EPPLER 655 AIRFOIL (e655-il)
EPPLER 655 AIRFOIL - Eppler E655 sailplane airfoil
| Details | Dat file | Parser | |
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(e655-il) EPPLER 655 AIRFOIL Eppler E655 sailplane airfoil Max thickness 17.3% at 37.3% chord. Max camber 3.9% at 42.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 655 AIRFOIL
35. 38.
0.0000200 0.0008800
0.0002200 0.0027400
0.0008500 0.0057000
0.0013800 0.0074100
0.0071200 0.0183800
0.0171900 0.0302100
0.0314600 0.0424200
0.0498100 0.0546300
0.0721000 0.0665300
0.0981500 0.0778600
0.1277600 0.0883900
0.1606600 0.0979300
0.1965600 0.1063100
0.2351200 0.1133900
0.2759800 0.1190400
0.3187300 0.1231500
0.3629400 0.1256100
0.4081600 0.1263500
0.4539000 0.1252100
0.4997500 0.1219900
0.5454700 0.1164700
0.5910000 0.1084700
0.6366800 0.0982200
0.6825000 0.0866000
0.7278399 0.0744700
0.7719700 0.0623600
0.8141500 0.0507500
0.8536000 0.0400000
0.8895500 0.0303500
0.9212700 0.0219600
0.9480700 0.0147900
0.9696000 0.0086800
0.9858500 0.0038500
0.9963200 0.0009200
1.0000000 0.0000000
0.0000200 0.0008800
0.0000300 -.0008900
0.0001100 -.0017300
0.0002400 -.0025300
0.0004600 -.0032800
0.0007700 -.0040100
0.0011700 -.0047400
0.0016500 -.0054700
0.0028000 -.0069400
0.0042100 -.0084100
0.0067600 -.0106100
0.0164400 -.0165400
0.0329200 -.0231900
0.0544700 -.0291700
0.0808600 -.0343800
0.1118400 -.0387500
0.1470900 -.0422700
0.1862500 -.0449400
0.2288800 -.0467700
0.2745100 -.0478000
0.3226100 -.0480500
0.3726200 -.0475300
0.4239300 -.0462600
0.4759200 -.0442100
0.5279800 -.0412900
0.5795400 -.0373500
0.6303200 -.0321100
0.6804000 -.0257400
0.7295300 -.0188300
0.7772500 -.0119800
0.8228900 -.0058400
0.8655400 -.0009900
0.9041500 0.0022300
0.9376400 0.0036500
0.9647900 0.0033200
0.9844400 0.0019400
0.9961400 0.0005600
1.0000000 0.0000000
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Polars for EPPLER 655 AIRFOIL (e655-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e655-il | 50,000 | 9 | 4.9 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e655-il | 50,000 | 5 | 14.6 at α=12.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e655-il | 100,000 | 9 | 36.4 at α=12° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e655-il | 100,000 | 5 | 30.7 at α=10.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e655-il | 200,000 | 9 | 69.2 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e655-il | 200,000 | 5 | 69.2 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e655-il | 500,000 | 9 | 116.8 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e655-il | 500,000 | 5 | 111.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e655-il | 1,000,000 | 9 | 150.5 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e655-il | 1,000,000 | 5 | 135.1 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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