S1046 17% (Danny Howell) (s1046-il)
S1046 17% (Danny Howell) - Selig S1046 airfoil
| Details | Dat file | Parser | |
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(s1046-il) S1046 17% (Danny Howell) Selig S1046 airfoil Max thickness 17% at 30.8% chord. Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
S1046 17% (Danny Howell)
1.00000 0.00000
0.99616 0.00022
0.98513 0.00134
0.96778 0.00347
0.94451 0.00634
0.91556 0.01001
0.88146 0.01459
0.84282 0.02007
0.80030 0.02639
0.75460 0.03341
0.70644 0.04097
0.65656 0.04882
0.60571 0.05665
0.55447 0.06395
0.50324 0.07044
0.45251 0.07597
0.40277 0.08035
0.35450 0.08339
0.30811 0.08495
0.26398 0.08492
0.22247 0.08324
0.18385 0.07984
0.14834 0.07476
0.11614 0.06815
0.08745 0.06017
0.06246 0.05106
0.04136 0.04107
0.02431 0.03052
0.01149 0.01974
0.00306 0.00925
0.00000 0.00000
0.00306 -0.00925
0.01149 -0.01974
0.02431 -0.03052
0.04136 -0.04107
0.06246 -0.05106
0.08745 -0.06017
0.11614 -0.06815
0.14834 -0.07476
0.18385 -0.07984
0.22247 -0.08324
0.26398 -0.08492
0.30811 -0.08495
0.35450 -0.08339
0.40277 -0.08035
0.45251 -0.07597
0.50324 -0.07044
0.55447 -0.06395
0.60571 -0.05665
0.65656 -0.04882
0.70644 -0.04097
0.75460 -0.03341
0.80030 -0.02639
0.84282 -0.02007
0.88146 -0.01459
0.91556 -0.01001
0.94451 -0.00634
0.96778 -0.00347
0.98513 -0.00134
0.99616 -0.00022
1.00000 0.00000
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Polars for S1046 17% (Danny Howell) (s1046-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| s1046-il | 50,000 | 9 | 16.2 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s1046-il | 50,000 | 5 | 25.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s1046-il | 100,000 | 9 | 37.2 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s1046-il | 100,000 | 5 | 40.5 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s1046-il | 200,000 | 9 | 55 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s1046-il | 200,000 | 5 | 54.6 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s1046-il | 500,000 | 9 | 77 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s1046-il | 500,000 | 5 | 70.4 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s1046-il | 1,000,000 | 9 | 90.9 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s1046-il | 1,000,000 | 5 | 80.9 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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