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EPPLER 545 AIRFOIL (e545-il)

EPPLER 545 AIRFOIL - Eppler E545 general aviation airfoil


Airfoil e545-il
Details Dat file Parser  
(e545-il) EPPLER 545 AIRFOIL
Eppler E545 general aviation airfoil
Max thickness 17.4% at 39.3% chord.
Max camber 1.8% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 545 AIRFOIL
       36.       37.

 0.0000100 -.0001300
 0.0000200 0.0006200
 0.0002300 0.0022000
 0.0006600 0.0038800
 0.0016600 0.0065400
 0.0035500 0.0101100
 0.0116800 0.0201300
 0.0242800 0.0307100
 0.0411900 0.0414300
 0.0622600 0.0519700
 0.0873100 0.0620700
 0.1161200 0.0715100
 0.1448300 0.0800900
 0.1839100 0.0876500
 0.2222400 0.0940500
 0.2630300 0.0991300
 0.3058600 0.1027600
 0.3502800 0.1047800
 0.3959400 0.1049500
 0.4426100 0.1031200
 0.4901700 0.0992800
 0.5384400 0.0937500
 0.5869900 0.0868500
 0.6353500 0.0788800
 0.6830400 0.0701500
 0.7295200 0.0609900
 0.7742299 0.0517200
 0.8165600 0.0426700
 0.8558800 0.0341100
 0.8915700 0.0262900
 0.9229700 0.0193600
 0.9495000 0.0134400
 0.9705800 0.0084000
 0.9861500 0.0040600
 0.9963100 0.0010300
 1.0000000 0.0000000

 0.0000100 -.0001300
 0.0000400 -.0008400
 0.0001700 -.0015100
 0.0004000 -.0021600
 0.0007300 -.0028200
 0.0011400 -.0034900
 0.0021700 -.0048500
 0.0034600 -.0062400
 0.0058500 -.0083800
 0.0123600 -.0129000
 0.0271700 -.0202900
 0.0470300 -.0275600
 0.0716600 -.0345700
 0.1007600 -.0411900
 0.1339900 -.0473700
 0.1708800 -.0530600
 0.2109600 -.0581200
 0.2536900 -.0624600
 0.2985600 -.0659100
 0.3450200 -.0683300
 0.3925000 -.0695400
 0.4404400 -.0693400
 0.4882100 -.0672400
 0.5358900 -.0625300
 0.5840600 -.0552700
 0.6330400 -.0462000
 0.6825900 -.0364600
 0.7318600 -.0270000
 0.7798700 -.0184400
 0.8255800 -.0112500
 0.8679400 -.0057100
 0.9058700 -.0019000
 0.9384100 0.0002900
 0.9647000 0.0011300
 0.9840800 0.0009900
 0.9959900 0.0003600
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 545 AIRFOIL (e545-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e545-il50,00096.7 at α=13.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e545-il50,000519.2 at α=11.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e545-il100,000943.3 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   e545-il100,000542.9 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e545-il200,000964.3 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e545-il200,000563.6 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e545-il500,000991 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e545-il500,000581.8 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e545-il1,000,0009106.4 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e545-il1,000,000585 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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