EPPLER 376 AIRFOIL (e376-il)
EPPLER 376 AIRFOIL - Eppler E376 ultralight airfoil
| Details | Dat file | Parser | |
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(e376-il) EPPLER 376 AIRFOIL Eppler E376 ultralight airfoil Max thickness 2.5% at 4.3% chord. Max camber 9% at 32.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 376 AIRFOIL
34.0 28.0
0.0000100 -.0003200
0.0015400 0.0052800
0.0064600 0.0125500
0.0149300 0.0207800
0.0270800 0.0296000
0.0428900 0.0386500
0.0623500 0.0476700
0.0853200 0.0564000
0.1116800 0.0646300
0.1411900 0.0721700
0.1736200 0.0787900
0.2086600 0.0843300
0.2459700 0.0885100
0.2853500 0.0910600
0.3266700 0.0918000
0.3697700 0.0907300
0.4144800 0.0878700
0.4606000 0.0833500
0.5079600 0.0774600
0.5561600 0.0706700
0.6045900 0.0633000
0.6526600 0.0556600
0.6997600 0.0479600
0.7452800 0.0403600
0.7886500 0.0330800
0.8293000 0.0262700
0.8666800 0.0200600
0.9003200 0.0145800
0.9297300 0.0099100
0.9544900 0.0061400
0.9742100 0.0033300
0.9884900 0.0014500
0.9971200 0.0003600
1.0000000 0.0000000
0.0000100 -.0003200
0.0020800 -.0029400
0.0085300 -.0020900
0.0201900 0.0026100
0.0381200 0.0114700
0.0634500 0.0243000
0.0974500 0.0402500
0.1412800 0.0579200
0.1960200 0.0742500
0.2596400 0.0843700
0.3261500 0.0869000
0.3920500 0.0845200
0.4565400 0.0793500
0.5191000 0.0723300
0.5792500 0.0643300
0.6366300 0.0558600
0.6909300 0.0473900
0.7418000 0.0391000
0.7888500 0.0312600
0.8317400 0.0240400
0.8701600 0.0176300
0.9038600 0.0121300
0.9326400 0.0076700
0.9563200 0.0043300
0.9749600 0.0021900
0.9886400 0.0009500
0.9971200 0.0002600
1.0000000 0.0000000
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Polars for EPPLER 376 AIRFOIL (e376-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e376-il | 50,000 | 9 | 19.3 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e376-il | 50,000 | 5 | 38.9 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e376-il | 100,000 | 9 | 105.6 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e376-il | 100,000 | 5 | 67.4 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e376-il | 200,000 | 9 | 92.7 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e376-il | 200,000 | 5 | 95 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e376-il | 500,000 | 9 | 135 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e376-il | 500,000 | 5 | 129.6 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e376-il | 1,000,000 | 9 | 156.2 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e376-il | 1,000,000 | 5 | 141.7 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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