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GOE 493 AIRFOIL (goe493-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 493 AIRFOIL (goe493-il)
Reynolds number: 1,000,000
Max Cl/Cd: 127.09 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe493-il-1000000.txt
Download as CSV file: xf-goe493-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 493 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
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.8278   0.08508   0.08209  -0.0746   1.0000   0.0113
 -17.000  -0.8431   0.07933   0.07625  -0.0774   1.0000   0.0114
 -16.750  -0.8602   0.07358   0.07041  -0.0801   1.0000   0.0114
 -16.500  -0.8751   0.06822   0.06496  -0.0826   1.0000   0.0114
 -16.250  -0.8929   0.06281   0.05945  -0.0851   1.0000   0.0115
 -16.000  -0.9078   0.05796   0.05451  -0.0871   1.0000   0.0115
 -15.750  -0.9205   0.05355   0.05000  -0.0888   1.0000   0.0116
 -15.500  -0.9347   0.04924   0.04560  -0.0902   1.0000   0.0116
 -15.250  -0.9472   0.04544   0.04172  -0.0911   1.0000   0.0116
 -15.000  -0.9629   0.04174   0.03793  -0.0914   1.0000   0.0117
 -14.750  -0.9799   0.03861   0.03472  -0.0906   1.0000   0.0117
 -14.500  -0.9777   0.03456   0.03054  -0.0949   0.9986   0.0118
 -14.250  -0.9736   0.02983   0.02566  -0.1011   0.9955   0.0122
 -14.000  -0.9602   0.02701   0.02273  -0.1051   0.9921   0.0123
 -13.750  -0.9436   0.02497   0.02059  -0.1079   0.9881   0.0127
 -13.500  -0.9226   0.02337   0.01890  -0.1105   0.9851   0.0129
 -13.250  -0.8983   0.02208   0.01754  -0.1128   0.9831   0.0132
 -13.000  -0.8814   0.02108   0.01646  -0.1129   0.9773   0.0136
 -12.750  -0.8581   0.02011   0.01542  -0.1138   0.9740   0.0140
 -12.500  -0.8297   0.01937   0.01459  -0.1153   0.9719   0.0144
 -12.250  -0.8002   0.01826   0.01339  -0.1175   0.9702   0.0149
 -12.000  -0.7829   0.01723   0.01230  -0.1170   0.9628   0.0155
 -11.750  -0.7539   0.01650   0.01151  -0.1184   0.9593   0.0161
 -11.500  -0.7223   0.01584   0.01079  -0.1201   0.9562   0.0168
 -11.250  -0.7026   0.01536   0.01024  -0.1192   0.9484   0.0173
 -11.000  -0.6747   0.01488   0.00969  -0.1199   0.9435   0.0178
 -10.750  -0.6569   0.01418   0.00891  -0.1187   0.9360   0.0189
 -10.500  -0.6346   0.01370   0.00839  -0.1181   0.9296   0.0198
 -10.250  -0.6107   0.01333   0.00795  -0.1178   0.9240   0.0209
 -10.000  -0.5898   0.01301   0.00758  -0.1167   0.9175   0.0218
  -9.750  -0.5680   0.01251   0.00703  -0.1160   0.9118   0.0236
  -9.500  -0.5460   0.01219   0.00666  -0.1151   0.9062   0.0253
  -9.250  -0.5248   0.01179   0.00623  -0.1141   0.9003   0.0278
  -9.000  -0.5007   0.01146   0.00586  -0.1136   0.8951   0.0308
  -8.750  -0.4795   0.01107   0.00548  -0.1125   0.8897   0.0355
  -8.500  -0.4573   0.01071   0.00513  -0.1117   0.8842   0.0419
  -8.250  -0.4335   0.01038   0.00479  -0.1111   0.8792   0.0505
  -8.000  -0.4105   0.01007   0.00452  -0.1104   0.8742   0.0603
  -7.750  -0.3868   0.00980   0.00428  -0.1097   0.8690   0.0701
  -7.500  -0.3617   0.00957   0.00406  -0.1093   0.8642   0.0790
  -7.250  -0.3365   0.00939   0.00387  -0.1089   0.8594   0.0863
  -7.000  -0.3114   0.00921   0.00371  -0.1084   0.8543   0.0931
  -6.750  -0.2857   0.00904   0.00352  -0.1081   0.8494   0.0999
  -6.500  -0.2596   0.00890   0.00335  -0.1078   0.8446   0.1060
  -6.250  -0.2343   0.00873   0.00319  -0.1074   0.8394   0.1124
  -6.000  -0.2084   0.00858   0.00303  -0.1070   0.8343   0.1194
  -5.750  -0.1821   0.00844   0.00287  -0.1068   0.8295   0.1272
  -5.500  -0.1565   0.00829   0.00274  -0.1064   0.8241   0.1360
  -5.250  -0.1310   0.00811   0.00259  -0.1060   0.8186   0.1477
  -5.000  -0.1050   0.00796   0.00245  -0.1057   0.8133   0.1604
  -4.750  -0.0795   0.00778   0.00232  -0.1053   0.8078   0.1766
  -4.500  -0.0538   0.00762   0.00220  -0.1049   0.8021   0.1946
  -4.250  -0.0279   0.00748   0.00208  -0.1045   0.7965   0.2130
  -4.000  -0.0026   0.00730   0.00197  -0.1041   0.7902   0.2352
  -3.750   0.0232   0.00716   0.00186  -0.1037   0.7842   0.2584
  -3.500   0.0487   0.00698   0.00178  -0.1033   0.7783   0.2857
  -3.250   0.0743   0.00684   0.00170  -0.1029   0.7718   0.3130
  -3.000   0.1001   0.00673   0.00163  -0.1025   0.7656   0.3396
  -2.750   0.1259   0.00662   0.00158  -0.1022   0.7586   0.3638
  -2.500   0.1518   0.00655   0.00153  -0.1017   0.7519   0.3886
  -2.250   0.1779   0.00646   0.00150  -0.1014   0.7444   0.4098
  -2.000   0.2035   0.00643   0.00147  -0.1009   0.7362   0.4284
  -1.750   0.2296   0.00638   0.00145  -0.1005   0.7275   0.4451
  -1.500   0.2553   0.00638   0.00142  -0.1001   0.7189   0.4607
  -1.250   0.2814   0.00635   0.00142  -0.0997   0.7100   0.4767
  -1.000   0.3072   0.00635   0.00141  -0.0992   0.7017   0.4913
  -0.750   0.3331   0.00635   0.00141  -0.0988   0.6926   0.5049
  -0.500   0.3587   0.00635   0.00142  -0.0983   0.6838   0.5190
  -0.250   0.3839   0.00637   0.00143  -0.0977   0.6742   0.5326
   0.000   0.4096   0.00637   0.00146  -0.0973   0.6653   0.5484
   0.250   0.4345   0.00640   0.00148  -0.0967   0.6564   0.5632
   0.500   0.4606   0.00641   0.00151  -0.0963   0.6484   0.5762
   0.750   0.4856   0.00646   0.00154  -0.0957   0.6407   0.5897
   1.000   0.5116   0.00645   0.00158  -0.0953   0.6333   0.6040
   1.250   0.5362   0.00649   0.00162  -0.0946   0.6257   0.6191
   1.500   0.5617   0.00648   0.00167  -0.0942   0.6185   0.6363
   1.750   0.5859   0.00651   0.00173  -0.0934   0.6107   0.6569
   2.000   0.6105   0.00650   0.00180  -0.0927   0.6034   0.6801
   2.250   0.6343   0.00653   0.00187  -0.0919   0.5957   0.7050
   2.500   0.6583   0.00654   0.00195  -0.0911   0.5891   0.7314
   3.000   0.7047   0.00659   0.00212  -0.0891   0.5732   0.7841
   3.250   0.7266   0.00663   0.00221  -0.0878   0.5634   0.8096
   3.500   0.7486   0.00664   0.00230  -0.0865   0.5535   0.8379
   3.750   0.7690   0.00667   0.00240  -0.0849   0.5435   0.8726
   4.000   0.7987   0.00672   0.00256  -0.0853   0.5292   0.9271
   4.250   0.8608   0.00695   0.00278  -0.0931   0.5125   0.9638
   4.500   0.9111   0.00718   0.00296  -0.0983   0.4967   0.9852
   4.750   0.9430   0.00742   0.00314  -0.0995   0.4775   1.0000
   5.000   0.9586   0.00763   0.00327  -0.0970   0.4571   1.0000
   5.250   0.9726   0.00790   0.00343  -0.0942   0.4347   1.0000
   5.500   0.9864   0.00817   0.00361  -0.0914   0.4108   1.0000
   5.750   0.9953   0.00850   0.00381  -0.0876   0.3847   1.0000
   6.000   1.0060   0.00884   0.00404  -0.0843   0.3604   1.0000
   6.250   1.0168   0.00924   0.00431  -0.0810   0.3353   1.0000
   6.500   1.0298   0.00962   0.00460  -0.0782   0.3139   1.0000
   6.750   1.0428   0.01003   0.00490  -0.0755   0.2916   1.0000
   7.000   1.0560   0.01048   0.00523  -0.0729   0.2662   1.0000
   7.250   1.0634   0.01117   0.00570  -0.0694   0.2218   1.0000
   7.500   1.0588   0.01240   0.00654  -0.0641   0.1537   1.0000
   7.750   1.0647   0.01328   0.00722  -0.0606   0.1172   1.0000
   8.000   1.0682   0.01433   0.00802  -0.0569   0.0752   1.0000
   8.250   1.0753   0.01526   0.00879  -0.0539   0.0488   1.0000
   8.500   1.0887   0.01592   0.00940  -0.0519   0.0406   1.0000
   8.750   1.1040   0.01650   0.00998  -0.0503   0.0377   1.0000
   9.000   1.1185   0.01715   0.01063  -0.0486   0.0351   1.0000
   9.250   1.1343   0.01774   0.01125  -0.0471   0.0339   1.0000
   9.500   1.1505   0.01833   0.01187  -0.0457   0.0327   1.0000
   9.750   1.1657   0.01899   0.01256  -0.0443   0.0318   1.0000
  10.000   1.1793   0.01976   0.01335  -0.0428   0.0303   1.0000
  10.250   1.1911   0.02066   0.01428  -0.0410   0.0293   1.0000
  10.500   1.2026   0.02162   0.01529  -0.0394   0.0284   1.0000
  10.750   1.2176   0.02237   0.01608  -0.0382   0.0279   1.0000
  11.000   1.2313   0.02321   0.01697  -0.0369   0.0273   1.0000
  11.250   1.2444   0.02412   0.01792  -0.0356   0.0266   1.0000
  11.500   1.2571   0.02508   0.01891  -0.0344   0.0258   1.0000
  11.750   1.2685   0.02614   0.02000  -0.0331   0.0250   1.0000
  12.000   1.2759   0.02752   0.02142  -0.0315   0.0243   1.0000
  12.250   1.2766   0.02945   0.02343  -0.0295   0.0236   1.0000
  12.500   1.2893   0.03052   0.02455  -0.0285   0.0232   1.0000
  12.750   1.3037   0.03148   0.02555  -0.0278   0.0226   1.0000
  13.000   1.3152   0.03267   0.02679  -0.0269   0.0220   1.0000
  13.250   1.3250   0.03405   0.02821  -0.0259   0.0214   1.0000
  13.500   1.3348   0.03545   0.02965  -0.0250   0.0209   1.0000
  13.750   1.3435   0.03698   0.03122  -0.0242   0.0204   1.0000
  14.000   1.3472   0.03899   0.03327  -0.0231   0.0199   1.0000
  14.250   1.3420   0.04185   0.03622  -0.0218   0.0193   1.0000
  14.500   1.3540   0.04321   0.03763  -0.0213   0.0190   1.0000
  14.750   1.3634   0.04483   0.03931  -0.0208   0.0186   1.0000
  15.000   1.3722   0.04653   0.04107  -0.0204   0.0181   1.0000
  15.250   1.3799   0.04835   0.04294  -0.0200   0.0177   1.0000
  15.500   1.3863   0.05034   0.04498  -0.0195   0.0172   1.0000
  15.750   1.3910   0.05254   0.04724  -0.0192   0.0169   1.0000
  16.000   1.3973   0.05460   0.04933  -0.0189   0.0164   1.0000
  16.250   1.3973   0.05739   0.05217  -0.0186   0.0160   1.0000
  16.500   1.3889   0.06110   0.05597  -0.0183   0.0156   1.0000
  16.750   1.3967   0.06311   0.05805  -0.0183   0.0154   1.0000
  17.000   1.4010   0.06554   0.06055  -0.0183   0.0150   1.0000
  17.250   1.4031   0.06824   0.06333  -0.0183   0.0148   1.0000
  17.500   1.4042   0.07110   0.06626  -0.0185   0.0145   1.0000
  17.750   1.4075   0.07370   0.06893  -0.0187   0.0142   1.0000
  18.000   1.4083   0.07664   0.07193  -0.0189   0.0139   1.0000
  18.250   1.4084   0.07971   0.07507  -0.0193   0.0137   1.0000
  18.500   1.4083   0.08287   0.07828  -0.0198   0.0134   1.0000
  18.750   1.4043   0.08653   0.08201  -0.0204   0.0131   1.0000
  19.000   1.3964   0.09071   0.08626  -0.0211   0.0128   1.0000
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