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E230 (9.96%) (e230-il)

E230 (9.96%) - Eppler E230 airfoil


Airfoil e230-il
Details Dat file Parser  
(e230-il) E230 (9.96%)
Eppler E230 airfoil
Max thickness 10% at 29.3% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
E230  (9.96%)                
   1.00000  0.00000
   0.99657 -0.00018
   0.98632 -0.00059
   0.96935 -0.00078
   0.94605 -0.00028
   0.91713  0.00117
   0.88330  0.00351
   0.84515  0.00660
   0.80327  0.01032
   0.75825  0.01449
   0.71067  0.01896
   0.66113  0.02354
   0.61019  0.02806
   0.55840  0.03235
   0.50634  0.03627
   0.45455  0.03968
   0.40355  0.04245
   0.35387  0.04447
   0.30597  0.04566
   0.26032  0.04594
   0.21733  0.04528
   0.17740  0.04365
   0.14085  0.04106
   0.10801  0.03757
   0.07914  0.03323
   0.05449  0.02814
   0.03424  0.02241
   0.01853  0.01620
   0.00744  0.00975
   0.00107  0.00351
   0.00045 -0.00235
   0.00566 -0.00858
   0.01567 -0.01534
   0.03028 -0.02212
   0.04937 -0.02861
   0.07283 -0.03460
   0.10048 -0.03994
   0.13213 -0.04449
   0.16753 -0.04819
   0.20639 -0.05099
   0.24838 -0.05286
   0.29313 -0.05382
   0.34021 -0.05392
   0.38916 -0.05322
   0.43946 -0.05178
   0.49060 -0.04967
   0.54202 -0.04698
   0.59317 -0.04378
   0.64349 -0.04018
   0.69243 -0.03626
   0.73944 -0.03213
   0.78397 -0.02789
   0.82552 -0.02364
   0.86359 -0.01947
   0.89769 -0.01549
   0.92740 -0.01177
   0.95228 -0.00830
   0.97219 -0.00503
   0.98712 -0.00225
   0.99667 -0.00054
   1.00000  0.00000
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Selig format dat file

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Polars for E230 (9.96%) (e230-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e230-il50,000923 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e230-il50,000524.4 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e230-il100,000932.6 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   e230-il100,000532.2 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   e230-il200,000941.6 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   e230-il200,000538.7 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   e230-il500,000950.4 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e230-il500,000549.7 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e230-il1,000,000957.7 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e230-il1,000,000558 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
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