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GOE 16K AIRFOIL (goe16k-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 16K AIRFOIL (goe16k-il)
Reynolds number: 1,000,000
Max Cl/Cd: 80.17 at α=3.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe16k-il-1000000.txt
Download as CSV file: xf-goe16k-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 16K 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.7470   0.07578   0.07252  -0.1670   0.9560   0.0246
 -19.500  -0.7731   0.06890   0.06550  -0.1713   0.9557   0.0245
 -19.250  -0.7902   0.06312   0.05960  -0.1752   0.9553   0.0246
 -19.000  -0.8113   0.06001   0.05641  -0.1728   0.9499   0.0251
 -18.750  -0.8385   0.05357   0.04983  -0.1762   0.9482   0.0250
 -18.500  -0.8378   0.04998   0.04614  -0.1788   0.9472   0.0254
 -18.250  -0.8530   0.04454   0.04057  -0.1825   0.9462   0.0261
 -18.000  -0.8509   0.04129   0.03725  -0.1850   0.9455   0.0267
 -17.750  -0.8490   0.03827   0.03413  -0.1870   0.9449   0.0269
 -17.500  -0.8381   0.03626   0.03205  -0.1886   0.9444   0.0281
 -17.250  -0.8285   0.03430   0.03001  -0.1899   0.9439   0.0284
 -17.000  -0.8470   0.03252   0.02814  -0.1852   0.9375   0.0285
 -16.750  -0.8365   0.03120   0.02673  -0.1850   0.9358   0.0290
 -16.500  -0.8325   0.02939   0.02483  -0.1844   0.9346   0.0292
 -16.250  -0.8218   0.02806   0.02344  -0.1842   0.9336   0.0301
 -16.000  -0.8082   0.02691   0.02228  -0.1840   0.9329   0.0311
 -15.750  -0.7889   0.02615   0.02147  -0.1843   0.9323   0.0319
 -15.500  -0.7683   0.02545   0.02073  -0.1846   0.9317   0.0326
 -15.250  -0.7739   0.02471   0.01992  -0.1798   0.9258   0.0330
 -15.000  -0.7590   0.02404   0.01917  -0.1787   0.9236   0.0336
 -14.750  -0.7447   0.02318   0.01824  -0.1779   0.9220   0.0343
 -14.500  -0.7312   0.02224   0.01727  -0.1769   0.9207   0.0351
 -14.250  -0.7106   0.02150   0.01649  -0.1770   0.9198   0.0358
 -14.000  -0.6851   0.02097   0.01592  -0.1778   0.9189   0.0366
 -13.750  -0.6611   0.02027   0.01516  -0.1785   0.9180   0.0372
 -13.500  -0.6520   0.02030   0.01516  -0.1752   0.9117   0.0382
 -13.250  -0.6303   0.01986   0.01465  -0.1749   0.9093   0.0388
 -13.000  -0.6071   0.01921   0.01390  -0.1752   0.9076   0.0392
 -12.750  -0.5861   0.01831   0.01294  -0.1755   0.9060   0.0400
 -12.500  -0.5555   0.01781   0.01243  -0.1772   0.9048   0.0411
 -12.250  -0.5369   0.01766   0.01226  -0.1760   0.9010   0.0421
 -12.000  -0.5245   0.01738   0.01193  -0.1735   0.8965   0.0427
 -11.750  -0.4982   0.01699   0.01148  -0.1742   0.8944   0.0436
 -11.500  -0.4697   0.01656   0.01098  -0.1752   0.8924   0.0442
 -11.250  -0.4363   0.01637   0.01072  -0.1771   0.8907   0.0448
 -11.000  -0.4155   0.01585   0.01014  -0.1766   0.8881   0.0453
 -10.750  -0.4177   0.01546   0.00973  -0.1710   0.8831   0.0466
 -10.500  -0.3991   0.01515   0.00939  -0.1697   0.8802   0.0474
 -10.250  -0.3742   0.01483   0.00904  -0.1699   0.8781   0.0482
 -10.000  -0.3435   0.01464   0.00881  -0.1711   0.8763   0.0494
  -9.750  -0.3123   0.01429   0.00840  -0.1726   0.8746   0.0501
  -9.500  -0.3052   0.01411   0.00818  -0.1686   0.8715   0.0505
  -9.250  -0.2922   0.01404   0.00808  -0.1658   0.8687   0.0512
  -9.000  -0.2750   0.01391   0.00792  -0.1639   0.8662   0.0516
  -8.750  -0.2592   0.01344   0.00740  -0.1620   0.8640   0.0524
  -8.500  -0.2363   0.01307   0.00700  -0.1616   0.8621   0.0538
  -8.250  -0.2085   0.01274   0.00664  -0.1622   0.8605   0.0549
  -8.000  -0.1746   0.01257   0.00645  -0.1641   0.8591   0.0564
  -7.750  -0.1602   0.01240   0.00626  -0.1616   0.8573   0.0567
  -7.500  -0.1527   0.01227   0.00610  -0.1574   0.8551   0.0573
  -7.250  -0.1368   0.01217   0.00598  -0.1551   0.8533   0.0583
  -7.000  -0.1176   0.01205   0.00584  -0.1536   0.8515   0.0589
  -6.750  -0.0966   0.01192   0.00568  -0.1525   0.8500   0.0592
  -6.500  -0.0761   0.01165   0.00538  -0.1512   0.8485   0.0612
  -6.250  -0.0523   0.01145   0.00518  -0.1508   0.8473   0.0629
  -6.000  -0.0247   0.01129   0.00501  -0.1512   0.8461   0.0644
  -5.750   0.0056   0.01113   0.00483  -0.1521   0.8451   0.0663
  -5.500   0.0381   0.01101   0.00468  -0.1536   0.8441   0.0677
  -5.250   0.0730   0.01084   0.00451  -0.1557   0.8431   0.0705
  -5.000   0.0896   0.01075   0.00445  -0.1535   0.8419   0.0742
  -4.750   0.0937   0.01072   0.00444  -0.1483   0.8401   0.0766
  -4.500   0.1062   0.01063   0.00439  -0.1452   0.8385   0.0846
  -4.250   0.1231   0.01037   0.00430  -0.1431   0.8370   0.1195
  -4.000   0.1428   0.01005   0.00425  -0.1418   0.8357   0.1807
  -3.750   0.1649   0.00994   0.00422  -0.1410   0.8346   0.2050
  -3.500   0.1887   0.00982   0.00419  -0.1404   0.8335   0.2300
  -3.250   0.2138   0.00973   0.00416  -0.1401   0.8325   0.2486
  -3.000   0.2396   0.00963   0.00414  -0.1401   0.8316   0.2697
  -2.750   0.2665   0.00954   0.00412  -0.1402   0.8307   0.2932
  -2.500   0.2936   0.00946   0.00412  -0.1404   0.8298   0.3200
  -2.250   0.3217   0.00937   0.00413  -0.1409   0.8289   0.3462
  -2.000   0.3539   0.00931   0.00414  -0.1423   0.8278   0.3711
  -1.750   0.3891   0.00926   0.00417  -0.1445   0.8267   0.3975
  -1.500   0.3697   0.00937   0.00433  -0.1337   0.8237   0.4069
  -1.250   0.3700   0.00938   0.00442  -0.1276   0.8207   0.4259
  -1.000   0.3852   0.00934   0.00446  -0.1250   0.8189   0.4519
  -0.750   0.4071   0.00914   0.00439  -0.1240   0.8167   0.4950
  -0.500   0.4227   0.00878   0.00435  -0.1216   0.8151   0.5912
  -0.250   0.5146   0.00872   0.00531  -0.1364   0.8156   0.8733
   0.000   0.5581   0.00899   0.00558  -0.1400   0.8145   0.8895
   0.250   0.5878   0.00925   0.00583  -0.1404   0.8130   0.9033
   0.500   0.6260   0.00945   0.00600  -0.1429   0.8112   0.9091
   0.750   0.6496   0.00967   0.00623  -0.1421   0.8098   0.9153
   1.000   0.6710   0.01007   0.00665  -0.1406   0.8084   0.9183
   1.250   0.6592   0.01044   0.00706  -0.1316   0.8055   0.9279
   1.500   0.6948   0.01072   0.00734  -0.1336   0.8041   0.9292
   1.750   0.7304   0.01090   0.00753  -0.1355   0.8020   0.9307
   2.000   0.7721   0.01106   0.00768  -0.1387   0.8000   0.9327
   2.250   0.8118   0.01106   0.00766  -0.1415   0.7972   0.9345
   2.500   0.8536   0.01107   0.00765  -0.1450   0.7947   0.9364
   2.750   0.8596   0.01149   0.00811  -0.1401   0.7912   0.9420
   3.000   0.8786   0.01170   0.00835  -0.1381   0.7865   0.9440
   3.250   0.9060   0.01174   0.00839  -0.1382   0.7825   0.9458
   3.500   0.9380   0.01170   0.00831  -0.1393   0.7769   0.9477
   3.750   0.9286   0.01220   0.00886  -0.1311   0.7704   0.9537
   4.000   0.9585   0.01224   0.00888  -0.1317   0.7625   0.9552
   4.250   0.9671   0.01261   0.00929  -0.1277   0.7560   0.9581
   4.500   0.9712   0.01309   0.00980  -0.1227   0.7515   0.9639
   4.750   0.9982   0.01316   0.00986  -0.1228   0.7430   0.9650
   5.000   1.0198   0.01341   0.01015  -0.1219   0.7345   0.9668
   5.250   1.0389   0.01373   0.01047  -0.1203   0.7232   0.9699
   5.500   1.0536   0.01436   0.01108  -0.1179   0.7035   0.9758
   5.750   1.0586   0.01514   0.01168  -0.1135   0.6624   0.9798
   6.000   1.0408   0.01666   0.01298  -0.1045   0.6195   0.9855
   6.250   1.0216   0.01838   0.01436  -0.0962   0.5490   0.9894
   6.500   1.0269   0.01927   0.01517  -0.0924   0.5209   0.9922
   6.750   0.9876   0.02176   0.01732  -0.0800   0.4549   0.9934
   7.000   0.9737   0.02337   0.01873  -0.0725   0.4179   0.9939
   7.250   0.9873   0.02358   0.01888  -0.0707   0.4011   0.9942
   7.500   0.9992   0.02403   0.01925  -0.0686   0.3790   0.9947
   7.750   1.0130   0.02449   0.01964  -0.0667   0.3593   0.9952
   8.000   1.0227   0.02516   0.02019  -0.0643   0.3315   0.9957
   8.250   1.0183   0.02652   0.02119  -0.0596   0.2670   0.9965
   8.500   1.0299   0.02714   0.02171  -0.0574   0.2435   0.9970
   8.750   1.0401   0.02784   0.02230  -0.0551   0.2202   0.9975
   9.000   1.0447   0.02883   0.02309  -0.0519   0.1849   0.9980
   9.250   1.0537   0.02960   0.02370  -0.0494   0.1600   0.9983
   9.500   1.0698   0.03001   0.02415  -0.0480   0.1570   0.9985
   9.750   1.0818   0.03063   0.02470  -0.0459   0.1434   0.9987
  10.000   1.0929   0.03131   0.02532  -0.0438   0.1307   0.9988
  10.250   1.1069   0.03184   0.02585  -0.0421   0.1255   0.9989
  10.500   1.1176   0.03254   0.02648  -0.0399   0.1118   0.9990
  10.750   1.1289   0.03322   0.02708  -0.0379   0.0996   0.9991
  11.000   1.1419   0.03383   0.02768  -0.0361   0.0944   0.9992
  11.250   1.1544   0.03447   0.02833  -0.0343   0.0895   0.9992
  11.500   1.1655   0.03520   0.02902  -0.0323   0.0816   0.9993
  11.750   1.1781   0.03585   0.02966  -0.0305   0.0773   0.9993
  12.000   1.1901   0.03655   0.03034  -0.0288   0.0718   0.9993
  12.250   1.2027   0.03723   0.03104  -0.0271   0.0691   0.9994
  12.500   1.2127   0.03809   0.03187  -0.0251   0.0638   0.9994
  12.750   1.2242   0.03885   0.03262  -0.0233   0.0587   0.9994
  13.000   1.2354   0.03964   0.03342  -0.0215   0.0557   0.9994
  13.250   1.2478   0.04034   0.03414  -0.0200   0.0533   0.9994
  13.500   1.2572   0.04129   0.03507  -0.0181   0.0493   0.9994
  13.750   1.2679   0.04215   0.03594  -0.0164   0.0455   0.9994
  14.000   1.2785   0.04303   0.03684  -0.0146   0.0437   0.9995
  14.250   1.2886   0.04394   0.03774  -0.0130   0.0399   0.9995
  14.500   1.2965   0.04505   0.03886  -0.0111   0.0376   0.9995
  14.750   1.3057   0.04608   0.03992  -0.0093   0.0353   0.9995
  15.000   1.3145   0.04715   0.04099  -0.0076   0.0326   0.9995
  15.250   1.3220   0.04831   0.04217  -0.0059   0.0306   0.9995
  15.500   1.3304   0.04944   0.04333  -0.0043   0.0298   0.9995
  15.750   1.3384   0.05062   0.04456  -0.0026   0.0289   0.9995
  16.000   1.3429   0.05209   0.04604  -0.0007   0.0270   0.9995
  16.250   1.3505   0.05336   0.04736   0.0008   0.0262   0.9995
  16.500   1.3578   0.05465   0.04871   0.0023   0.0255   0.9995
  16.750   1.3649   0.05601   0.05010   0.0037   0.0246   0.9995
  17.000   1.3707   0.05747   0.05160   0.0052   0.0240   0.9995
  17.250   1.3695   0.05961   0.05379   0.0071   0.0229   0.9995
  17.500   1.3738   0.06127   0.05551   0.0085   0.0226   0.9995
  17.750   1.3811   0.06269   0.05700   0.0097   0.0215   0.9995
  18.000   1.3848   0.06445   0.05882   0.0109   0.0218   0.9995
  18.250   1.3874   0.06635   0.06078   0.0122   0.0210   0.9995
  18.500   1.3853   0.06874   0.06318   0.0135   0.0191   0.9994
  18.750   1.3903   0.07049   0.06502   0.0145   0.0201   0.9994
  19.000   1.3965   0.07212   0.06669   0.0153   0.0186   0.9994
  19.250   1.3976   0.07429   0.06891   0.0162   0.0179   0.9994
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