EPPLER 341 AIRFOIL (e341-il)
EPPLER 341 AIRFOIL - Eppler E341 flying wing airfoil
| Details | Dat file | Parser | |
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(e341-il) EPPLER 341 AIRFOIL Eppler E341 flying wing airfoil Max thickness 13.9% at 32.8% chord. Max camber 3% at 23.2% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 341 AIRFOIL
33. 40.
0.0000300 0.0008200
0.0003300 0.0034000
0.0021100 0.0091000
0.0083700 0.0195700
0.0186500 0.0307200
0.0328600 0.0420800
0.0509000 0.0532500
0.0726000 0.0638900
0.0977700 0.0736900
0.1262100 0.0823400
0.1576700 0.0895300
0.1919400 0.0949400
0.2288400 0.0982600
0.2683600 0.0992100
0.3106300 0.0977500
0.3556100 0.0942700
0.4029400 0.0891200
0.4522000 0.0826000
0.5029100 0.0750600
0.5545100 0.0668400
0.6063900 0.0582900
0.6578900 0.0497400
0.7082700 0.0414800
0.7567800 0.0337700
0.8026600 0.0268100
0.8451600 0.0207100
0.8835400 0.0155200
0.9171399 0.0112100
0.9453501 0.0075900
0.9679900 0.0043700
0.9850900 0.0017600
0.9961300 0.0003500
1.0000000 0.0000000
0.0000300 0.0008200
0.0000500 -.0007900
0.0002500 -.0022800
0.0004200 -.0029700
0.0006400 -.0036200
0.0009400 -.0042100
0.0013300 -.0047600
0.0018200 -.0053000
0.0023900 -.0058400
0.0037700 -.0068900
0.0054300 -.0079200
0.0084000 -.0094600
0.0131300 -.0114600
0.0291700 -.0161800
0.0508700 -.0204300
0.0779400 -.0242400
0.1100900 -.0277300
0.1468500 -.0311000
0.1875900 -.0343900
0.2316800 -.0375400
0.2785100 -.0404500
0.3275000 -.0429700
0.3781200 -.0450000
0.4298100 -.0464900
0.4820200 -.0473900
0.5341800 -.0476600
0.5857000 -.0472700
0.6360200 -.0462000
0.6845800 -.0444300
0.7308600 -.0419300
0.7743200 -.0386400
0.8144300 -.0343600
0.8512300 -.0286500
0.8852500 -.0218600
0.9164300 -.0150900
0.9440100 -.0091900
0.9671000 -.0046100
0.9848101 -.0016500
0.9961000 0.0003000
1.0000000 0.0000000
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Polars for EPPLER 341 AIRFOIL (e341-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e341-il | 50,000 | 9 | 13.6 at α=1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e341-il | 50,000 | 5 | 23.1 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e341-il | 100,000 | 9 | 28.7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e341-il | 100,000 | 5 | 42.4 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e341-il | 200,000 | 9 | 59.1 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e341-il | 200,000 | 5 | 60.1 at α=10.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e341-il | 500,000 | 9 | 85.3 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e341-il | 500,000 | 5 | 80.7 at α=10.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e341-il | 1,000,000 | 9 | 102.8 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e341-il | 1,000,000 | 5 | 101.7 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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