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FX 66-S-196 V1 AIRFOIL (fx66196v-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 66-S-196 V1 AIRFOIL (fx66196v-il)
Reynolds number: 500,000
Max Cl/Cd: 104.46 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx66196v-il-500000-n5.txt
Download as CSV file: xf-fx66196v-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -0.5970   0.10336   0.10057  -0.0640   0.9570   0.0082
 -16.750  -0.6207   0.09100   0.08795  -0.0741   0.9462   0.0083
 -16.500  -0.6282   0.08075   0.07744  -0.0849   0.9334   0.0082
 -16.250  -0.6229   0.07137   0.06773  -0.0974   0.9134   0.0084
 -16.000  -0.6132   0.06434   0.06032  -0.1074   0.8842   0.0085
 -15.750  -0.6127   0.05962   0.05529  -0.1119   0.8563   0.0087
 -15.500  -0.6159   0.05586   0.05130  -0.1141   0.8339   0.0086
 -15.250  -0.6148   0.05298   0.04820  -0.1156   0.8146   0.0089
 -15.000  -0.6173   0.04997   0.04499  -0.1166   0.7976   0.0088
 -14.750  -0.6181   0.04732   0.04222  -0.1176   0.7833   0.0091
 -14.500  -0.6187   0.04484   0.03958  -0.1180   0.7671   0.0092
 -14.000  -0.6137   0.04076   0.03523  -0.1186   0.7418   0.0094
 -13.750  -0.6096   0.03895   0.03330  -0.1187   0.7301   0.0095
 -13.500  -0.6044   0.03729   0.03152  -0.1187   0.7197   0.0097
 -13.250  -0.6003   0.03555   0.02965  -0.1184   0.7104   0.0097
 -13.000  -0.5940   0.03403   0.02802  -0.1182   0.7018   0.0098
 -12.750  -0.5860   0.03270   0.02659  -0.1179   0.6933   0.0101
 -12.500  -0.5794   0.03125   0.02503  -0.1174   0.6856   0.0102
 -12.250  -0.5710   0.02999   0.02367  -0.1169   0.6776   0.0105
 -12.000  -0.5624   0.02877   0.02234  -0.1164   0.6698   0.0107
 -11.750  -0.5535   0.02759   0.02105  -0.1157   0.6625   0.0109
 -11.500  -0.5443   0.02646   0.01982  -0.1150   0.6558   0.0111
 -11.250  -0.5345   0.02540   0.01866  -0.1142   0.6490   0.0113
 -11.000  -0.5245   0.02440   0.01755  -0.1133   0.6425   0.0115
 -10.750  -0.5176   0.02319   0.01629  -0.1123   0.6369   0.0118
 -10.500  -0.5091   0.02216   0.01518  -0.1112   0.6313   0.0120
 -10.250  -0.4994   0.02125   0.01421  -0.1100   0.6263   0.0124
 -10.000  -0.4899   0.02038   0.01330  -0.1088   0.6211   0.0127
  -9.750  -0.4813   0.01969   0.01254  -0.1071   0.6161   0.0132
  -9.500  -0.4739   0.01909   0.01186  -0.1050   0.6116   0.0135
  -9.250  -0.4593   0.01851   0.01121  -0.1038   0.6071   0.0140
  -9.000  -0.4424   0.01802   0.01063  -0.1028   0.6024   0.0146
  -8.750  -0.4262   0.01745   0.00999  -0.1018   0.5982   0.0152
  -8.500  -0.4076   0.01693   0.00943  -0.1010   0.5944   0.0159
  -8.250  -0.3872   0.01649   0.00894  -0.1004   0.5904   0.0166
  -8.000  -0.3659   0.01608   0.00846  -0.0999   0.5865   0.0175
  -7.750  -0.3438   0.01572   0.00801  -0.0994   0.5830   0.0184
  -7.500  -0.3217   0.01529   0.00755  -0.0991   0.5799   0.0196
  -7.250  -0.2982   0.01493   0.00716  -0.0988   0.5766   0.0212
  -7.000  -0.2739   0.01463   0.00680  -0.0987   0.5733   0.0230
  -6.750  -0.2500   0.01428   0.00641  -0.0985   0.5702   0.0254
  -6.500  -0.2252   0.01400   0.00608  -0.0983   0.5674   0.0281
  -6.250  -0.2002   0.01370   0.00576  -0.0983   0.5648   0.0318
  -6.000  -0.1744   0.01342   0.00547  -0.0983   0.5622   0.0371
  -5.750  -0.1486   0.01313   0.00518  -0.0984   0.5596   0.0446
  -5.500  -0.1228   0.01284   0.00490  -0.0985   0.5569   0.0557
  -5.250  -0.0972   0.01251   0.00462  -0.0985   0.5545   0.0740
  -5.000  -0.0717   0.01215   0.00434  -0.0986   0.5521   0.1027
  -4.750  -0.0464   0.01173   0.00405  -0.0988   0.5501   0.1448
  -4.500  -0.0216   0.01110   0.00369  -0.0990   0.5481   0.2176
  -4.250   0.0024   0.01031   0.00328  -0.0993   0.5460   0.3200
  -4.000   0.0277   0.00983   0.00316  -0.0994   0.5440   0.4263
  -3.750   0.0560   0.00981   0.00315  -0.0997   0.5419   0.4522
  -3.500   0.0845   0.00984   0.00315  -0.0999   0.5397   0.4685
  -3.250   0.1129   0.00989   0.00315  -0.1002   0.5377   0.4816
  -3.000   0.1413   0.00997   0.00317  -0.1004   0.5359   0.4942
  -2.750   0.1699   0.01004   0.00319  -0.1007   0.5342   0.5043
  -2.500   0.1986   0.01006   0.00320  -0.1010   0.5326   0.5106
  -2.250   0.2273   0.01009   0.00320  -0.1013   0.5310   0.5151
  -2.000   0.2560   0.01012   0.00317  -0.1016   0.5294   0.5182
  -1.750   0.2847   0.01014   0.00314  -0.1020   0.5278   0.5203
  -1.500   0.3133   0.01017   0.00312  -0.1023   0.5263   0.5222
  -1.250   0.3417   0.01018   0.00310  -0.1026   0.5249   0.5240
  -1.000   0.3700   0.01020   0.00310  -0.1029   0.5235   0.5260
  -0.750   0.3984   0.01024   0.00311  -0.1031   0.5222   0.5277
  -0.500   0.4267   0.01029   0.00312  -0.1034   0.5209   0.5292
  -0.250   0.4551   0.01034   0.00314  -0.1038   0.5197   0.5308
   0.000   0.4837   0.01037   0.00316  -0.1041   0.5186   0.5325
   0.250   0.5122   0.01040   0.00319  -0.1044   0.5175   0.5341
   0.500   0.5406   0.01045   0.00323  -0.1048   0.5163   0.5358
   0.750   0.5690   0.01050   0.00327  -0.1051   0.5152   0.5375
   1.000   0.5973   0.01054   0.00332  -0.1054   0.5140   0.5391
   1.250   0.6254   0.01059   0.00338  -0.1057   0.5129   0.5408
   1.500   0.6535   0.01064   0.00344  -0.1060   0.5118   0.5426
   1.750   0.6816   0.01070   0.00351  -0.1063   0.5107   0.5446
   2.000   0.7096   0.01077   0.00359  -0.1066   0.5097   0.5467
   2.250   0.7376   0.01085   0.00367  -0.1068   0.5087   0.5490
   2.500   0.7656   0.01093   0.00376  -0.1071   0.5078   0.5514
   2.750   0.7936   0.01103   0.00385  -0.1074   0.5068   0.5539
   3.000   0.8214   0.01113   0.00396  -0.1077   0.5056   0.5562
   3.250   0.8494   0.01123   0.00409  -0.1080   0.5045   0.5586
   3.500   0.8770   0.01130   0.00422  -0.1082   0.5038   0.5613
   3.750   0.9046   0.01139   0.00435  -0.1085   0.5030   0.5641
   4.000   0.9322   0.01148   0.00449  -0.1087   0.5022   0.5671
   4.500   0.9870   0.01167   0.00479  -0.1092   0.5004   0.5729
   4.750   1.0141   0.01176   0.00494  -0.1093   0.4992   0.5762
   5.000   1.0410   0.01185   0.00510  -0.1094   0.4978   0.5799
   5.250   1.0680   0.01196   0.00526  -0.1096   0.4967   0.5837
   5.500   1.0950   0.01207   0.00543  -0.1097   0.4957   0.5874
   5.750   1.1218   0.01218   0.00562  -0.1099   0.4948   0.5916
   6.000   1.1484   0.01230   0.00580  -0.1100   0.4937   0.5964
   6.250   1.1752   0.01243   0.00598  -0.1101   0.4926   0.6012
   6.500   1.2020   0.01256   0.00618  -0.1103   0.4916   0.6062
   6.750   1.2289   0.01271   0.00638  -0.1104   0.4901   0.6121
   7.250   1.2795   0.01297   0.00684  -0.1102   0.4873   0.6242
   7.500   1.3033   0.01307   0.00707  -0.1098   0.4851   0.6312
   7.750   1.3268   0.01316   0.00727  -0.1093   0.4825   0.6382
   8.000   1.3501   0.01325   0.00746  -0.1088   0.4798   0.6461
   8.250   1.3693   0.01325   0.00749  -0.1074   0.4732   0.6545
   8.500   1.3810   0.01322   0.00756  -0.1046   0.4618   0.6642
   8.750   1.3869   0.01330   0.00769  -0.1007   0.4477   0.6746
   9.000   1.3926   0.01357   0.00800  -0.0970   0.4314   0.6861
   9.500   1.3779   0.01532   0.00958  -0.0864   0.3666   0.7121
   9.750   1.3581   0.01715   0.01130  -0.0804   0.3337   0.7279
  10.250   1.3241   0.02169   0.01579  -0.0712   0.2819   0.7700
  10.500   1.3039   0.02485   0.01894  -0.0677   0.2545   0.8011
  10.750   1.2929   0.02797   0.02215  -0.0659   0.2298   0.8541
  11.250   1.2722   0.03647   0.03058  -0.0665   0.1705   1.0000
  11.500   1.2593   0.04011   0.03414  -0.0651   0.1490   1.0000
  11.750   1.2484   0.04369   0.03764  -0.0639   0.1285   1.0000
  12.000   1.2406   0.04702   0.04090  -0.0629   0.1093   1.0000
  12.250   1.2332   0.05038   0.04417  -0.0620   0.0902   1.0000
  12.500   1.2273   0.05363   0.04733  -0.0612   0.0718   1.0000
  12.750   1.2249   0.05659   0.05023  -0.0606   0.0581   1.0000
  13.000   1.2234   0.05949   0.05307  -0.0600   0.0458   1.0000
  13.250   1.2237   0.06226   0.05580  -0.0596   0.0365   1.0000
  13.500   1.2255   0.06486   0.05838  -0.0593   0.0287   1.0000
  13.750   1.2284   0.06741   0.06093  -0.0590   0.0235   1.0000
  14.000   1.2329   0.06979   0.06332  -0.0588   0.0196   1.0000
  14.250   1.2377   0.07218   0.06573  -0.0586   0.0171   1.0000
  14.500   1.2419   0.07465   0.06822  -0.0585   0.0149   1.0000
  14.750   1.2478   0.07691   0.07053  -0.0584   0.0138   1.0000
  15.000   1.2530   0.07930   0.07295  -0.0583   0.0125   1.0000
  15.250   1.2571   0.08183   0.07551  -0.0583   0.0115   1.0000
  15.500   1.2625   0.08423   0.07796  -0.0583   0.0109   1.0000
  15.750   1.2681   0.08663   0.08043  -0.0583   0.0103   1.0000
  16.000   1.2729   0.08914   0.08300  -0.0584   0.0098   1.0000
  16.250   1.2774   0.09166   0.08557  -0.0585   0.0093   1.0000
  16.500   1.2805   0.09440   0.08836  -0.0587   0.0088   1.0000
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