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GOE 535 AIRFOIL (goe535-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 535 AIRFOIL (goe535-il)
Reynolds number: 500,000
Max Cl/Cd: 90.87 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe535-il-500000-n5.txt
Download as CSV file: xf-goe535-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 535 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.6753   0.07482   0.07129  -0.0770   1.0000   0.0326
 -14.750  -0.7304   0.06404   0.06031  -0.0834   1.0000   0.0326
 -14.500  -0.7636   0.05739   0.05353  -0.0866   1.0000   0.0327
 -14.250  -0.7931   0.05226   0.04831  -0.0883   1.0000   0.0327
 -14.000  -0.7947   0.04673   0.04265  -0.0953   0.9971   0.0329
 -13.750  -0.7911   0.04209   0.03790  -0.1017   0.9920   0.0332
 -13.500  -0.7886   0.03806   0.03376  -0.1069   0.9853   0.0334
 -13.250  -0.7763   0.03430   0.02987  -0.1133   0.9797   0.0338
 -13.000  -0.7635   0.03105   0.02650  -0.1182   0.9713   0.0340
 -12.750  -0.7372   0.02813   0.02345  -0.1244   0.9673   0.0344
 -12.500  -0.7124   0.02576   0.02093  -0.1290   0.9616   0.0347
 -12.250  -0.6837   0.02369   0.01876  -0.1334   0.9561   0.0351
 -12.000  -0.6501   0.02219   0.01719  -0.1372   0.9527   0.0355
 -11.750  -0.6195   0.02109   0.01604  -0.1395   0.9481   0.0360
 -11.500  -0.5923   0.02019   0.01507  -0.1406   0.9408   0.0364
 -11.250  -0.5575   0.01930   0.01411  -0.1430   0.9351   0.0370
 -11.000  -0.5288   0.01855   0.01328  -0.1439   0.9240   0.0375
 -10.750  -0.4959   0.01782   0.01245  -0.1454   0.9119   0.0382
 -10.500  -0.4653   0.01719   0.01169  -0.1464   0.8982   0.0388
 -10.250  -0.4383   0.01659   0.01103  -0.1467   0.8838   0.0393
 -10.000  -0.4108   0.01609   0.01046  -0.1469   0.8687   0.0400
  -9.750  -0.3838   0.01566   0.00993  -0.1468   0.8517   0.0408
  -9.500  -0.3577   0.01529   0.00945  -0.1466   0.8326   0.0416
  -9.250  -0.3321   0.01496   0.00898  -0.1461   0.8132   0.0426
  -9.000  -0.3069   0.01465   0.00855  -0.1456   0.7946   0.0435
  -8.750  -0.2820   0.01437   0.00818  -0.1450   0.7761   0.0445
  -8.500  -0.2567   0.01413   0.00785  -0.1443   0.7580   0.0456
  -8.250  -0.2313   0.01391   0.00751  -0.1437   0.7414   0.0468
  -8.000  -0.2058   0.01369   0.00717  -0.1431   0.7268   0.0480
  -7.750  -0.1802   0.01348   0.00691  -0.1425   0.7135   0.0492
  -7.500  -0.1539   0.01330   0.00667  -0.1420   0.7011   0.0506
  -7.250  -0.1279   0.01315   0.00641  -0.1414   0.6886   0.0521
  -7.000  -0.1016   0.01297   0.00616  -0.1409   0.6759   0.0535
  -6.750  -0.0752   0.01284   0.00598  -0.1404   0.6645   0.0550
  -6.500  -0.0485   0.01272   0.00580  -0.1399   0.6534   0.0567
  -6.250  -0.0218   0.01261   0.00559  -0.1394   0.6435   0.0584
  -6.000   0.0049   0.01247   0.00542  -0.1389   0.6325   0.0599
  -5.750   0.0316   0.01238   0.00527  -0.1384   0.6220   0.0615
  -5.500   0.0584   0.01228   0.00510  -0.1379   0.6104   0.0631
  -5.250   0.0852   0.01220   0.00492  -0.1374   0.6002   0.0646
  -5.000   0.1119   0.01206   0.00476  -0.1369   0.5898   0.0661
  -4.750   0.1387   0.01199   0.00464  -0.1364   0.5801   0.0677
  -4.500   0.1656   0.01192   0.00451  -0.1359   0.5689   0.0695
  -4.250   0.1923   0.01188   0.00438  -0.1354   0.5582   0.0711
  -4.000   0.2188   0.01176   0.00423  -0.1349   0.5466   0.0727
  -3.750   0.2455   0.01169   0.00412  -0.1344   0.5365   0.0745
  -3.500   0.2722   0.01165   0.00402  -0.1339   0.5260   0.0765
  -3.250   0.2991   0.01163   0.00393  -0.1333   0.5160   0.0783
  -3.000   0.3254   0.01155   0.00380  -0.1328   0.5051   0.0801
  -2.750   0.3520   0.01148   0.00370  -0.1323   0.4956   0.0819
  -2.500   0.3786   0.01145   0.00362  -0.1317   0.4863   0.0839
  -2.250   0.4053   0.01144   0.00355  -0.1312   0.4786   0.0857
  -2.000   0.4322   0.01141   0.00348  -0.1307   0.4704   0.0874
  -1.500   0.4854   0.01135   0.00336  -0.1297   0.4556   0.0927
  -1.250   0.5122   0.01135   0.00332  -0.1292   0.4491   0.0952
  -1.000   0.5385   0.01136   0.00330  -0.1286   0.4427   0.0988
  -0.750   0.5654   0.01134   0.00328  -0.1282   0.4372   0.1041
  -0.500   0.5922   0.01131   0.00326  -0.1277   0.4314   0.1122
  -0.250   0.6184   0.01128   0.00326  -0.1272   0.4260   0.1296
   0.000   0.6440   0.01117   0.00326  -0.1266   0.4210   0.1793
   0.250   0.6704   0.01099   0.00325  -0.1262   0.4167   0.2389
   0.500   0.6963   0.01085   0.00334  -0.1257   0.4116   0.3207
   0.750   0.7225   0.01091   0.00344  -0.1251   0.4071   0.3509
   1.000   0.7483   0.01102   0.00354  -0.1245   0.4022   0.3703
   1.250   0.7751   0.01110   0.00363  -0.1240   0.3983   0.3859
   1.500   0.8016   0.01117   0.00374  -0.1235   0.3940   0.3992
   1.750   0.8278   0.01128   0.00383  -0.1229   0.3892   0.4092
   2.000   0.8530   0.01141   0.00394  -0.1221   0.3838   0.4186
   2.250   0.8790   0.01152   0.00405  -0.1215   0.3788   0.4272
   2.500   0.9049   0.01161   0.00415  -0.1209   0.3731   0.4356
   2.750   0.9301   0.01174   0.00428  -0.1201   0.3679   0.4436
   3.000   0.9547   0.01190   0.00440  -0.1193   0.3632   0.4508
   3.250   0.9806   0.01200   0.00451  -0.1187   0.3593   0.4567
   3.500   1.0060   0.01210   0.00465  -0.1180   0.3553   0.4630
   3.750   1.0308   0.01224   0.00479  -0.1173   0.3509   0.4698
   4.000   1.0548   0.01241   0.00492  -0.1164   0.3465   0.4753
   4.250   1.0791   0.01254   0.00507  -0.1155   0.3423   0.4801
   4.500   1.1038   0.01266   0.00522  -0.1147   0.3378   0.4851
   4.750   1.1275   0.01282   0.00538  -0.1138   0.3329   0.4904
   5.000   1.1501   0.01301   0.00554  -0.1127   0.3283   0.4957
   5.250   1.1732   0.01317   0.00572  -0.1117   0.3242   0.5007
   5.500   1.1959   0.01331   0.00589  -0.1106   0.3199   0.5064
   5.750   1.2171   0.01347   0.00607  -0.1092   0.3151   0.5126
   6.000   1.2368   0.01369   0.00627  -0.1076   0.3103   0.5185
   6.250   1.2579   0.01387   0.00648  -0.1062   0.3058   0.5244
   6.500   1.2786   0.01407   0.00671  -0.1048   0.3004   0.5316
   6.750   1.2979   0.01433   0.00696  -0.1032   0.2950   0.5386
   7.000   1.3170   0.01459   0.00723  -0.1016   0.2899   0.5451
   7.250   1.3371   0.01482   0.00749  -0.1001   0.2845   0.5521
   7.500   1.3547   0.01515   0.00780  -0.0983   0.2778   0.5588
   7.750   1.3728   0.01545   0.00812  -0.0966   0.2717   0.5653
   8.000   1.3908   0.01577   0.00845  -0.0950   0.2650   0.5726
   8.500   1.4246   0.01649   0.00920  -0.0914   0.2535   0.5873
   8.750   1.4403   0.01691   0.00962  -0.0895   0.2468   0.5958
   9.000   1.4550   0.01736   0.01009  -0.0876   0.2405   0.6050
   9.250   1.4707   0.01778   0.01055  -0.0858   0.2342   0.6166
   9.500   1.4840   0.01831   0.01111  -0.0837   0.2286   0.6318
   9.750   1.4991   0.01875   0.01165  -0.0820   0.2237   0.6583
  11.250   1.6263   0.02297   0.01635  -0.0818   0.1916   1.0000
  11.500   1.6382   0.02392   0.01731  -0.0803   0.1875   1.0000
  11.750   1.6476   0.02507   0.01846  -0.0788   0.1835   1.0000
  12.000   1.6601   0.02606   0.01950  -0.0776   0.1802   1.0000
  12.250   1.6711   0.02719   0.02066  -0.0763   0.1761   1.0000
  12.500   1.6791   0.02858   0.02207  -0.0750   0.1721   1.0000
  12.750   1.6865   0.03007   0.02358  -0.0738   0.1684   1.0000
  13.000   1.6963   0.03142   0.02499  -0.0728   0.1651   1.0000
  13.250   1.7038   0.03300   0.02660  -0.0718   0.1615   1.0000
  13.500   1.7089   0.03484   0.02848  -0.0709   0.1584   1.0000
  13.750   1.7136   0.03677   0.03045  -0.0700   0.1556   1.0000
  14.000   1.7213   0.03847   0.03221  -0.0693   0.1528   1.0000
  14.250   1.7261   0.04047   0.03427  -0.0686   0.1496   1.0000
  14.500   1.7277   0.04285   0.03670  -0.0679   0.1462   1.0000
  14.750   1.7278   0.04544   0.03933  -0.0673   0.1431   1.0000
  15.000   1.7317   0.04766   0.04162  -0.0669   0.1397   1.0000
  15.250   1.7313   0.05038   0.04440  -0.0664   0.1357   1.0000
  15.500   1.7263   0.05367   0.04774  -0.0661   0.1320   1.0000
  15.750   1.7258   0.05653   0.05067  -0.0659   0.1278   1.0000
  16.000   1.7185   0.06019   0.05436  -0.0658   0.1225   1.0000
  16.250   1.7114   0.06392   0.05814  -0.0658   0.1171   1.0000
  16.500   1.6985   0.06845   0.06270  -0.0661   0.1107   1.0000
  16.750   1.6860   0.07296   0.06726  -0.0664   0.1037   1.0000
  17.000   1.6692   0.07813   0.07245  -0.0670   0.0970   1.0000
  17.250   1.6514   0.08352   0.07788  -0.0677   0.0910   1.0000
  17.500   1.6345   0.08887   0.08327  -0.0686   0.0858   1.0000
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