FX 63-120 AIRFOIL (fx63120-il)
FX 63-120 AIRFOIL - Wortmann FX 63-120 airfoil
| Details | Dat file | Parser | |
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(fx63120-il) FX 63-120 AIRFOIL Wortmann FX 63-120 airfoil Max thickness 12% at 30.8% chord. Max camber 5.2% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
FX 63-120 AIRFOIL
18. 18.
0.0000000 0.0000000
0.0090000 0.0240000
0.0260000 0.0385000
0.0380000 0.0460000
0.0670000 0.0598000
0.1030000 0.0728000
0.1460000 0.0843000
0.1960000 0.0938000
0.2500000 0.1009000
0.3080000 0.1053000
0.4020000 0.1063000
0.5000000 0.1014000
0.5970000 0.0905000
0.6910000 0.0752000
0.8040000 0.0522000
0.8960000 0.0311000
0.9480000 0.0180000
1.0000000 0.0000000
0.0000000 0.0000000
0.0090000 -.0083000
0.0260000 -.0130000
0.0380000 -.0149000
0.0670000 -.0174000
0.1030000 -.0191000
0.1460000 -.0198000
0.1960000 -.0194000
0.2500000 -.0178000
0.3080000 -.0148000
0.4020000 -.0057000
0.5000000 0.0033000
0.5970000 0.0129000
0.6910000 0.0205000
0.8040000 0.0242000
0.8960000 0.0198000
0.9480000 0.0133000
1.0000000 0.0000000
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Similar airfoils
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Polars for FX 63-120 AIRFOIL (fx63120-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx63120-il | 50,000 | 9 | 36.7 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63120-il | 50,000 | 5 | 40 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63120-il | 100,000 | 9 | 64.7 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63120-il | 100,000 | 5 | 67.1 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63120-il | 200,000 | 9 | 93.7 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63120-il | 200,000 | 5 | 90 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63120-il | 500,000 | 9 | 125.7 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63120-il | 500,000 | 5 | 114.7 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63120-il | 1,000,000 | 9 | 147.6 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63120-il | 1,000,000 | 5 | 129.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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