EPPLER 817 HYDROFOIL AIRFOIL (e817-il)
EPPLER 817 HYDROFOIL AIRFOIL - Eppler E817 hydrofoil
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(e817-il) EPPLER 817 HYDROFOIL AIRFOIL Eppler E817 hydrofoil Max thickness 11% at 32.9% chord. Max camber 2.9% at 66.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 817 HYDROFOIL AIRFOIL
35. 34.
0.0000100 -.0000500
0.0001600 0.0008700
0.0009300 0.0024200
0.0027300 0.0047200
0.0069500 0.0084800
0.0118000 0.0117500
0.0252100 0.0185000
0.0434200 0.0253300
0.0662600 0.0321300
0.0934500 0.0387700
0.1246900 0.0451200
0.1596500 0.0510500
0.1979700 0.0564500
0.2392500 0.0612400
0.2830700 0.0653300
0.3289600 0.0686400
0.3764500 0.0711100
0.4250500 0.0727100
0.4742400 0.0733700
0.5235300 0.0730900
0.5723800 0.0718300
0.6203000 0.0695600
0.6667600 0.0662700
0.7112500 0.0618100
0.7536100 0.0559100
0.7940200 0.0487800
0.8323200 0.0410700
0.8679600 0.0333500
0.9003500 0.0259600
0.9289200 0.0191900
0.9530900 0.0131500
0.9725400 0.0078300
0.9872300 0.0035200
0.9966800 0.0008500
1.0000000 0.0000000
0.0000100 -.0000500
0.0002000 -.0009600
0.0010300 -.0024800
0.0029300 -.0047000
0.0072900 -.0082700
0.0123200 -.0113600
0.0259000 -.0174900
0.0441600 -.0234400
0.0668600 -.0290600
0.0936800 -.0341900
0.1242800 -.0386000
0.1582800 -.0420200
0.1954800 -.0440400
0.2358800 -.0445200
0.2793500 -.0436000
0.3255500 -.0414200
0.3741000 -.0381000
0.3741000 -.0381000
0.4246000 -.0338300
0.4766000 -.0288000
0.5296000 -.0232800
0.5830400 -.0175200
0.6363100 -.0118300
0.6887500 -.0065000
0.7396500 -.0018100
0.7882300 0.0019900
0.8336900 0.0047200
0.8752100 0.0062700
0.9119800 0.0066200
0.9432200 0.0058500
0.9681100 0.0041700
0.9859400 0.0021600
0.9965200 0.0005900
1.0000000 0.0000000
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Polars for EPPLER 817 HYDROFOIL AIRFOIL (e817-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e817-il | 50,000 | 9 | 26.9 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e817-il | 50,000 | 5 | 29.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e817-il | 100,000 | 9 | 40.9 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e817-il | 100,000 | 5 | 47.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e817-il | 200,000 | 9 | 79.9 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e817-il | 200,000 | 5 | 71.3 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e817-il | 500,000 | 9 | 113.7 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e817-il | 500,000 | 5 | 98.2 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e817-il | 1,000,000 | 9 | 138.1 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e817-il | 1,000,000 | 5 | 112.4 at α=1.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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