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EPPLER E852 AIRFOIL (e852-il)

EPPLER E852 AIRFOIL - Eppler E852 propeller airfoil


Airfoil e852-il
Details Dat file Parser  
(e852-il) EPPLER E852 AIRFOIL
Eppler E852 propeller airfoil
Max thickness 10.1% at 37.2% chord.
Max camber 2.8% at 61.2% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER E852 AIRFOIL
      35.0      33.0

 0.0000000 0.0000000
 0.0000500 0.0008500
 0.0006000 0.0023300
 0.0020600 0.0045501
 0.0056501 0.0082302
 0.0125803 0.0131703
 0.0259205 0.0200004
 0.0438709 0.0269005
 0.0663213 0.0337007
 0.0930619 0.0403208
 0.1238025 0.0466209
 0.1582132 0.0525010
 0.1959339 0.0578312
 0.2365747 0.0625113
 0.2797056 0.0664513
 0.3248965 0.0695714
 0.3716574 0.0717914
 0.4194984 0.0730415
 0.4679393 0.0732315
 0.5164403 0.0722714
 0.5646413 0.0699614
 0.6122723 0.0663013
 0.6591032 0.0613712
 0.7049041 0.0554311
 0.7492850 0.0489310
 0.7916659 0.0422108
 0.8314466 0.0355407
 0.8680673 0.0291106
 0.9009680 0.0230705
 0.9296386 0.0175203
 0.9536191 0.0124402
 0.9727795 0.0077102
 0.9872597 0.0036701
 0.9966699 0.0011200
 1.0000000 0.0003100

 0.0000000 0.0000000
 0.0003000 -.0008100
 0.0012900 -.0021200
 0.0034101 -.0039501
 0.0081402 -.0067501
 0.0106302 -.0078902
 0.0239505 -.0123702
 0.0423108 -.0164903
 0.0655613 -.0201404
 0.0934819 -.0233505
 0.1257225 -.0261105
 0.1618632 -.0283706
 0.2014740 -.0300506
 0.2440749 -.0310606
 0.2891558 -.0312506
 0.3363467 -.0303906
 0.3853877 -.0283706
 0.4360387 -.0252005
 0.4881098 -.0211004
 0.5412208 -.0165403
 0.5946919 -.0119302
 0.6477929 -.0075502
 0.6997740 -.0036501
 0.7498550 -.0004000
 0.7972659 0.0020700
 0.8412368 0.0036901
 0.8810276 0.0044801
 0.9159783 0.0045101
 0.9454688 0.0039101
 0.9689894 0.0029101
 0.9860997 0.0017400
 0.9965099 0.0007300
 1.0000000 0.0003100
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER E852 AIRFOIL (e852-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e852-il50,000936.5 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e852-il50,000535.6 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   e852-il100,000958.6 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e852-il100,000557.3 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   e852-il200,000984.2 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e852-il200,000579.7 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   e852-il500,0009119.6 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e852-il500,000598.9 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   e852-il1,000,0009132.1 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   e852-il1,000,0005106.5 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
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