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GOE 508 AIRFOIL (goe508-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 508 AIRFOIL (goe508-il)
Reynolds number: 1,000,000
Max Cl/Cd: 132.85 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe508-il-1000000.txt
Download as CSV file: xf-goe508-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 508 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
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.5962   0.04211   0.03930  -0.1352   0.9480   0.0286
 -14.000  -0.5780   0.03298   0.02969  -0.1552   0.9223   0.0288
 -13.750  -0.5806   0.03009   0.02645  -0.1577   0.8810   0.0289
 -13.500  -0.5911   0.02841   0.02454  -0.1553   0.8566   0.0289
 -13.250  -0.5970   0.02727   0.02321  -0.1523   0.8407   0.0290
 -12.750  -0.6047   0.02524   0.02088  -0.1449   0.8190   0.0291
 -12.500  -0.6039   0.02457   0.02006  -0.1411   0.8105   0.0292
 -12.250  -0.6062   0.02292   0.01823  -0.1377   0.8035   0.0294
 -12.000  -0.6006   0.02160   0.01678  -0.1350   0.7968   0.0296
 -11.750  -0.5879   0.02080   0.01588  -0.1330   0.7907   0.0298
 -11.500  -0.5717   0.02014   0.01516  -0.1315   0.7859   0.0300
 -11.250  -0.5540   0.01957   0.01454  -0.1301   0.7806   0.0303
 -11.000  -0.5356   0.01904   0.01393  -0.1287   0.7753   0.0305
 -10.750  -0.5164   0.01856   0.01336  -0.1274   0.7699   0.0307
 -10.500  -0.4962   0.01802   0.01277  -0.1263   0.7655   0.0310
 -10.250  -0.4756   0.01751   0.01220  -0.1252   0.7607   0.0312
 -10.000  -0.4547   0.01703   0.01163  -0.1240   0.7559   0.0315
  -9.750  -0.4329   0.01663   0.01113  -0.1230   0.7511   0.0318
  -9.500  -0.4109   0.01611   0.01057  -0.1221   0.7471   0.0321
  -9.250  -0.3877   0.01575   0.01014  -0.1213   0.7423   0.0325
  -9.000  -0.3648   0.01536   0.00965  -0.1204   0.7373   0.0328
  -8.750  -0.3410   0.01507   0.00928  -0.1196   0.7324   0.0330
  -8.500  -0.3166   0.01474   0.00890  -0.1189   0.7283   0.0332
  -8.250  -0.2965   0.01387   0.00797  -0.1177   0.7236   0.0337
  -8.000  -0.2734   0.01345   0.00751  -0.1168   0.7188   0.0342
  -7.750  -0.2493   0.01315   0.00715  -0.1161   0.7140   0.0346
  -7.500  -0.2240   0.01286   0.00686  -0.1155   0.7099   0.0350
  -7.250  -0.1989   0.01258   0.00655  -0.1149   0.7048   0.0355
  -7.000  -0.1741   0.01233   0.00624  -0.1142   0.6997   0.0360
  -6.750  -0.1488   0.01209   0.00596  -0.1136   0.6946   0.0365
  -6.500  -0.1230   0.01185   0.00568  -0.1131   0.6897   0.0370
  -6.250  -0.0972   0.01166   0.00544  -0.1126   0.6844   0.0374
  -6.000  -0.0735   0.01131   0.00502  -0.1117   0.6789   0.0381
  -5.750  -0.0482   0.01100   0.00472  -0.1112   0.6743   0.0388
  -5.500  -0.0221   0.01082   0.00453  -0.1107   0.6689   0.0397
  -5.250   0.0037   0.01069   0.00435  -0.1102   0.6632   0.0406
  -5.000   0.0299   0.01053   0.00417  -0.1097   0.6579   0.0415
  -4.750   0.0565   0.01040   0.00400  -0.1093   0.6520   0.0422
  -4.500   0.0809   0.01013   0.00369  -0.1085   0.6459   0.0434
  -4.250   0.1068   0.00997   0.00353  -0.1080   0.6403   0.0447
  -4.000   0.1333   0.00984   0.00339  -0.1076   0.6346   0.0460
  -3.750   0.1594   0.00976   0.00326  -0.1071   0.6286   0.0473
  -3.500   0.1848   0.00958   0.00306  -0.1065   0.6229   0.0492
  -3.250   0.2111   0.00945   0.00293  -0.1060   0.6167   0.0513
  -3.000   0.2368   0.00941   0.00283  -0.1055   0.6096   0.0532
  -2.750   0.2624   0.00924   0.00268  -0.1049   0.6030   0.0566
  -2.500   0.2885   0.00917   0.00258  -0.1044   0.5965   0.0596
  -2.250   0.3134   0.00908   0.00248  -0.1037   0.5905   0.0649
  -2.000   0.3398   0.00896   0.00241  -0.1033   0.5859   0.0740
  -1.750   0.3656   0.00887   0.00238  -0.1028   0.5804   0.0910
  -1.500   0.3910   0.00886   0.00237  -0.1022   0.5743   0.1028
  -1.250   0.4173   0.00880   0.00234  -0.1018   0.5689   0.1121
  -1.000   0.4437   0.00878   0.00232  -0.1014   0.5638   0.1192
  -0.750   0.4694   0.00876   0.00230  -0.1009   0.5592   0.1268
  -0.500   0.4948   0.00876   0.00230  -0.1003   0.5546   0.1348
  -0.250   0.5215   0.00871   0.00229  -0.1000   0.5506   0.1443
   0.000   0.5472   0.00867   0.00228  -0.0995   0.5460   0.1603
   0.250   0.5717   0.00861   0.00230  -0.0988   0.5415   0.1887
   0.500   0.5957   0.00854   0.00233  -0.0980   0.5371   0.2330
   0.750   0.6203   0.00836   0.00235  -0.0974   0.5337   0.2955
   1.000   0.6428   0.00813   0.00238  -0.0964   0.5293   0.3928
   1.250   0.6615   0.00779   0.00244  -0.0947   0.5251   0.5425
   1.500   0.6763   0.00747   0.00253  -0.0920   0.5203   0.6987
   1.750   0.6906   0.00706   0.00265  -0.0888   0.5169   0.8618
   2.000   0.7622   0.00715   0.00288  -0.0981   0.5107   0.9540
   2.250   0.8099   0.00733   0.00300  -0.1023   0.5056   0.9687
   2.500   0.8447   0.00749   0.00312  -0.1038   0.5015   0.9789
   2.750   0.8848   0.00758   0.00320  -0.1064   0.4976   0.9836
   3.000   0.9230   0.00771   0.00329  -0.1086   0.4930   0.9882
   3.250   0.9632   0.00789   0.00342  -0.1113   0.4880   0.9935
   3.750   1.0560   0.00811   0.00358  -0.1194   0.4779   1.0000
   4.000   1.0743   0.00820   0.00365  -0.1175   0.4729   1.0000
   4.250   1.0914   0.00833   0.00375  -0.1155   0.4678   1.0000
   4.500   1.1115   0.00839   0.00381  -0.1139   0.4629   1.0000
   4.750   1.1292   0.00850   0.00390  -0.1119   0.4564   1.0000
   5.000   1.1454   0.00865   0.00401  -0.1096   0.4493   1.0000
   5.250   1.1623   0.00878   0.00412  -0.1075   0.4400   1.0000
   5.500   1.1766   0.00896   0.00425  -0.1048   0.4294   1.0000
   5.750   1.1856   0.00918   0.00441  -0.1011   0.4161   1.0000
   6.000   1.1915   0.00942   0.00458  -0.0968   0.4010   1.0000
   6.250   1.1978   0.00975   0.00482  -0.0927   0.3812   1.0000
   6.500   1.2018   0.01024   0.00518  -0.0883   0.3560   1.0000
   6.750   1.2037   0.01091   0.00568  -0.0838   0.3268   1.0000
   7.000   1.2074   0.01162   0.00624  -0.0799   0.3020   1.0000
   7.250   1.2158   0.01224   0.00678  -0.0768   0.2845   1.0000
   7.500   1.2249   0.01290   0.00735  -0.0741   0.2697   1.0000
   7.750   1.2377   0.01346   0.00787  -0.0720   0.2598   1.0000
   8.000   1.2503   0.01407   0.00843  -0.0699   0.2509   1.0000
   8.250   1.2647   0.01463   0.00898  -0.0683   0.2451   1.0000
   8.500   1.2779   0.01529   0.00961  -0.0665   0.2394   1.0000
   8.750   1.2947   0.01581   0.01014  -0.0653   0.2362   1.0000
   9.000   1.3110   0.01636   0.01070  -0.0640   0.2330   1.0000
   9.250   1.3260   0.01701   0.01135  -0.0627   0.2295   1.0000
   9.500   1.3393   0.01778   0.01212  -0.0613   0.2257   1.0000
   9.750   1.3525   0.01858   0.01291  -0.0599   0.2223   1.0000
  10.000   1.3701   0.01915   0.01352  -0.0590   0.2207   1.0000
  10.250   1.3867   0.01978   0.01418  -0.0581   0.2188   1.0000
  10.500   1.4019   0.02052   0.01495  -0.0571   0.2166   1.0000
  10.750   1.4160   0.02135   0.01578  -0.0560   0.2141   1.0000
  11.000   1.4280   0.02231   0.01675  -0.0548   0.2110   1.0000
  11.250   1.4367   0.02352   0.01796  -0.0533   0.2069   1.0000
  11.500   1.4539   0.02419   0.01867  -0.0526   0.2057   1.0000
  11.750   1.4703   0.02491   0.01943  -0.0520   0.2027   1.0000
  12.000   1.4838   0.02585   0.02040  -0.0510   0.2004   1.0000
  12.250   1.4958   0.02690   0.02146  -0.0500   0.1976   1.0000
  12.500   1.5047   0.02820   0.02276  -0.0489   0.1940   1.0000
  12.750   1.5159   0.02936   0.02396  -0.0479   0.1913   1.0000
  13.000   1.5314   0.03022   0.02486  -0.0474   0.1887   1.0000
  13.250   1.5442   0.03127   0.02593  -0.0466   0.1852   1.0000
  13.500   1.5529   0.03268   0.02735  -0.0456   0.1811   1.0000
  13.750   1.5614   0.03412   0.02880  -0.0447   0.1771   1.0000
  14.000   1.5738   0.03528   0.03000  -0.0441   0.1731   1.0000
  14.250   1.5838   0.03663   0.03137  -0.0433   0.1689   1.0000
  14.500   1.5888   0.03844   0.03317  -0.0424   0.1635   1.0000
  14.750   1.5985   0.03984   0.03460  -0.0417   0.1585   1.0000
  15.000   1.6011   0.04191   0.03665  -0.0407   0.1513   1.0000
  15.250   1.6072   0.04369   0.03843  -0.0400   0.1454   1.0000
  15.500   1.6075   0.04603   0.04075  -0.0391   0.1380   1.0000
  15.750   1.6076   0.04840   0.04311  -0.0382   0.1303   1.0000
  16.000   1.6082   0.05076   0.04547  -0.0375   0.1239   1.0000
  16.250   1.6057   0.05349   0.04818  -0.0367   0.1170   1.0000
  16.500   1.6068   0.05589   0.05060  -0.0361   0.1117   1.0000
  16.750   1.6053   0.05855   0.05325  -0.0355   0.1059   1.0000
  17.000   1.6055   0.06112   0.05584  -0.0350   0.1003   1.0000
  17.250   1.6027   0.06400   0.05871  -0.0346   0.0938   1.0000
  17.500   1.5976   0.06718   0.06187  -0.0342   0.0850   1.0000
  17.750   1.5837   0.07135   0.06598  -0.0337   0.0719   1.0000
  18.000   1.5773   0.07477   0.06939  -0.0335   0.0662   1.0000
  18.250   1.5721   0.07815   0.07280  -0.0334   0.0629   1.0000
  18.500   1.5691   0.08129   0.07598  -0.0334   0.0604   1.0000
  18.750   1.5682   0.08421   0.07894  -0.0334   0.0590   1.0000
  19.000   1.5635   0.08763   0.08242  -0.0336   0.0571   1.0000
  19.250   1.5603   0.09090   0.08573  -0.0338   0.0556   1.0000
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