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EPPLER 793 AIRFOIL (e793-il)

EPPLER 793 AIRFOIL - Eppler E793 general purpose airfoil (gyroflug speed canard canard)


Airfoil e793-il
Details Dat file Parser  
(e793-il) EPPLER 793 AIRFOIL
Eppler E793 general purpose airfoil (gyroflug speed canard canard)
Max thickness 15.6% at 26.7% chord.
Max camber 4.2% at 44.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 793 AIRFOIL
       33.       29.

 0.0001200 -.0020000
 0.0017200 0.0080900
 0.0075500 0.0196000
 0.0174600 0.0318100
 0.0313400 0.0442500
 0.0491100 0.0565500
 0.0706200 0.0683600
 0.0956900 0.0794300
 0.1240900 0.0894700
 0.1555600 0.0981900
 0.1899300 0.1052400
 0.2270700 0.1104300
 0.2668200 0.1136700
 0.3089900 0.1149300
 0.3533200 0.1142800
 0.3995300 0.1118100
 0.4472700 0.1077500
 0.4960800 0.1023200
 0.5454600 0.0957300
 0.5949100 0.0881800
 0.6438900 0.0799200
 0.6918499 0.0711800
 0.7382200 0.0622100
 0.7824299 0.0532300
 0.8239000 0.0444700
 0.8620700 0.0361300
 0.8963700 0.0283500
 0.9263099 0.0212600
 0.9513600 0.0148600
 0.9713900 0.0090200
 0.9865700 0.0041100
 0.9964800 0.0010000
 1.0000000 0.0000000

 0.0001200 -.0020000
 0.0040800 -.0102500
 0.0141600 -.0174900
 0.0294900 -.0242900
 0.0496800 -.0303900
 0.0744500 -.0356100
 0.1035300 -.0398100
 0.1366100 -.0428100
 0.1734200 -.0444600
 0.2137200 -.0446300
 0.2572600 -.0432700
 0.3039000 -.0403800
 0.3534100 -.0362900
 0.4053200 -.0313000
 0.4591200 -.0257300
 0.5141900 -.0198900
 0.5698600 -.0140900
 0.6253900 -.0086500
 0.6800100 -.0038200
 0.7328700 0.0001700
 0.7831200 0.0031700
 0.8299100 0.0051100
 0.8724100 0.0059700
 0.9098400 0.0058600
 0.9414900 0.0049500
 0.9667500 0.0035100
 0.9851300 0.0019000
 0.9962700 0.0005500
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for EPPLER 793 AIRFOIL (e793-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e793-il50,00099.3 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e793-il50,000530.4 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   e793-il100,000943.3 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e793-il100,000552.4 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e793-il200,000969.7 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e793-il200,000572.6 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e793-il500,0009102.5 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   e793-il500,0005100.8 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e793-il1,000,0009129.2 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e793-il1,000,0005123 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
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