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FX S 02-196 AIRFOIL (fxs02196-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX S 02-196 AIRFOIL (fxs02196-il)
Reynolds number: 500,000
Max Cl/Cd: 46.54 at α=4°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fxs02196-il-500000-n5.txt
Download as CSV file: xf-fxs02196-il-500000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.5879   0.10783   0.10507  -0.0609   1.0000   0.0091
 -17.000  -0.6557   0.09017   0.08706  -0.0710   1.0000   0.0089
 -16.750  -0.6769   0.08256   0.07929  -0.0754   1.0000   0.0090
 -16.500  -0.6909   0.07657   0.07317  -0.0788   1.0000   0.0091
 -16.250  -0.6958   0.07075   0.06719  -0.0832   0.9670   0.0093
 -16.000  -0.6835   0.06405   0.06024  -0.0931   0.9433   0.0096
 -15.750  -0.6659   0.05715   0.05290  -0.1043   0.9207   0.0106
 -15.500  -0.6459   0.05326   0.04875  -0.1110   0.8886   0.0107
 -15.000  -0.6377   0.04863   0.04368  -0.1133   0.8356   0.0113
 -14.750  -0.6364   0.04641   0.04127  -0.1136   0.8174   0.0116
 -14.500  -0.6350   0.04429   0.03894  -0.1139   0.8013   0.0121
 -14.250  -0.6336   0.04229   0.03671  -0.1141   0.7872   0.0125
 -14.000  -0.6342   0.04029   0.03444  -0.1142   0.7741   0.0129
 -13.750  -0.6315   0.03855   0.03251  -0.1143   0.7617   0.0132
 -13.500  -0.6226   0.03726   0.03113  -0.1139   0.7499   0.0133
 -13.250  -0.6133   0.03604   0.02985  -0.1136   0.7386   0.0135
 -13.000  -0.6043   0.03481   0.02852  -0.1133   0.7288   0.0137
 -12.750  -0.5950   0.03364   0.02726  -0.1129   0.7189   0.0141
 -12.500  -0.5849   0.03250   0.02601  -0.1124   0.7101   0.0142
 -12.250  -0.5752   0.03138   0.02478  -0.1120   0.7011   0.0146
 -12.000  -0.5656   0.03030   0.02357  -0.1115   0.6919   0.0150
 -11.750  -0.5539   0.02932   0.02248  -0.1109   0.6838   0.0151
 -11.500  -0.5451   0.02831   0.02130  -0.1103   0.6756   0.0154
 -11.250  -0.5385   0.02734   0.02015  -0.1097   0.6680   0.0157
 -11.000  -0.5281   0.02649   0.01917  -0.1090   0.6608   0.0158
 -10.750  -0.5026   0.02580   0.01858  -0.1082   0.6531   0.0163
 -10.500  -0.4872   0.02504   0.01779  -0.1073   0.6455   0.0166
 -10.250  -0.4726   0.02428   0.01700  -0.1065   0.6376   0.0170
  -9.750  -0.4441   0.02285   0.01544  -0.1046   0.6223   0.0173
  -9.500  -0.4303   0.02213   0.01467  -0.1036   0.6156   0.0174
  -9.250  -0.4172   0.02148   0.01392  -0.1025   0.6070   0.0178
  -9.000  -0.4040   0.02080   0.01319  -0.1014   0.6007   0.0179
  -8.750  -0.3919   0.02022   0.01252  -0.1000   0.5953   0.0182
  -8.500  -0.3833   0.01968   0.01190  -0.0981   0.5895   0.0185
  -8.250  -0.3698   0.01901   0.01121  -0.0970   0.5856   0.0186
  -8.000  -0.3575   0.01817   0.01039  -0.0957   0.5802   0.0190
  -7.750  -0.3409   0.01754   0.00974  -0.0948   0.5757   0.0192
  -7.500  -0.3216   0.01703   0.00918  -0.0942   0.5714   0.0194
  -7.000  -0.2800   0.01604   0.00811  -0.0934   0.5644   0.0202
  -6.750  -0.2570   0.01561   0.00765  -0.0932   0.5599   0.0206
  -6.500  -0.2331   0.01526   0.00724  -0.0931   0.5545   0.0208
  -6.250  -0.2088   0.01494   0.00686  -0.0929   0.5490   0.0208
  -6.000  -0.1836   0.01464   0.00650  -0.0930   0.5447   0.0209
  -5.750  -0.1576   0.01435   0.00618  -0.0931   0.5409   0.0209
  -5.500  -0.1314   0.01407   0.00587  -0.0932   0.5375   0.0210
  -5.250  -0.1048   0.01381   0.00558  -0.0934   0.5339   0.0211
  -5.000  -0.0784   0.01361   0.00530  -0.0935   0.5279   0.0212
  -4.750  -0.0512   0.01340   0.00506  -0.0937   0.5214   0.0213
  -4.500  -0.0240   0.01322   0.00482  -0.0939   0.5124   0.0214
  -4.250   0.0030   0.01308   0.00462  -0.0941   0.5046   0.0216
  -4.000   0.0308   0.01293   0.00443  -0.0944   0.4982   0.0217
  -3.750   0.0585   0.01281   0.00426  -0.0946   0.4920   0.0218
  -3.500   0.0860   0.01272   0.00411  -0.0948   0.4851   0.0220
  -3.250   0.1140   0.01262   0.00397  -0.0951   0.4784   0.0222
  -3.000   0.1416   0.01255   0.00385  -0.0953   0.4700   0.0225
  -2.750   0.1695   0.01248   0.00374  -0.0956   0.4626   0.0231
  -2.500   0.1975   0.01242   0.00365  -0.0959   0.4514   0.0236
  -2.250   0.2248   0.01242   0.00360  -0.0961   0.4344   0.0249
  -2.000   0.2395   0.01333   0.00395  -0.0944   0.3077   0.0257
  -1.750   0.2597   0.01391   0.00425  -0.0935   0.2382   0.0309
  -1.500   0.2847   0.01411   0.00435  -0.0933   0.2196   0.0326
  -1.250   0.3080   0.01442   0.00451  -0.0928   0.1729   0.0333
  -1.000   0.3337   0.01456   0.00459  -0.0928   0.1426   0.0338
  -0.750   0.3579   0.01478   0.00471  -0.0925   0.1255   0.0345
  -0.500   0.3843   0.01487   0.00477  -0.0925   0.1215   0.0352
  -0.250   0.4111   0.01492   0.00482  -0.0925   0.1188   0.0360
   0.000   0.4362   0.01507   0.00492  -0.0924   0.0942   0.0367
   0.250   0.4613   0.01521   0.00502  -0.0922   0.0888   0.0376
   0.500   0.4870   0.01531   0.00510  -0.0921   0.0853   0.0389
   0.750   0.5125   0.01542   0.00520  -0.0920   0.0825   0.0404
   1.000   0.5375   0.01554   0.00532  -0.0917   0.0798   0.0414
   1.250   0.5628   0.01564   0.00541  -0.0916   0.0774   0.0436
   1.500   0.5868   0.01579   0.00557  -0.0913   0.0606   0.0626
   1.750   0.6103   0.01596   0.00573  -0.0908   0.0591   0.0667
   2.000   0.6334   0.01614   0.00589  -0.0903   0.0571   0.0711
   2.250   0.6565   0.01627   0.00607  -0.0899   0.0558   0.1007
   2.500   0.6791   0.01642   0.00625  -0.0893   0.0550   0.1115
   2.750   0.7006   0.01653   0.00644  -0.0886   0.0543   0.1522
   3.000   0.7202   0.01665   0.00663  -0.0876   0.0536   0.1929
   3.250   0.7389   0.01680   0.00686  -0.0864   0.0531   0.2142
   3.500   0.7594   0.01681   0.00710  -0.0859   0.0524   0.3150
   3.750   0.7808   0.01680   0.00745  -0.0857   0.0519   0.4421
   4.000   0.7981   0.01715   0.00787  -0.0844   0.0513   0.4585
   4.250   0.8151   0.01754   0.00833  -0.0832   0.0510   0.4751
   4.500   0.8312   0.01799   0.00884  -0.0819   0.0505   0.4901
   4.750   0.8470   0.01849   0.00936  -0.0806   0.0502   0.4987
   5.000   0.8630   0.01900   0.00992  -0.0794   0.0499   0.5076
   5.250   0.8790   0.01954   0.01052  -0.0783   0.0497   0.5185
   5.500   0.8950   0.02011   0.01116  -0.0773   0.0491   0.5269
   5.750   0.9103   0.02075   0.01185  -0.0762   0.0485   0.5345
   6.000   0.9253   0.02145   0.01259  -0.0752   0.0476   0.5405
   6.250   0.9401   0.02219   0.01339  -0.0742   0.0467   0.5494
   6.500   0.9543   0.02300   0.01424  -0.0733   0.0459   0.5573
   6.750   0.9682   0.02385   0.01514  -0.0724   0.0448   0.5623
   7.000   0.9825   0.02472   0.01606  -0.0715   0.0440   0.5678
   7.250   0.9966   0.02562   0.01702  -0.0707   0.0428   0.5717
   7.500   1.0099   0.02661   0.01805  -0.0699   0.0357   0.5771
   7.750   1.0193   0.02791   0.01937  -0.0689   0.0351   0.5811
   8.000   1.0296   0.02917   0.02066  -0.0680   0.0344   0.5873
   8.250   1.0406   0.03042   0.02196  -0.0672   0.0338   0.5929
   8.500   1.0513   0.03173   0.02330  -0.0665   0.0333   0.5986
   8.750   1.0622   0.03302   0.02465  -0.0658   0.0329   0.6053
   9.000   1.0726   0.03441   0.02609  -0.0651   0.0325   0.6122
   9.250   1.0832   0.03579   0.02751  -0.0645   0.0323   0.6183
   9.500   1.0932   0.03725   0.02904  -0.0639   0.0322   0.6240
   9.750   1.1034   0.03872   0.03058  -0.0633   0.0320   0.6323
  10.000   1.1133   0.04027   0.03220  -0.0629   0.0319   0.6412
  10.250   1.1233   0.04182   0.03383  -0.0624   0.0317   0.6504
  10.750   1.1427   0.04508   0.03726  -0.0616   0.0315   0.6732
  11.000   1.1528   0.04670   0.03896  -0.0613   0.0313   0.6837
  11.250   1.1618   0.04846   0.04082  -0.0610   0.0312   0.6964
  11.500   1.1712   0.05021   0.04266  -0.0607   0.0310   0.7088
  12.000   1.1874   0.05405   0.04670  -0.0603   0.0305   0.7386
  12.250   1.1949   0.05606   0.04883  -0.0601   0.0302   0.7564
  12.500   1.2017   0.05814   0.05102  -0.0599   0.0298   0.7792
  12.750   1.2058   0.06047   0.05350  -0.0595   0.0294   0.8105
  13.000   1.2085   0.06233   0.05563  -0.0583   0.0291   0.8895
  13.250   1.2142   0.06453   0.05794  -0.0584   0.0289   1.0000
  13.500   1.2212   0.06686   0.06031  -0.0585   0.0287   1.0000
  13.750   1.2293   0.06908   0.06258  -0.0587   0.0285   1.0000
  14.000   1.2373   0.07132   0.06487  -0.0589   0.0284   1.0000
  14.250   1.2446   0.07368   0.06729  -0.0592   0.0282   1.0000
  14.500   1.2513   0.07615   0.06981  -0.0595   0.0279   1.0000
  14.750   1.2582   0.07860   0.07231  -0.0598   0.0275   1.0000
  15.000   1.2643   0.08117   0.07494  -0.0602   0.0270   1.0000
  15.250   1.2687   0.08402   0.07784  -0.0606   0.0267   1.0000
  15.500   1.2740   0.08676   0.08062  -0.0611   0.0264   1.0000
  15.750   1.2785   0.08960   0.08351  -0.0617   0.0261   1.0000
  16.000   1.2825   0.09253   0.08648  -0.0622   0.0258   1.0000
  16.250   1.2856   0.09564   0.08962  -0.0629   0.0255   1.0000
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