EPPLER 336 AIRFOIL (e336-il)
EPPLER 336 AIRFOIL - Eppler E336 flying wing airfoil
| Details | Dat file | Parser | |
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(e336-il) EPPLER 336 AIRFOIL Eppler E336 flying wing airfoil Max thickness 12.8% at 28.1% chord. Max camber 2.8% at 23.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 336 AIRFOIL
34. 39.
0.0000100 -.0003800
0.0000500 0.0011300
0.0004400 0.0035400
0.0018800 0.0077500
0.0079400 0.0174600
0.0180600 0.0278500
0.0321600 0.0384500
0.0501300 0.0488700
0.0718500 0.0587700
0.0971100 0.0678700
0.1257100 0.0758500
0.1574200 0.0824500
0.1920400 0.0873500
0.2294200 0.0903000
0.2694900 0.0911000
0.3022800 0.0897300
0.3576900 0.0865100
0.4053600 0.0817500
0.4548600 0.0757400
0.5057100 0.0687800
0.5573500 0.0611900
0.6091800 0.0532900
0.6605200 0.0454000
0.7106900 0.0377900
0.7589300 0.0306900
0.8045099 0.0242900
0.8466800 0.0186900
0.8847500 0.0139500
0.9180600 0.0100300
0.9460400 0.0067500
0.9684600 0.0038500
0.9853600 0.0015300
0.9962100 0.0003000
1.0000000 0.0000000
0.0000100 -.0003800
0.0001400 -.0017700
0.0002800 -.0024200
0.0004700 -.0030200
0.0007300 -.0035800
0.0010900 -.0040900
0.0015500 -.0045900
0.0021000 -.0050800
0.0034100 -.0060600
0.0049900 -.0070100
0.0078500 -.0084300
0.0140700 -.0108600
0.0303900 -.0151900
0.0523100 -.0190500
0.0795600 -.0224900
0.1118700 -.0256300
0.1487600 -.0286700
0.1896100 -.0316700
0.2337900 -.0345600
0.2806900 -.0372400
0.3297400 -.0395700
0.3804000 -.0414600
0.4321200 -.0428500
0.4843500 -.0436800
0.5365000 -.0439400
0.5880200 -.0435900
0.6383400 -.0426100
0.6868900 -.0409800
0.7331500 -.0386600
0.7766001 -.0356300
0.8167300 -.0316700
0.8535100 -.0264300
0.8874100 -.0202300
0.9183000 -.0140700
0.9454100 -.0087000
0.9679700 -.0044700
0.9852101 -.0016500
0.9962000 -.0003100
1.0000000 0.0000000
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Polars for EPPLER 336 AIRFOIL (e336-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e336-il | 50,000 | 9 | 16.1 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e336-il | 50,000 | 5 | 25.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e336-il | 100,000 | 9 | 35.7 at α=11.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e336-il | 100,000 | 5 | 44.8 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e336-il | 200,000 | 9 | 61.7 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e336-il | 200,000 | 5 | 62.4 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e336-il | 500,000 | 9 | 87.8 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e336-il | 500,000 | 5 | 78.6 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e336-il | 1,000,000 | 9 | 99 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e336-il | 1,000,000 | 5 | 96.7 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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