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EPPLER 1200 AIRFOIL (e1200-il)

EPPLER 1200 AIRFOIL - Eppler E1200 general aviation airfoil


Airfoil e1200-il
Details Dat file Parser  
(e1200-il) EPPLER 1200 AIRFOIL
Eppler E1200 general aviation airfoil
Max thickness 16.9% at 36.1% chord.
Max camber 3.5% at 50.2% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 1200 AIRFOIL
      33.0      30.0
 
 0.0000000 0.0000000
 0.0013220 0.0072612
 0.0065853 0.0188100
 0.0159290 0.0310076
 0.0293227 0.0433341
 0.0467364 0.0553794
 0.0681101 0.0668236
 0.0933636 0.0774067
 0.1223668 0.0869288
 0.1549898 0.0952398
 0.1910125 0.1023098
 0.2301150 0.1081789
 0.2718071 0.1128172
 0.3156289 0.1161650
 0.3610904 0.1181422
 0.4076715 0.1186891
 0.4548522 0.1177158
 0.5021124 0.1150724
 0.5490720 0.1105291
 0.5955412 0.1039759
 0.6414397 0.0954028
 0.6868677 0.0851498
 0.7316154 0.0739870
 0.7750631 0.0625846
 0.8165308 0.0514027
 0.8553086 0.0408615
 0.8906666 0.0312414
 0.9219148 0.0227524
 0.9483633 0.0154048
 0.9696720 0.0090787
 0.9858308 0.0040441
 0.9963002 0.0009611
 1.0000000 -.0000000
 
 0.0000000 0.0000000
 0.0049522 -.0106754
 0.0049970 -.0107202
 0.0161252 -.0177734
 0.0327137 -.0243882
 0.0544324 -.0303845
 0.0810215 -.0356521
 0.1122009 -.0401309
 0.1476605 -.0438410
 0.1869905 -.0468221
 0.2296807 -.0490842
 0.2751912 -.0505970
 0.3229620 -.0513305
 0.3724030 -.0512144
 0.4229043 -.0501786
 0.4738359 -.0480129
 0.5248280 -.0443971
 0.5757204 -.0392414
 0.6264533 -.0325955
 0.6771064 -.0249296
 0.7273197 -.0172036
 0.7762026 -.0101872
 0.8227552 -.0043602
 0.8659472 -.0000723
 0.9047088 0.0025569
 0.9380398 0.0035375
 0.9649002 0.0030899
 0.9844002 0.0018044
 0.9961101 0.0005311
 1.0000000 -.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 1200 AIRFOIL (e1200-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e1200-il50,00099.3 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e1200-il50,000523.4 at α=10.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e1200-il100,000946.9 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e1200-il100,000539.5 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   e1200-il200,000969.5 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   e1200-il200,000568.2 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e1200-il500,0009107.4 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e1200-il500,000596.1 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e1200-il1,000,0009131.8 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e1200-il1,000,0005109.4 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
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