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GOE 15K AIRFOIL (goe15k-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 15K AIRFOIL (goe15k-il)
Reynolds number: 500,000
Max Cl/Cd: 67.7 at α=4°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe15k-il-500000-n5.txt
Download as CSV file: xf-goe15k-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.000  -0.5038   0.12727   0.12433  -0.1054   0.9700   0.0127
 -17.750  -0.5406   0.11581   0.11272  -0.1109   0.9695   0.0125
 -17.500  -0.5705   0.10609   0.10290  -0.1160   0.9691   0.0124
 -17.250  -0.6106   0.09505   0.09175  -0.1220   0.9686   0.0123
 -17.000  -0.6527   0.08404   0.08058  -0.1282   0.9681   0.0122
 -16.750  -0.6990   0.07496   0.07138  -0.1308   0.9647   0.0120
 -16.500  -0.7516   0.06385   0.06012  -0.1363   0.9619   0.0115
 -16.250  -0.7824   0.05483   0.05090  -0.1425   0.9600   0.0115
 -16.000  -0.7949   0.04831   0.04416  -0.1481   0.9587   0.0119
 -15.750  -0.8060   0.04270   0.03836  -0.1527   0.9576   0.0118
 -15.500  -0.8278   0.03931   0.03482  -0.1508   0.9519   0.0120
 -15.250  -0.8356   0.03648   0.03185  -0.1505   0.9489   0.0120
 -15.000  -0.8336   0.03435   0.02955  -0.1501   0.9472   0.0124
 -14.750  -0.8326   0.03224   0.02731  -0.1494   0.9459   0.0128
 -14.500  -0.8436   0.03097   0.02593  -0.1446   0.9395   0.0127
 -14.250  -0.8412   0.02953   0.02438  -0.1425   0.9364   0.0129
 -14.000  -0.8321   0.02831   0.02307  -0.1411   0.9347   0.0136
 -13.750  -0.8238   0.02700   0.02163  -0.1394   0.9332   0.0138
 -13.500  -0.8236   0.02632   0.02087  -0.1353   0.9279   0.0141
 -13.250  -0.8173   0.02542   0.01986  -0.1324   0.9244   0.0149
 -13.000  -0.8045   0.02461   0.01893  -0.1306   0.9223   0.0153
 -12.750  -0.7915   0.02370   0.01791  -0.1289   0.9207   0.0156
 -12.500  -0.7777   0.02272   0.01686  -0.1273   0.9195   0.0164
 -12.250  -0.7720   0.02215   0.01622  -0.1237   0.9148   0.0170
 -12.000  -0.7612   0.02154   0.01551  -0.1210   0.9113   0.0178
 -11.750  -0.7448   0.02088   0.01475  -0.1195   0.9091   0.0186
 -11.500  -0.7252   0.02019   0.01399  -0.1186   0.9075   0.0200
 -11.250  -0.7032   0.01951   0.01325  -0.1182   0.9063   0.0213
 -11.000  -0.6789   0.01889   0.01254  -0.1182   0.9053   0.0229
 -10.750  -0.6532   0.01828   0.01187  -0.1185   0.9044   0.0244
 -10.500  -0.6507   0.01810   0.01166  -0.1135   0.8979   0.0260
 -10.250  -0.6300   0.01768   0.01118  -0.1125   0.8956   0.0280
 -10.000  -0.6050   0.01728   0.01075  -0.1125   0.8940   0.0305
  -9.750  -0.5770   0.01697   0.01042  -0.1130   0.8927   0.0332
  -9.500  -0.5477   0.01664   0.01001  -0.1138   0.8916   0.0357
  -9.250  -0.5176   0.01627   0.00961  -0.1149   0.8906   0.0378
  -9.000  -0.4855   0.01600   0.00932  -0.1163   0.8897   0.0401
  -8.750  -0.4795   0.01599   0.00926  -0.1118   0.8848   0.0418
  -8.500  -0.4598   0.01588   0.00909  -0.1103   0.8818   0.0438
  -8.250  -0.4347   0.01569   0.00882  -0.1101   0.8799   0.0449
  -8.000  -0.4084   0.01533   0.00840  -0.1102   0.8783   0.0463
  -7.750  -0.3807   0.01494   0.00799  -0.1106   0.8770   0.0484
  -7.500  -0.3510   0.01461   0.00761  -0.1115   0.8758   0.0496
  -7.250  -0.3188   0.01434   0.00730  -0.1129   0.8748   0.0516
  -7.000  -0.3003   0.01422   0.00714  -0.1112   0.8721   0.0535
  -6.750  -0.2929   0.01412   0.00699  -0.1068   0.8681   0.0544
  -6.500  -0.2728   0.01400   0.00683  -0.1054   0.8658   0.0554
  -6.250  -0.2491   0.01382   0.00660  -0.1048   0.8640   0.0560
  -6.000  -0.2232   0.01349   0.00622  -0.1047   0.8625   0.0574
  -5.750  -0.1952   0.01315   0.00585  -0.1051   0.8613   0.0589
  -5.500  -0.1651   0.01288   0.00554  -0.1060   0.8602   0.0599
  -5.250  -0.1332   0.01262   0.00527  -0.1073   0.8593   0.0622
  -5.000  -0.0998   0.01240   0.00500  -0.1089   0.8584   0.0632
  -4.750  -0.0994   0.01242   0.00503  -0.1028   0.8550   0.0643
  -4.500  -0.0856   0.01237   0.00495  -0.0999   0.8524   0.0653
  -4.250  -0.0657   0.01228   0.00483  -0.0983   0.8504   0.0665
  -4.000  -0.0420   0.01216   0.00469  -0.0976   0.8487   0.0680
  -3.750  -0.0160   0.01203   0.00454  -0.0975   0.8472   0.0691
  -3.500   0.0122   0.01185   0.00437  -0.0978   0.8460   0.0743
  -3.250   0.0421   0.01169   0.00423  -0.0986   0.8450   0.0808
  -3.000   0.0739   0.01139   0.00407  -0.0999   0.8442   0.1118
  -2.750   0.1065   0.01105   0.00395  -0.1015   0.8434   0.1695
  -2.500   0.1400   0.01083   0.00385  -0.1032   0.8427   0.2051
  -2.250   0.1428   0.01088   0.00397  -0.0977   0.8399   0.2213
  -2.000   0.1511   0.01085   0.00407  -0.0935   0.8373   0.2531
  -1.750   0.1681   0.01078   0.00410  -0.0914   0.8350   0.2820
  -1.500   0.1900   0.01069   0.00412  -0.0903   0.8333   0.3105
  -1.250   0.2144   0.01061   0.00411  -0.0898   0.8320   0.3381
  -1.000   0.2405   0.01051   0.00411  -0.0897   0.8308   0.3661
  -0.750   0.2681   0.01036   0.00408  -0.0900   0.8297   0.4023
  -0.500   0.3014   0.01014   0.00398  -0.0915   0.8280   0.4405
  -0.250   0.3339   0.00982   0.00388  -0.0929   0.8262   0.5034
   0.000   0.3109   0.00995   0.00418  -0.0814   0.8201   0.5428
   0.500   0.5290   0.01022   0.00573  -0.1184   0.8229   0.9158
   0.750   0.5471   0.01053   0.00606  -0.1161   0.8195   0.9266
   1.000   0.5750   0.01070   0.00622  -0.1162   0.8166   0.9322
   1.250   0.6062   0.01089   0.00641  -0.1171   0.8147   0.9387
   1.500   0.6358   0.01101   0.00653  -0.1176   0.8128   0.9436
   1.750   0.6739   0.01104   0.00655  -0.1201   0.8094   0.9455
   2.000   0.6776   0.01139   0.00694  -0.1147   0.8045   0.9526
   2.250   0.7030   0.01149   0.00703  -0.1142   0.7987   0.9558
   2.500   0.7467   0.01142   0.00696  -0.1180   0.7953   0.9570
   2.750   0.7501   0.01172   0.00731  -0.1126   0.7868   0.9619
   3.000   0.7739   0.01176   0.00731  -0.1117   0.7793   0.9656
   3.250   0.7924   0.01197   0.00758  -0.1098   0.7699   0.9683
   3.500   0.8094   0.01215   0.00775  -0.1075   0.7536   0.9723
   3.750   0.8217   0.01239   0.00798  -0.1042   0.7373   0.9762
   4.000   0.8449   0.01248   0.00800  -0.1033   0.7077   0.9783
   4.250   0.8457   0.01309   0.00823  -0.0976   0.6365   0.9826
   4.500   0.8438   0.01396   0.00883  -0.0916   0.5841   0.9865
   4.750   0.8367   0.01500   0.00953  -0.0849   0.5099   0.9891
   5.000   0.8292   0.01634   0.01050  -0.0785   0.4376   0.9927
   5.250   0.8399   0.01706   0.01109  -0.0757   0.4073   0.9947
   5.500   0.8547   0.01757   0.01147  -0.0738   0.3784   0.9959
   5.750   0.8709   0.01805   0.01185  -0.0722   0.3494   0.9973
   6.000   0.8867   0.01865   0.01229  -0.0706   0.3121   0.9989
   6.250   0.8993   0.01942   0.01282  -0.0685   0.2610   1.0000
   6.500   0.9044   0.02018   0.01339  -0.0646   0.2229   1.0000
   6.750   0.9111   0.02090   0.01394  -0.0612   0.1891   1.0000
   7.000   0.9246   0.02134   0.01435  -0.0589   0.1774   1.0000
   7.250   0.9340   0.02199   0.01487  -0.0560   0.1531   1.0000
   7.500   0.9466   0.02250   0.01533  -0.0536   0.1382   1.0000
   7.750   0.9577   0.02312   0.01582  -0.0510   0.1145   1.0000
   8.000   0.9709   0.02363   0.01630  -0.0488   0.1020   1.0000
   8.250   0.9839   0.02418   0.01680  -0.0466   0.0911   1.0000
   8.750   1.0114   0.02520   0.01779  -0.0426   0.0777   1.0000
   9.000   1.0247   0.02577   0.01833  -0.0405   0.0703   1.0000
   9.250   1.0389   0.02629   0.01886  -0.0386   0.0659   1.0000
   9.500   1.0520   0.02689   0.01944  -0.0365   0.0608   1.0000
   9.750   1.0665   0.02740   0.01999  -0.0347   0.0570   1.0000
  10.000   1.0807   0.02796   0.02057  -0.0329   0.0534   1.0000
  10.250   1.0942   0.02856   0.02118  -0.0310   0.0482   1.0000
  10.500   1.1070   0.02921   0.02181  -0.0291   0.0416   1.0000
  10.750   1.1199   0.02987   0.02247  -0.0272   0.0367   1.0000
  11.000   1.1321   0.03059   0.02317  -0.0252   0.0319   1.0000
  11.250   1.1441   0.03132   0.02391  -0.0233   0.0282   1.0000
  11.500   1.1547   0.03216   0.02476  -0.0211   0.0243   1.0000
  11.750   1.1669   0.03290   0.02555  -0.0193   0.0232   1.0000
  12.000   1.1786   0.03369   0.02636  -0.0174   0.0215   1.0000
  12.250   1.1888   0.03461   0.02731  -0.0154   0.0200   1.0000
  12.500   1.2003   0.03543   0.02818  -0.0136   0.0185   1.0000
  12.750   1.2105   0.03637   0.02917  -0.0116   0.0178   1.0000
  13.000   1.2192   0.03744   0.03028  -0.0096   0.0163   1.0000
  13.250   1.2289   0.03843   0.03133  -0.0077   0.0162   1.0000
  13.500   1.2388   0.03942   0.03240  -0.0059   0.0152   1.0000
  13.750   1.2482   0.04047   0.03350  -0.0041   0.0142   1.0000
  14.000   1.2563   0.04163   0.03473  -0.0022   0.0140   1.0000
  14.250   1.2645   0.04281   0.03597  -0.0004   0.0138   1.0000
  14.500   1.2699   0.04424   0.03745   0.0016   0.0131   1.0000
  14.750   1.2756   0.04567   0.03896   0.0035   0.0130   1.0000
  15.000   1.2830   0.04700   0.04037   0.0052   0.0122   1.0000
  15.250   1.2888   0.04845   0.04192   0.0069   0.0120   1.0000
  15.500   1.2937   0.05002   0.04357   0.0086   0.0116   1.0000
  15.750   1.3012   0.05137   0.04497   0.0099   0.0109   1.0000
  16.000   1.2998   0.05361   0.04729   0.0119   0.0107   1.0000
  16.250   1.3022   0.05554   0.04931   0.0134   0.0105   1.0000
  16.500   1.3054   0.05743   0.05129   0.0147   0.0104   1.0000
  16.750   1.3056   0.05968   0.05366   0.0162   0.0100   1.0000
  17.000   1.3109   0.06144   0.05550   0.0172   0.0092   1.0000
  17.250   1.3074   0.06418   0.05836   0.0185   0.0097   1.0000
  17.500   1.3045   0.06697   0.06127   0.0195   0.0095   1.0000
  17.750   1.3079   0.06907   0.06346   0.0201   0.0092   1.0000
  18.000   1.2981   0.07283   0.06735   0.0209   0.0094   1.0000
  18.250   1.2943   0.07599   0.07062   0.0214   0.0089   1.0000
  18.500   1.2885   0.07945   0.07420   0.0216   0.0092   1.0000
  18.750   1.2847   0.08275   0.07759   0.0216   0.0088   1.0000
  19.000   1.2778   0.08660   0.08157   0.0213   0.0088   1.0000
  19.250   1.2661   0.09125   0.08634   0.0207   0.0087   1.0000
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