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EPPLER 1210 AIRFOIL (e1210-il)

EPPLER 1210 AIRFOIL - Eppler E1210 general aviation airfoil


Airfoil e1210-il
Details Dat file Parser  
(e1210-il) EPPLER 1210 AIRFOIL
Eppler E1210 general aviation airfoil
Max thickness 15.9% at 21.1% chord.
Max camber 5.2% at 33.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 1210 AIRFOIL
      33.0      29.0
 
 0.0000000 0.0000000
 0.0019187 0.0120735
 0.0075094 0.0260532
 0.0167402 0.0405828
 0.0296010 0.0551821
 0.0459818 0.0694713
 0.0657626 0.0830502
 0.0887533 0.0955690
 0.1147539 0.1065476
 0.1437745 0.1155061
 0.1759049 0.1222544
 0.2110452 0.1267325
 0.2491054 0.1288605
 0.2899455 0.1287383
 0.3333054 0.1265160
 0.3788753 0.1223235
 0.4263151 0.1163710
 0.4752148 0.1089283
 0.5251344 0.1002656
 0.5755740 0.0907229
 0.6259636 0.0806202
 0.6756831 0.0703075
 0.7240927 0.0600849
 0.7705122 0.0502424
 0.8142418 0.0410200
 0.8545914 0.0325879
 0.8909011 0.0250659
 0.9225708 0.0184942
 0.9490406 0.0127528
 0.9701403 0.0076216
 0.9860602 0.0033908
 0.9963701 0.0007902
 1.0000000 -.0000000
 
 0.0000000 0.0000000
 0.0024474 -.0110466
 0.0102570 -.0194770
 0.0232366 -.0268977
 0.0408363 -.0326487
 0.0631962 -.0363399
 0.0905362 -.0377614
 0.1232563 -.0371431
 0.1612764 -.0351551
 0.2040367 -.0322874
 0.2509370 -.0288099
 0.3013373 -.0249726
 0.3545476 -.0209555
 0.4098679 -.0169584
 0.4665383 -.0130914
 0.5238185 -.0095045
 0.5809288 -.0062876
 0.6370991 -.0035006
 0.6915894 -.0012235
 0.7436395 0.0005237
 0.7925397 0.0017411
 0.8376198 0.0024487
 0.8782199 0.0026765
 0.9137599 0.0025146
 0.9437100 0.0020730
 0.9676700 0.0015317
 0.9853400 0.0009208
 0.9962800 0.0003002
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 1210 AIRFOIL (e1210-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e1210-il50,00098.9 at α=0°Mach=0 Ncrit=9Xfoil predictionDetails
   e1210-il50,000525.8 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   e1210-il100,000935.3 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e1210-il100,000545.9 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e1210-il200,000960.3 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e1210-il200,000565.1 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e1210-il500,000992.2 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   e1210-il500,000593.2 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e1210-il1,000,0009119.5 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e1210-il1,000,0005117.1 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
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