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EPPLER 556 AIRFOIL (e556-il)

EPPLER 556 AIRFOIL - Eppler E556 general aviation airfoil


Airfoil e556-il
Details Dat file Parser  
(e556-il) EPPLER 556 AIRFOIL
Eppler E556 general aviation airfoil
Max thickness 16% at 31.1% chord.
Max camber 3.1% at 61.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 556 AIRFOIL
       35.       38.

 0.0000100 0.0004500
 0.0001600 0.0021100
 0.0005000 0.0038600
 0.0013700 0.0066000
 0.0058100 0.0145700
 0.0153200 0.0250700
 0.0291200 0.0358500
 0.0471100 0.0465400
 0.0691400 0.0568400
 0.0950500 0.0665100
 0.1246300 0.0753600
 0.1576200 0.0831900
 0.1937100 0.0898500
 0.2325700 0.0951600
 0.2739000 0.0989300
 0.3174600 0.1010700
 0.3629300 0.1016300
 0.4099200 0.1006100
 0.4580500 0.0980800
 0.5069300 0.0941600
 0.5561100 0.0889900
 0.6051400 0.0827700
 0.6535200 0.0756900
 0.7007599 0.0679800
 0.7463300 0.0599000
 0.7896800 0.0516600
 0.8302800 0.0435200
 0.8675700 0.0356600
 0.9010100 0.0282700
 0.9301200 0.0214800
 0.9544300 0.0154000
 0.9735100 0.0099500
 0.9874600 0.0049900
 0.9966200 0.0013200
 1.0000000 0.0000000

 0.0000100 0.0004500
 0.0000200 -.0003400
 0.0000900 -.0011000
 0.0002400 -.0018100
 0.0004900 -.0025100
 0.0008200 -.0032200
 0.0012400 -.0039400
 0.0022600 -.0053900
 0.0035400 -.0068700
 0.0058700 -.0091300
 0.0075700 -.0105700
 0.0197200 -.0182000
 0.0368300 -.0256800
 0.0586000 -.0328000
 0.0847600 -.0394000
 0.1149900 -.0453900
 0.1488300 -.0506300
 0.1858100 -.0549600
 0.2254300 -.0581400
 0.2671700 -.0597800
 0.3108000 -.0593500
 0.3564400 -.0565800
 0.4041700 -.0515100
 0.4541600 -.0444600
 0.5062600 -.0362300
 0.5598700 -.0275600
 0.6142500 -.0190100
 0.6685500 -.0111000
 0.7218600 -.0042500
 0.7731900 0.0011900
 0.8215300 0.0050400
 0.8658700 0.0072000
 0.9052200 0.0077600
 0.9386700 0.0069100
 0.9653900 0.0050200
 0.9846600 0.0026900
 0.9961799 0.0007600
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 556 AIRFOIL (e556-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e556-il50,000925.5 at α=11.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e556-il50,000532.5 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e556-il100,000952.9 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e556-il100,000553.2 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e556-il200,000972.3 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e556-il200,000570.2 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e556-il500,000997.9 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e556-il500,000590.8 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e556-il1,000,0009116.4 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e556-il1,000,0005105.2 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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