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GOE 423 AIRFOIL (goe423-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 423 AIRFOIL (goe423-il)
Reynolds number: 1,000,000
Max Cl/Cd: 133.36 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe423-il-1000000.txt
Download as CSV file: xf-goe423-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 423 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.8631   0.05704   0.05446  -0.1067   1.0000   0.0367
 -16.250  -0.9271   0.04641   0.04358  -0.1132   1.0000   0.0367
 -16.000  -0.9299   0.04081   0.03779  -0.1204   0.9972   0.0370
 -15.750  -0.9240   0.03697   0.03380  -0.1256   0.9946   0.0373
 -15.500  -0.9134   0.03420   0.03088  -0.1292   0.9921   0.0377
 -15.250  -0.9027   0.03218   0.02873  -0.1312   0.9870   0.0380
 -15.000  -0.8882   0.03059   0.02701  -0.1327   0.9824   0.0383
 -14.750  -0.8792   0.02938   0.02567  -0.1322   0.9743   0.0385
 -14.500  -0.8696   0.02849   0.02467  -0.1310   0.9665   0.0387
 -14.250  -0.8781   0.02621   0.02220  -0.1278   0.9561   0.0392
 -14.000  -0.8690   0.02539   0.02133  -0.1257   0.9484   0.0395
 -13.750  -0.8542   0.02484   0.02074  -0.1242   0.9412   0.0398
 -13.500  -0.8372   0.02432   0.02018  -0.1230   0.9347   0.0401
 -13.250  -0.8196   0.02379   0.01959  -0.1219   0.9274   0.0404
 -13.000  -0.8010   0.02334   0.01906  -0.1208   0.9207   0.0407
 -12.750  -0.7815   0.02285   0.01851  -0.1199   0.9125   0.0411
 -12.500  -0.7622   0.02231   0.01787  -0.1189   0.9050   0.0415
 -12.250  -0.7421   0.02169   0.01717  -0.1181   0.8966   0.0418
 -12.000  -0.7222   0.02107   0.01643  -0.1172   0.8879   0.0422
 -11.750  -0.7011   0.02047   0.01572  -0.1165   0.8785   0.0426
 -11.500  -0.6793   0.02001   0.01513  -0.1158   0.8693   0.0430
 -11.250  -0.6565   0.01962   0.01464  -0.1152   0.8594   0.0433
 -11.000  -0.6334   0.01928   0.01417  -0.1145   0.8498   0.0435
 -10.750  -0.6143   0.01803   0.01276  -0.1137   0.8391   0.0440
 -10.500  -0.5922   0.01726   0.01193  -0.1131   0.8288   0.0445
 -10.250  -0.5688   0.01682   0.01141  -0.1125   0.8173   0.0449
 -10.000  -0.5445   0.01645   0.01098  -0.1121   0.8048   0.0453
  -9.750  -0.5201   0.01614   0.01059  -0.1116   0.7911   0.0457
  -9.500  -0.4957   0.01589   0.01025  -0.1111   0.7740   0.0462
  -9.250  -0.4718   0.01563   0.00986  -0.1105   0.7500   0.0466
  -9.000  -0.4491   0.01539   0.00944  -0.1096   0.7135   0.0471
  -8.750  -0.4269   0.01522   0.00904  -0.1087   0.6736   0.0475
  -8.500  -0.4032   0.01499   0.00867  -0.1080   0.6511   0.0479
  -8.250  -0.3788   0.01476   0.00832  -0.1075   0.6370   0.0483
  -8.000  -0.3535   0.01454   0.00800  -0.1071   0.6272   0.0486
  -7.750  -0.3280   0.01435   0.00773  -0.1067   0.6192   0.0489
  -7.500  -0.3037   0.01382   0.00713  -0.1062   0.6132   0.0494
  -7.250  -0.2799   0.01332   0.00659  -0.1056   0.6073   0.0503
  -7.000  -0.2545   0.01308   0.00632  -0.1053   0.6018   0.0508
  -6.750  -0.2282   0.01284   0.00606  -0.1050   0.5980   0.0514
  -6.500  -0.2021   0.01262   0.00582  -0.1048   0.5939   0.0519
  -6.250  -0.1761   0.01243   0.00558  -0.1044   0.5898   0.0525
  -6.000  -0.1503   0.01226   0.00536  -0.1041   0.5854   0.0531
  -5.750  -0.1237   0.01207   0.00514  -0.1039   0.5823   0.0538
  -5.500  -0.0969   0.01188   0.00493  -0.1037   0.5796   0.0543
  -5.250  -0.0700   0.01173   0.00475  -0.1035   0.5764   0.0548
  -5.000  -0.0435   0.01157   0.00456  -0.1033   0.5732   0.0553
  -4.750  -0.0191   0.01121   0.00417  -0.1027   0.5701   0.0566
  -4.500   0.0068   0.01107   0.00400  -0.1024   0.5666   0.0575
  -4.250   0.0337   0.01093   0.00385  -0.1022   0.5643   0.0584
  -4.000   0.0608   0.01078   0.00371  -0.1021   0.5624   0.0593
  -3.750   0.0880   0.01066   0.00357  -0.1020   0.5603   0.0603
  -3.500   0.1153   0.01055   0.00345  -0.1018   0.5581   0.0611
  -3.250   0.1426   0.01047   0.00335  -0.1017   0.5558   0.0618
  -3.000   0.1686   0.01028   0.00314  -0.1014   0.5536   0.0636
  -2.750   0.1952   0.01018   0.00304  -0.1012   0.5512   0.0654
  -2.500   0.2221   0.01015   0.00298  -0.1010   0.5484   0.0672
  -2.250   0.2495   0.01009   0.00292  -0.1009   0.5465   0.0688
  -2.000   0.2769   0.00997   0.00281  -0.1009   0.5452   0.0712
  -1.750   0.3042   0.00986   0.00273  -0.1008   0.5435   0.0747
  -1.500   0.3317   0.00979   0.00267  -0.1007   0.5417   0.0786
  -1.250   0.3587   0.00967   0.00261  -0.1006   0.5399   0.0881
  -1.000   0.3852   0.00951   0.00258  -0.1004   0.5382   0.1210
  -0.750   0.4121   0.00941   0.00257  -0.1003   0.5364   0.1462
  -0.500   0.4392   0.00937   0.00257  -0.1002   0.5347   0.1626
  -0.250   0.4661   0.00933   0.00257  -0.1001   0.5327   0.1817
   0.000   0.4925   0.00924   0.00261  -0.1000   0.5305   0.2280
   0.250   0.5189   0.00910   0.00266  -0.0999   0.5289   0.2897
   0.500   0.5447   0.00886   0.00266  -0.0996   0.5279   0.3657
   0.750   0.5678   0.00842   0.00271  -0.0989   0.5268   0.5314
   1.000   0.5932   0.00825   0.00276  -0.0986   0.5255   0.6068
   1.250   0.6165   0.00797   0.00281  -0.0977   0.5241   0.7075
   1.500   0.6364   0.00763   0.00293  -0.0959   0.5226   0.8509
   1.750   0.6638   0.00759   0.00307  -0.0955   0.5212   0.9209
   2.000   0.7029   0.00772   0.00324  -0.0978   0.5198   0.9566
   2.250   0.7416   0.00788   0.00338  -0.1002   0.5184   0.9731
   2.500   0.7818   0.00804   0.00352  -0.1029   0.5169   0.9821
   2.750   0.8243   0.00820   0.00363  -0.1062   0.5148   0.9852
   3.000   0.8620   0.00836   0.00375  -0.1085   0.5113   0.9883
   3.250   0.8986   0.00838   0.00379  -0.1105   0.5083   0.9925
   3.500   0.9411   0.00840   0.00380  -0.1138   0.5042   0.9947
   3.750   0.9807   0.00845   0.00383  -0.1166   0.5006   0.9968
   4.000   1.0174   0.00858   0.00391  -0.1187   0.4957   0.9988
   4.250   1.0505   0.00863   0.00396  -0.1201   0.4924   1.0000
   4.500   1.0718   0.00865   0.00400  -0.1189   0.4896   1.0000
   4.750   1.0929   0.00868   0.00405  -0.1176   0.4868   1.0000
   5.000   1.1127   0.00874   0.00409  -0.1161   0.4827   1.0000
   5.250   1.1309   0.00887   0.00418  -0.1142   0.4779   1.0000
   5.500   1.1519   0.00889   0.00424  -0.1129   0.4746   1.0000
   5.750   1.1723   0.00893   0.00430  -0.1115   0.4702   1.0000
   6.000   1.1903   0.00902   0.00438  -0.1096   0.4647   1.0000
   6.250   1.2084   0.00912   0.00447  -0.1077   0.4583   1.0000
   6.500   1.2269   0.00920   0.00455  -0.1060   0.4506   1.0000
   6.750   1.2419   0.00934   0.00466  -0.1035   0.4424   1.0000
   7.000   1.2537   0.00948   0.00478  -0.1003   0.4304   1.0000
   7.250   1.2648   0.00974   0.00496  -0.0971   0.4101   1.0000
   7.500   1.2630   0.01057   0.00550  -0.0918   0.3576   1.0000
   7.750   1.2566   0.01185   0.00644  -0.0860   0.3016   1.0000
   8.000   1.2530   0.01313   0.00745  -0.0811   0.2534   1.0000
   8.250   1.2468   0.01463   0.00866  -0.0761   0.2035   1.0000
   8.500   1.2242   0.01706   0.01069  -0.0693   0.1312   1.0000
   8.750   1.2085   0.01944   0.01282  -0.0640   0.0818   1.0000
   9.000   1.2005   0.02161   0.01482  -0.0603   0.0480   1.0000
   9.250   1.2092   0.02285   0.01606  -0.0585   0.0431   1.0000
   9.500   1.2200   0.02399   0.01722  -0.0571   0.0410   1.0000
   9.750   1.2292   0.02529   0.01853  -0.0557   0.0391   1.0000
  10.000   1.2392   0.02658   0.01985  -0.0544   0.0379   1.0000
  10.250   1.2502   0.02782   0.02113  -0.0533   0.0371   1.0000
  10.500   1.2601   0.02919   0.02254  -0.0522   0.0363   1.0000
  10.750   1.2690   0.03070   0.02409  -0.0511   0.0356   1.0000
  11.000   1.2768   0.03235   0.02577  -0.0500   0.0349   1.0000
  11.250   1.2831   0.03419   0.02765  -0.0489   0.0343   1.0000
  11.500   1.2872   0.03627   0.02978  -0.0478   0.0336   1.0000
  11.750   1.2929   0.03827   0.03184  -0.0470   0.0332   1.0000
  12.000   1.3010   0.04007   0.03369  -0.0463   0.0329   1.0000
  12.250   1.3085   0.04195   0.03562  -0.0456   0.0325   1.0000
  12.500   1.3152   0.04393   0.03764  -0.0450   0.0320   1.0000
  12.750   1.3210   0.04600   0.03976  -0.0443   0.0316   1.0000
  13.000   1.3265   0.04811   0.04192  -0.0437   0.0313   1.0000
  13.250   1.3310   0.05034   0.04420  -0.0430   0.0309   1.0000
  13.500   1.3351   0.05262   0.04652  -0.0424   0.0306   1.0000
  13.750   1.3385   0.05496   0.04891  -0.0418   0.0303   1.0000
  14.000   1.3403   0.05752   0.05151  -0.0412   0.0299   1.0000
  14.250   1.3412   0.06016   0.05420  -0.0406   0.0296   1.0000
  14.500   1.3393   0.06317   0.05727  -0.0400   0.0293   1.0000
  14.750   1.3348   0.06643   0.06059  -0.0394   0.0289   1.0000
  15.000   1.3385   0.06887   0.06309  -0.0390   0.0287   1.0000
  15.250   1.3449   0.07101   0.06527  -0.0388   0.0285   1.0000
  15.500   1.3493   0.07341   0.06773  -0.0385   0.0283   1.0000
  15.750   1.3533   0.07586   0.07024  -0.0383   0.0280   1.0000
  16.000   1.3574   0.07828   0.07270  -0.0381   0.0278   1.0000
  16.250   1.3596   0.08095   0.07543  -0.0379   0.0275   1.0000
  16.500   1.3632   0.08347   0.07799  -0.0378   0.0273   1.0000
  16.750   1.3663   0.08606   0.08063  -0.0377   0.0270   1.0000
  17.000   1.3688   0.08876   0.08338  -0.0377   0.0267   1.0000
  17.250   1.3724   0.09130   0.08596  -0.0377   0.0265   1.0000
  17.500   1.3751   0.09396   0.08866  -0.0378   0.0262   1.0000
  17.750   1.3771   0.09672   0.09146  -0.0378   0.0259   1.0000
  18.000   1.3794   0.09941   0.09418  -0.0379   0.0256   1.0000
  18.250   1.3794   0.10240   0.09721  -0.0381   0.0254   1.0000
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