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FX 66-S-196 V1 AIRFOIL (fx66196v-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 66-S-196 V1 AIRFOIL (fx66196v-il)
Reynolds number: 1,000,000
Max Cl/Cd: 132.69 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx66196v-il-1000000-n5.txt
Download as CSV file: xf-fx66196v-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 66-S-196 V1 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
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -0.7780   0.09188   0.08913  -0.0680   0.9484   0.0059
 -18.000  -0.7816   0.08248   0.07950  -0.0783   0.9319   0.0059
 -17.750  -0.7639   0.07444   0.07120  -0.0908   0.9114   0.0060
 -17.500  -0.7549   0.06647   0.06287  -0.1023   0.8777   0.0060
 -17.250  -0.7502   0.06189   0.05801  -0.1073   0.8416   0.0060
 -17.000  -0.7532   0.05792   0.05387  -0.1099   0.8281   0.0061
 -16.750  -0.7488   0.05509   0.05087  -0.1118   0.8081   0.0062
 -16.500  -0.7516   0.05167   0.04729  -0.1136   0.7897   0.0062
 -16.250  -0.7499   0.04893   0.04440  -0.1150   0.7753   0.0063
 -16.000  -0.7466   0.04650   0.04184  -0.1160   0.7618   0.0063
 -15.750  -0.7445   0.04409   0.03928  -0.1169   0.7461   0.0064
 -15.500  -0.7433   0.04168   0.03673  -0.1176   0.7338   0.0064
 -15.250  -0.7342   0.04012   0.03506  -0.1181   0.7220   0.0065
 -15.000  -0.7334   0.03791   0.03274  -0.1184   0.7114   0.0065
 -14.750  -0.7319   0.03586   0.03059  -0.1186   0.7011   0.0067
 -14.500  -0.7290   0.03399   0.02862  -0.1186   0.6930   0.0068
 -14.250  -0.7243   0.03233   0.02686  -0.1185   0.6836   0.0068
 -13.750  -0.7100   0.02949   0.02387  -0.1180   0.6663   0.0071
 -13.250  -0.6914   0.02710   0.02134  -0.1173   0.6517   0.0074
 -13.000  -0.6831   0.02589   0.02005  -0.1167   0.6446   0.0075
 -12.750  -0.6706   0.02497   0.01907  -0.1163   0.6389   0.0077
 -12.500  -0.6618   0.02383   0.01786  -0.1157   0.6327   0.0078
 -12.250  -0.6509   0.02286   0.01682  -0.1150   0.6273   0.0080
 -12.000  -0.6404   0.02187   0.01577  -0.1142   0.6220   0.0081
 -11.750  -0.6296   0.02094   0.01477  -0.1134   0.6163   0.0083
 -11.500  -0.6187   0.02007   0.01383  -0.1125   0.6110   0.0084
 -11.250  -0.6088   0.01917   0.01288  -0.1113   0.6060   0.0085
 -11.000  -0.5985   0.01840   0.01203  -0.1101   0.6006   0.0086
 -10.750  -0.5903   0.01768   0.01125  -0.1083   0.5961   0.0088
 -10.500  -0.5861   0.01706   0.01057  -0.1056   0.5919   0.0089
 -10.250  -0.5728   0.01648   0.00993  -0.1042   0.5874   0.0093
 -10.000  -0.5561   0.01601   0.00941  -0.1031   0.5830   0.0096
  -9.750  -0.5371   0.01559   0.00895  -0.1023   0.5795   0.0099
  -9.500  -0.5167   0.01519   0.00851  -0.1017   0.5760   0.0102
  -9.250  -0.4954   0.01483   0.00810  -0.1011   0.5723   0.0106
  -9.000  -0.4735   0.01449   0.00770  -0.1006   0.5687   0.0110
  -8.750  -0.4506   0.01418   0.00733  -0.1002   0.5655   0.0113
  -8.500  -0.4274   0.01383   0.00695  -0.0999   0.5627   0.0119
  -8.250  -0.4037   0.01349   0.00659  -0.0997   0.5596   0.0126
  -8.000  -0.3794   0.01320   0.00627  -0.0995   0.5564   0.0133
  -7.750  -0.3545   0.01295   0.00597  -0.0994   0.5533   0.0141
  -7.500  -0.3292   0.01272   0.00569  -0.0993   0.5503   0.0148
  -7.250  -0.3038   0.01242   0.00539  -0.0993   0.5480   0.0160
  -7.000  -0.2779   0.01217   0.00512  -0.0993   0.5453   0.0173
  -6.750  -0.2515   0.01197   0.00488  -0.0993   0.5426   0.0186
  -6.500  -0.2253   0.01173   0.00463  -0.0994   0.5399   0.0206
  -6.250  -0.1988   0.01154   0.00441  -0.0995   0.5372   0.0230
  -6.000  -0.1722   0.01133   0.00419  -0.0996   0.5349   0.0263
  -5.750  -0.1450   0.01113   0.00399  -0.0998   0.5330   0.0302
  -5.500  -0.1179   0.01093   0.00380  -0.1000   0.5309   0.0357
  -5.250  -0.0908   0.01072   0.00360  -0.1002   0.5288   0.0444
  -5.000  -0.0637   0.01050   0.00341  -0.1004   0.5266   0.0567
  -4.750  -0.0367   0.01026   0.00323  -0.1006   0.5244   0.0739
  -4.500  -0.0099   0.01000   0.00304  -0.1008   0.5222   0.0999
  -4.000   0.0433   0.00930   0.00263  -0.1013   0.5187   0.1886
  -3.750   0.0692   0.00877   0.00238  -0.1015   0.5174   0.2673
  -3.500   0.0947   0.00820   0.00211  -0.1017   0.5159   0.3580
  -3.250   0.1216   0.00791   0.00205  -0.1019   0.5144   0.4334
  -3.000   0.1503   0.00789   0.00204  -0.1023   0.5129   0.4521
  -2.750   0.1790   0.00789   0.00204  -0.1026   0.5114   0.4659
  -2.500   0.2079   0.00792   0.00205  -0.1029   0.5099   0.4763
  -2.250   0.2366   0.00795   0.00207  -0.1032   0.5085   0.4841
  -2.000   0.2654   0.00801   0.00207  -0.1036   0.5070   0.4901
  -1.750   0.2939   0.00803   0.00208  -0.1039   0.5055   0.4943
  -1.500   0.3226   0.00805   0.00208  -0.1042   0.5043   0.4972
  -1.250   0.3516   0.00806   0.00208  -0.1046   0.5035   0.4996
  -1.000   0.3805   0.00808   0.00209  -0.1049   0.5025   0.5017
  -0.750   0.4094   0.00810   0.00209  -0.1053   0.5015   0.5035
  -0.500   0.4383   0.00813   0.00210  -0.1057   0.5005   0.5049
  -0.250   0.4671   0.00816   0.00211  -0.1060   0.4994   0.5059
   0.000   0.4957   0.00818   0.00212  -0.1064   0.4982   0.5071
   0.250   0.5242   0.00820   0.00214  -0.1067   0.4972   0.5087
   0.500   0.5527   0.00823   0.00217  -0.1070   0.4961   0.5102
   0.750   0.5811   0.00826   0.00221  -0.1073   0.4950   0.5117
   1.000   0.6094   0.00831   0.00224  -0.1076   0.4940   0.5132
   1.250   0.6376   0.00835   0.00229  -0.1079   0.4929   0.5148
   1.500   0.6657   0.00841   0.00234  -0.1082   0.4919   0.5164
   1.750   0.6937   0.00847   0.00240  -0.1084   0.4908   0.5181
   2.000   0.7216   0.00854   0.00247  -0.1087   0.4897   0.5197
   2.250   0.7499   0.00859   0.00253  -0.1090   0.4890   0.5213
   2.750   0.8064   0.00867   0.00266  -0.1096   0.4877   0.5248
   3.000   0.8344   0.00872   0.00273  -0.1099   0.4869   0.5270
   3.250   0.8625   0.00876   0.00281  -0.1101   0.4860   0.5295
   3.500   0.8904   0.00881   0.00289  -0.1104   0.4851   0.5320
   3.750   0.9183   0.00887   0.00298  -0.1107   0.4843   0.5344
   4.000   0.9461   0.00893   0.00307  -0.1109   0.4835   0.5367
   4.500   1.0011   0.00905   0.00326  -0.1113   0.4814   0.5416
   4.750   1.0284   0.00912   0.00336  -0.1115   0.4804   0.5446
   5.000   1.0556   0.00919   0.00347  -0.1116   0.4794   0.5476
   5.250   1.0826   0.00927   0.00358  -0.1118   0.4784   0.5507
   5.500   1.1093   0.00937   0.00370  -0.1118   0.4771   0.5535
   5.750   1.1357   0.00946   0.00383  -0.1119   0.4756   0.5567
   6.000   1.1621   0.00956   0.00397  -0.1119   0.4741   0.5604
   6.250   1.1889   0.00962   0.00410  -0.1120   0.4730   0.5643
   6.500   1.2156   0.00969   0.00423  -0.1121   0.4718   0.5680
   6.750   1.2420   0.00975   0.00436  -0.1121   0.4702   0.5717
   7.000   1.2681   0.00982   0.00449  -0.1121   0.4684   0.5761
   7.250   1.2935   0.00989   0.00462  -0.1119   0.4659   0.5808
   7.500   1.3155   0.01002   0.00475  -0.1111   0.4599   0.5853
   7.750   1.3375   0.01008   0.00484  -0.1103   0.4478   0.5906
   8.000   1.3565   0.01026   0.00501  -0.1090   0.4322   0.5963
   8.250   1.3607   0.01072   0.00532  -0.1049   0.3914   0.6017
   8.500   1.3380   0.01208   0.00637  -0.0963   0.3361   0.6069
   8.750   1.3243   0.01336   0.00749  -0.0899   0.3010   0.6130
   9.000   1.3037   0.01510   0.00904  -0.0831   0.2605   0.6185
   9.250   1.2925   0.01674   0.01059  -0.0783   0.2336   0.6251
   9.500   1.2815   0.01863   0.01239  -0.0742   0.2089   0.6321
   9.750   1.2717   0.02069   0.01440  -0.0706   0.1866   0.6392
  10.000   1.2628   0.02292   0.01658  -0.0676   0.1668   0.6474
  10.250   1.2529   0.02541   0.01904  -0.0648   0.1467   0.6559
  10.500   1.2422   0.02812   0.02170  -0.0623   0.1278   0.6653
  10.750   1.2313   0.03100   0.02455  -0.0600   0.1081   0.6760
  11.000   1.2219   0.03388   0.02741  -0.0581   0.0909   0.6871
  11.250   1.2180   0.03646   0.02999  -0.0567   0.0779   0.7003
  11.500   1.2131   0.03919   0.03272  -0.0554   0.0638   0.7160
  11.750   1.2089   0.04198   0.03552  -0.0543   0.0495   0.7344
  12.000   1.2089   0.04447   0.03805  -0.0536   0.0395   0.7575
  12.250   1.2124   0.04681   0.04048  -0.0532   0.0323   0.7934
  12.500   1.2365   0.04976   0.04373  -0.0579   0.0235   0.9019
  13.000   1.2987   0.05628   0.05034  -0.0700   0.0128   1.0000
  13.250   1.3038   0.05854   0.05262  -0.0696   0.0114   1.0000
  13.500   1.3110   0.06059   0.05470  -0.0693   0.0103   1.0000
  13.750   1.3173   0.06275   0.05690  -0.0691   0.0098   1.0000
  14.000   1.3233   0.06493   0.05910  -0.0688   0.0090   1.0000
  14.250   1.3295   0.06708   0.06129  -0.0685   0.0083   1.0000
  14.500   1.3357   0.06927   0.06352  -0.0683   0.0079   1.0000
  14.750   1.3424   0.07139   0.06567  -0.0681   0.0075   1.0000
  15.000   1.3482   0.07361   0.06793  -0.0678   0.0070   1.0000
  15.250   1.3522   0.07605   0.07041  -0.0676   0.0065   1.0000
  15.500   1.3582   0.07824   0.07263  -0.0674   0.0063   1.0000
  15.750   1.3646   0.08039   0.07483  -0.0673   0.0061   1.0000
  16.000   1.3695   0.08277   0.07726  -0.0672   0.0058   1.0000
  16.250   1.3750   0.08505   0.07958  -0.0671   0.0056   1.0000
  16.500   1.3802   0.08737   0.08193  -0.0670   0.0053   1.0000
  16.750   1.3836   0.08992   0.08454  -0.0669   0.0051   1.0000
  17.000   1.3870   0.09244   0.08709  -0.0669   0.0048   1.0000
  17.250   1.3908   0.09490   0.08961  -0.0668   0.0047   1.0000
  17.500   1.3933   0.09758   0.09233  -0.0668   0.0046   1.0000
  17.750   1.3970   0.10010   0.09490  -0.0669   0.0045   1.0000
  18.000   1.4019   0.10248   0.09734  -0.0670   0.0043   1.0000
  18.250   1.4041   0.10522   0.10013  -0.0671   0.0042   1.0000
  18.500   1.4067   0.10789   0.10286  -0.0673   0.0041   1.0000
  18.750   1.4098   0.11047   0.10550  -0.0675   0.0039   1.0000
  19.000   1.4117   0.11324   0.10832  -0.0678   0.0038   1.0000
  19.250   1.4132   0.11609   0.11122  -0.0681   0.0037   1.0000
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