EPPLER 379 AIRFOIL (e379-il)
EPPLER 379 AIRFOIL - Eppler E379 ultralight airfoil
| Details | Dat file | Parser | |
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(e379-il) EPPLER 379 AIRFOIL Eppler E379 ultralight airfoil Max thickness 2.2% at 5.8% chord. Max camber 8% at 31.8% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 379 AIRFOIL
34.0 28.0
0.0000900 -.0006600
0.0011600 0.0040000
0.0052900 0.0106000
0.0129200 0.0182700
0.0241900 0.0266200
0.0391600 0.0352400
0.0577900 0.0438800
0.0799900 0.0522800
0.1056200 0.0602200
0.1344700 0.0674900
0.1663000 0.0739000
0.2008100 0.0792600
0.2376700 0.0832900
0.2766800 0.0857000
0.3177200 0.0863200
0.3606500 0.0851300
0.4053100 0.0821700
0.4515200 0.0775700
0.4991100 0.0716200
0.5476800 0.0648100
0.5966200 0.0575100
0.6453100 0.0500000
0.6931200 0.0425000
0.7394200 0.0352200
0.7836100 0.0283400
0.8251100 0.0220000
0.8633500 0.0163200
0.8977900 0.0114300
0.9279500 0.0073900
0.9533900 0.0042800
0.9736400 0.0021400
0.9882700 0.0008500
0.9970700 0.0002000
1.0000000 0.0000000
0.0000900 -.0006600
0.0028200 -.0010600
0.0116200 0.0024000
0.0271000 0.0088400
0.0494600 0.0182000
0.0794600 0.0299700
0.1176800 0.0432500
0.1647100 0.0563000
0.2194800 0.0664600
0.2793000 0.0722700
0.3416500 0.0741200
0.4049200 0.0725100
0.4677100 0.0682600
0.5290000 0.0620900
0.5880600 0.0548800
0.6444600 0.0471400
0.6977800 0.0393500
0.7476400 0.0317600
0.7936800 0.0246800
0.8355900 0.0182500
0.8730800 0.0126900
0.9059200 0.0080600
0.9339300 0.0044900
0.9569500 0.0020400
0.9751000 0.0007900
0.9885700 0.0003300
0.9970700 0.0001200
1.0000000 0.0000000
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Polars for EPPLER 379 AIRFOIL (e379-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e379-il | 50,000 | 9 | 23.2 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e379-il | 50,000 | 5 | 40.6 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e379-il | 100,000 | 9 | 74.6 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e379-il | 100,000 | 5 | 66.8 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e379-il | 200,000 | 9 | 117.8 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e379-il | 200,000 | 5 | 91.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e379-il | 500,000 | 9 | 128 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e379-il | 500,000 | 5 | 118.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e379-il | 1,000,000 | 0 | 135.6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
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