EPPLER 864 STRUT AIRFOIL (e864-il)
EPPLER 864 STRUT AIRFOIL - Eppler E864 strut airfoil
| Details | Dat file | Parser | |
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(e864-il) EPPLER 864 STRUT AIRFOIL Eppler E864 strut airfoil Max thickness 38.8% at 32.7% chord. Max camber 0.1% at 10.8% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 864 STRUT AIRFOIL
31. 31.
0.0000000 0.0000000
0.0027700 0.0213500
0.0105700 0.0433300
0.0227200 0.0653000
0.0389200 0.0867600
0.0589800 0.1072600
0.0826500 0.1264000
0.1079100 0.1438200
0.1398900 0.1591900
0.1729000 0.1721900
0.2084100 0.1825300
0.2460800 0.1898800
0.2856500 0.1938600
0.3269200 0.1941300
0.3699800 0.1902000
0.4154900 0.1822200
0.4635900 0.1711700
0.5137600 0.1579300
0.5653400 0.1431700
0.6176200 0.1275300
0.6697600 0.1115900
0.7208600 0.0958400
0.7745800 0.0791500
0.8240600 0.0636500
0.8685700 0.0496400
0.9074400 0.0373500
0.9400800 0.0270100
0.9659900 0.0187900
0.9847900 0.0128300
0.9961799 0.0092100
1.0000000 0.0080000
0.0000000 0.0000000
0.0027700 -.0213500
0.0105700 -.0433300
0.0227200 -.0653000
0.0389200 -.0867600
0.0589800 -.1072600
0.0826500 -.1264000
0.1097100 -.1438200
0.1398900 -.1591900
0.1729000 -.1721900
0.2084100 -.1825300
0.2460800 -.1898800
0.2856500 -.1938600
0.3269200 -.1941300
0.3699800 -.1902000
0.4154900 -.1822200
0.4635900 -.1711700
0.5137600 -.1579300
0.5653400 -.1431700
0.6176200 -.1275300
0.6697600 -.1115900
0.7208600 -.0958400
0.7745800 -.0791500
0.8240600 -.0636500
0.8685700 -.0496400
0.9077400 -.0373500
0.9400800 -.0270100
0.9659900 -.0187900
0.9847900 -.0128300
0.9961799 -.0092100
1.0000000 -.0080000
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Polars for EPPLER 864 STRUT AIRFOIL (e864-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e864-il | 50,000 | 9 | 2.5 at α=-8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e864-il | 50,000 | 5 | 3.7 at α=-2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e864-il | 100,000 | 9 | 4.2 at α=-4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e864-il | 100,000 | 5 | 4.9 at α=-3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e864-il | 200,000 | 9 | 7.6 at α=-1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e864-il | 200,000 | 5 | 15 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e864-il | 500,000 | 9 | 37.7 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e864-il | 500,000 | 5 | 33.1 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e864-il | 1,000,000 | 9 | 50.3 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e864-il | 1,000,000 | 5 | 46.7 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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