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FX 71-L-150/25 AIRFOIL (fx711525-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 71-L-150/25 AIRFOIL (fx711525-il)
Reynolds number: 1,000,000
Max Cl/Cd: 57.39 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx711525-il-1000000-n5.txt
Download as CSV file: xf-fx711525-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 71-L-150/25 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  -1.0851   0.12879   0.12564   0.0076   1.0000   0.0091
 -19.500  -1.0965   0.12246   0.11920   0.0040   1.0000   0.0091
 -19.250  -1.1068   0.11635   0.11299   0.0007   1.0000   0.0091
 -19.000  -1.1155   0.11073   0.10729  -0.0024   1.0000   0.0092
 -18.750  -1.1253   0.10502   0.10147  -0.0054   1.0000   0.0091
 -18.500  -1.1346   0.09953   0.09589  -0.0081   1.0000   0.0092
 -18.250  -1.1432   0.09427   0.09052  -0.0107   1.0000   0.0091
 -18.000  -1.1514   0.08921   0.08536  -0.0131   1.0000   0.0091
 -17.750  -1.1571   0.08461   0.08068  -0.0152   1.0000   0.0091
 -17.500  -1.1641   0.07995   0.07593  -0.0172   1.0000   0.0092
 -17.250  -1.1687   0.07573   0.07162  -0.0190   1.0000   0.0092
 -17.000  -1.1735   0.07162   0.06742  -0.0206   1.0000   0.0092
 -16.750  -1.1768   0.06777   0.06348  -0.0221   1.0000   0.0092
 -16.500  -1.1791   0.06414   0.05976  -0.0234   1.0000   0.0092
 -16.250  -1.1812   0.06065   0.05620  -0.0245   1.0000   0.0092
 -16.000  -1.1818   0.05744   0.05290  -0.0254   1.0000   0.0092
 -15.750  -1.1835   0.05432   0.04971  -0.0258   0.9864   0.0092
 -15.500  -1.1415   0.04982   0.04502  -0.0368   0.9187   0.0092
 -15.250  -1.1357   0.04761   0.04243  -0.0377   0.8213   0.0093
 -14.750  -1.1321   0.04299   0.03757  -0.0377   0.8018   0.0093
 -14.500  -1.1283   0.04095   0.03544  -0.0376   0.7972   0.0093
 -14.250  -1.1248   0.03895   0.03335  -0.0373   0.7931   0.0094
 -14.000  -1.1199   0.03713   0.03145  -0.0370   0.7893   0.0094
 -13.750  -1.1157   0.03527   0.02953  -0.0365   0.7866   0.0094
 -13.500  -1.1095   0.03366   0.02785  -0.0359   0.7836   0.0095
 -13.250  -1.1038   0.03205   0.02617  -0.0352   0.7806   0.0095
 -13.000  -1.0964   0.03063   0.02468  -0.0345   0.7777   0.0095
 -12.750  -1.0893   0.02924   0.02322  -0.0336   0.7749   0.0095
 -12.500  -1.0820   0.02787   0.02180  -0.0326   0.7725   0.0095
 -12.250  -1.0738   0.02661   0.02048  -0.0316   0.7699   0.0095
 -12.000  -1.0644   0.02546   0.01929  -0.0305   0.7668   0.0096
 -11.750  -1.0550   0.02436   0.01814  -0.0294   0.7635   0.0096
 -11.500  -1.0461   0.02327   0.01699  -0.0281   0.7600   0.0096
 -11.250  -1.0378   0.02218   0.01584  -0.0267   0.7568   0.0096
 -11.000  -1.0271   0.02125   0.01487  -0.0254   0.7532   0.0097
 -10.750  -1.0181   0.02033   0.01390  -0.0237   0.7495   0.0097
 -10.500  -1.0081   0.01958   0.01309  -0.0219   0.7460   0.0097
 -10.250  -0.9989   0.01888   0.01234  -0.0196   0.7427   0.0098
 -10.000  -0.9886   0.01829   0.01170  -0.0172   0.7396   0.0098
  -9.750  -0.9768   0.01776   0.01113  -0.0149   0.7363   0.0098
  -9.500  -0.9602   0.01723   0.01057  -0.0135   0.7328   0.0099
  -9.250  -0.9417   0.01676   0.01005  -0.0122   0.7293   0.0100
  -9.000  -0.9225   0.01629   0.00955  -0.0111   0.7259   0.0101
  -8.750  -0.9025   0.01584   0.00905  -0.0101   0.7226   0.0102
  -8.500  -0.8813   0.01541   0.00860  -0.0092   0.7200   0.0102
  -8.250  -0.8596   0.01498   0.00814  -0.0084   0.7171   0.0103
  -8.000  -0.8372   0.01459   0.00772  -0.0077   0.7140   0.0103
  -7.750  -0.8142   0.01421   0.00732  -0.0070   0.7109   0.0104
  -7.500  -0.7908   0.01386   0.00693  -0.0064   0.7077   0.0104
  -7.250  -0.7670   0.01353   0.00656  -0.0059   0.7046   0.0105
  -7.000  -0.7426   0.01320   0.00622  -0.0054   0.7017   0.0106
  -6.750  -0.7177   0.01290   0.00590  -0.0050   0.6985   0.0107
  -6.500  -0.6926   0.01261   0.00559  -0.0046   0.6947   0.0108
  -6.250  -0.6671   0.01234   0.00530  -0.0043   0.6910   0.0108
  -6.000  -0.6417   0.01207   0.00501  -0.0039   0.6875   0.0110
  -5.750  -0.6161   0.01180   0.00471  -0.0036   0.6841   0.0112
  -5.500  -0.5899   0.01154   0.00445  -0.0033   0.6810   0.0115
  -5.250  -0.5635   0.01130   0.00420  -0.0031   0.6771   0.0119
  -5.000  -0.5369   0.01109   0.00398  -0.0029   0.6726   0.0122
  -4.750  -0.5102   0.01089   0.00376  -0.0027   0.6681   0.0126
  -4.500  -0.4833   0.01071   0.00356  -0.0026   0.6639   0.0131
  -4.250  -0.4562   0.01051   0.00337  -0.0024   0.6592   0.0143
  -4.000  -0.4296   0.01027   0.00317  -0.0022   0.6534   0.0242
  -3.750  -0.4026   0.01008   0.00299  -0.0021   0.6478   0.0296
  -3.500  -0.3764   0.00979   0.00278  -0.0019   0.6433   0.0498
  -3.250  -0.3505   0.00942   0.00256  -0.0016   0.6387   0.0813
  -2.750  -0.2984   0.00876   0.00216  -0.0012   0.6290   0.1501
  -2.500  -0.2740   0.00821   0.00190  -0.0008   0.6245   0.2225
  -2.250  -0.2498   0.00760   0.00164  -0.0004   0.6200   0.3071
  -2.000  -0.2251   0.00707   0.00143   0.0000   0.6146   0.3874
  -1.750  -0.1984   0.00681   0.00132   0.0001   0.6088   0.4332
  -1.500  -0.1710   0.00661   0.00125   0.0002   0.6031   0.4708
  -1.250  -0.1428   0.00652   0.00121   0.0002   0.5967   0.4950
  -1.000  -0.1144   0.00646   0.00118   0.0002   0.5907   0.5118
  -0.750  -0.0862   0.00638   0.00118   0.0002   0.5861   0.5358
  -0.500  -0.0574   0.00636   0.00118   0.0001   0.5814   0.5516
  -0.250  -0.0289   0.00633   0.00117   0.0001   0.5750   0.5612
   0.000   0.0000   0.00636   0.00116   0.0000   0.5683   0.5682
   0.250   0.0289   0.00633   0.00117  -0.0001   0.5614   0.5749
   0.500   0.0574   0.00636   0.00118  -0.0001   0.5515   0.5813
   0.750   0.0861   0.00639   0.00118  -0.0002   0.5345   0.5861
   1.000   0.1144   0.00646   0.00118  -0.0002   0.5112   0.5907
   1.250   0.1428   0.00652   0.00121  -0.0002   0.4943   0.5967
   1.500   0.1710   0.00662   0.00125  -0.0002   0.4703   0.6031
   1.750   0.1983   0.00682   0.00132  -0.0001   0.4310   0.6088
   2.000   0.2250   0.00708   0.00144   0.0000   0.3856   0.6146
   2.250   0.2497   0.00762   0.00165   0.0004   0.3035   0.6200
   2.500   0.2741   0.00820   0.00190   0.0008   0.2231   0.6245
   2.750   0.2982   0.00878   0.00217   0.0012   0.1471   0.6290
   3.000   0.3244   0.00909   0.00236   0.0014   0.1131   0.6339
   3.250   0.3505   0.00942   0.00256   0.0016   0.0814   0.6387
   3.500   0.3764   0.00979   0.00278   0.0019   0.0495   0.6432
   3.750   0.4025   0.01009   0.00300   0.0021   0.0289   0.6478
   4.000   0.4296   0.01027   0.00317   0.0022   0.0240   0.6534
   4.250   0.4562   0.01052   0.00338   0.0024   0.0141   0.6592
   4.500   0.4833   0.01071   0.00356   0.0026   0.0131   0.6639
   4.750   0.5102   0.01089   0.00376   0.0027   0.0126   0.6681
   5.000   0.5369   0.01109   0.00397   0.0029   0.0122   0.6726
   5.250   0.5636   0.01130   0.00420   0.0031   0.0119   0.6771
   5.500   0.5899   0.01154   0.00445   0.0033   0.0115   0.6810
   5.750   0.6162   0.01179   0.00470   0.0036   0.0113   0.6841
   6.000   0.6417   0.01206   0.00501   0.0039   0.0110   0.6875
   6.250   0.6672   0.01233   0.00530   0.0043   0.0109   0.6910
   6.500   0.6926   0.01260   0.00559   0.0046   0.0108   0.6946
   6.750   0.7178   0.01289   0.00590   0.0050   0.0107   0.6984
   7.000   0.7426   0.01320   0.00622   0.0054   0.0106   0.7018
   7.250   0.7670   0.01353   0.00657   0.0059   0.0105   0.7046
   7.500   0.7909   0.01386   0.00693   0.0064   0.0105   0.7077
   7.750   0.8143   0.01421   0.00731   0.0070   0.0104   0.7108
   8.000   0.8372   0.01459   0.00772   0.0077   0.0103   0.7140
   8.250   0.8597   0.01498   0.00814   0.0084   0.0103   0.7171
   8.500   0.8814   0.01540   0.00859   0.0092   0.0102   0.7199
   8.750   0.9025   0.01585   0.00906   0.0101   0.0102   0.7226
   9.000   0.9229   0.01627   0.00952   0.0111   0.0101   0.7259
   9.250   0.9420   0.01675   0.01004   0.0122   0.0100   0.7293
   9.500   0.9600   0.01725   0.01059   0.0135   0.0100   0.7328
   9.750   0.9769   0.01776   0.01113   0.0149   0.0098   0.7363
  10.000   0.9893   0.01827   0.01168   0.0171   0.0098   0.7396
  10.250   0.9991   0.01888   0.01234   0.0195   0.0098   0.7427
  10.500   1.0089   0.01955   0.01306   0.0217   0.0098   0.7459
  10.750   1.0177   0.02036   0.01393   0.0237   0.0097   0.7495
  11.000   1.0280   0.02122   0.01483   0.0253   0.0097   0.7532
  11.250   1.0376   0.02220   0.01586   0.0267   0.0097   0.7568
  11.500   1.0478   0.02318   0.01689   0.0279   0.0096   0.7600
  11.750   1.0561   0.02430   0.01808   0.0293   0.0096   0.7635
  12.000   1.0663   0.02534   0.01917   0.0304   0.0096   0.7669
  12.250   1.0749   0.02655   0.02042   0.0315   0.0095   0.7699
  12.500   1.0819   0.02791   0.02183   0.0326   0.0096   0.7725
  12.750   1.0922   0.02905   0.02302   0.0334   0.0095   0.7749
  13.000   1.0993   0.03043   0.02448   0.0343   0.0095   0.7777
  13.250   1.1048   0.03200   0.02612   0.0352   0.0094   0.7807
  13.500   1.1106   0.03359   0.02778   0.0359   0.0095   0.7837
  13.750   1.1170   0.03519   0.02944   0.0364   0.0094   0.7866
  14.000   1.1217   0.03701   0.03133   0.0369   0.0094   0.7893
  14.250   1.1263   0.03884   0.03324   0.0372   0.0094   0.7931
  14.500   1.1306   0.04077   0.03525   0.0375   0.0093   0.7973
  14.750   1.1333   0.04291   0.03749   0.0376   0.0093   0.8018
  15.250   1.1384   0.04736   0.04217   0.0376   0.0093   0.8220
  15.500   1.1417   0.04979   0.04500   0.0369   0.0093   0.9174
  15.750   1.1827   0.05422   0.04960   0.0263   0.0092   0.9987
  16.000   1.1843   0.05731   0.05278   0.0252   0.0092   1.0000
  16.250   1.1838   0.06053   0.05608   0.0242   0.0092   1.0000
  16.500   1.1820   0.06399   0.05962   0.0231   0.0092   1.0000
  16.750   1.1808   0.06749   0.06319   0.0218   0.0092   1.0000
  17.000   1.1762   0.07150   0.06729   0.0203   0.0092   1.0000
  17.250   1.1710   0.07566   0.07155   0.0187   0.0092   1.0000
  17.500   1.1662   0.07991   0.07588   0.0169   0.0091   1.0000
  17.750   1.1605   0.08441   0.08048   0.0149   0.0091   1.0000
  18.000   1.1534   0.08917   0.08533   0.0128   0.0092   1.0000
  18.250   1.1460   0.09413   0.09039   0.0104   0.0092   1.0000
  18.500   1.1376   0.09935   0.09570   0.0079   0.0091   1.0000
  18.750   1.1288   0.10479   0.10123   0.0051   0.0091   1.0000
  19.000   1.1197   0.11031   0.10684   0.0023   0.0091   1.0000
  19.250   1.1098   0.11615   0.11277  -0.0009   0.0091   1.0000
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