EPPLER 334 AIRFOIL (e334-il)
EPPLER 334 AIRFOIL - Eppler E334 flying wing airfoil
| Details | Dat file | Parser | |
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(e334-il) EPPLER 334 AIRFOIL Eppler E334 flying wing airfoil Max thickness 11.9% at 30.3% chord. Max camber 4% at 25.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 334 AIRFOIL
34. 39.
0.0000100 0.0002300
0.0001600 0.0025300
0.0008200 0.0054600
0.0053600 0.0149100
0.0138500 0.0253400
0.0262400 0.0362200
0.0424800 0.0471300
0.0624800 0.0577300
0.0860700 0.0677500
0.1130600 0.0768800
0.1432400 0.0848600
0.1763700 0.0914300
0.2122300 0.0963000
0.2506600 0.0992500
0.2915500 0.1000900
0.3348800 0.0988300
0.3805100 0.0957600
0.4280600 0.0911500
0.4771000 0.0852700
0.5271500 0.0783900
0.5776600 0.0708100
0.6280700 0.0628100
0.6777400 0.0546800
0.7260100 0.0466700
0.7722100 0.0390100
0.8156600 0.0318700
0.8557000 0.0253900
0.8916900 0.0196200
0.9230700 0.0145800
0.9493100 0.0101300
0.9702700 0.0060600
0.9861200 0.0026400
0.9963800 0.0006000
1.0000000 0.0000000
0.0000100 0.0002300
0.0001000 -.0011700
0.0003600 -.0024600
0.0005500 -.0030500
0.0008000 -.0035900
0.0011000 -.0040700
0.0015000 -.0045000
0.0020000 -.0049100
0.0025900 -.0053000
0.0039900 -.0060400
0.0056700 -.0067300
0.0086800 -.0076700
0.0171200 -.0095100
0.0352300 -.0116500
0.0593200 -.0130900
0.0891300 -.0141200
0.1241800 -.0150700
0.1637900 -.0161200
0.2072700 -.0172700
0.2539500 -.0184600
0.3032200 -.0195600
0.3545200 -.0205000
0.4072500 -.0212300
0.4608300 -.0217300
0.5146300 -.0219600
0.5680400 -.0219100
0.6204500 -.0215400
0.6712700 -.0208300
0.7199000 -.0197300
0.7657900 -.0182000
0.8083900 -.0160400
0.8475900 -.0129300
0.8836500 -.0091900
0.9162600 -.0056600
0.9446200 -.0028600
0.9679200 -.0009900
0.9853900 -.0000800
0.9962900 -.0000700
1.0000000 0.0000000
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Polars for EPPLER 334 AIRFOIL (e334-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e334-il | 50,000 | 9 | 16.6 at α=0.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e334-il | 50,000 | 5 | 27.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e334-il | 100,000 | 9 | 39.9 at α=12° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e334-il | 100,000 | 5 | 48.6 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e334-il | 200,000 | 9 | 66.1 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e334-il | 200,000 | 5 | 70 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e334-il | 500,000 | 9 | 100.8 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e334-il | 500,000 | 5 | 98.4 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e334-il | 1,000,000 | 9 | 125.6 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e334-il | 1,000,000 | 5 | 116.5 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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