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E392 (10.15%) (e392-il)

E392 (10.15%) - Eppler E392 low Reynolds number airfoil


Airfoil e392-il
Details Dat file Parser  
(e392-il) E392 (10.15%)
Eppler E392 low Reynolds number airfoil
Max thickness 10.1% at 31.6% chord.
Max camber 3.7% at 45.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
E392  (10.15%)               
   1.00000  0.00000
   0.99676  0.00056
   0.98727  0.00233
   0.97208  0.00537
   0.95169  0.00949
   0.92641  0.01440
   0.89649  0.01996
   0.86230  0.02615
   0.82432  0.03289
   0.78311  0.04006
   0.73922  0.04751
   0.69325  0.05505
   0.64581  0.06247
   0.59751  0.06954
   0.54900  0.07592
   0.50073  0.08119
   0.45301  0.08506
   0.40613  0.08736
   0.36037  0.08800
   0.31598  0.08694
   0.27316  0.08429
   0.23222  0.08027
   0.19359  0.07509
   0.15765  0.06889
   0.12476  0.06181
   0.09525  0.05401
   0.06938  0.04565
   0.04738  0.03690
   0.02942  0.02799
   0.01564  0.01913
   0.00607  0.01068
   0.00080  0.00315
   0.00065 -0.00254
   0.00631 -0.00696
   0.01756 -0.01090
   0.03413 -0.01407
   0.05588 -0.01641
   0.08268 -0.01793
   0.11428 -0.01870
   0.15039 -0.01879
   0.19060 -0.01829
   0.23449 -0.01728
   0.28155 -0.01583
   0.33122 -0.01398
   0.38297 -0.01175
   0.43632 -0.00920
   0.49071 -0.00646
   0.54559 -0.00370
   0.60029 -0.00112
   0.65408  0.00113
   0.70625  0.00296
   0.75608  0.00432
   0.80289  0.00516
   0.84603  0.00549
   0.88489  0.00533
   0.91889  0.00474
   0.94753  0.00377
   0.97031  0.00254
   0.98677  0.00129
   0.99669  0.00035
   1.00000  0.00000
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Polars for E392 (10.15%) (e392-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e392-il50,000937.2 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   e392-il50,000537.6 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   e392-il100,000961.2 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   e392-il100,000561.8 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   e392-il200,000986.2 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   e392-il200,000584.6 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   e392-il500,0009120.6 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e392-il500,0005113.6 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e392-il1,000,0009146.6 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e392-il1,000,0005134 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
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