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EPPLER 715 AIRFOIL (e715-il)

EPPLER 715 AIRFOIL - Eppler E715 tailplane airfoil


Airfoil e715-il
Details Dat file Parser  
(e715-il) EPPLER 715 AIRFOIL
Eppler E715 tailplane airfoil
Max thickness 15% at 33.1% chord.
Max camber 2.8% at 42% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 715 AIRFOIL
       34.       34.

 0.0000100 0.0003100
 0.0002800 0.0026500
 0.0013600 0.0060700
 0.0043600 0.0116400
 0.0097900 0.0184500
 0.0213500 0.0288400
 0.0371000 0.0394200
 0.0569100 0.0498800
 0.0805900 0.0599400
 0.1079200 0.0693800
 0.1386300 0.0779700
 0.1724300 0.0855300
 0.2089800 0.0918800
 0.2479000 0.0968400
 0.2887800 0.1002200
 0.3311800 0.1017500
 0.3748300 0.1010800
 0.4196100 0.0979500
 0.4656200 0.0921600
 0.5132600 0.0840500
 0.5624200 0.0745800
 0.6124100 0.0645100
 0.6624600 0.0543700
 0.7117600 0.0445900
 0.7595000 0.0355000
 0.8048400 0.0273400
 0.8469900 0.0202800
 0.8851700 0.0143800
 0.9187000 0.0096500
 0.9469500 0.0059800
 0.9695200 0.0031900
 0.9861600 0.0012600
 0.9964800 0.0002600
 1.0000000 0.0000000

 0.0000100 0.0003100
 0.0001400 -.0011000
 0.0006100 -.0024500
 0.0018800 -.0045300
 0.0044000 -.0073900
 0.0097500 -.0117200
 0.0132700 -.0139800
 0.0278200 -.0210700
 0.0471100 -.0277200
 0.0709400 -.0337300
 0.0990600 -.0389500
 0.1312200 -.0432700
 0.1670900 -.0465800
 0.2063200 -.0488400
 0.2485200 -.0499400
 0.2932400 -.0498400
 0.3399800 -.0483300
 0.3885100 -.0451500
 0.4387300 -.0400800
 0.4912500 -.0333400
 0.5459900 -.0265600
 0.6013500 -.0207900
 0.6559200 -.0160200
 0.7087300 -.0121600
 0.7589600 -.0090900
 0.8058700 -.0067500
 0.8487500 -.0050200
 0.8870400 -.0037400
 0.9202500 -.0027800
 0.9479600 -.0019700
 0.9700000 -.0011400
 0.9863099 -.0004000
 0.9965000 -.0000500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 715 AIRFOIL (e715-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e715-il50,00095.7 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e715-il50,000515.7 at α=12.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e715-il100,000943.2 at α=10.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e715-il100,000544.3 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
   e715-il200,000974.6 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e715-il200,000574.9 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e715-il500,0009113.3 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   e715-il500,000598 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e715-il1,000,0009136.7 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e715-il1,000,0005111.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
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