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CLARK Y AIRFOIL (clarky-il)

CLARK Y AIRFOIL - CLARK Y airfoil


Airfoil clarky-il
Details Dat file Parser  
(clarky-il) CLARK Y AIRFOIL
CLARK Y airfoil
Max thickness 11.7% at 28% chord.
Max camber 3.4% at 42% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 CLARK Y AIRFOIL
      61.0      61.0
 
 0.0000000 0.0000000
 0.0005000 0.0023390
 0.0010000 0.0037271
 0.0020000 0.0058025
 0.0040000 0.0089238
 0.0080000 0.0137350
 0.0120000 0.0178581
 0.0200000 0.0253735
 0.0300000 0.0330215
 0.0400000 0.0391283
 0.0500000 0.0442753
 0.0600000 0.0487571
 0.0800000 0.0564308
 0.1000000 0.0629981
 0.1200000 0.0686204
 0.1400000 0.0734360
 0.1600000 0.0775707
 0.1800000 0.0810687
 0.2000000 0.0839202
 0.2200000 0.0861433
 0.2400000 0.0878308
 0.2600000 0.0890840
 0.2800000 0.0900016
 0.3000000 0.0906804
 0.3200000 0.0911857
 0.3400000 0.0915079
 0.3600000 0.0916266
 0.3800000 0.0915212
 0.4000000 0.0911712
 0.4200000 0.0905657
 0.4400000 0.0897175
 0.4600000 0.0886427
 0.4800000 0.0873572
 0.5000000 0.0858772
 0.5200000 0.0842145
 0.5400000 0.0823712
 0.5600000 0.0803480
 0.5800000 0.0781451
 0.6000000 0.0757633
 0.6200000 0.0732055
 0.6400000 0.0704822
 0.6600000 0.0676046
 0.6800000 0.0645843
 0.7000000 0.0614329
 0.7200000 0.0581599
 0.7400000 0.0547675
 0.7600000 0.0512565
 0.7800000 0.0476281
 0.8000000 0.0438836
 0.8200000 0.0400245
 0.8400000 0.0360536
 0.8600000 0.0319740
 0.8800000 0.0277891
 0.9000000 0.0235025
 0.9200000 0.0191156
 0.9400000 0.0146239
 0.9600000 0.0100232
 0.9700000 0.0076868
 0.9800000 0.0053335
 0.9900000 0.0029690
 1.0000000 0.0005993
 
 0.0000000 0.0000000
 0.0005000 -.0046700
 0.0010000 -.0059418
 0.0020000 -.0078113
 0.0040000 -.0105126
 0.0080000 -.0142862
 0.0120000 -.0169733
 0.0200000 -.0202723
 0.0300000 -.0226056
 0.0400000 -.0245211
 0.0500000 -.0260452
 0.0600000 -.0271277
 0.0800000 -.0284595
 0.1000000 -.0293786
 0.1200000 -.0299633
 0.1400000 -.0302404
 0.1600000 -.0302546
 0.1800000 -.0300490
 0.2000000 -.0296656
 0.2200000 -.0291445
 0.2400000 -.0285181
 0.2600000 -.0278164
 0.2800000 -.0270696
 0.3000000 -.0263079
 0.3200000 -.0255565
 0.3400000 -.0248176
 0.3600000 -.0240870
 0.3800000 -.0233606
 0.4000000 -.0226341
 0.4200000 -.0219042
 0.4400000 -.0211708
 0.4600000 -.0204353
 0.4800000 -.0196986
 0.5000000 -.0189619
 0.5200000 -.0182262
 0.5400000 -.0174914
 0.5600000 -.0167572
 0.5800000 -.0160232
 0.6000000 -.0152893
 0.6200000 -.0145551
 0.6400000 -.0138207
 0.6600000 -.0130862
 0.6800000 -.0123515
 0.7000000 -.0116169
 0.7200000 -.0108823
 0.7400000 -.0101478
 0.7600000 -.0094133
 0.7800000 -.0086788
 0.8000000 -.0079443
 0.8200000 -.0072098
 0.8400000 -.0064753
 0.8600000 -.0057408
 0.8800000 -.0050063
 0.9000000 -.0042718
 0.9200000 -.0035373
 0.9400000 -.0028028
 0.9600000 -.0020683
 0.9700000 -.0017011
 0.9800000 -.0013339
 0.9900000 -.0009666
 1.0000000 -.0005993
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Lednicer format dat file
Selig format dat file

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Polars for CLARK Y AIRFOIL (clarky-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   clarky-il50,000929.6 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   clarky-il50,000536.5 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   clarky-il100,000953 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   clarky-il100,000554.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   clarky-il200,000973.2 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   clarky-il200,000569.7 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   clarky-il500,000998.7 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   clarky-il500,000590.9 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   clarky-il1,000,0009114.8 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   clarky-il1,000,0005108.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
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