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GOE 679 AIRFOIL (goe679-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 679 AIRFOIL (goe679-il)
Reynolds number: 1,000,000
Max Cl/Cd: 88.83 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe679-il-1000000-n5.txt
Download as CSV file: xf-goe679-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 679 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.7687   0.08510   0.08160  -0.0936   0.9927   0.0267
 -17.500  -0.7780   0.08029   0.07673  -0.0964   0.9919   0.0268
 -17.250  -0.7877   0.07560   0.07197  -0.0990   0.9907   0.0268
 -17.000  -0.8042   0.07010   0.06639  -0.1025   0.9895   0.0268
 -16.750  -0.8225   0.06418   0.06038  -0.1064   0.9882   0.0269
 -16.500  -0.8474   0.05745   0.05354  -0.1110   0.9868   0.0269
 -16.250  -0.8714   0.05049   0.04645  -0.1161   0.9854   0.0269
 -16.000  -0.8907   0.04336   0.03916  -0.1222   0.9840   0.0269
 -15.750  -0.8992   0.03697   0.03261  -0.1289   0.9828   0.0269
 -15.500  -0.8986   0.03242   0.02791  -0.1341   0.9818   0.0270
 -15.250  -0.8960   0.02859   0.02395  -0.1387   0.9808   0.0272
 -15.000  -0.9088   0.02660   0.02187  -0.1362   0.9758   0.0272
 -14.750  -0.9033   0.02477   0.01996  -0.1364   0.9730   0.0274
 -14.500  -0.8907   0.02343   0.01855  -0.1367   0.9712   0.0276
 -14.250  -0.8737   0.02235   0.01743  -0.1369   0.9698   0.0279
 -14.000  -0.8532   0.02140   0.01642  -0.1374   0.9688   0.0280
 -13.750  -0.8559   0.02079   0.01576  -0.1328   0.9632   0.0281
 -13.500  -0.8422   0.02011   0.01503  -0.1312   0.9600   0.0283
 -13.250  -0.8237   0.01945   0.01433  -0.1303   0.9579   0.0285
 -13.000  -0.8029   0.01882   0.01366  -0.1297   0.9564   0.0286
 -12.750  -0.7792   0.01822   0.01302  -0.1295   0.9553   0.0289
 -12.500  -0.7795   0.01784   0.01261  -0.1243   0.9479   0.0290
 -12.250  -0.7588   0.01727   0.01199  -0.1234   0.9448   0.0292
 -12.000  -0.7329   0.01671   0.01140  -0.1234   0.9426   0.0294
 -11.750  -0.7041   0.01617   0.01082  -0.1239   0.9410   0.0296
 -11.500  -0.7004   0.01587   0.01048  -0.1192   0.9321   0.0298
 -11.250  -0.6743   0.01540   0.00998  -0.1191   0.9283   0.0300
 -11.000  -0.6407   0.01492   0.00945  -0.1204   0.9258   0.0303
 -10.750  -0.6261   0.01459   0.00909  -0.1178   0.9155   0.0304
 -10.500  -0.5864   0.01411   0.00856  -0.1203   0.9085   0.0306
 -10.250  -0.5382   0.01350   0.00788  -0.1247   0.8897   0.0312
 -10.000  -0.4707   0.01299   0.00720  -0.1332   0.8547   0.0318
  -9.750  -0.4451   0.01282   0.00685  -0.1328   0.8227   0.0322
  -9.250  -0.4076   0.01248   0.00634  -0.1290   0.7909   0.0329
  -9.000  -0.3885   0.01231   0.00611  -0.1271   0.7797   0.0334
  -8.750  -0.3690   0.01215   0.00588  -0.1254   0.7683   0.0337
  -8.500  -0.3491   0.01199   0.00567  -0.1236   0.7589   0.0342
  -8.250  -0.3283   0.01182   0.00545  -0.1221   0.7505   0.0347
  -7.750  -0.2878   0.01145   0.00501  -0.1188   0.7339   0.0363
  -7.500  -0.2676   0.01129   0.00481  -0.1170   0.7249   0.0372
  -7.250  -0.2465   0.01114   0.00462  -0.1155   0.7173   0.0381
  -7.000  -0.2249   0.01099   0.00444  -0.1141   0.7095   0.0391
  -6.750  -0.2051   0.01084   0.00425  -0.1122   0.7014   0.0406
  -6.500  -0.1833   0.01068   0.00408  -0.1108   0.6937   0.0426
  -6.250  -0.1646   0.01053   0.00390  -0.1088   0.6836   0.0453
  -6.000  -0.1448   0.01036   0.00372  -0.1069   0.6756   0.0490
  -5.750  -0.1253   0.01019   0.00355  -0.1050   0.6666   0.0542
  -5.500  -0.1067   0.01000   0.00336  -0.1030   0.6579   0.0627
  -5.250  -0.0875   0.00981   0.00319  -0.1010   0.6468   0.0733
  -5.000  -0.0685   0.00965   0.00305  -0.0990   0.6351   0.0846
  -4.750  -0.0496   0.00956   0.00293  -0.0970   0.6213   0.0934
  -4.500  -0.0294   0.00948   0.00284  -0.0952   0.6060   0.1015
  -4.250  -0.0091   0.00942   0.00275  -0.0935   0.5909   0.1079
  -4.000   0.0109   0.00941   0.00269  -0.0916   0.5739   0.1143
  -3.750   0.0308   0.00940   0.00263  -0.0898   0.5560   0.1198
  -3.500   0.0512   0.00944   0.00259  -0.0880   0.5390   0.1238
  -3.250   0.0713   0.00945   0.00256  -0.0863   0.5233   0.1289
  -3.000   0.0931   0.00945   0.00253  -0.0848   0.5101   0.1336
  -2.750   0.1147   0.00946   0.00251  -0.0833   0.4979   0.1392
  -2.250   0.1586   0.00949   0.00248  -0.0806   0.4758   0.1518
  -1.750   0.2035   0.00954   0.00248  -0.0779   0.4569   0.1624
  -1.500   0.2256   0.00957   0.00249  -0.0766   0.4481   0.1679
  -1.250   0.2485   0.00958   0.00250  -0.0754   0.4410   0.1734
  -0.750   0.2926   0.00967   0.00255  -0.0727   0.4238   0.1859
  -0.500   0.3152   0.00970   0.00257  -0.0714   0.4163   0.1928
  -0.250   0.3368   0.00976   0.00261  -0.0700   0.4086   0.1991
   0.000   0.3592   0.00979   0.00265  -0.0687   0.4030   0.2063
   0.250   0.3824   0.00982   0.00268  -0.0676   0.3980   0.2129
   0.500   0.4042   0.00986   0.00273  -0.0663   0.3920   0.2234
   1.000   0.4493   0.00995   0.00283  -0.0638   0.3820   0.2407
   1.500   0.4933   0.01006   0.00296  -0.0612   0.3713   0.2607
   1.750   0.5150   0.01013   0.00303  -0.0598   0.3659   0.2706
   2.000   0.5372   0.01017   0.00310  -0.0586   0.3617   0.2817
   2.250   0.5591   0.01023   0.00317  -0.0573   0.3569   0.2927
   2.500   0.5796   0.01033   0.00327  -0.0557   0.3508   0.3046
   2.750   0.6016   0.01038   0.00335  -0.0545   0.3468   0.3183
   3.000   0.6234   0.01044   0.00344  -0.0532   0.3412   0.3327
   3.250   0.6438   0.01051   0.00355  -0.0517   0.3358   0.3538
   3.500   0.6634   0.01060   0.00367  -0.0500   0.3308   0.3762
   3.750   0.6836   0.01062   0.00379  -0.0485   0.3260   0.4092
   4.000   0.7028   0.01065   0.00392  -0.0468   0.3207   0.4510
   4.250   0.7200   0.01071   0.00408  -0.0447   0.3139   0.5055
   4.500   0.7371   0.01061   0.00424  -0.0426   0.3097   0.5941
   4.750   0.7521   0.01055   0.00441  -0.0400   0.3042   0.6824
   5.000   0.7615   0.01039   0.00464  -0.0362   0.2988   0.8118
   5.500   0.9815   0.01114   0.00556  -0.0721   0.2748   0.9981
   5.750   1.0171   0.01145   0.00581  -0.0740   0.2671   1.0000
   6.000   1.0331   0.01169   0.00601  -0.0718   0.2603   1.0000
   6.250   1.0504   0.01193   0.00621  -0.0698   0.2539   1.0000
   6.500   1.0666   0.01223   0.00646  -0.0677   0.2465   1.0000
   6.750   1.0851   0.01245   0.00667  -0.0660   0.2426   1.0000
   7.000   1.1019   0.01276   0.00694  -0.0641   0.2358   1.0000
   7.250   1.1192   0.01307   0.00722  -0.0623   0.2306   1.0000
   7.500   1.1382   0.01334   0.00747  -0.0609   0.2264   1.0000
   7.750   1.1561   0.01365   0.00777  -0.0593   0.2219   1.0000
   8.000   1.1725   0.01404   0.00812  -0.0575   0.2165   1.0000
   8.250   1.1913   0.01434   0.00842  -0.0561   0.2132   1.0000
   8.500   1.2103   0.01465   0.00873  -0.0547   0.2104   1.0000
   8.750   1.2273   0.01505   0.00910  -0.0532   0.2060   1.0000
   9.000   1.2439   0.01548   0.00952  -0.0516   0.2020   1.0000
   9.250   1.2623   0.01585   0.00989  -0.0502   0.1994   1.0000
   9.500   1.2803   0.01623   0.01028  -0.0489   0.1970   1.0000
   9.750   1.2981   0.01664   0.01069  -0.0476   0.1945   1.0000
  10.000   1.3151   0.01710   0.01115  -0.0462   0.1915   1.0000
  10.250   1.3309   0.01763   0.01167  -0.0448   0.1887   1.0000
  10.500   1.3471   0.01815   0.01220  -0.0434   0.1858   1.0000
  10.750   1.3645   0.01863   0.01270  -0.0422   0.1837   1.0000
  11.000   1.3812   0.01915   0.01324  -0.0410   0.1817   1.0000
  11.250   1.3975   0.01971   0.01381  -0.0397   0.1795   1.0000
  11.500   1.4127   0.02034   0.01446  -0.0384   0.1773   1.0000
  11.750   1.4273   0.02103   0.01515  -0.0371   0.1748   1.0000
  12.000   1.4408   0.02180   0.01593  -0.0358   0.1721   1.0000
  12.250   1.4570   0.02243   0.01659  -0.0348   0.1706   1.0000
  12.500   1.4719   0.02315   0.01734  -0.0336   0.1686   1.0000
  12.750   1.4862   0.02392   0.01813  -0.0325   0.1663   1.0000
  13.000   1.4986   0.02484   0.01906  -0.0313   0.1635   1.0000
  13.250   1.5106   0.02581   0.02004  -0.0301   0.1609   1.0000
  13.500   1.5223   0.02682   0.02107  -0.0290   0.1586   1.0000
  13.750   1.5362   0.02770   0.02199  -0.0281   0.1571   1.0000
  14.000   1.5485   0.02870   0.02303  -0.0271   0.1552   1.0000
  14.250   1.5602   0.02976   0.02412  -0.0261   0.1530   1.0000
  14.500   1.5704   0.03096   0.02535  -0.0251   0.1510   1.0000
  14.750   1.5792   0.03229   0.02669  -0.0241   0.1485   1.0000
  15.000   1.5877   0.03368   0.02812  -0.0231   0.1464   1.0000
  15.250   1.5986   0.03488   0.02936  -0.0223   0.1448   1.0000
  15.500   1.6074   0.03628   0.03081  -0.0215   0.1427   1.0000
  15.750   1.6142   0.03786   0.03242  -0.0206   0.1394   1.0000
  16.000   1.6157   0.03995   0.03450  -0.0196   0.1349   1.0000
  16.250   1.6226   0.04161   0.03622  -0.0189   0.1325   1.0000
  16.500   1.6279   0.04343   0.03807  -0.0183   0.1291   1.0000
  16.750   1.6278   0.04579   0.04045  -0.0175   0.1252   1.0000
  17.000   1.6281   0.04817   0.04286  -0.0169   0.1208   1.0000
  17.250   1.6264   0.05080   0.04552  -0.0163   0.1161   1.0000
  17.500   1.6240   0.05357   0.04831  -0.0159   0.1123   1.0000
  17.750   1.6173   0.05682   0.05159  -0.0155   0.1063   1.0000
  18.000   1.6088   0.06035   0.05515  -0.0153   0.1013   1.0000
  18.250   1.5976   0.06427   0.05910  -0.0152   0.0962   1.0000
  18.500   1.5872   0.06817   0.06304  -0.0153   0.0922   1.0000
  18.750   1.5786   0.07193   0.06686  -0.0155   0.0896   1.0000
  19.000   1.5684   0.07595   0.07093  -0.0159   0.0873   1.0000
  19.250   1.5577   0.08010   0.07514  -0.0163   0.0849   1.0000
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