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EPPLER 856 AIRFOIL (e856-il)

EPPLER 856 AIRFOIL - Eppler E856 propeller airfoil


Airfoil e856-il
Details Dat file Parser  
(e856-il) EPPLER 856 AIRFOIL
Eppler E856 propeller airfoil
Max thickness 18.2% at 31.9% chord.
Max camber 4.2% at 50.2% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 856 AIRFOIL
       34.       34.

 0.0000700 0.0014000
 0.0007400 0.0054000
 0.0031200 0.0119900
 0.0091900 0.0222200
 0.0201700 0.0349000
 0.0352400 0.0479400
 0.0542700 0.0609500
 0.0770900 0.0736500
 0.1034500 0.0857900
 0.1330700 0.0971000
 0.1656100 0.1072900
 0.2007400 0.1160800
 0.2380900 0.1231100
 0.2774500 0.1279700
 0.3187800 0.1304500
 0.3619700 0.1304500
 0.4070300 0.1280500
 0.4537600 0.1236400
 0.5017300 0.1175800
 0.5504500 0.1101500
 0.5994000 0.1016500
 0.6480000 0.0923900
 0.6956800 0.0826600
 0.7418000 0.0727200
 0.7857500 0.0628300
 0.8269000 0.0532000
 0.8646500 0.0440000
 0.8983999 0.0353500
 0.9276500 0.0273300
 0.9518600 0.0198300
 0.9710800 0.0125000
 0.9859600 0.0058600
 0.9961900 0.0014400
 1.0000000 0.0000000

 0.0000700 0.0014000
 0.0001000 -.0013100
 0.0004400 -.0029300
 0.0011300 -.0044600
 0.0027500 -.0067800
 0.0058100 -.0099200
 0.0120600 -.0146200
 0.0138600 -.0157500
 0.0292000 -.0232000
 0.0495200 -.0300500
 0.0745700 -.0361300
 0.1041000 -.0413800
 0.1377200 -.0457800
 0.1749600 -.0492300
 0.2153300 -.0516000
 0.2583200 -.0526100
 0.3036200 -.0519100
 0.3511300 -.0493300
 0.4007800 -.0448600
 0.4526200 -.0388000
 0.5063800 -.0319200
 0.5613100 -.0248200
 0.6166100 -.0179700
 0.6714000 -.0117500
 0.7247600 -.0064400
 0.7757500 -.0022300
 0.8234400 0.0007600
 0.8669100 0.0025600
 0.9053100 0.0032700
 0.9378800 0.0031500
 0.9641001 0.0025600
 0.9836300 0.0016500
 0.9958300 0.0005500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 856 AIRFOIL (e856-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e856-il50,00094.6 at α=10.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e856-il50,000518.8 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e856-il100,000928.6 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e856-il100,000546.3 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e856-il200,000964.8 at α=10.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e856-il200,000570.1 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e856-il500,0009100.8 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e856-il500,000599.7 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e856-il1,000,0009128.9 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e856-il1,000,0005118.5 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
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