EPPLER 328 AIRFOIL (e328-il)
EPPLER 328 AIRFOIL - Eppler E328 flying wing airfoil
| Details | Dat file | Parser | |
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(e328-il) EPPLER 328 AIRFOIL Eppler E328 flying wing airfoil Max thickness 13.3% at 31.5% chord. Max camber 3% at 22.1% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 328 AIRFOIL
33. 40.
0.0000200 0.0008000
0.0003400 0.0032800
0.0032300 0.0109400
0.0105100 0.0211300
0.0218400 0.0318600
0.0371400 0.0427000
0.0563000 0.0532800
0.0791800 0.0633100
0.1055600 0.0724800
0.1352400 0.0805300
0.1679900 0.0871700
0.2035900 0.0921300
0.2418900 0.0951800
0.2827600 0.0961600
0.3261900 0.0950700
0.3720000 0.0921900
0.4198300 0.0877800
0.4692300 0.0821100
0.5197100 0.0754600
0.5707500 0.0681100
0.6217400 0.0603500
0.6720300 0.0524700
0.7209800 0.0447200
0.7678700 0.0373200
0.8120201 0.0304500
0.8527400 0.0242300
0.8893800 0.0187300
0.9213600 0.0139300
0.9481400 0.0097000
0.9695600 0.0057900
0.9857700 0.0025100
0.9962900 0.0005600
1.0000000 0.0000000
0.0000200 0.0008000
0.0000200 -.0007300
0.0001900 -.0021500
0.0003400 -.0028000
0.0005500 -.0034100
0.0008200 -.0039700
0.0011900 -.0044800
0.0016600 -.0049800
0.0022200 -.0054700
0.0035500 -.0064400
0.0051600 -.0074000
0.0080500 -.0088100
0.0098900 -.0095800
0.0244100 -.0138800
0.0447100 -.0176900
0.0705100 -.0210500
0.1015300 -.0241100
0.1372900 -.0270900
0.1771600 -.0300400
0.2205000 -.0329100
0.2666800 -.0355900
0.3151300 -.0379400
0.3653200 -.0398300
0.4166800 -.0412200
0.4686500 -.0420400
0.5206500 -.0422300
0.5721000 -.0417500
0.6224300 -.0405300
0.6710500 -.0384900
0.7174100 -.0353900
0.7614100 -.0308100
0.8034200 -.0249900
0.8433400 -.0188300
0.8804700 -.0130500
0.9140400 -.0081100
0.9431900 -.0043100
0.9671100 -.0017600
0.9850300 -.0004000
0.9962000 -.0000100
1.0000000 0.0000000
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Polars for EPPLER 328 AIRFOIL (e328-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e328-il | 50,000 | 9 | 17.6 at α=1° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e328-il | 50,000 | 5 | 27.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e328-il | 100,000 | 9 | 37.7 at α=12.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e328-il | 100,000 | 5 | 46.6 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e328-il | 200,000 | 9 | 63.5 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e328-il | 200,000 | 5 | 63.6 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e328-il | 500,000 | 9 | 88.9 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e328-il | 500,000 | 5 | 86.7 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e328-il | 1,000,000 | 9 | 111.1 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e328-il | 1,000,000 | 5 | 105.1 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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