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EPPLER E854 AIRFOIL (e854-il)

EPPLER E854 AIRFOIL - Eppler E854 propeller airfoil


Airfoil e854-il
Details Dat file Parser  
(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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Lednicer format dat file
Selig format dat file

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Polars for EPPLER E854 AIRFOIL (e854-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e854-il50,000932.7 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e854-il50,000531.8 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e854-il100,000957.4 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e854-il100,000558.1 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e854-il200,000982.4 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e854-il200,000580.6 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e854-il500,0009115.9 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   e854-il500,0005103.9 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e854-il1,000,0009136.3 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e854-il1,000,0005117.5 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
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