Supermarine 371-II (tip) (supermarine371ii-il)
Supermarine 371-II (tip) - Supermarine 371-II tip airfoil
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(supermarine371ii-il) Supermarine 371-II (tip) Supermarine 371-II tip airfoil Max thickness 8.4% at 50% chord. Max camber 0.9% at 45% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
Supermarine 371-II (tip) 1.00 0.0000 0.95 0.0044 0.90 0.0101 0.85 0.0168 0.80 0.0236 0.75 0.0305 0.70 0.0372 0.65 0.0430 0.60 0.0476 0.55 0.0501 0.50 0.0511 0.45 0.0510 0.40 0.0500 0.35 0.0482 0.30 0.0456 0.25 0.0424 0.20 0.0382 0.15 0.0331 0.10 0.0269 0.075 0.0230 0.050 0.0185 0.025 0.0127 0.010 0.0079 0.005 0.0055 0.000 0.0000 0.005 -0.0046 0.010 -0.0064 0.025 -0.0098 0.050 -0.0134 0.075 -0.0160 0.100 -0.0183 0.15 -0.0218 0.20 -0.0248 0.25 -0.0271 0.30 -0.0291 0.35 -0.0306 0.40 -0.0318 0.45 -0.0324 0.5 -0.0325 0.55 -0.0319 0.60 -0.0304 0.65 -0.0273 0.70 -0.0232 0.75 -0.0196 0.80 -0.0142 0.85 -0.0099 0.90 -0.0058 0.95 -0.0024 1.00 0.0000 |
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Polars for Supermarine 371-II (tip) (supermarine371ii-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| supermarine371ii-il | 50,000 | 9 | 19.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| supermarine371ii-il | 50,000 | 5 | 23.1 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| supermarine371ii-il | 100,000 | 9 | 29.9 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| supermarine371ii-il | 100,000 | 5 | 37.5 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| supermarine371ii-il | 200,000 | 9 | 51.2 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| supermarine371ii-il | 200,000 | 5 | 45.7 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| supermarine371ii-il | 500,000 | 9 | 63.7 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| supermarine371ii-il | 500,000 | 5 | 54.3 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| supermarine371ii-il | 1,000,000 | 9 | 73.8 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| supermarine371ii-il | 1,000,000 | 5 | 58.7 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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