EPPLER 635 AIRFOIL (e635-il)
EPPLER 635 AIRFOIL - Eppler E635 airfoil
| Details | Dat file | Parser | |
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(e635-il) EPPLER 635 AIRFOIL Eppler E635 airfoil Max thickness 11.6% at 26.2% chord. Max camber 2.9% at 22.2% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 635 AIRFOIL
32. 30.
0.0002200 0.0000000
0.0015200 0.0075400
0.0069700 0.0167000
0.0164500 0.0266000
0.0298900 0.0367400
0.0471900 0.0467400
0.0682100 0.0562600
0.0927700 0.0650100
0.1206500 0.0727100
0.1515400 0.0790100
0.1853400 0.0834500
0.2220600 0.0858700
0.2616200 0.0861400
0.3040400 0.0842900
0.3492000 0.0806000
0.3967600 0.0754100
0.4463100 0.0690200
0.4973700 0.0617500
0.5493700 0.0539600
0.6017100 0.0459600
0.6537001 0.0381000
0.7046300 0.0306600
0.7537000 0.0238800
0.8001700 0.0179700
0.8432600 0.0130000
0.8822200 0.0090200
0.9163700 0.0059800
0.9451000 0.0036700
0.9681200 0.0018300
0.9853399 0.0005400
0.9962400 0.0000400
1.0000000 0.0000000
0.0002200 0.0000000
0.0047000 -.0054100
0.0157900 -.0096400
0.0326700 -.0134200
0.0551100 -.0166800
0.0828400 -.0195100
0.1156100 -.0220200
0.1529500 -.0244300
0.1942300 -.0268100
0.2388300 -.0291100
0.2861300 -.0312400
0.3355500 -.0330800
0.3865800 -.0345400
0.4386300 -.0355500
0.4911700 -.0361100
0.5436200 -.0361800
0.5954100 -.0357300
0.6459700 -.0347500
0.6947700 -.0332300
0.7413000 -.0311000
0.7851800 -.0284000
0.8259800 -.0252000
0.8633500 -.0216200
0.8969000 -.0177900
0.9262500 -.0138800
0.9510200 -.0100100
0.9710200 -.0061500
0.9863200 -.0027400
0.9964000 -.0006300
1.0000000 0.0000000
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Polars for EPPLER 635 AIRFOIL (e635-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e635-il | 50,000 | 9 | 14.6 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e635-il | 50,000 | 5 | 24 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e635-il | 100,000 | 9 | 36.3 at α=12° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e635-il | 100,000 | 5 | 43.4 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e635-il | 200,000 | 9 | 60.6 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e635-il | 200,000 | 5 | 64 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e635-il | 500,000 | 9 | 92.1 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e635-il | 500,000 | 5 | 88 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e635-il | 1,000,000 | 9 | 113.4 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e635-il | 1,000,000 | 5 | 100 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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