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EPPLER 604 AIRFOIL (e604-il)

EPPLER 604 AIRFOIL - Eppler E604 sailplane airfoil


Airfoil e604-il
Details Dat file Parser  
(e604-il) EPPLER 604 AIRFOIL
Eppler E604 sailplane airfoil
Max thickness 18.8% at 37.3% chord.
Max camber 3.4% at 42.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 604 AIRFOIL
       35.       36.

 0.0000500 -.0008300
 0.0000600 0.0017700
 0.0003200 0.0036300
 0.0013300 0.0073600
 0.0071200 0.0182300
 0.0173400 0.0300300
 0.0318200 0.0422300
 0.0504500 0.0544600
 0.0730800 0.0664000
 0.0995100 0.0778200
 0.1295000 0.0884800
 0.1627900 0.0981900
 0.1990500 0.1067600
 0.2379400 0.1140500
 0.2790500 0.1199000
 0.3219700 0.1241700
 0.3663000 0.1266800
 0.4116600 0.1273100
 0.4576700 0.1259500
 0.5040100 0.1225200
 0.5504100 0.1169100
 0.5968400 0.1091900
 0.6431800 0.0998300
 0.6889900 0.0893300
 0.7337700 0.0781100
 0.7770100 0.0666000
 0.8181100 0.0551800
 0.8564700 0.0442600
 0.8914400 0.0341500
 0.9223400 0.0251000
 0.9485000 0.0171700
 0.9696000 0.0102200
 0.9857000 0.0045800
 0.9962400 0.0011000
 1.0000000 0.0000000

 0.0000500 -.0008300
 0.0001700 -.0016200
 0.0003700 -.0023700
 0.0006600 -.0031000
 0.0010500 -.0038200
 0.0015300 -.0045600
 0.0026800 -.0060300
 0.0041000 -.0075200
 0.0066700 -.0097700
 0.0177500 -.0166100
 0.0349100 -.0237600
 0.0571600 -.0304500
 0.0842500 -.0366100
 0.1158300 -.0422300
 0.1514700 -.0472600
 0.1906900 -.0516300
 0.2330200 -.0552500
 0.2779400 -.0580500
 0.3249000 -.0599500
 0.3733000 -.0608600
 0.4225100 -.0606400
 0.4718800 -.0589400
 0.5211400 -.0552200
 0.5704800 -.0493200
 0.6200500 -.0415700
 0.6697600 -.0325500
 0.7194100 -.0230300
 0.7684000 -.0140400
 0.8156900 -.0063900
 0.8600800 -.0006000
 0.9003500 0.0030500
 0.9352700 0.0045000
 0.9635100 0.0039700
 0.9839000 0.0022900
 0.9960100 0.0006600
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 604 AIRFOIL (e604-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e604-il50,00095.2 at α=12°Mach=0 Ncrit=9Xfoil predictionDetails
   e604-il50,000513.8 at α=14.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e604-il100,000934.1 at α=12.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e604-il100,000530.1 at α=10.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e604-il200,000965.1 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e604-il200,000567.1 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   e604-il500,0009106.7 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e604-il500,0005101.8 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   e604-il1,000,0009136.3 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e604-il1,000,0005123.8 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
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