S4062-095-87 (s4062-il)
S4062-095-87 - Selig S4062 low Reynolds number airfoil
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(s4062-il) S4062-095-87 Selig S4062 low Reynolds number airfoil Max thickness 9.5% at 31.7% chord. Max camber 4% at 50.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
S4062-095-87 1.00000 0.00000 0.99671 0.00041 0.98696 0.00178 0.97107 0.00438 0.94954 0.00836 0.92297 0.01374 0.89200 0.02036 0.85727 0.02799 0.81936 0.03628 0.77881 0.04487 0.73609 0.05339 0.69165 0.06147 0.64586 0.06881 0.59909 0.07513 0.55168 0.08024 0.50397 0.08399 0.45626 0.08630 0.40887 0.08717 0.36217 0.08673 0.31661 0.08510 0.27271 0.08239 0.23092 0.07864 0.19171 0.07393 0.15550 0.06828 0.12259 0.06173 0.09326 0.05435 0.06769 0.04627 0.04604 0.03765 0.02843 0.02876 0.01499 0.01986 0.00578 0.01124 0.00081 0.00339 0.00061 -.00262 0.00608 -.00725 0.01719 -.01145 0.03342 -.01482 0.05470 -.01716 0.08097 -.01844 0.11211 -.01868 0.14793 -.01800 0.18813 -.01659 0.23229 -.01462 0.27993 -.01224 0.33049 -.00965 0.38336 -.00700 0.43788 -.00441 0.49336 -.00199 0.54909 0.00015 0.60436 0.00196 0.65845 0.00337 0.71066 0.00437 0.76031 0.00495 0.80673 0.00511 0.84932 0.00491 0.88751 0.00439 0.92078 0.00364 0.94869 0.00273 0.97086 0.00178 0.98695 0.00090 0.99673 0.00025 1.00000 0.00000 |
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Polars for S4062-095-87 (s4062-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| s4062-il | 50,000 | 9 | 38.7 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4062-il | 50,000 | 5 | 38.4 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4062-il | 100,000 | 9 | 62.7 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4062-il | 100,000 | 5 | 61.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4062-il | 200,000 | 9 | 90.5 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4062-il | 200,000 | 5 | 86.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4062-il | 500,000 | 9 | 128.5 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4062-il | 500,000 | 5 | 114.5 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4062-il | 1,000,000 | 9 | 155 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4062-il | 1,000,000 | 5 | 131 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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