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GOE 15K AIRFOIL (goe15k-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 15K AIRFOIL (goe15k-il)
Reynolds number: 1,000,000
Max Cl/Cd: 83.13 at α=1.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe15k-il-1000000-n5.txt
Download as CSV file: xf-goe15k-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 15K 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
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -0.6322   0.09604   0.09329  -0.1326   0.9696   0.0086
 -18.250  -0.7126   0.07994   0.07696  -0.1408   0.9692   0.0083
 -18.000  -0.7733   0.06717   0.06395  -0.1480   0.9687   0.0081
 -17.750  -0.8153   0.05691   0.05349  -0.1547   0.9683   0.0079
 -17.500  -0.8487   0.04739   0.04374  -0.1622   0.9679   0.0077
 -17.250  -0.8829   0.04268   0.03890  -0.1604   0.9626   0.0079
 -17.000  -0.8884   0.03904   0.03513  -0.1623   0.9609   0.0079
 -16.750  -0.8991   0.03524   0.03119  -0.1637   0.9596   0.0082
 -16.500  -0.9001   0.03273   0.02855  -0.1640   0.9586   0.0078
 -16.250  -0.8978   0.03065   0.02637  -0.1639   0.9578   0.0082
 -16.000  -0.8914   0.02899   0.02464  -0.1637   0.9572   0.0088
 -15.750  -0.9119   0.02781   0.02335  -0.1569   0.9503   0.0085
 -15.500  -0.9080   0.02642   0.02187  -0.1551   0.9483   0.0087
 -15.250  -0.8986   0.02527   0.02063  -0.1539   0.9470   0.0088
 -15.000  -0.8867   0.02423   0.01951  -0.1527   0.9459   0.0094
 -14.750  -0.8900   0.02368   0.01891  -0.1477   0.9398   0.0097
 -14.500  -0.8849   0.02276   0.01790  -0.1449   0.9365   0.0097
 -14.250  -0.8749   0.02189   0.01693  -0.1428   0.9345   0.0097
 -14.000  -0.8582   0.02120   0.01615  -0.1417   0.9332   0.0100
 -13.750  -0.8548   0.02055   0.01544  -0.1379   0.9281   0.0104
 -13.500  -0.8430   0.01990   0.01473  -0.1357   0.9245   0.0107
 -13.250  -0.8271   0.01913   0.01389  -0.1344   0.9224   0.0114
 -13.000  -0.8063   0.01851   0.01320  -0.1339   0.9207   0.0116
 -12.750  -0.7832   0.01790   0.01252  -0.1338   0.9193   0.0120
 -12.500  -0.7671   0.01739   0.01194  -0.1322   0.9156   0.0124
 -12.250  -0.7490   0.01682   0.01130  -0.1310   0.9119   0.0132
 -12.000  -0.7253   0.01625   0.01067  -0.1309   0.9093   0.0138
 -11.750  -0.6979   0.01570   0.01006  -0.1316   0.9072   0.0145
 -11.500  -0.6696   0.01518   0.00949  -0.1326   0.9052   0.0160
 -11.250  -0.6496   0.01474   0.00900  -0.1315   0.9012   0.0170
 -11.000  -0.6288   0.01435   0.00856  -0.1306   0.8972   0.0184
 -10.750  -0.6036   0.01398   0.00813  -0.1307   0.8940   0.0194
 -10.500  -0.5762   0.01355   0.00766  -0.1312   0.8913   0.0212
 -10.250  -0.5501   0.01319   0.00727  -0.1314   0.8885   0.0236
 -10.000  -0.5344   0.01293   0.00700  -0.1293   0.8841   0.0263
  -9.750  -0.5123   0.01268   0.00671  -0.1285   0.8805   0.0279
  -9.500  -0.4865   0.01243   0.00647  -0.1285   0.8775   0.0317
  -9.250  -0.4578   0.01219   0.00621  -0.1292   0.8751   0.0343
  -9.000  -0.4369   0.01204   0.00602  -0.1280   0.8720   0.0359
  -8.750  -0.4198   0.01189   0.00588  -0.1260   0.8685   0.0381
  -8.500  -0.3984   0.01174   0.00571  -0.1249   0.8653   0.0402
  -8.250  -0.3740   0.01160   0.00556  -0.1245   0.8627   0.0420
  -8.000  -0.3475   0.01147   0.00538  -0.1246   0.8604   0.0433
  -7.500  -0.3043   0.01122   0.00505  -0.1224   0.8555   0.0446
  -7.250  -0.2857   0.01115   0.00495  -0.1205   0.8526   0.0451
  -7.000  -0.2656   0.01098   0.00475  -0.1191   0.8500   0.0468
  -6.750  -0.2433   0.01077   0.00451  -0.1182   0.8477   0.0483
  -6.500  -0.2188   0.01061   0.00434  -0.1178   0.8458   0.0498
  -6.250  -0.1925   0.01049   0.00420  -0.1177   0.8440   0.0513
  -6.000  -0.1641   0.01034   0.00403  -0.1182   0.8424   0.0523
  -5.750  -0.1473   0.01025   0.00392  -0.1159   0.8405   0.0530
  -5.500  -0.1286   0.01014   0.00378  -0.1141   0.8387   0.0534
  -5.250  -0.1081   0.01005   0.00368  -0.1126   0.8368   0.0544
  -5.000  -0.0862   0.00994   0.00355  -0.1115   0.8350   0.0545
  -4.750  -0.0630   0.00984   0.00343  -0.1107   0.8333   0.0554
  -4.500  -0.0387   0.00975   0.00332  -0.1102   0.8317   0.0558
  -4.250  -0.0132   0.00966   0.00321  -0.1099   0.8303   0.0561
  -4.000   0.0137   0.00952   0.00305  -0.1099   0.8290   0.0581
  -3.750   0.0422   0.00943   0.00294  -0.1104   0.8277   0.0587
  -3.500   0.0712   0.00931   0.00283  -0.1109   0.8262   0.0618
  -3.250   0.0889   0.00925   0.00278  -0.1087   0.8247   0.0629
  -3.000   0.1091   0.00918   0.00273  -0.1072   0.8233   0.0658
  -2.750   0.1303   0.00911   0.00268  -0.1059   0.8219   0.0690
  -2.500   0.1526   0.00901   0.00263  -0.1049   0.8204   0.0790
  -2.250   0.1761   0.00877   0.00256  -0.1042   0.8191   0.1228
  -2.000   0.1996   0.00852   0.00251  -0.1036   0.8176   0.1752
  -1.750   0.2242   0.00840   0.00247  -0.1032   0.8161   0.2007
  -1.500   0.2501   0.00830   0.00243  -0.1030   0.8138   0.2217
  -1.250   0.2799   0.00817   0.00237  -0.1037   0.8116   0.2499
  -1.000   0.3027   0.00806   0.00238  -0.1028   0.8096   0.2817
  -0.750   0.3146   0.00799   0.00241  -0.0994   0.8066   0.3082
  -0.500   0.3336   0.00793   0.00243  -0.0976   0.8045   0.3329
  -0.250   0.3529   0.00788   0.00245  -0.0958   0.8021   0.3546
   0.000   0.3745   0.00778   0.00245  -0.0946   0.7994   0.3856
   0.250   0.4000   0.00768   0.00245  -0.0943   0.7975   0.4171
   0.500   0.4297   0.00763   0.00243  -0.0950   0.7947   0.4334
   0.750   0.4397   0.00752   0.00251  -0.0911   0.7922   0.4833
   1.000   0.4546   0.00733   0.00256  -0.0884   0.7900   0.5552
   1.250   0.4399   0.00662   0.00259  -0.0788   0.7861   0.7737
   1.750   0.6343   0.00763   0.00407  -0.1111   0.7798   0.9245
   2.000   0.6440   0.00795   0.00442  -0.1069   0.7722   0.9373
   2.250   0.6568   0.00810   0.00455  -0.1035   0.7662   0.9436
   2.500   0.6840   0.00826   0.00472  -0.1036   0.7608   0.9458
   2.750   0.6934   0.00854   0.00497  -0.0994   0.7470   0.9515
   3.000   0.6994   0.00882   0.00521  -0.0945   0.7269   0.9556
   3.250   0.7117   0.00920   0.00548  -0.0912   0.6929   0.9577
   3.500   0.6848   0.01020   0.00621  -0.0790   0.6371   0.9656
   3.750   0.6859   0.01118   0.00691  -0.0737   0.5773   0.9673
   4.000   0.6760   0.01241   0.00777  -0.0663   0.4895   0.9697
   4.250   0.6680   0.01366   0.00868  -0.0594   0.4175   0.9740
   4.500   0.6784   0.01423   0.00915  -0.0561   0.3941   0.9763
   4.750   0.7035   0.01460   0.00945  -0.0562   0.3723   0.9770
   5.000   0.7302   0.01507   0.00980  -0.0568   0.3450   0.9783
   5.250   0.7521   0.01550   0.01014  -0.0562   0.3196   0.9795
   5.500   0.7655   0.01619   0.01065  -0.0539   0.2769   0.9812
   5.750   0.7749   0.01702   0.01126  -0.0509   0.2325   0.9836
   6.000   0.7872   0.01763   0.01179  -0.0482   0.2116   0.9856
   6.250   0.8066   0.01809   0.01213  -0.0473   0.1853   0.9861
   6.500   0.8257   0.01853   0.01247  -0.0463   0.1620   0.9866
   6.750   0.8428   0.01901   0.01283  -0.0449   0.1384   0.9870
   7.000   0.8659   0.01925   0.01308  -0.0445   0.1351   0.9875
   7.250   0.8806   0.01992   0.01355  -0.0428   0.1002   0.9882
   7.500   0.8996   0.02031   0.01392  -0.0417   0.0917   0.9887
   7.750   0.9164   0.02079   0.01432  -0.0403   0.0785   0.9892
   8.250   0.9529   0.02159   0.01509  -0.0378   0.0666   0.9902
   8.500   0.9719   0.02198   0.01548  -0.0367   0.0640   0.9908
   8.750   0.9891   0.02248   0.01595  -0.0355   0.0563   0.9915
   9.000   1.0067   0.02290   0.01637  -0.0341   0.0543   0.9919
   9.250   1.0232   0.02336   0.01683  -0.0326   0.0506   0.9923
   9.500   1.0407   0.02377   0.01727  -0.0313   0.0486   0.9927
   9.750   1.0556   0.02438   0.01783  -0.0296   0.0409   0.9933
  10.000   1.0717   0.02507   0.01850  -0.0281   0.0357   0.9944
  10.250   1.0871   0.02561   0.01902  -0.0266   0.0296   0.9946
  10.500   1.1021   0.02619   0.01956  -0.0251   0.0245   0.9947
  10.750   1.1181   0.02672   0.02010  -0.0237   0.0224   0.9948
  11.000   1.1328   0.02733   0.02071  -0.0222   0.0200   0.9950
  11.250   1.1481   0.02790   0.02130  -0.0208   0.0182   0.9951
  11.500   1.1625   0.02854   0.02196  -0.0192   0.0169   0.9953
  11.750   1.1774   0.02915   0.02260  -0.0178   0.0162   0.9954
  12.000   1.1925   0.02975   0.02322  -0.0164   0.0152   0.9956
  12.250   1.2063   0.03043   0.02394  -0.0149   0.0145   0.9957
  12.500   1.2190   0.03117   0.02468  -0.0132   0.0131   0.9958
  12.750   1.2328   0.03186   0.02542  -0.0117   0.0129   0.9959
  13.000   1.2469   0.03263   0.02622  -0.0104   0.0118   0.9962
  13.250   1.2623   0.03337   0.02700  -0.0094   0.0117   0.9966
  13.500   1.2738   0.03424   0.02790  -0.0077   0.0110   0.9967
  13.750   1.2844   0.03513   0.02883  -0.0059   0.0103   0.9967
  14.000   1.2949   0.03603   0.02978  -0.0042   0.0103   0.9967
  14.250   1.3067   0.03685   0.03063  -0.0026   0.0098   0.9968
  14.500   1.3165   0.03781   0.03164  -0.0008   0.0094   0.9968
  14.750   1.3251   0.03884   0.03274   0.0011   0.0095   0.9967
  15.000   1.3326   0.04000   0.03394   0.0031   0.0089   0.9967
  15.250   1.3411   0.04107   0.03506   0.0049   0.0087   0.9966
  15.500   1.3473   0.04233   0.03638   0.0069   0.0086   0.9965
  15.750   1.3566   0.04334   0.03743   0.0084   0.0079   0.9965
  16.000   1.3605   0.04481   0.03898   0.0106   0.0079   0.9964
  16.250   1.3667   0.04610   0.04034   0.0124   0.0077   0.9963
  16.500   1.3745   0.04725   0.04151   0.0139   0.0072   0.9962
  16.750   1.3753   0.04904   0.04340   0.0161   0.0073   0.9960
  17.000   1.3796   0.05054   0.04492   0.0179   0.0064   0.9959
  17.250   1.3842   0.05205   0.04654   0.0195   0.0070   0.9958
  17.500   1.3849   0.05397   0.04853   0.0213   0.0069   0.9957
  17.750   1.3853   0.05594   0.05055   0.0229   0.0066   0.9956
  18.000   1.3874   0.05782   0.05253   0.0243   0.0068   0.9956
  18.250   1.3874   0.06001   0.05479   0.0257   0.0063   0.9955
  18.500   1.3867   0.06253   0.05741   0.0265   0.0066   0.9957
  18.750   1.3907   0.06459   0.05954   0.0269   0.0062   0.9958
  19.000   1.3887   0.06714   0.06218   0.0279   0.0062   0.9957
  19.250   1.3834   0.07008   0.06523   0.0289   0.0062   0.9957
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