St. CYR 234 (Bartel 17-IC) (stcyr234-il)
St. CYR 234 (Bartel 17-IC) - St. CYR 234 (Bartel 17-IC) airfoil
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(stcyr234-il) St. CYR 234 (Bartel 17-IC) St. CYR 234 (Bartel 17-IC) airfoil Max thickness 16% at 20% chord. Max camber 5.1% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
St. CYR 234 (Bartel 17-IC) 1.0000 0.0000 0.9500 0.0200 0.9000 0.0400 0.8000 0.0775 0.7000 0.1080 0.6000 0.1330 0.5000 0.1520 0.4000 0.1610 0.3000 0.1655 0.2000 0.1620 0.1500 0.1570 0.1000 0.1460 0.0750 0.1380 0.0500 0.1270 0.0250 0.1100 0.0125 0.0955 0.0000 0.0642 0.0125 0.0375 0.0250 0.0270 0.0500 0.0140 0.0750 0.0085 0.1000 0.0050 0.1500 0.0025 0.2000 0.0020 0.3000 0.0065 0.4000 0.0110 0.5000 0.0135 0.6000 0.0190 0.7000 0.0135 0.8000 0.0105 0.9000 0.0050 0.9500 0.0025 1.0000 0.0000 |
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Polars for St. CYR 234 (Bartel 17-IC) (stcyr234-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| stcyr234-il | 50,000 | 9 | 28 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| stcyr234-il | 50,000 | 5 | 26.8 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| stcyr234-il | 100,000 | 9 | 47.2 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| stcyr234-il | 100,000 | 5 | 42.1 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| stcyr234-il | 200,000 | 9 | 72.9 at α=1° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| stcyr234-il | 200,000 | 5 | 58 at α=0° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| stcyr234-il | 500,000 | 9 | 87.3 at α=0° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| stcyr234-il | 500,000 | 5 | 66.5 at α=-1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| stcyr234-il | 1,000,000 | 9 | 93.7 at α=-1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| stcyr234-il | 1,000,000 | 5 | 67.8 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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