EPPLER 1098 AIRFOIL (e1098-il)
EPPLER 1098 AIRFOIL - Eppler E1098 general aviation airfoil
| Details | Dat file | Parser | |
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(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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Polars for EPPLER 1098 AIRFOIL (e1098-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e1098-il | 50,000 | 9 | 5.3 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e1098-il | 50,000 | 5 | 14.1 at α=13.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e1098-il | 100,000 | 9 | 29.8 at α=12.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e1098-il | 100,000 | 5 | 24.9 at α=11.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e1098-il | 200,000 | 9 | 51.9 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e1098-il | 200,000 | 5 | 63.7 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e1098-il | 500,000 | 9 | 117.3 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e1098-il | 500,000 | 5 | 112.5 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e1098-il | 1,000,000 | 9 | 151.8 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e1098-il | 1,000,000 | 5 | 139.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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