EPPLER 540 AIRFOIL (e540-il)
EPPLER 540 AIRFOIL - Eppler E540 general aviation airfoil
| Details | Dat file | Parser | |
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(e540-il) EPPLER 540 AIRFOIL Eppler E540 general aviation airfoil Max thickness 16.9% at 45.5% chord. Max camber 1.6% at 35.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 540 AIRFOIL
36. 37.
0.0000100 0.0002300
0.0000600 0.0009100
0.0003500 0.0023500
0.0008500 0.0038800
0.0019700 0.0063200
0.0029300 0.0079800
0.0107200 0.0170100
0.0231600 0.0266500
0.0400700 0.0365000
0.0613200 0.0462500
0.0866900 0.0556600
0.1159700 0.0645300
0.1488800 0.0726900
0.1851000 0.0799900
0.2242800 0.0863100
0.2660200 0.0915400
0.3099000 0.0955900
0.3554600 0.0983700
0.4022200 0.0997900
0.4496700 0.0997700
0.4973000 0.0981600
0.5447200 0.0947000
0.5918400 0.0892500
0.6386600 0.0819900
0.6850100 0.0734700
0.7303900 0.0642100
0.7742500 0.0546200
0.8159800 0.0451100
0.8549600 0.0360300
0.8905200 0.0276900
0.9219900 0.0203000
0.9487000 0.0140000
0.9700200 0.0087000
0.9858400 0.0041800
0.9962100 0.0010500
1.0000000 0.0000000
0.0000100 0.0002300
0.0000100 -.0004100
0.0001100 -.0010100
0.0003100 -.0016000
0.0006100 -.0021900
0.0009900 -.0028000
0.0019600 -.0040400
0.0031900 -.0053100
0.0054900 -.0072700
0.0141300 -.0127000
0.0296900 -.0195600
0.0503500 -.0263100
0.0758500 -.0328200
0.1058900 -.0390100
0.1401400 -.0448400
0.1781000 -.0502700
0.2193100 -.0552200
0.2632300 -.0595900
0.3093200 -.0632800
0.3570400 -.0661700
0.4058000 -.0681500
0.4550500 -.0690900
0.5042000 -.0688300
0.5526500 -.0672200
0.5998100 -.0638000
0.6456800 -.0578900
0.6908800 -.0494300
0.7360399 -.0391600
0.7810900 -.0286400
0.8249400 -.0191000
0.8663600 -.0112100
0.9041100 -.0053600
0.9369300 -.0016000
0.9637400 0.0002800
0.9836300 0.0007000
0.9958700 0.0003100
1.0000000 0.0000000
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Polars for EPPLER 540 AIRFOIL (e540-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e540-il | 50,000 | 9 | 24.3 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e540-il | 50,000 | 5 | 20.1 at α=10.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e540-il | 100,000 | 9 | 38.3 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e540-il | 100,000 | 5 | 33.4 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e540-il | 200,000 | 9 | 54 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e540-il | 200,000 | 5 | 57 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e540-il | 500,000 | 9 | 85.3 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e540-il | 500,000 | 5 | 82.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e540-il | 1,000,000 | 9 | 110 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e540-il | 1,000,000 | 5 | 97.5 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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