EPPLER 360 AIRFOIL (e360-il)
EPPLER 360 AIRFOIL - Eppler E360 rotorcraft airfoil
| Details | Dat file | Parser | |
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(e360-il) EPPLER 360 AIRFOIL Eppler E360 rotorcraft airfoil Max thickness 12.2% at 36.9% chord. Max camber 1.6% at 27.2% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 360 AIRFOIL
34. 39.
0.0000100 -.0005100
0.0000400 0.0010500
0.0004000 0.0035100
0.0011800 0.0062200
0.0063900 0.0152700
0.0156500 0.0245600
0.0291000 0.0335500
0.0467900 0.0418700
0.0688200 0.0492500
0.0952700 0.0556900
0.1259300 0.0613400
0.1603900 0.0662000
0.1982200 0.0702100
0.2389900 0.0732700
0.2822200 0.0753000
0.3274200 0.0761300
0.3742000 0.0755500
0.4223000 0.0734600
0.4714600 0.0698500
0.5215100 0.0649100
0.5720600 0.0590300
0.6225400 0.0525700
0.6723500 0.0458300
0.7208400 0.0390600
0.7673600 0.0324600
0.8112400 0.0263100
0.8518300 0.0206800
0.8884900 0.0157000
0.9206300 0.0113900
0.9477000 0.0076900
0.9694500 0.0044300
0.9858300 0.0018400
0.9963300 0.0003900
1.0000000 0.0000000
0.0000100 -.0005100
0.0001600 -.0019700
0.0003000 -.0026600
0.0004900 -.0033100
0.0007600 -.0039200
0.0011100 -.0044900
0.0015500 -.0050600
0.0020700 -.0056300
0.0033200 -.0067700
0.0048300 -.0079100
0.0075300 -.0096100
0.0155600 -.0134700
0.0317700 -.0188000
0.0532200 -.0237000
0.0796200 -.0282200
0.1106200 -.0323400
0.1458300 -.0360300
0.1848400 -.0392500
0.2271800 -.0419600
0.2723800 -.0441200
0.3199200 -.0457100
0.3692500 -.0466800
0.4198300 -.0470000
0.4710700 -.0466300
0.5224000 -.0454900
0.5733200 -.0434500
0.6234700 -.0405100
0.6724401 -.0367200
0.7198400 -.0322200
0.7653100 -.0271800
0.8084800 -.0219200
0.8488200 -.0168500
0.8856600 -.0122800
0.9183200 -.0083700
0.9461901 -.0051900
0.9687700 -.0027000
0.9856700 -.0009900
0.9963300 -.0001800
1.0000000 0.0000000
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Polars for EPPLER 360 AIRFOIL (e360-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e360-il | 50,000 | 9 | 30.2 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e360-il | 50,000 | 5 | 31.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e360-il | 100,000 | 9 | 47.6 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e360-il | 100,000 | 5 | 46 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e360-il | 200,000 | 9 | 63.3 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e360-il | 200,000 | 5 | 52.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e360-il | 500,000 | 9 | 69.9 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e360-il | 500,000 | 5 | 69 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e360-il | 1,000,000 | 9 | 86 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e360-il | 1,000,000 | 5 | 84 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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