EPPLER 338 AIRFOIL (e338-il)
EPPLER 338 AIRFOIL - Eppler E338 flying wing airfoil
| Details | Dat file | Parser | |
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(e338-il) EPPLER 338 AIRFOIL Eppler E338 flying wing airfoil Max thickness 13.3% at 31.1% chord. Max camber 3.7% at 26.2% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 338 AIRFOIL
34. 39.
0.0000100 0.0003600
0.0001900 0.0028100
0.0003900 0.0039700
0.0042100 0.0136600
0.0120400 0.0244600
0.0238100 0.0357900
0.0399400 0.0472000
0.0588300 0.0583500
0.0818300 0.0689100
0.1082300 0.0785900
0.1378100 0.0870900
0.1703500 0.0941300
0.2056000 0.0994200
0.2434100 0.1026700
0.2836900 0.1036500
0.3265400 0.1023400
0.3718400 0.0990800
0.4192300 0.0941900
0.4682800 0.0879400
0.5185000 0.0806600
0.5693700 0.0726500
0.6202700 0.0642300
0.6705700 0.0557100
0.7195700 0.0473500
0.7665899 0.0394100
0.8109000 0.0320500
0.8518100 0.0254300
0.8886400 0.0195800
0.9208000 0.0145200
0.9477201 0.0100900
0.9692700 0.0060100
0.9856099 0.0025900
0.9962400 0.0005700
1.0000000 0.0000000
0.0000100 0.0003600
0.0000900 -.0011500
0.0003400 -.0025500
0.0005300 -.0032000
0.0007800 -.0038000
0.0010900 -.0043400
0.0015000 -.0048400
0.0020100 -.0053200
0.0026100 -.0057800
0.0040300 -.0066900
0.0057300 -.0075500
0.0087800 -.0087800
0.0207000 -.0120300
0.0400700 -.0151700
0.0652000 -.0177300
0.0958200 -.0199300
0.1314400 -.0220400
0.1713900 -.0241900
0.2150200 -.0263200
0.2616800 -.0283800
0.3107600 -.0302000
0.3617300 -.0317200
0.4140000 -.0328700
0.4669900 -.0336200
0.5201100 -.0339400
0.5727500 -.0337800
0.6243200 -.0331400
0.6742401 -.0319700
0.7219400 -.0302300
0.7668700 -.0278700
0.8084900 -.0246500
0.8467800 -.0201900
0.8822200 -.0148300
0.9146200 -.0096000
0.9431500 -.0052800
0.9668800 -.0022300
0.9848600 -.0005600
0.9961400 -.0000300
1.0000000 0.0000000
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Polars for EPPLER 338 AIRFOIL (e338-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e338-il | 50,000 | 9 | 15.8 at α=0.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e338-il | 50,000 | 5 | 26.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e338-il | 100,000 | 9 | 33.8 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e338-il | 100,000 | 5 | 45.9 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e338-il | 200,000 | 9 | 63.3 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e338-il | 200,000 | 5 | 67.8 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e338-il | 500,000 | 9 | 97.4 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e338-il | 500,000 | 5 | 88.6 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e338-il | 1,000,000 | 9 | 114 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e338-il | 1,000,000 | 5 | 108.2 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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