FX LIII-142 K 25 AIRFOIL (fxl142k-il)
FX LIII-142 K 25 AIRFOIL - Wortmann FX LIII-142 K 25 airfoil
| Details | Dat file | Parser | |
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(fxl142k-il) FX LIII-142 K 25 AIRFOIL Wortmann FX LIII-142 K 25 airfoil Max thickness 14.2% at 30.9% chord. Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
FX LIII-142 K 25 AIRFOIL
49. 49.
0.0000000 0.0000000
0.0010200 0.0042000
0.0042200 0.0098000
0.0096000 0.0162000
0.0170200 0.0224000
0.0265000 0.0282000
0.0380200 0.0334000
0.0515800 0.0388000
0.0669400 0.0436000
0.0842200 0.0484000
0.1033000 0.0524000
0.1240300 0.0562000
0.1464300 0.0596000
0.1703700 0.0628000
0.1955800 0.0656000
0.2222100 0.0678000
0.2499800 0.0694000
0.2789100 0.0706000
0.3086100 0.0710000
0.3393300 0.0708000
0.3705600 0.0698000
0.4024300 0.0682000
0.4346900 0.0660000
0.4673300 0.0630000
0.4999700 0.0590000
0.5327400 0.0552000
0.5652500 0.0506000
0.5975000 0.0463000
0.6293800 0.0416000
0.6607400 0.0378000
0.6913300 0.0334000
0.7211500 0.0292000
0.7499501 0.0260000
0.7777300 0.0234000
0.8043500 0.0192000
0.8297000 0.0162000
0.8535000 0.0138000
0.8759000 0.0114000
0.8964400 0.0096000
0.9157100 0.0076000
0.9329900 0.0058000
0.9484800 0.0048000
0.9619200 0.0034000
0.9734400 0.0026000
0.9829100 0.0020000
0.9903400 0.0014000
0.9957100 0.0008000
0.9989100 0.0006000
1.0000000 0.0000000
0.0000000 0.0000000
0.0010200 -.0042000
0.0042200 -.0098000
0.0096000 -.0162000
0.0170200 -.0224000
0.0265000 -.0282000
0.0380200 -.0334000
0.0515800 -.0388000
0.0669400 -.0436000
0.0842200 -.0484000
0.1033000 -.0524000
0.1240300 -.0562000
0.1464300 -.0596000
0.1703700 -.0628000
0.1955800 -.0656000
0.2222100 -.0678000
0.2499800 -.0694000
0.2789100 -.0706000
0.3086100 -.0710000
0.3393300 -.0708000
0.3705600 -.0698000
0.4024300 -.0682000
0.4346900 -.0660000
0.4673300 -.0630000
0.4999700 -.0590000
0.5327400 -.0552000
0.5652500 -.0506000
0.5975000 -.0463000
0.6293800 -.0416000
0.6607400 -.0378000
0.6913300 -.0334000
0.7211500 -.0292000
0.7499501 -.0260000
0.7777300 -.0234000
0.8043500 -.0192000
0.8297000 -.0162000
0.8535000 -.0138000
0.8759000 -.0114000
0.8964400 -.0096000
0.9157100 -.0076000
0.9329900 -.0058000
0.9484800 -.0048000
0.9619200 -.0034000
0.9734400 -.0026000
0.9829100 -.0020000
0.9903400 -.0014000
0.9957100 -.0008000
0.9989100 -.0006000
1.0000000 0.0000000
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Polars for FX LIII-142 K 25 AIRFOIL (fxl142k-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fxl142k-il | 50,000 | 9 | 27.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxl142k-il | 50,000 | 5 | 28.3 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fxl142k-il | 100,000 | 9 | 42.1 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxl142k-il | 100,000 | 5 | 39.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fxl142k-il | 200,000 | 9 | 54.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxl142k-il | 200,000 | 5 | 47.5 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fxl142k-il | 500,000 | 9 | 63.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxl142k-il | 500,000 | 5 | 60.6 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fxl142k-il | 1,000,000 | 9 | 75.2 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxl142k-il | 1,000,000 | 5 | 72.1 at α=11.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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