EPPLER E854 AIRFOIL (e854-il)
EPPLER E854 AIRFOIL - Eppler E854 propeller airfoil
| Details | Dat file | Parser | |
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(e854-il) EPPLER E854 AIRFOIL Eppler E854 propeller airfoil Max thickness 13.4% at 32.3% chord. Max camber 3.3% at 55.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER E854 AIRFOIL
35.0 33.0
0.0000000 0.0000000
0.0003400 0.0019900
0.0015200 0.0049501
0.0046801 0.0098502
0.0061901 0.0116702
0.0160303 0.0206804
0.0302806 0.0300906
0.0488510 0.0395708
0.0715914 0.0488910
0.0982920 0.0579012
0.1286326 0.0664013
0.1623033 0.0742115
0.1989440 0.0811516
0.2381848 0.0870317
0.2796056 0.0916918
0.3227764 0.0948619
0.3674273 0.0962619
0.4134183 0.0957919
0.4605492 0.0935219
0.5086002 0.0896118
0.5572211 0.0844017
0.6059021 0.0782116
0.6540830 0.0712914
0.7012140 0.0638913
0.7466849 0.0562511
0.7899358 0.0485610
0.8303666 0.0410208
0.8674273 0.0337707
0.9005880 0.0269305
0.9293585 0.0205704
0.9532791 0.0146403
0.9723294 0.0089402
0.9868597 0.0039101
0.9965199 0.0006300
1.0000000 -.0004200
0.0000000 0.0000000
0.0000900 -.0011500
0.0005200 -.0022500
0.0017500 -.0039601
0.0042201 -.0063101
0.0095402 -.0098902
0.0193904 -.0144703
0.0364207 -.0199104
0.0583512 -.0247905
0.0850017 -.0290506
0.1160723 -.0327207
0.1511430 -.0357507
0.1897638 -.0380608
0.2314546 -.0395508
0.2756955 -.0400308
0.3221264 -.0392608
0.3704774 -.0370607
0.4205784 -.0333507
0.4724394 -.0283606
0.5257605 -.0227205
0.5798316 -.0169503
0.6338927 -.0114402
0.6871337 -.0064801
0.7387148 -.0023300
0.7877657 0.0008600
0.8334467 0.0030201
0.8749475 0.0041301
0.9115082 0.0043001
0.9424188 0.0037001
0.9671493 0.0026001
0.9852297 0.0012800
0.9962799 0.0000900
1.0000000 -.0004200
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Polars for EPPLER E854 AIRFOIL (e854-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e854-il | 50,000 | 9 | 32.7 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e854-il | 50,000 | 5 | 31.8 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e854-il | 100,000 | 9 | 57.4 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e854-il | 100,000 | 5 | 58.1 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e854-il | 200,000 | 9 | 82.4 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e854-il | 200,000 | 5 | 80.6 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e854-il | 500,000 | 9 | 115.9 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e854-il | 500,000 | 5 | 103.9 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e854-il | 1,000,000 | 9 | 136.3 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e854-il | 1,000,000 | 5 | 117.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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