St. CYR 24 (Bartel 35-IIIC) (stcyr24-il)
St. CYR 24 (Bartel 35-IIIC) - St. CYR 24 (Bartel 35-IIIC) airfoil
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(stcyr24-il) St. CYR 24 (Bartel 35-IIIC) St. CYR 24 (Bartel 35-IIIC) airfoil Max thickness 12.4% at 30% chord. Max camber 5.9% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
St. CYR 24 (Bartel 35-IIIC) 1.0000 0.0000 0.9500 0.0170 0.9000 0.0330 0.8000 0.0635 0.7000 0.0915 0.6000 0.1125 0.5000 0.1260 0.4000 0.1340 0.3000 0.1355 0.2000 0.1285 0.1500 0.1210 0.1000 0.1090 0.0750 0.0990 0.0500 0.0865 0.0250 0.0690 0.0125 0.0570 0.0000 0.0256 0.0125 0.0080 0.0250 0.0035 0.0500 0.0010 0.0750 0.0010 0.1000 0.0020 0.1500 0.0035 0.2000 0.0070 0.3000 0.0120 0.4000 0.0140 0.5000 0.0145 0.6000 0.0140 0.7000 0.0130 0.8000 0.0100 0.9000 0.0050 0.9500 0.0030 1.0000 0.0000 |
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Polars for St. CYR 24 (Bartel 35-IIIC) (stcyr24-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| stcyr24-il | 50,000 | 9 | 29.4 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| stcyr24-il | 50,000 | 5 | 31.1 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| stcyr24-il | 100,000 | 9 | 56.8 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| stcyr24-il | 100,000 | 5 | 53.1 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| stcyr24-il | 200,000 | 9 | 82.5 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| stcyr24-il | 200,000 | 5 | 74.2 at α=0.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| stcyr24-il | 500,000 | 9 | 116.5 at α=0.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| stcyr24-il | 500,000 | 5 | 89.8 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| stcyr24-il | 1,000,000 | 9 | 126.9 at α=1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| stcyr24-il | 1,000,000 | 5 | 95.5 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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