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E180 (8.59%) (e180-il)

E180 (8.59%) - Eppler E180 low Reynolds number airfoil


Airfoil e180-il
Details Dat file Parser  
(e180-il) E180 (8.59%)
Eppler E180 low Reynolds number airfoil
Max thickness 8.6% at 33.5% chord.
Max camber 2% at 38.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
E180  (8.59%)                
   1.00000  0.00000
   0.99677  0.00008
   0.98714  0.00042
   0.97128  0.00121
   0.94943  0.00267
   0.92203  0.00502
   0.88966  0.00832
   0.85292  0.01253
   0.81239  0.01755
   0.76872  0.02327
   0.72254  0.02952
   0.67454  0.03611
   0.62541  0.04278
   0.57584  0.04918
   0.52633  0.05484
   0.47723  0.05943
   0.42885  0.06273
   0.38147  0.06462
   0.33536  0.06502
   0.29074  0.06401
   0.24793  0.06182
   0.20741  0.05860
   0.16959  0.05448
   0.13487  0.04955
   0.10359  0.04391
   0.07605  0.03768
   0.05251  0.03099
   0.03315  0.02398
   0.01812  0.01684
   0.00746  0.00983
   0.00125  0.00344
   0.00033 -0.00163
   0.00512 -0.00596
   0.01526 -0.01015
   0.03053 -0.01380
   0.05084 -0.01680
   0.07609 -0.01912
   0.10608 -0.02079
   0.14054 -0.02185
   0.17912 -0.02235
   0.22144 -0.02235
   0.26703 -0.02194
   0.31539 -0.02118
   0.36597 -0.02014
   0.41819 -0.01889
   0.47144 -0.01750
   0.52510 -0.01600
   0.57854 -0.01446
   0.63113 -0.01289
   0.68225 -0.01135
   0.73130 -0.00985
   0.77769 -0.00842
   0.82088 -0.00707
   0.86035 -0.00582
   0.89563 -0.00465
   0.92628 -0.00358
   0.95192 -0.00256
   0.97234 -0.00153
   0.98741 -0.00064
   0.99679 -0.00013
   1.00000  0.00000
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Polars for E180 (8.59%) (e180-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e180-il50,000935.5 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   e180-il50,000536.2 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e180-il100,000952.7 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e180-il100,000551.8 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e180-il200,000971 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e180-il200,000566 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   e180-il500,000993.7 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e180-il500,000582.3 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e180-il1,000,0009109.3 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e180-il1,000,000591.7 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
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