Supermarine 371-I (root) (supermarine371i-il)
Supermarine 371-I (root) - Supermarine 371-I root airfoil
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(supermarine371i-il) Supermarine 371-I (root) Supermarine 371-I root airfoil Max thickness 13% at 40% chord. Max camber 0.9% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
Supermarine 371-I (root) 1.00 0.0000 0.95 0.0064 0.90 0.0142 0.85 0.0230 0.80 0.0323 0.75 0.0417 0.70 0.0507 0.65 0.0589 0.60 0.0657 0.55 0.0703 0.50 0.0728 0.45 0.0740 0.40 0.0741 0.35 0.0730 0.30 0.0708 0.25 0.0674 0.20 0.0625 0.15 0.0559 0.10 0.0468 0.075 0.0410 0.050 0.0337 0.025 0.0238 0.010 0.0149 0.005 0.0105 0.000 0.0000 0.005 -0.0097 0.010 -0.0135 0.025 -0.0207 0.050 -0.0284 0.075 -0.0349 0.100 -0.0380 0.15 -0.0444 0.20 -0.0490 0.25 -0.0522 0.30 -0.0543 0.35 -0.0556 0.40 -0.0559 0.45 -0.0555 0.5 -0.0542 0.55 -0.0519 0.60 -0.0489 0.65 -0.0431 0.70 -0.0368 0.75 -0.0299 0.80 -0.0229 0.85 -0.0161 0.90 -0.0098 0.95 -0.0044 1.00 0.0000 |
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Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file |
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Polars for Supermarine 371-I (root) (supermarine371i-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| supermarine371i-il | 50,000 | 9 | 28.6 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| supermarine371i-il | 50,000 | 5 | 27.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| supermarine371i-il | 100,000 | 9 | 46.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| supermarine371i-il | 100,000 | 5 | 41 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| supermarine371i-il | 200,000 | 9 | 57.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| supermarine371i-il | 200,000 | 5 | 52.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| supermarine371i-il | 500,000 | 9 | 78.5 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| supermarine371i-il | 500,000 | 5 | 64 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| supermarine371i-il | 1,000,000 | 9 | 89.3 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| supermarine371i-il | 1,000,000 | 5 | 66.4 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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