EPPLER E836 HYDROFOIL AIRFOIL (e836-il)
EPPLER E836 HYDROFOIL AIRFOIL - Eppler E836 hydrofoil
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(e836-il) EPPLER E836 HYDROFOIL AIRFOIL Eppler E836 hydrofoil Max thickness 12.6% at 42.8% chord. Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER E836 HYDROFOIL AIRFOIL
31.0 31.0
0.0000000 0.0000000
0.0030700 0.0056000
0.0117600 0.0121800
0.0253900 0.0190300
0.0437600 0.0258400
0.0666900 0.0324100
0.0939700 0.0385800
0.1253500 0.0442300
0.1604900 0.0492900
0.1990600 0.0536500
0.2406400 0.0572700
0.2848000 0.0600900
0.3310600 0.0620500
0.3789100 0.0631000
0.4278400 0.0632000
0.4773000 0.0622300
0.5268400 0.0600600
0.5761500 0.0566200
0.6249000 0.0520000
0.6727700 0.0463300
0.7194500 0.0398300
0.7646500 0.0328600
0.8078900 0.0259900
0.8484300 0.0196600
0.8855100 0.0141300
0.9183800 0.0095600
0.9463400 0.0059300
0.9689100 0.0031200
0.9857600 0.0011800
0.9963600 0.0002200
1.0000000 0.0000000
0.0000000 0.0000000
0.0030700 -.0056000
0.0117600 -.0121800
0.0253900 -.0190300
0.0437600 -.0258400
0.0666900 -.0324100
0.0939700 -.0385800
0.1253500 -.0442300
0.1604900 -.0492900
0.1990600 -.0536500
0.2406400 -.0572700
0.2848000 -.0600900
0.3310600 -.0620500
0.3789100 -.0631000
0.4278400 -.0632000
0.4773000 -.0622300
0.5268400 -.0600600
0.5761500 -.0566200
0.6249000 -.0520000
0.6727700 -.0463300
0.7194500 -.0398300
0.7646500 -.0328600
0.8078900 -.0259900
0.8484300 -.0196600
0.8855100 -.0141300
0.9183800 -.0095600
0.9463400 -.0059300
0.9689100 -.0031200
0.9857600 -.0011800
0.9963600 -.0002200
1.0000000 0.0000000
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Polars for EPPLER E836 HYDROFOIL AIRFOIL (e836-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e836-il | 50,000 | 9 | 28.7 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e836-il | 50,000 | 5 | 28.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e836-il | 100,000 | 9 | 43.1 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e836-il | 100,000 | 5 | 34.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e836-il | 200,000 | 9 | 45.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e836-il | 200,000 | 5 | 42.4 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e836-il | 500,000 | 9 | 60 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e836-il | 500,000 | 5 | 49.9 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e836-il | 1,000,000 | 9 | 67.1 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e836-il | 1,000,000 | 5 | 59.1 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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