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E176 (8.83%) (e176-il)

E176 (8.83%) - Eppler E176 low Reynolds number airfoil


Airfoil e176-il
Details Dat file Parser  
(e176-il) E176 (8.83%)
Eppler E176 low Reynolds number airfoil
Max thickness 8.8% at 30.5% chord.
Max camber 2.9% at 44.2% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
 E176  (8.83%)                
   1.00000  0.00000
   0.99678  0.00031
   0.98727  0.00132
   0.97179  0.00320
   0.95073  0.00595
   0.92447  0.00956
   0.89342  0.01397
   0.85806  0.01914
   0.81892  0.02499
   0.77659  0.03141
   0.73165  0.03823
   0.68475  0.04528
   0.63652  0.05232
   0.58763  0.05911
   0.53871  0.06522
   0.49013  0.07021
   0.44218  0.07388
   0.39516  0.07604
   0.34934  0.07662
   0.30496  0.07560
   0.26220  0.07316
   0.22148  0.06954
   0.18324  0.06488
   0.14785  0.05932
   0.11568  0.05298
   0.08703  0.04598
   0.06216  0.03848
   0.04129  0.03065
   0.02457  0.02268
   0.01210  0.01480
   0.00391  0.00737
   0.00010  0.00105
   0.00179 -0.00384
   0.00934 -0.00782
   0.02220 -0.01113
   0.04033 -0.01367
   0.06361 -0.01540
   0.09190 -0.01637
   0.12494 -0.01666
   0.16243 -0.01635
   0.20396 -0.01556
   0.24910 -0.01438
   0.29731 -0.01292
   0.34805 -0.01127
   0.40072 -0.00954
   0.45470 -0.00779
   0.50931 -0.00612
   0.56391 -0.00455
   0.61782 -0.00315
   0.67039 -0.00194
   0.72097 -0.00095
   0.76894 -0.00019
   0.81371  0.00035
   0.85472  0.00067
   0.89145  0.00080
   0.92343  0.00077
   0.95024  0.00065
   0.97157  0.00050
   0.98718  0.00032
   0.99676  0.00011
   1.00000  0.00000
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Polars for E176 (8.83%) (e176-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e176-il50,000937.7 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e176-il50,000538.7 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e176-il100,000959.1 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e176-il100,000558.9 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e176-il200,000981.1 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e176-il200,000578.4 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e176-il500,0009110.7 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e176-il500,0005103.4 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e176-il1,000,0009132.9 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e176-il1,000,0005119.6 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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