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EPPLER 625 AIRFOIL (e625-il)

EPPLER 625 AIRFOIL - Eppler E625 airfoil


Airfoil e625-il
Details Dat file Parser  
(e625-il) EPPLER 625 AIRFOIL
Eppler E625 airfoil
Max thickness 13% at 30% chord.
Max camber 2.9% at 22.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 625 AIRFOIL
       50.       50.

 0.0000000 0.0002400
 0.0005000 0.0041700
 0.0010000 0.0058800
 0.0015000 0.0072900
 0.0020000 0.0085500
 0.0025000 0.0097300
 0.0030000 0.0108400
 0.0040000 0.0129000
 0.0050000 0.0147700
 0.0075000 0.0188600
 0.0100000 0.0223500
 0.0125000 0.0254300
 0.0150000 0.0282300
 0.0200000 0.0332200
 0.0250000 0.0376300
 0.0350000 0.0452100
 0.0500000 0.0544200
 0.0750000 0.0660300
 0.1000000 0.0745400
 0.1250000 0.0808800
 0.1500000 0.0855800
 0.1750000 0.0889300
 0.2000000 0.0911800
 0.2250000 0.0925100
 0.2500000 0.0930900
 0.2750000 0.0930600
 0.3000000 0.0924800
 0.3500000 0.0899600
 0.4000000 0.0859200
 0.4500000 0.0806700
 0.5000000 0.0744500
 0.5500000 0.0674900
 0.6000000 0.0599600
 0.6500000 0.0520300
 0.6750000 0.0479900
 0.7000000 0.0439100
 0.7250000 0.0398200
 0.7500000 0.0357400
 0.7750000 0.0317000
 0.8000000 0.0277100
 0.8250000 0.0238000
 0.8500000 0.0199900
 0.8750000 0.0163300
 0.9000000 0.0128000
 0.9250000 0.0094300
 0.9500000 0.0061900
 0.9700000 0.0036800
 0.9800000 0.0024400
 0.9900000 0.0012100
 1.0000000 0.0000000

 0.0000000 0.0002400
 0.0005000 -.0033100
 0.0010000 -.0046800
 0.0015000 -.0057200
 0.0020000 -.0065800
 0.0025000 -.0073200
 0.0030000 -.0079600
 0.0040000 -.0090200
 0.0050000 -.0098800
 0.0075000 -.0114900
 0.0100000 -.0126800
 0.0125000 -.0136700
 0.0150000 -.0145700
 0.0200000 -.0162100
 0.0250000 -.0176600
 0.0350000 -.0200600
 0.0500000 -.0227400
 0.0750000 -.0258600
 0.1000000 -.0280600
 0.1250000 -.0297600
 0.1500000 -.0311600
 0.1750000 -.0323700
 0.2000000 -.0334800
 0.2250000 -.0345400
 0.2500000 -.0355600
 0.2750000 -.0365600
 0.3000000 -.0375200
 0.3500000 -.0393400
 0.4000000 -.0408800
 0.4500000 -.0420300
 0.5000000 -.0427200
 0.5500000 -.0428800
 0.6000000 -.0424500
 0.6500000 -.0413200
 0.6750000 -.0404200
 0.7000000 -.0392600
 0.7250000 -.0378100
 0.7500000 -.0360200
 0.7750000 -.0338800
 0.8000000 -.0313900
 0.8250000 -.0285100
 0.8500000 -.0252200
 0.8750000 -.0215700
 0.9000000 -.0176000
 0.9250000 -.0134000
 0.9500000 -.0090200
 0.9700000 -.0054400
 0.9800000 -.0036300
 0.9900000 -.0018200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 625 AIRFOIL (e625-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e625-il50,000918.8 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e625-il50,000528.8 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   e625-il100,000939.2 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e625-il100,000544.5 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   e625-il200,000958 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e625-il200,000560.1 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e625-il500,000982.9 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e625-il500,000576.5 at α=9.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e625-il1,000,000996.7 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e625-il1,000,000593.2 at α=9.75°Mach=0 Ncrit=5Xfoil predictionDetails
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