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EPPLER 1098 AIRFOIL (e1098-il)

EPPLER 1098 AIRFOIL - Eppler E1098 general aviation airfoil


Airfoil e1098-il
Details Dat file Parser  
(e1098-il) EPPLER 1098 AIRFOIL
Eppler E1098 general aviation airfoil
Max thickness 18.9% at 36.6% chord.
Max camber 3.7% at 54.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 EPPLER 1098 AIRFOIL
       33.       30.

 0.0000000 0.0000000
 0.0012734 0.0052896
 0.0071987 0.0158536
 0.0175285 0.0275484
 0.0320334 0.0397469
 0.0506445 0.0519772
 0.0732793 0.0639683
 0.0997127 0.0755306
 0.1296339 0.0864041
 0.1627977 0.0963134
 0.1989595 0.1051007
 0.2377671 0.1126733
 0.2787850 0.1189112
 0.3215674 0.1236708
 0.3656456 0.1268185
 0.4105355 0.1281930
 0.4557306 0.1276271
 0.5006816 0.1247186
 0.5454305 0.1187841
 0.5907146 0.1099341
 0.6366766 0.0992039
 0.6827371 0.0874585
 0.7282305 0.0752860
 0.7724453 0.0632013
 0.8146316 0.0516205
 0.8540272 0.0408789
 0.8898773 0.0312064
 0.9214655 0.0227460
 0.9481131 0.0154594
 0.9695235 0.0091452
 0.9857414 0.0040740
 0.9962760 0.0009688
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0004746 -.0029776
 0.0062814 -.0098859
 0.0186816 -.0170816
 0.0364505 -.0243112
 0.0591566 -.0313477
 0.0864272 -.0380246
 0.1178772 -.0441931
 0.1531004 -.0497124
 0.1916554 -.0544503
 0.2330732 -.0582662
 0.2768521 -.0610211
 0.3224651 -.0625371
 0.3693560 -.0626158
 0.4169266 -.0607879
 0.4652361 -.0562835
 0.5150946 -.0492199
 0.5666348 -.0407374
 0.6191724 -.0317886
 0.6718973 -.0230272
 0.7239064 -.0150103
 0.7742203 -.0081683
 0.8218132 -.0028015
 0.8656485 0.0009319
 0.9047171 0.0030316
 0.9380802 0.0036352
 0.9648611 0.0030397
 0.9843320 0.0017727
 0.9960827 0.0005276
 1.0000000 -.0000000
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Lednicer format dat file
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Polars for EPPLER 1098 AIRFOIL (e1098-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e1098-il50,00095.3 at α=11.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e1098-il50,000514.1 at α=13.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e1098-il100,000929.8 at α=12.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e1098-il100,000524.9 at α=11.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e1098-il200,000951.9 at α=10.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e1098-il200,000563.7 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   e1098-il500,0009117.3 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e1098-il500,0005112.5 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   e1098-il1,000,0009151.8 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e1098-il1,000,0005139.8 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
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