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FX S 02-196 AIRFOIL (fxs02196-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: FX S 02-196 AIRFOIL (fxs02196-il)
Reynolds number: 500,000
Max Cl/Cd: 53.06 at α=4.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fxs02196-il-500000.txt
Download as CSV file: xf-fxs02196-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX S 02-196 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
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.4895   0.10475   0.10213  -0.0662   1.0000   0.0156
 -15.750  -0.5220   0.09379   0.09104  -0.0725   1.0000   0.0155
 -15.500  -0.5237   0.08981   0.08707  -0.0743   1.0000   0.0153
 -15.250  -0.5567   0.08003   0.07711  -0.0804   1.0000   0.0152
 -15.000  -0.5828   0.07248   0.06939  -0.0849   1.0000   0.0151
 -14.750  -0.6028   0.06651   0.06328  -0.0880   1.0000   0.0149
 -14.500  -0.6276   0.06056   0.05711  -0.0910   1.0000   0.0150
 -14.250  -0.6414   0.05363   0.04986  -0.0981   0.9650   0.0151
 -14.000  -0.6484   0.04574   0.04134  -0.1113   0.9399   0.0155
 -13.750  -0.6217   0.04165   0.03703  -0.1178   0.9149   0.0163
 -13.500  -0.6038   0.03960   0.03480  -0.1197   0.8854   0.0166
 -13.250  -0.6009   0.03776   0.03275  -0.1195   0.8598   0.0172
 -13.000  -0.6054   0.03578   0.03048  -0.1186   0.8390   0.0177
 -12.750  -0.6237   0.03383   0.02814  -0.1172   0.8194   0.0182
 -12.500  -0.6324   0.03243   0.02645  -0.1155   0.8033   0.0184
 -12.000  -0.5889   0.02916   0.02301  -0.1144   0.7803   0.0209
 -11.750  -0.5635   0.02803   0.02187  -0.1135   0.7697   0.0218
 -11.500  -0.5496   0.02716   0.02096  -0.1126   0.7574   0.0225
 -11.250  -0.5373   0.02624   0.01990  -0.1116   0.7462   0.0232
 -11.000  -0.5238   0.02540   0.01891  -0.1106   0.7354   0.0235
 -10.750  -0.5086   0.02454   0.01800  -0.1095   0.7258   0.0240
 -10.500  -0.4952   0.02381   0.01723  -0.1085   0.7153   0.0244
 -10.250  -0.4814   0.02313   0.01649  -0.1077   0.7061   0.0250
 -10.000  -0.4674   0.02241   0.01570  -0.1066   0.6965   0.0252
  -9.750  -0.4538   0.02173   0.01494  -0.1055   0.6876   0.0256
  -9.500  -0.4410   0.02097   0.01411  -0.1043   0.6794   0.0258
  -9.000  -0.4184   0.01960   0.01260  -0.1014   0.6628   0.0266
  -8.750  -0.4084   0.01914   0.01209  -0.0997   0.6557   0.0270
  -8.500  -0.3913   0.01884   0.01171  -0.0989   0.6485   0.0276
  -8.250  -0.3746   0.01827   0.01112  -0.0979   0.6428   0.0278
  -8.000  -0.3549   0.01790   0.01067  -0.0972   0.6359   0.0284
  -7.750  -0.3362   0.01744   0.01012  -0.0964   0.6304   0.0288
  -7.500  -0.3168   0.01691   0.00955  -0.0958   0.6257   0.0290
  -7.250  -0.2951   0.01650   0.00910  -0.0953   0.6210   0.0295
  -7.000  -0.2725   0.01615   0.00871  -0.0950   0.6162   0.0299
  -6.750  -0.2486   0.01591   0.00840  -0.0948   0.6108   0.0307
  -6.500  -0.2249   0.01557   0.00802  -0.0946   0.6059   0.0314
  -6.250  -0.2011   0.01514   0.00756  -0.0944   0.6010   0.0318
  -6.000  -0.1769   0.01476   0.00713  -0.0943   0.5961   0.0323
  -5.750  -0.1519   0.01444   0.00673  -0.0943   0.5917   0.0327
  -5.500  -0.1268   0.01413   0.00637  -0.0943   0.5874   0.0333
  -5.250  -0.1002   0.01379   0.00603  -0.0945   0.5842   0.0341
  -5.000  -0.0733   0.01350   0.00571  -0.0947   0.5789   0.0354
  -4.750  -0.0465   0.01327   0.00540  -0.0948   0.5726   0.0366
  -4.500  -0.0200   0.01301   0.00507  -0.0950   0.5663   0.0381
  -4.250   0.0080   0.01278   0.00481  -0.0953   0.5616   0.0397
  -4.000   0.0358   0.01256   0.00454  -0.0956   0.5570   0.0410
  -3.750   0.0637   0.01238   0.00431  -0.0959   0.5529   0.0425
  -3.500   0.0916   0.01228   0.00413  -0.0961   0.5483   0.0435
  -3.250   0.1201   0.01218   0.00400  -0.0965   0.5444   0.0442
  -3.000   0.1488   0.01205   0.00388  -0.0969   0.5401   0.0455
  -2.750   0.1772   0.01193   0.00376  -0.0972   0.5352   0.0476
  -2.500   0.2055   0.01184   0.00367  -0.0975   0.5307   0.0609
  -2.250   0.2337   0.01184   0.00361  -0.0978   0.5264   0.0627
  -2.000   0.2627   0.01176   0.00353  -0.0982   0.5228   0.0642
  -1.750   0.2916   0.01170   0.00347  -0.0986   0.5184   0.0656
  -1.500   0.3200   0.01167   0.00340  -0.0989   0.5123   0.0677
  -1.250   0.3478   0.01167   0.00334  -0.0991   0.5053   0.0685
  -1.000   0.3765   0.01162   0.00328  -0.0994   0.4986   0.0696
  -0.750   0.4048   0.01160   0.00324  -0.0997   0.4927   0.0715
  -0.500   0.4326   0.01161   0.00321  -0.1000   0.4870   0.0741
  -0.250   0.4613   0.01154   0.00318  -0.1004   0.4811   0.0949
   0.000   0.4893   0.01156   0.00318  -0.1006   0.4734   0.1028
   0.250   0.5165   0.01160   0.00318  -0.1008   0.4645   0.1094
   0.500   0.5449   0.01151   0.00315  -0.1012   0.4517   0.1473
   0.750   0.5705   0.01154   0.00314  -0.1013   0.4228   0.1939
   1.000   0.5849   0.01225   0.00353  -0.0997   0.3352   0.2502
   1.250   0.6042   0.01237   0.00390  -0.0996   0.2731   0.4264
   1.500   0.6222   0.01298   0.00438  -0.0984   0.2241   0.4537
   1.750   0.6469   0.01319   0.00462  -0.0982   0.2045   0.4714
   2.000   0.6661   0.01370   0.00501  -0.0971   0.1749   0.4892
   2.250   0.6892   0.01398   0.00526  -0.0966   0.1667   0.5001
   2.500   0.7142   0.01413   0.00546  -0.0963   0.1602   0.5127
   2.750   0.7322   0.01460   0.00584  -0.0950   0.1323   0.5190
   3.000   0.7543   0.01485   0.00608  -0.0943   0.1279   0.5237
   3.250   0.7758   0.01510   0.00636  -0.0936   0.1246   0.5315
   3.500   0.7955   0.01538   0.00664  -0.0924   0.1218   0.5385
   3.750   0.8152   0.01557   0.00688  -0.0913   0.1205   0.5456
   4.000   0.8343   0.01580   0.00713  -0.0900   0.1185   0.5523
   4.250   0.8532   0.01608   0.00743  -0.0888   0.1151   0.5585
   4.500   0.8640   0.01665   0.00798  -0.0865   0.0945   0.5646
   4.750   0.8799   0.01708   0.00843  -0.0850   0.0932   0.5707
   5.000   0.8947   0.01759   0.00894  -0.0835   0.0913   0.5786
   5.250   0.9085   0.01814   0.00955  -0.0819   0.0890   0.5858
   5.500   0.9235   0.01869   0.01014  -0.0806   0.0876   0.5921
   5.750   0.9387   0.01928   0.01076  -0.0793   0.0865   0.5981
   6.000   0.9540   0.01988   0.01142  -0.0782   0.0852   0.6040
   6.250   0.9688   0.02053   0.01214  -0.0771   0.0843   0.6113
   6.500   0.9833   0.02127   0.01290  -0.0760   0.0834   0.6180
   6.750   0.9968   0.02206   0.01375  -0.0749   0.0821   0.6235
   7.000   1.0102   0.02290   0.01465  -0.0738   0.0811   0.6294
   7.250   1.0230   0.02382   0.01563  -0.0728   0.0802   0.6352
   7.500   1.0354   0.02481   0.01666  -0.0718   0.0793   0.6420
   7.750   1.0498   0.02568   0.01762  -0.0711   0.0784   0.6489
   8.000   1.0633   0.02664   0.01865  -0.0703   0.0776   0.6571
   8.250   1.0767   0.02764   0.01973  -0.0695   0.0764   0.6652
   8.500   1.0918   0.02854   0.02072  -0.0689   0.0660   0.6743
   8.750   1.0977   0.03014   0.02234  -0.0678   0.0641   0.6832
   9.000   1.1047   0.03171   0.02395  -0.0668   0.0615   0.6936
   9.250   1.1141   0.03311   0.02542  -0.0660   0.0602   0.7047
   9.500   1.1232   0.03456   0.02695  -0.0653   0.0595   0.7175
   9.750   1.1327   0.03598   0.02847  -0.0645   0.0590   0.7338
  10.000   1.1417   0.03748   0.03009  -0.0638   0.0585   0.7537
  10.250   1.1498   0.03904   0.03178  -0.0631   0.0578   0.7777
  10.500   1.1573   0.04060   0.03351  -0.0622   0.0573   0.8125
  10.750   1.1585   0.04197   0.03518  -0.0600   0.0565   0.9030
  11.000   1.1670   0.04377   0.03707  -0.0599   0.0556   1.0000
  11.250   1.1766   0.04550   0.03883  -0.0596   0.0550   1.0000
  11.500   1.1858   0.04731   0.04070  -0.0594   0.0542   1.0000
  11.750   1.1945   0.04919   0.04263  -0.0592   0.0532   1.0000
  12.000   1.2013   0.05128   0.04476  -0.0590   0.0518   1.0000
  12.250   1.2059   0.05365   0.04717  -0.0588   0.0507   1.0000
  12.500   1.2135   0.05572   0.04928  -0.0586   0.0497   1.0000
  12.750   1.2261   0.05729   0.05091  -0.0587   0.0486   1.0000
  13.000   1.2361   0.05918   0.05286  -0.0587   0.0471   1.0000
  13.250   1.2456   0.06113   0.05485  -0.0587   0.0457   1.0000
  13.500   1.2551   0.06309   0.05685  -0.0588   0.0447   1.0000
  13.750   1.2664   0.06486   0.05868  -0.0589   0.0432   1.0000
  14.000   1.2762   0.06685   0.06073  -0.0590   0.0414   1.0000
  14.250   1.2861   0.06882   0.06273  -0.0592   0.0399   1.0000
  14.500   1.2968   0.07071   0.06461  -0.0594   0.0386   1.0000
  14.750   1.3062   0.07276   0.06666  -0.0597   0.0374   1.0000
  15.000   1.3129   0.07518   0.06908  -0.0599   0.0363   1.0000
  15.250   1.3189   0.07770   0.07164  -0.0602   0.0357   1.0000
  15.500   1.3247   0.08028   0.07427  -0.0606   0.0353   1.0000
  15.750   1.3282   0.08321   0.07726  -0.0610   0.0348   1.0000
  16.000   1.3314   0.08619   0.08029  -0.0615   0.0343   1.0000
  16.250   1.3349   0.08914   0.08330  -0.0620   0.0339   1.0000
  16.500   1.3355   0.09254   0.08673  -0.0627   0.0332   1.0000
  16.750   1.3355   0.09608   0.09031  -0.0634   0.0327   1.0000
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