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GOE 16K AIRFOIL (goe16k-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 16K AIRFOIL (goe16k-il)
Reynolds number: 1,000,000
Max Cl/Cd: 70.87 at α=2.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe16k-il-1000000-n5.txt
Download as CSV file: xf-goe16k-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.6958   0.07375   0.07025  -0.1756   0.9477   0.0154
 -19.500  -0.7271   0.06649   0.06285  -0.1797   0.9471   0.0153
 -19.250  -0.7569   0.05950   0.05571  -0.1836   0.9466   0.0154
 -19.000  -0.7774   0.05357   0.04966  -0.1873   0.9461   0.0156
 -18.750  -0.8235   0.04814   0.04410  -0.1853   0.9398   0.0161
 -18.500  -0.8339   0.04399   0.03984  -0.1874   0.9379   0.0163
 -18.250  -0.8398   0.04030   0.03602  -0.1893   0.9363   0.0162
 -18.000  -0.8467   0.03679   0.03240  -0.1908   0.9350   0.0169
 -17.750  -0.8475   0.03417   0.02968  -0.1914   0.9339   0.0170
 -17.500  -0.8647   0.03229   0.02770  -0.1876   0.9272   0.0170
 -17.250  -0.8655   0.03048   0.02580  -0.1866   0.9245   0.0176
 -17.000  -0.8604   0.02885   0.02409  -0.1860   0.9228   0.0185
 -16.750  -0.8525   0.02737   0.02253  -0.1856   0.9214   0.0185
 -16.500  -0.8474   0.02596   0.02105  -0.1844   0.9193   0.0194
 -16.250  -0.8477   0.02484   0.01987  -0.1817   0.9144   0.0205
 -16.000  -0.8369   0.02379   0.01874  -0.1807   0.9117   0.0210
 -15.750  -0.8223   0.02277   0.01766  -0.1804   0.9097   0.0223
 -15.500  -0.8042   0.02180   0.01663  -0.1806   0.9081   0.0235
 -15.250  -0.7838   0.02096   0.01572  -0.1810   0.9064   0.0244
 -15.000  -0.7737   0.02033   0.01503  -0.1790   0.9017   0.0253
 -14.750  -0.7578   0.01966   0.01433  -0.1781   0.8979   0.0274
 -14.500  -0.7367   0.01907   0.01370  -0.1782   0.8949   0.0290
 -14.250  -0.7131   0.01852   0.01307  -0.1787   0.8923   0.0303
 -14.000  -0.6974   0.01808   0.01260  -0.1774   0.8883   0.0317
 -13.750  -0.6811   0.01770   0.01219  -0.1760   0.8836   0.0332
 -13.500  -0.6599   0.01734   0.01177  -0.1757   0.8800   0.0345
 -13.250  -0.6359   0.01694   0.01129  -0.1759   0.8769   0.0353
 -13.000  -0.6213   0.01658   0.01086  -0.1741   0.8729   0.0356
 -12.750  -0.6068   0.01633   0.01059  -0.1720   0.8688   0.0371
 -12.500  -0.5912   0.01599   0.01019  -0.1704   0.8650   0.0372
 -12.250  -0.5701   0.01573   0.00990  -0.1697   0.8620   0.0384
 -12.000  -0.5482   0.01547   0.00959  -0.1692   0.8592   0.0395
 -11.750  -0.5346   0.01533   0.00942  -0.1667   0.8562   0.0407
 -11.500  -0.5207   0.01515   0.00919  -0.1644   0.8530   0.0413
 -11.250  -0.5039   0.01497   0.00897  -0.1626   0.8502   0.0419
 -11.000  -0.4855   0.01477   0.00871  -0.1612   0.8476   0.0423
 -10.750  -0.4675   0.01449   0.00837  -0.1598   0.8451   0.0424
 -10.250  -0.4342   0.01401   0.00786  -0.1561   0.8408   0.0447
 -10.000  -0.4196   0.01386   0.00769  -0.1538   0.8387   0.0456
  -9.750  -0.4044   0.01366   0.00745  -0.1515   0.8366   0.0457
  -9.500  -0.3863   0.01353   0.00730  -0.1499   0.8347   0.0469
  -9.250  -0.3681   0.01335   0.00708  -0.1482   0.8327   0.0474
  -9.000  -0.3481   0.01320   0.00690  -0.1470   0.8311   0.0480
  -8.750  -0.3276   0.01303   0.00667  -0.1458   0.8293   0.0483
  -8.500  -0.3053   0.01287   0.00647  -0.1450   0.8276   0.0489
  -8.000  -0.2640   0.01257   0.00611  -0.1427   0.8247   0.0497
  -7.750  -0.2482   0.01242   0.00594  -0.1404   0.8232   0.0496
  -7.500  -0.2316   0.01220   0.00571  -0.1383   0.8219   0.0517
  -7.250  -0.2134   0.01203   0.00553  -0.1366   0.8205   0.0522
  -7.000  -0.1942   0.01190   0.00539  -0.1351   0.8192   0.0531
  -6.750  -0.1741   0.01177   0.00524  -0.1337   0.8178   0.0534
  -6.500  -0.1529   0.01163   0.00510  -0.1326   0.8166   0.0545
  -6.250  -0.1310   0.01152   0.00497  -0.1316   0.8154   0.0554
  -6.000  -0.1082   0.01140   0.00483  -0.1308   0.8143   0.0558
  -5.750  -0.0846   0.01129   0.00469  -0.1302   0.8131   0.0570
  -5.500  -0.0597   0.01118   0.00456  -0.1299   0.8121   0.0573
  -5.250  -0.0336   0.01109   0.00446  -0.1298   0.8111   0.0580
  -5.000  -0.0058   0.01095   0.00430  -0.1302   0.8100   0.0588
  -4.750   0.0227   0.01083   0.00418  -0.1307   0.8091   0.0607
  -4.500   0.0408   0.01074   0.00411  -0.1288   0.8083   0.0632
  -4.250   0.0589   0.01067   0.00405  -0.1269   0.8073   0.0650
  -4.000   0.0776   0.01062   0.00401  -0.1251   0.8061   0.0653
  -3.750   0.0970   0.01056   0.00396  -0.1235   0.8049   0.0674
  -3.500   0.1178   0.01046   0.00391  -0.1223   0.8038   0.0744
  -3.250   0.1390   0.01029   0.00384  -0.1211   0.8027   0.0951
  -3.000   0.1601   0.01022   0.00380  -0.1199   0.8017   0.1057
  -2.750   0.1816   0.00999   0.00375  -0.1189   0.8007   0.1497
  -2.500   0.2037   0.00985   0.00373  -0.1180   0.7997   0.1781
  -2.250   0.2265   0.00977   0.00371  -0.1172   0.7987   0.1937
  -2.000   0.2503   0.00969   0.00369  -0.1166   0.7976   0.2113
  -1.750   0.2757   0.00958   0.00366  -0.1164   0.7964   0.2333
  -1.500   0.3057   0.00943   0.00359  -0.1173   0.7941   0.2617
  -1.250   0.3359   0.00933   0.00356  -0.1182   0.7925   0.2849
  -1.000   0.3390   0.00938   0.00367  -0.1127   0.7902   0.2958
  -0.750   0.3528   0.00936   0.00373  -0.1099   0.7882   0.3161
  -0.500   0.3707   0.00936   0.00377  -0.1079   0.7864   0.3277
  -0.250   0.3873   0.00930   0.00382  -0.1056   0.7840   0.3586
   0.000   0.4076   0.00928   0.00385  -0.1042   0.7825   0.3724
   0.250   0.4292   0.00923   0.00383  -0.1031   0.7795   0.3885
   0.500   0.4559   0.00917   0.00382  -0.1031   0.7780   0.4058
   0.750   0.4799   0.00904   0.00384  -0.1026   0.7760   0.4521
   1.000   0.4913   0.00891   0.00396  -0.0993   0.7749   0.5219
   1.250   0.5017   0.00900   0.00410  -0.0956   0.7724   0.5320
   1.750   0.6435   0.00941   0.00583  -0.1159   0.7709   0.9029
   2.000   0.6558   0.00968   0.00611  -0.1125   0.7671   0.9136
   2.250   0.6782   0.00976   0.00620  -0.1116   0.7663   0.9171
   2.500   0.7060   0.00999   0.00642  -0.1117   0.7630   0.9233
   2.750   0.7165   0.01011   0.00654  -0.1080   0.7593   0.9306
   3.000   0.7253   0.01055   0.00701  -0.1040   0.7514   0.9330
   3.250   0.7516   0.01070   0.00718  -0.1040   0.7504   0.9351
   3.500   0.7618   0.01091   0.00737  -0.1003   0.7431   0.9399
   3.750   0.7653   0.01140   0.00784  -0.0951   0.7299   0.9442
   4.000   0.7870   0.01175   0.00822  -0.0941   0.7215   0.9460
   4.250   0.7604   0.01285   0.00909  -0.0826   0.6703   0.9513
   4.500   0.7551   0.01356   0.00971  -0.0758   0.6491   0.9548
   4.750   0.7643   0.01458   0.01060  -0.0726   0.6194   0.9565
   5.000   0.7615   0.01584   0.01171  -0.0670   0.5831   0.9588
   5.250   0.7215   0.01784   0.01339  -0.0540   0.5108   0.9630
   5.500   0.7188   0.01919   0.01456  -0.0488   0.4675   0.9655
   5.750   0.7208   0.02038   0.01553  -0.0448   0.4235   0.9662
   6.000   0.7364   0.02107   0.01614  -0.0433   0.4046   0.9669
   6.250   0.7576   0.02182   0.01681  -0.0430   0.3837   0.9683
   6.500   0.7752   0.02241   0.01734  -0.0418   0.3667   0.9694
   6.750   0.7935   0.02309   0.01795  -0.0408   0.3489   0.9716
   7.000   0.7833   0.02419   0.01893  -0.0336   0.3217   0.9749
   7.250   0.8146   0.02450   0.01925  -0.0354   0.3157   0.9754
   7.500   0.8350   0.02503   0.01970  -0.0350   0.2968   0.9758
   7.750   0.8469   0.02579   0.02030  -0.0330   0.2644   0.9762
   8.000   0.8550   0.02662   0.02098  -0.0303   0.2334   0.9765
   8.250   0.8660   0.02755   0.02172  -0.0284   0.1969   0.9770
   8.500   0.8830   0.02808   0.02220  -0.0272   0.1848   0.9774
   8.750   0.8991   0.02869   0.02274  -0.0260   0.1684   0.9780
   9.000   0.9140   0.02936   0.02332  -0.0246   0.1502   0.9785
   9.250   0.9323   0.02980   0.02378  -0.0236   0.1480   0.9790
   9.500   0.9463   0.03043   0.02435  -0.0220   0.1355   0.9795
   9.750   0.9596   0.03109   0.02493  -0.0203   0.1216   0.9800
  10.000   0.9736   0.03173   0.02551  -0.0186   0.1105   0.9804
  10.250   0.9869   0.03237   0.02610  -0.0170   0.0990   0.9810
  10.500   1.0016   0.03295   0.02668  -0.0154   0.0955   0.9815
  10.750   1.0150   0.03365   0.02737  -0.0137   0.0903   0.9824
  11.250   1.0373   0.03525   0.02896  -0.0091   0.0815   0.9849
  11.500   1.0472   0.03615   0.02971  -0.0073   0.0644   0.9850
  11.750   1.0682   0.03644   0.03011  -0.0069   0.0711   0.9851
  12.000   1.0803   0.03723   0.03086  -0.0054   0.0624   0.9853
  12.250   1.0932   0.03798   0.03156  -0.0041   0.0562   0.9854
  12.500   1.1100   0.03851   0.03214  -0.0032   0.0562   0.9855
  12.750   1.1249   0.03918   0.03281  -0.0021   0.0523   0.9856
  13.000   1.1379   0.04009   0.03367  -0.0010   0.0442   0.9859
  13.250   1.1572   0.04061   0.03430  -0.0007   0.0491   0.9861
  13.500   1.1682   0.04153   0.03517   0.0008   0.0423   0.9862
  13.750   1.1796   0.04238   0.03601   0.0023   0.0374   0.9863
  14.000   1.1878   0.04345   0.03705   0.0041   0.0317   0.9863
  14.250   1.1999   0.04428   0.03792   0.0055   0.0312   0.9864
  14.500   1.2085   0.04533   0.03896   0.0072   0.0274   0.9864
  14.750   1.2188   0.04629   0.03994   0.0087   0.0258   0.9865
  15.000   1.2266   0.04742   0.04109   0.0105   0.0239   0.9865
  15.250   1.2361   0.04845   0.04215   0.0120   0.0222   0.9865
  15.500   1.2473   0.04935   0.04309   0.0133   0.0225   0.9865
  15.750   1.2543   0.05059   0.04437   0.0149   0.0211   0.9866
  16.000   1.2612   0.05183   0.04563   0.0166   0.0193   0.9866
  16.250   1.2692   0.05299   0.04682   0.0180   0.0182   0.9866
  16.500   1.2778   0.05415   0.04804   0.0194   0.0187   0.9866
  16.750   1.2836   0.05555   0.04946   0.0209   0.0172   0.9866
  17.000   1.2885   0.05704   0.05099   0.0224   0.0166   0.9866
  17.250   1.2968   0.05829   0.05229   0.0236   0.0158   0.9866
  17.500   1.3024   0.05979   0.05384   0.0249   0.0152   0.9867
  17.750   1.3086   0.06146   0.05555   0.0258   0.0145   0.9868
  18.000   1.3147   0.06317   0.05729   0.0265   0.0135   0.9870
  18.250   1.3203   0.06480   0.05897   0.0275   0.0131   0.9871
  18.500   1.3245   0.06646   0.06070   0.0286   0.0132   0.9871
  18.750   1.3268   0.06838   0.06267   0.0298   0.0120   0.9871
  19.000   1.3295   0.07026   0.06461   0.0308   0.0122   0.9871
  19.250   1.3318   0.07221   0.06664   0.0318   0.0126   0.9871
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