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FX 71-L-150/30 AIRFOIL (fx71l150-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 71-L-150/30 AIRFOIL (fx71l150-il)
Reynolds number: 1,000,000
Max Cl/Cd: 58.27 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx71l150-il-1000000-n5.txt
Download as CSV file: xf-fx71l150-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 71-L-150/30 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
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -1.0867   0.12368   0.12051   0.0041   1.0000   0.0090
 -19.250  -1.0969   0.11770   0.11443   0.0008   1.0000   0.0090
 -19.000  -1.1086   0.11157   0.10819  -0.0024   1.0000   0.0090
 -18.750  -1.1193   0.10579   0.10232  -0.0053   1.0000   0.0090
 -18.500  -1.1295   0.10019   0.09662  -0.0081   1.0000   0.0090
 -18.250  -1.1401   0.09467   0.09099  -0.0107   1.0000   0.0090
 -18.000  -1.1484   0.08967   0.08589  -0.0130   1.0000   0.0089
 -17.750  -1.1573   0.08464   0.08077  -0.0152   1.0000   0.0090
 -17.500  -1.1651   0.07990   0.07593  -0.0172   1.0000   0.0090
 -17.250  -1.1704   0.07564   0.07157  -0.0189   1.0000   0.0090
 -17.000  -1.1753   0.07150   0.06735  -0.0205   1.0000   0.0090
 -16.750  -1.1800   0.06748   0.06324  -0.0220   1.0000   0.0090
 -16.500  -1.1827   0.06385   0.05952  -0.0233   1.0000   0.0090
 -16.250  -1.1846   0.06040   0.05598  -0.0244   1.0000   0.0090
 -16.000  -1.1860   0.05707   0.05257  -0.0254   1.0000   0.0090
 -15.750  -1.1879   0.05378   0.04920  -0.0262   1.0000   0.0090
 -15.500  -1.1865   0.05096   0.04630  -0.0269   1.0000   0.0090
 -15.250  -1.1833   0.04809   0.04335  -0.0279   0.9985   0.0090
 -15.000  -1.1324   0.04387   0.03889  -0.0402   0.8992   0.0091
 -14.750  -1.1338   0.04214   0.03671  -0.0390   0.7860   0.0091
 -14.500  -1.1318   0.04007   0.03452  -0.0387   0.7721   0.0091
 -14.000  -1.1250   0.03624   0.03049  -0.0379   0.7533   0.0092
 -13.500  -1.1150   0.03287   0.02696  -0.0367   0.7446   0.0092
 -13.250  -1.1105   0.03121   0.02522  -0.0359   0.7417   0.0094
 -13.000  -1.1033   0.02980   0.02374  -0.0351   0.7389   0.0094
 -12.750  -1.0965   0.02842   0.02228  -0.0341   0.7360   0.0093
 -12.250  -1.0810   0.02587   0.01961  -0.0321   0.7307   0.0094
 -12.000  -1.0727   0.02466   0.01834  -0.0310   0.7280   0.0095
 -11.750  -1.0638   0.02353   0.01715  -0.0298   0.7258   0.0095
 -11.500  -1.0550   0.02246   0.01602  -0.0285   0.7236   0.0095
 -11.250  -1.0458   0.02150   0.01500  -0.0271   0.7215   0.0096
 -11.000  -1.0369   0.02062   0.01405  -0.0254   0.7195   0.0097
 -10.750  -1.0279   0.01980   0.01319  -0.0234   0.7175   0.0097
 -10.500  -1.0189   0.01908   0.01243  -0.0212   0.7153   0.0098
 -10.250  -1.0086   0.01849   0.01180  -0.0188   0.7129   0.0099
 -10.000  -0.9980   0.01797   0.01124  -0.0163   0.7106   0.0099
  -9.750  -0.9827   0.01748   0.01070  -0.0146   0.7085   0.0100
  -9.500  -0.9649   0.01701   0.01019  -0.0133   0.7066   0.0101
  -9.250  -0.9458   0.01653   0.00969  -0.0121   0.7043   0.0102
  -9.000  -0.9256   0.01610   0.00923  -0.0111   0.7017   0.0102
  -8.750  -0.9046   0.01568   0.00879  -0.0102   0.6990   0.0103
  -8.500  -0.8829   0.01529   0.00837  -0.0094   0.6964   0.0103
  -8.250  -0.8609   0.01490   0.00794  -0.0086   0.6937   0.0104
  -8.000  -0.8393   0.01443   0.00744  -0.0077   0.6906   0.0106
  -7.750  -0.8166   0.01402   0.00701  -0.0070   0.6872   0.0107
  -7.500  -0.7931   0.01366   0.00662  -0.0064   0.6834   0.0109
  -7.250  -0.7693   0.01332   0.00624  -0.0058   0.6799   0.0111
  -7.000  -0.7448   0.01301   0.00591  -0.0054   0.6766   0.0112
  -6.750  -0.7199   0.01272   0.00560  -0.0049   0.6735   0.0114
  -6.500  -0.6947   0.01245   0.00531  -0.0045   0.6702   0.0115
  -6.250  -0.6692   0.01220   0.00503  -0.0042   0.6673   0.0117
  -6.000  -0.6434   0.01197   0.00477  -0.0039   0.6647   0.0119
  -5.750  -0.6172   0.01174   0.00453  -0.0036   0.6622   0.0121
  -5.500  -0.5909   0.01151   0.00430  -0.0034   0.6593   0.0124
  -5.250  -0.5643   0.01131   0.00409  -0.0032   0.6563   0.0127
  -5.000  -0.5376   0.01112   0.00389  -0.0030   0.6533   0.0130
  -4.750  -0.5111   0.01092   0.00368  -0.0028   0.6504   0.0142
  -4.500  -0.4849   0.01063   0.00345  -0.0025   0.6477   0.0249
  -4.250  -0.4581   0.01040   0.00326  -0.0024   0.6442   0.0309
  -4.000  -0.4322   0.01007   0.00303  -0.0021   0.6403   0.0504
  -3.750  -0.4062   0.00975   0.00281  -0.0018   0.6363   0.0724
  -3.500  -0.3796   0.00948   0.00262  -0.0016   0.6321   0.0924
  -3.250  -0.3544   0.00905   0.00237  -0.0013   0.6268   0.1352
  -3.000  -0.3284   0.00870   0.00216  -0.0011   0.6209   0.1726
  -2.750  -0.3029   0.00831   0.00195  -0.0008   0.6161   0.2201
  -2.500  -0.2768   0.00795   0.00177  -0.0006   0.6119   0.2684
  -2.250  -0.2511   0.00754   0.00158  -0.0003   0.6076   0.3246
  -2.000  -0.2249   0.00721   0.00143  -0.0001   0.6036   0.3727
  -1.750  -0.1980   0.00696   0.00132   0.0000   0.5995   0.4153
  -1.500  -0.1710   0.00671   0.00124   0.0002   0.5957   0.4620
  -1.250  -0.1434   0.00654   0.00120   0.0003   0.5899   0.4969
  -1.000  -0.1152   0.00647   0.00118   0.0003   0.5831   0.5222
  -0.750  -0.0866   0.00643   0.00117   0.0002   0.5776   0.5370
  -0.500  -0.0578   0.00639   0.00116   0.0002   0.5719   0.5464
  -0.250  -0.0290   0.00639   0.00115   0.0001   0.5649   0.5536
   0.000   0.0000   0.00640   0.00114   0.0000   0.5585   0.5586
   0.250   0.0290   0.00639   0.00115  -0.0001   0.5537   0.5647
   0.500   0.0578   0.00639   0.00116  -0.0002   0.5468   0.5722
   0.750   0.0866   0.00643   0.00117  -0.0002   0.5368   0.5778
   1.000   0.1152   0.00647   0.00118  -0.0003   0.5218   0.5831
   1.250   0.1433   0.00654   0.00120  -0.0003   0.4953   0.5899
   1.500   0.1708   0.00673   0.00124  -0.0002   0.4592   0.5957
   1.750   0.1980   0.00696   0.00132   0.0000   0.4156   0.5996
   2.000   0.2248   0.00721   0.00144   0.0001   0.3714   0.6036
   2.250   0.2509   0.00757   0.00159   0.0003   0.3199   0.6076
   2.500   0.2768   0.00795   0.00177   0.0006   0.2673   0.6119
   2.750   0.3028   0.00832   0.00195   0.0008   0.2193   0.6161
   3.000   0.3286   0.00868   0.00216   0.0010   0.1759   0.6209
   3.250   0.3545   0.00904   0.00237   0.0013   0.1368   0.6267
   3.500   0.3797   0.00947   0.00261   0.0016   0.0935   0.6320
   3.750   0.4061   0.00975   0.00281   0.0018   0.0719   0.6363
   4.000   0.4321   0.01008   0.00303   0.0021   0.0494   0.6403
   4.250   0.4580   0.01040   0.00326   0.0024   0.0306   0.6442
   4.500   0.4849   0.01063   0.00345   0.0025   0.0240   0.6477
   4.750   0.5110   0.01093   0.00369   0.0028   0.0140   0.6504
   5.000   0.5376   0.01112   0.00389   0.0030   0.0129   0.6533
   5.250   0.5643   0.01131   0.00409   0.0032   0.0126   0.6563
   5.500   0.5909   0.01152   0.00430   0.0034   0.0124   0.6593
   5.750   0.6173   0.01173   0.00453   0.0036   0.0121   0.6622
   6.000   0.6435   0.01197   0.00477   0.0039   0.0119   0.6647
   6.250   0.6693   0.01220   0.00503   0.0042   0.0117   0.6673
   6.500   0.6947   0.01245   0.00530   0.0045   0.0115   0.6703
   6.750   0.7199   0.01272   0.00560   0.0049   0.0114   0.6736
   7.000   0.7448   0.01302   0.00592   0.0054   0.0112   0.6767
   7.250   0.7694   0.01332   0.00624   0.0058   0.0111   0.6798
   7.500   0.7933   0.01366   0.00661   0.0064   0.0109   0.6833
   7.750   0.8167   0.01402   0.00700   0.0070   0.0108   0.6872
   8.000   0.8396   0.01441   0.00743   0.0077   0.0106   0.6907
   8.250   0.8612   0.01488   0.00792   0.0085   0.0104   0.6937
   8.500   0.8830   0.01529   0.00836   0.0094   0.0103   0.6963
   8.750   0.9046   0.01569   0.00879   0.0102   0.0103   0.6990
   9.000   0.9257   0.01610   0.00923   0.0111   0.0102   0.7017
   9.250   0.9456   0.01655   0.00971   0.0121   0.0102   0.7043
   9.500   0.9648   0.01702   0.01020   0.0133   0.0101   0.7066
   9.750   0.9825   0.01750   0.01072   0.0146   0.0101   0.7085
  10.000   0.9981   0.01798   0.01124   0.0163   0.0100   0.7106
  10.250   1.0090   0.01849   0.01180   0.0188   0.0099   0.7129
  10.500   1.0187   0.01910   0.01245   0.0212   0.0098   0.7153
  10.750   1.0286   0.01978   0.01317   0.0233   0.0099   0.7175
  11.000   1.0375   0.02060   0.01403   0.0253   0.0097   0.7195
  11.250   1.0463   0.02149   0.01498   0.0270   0.0097   0.7215
  11.500   1.0558   0.02243   0.01599   0.0284   0.0096   0.7236
  11.750   1.0645   0.02351   0.01713   0.0297   0.0095   0.7257
  12.000   1.0739   0.02460   0.01827   0.0309   0.0096   0.7280
  12.250   1.0823   0.02581   0.01954   0.0320   0.0094   0.7306
  12.750   1.0977   0.02836   0.02222   0.0341   0.0093   0.7361
  13.000   1.1041   0.02978   0.02372   0.0350   0.0093   0.7389
  13.250   1.1104   0.03125   0.02526   0.0359   0.0092   0.7418
  13.500   1.1164   0.03279   0.02687   0.0366   0.0093   0.7446
  14.000   1.1254   0.03624   0.03049   0.0378   0.0092   0.7537
  14.500   1.1333   0.03997   0.03441   0.0386   0.0092   0.7731
  14.750   1.1346   0.04210   0.03668   0.0390   0.0091   0.7870
  15.000   1.1364   0.04387   0.03893   0.0394   0.0091   0.9122
  15.250   1.1868   0.04795   0.04320   0.0276   0.0091   0.9988
  15.500   1.1896   0.05085   0.04618   0.0266   0.0090   1.0000
  15.750   1.1898   0.05380   0.04922   0.0259   0.0090   1.0000
  16.000   1.1898   0.05688   0.05238   0.0250   0.0091   1.0000
  16.250   1.1878   0.06029   0.05587   0.0240   0.0090   1.0000
  16.500   1.1853   0.06383   0.05950   0.0229   0.0089   1.0000
  16.750   1.1827   0.06746   0.06322   0.0216   0.0090   1.0000
  17.000   1.1797   0.07124   0.06708   0.0202   0.0090   1.0000
  17.250   1.1735   0.07557   0.07151   0.0185   0.0090   1.0000
  17.500   1.1659   0.08015   0.07619   0.0167   0.0089   1.0000
  17.750   1.1601   0.08461   0.08074   0.0148   0.0090   1.0000
  18.000   1.1509   0.08970   0.08593   0.0125   0.0089   1.0000
  18.250   1.1428   0.09467   0.09099   0.0103   0.0090   1.0000
  18.500   1.1337   0.09993   0.09635   0.0078   0.0090   1.0000
  18.750   1.1218   0.10583   0.10235   0.0049   0.0090   1.0000
  19.000   1.1119   0.11145   0.10808   0.0021   0.0090   1.0000
  19.250   1.1003   0.11749   0.11422  -0.0011   0.0090   1.0000
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