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EPPLER 908 AIRFOIL (e908-il)

EPPLER 908 AIRFOIL - Eppler E908 hydrofoil


Airfoil e908-il
Details Dat file Parser  
(e908-il) EPPLER 908 AIRFOIL
Eppler E908 hydrofoil
Max thickness 9% at 44.8% chord.
Max camber 2.8% at 66.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 908 AIRFOIL
      57.0      53.0
 
 0.0000200 0.0002300
 0.0013500 0.0022400
 0.0044000 0.0047600
 0.0090500 0.0075800
 0.0152400 0.0106200
 0.0229500 0.0138100
 0.0321400 0.0171300
 0.0427900 0.0205200
 0.0548500 0.0239600
 0.0682900 0.0274300
 0.0830600 0.0308900
 0.0991200 0.0343400
 0.1164200 0.0377600
 0.1348800 0.0411400
 0.1544200 0.0444400
 0.1750000 0.0476200
 0.1965300 0.0506700
 0.2189700 0.0535700
 0.2422300 0.0562900
 0.2662500 0.0588300
 0.2909500 0.0611800
 0.3162200 0.0633200
 0.3419900 0.0652100
 0.3681900 0.0668400
 0.3947300 0.0681900
 0.4215200 0.0692500
 0.4484900 0.0700000
 0.4755400 0.0704000
 0.5026400 0.0704100
 0.5297700 0.0700700
 0.5568400 0.0694100
 0.5837600 0.0684600
 0.6104400 0.0672300
 0.6367800 0.0657300
 0.6627100 0.0639800
 0.6881300 0.0619800
 0.7129500 0.0597300
 0.7371000 0.0572600
 0.7604900 0.0545500
 0.7830300 0.0516100
 0.8046400 0.0484200
 0.8252900 0.0448800
 0.8450900 0.0409700
 0.8641200 0.0368800
 0.8822700 0.0327800
 0.8994200 0.0287400
 0.9154600 0.0248400
 0.9302900 0.0210900
 0.9438100 0.0175500
 0.9559200 0.0141800
 0.9665800 0.0109200
 0.9759200 0.0078100
 0.9839500 0.0050100
 0.9906000 0.0027300
 0.9956700 0.0011200
 0.9988900 0.0002500
 1.0000000 0.0000000
 
 0.0000200 0.0002300
 0.0008300 -.0015400
 0.0037500 -.0035500
 0.0083200 -.0057100
 0.0145000 -.0079300
 0.0222200 -.0101400
 0.0314400 -.0123000
 0.0421300 -.0143700
 0.0542200 -.0163000
 0.0676800 -.0180300
 0.0824900 -.0194400
 0.0987600 -.0205100
 0.1165100 -.0213300
 0.1356500 -.0219700
 0.1561200 -.0224600
 0.1778300 -.0228000
 0.2006900 -.0230200
 0.2246200 -.0231200
 0.2495300 -.0231100
 0.2753200 -.0230000
 0.3019000 -.0227800
 0.3291600 -.0224700
 0.3570000 -.0220600
 0.3853300 -.0215400
 0.4140300 -.0209300
 0.4429900 -.0202000
 0.4721200 -.0193600
 0.5013000 -.0183800
 0.5304100 -.0172400
 0.5593400 -.0158800
 0.5881000 -.0141400
 0.6168300 -.0120900
 0.6455100 -.0099300
 0.6739800 -.0078000
 0.7020900 -.0057700
 0.7297000 -.0039000
 0.7566500 -.0023300
 0.7828100 -.0007700
 0.8080400 0.0004500
 0.8321900 0.0014200
 0.8551400 0.0021400
 0.8767600 0.0026300
 0.8969300 0.0028900
 0.9155500 0.0029500
 0.9325100 0.0028400
 0.9477100 0.0026000
 0.9611000 0.0022900
 0.9726500 0.0019300
 0.9822900 0.0015100
 0.9899300 0.0010400
 0.9954900 0.0005600
 0.9988700 0.0001700
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for EPPLER 908 AIRFOIL (e908-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e908-il50,000922.2 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   e908-il50,000524.4 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   e908-il100,000932.2 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e908-il100,000541.2 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e908-il200,000947.8 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e908-il200,000562.8 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   e908-il500,0009107.2 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e908-il500,000591.8 at α=2°Mach=0 Ncrit=5Xfoil predictionDetails
   e908-il1,000,0009137 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e908-il1,000,0005117.9 at α=1°Mach=0 Ncrit=5Xfoil predictionDetails
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