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E224 (10.17%) (e224-il)

E224 (10.17%) - Eppler E224 low Reynolds number airfoil


Airfoil e224-il
Details Dat file Parser  
(e224-il) E224 (10.17%)
Eppler E224 low Reynolds number airfoil
Max thickness 10.2% at 29.8% chord.
Max camber 1.5% at 54.2% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
E224  (10.17%)               
   1.00000  0.00000
   0.99664  0.00048
   0.98692  0.00205
   0.97152  0.00472
   0.95089  0.00820
   0.92524  0.01226
   0.89489  0.01692
   0.86033  0.02207
   0.82203  0.02756
   0.78048  0.03324
   0.73619  0.03894
   0.68967  0.04450
   0.64143  0.04975
   0.59200  0.05452
   0.54189  0.05869
   0.49160  0.06210
   0.44164  0.06467
   0.39248  0.06628
   0.34460  0.06689
   0.29844  0.06643
   0.25442  0.06489
   0.21293  0.06227
   0.17434  0.05861
   0.13898  0.05396
   0.10714  0.04841
   0.07909  0.04207
   0.05503  0.03508
   0.03517  0.02761
   0.01961  0.01986
   0.00845  0.01212
   0.00179  0.00477
   0.00014 -0.00124
   0.00430 -0.00657
   0.01402 -0.01224
   0.02867 -0.01766
   0.04808 -0.02260
   0.07209 -0.02687
   0.10055 -0.03039
   0.13322 -0.03307
   0.16984 -0.03488
   0.21008 -0.03584
   0.25358 -0.03595
   0.29995 -0.03528
   0.34871 -0.03389
   0.39939 -0.03187
   0.45145 -0.02933
   0.50434 -0.02637
   0.55747 -0.02312
   0.61024 -0.01970
   0.66205 -0.01622
   0.71229 -0.01282
   0.76035 -0.00962
   0.80562 -0.00671
   0.84750 -0.00422
   0.88541 -0.00221
   0.91879 -0.00075
   0.94708  0.00012
   0.96977  0.00047
   0.98639  0.00041
   0.99657  0.00015
   1.00000  0.00000
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Polars for E224 (10.17%) (e224-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e224-il50,000933.7 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e224-il50,000535.8 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   e224-il100,000951.2 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e224-il100,000550.2 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e224-il200,000968.2 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   e224-il200,000563.4 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e224-il500,000989.2 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e224-il500,000579.1 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   e224-il1,000,0009102.9 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e224-il1,000,000588.9 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
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