Airfoil Tools
Search 1636 airfoils Google+
You have 0 airfoils loaded.
Your Reynold number range is 50,000 to 1,000,000. (set)

EPPLER 59 AIRFOIL (e59-il)

EPPLER 59 AIRFOIL - Eppler E59 low Reynolds number airfoil


Airfoil e59-il
Details Dat file Parser  
(e59-il) EPPLER 59 AIRFOIL
Eppler E59 low Reynolds number airfoil
Max thickness 5.6% at 25% chord.
Max camber 5.2% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 59 AIRFOIL
       18.       18.

 0.0000000 0.0000000
 0.0125000 0.0160000
 0.0250000 0.0220000
 0.0500000 0.0320000
 0.0750000 0.0395000
 0.1000000 0.0460000
 0.1500000 0.0560000
 0.2000000 0.0630000
 0.2500000 0.0680000
 0.3000000 0.0720000
 0.4000000 0.0770000
 0.5000000 0.0760000
 0.6000000 0.0730000
 0.7000000 0.0650000
 0.8000000 0.0520000
 0.9000000 0.0320000
 0.9500000 0.0180000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0060000
 0.0250000 -.0070000
 0.0500000 -.0060000
 0.0750000 -.0040000
 0.1000000 -.0020000
 0.1500000 0.0030000
 0.2000000 0.0080000
 0.2500000 0.0120000
 0.3000000 0.0160000
 0.4000000 0.0230000
 0.5000000 0.0280000
 0.6000000 0.0310000
 0.7000000 0.0300000
 0.8000000 0.0270000
 0.9000000 0.0190000
 0.9500000 0.0120000
 1.0000000 0.0000000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

E62 (5.62%)PreviewDetails
GOE 494 AIRFOILPreviewDetails
ARA-D 6% AIRFOILPreviewDetails
E71 (5.15%)PreviewDetails
GOE 484 AIRFOILPreviewDetails
GOE 123 AIRFOILPreviewDetails
davissmPreviewDetails
E61 (5.64%)PreviewDetails
E471 (6.25%)PreviewDetails
AH-7-47-6 AIRFOILPreviewDetails

Polars for EPPLER 59 AIRFOIL (e59-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e59-il50,000943.1 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e59-il50,000546.2 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e59-il100,000969.9 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e59-il100,000570.6 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   e59-il200,0009103.6 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e59-il200,000599.6 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e59-il500,0009155.6 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e59-il500,0005119.3 at α=0.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e59-il1,000,0009188.8 at α=0.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e59-il1,000,0005108.8 at α=-1°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit