EPPLER 377 (MODIFIED) AIRFOIL (e377m-il)
EPPLER 377 (MODIFIED) AIRFOIL - Eppler E377 (modified) ultralight airfoil
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(e377m-il) EPPLER 377 (MODIFIED) AIRFOIL Eppler E377 (modified) ultralight airfoil Max thickness 3.8% at 6.1% chord. Max camber 9.2% at 32.6% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 377 (MODIFIED) AIRFOIL
34.0 33.0
0.0001000 -.0010200
0.0013600 0.0048200
0.0060200 0.0124400
0.0142800 0.0210200
0.0262500 0.0301300
0.0419600 0.0394500
0.0613400 0.0487100
0.0842800 0.0576700
0.1106200 0.0661100
0.1401400 0.0738100
0.1725900 0.0805900
0.2076600 0.0862500
0.2450300 0.0905400
0.2844600 0.0931600
0.3258400 0.0939700
0.3690100 0.0929200
0.4137900 0.0900600
0.4599800 0.0855300
0.5074100 0.0795900
0.5556700 0.0727200
0.6041600 0.0652700
0.6522900 0.0575100
0.6994400 0.0496600
0.7450100 0.0419300
0.7884100 0.0344900
0.8290900 0.0275100
0.8665000 0.0211200
0.9001500 0.0154500
0.9295700 0.0106000
0.9543400 0.0066400
0.9740700 0.0036300
0.9884100 0.0015900
0.9971000 0.0004000
1.0000000 0.0000000
0.0001000 -.0010200
0.0032400 -.0040600
0.0114100 -.0046300
0.0244200 -.0020400
0.0429000 0.0036300
0.0650000 0.0125000
0.0875800 0.0243100
0.1122700 0.0391600
0.1400000 0.0550000
0.1717600 0.0688200
0.2077000 0.0793000
0.2450000 0.0855000
0.2845000 0.0882000
0.3263400 0.0886000
0.3695600 0.0871300
0.4138000 0.0841000
0.4610000 0.0796400
0.5084400 0.0741100
0.5557000 0.0677000
0.6048600 0.0602700
0.6529100 0.0524900
0.6994000 0.0447000
0.7453900 0.0369200
0.7887800 0.0295000
0.8291000 0.0225000
0.8666800 0.0159700
0.9002900 0.0105800
0.9296000 0.0066000
0.9545200 0.0039100
0.9742300 0.0021200
0.9884900 0.0009300
0.9971100 0.0002300
1.0000000 0.0000000
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Polars for EPPLER 377 (MODIFIED) AIRFOIL (e377m-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e377m-il | 50,000 | 9 | 17.8 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e377m-il | 50,000 | 5 | 36.8 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e377m-il | 100,000 | 9 | 61.6 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e377m-il | 100,000 | 5 | 63.8 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e377m-il | 200,000 | 9 | 86.4 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e377m-il | 200,000 | 5 | 86.7 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e377m-il | 500,000 | 9 | 117.7 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e377m-il | 500,000 | 5 | 115.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e377m-il | 1,000,000 | 9 | 142.6 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e377m-il | 1,000,000 | 5 | 137 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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