WB-135/35 13.5% smoothed (wb13535sm-il)
WB-135/35 13.5% smoothed - Woody Blanchard WB135/35 R/C sailplane airfoil
| Details | Dat file | Parser | |
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(wb13535sm-il) WB-135/35 13.5% smoothed Woody Blanchard WB135/35 R/C sailplane airfoil Max thickness 13.6% at 25% chord. Max camber 3.8% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
WB-135/35 13.5% smoothed 1.00000 0.0 0.95000 0.01200 0.90000 0.02310 0.85000 0.03425 0.80000 0.04500 0.75000 0.05510 0.70000 0.06465 0.65000 0.07360 0.60000 0.08175 0.55000 0.08875 0.50000 0.09425 0.45000 0.09790 0.40000 0.09975 0.35000 0.10000 0.30000 0.09900 0.27500 0.09800 0.25000 0.09660 0.22500 0.09470 0.20000 0.09200 0.17500 0.08825 0.15000 0.08325 0.12500 0.07700 0.10000 0.06915 0.07500 0.05900 0.05000 0.04650 0.02500 0.03000 0.01250 0.01875 0.0 0.0 0.01250 -0.01200 0.02500 -0.01800 0.05000 -0.02670 0.07500 -0.03275 0.10000 -0.03685 0.12500 -0.03930 0.15000 -0.04050 0.17500 -0.04085 0.20000 -0.04060 0.22500 -0.03995 0.25000 -0.03890 0.27500 -0.03750 0.30000 -0.03575 0.35000 -0.03185 0.40000 -0.02775 0.45000 -0.02350 0.50000 -0.01925 0.55000 -0.01532 0.60000 -0.01200 0.65000 -0.00940 0.70000 -0.00750 0.75000 -0.00600 0.80000 -0.00500 0.85000 -0.00400 0.90000 -0.00325 0.95000 -0.00250 1.00000 0.0 |
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Polars for WB-135/35 13.5% smoothed (wb13535sm-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| wb13535sm-il | 50,000 | 9 | 26.6 at α=11.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb13535sm-il | 50,000 | 5 | 33.4 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| wb13535sm-il | 100,000 | 9 | 51.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb13535sm-il | 100,000 | 5 | 51.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| wb13535sm-il | 200,000 | 9 | 73.8 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb13535sm-il | 200,000 | 5 | 68.8 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| wb13535sm-il | 500,000 | 9 | 101.3 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb13535sm-il | 500,000 | 5 | 84.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| wb13535sm-il | 1,000,000 | 9 | 108.2 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb13535sm-il | 1,000,000 | 5 | 102.4 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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