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EPPLER 333 AIRFOIL (e333-il)

EPPLER 333 AIRFOIL - Eppler E333 flying wing airfoil


Airfoil e333-il
Details Dat file Parser  
(e333-il) EPPLER 333 AIRFOIL
Eppler E333 flying wing airfoil
Max thickness 11.7% at 31.3% chord.
Max camber 3.5% at 26.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 333 AIRFOIL
       33.       39.

 0.0000400 0.0008100
 0.0003400 0.0032500
 0.0039300 0.0120400
 0.0115600 0.0219600
 0.0231400 0.0324000
 0.0386400 0.0429200
 0.0579300 0.0531800
 0.0809000 0.0628800
 0.1073400 0.0717300
 0.1370500 0.0794700
 0.1697900 0.0858200
 0.2053500 0.0905100
 0.2435900 0.0933100
 0.2843800 0.0940700
 0.3277100 0.0927900
 0.3734200 0.0897400
 0.4211200 0.0852000
 0.4704000 0.0794300
 0.5207700 0.0727200
 0.5716900 0.0653500
 0.6225600 0.0576100
 0.6727500 0.0497900
 0.7216001 0.0421500
 0.7684100 0.0349000
 0.8124800 0.0282200
 0.8531401 0.0222300
 0.8897400 0.0169900
 0.9216900 0.0124800
 0.9484400 0.0085800
 0.9698500 0.0050500
 0.9858900 0.0021500
 0.9963600 0.0004700
 1.0000000 0.0000000

 0.0000400 0.0008100
 0.0000400 -.0006100
 0.0002300 -.0019000
 0.0003900 -.0025000
 0.0006000 -.0030500
 0.0008700 -.0035400
 0.0012400 -.0039800
 0.0017200 -.0044000
 0.0022700 -.0048200
 0.0036100 -.0056100
 0.0052200 -.0063700
 0.0081200 -.0074700
 0.0215000 -.0105800
 0.0410400 -.0130700
 0.0663200 -.0149800
 0.0970800 -.0165300
 0.1328600 -.0180300
 0.1729800 -.0195900
 0.2167800 -.0212000
 0.2636100 -.0227900
 0.3128800 -.0242300
 0.3640300 -.0254300
 0.4164900 -.0263500
 0.4696600 -.0269500
 0.5229600 -.0272100
 0.5757900 -.0271000
 0.6275400 -.0265900
 0.6776300 -.0256700
 0.7255100 -.0242900
 0.7706200 -.0224000
 0.8124400 -.0198400
 0.8508500 -.0163100
 0.8861300 -.0121000
 0.9179900 -.0080400
 0.9456500 -.0046600
 0.9683900 -.0021600
 0.9855200 -.0006400
 0.9963000 -.0000700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 333 AIRFOIL (e333-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e333-il50,000917.4 at α=1°Mach=0 Ncrit=9Xfoil predictionDetails
   e333-il50,000527.8 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   e333-il100,000940.6 at α=11.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e333-il100,000548 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   e333-il200,000965.1 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   e333-il200,000568.8 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   e333-il500,000999.1 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e333-il500,000592.1 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e333-il1,000,0009117.1 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e333-il1,000,0005109.5 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
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