EPPLER 604 AIRFOIL (e604-il)
EPPLER 604 AIRFOIL - Eppler E604 sailplane airfoil
| Details | Dat file | Parser | |
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(e604-il) EPPLER 604 AIRFOIL Eppler E604 sailplane airfoil Max thickness 18.8% at 37.3% chord. Max camber 3.4% at 42.3% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 604 AIRFOIL
35. 36.
0.0000500 -.0008300
0.0000600 0.0017700
0.0003200 0.0036300
0.0013300 0.0073600
0.0071200 0.0182300
0.0173400 0.0300300
0.0318200 0.0422300
0.0504500 0.0544600
0.0730800 0.0664000
0.0995100 0.0778200
0.1295000 0.0884800
0.1627900 0.0981900
0.1990500 0.1067600
0.2379400 0.1140500
0.2790500 0.1199000
0.3219700 0.1241700
0.3663000 0.1266800
0.4116600 0.1273100
0.4576700 0.1259500
0.5040100 0.1225200
0.5504100 0.1169100
0.5968400 0.1091900
0.6431800 0.0998300
0.6889900 0.0893300
0.7337700 0.0781100
0.7770100 0.0666000
0.8181100 0.0551800
0.8564700 0.0442600
0.8914400 0.0341500
0.9223400 0.0251000
0.9485000 0.0171700
0.9696000 0.0102200
0.9857000 0.0045800
0.9962400 0.0011000
1.0000000 0.0000000
0.0000500 -.0008300
0.0001700 -.0016200
0.0003700 -.0023700
0.0006600 -.0031000
0.0010500 -.0038200
0.0015300 -.0045600
0.0026800 -.0060300
0.0041000 -.0075200
0.0066700 -.0097700
0.0177500 -.0166100
0.0349100 -.0237600
0.0571600 -.0304500
0.0842500 -.0366100
0.1158300 -.0422300
0.1514700 -.0472600
0.1906900 -.0516300
0.2330200 -.0552500
0.2779400 -.0580500
0.3249000 -.0599500
0.3733000 -.0608600
0.4225100 -.0606400
0.4718800 -.0589400
0.5211400 -.0552200
0.5704800 -.0493200
0.6200500 -.0415700
0.6697600 -.0325500
0.7194100 -.0230300
0.7684000 -.0140400
0.8156900 -.0063900
0.8600800 -.0006000
0.9003500 0.0030500
0.9352700 0.0045000
0.9635100 0.0039700
0.9839000 0.0022900
0.9960100 0.0006600
1.0000000 0.0000000
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Polars for EPPLER 604 AIRFOIL (e604-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e604-il | 50,000 | 9 | 5.2 at α=12° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e604-il | 50,000 | 5 | 13.8 at α=14.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e604-il | 100,000 | 9 | 34.1 at α=12.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e604-il | 100,000 | 5 | 30.1 at α=10.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e604-il | 200,000 | 9 | 65.1 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e604-il | 200,000 | 5 | 67.1 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e604-il | 500,000 | 9 | 106.7 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e604-il | 500,000 | 5 | 101.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e604-il | 1,000,000 | 9 | 136.3 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e604-il | 1,000,000 | 5 | 123.8 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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