EPPLER 858 AIRFOIL (e858-il)
EPPLER 858 AIRFOIL - Eppler E858 propeller airfoil
| Details | Dat file | Parser | |
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(e858-il) EPPLER 858 AIRFOIL Eppler E858 propeller airfoil Max thickness 22.7% at 26.6% chord. Max camber 4.7% at 44.3% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 858 AIRFOIL
34. 34.
0.0000700 0.0020500
0.0010800 0.0104000
0.0034000 0.0188300
0.0106000 0.0346800
0.0216600 0.0511900
0.0364600 0.0678600
0.0548600 0.0842800
0.0766700 0.1000800
0.1016500 0.1148900
0.1295200 0.1283300
0.1599700 0.1399200
0.1929100 0.1491500
0.2283300 0.1556900
0.2662200 0.1592800
0.3067800 0.1599100
0.3499500 0.1579400
0.3953500 0.1537000
0.4425900 0.1474500
0.4912400 0.1394800
0.5407900 0.1301200
0.5906900 0.1197000
0.6403500 0.1085500
0.6891500 0.0969900
0.7364000 0.0853200
0.7814400 0.0738200
0.8236000 0.0626900
0.8622100 0.0521100
0.8966000 0.0421700
0.9263800 0.0329500
0.9508100 0.0242400
0.9700701 0.0155500
0.9851300 0.0074100
0.9958700 0.0018400
1.0000000 0.0000000
0.0000700 0.0020500
0.0002700 -.0030600
0.0009300 -.0065600
0.0016700 -.0086800
0.0027600 -.0106800
0.0050000 -.0136700
0.0089100 -.0176500
0.0164800 -.0235500
0.0231900 -.0277600
0.0421000 -.0368500
0.0657300 -.0450700
0.0937900 -.0522400
0.1259500 -.0582500
0.1618000 -.0630000
0.2008100 -.0663600
0.2424700 -.0679900
0.2865400 -.0673900
0.3330800 -.0644100
0.3821300 -.0591100
0.4338100 -.0518800
0.4878700 -.0436000
0.5435500 -.0350000
0.5999700 -.0266400
0.6562100 -.0189500
0.7112500 -.0122900
0.7640899 -.0068700
0.8136799 -.0028400
0.8590400 -.0001700
0.8992200 0.0012500
0.9333799 0.0017700
0.9610500 0.0018400
0.9820000 0.0014700
0.9953700 0.0005600
1.0000000 0.0000000
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Polars for EPPLER 858 AIRFOIL (e858-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e858-il | 50,000 | 9 | 3 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e858-il | 50,000 | 5 | 13 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e858-il | 100,000 | 9 | 21.5 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e858-il | 100,000 | 5 | 34.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e858-il | 200,000 | 9 | 48.7 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e858-il | 200,000 | 5 | 51.5 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e858-il | 500,000 | 9 | 73.5 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e858-il | 500,000 | 5 | 67.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e858-il | 1,000,000 | 9 | 88.1 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e858-il | 1,000,000 | 5 | 87.4 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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