EPPLER 378 AIRFOIL (e378-il)
EPPLER 378 AIRFOIL - Eppler E378 ultralight airfoil
| Details | Dat file | Parser | |
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(e378-il) EPPLER 378 AIRFOIL Eppler E378 ultralight airfoil Max thickness 4.1% at 7.8% chord. Max camber 8.1% at 35.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 378 AIRFOIL
34.0 28.0
0.0005500 -.0020100
0.0006400 0.0028500
0.0042600 0.0098500
0.0115300 0.0179500
0.0225500 0.0266600
0.0373400 0.0356300
0.0558600 0.0445700
0.0780100 0.0532500
0.1036200 0.0614400
0.1324800 0.0689400
0.1643500 0.0755400
0.1989200 0.0810500
0.2358600 0.0852100
0.2749600 0.0877200
0.3161100 0.0884100
0.3591600 0.0872600
0.4039600 0.0843000
0.4502700 0.0796800
0.4979800 0.0736800
0.5466800 0.0668000
0.5957400 0.0594000
0.6445500 0.0517700
0.6924700 0.0441300
0.7388800 0.0367000
0.7831800 0.0296400
0.8247600 0.0231200
0.8630800 0.0172700
0.8976000 0.0121900
0.9278300 0.0079700
0.9533300 0.0046900
0.9736200 0.0024000
0.9882700 0.0010000
0.9970700 0.0002400
1.0000000 0.0000000
0.0005500 -.0020100
0.0052100 -.0042300
0.0152800 -.0042400
0.0302700 -.0017200
0.0507400 0.0037800
0.0773300 0.0122400
0.1107600 0.0232900
0.1515500 0.0360600
0.1999500 0.0493200
0.2557200 0.0614800
0.3181300 0.0705200
0.3846600 0.0741400
0.4513300 0.0723200
0.5158700 0.0672400
0.5777700 0.0603800
0.6365700 0.0525300
0.6919000 0.0442800
0.7433900 0.0360700
0.7907300 0.0282500
0.8336300 0.0211000
0.8718600 0.0148100
0.9052200 0.0095600
0.9335600 0.0054500
0.9567800 0.0025900
0.9750400 0.0010500
0.9885600 0.0004300
0.9970700 0.0001300
1.0000000 0.0000000
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Polars for EPPLER 378 AIRFOIL (e378-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e378-il | 50,000 | 9 | 32.6 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e378-il | 50,000 | 5 | 38.3 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e378-il | 100,000 | 9 | 37 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e378-il | 100,000 | 5 | 65.1 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e378-il | 200,000 | 9 | 36.6 at α=12.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e378-il | 200,000 | 5 | 90.7 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e378-il | 500,000 | 9 | 37.1 at α=13.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e378-il | 500,000 | 5 | 124.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e378-il | 1,000,000 | 9 | 41 at α=14° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e378-il | 1,000,000 | 5 | 134.5 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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