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GOE 625 AIRFOIL (goe625-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 625 AIRFOIL (goe625-il)
Reynolds number: 500,000
Max Cl/Cd: 80.79 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe625-il-500000.txt
Download as CSV file: xf-goe625-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 625 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.8189   0.05869   0.05522  -0.1082   0.9979   0.0487
 -16.000  -0.8317   0.05027   0.04663  -0.1181   0.9944   0.0493
 -15.750  -0.8301   0.04396   0.04016  -0.1269   0.9911   0.0499
 -15.500  -0.8239   0.03905   0.03508  -0.1342   0.9855   0.0507
 -15.250  -0.8145   0.03509   0.03091  -0.1403   0.9803   0.0515
 -15.000  -0.8097   0.03212   0.02771  -0.1434   0.9704   0.0523
 -14.750  -0.8025   0.03006   0.02549  -0.1444   0.9612   0.0530
 -14.500  -0.7904   0.02904   0.02444  -0.1438   0.9521   0.0537
 -14.250  -0.7782   0.02834   0.02372  -0.1426   0.9426   0.0543
 -14.000  -0.7670   0.02771   0.02302  -0.1409   0.9338   0.0550
 -13.750  -0.7581   0.02715   0.02238  -0.1387   0.9239   0.0557
 -13.500  -0.7454   0.02646   0.02154  -0.1371   0.9163   0.0568
 -13.250  -0.7328   0.02571   0.02060  -0.1356   0.9079   0.0578
 -13.000  -0.7178   0.02490   0.01966  -0.1343   0.9007   0.0588
 -12.750  -0.6967   0.02456   0.01933  -0.1335   0.8944   0.0596
 -12.500  -0.6752   0.02427   0.01903  -0.1327   0.8876   0.0605
 -12.250  -0.6543   0.02390   0.01858  -0.1318   0.8815   0.0615
 -12.000  -0.6340   0.02343   0.01796  -0.1309   0.8753   0.0628
 -11.750  -0.6138   0.02297   0.01732  -0.1300   0.8686   0.0640
 -11.500  -0.5928   0.02219   0.01647  -0.1293   0.8629   0.0651
 -11.250  -0.5684   0.02188   0.01617  -0.1288   0.8573   0.0661
 -11.000  -0.5441   0.02162   0.01590  -0.1283   0.8507   0.0672
 -10.750  -0.5205   0.02129   0.01546  -0.1277   0.8442   0.0686
 -10.500  -0.4968   0.02096   0.01497  -0.1271   0.8381   0.0699
 -10.250  -0.4733   0.02057   0.01443  -0.1265   0.8320   0.0710
 -10.000  -0.4490   0.01973   0.01362  -0.1262   0.8265   0.0723
  -9.750  -0.4230   0.01940   0.01325  -0.1260   0.8215   0.0734
  -9.500  -0.3973   0.01908   0.01290  -0.1257   0.8163   0.0747
  -9.250  -0.3715   0.01875   0.01250  -0.1254   0.8106   0.0761
  -9.000  -0.3455   0.01849   0.01210  -0.1250   0.8053   0.0774
  -8.750  -0.3198   0.01796   0.01143  -0.1247   0.8002   0.0786
  -8.500  -0.2941   0.01730   0.01082  -0.1245   0.7943   0.0798
  -8.250  -0.2674   0.01694   0.01045  -0.1243   0.7882   0.0810
  -8.000  -0.2404   0.01666   0.01009  -0.1241   0.7824   0.0824
  -7.750  -0.2136   0.01635   0.00974  -0.1239   0.7760   0.0837
  -7.500  -0.1865   0.01608   0.00938  -0.1237   0.7692   0.0850
  -7.250  -0.1588   0.01591   0.00907  -0.1235   0.7631   0.0859
  -7.000  -0.1331   0.01514   0.00834  -0.1233   0.7565   0.0876
  -6.750  -0.1060   0.01482   0.00801  -0.1232   0.7492   0.0890
  -6.500  -0.0786   0.01458   0.00771  -0.1230   0.7425   0.0904
  -6.250  -0.0512   0.01430   0.00742  -0.1228   0.7345   0.0917
  -6.000  -0.0238   0.01406   0.00709  -0.1226   0.7264   0.0928
  -5.750   0.0038   0.01385   0.00682  -0.1225   0.7179   0.0939
  -5.500   0.0306   0.01351   0.00642  -0.1222   0.7085   0.0951
  -5.250   0.0571   0.01315   0.00605  -0.1219   0.6987   0.0965
  -5.000   0.0837   0.01294   0.00579  -0.1216   0.6873   0.0978
  -4.750   0.1106   0.01276   0.00559  -0.1213   0.6745   0.0993
  -4.500   0.1372   0.01263   0.00538  -0.1210   0.6605   0.1009
  -4.250   0.1634   0.01252   0.00518  -0.1206   0.6446   0.1023
  -4.000   0.1893   0.01245   0.00500  -0.1201   0.6267   0.1035
  -3.750   0.2141   0.01230   0.00479  -0.1194   0.6066   0.1055
  -3.500   0.2387   0.01227   0.00467  -0.1188   0.5849   0.1076
  -3.250   0.2632   0.01230   0.00460  -0.1180   0.5635   0.1101
  -3.000   0.2878   0.01236   0.00454  -0.1174   0.5446   0.1128
  -2.750   0.3123   0.01237   0.00448  -0.1167   0.5291   0.1161
  -2.500   0.3368   0.01243   0.00447  -0.1161   0.5163   0.1204
  -2.250   0.3630   0.01245   0.00445  -0.1157   0.5062   0.1258
  -2.000   0.3879   0.01251   0.00448  -0.1151   0.4974   0.1341
  -1.750   0.4146   0.01250   0.00450  -0.1149   0.4905   0.1446
  -1.500   0.4405   0.01256   0.00454  -0.1145   0.4838   0.1556
  -1.250   0.4663   0.01269   0.00461  -0.1141   0.4781   0.1650
  -1.000   0.4933   0.01267   0.00464  -0.1140   0.4738   0.1735
  -0.750   0.5200   0.01274   0.00469  -0.1138   0.4694   0.1806
  -0.500   0.5461   0.01280   0.00472  -0.1135   0.4654   0.1872
  -0.250   0.5718   0.01290   0.00479  -0.1131   0.4614   0.1941
   0.000   0.5987   0.01299   0.00486  -0.1130   0.4583   0.2001
   0.250   0.6256   0.01298   0.00490  -0.1129   0.4555   0.2079
   0.500   0.6522   0.01301   0.00495  -0.1127   0.4524   0.2162
   0.750   0.6785   0.01305   0.00501  -0.1125   0.4493   0.2262
   1.250   0.7306   0.01316   0.00520  -0.1120   0.4434   0.2663
   1.500   0.7569   0.01306   0.00537  -0.1121   0.4404   0.3588
   1.750   0.7810   0.01265   0.00552  -0.1117   0.4383   0.5314
   2.000   0.8011   0.01212   0.00574  -0.1103   0.4355   0.7591
   2.250   0.8175   0.01195   0.00598  -0.1073   0.4326   0.9119
   2.500   0.8591   0.01215   0.00617  -0.1101   0.4291   0.9807
   2.750   0.9049   0.01244   0.00636  -0.1141   0.4253   1.0000
   3.000   0.9275   0.01268   0.00651  -0.1132   0.4217   1.0000
   3.250   0.9482   0.01277   0.00661  -0.1119   0.4199   1.0000
   3.500   0.9703   0.01290   0.00672  -0.1109   0.4179   1.0000
   3.750   0.9931   0.01305   0.00685  -0.1101   0.4158   1.0000
   4.000   1.0153   0.01321   0.00699  -0.1091   0.4135   1.0000
   4.250   1.0370   0.01337   0.00713  -0.1081   0.4111   1.0000
   4.500   1.0590   0.01357   0.00729  -0.1072   0.4087   1.0000
   4.750   1.0830   0.01382   0.00748  -0.1067   0.4061   1.0000
   5.000   1.1109   0.01413   0.00772  -0.1070   0.4033   1.0000
   5.250   1.1315   0.01429   0.00791  -0.1058   0.4018   1.0000
   5.500   1.1530   0.01447   0.00811  -0.1048   0.3999   1.0000
   5.750   1.1750   0.01467   0.00833  -0.1040   0.3977   1.0000
   6.000   1.1972   0.01488   0.00854  -0.1032   0.3954   1.0000
   6.250   1.2191   0.01511   0.00876  -0.1024   0.3930   1.0000
   6.500   1.2409   0.01536   0.00900  -0.1016   0.3904   1.0000
   6.750   1.2642   0.01567   0.00925  -0.1012   0.3876   1.0000
   7.000   1.2890   0.01598   0.00954  -0.1010   0.3847   1.0000
   7.250   1.3084   0.01623   0.00985  -0.0999   0.3827   1.0000
   7.500   1.3285   0.01650   0.01016  -0.0989   0.3802   1.0000
   7.750   1.3482   0.01680   0.01047  -0.0979   0.3772   1.0000
   8.000   1.3677   0.01711   0.01080  -0.0969   0.3742   1.0000
   8.250   1.3874   0.01747   0.01113  -0.0960   0.3711   1.0000
   8.500   1.4096   0.01787   0.01148  -0.0955   0.3674   1.0000
   8.750   1.4273   0.01824   0.01194  -0.0944   0.3650   1.0000
   9.000   1.4455   0.01865   0.01239  -0.0934   0.3618   1.0000
   9.250   1.4633   0.01908   0.01285  -0.0924   0.3581   1.0000
   9.500   1.4801   0.01958   0.01335  -0.0913   0.3541   1.0000
   9.750   1.4969   0.02015   0.01389  -0.0902   0.3498   1.0000
  10.000   1.5142   0.02067   0.01449  -0.0893   0.3458   1.0000
  10.250   1.5312   0.02124   0.01510  -0.0884   0.3413   1.0000
  10.500   1.5462   0.02192   0.01578  -0.0873   0.3367   1.0000
  10.750   1.5610   0.02266   0.01652  -0.0862   0.3323   1.0000
  11.000   1.5780   0.02330   0.01723  -0.0854   0.3272   1.0000
  11.250   1.5916   0.02414   0.01808  -0.0843   0.3215   1.0000
  11.500   1.6035   0.02510   0.01904  -0.0831   0.3161   1.0000
  11.750   1.6180   0.02595   0.01994  -0.0822   0.3098   1.0000
  12.000   1.6274   0.02713   0.02111  -0.0808   0.3033   1.0000
  12.250   1.6391   0.02822   0.02222  -0.0797   0.2969   1.0000
  12.500   1.6475   0.02958   0.02357  -0.0784   0.2897   1.0000
  12.750   1.6549   0.03102   0.02501  -0.0771   0.2829   1.0000
  13.000   1.6620   0.03254   0.02654  -0.0759   0.2758   1.0000
  13.250   1.6651   0.03440   0.02838  -0.0744   0.2694   1.0000
  13.500   1.6738   0.03588   0.02990  -0.0735   0.2636   1.0000
  13.750   1.6773   0.03782   0.03183  -0.0722   0.2583   1.0000
  14.000   1.6815   0.03971   0.03373  -0.0711   0.2537   1.0000
  14.250   1.6892   0.04137   0.03545  -0.0703   0.2496   1.0000
  14.500   1.6930   0.04340   0.03750  -0.0693   0.2453   1.0000
  14.750   1.6943   0.04567   0.03977  -0.0682   0.2414   1.0000
  15.000   1.6992   0.04768   0.04183  -0.0675   0.2382   1.0000
  15.250   1.7059   0.04954   0.04377  -0.0669   0.2351   1.0000
  15.500   1.7089   0.05178   0.04606  -0.0662   0.2318   1.0000
  15.750   1.7096   0.05427   0.04857  -0.0654   0.2287   1.0000
  16.000   1.7087   0.05691   0.05121  -0.0647   0.2254   1.0000
  16.250   1.7131   0.05915   0.05355  -0.0643   0.2229   1.0000
  16.500   1.7169   0.06145   0.05593  -0.0640   0.2201   1.0000
  16.750   1.7172   0.06413   0.05868  -0.0636   0.2171   1.0000
  17.000   1.7156   0.06703   0.06161  -0.0632   0.2143   1.0000
  17.250   1.7134   0.06996   0.06454  -0.0628   0.2112   1.0000
  17.500   1.7143   0.07270   0.06738  -0.0626   0.2088   1.0000
  17.750   1.7148   0.07551   0.07029  -0.0626   0.2060   1.0000
  18.000   1.7132   0.07854   0.07339  -0.0625   0.2031   1.0000
  18.250   1.7097   0.08180   0.07669  -0.0625   0.2002   1.0000
  18.500   1.7064   0.08500   0.07990  -0.0625   0.1973   1.0000
  18.750   1.7049   0.08810   0.08309  -0.0626   0.1948   1.0000
  19.000   1.7038   0.09118   0.08628  -0.0629   0.1919   1.0000
  19.250   1.6989   0.09474   0.08991  -0.0632   0.1884   1.0000
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