.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s8036-il | 500,000 | 9 | 87.3 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s8036-il | 500,000 | 5 | 73.3 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s8036-il | 1,000,000 | 9 | 99.6 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s8036-il | 1,000,000 | 5 | 82.1 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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