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FX S 02-196 AIRFOIL (fxs02196-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX S 02-196 AIRFOIL (fxs02196-il)
Reynolds number: 1,000,000
Max Cl/Cd: 60.12 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fxs02196-il-1000000.txt
Download as CSV file: xf-fxs02196-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -0.7659   0.11323   0.11075  -0.0546   1.0000   0.0083
 -19.250  -0.7977   0.10350   0.10085  -0.0600   1.0000   0.0083
 -19.000  -0.8189   0.09597   0.09318  -0.0642   1.0000   0.0082
 -18.750  -0.8346   0.08959   0.08669  -0.0677   1.0000   0.0082
 -18.500  -0.8476   0.08387   0.08084  -0.0709   1.0000   0.0083
 -18.250  -0.8579   0.07868   0.07554  -0.0737   1.0000   0.0083
 -18.000  -0.8654   0.07411   0.07089  -0.0760   1.0000   0.0083
 -17.750  -0.8640   0.07077   0.06749  -0.0779   1.0000   0.0084
 -17.500  -0.8618   0.06764   0.06430  -0.0796   1.0000   0.0085
 -17.250  -0.8533   0.06533   0.06198  -0.0809   1.0000   0.0086
 -17.000  -0.8481   0.06272   0.05933  -0.0823   1.0000   0.0087
 -16.750  -0.8440   0.06005   0.05661  -0.0837   1.0000   0.0088
 -16.500  -0.8381   0.05765   0.05417  -0.0849   1.0000   0.0089
 -16.250  -0.8336   0.05514   0.05162  -0.0861   1.0000   0.0090
 -16.000  -0.8307   0.05259   0.04899  -0.0871   1.0000   0.0091
 -15.750  -0.8226   0.05062   0.04700  -0.0881   1.0000   0.0093
 -15.500  -0.8214   0.04779   0.04408  -0.0888   0.9723   0.0093
 -15.250  -0.7792   0.04476   0.04092  -0.0978   0.9520   0.0098
 -15.000  -0.7303   0.04120   0.03712  -0.1090   0.9367   0.0107
 -14.750  -0.6853   0.03885   0.03454  -0.1177   0.8995   0.0109
 -14.500  -0.6761   0.03753   0.03304  -0.1181   0.8640   0.0111
 -14.250  -0.6710   0.03628   0.03160  -0.1175   0.8338   0.0114
 -14.000  -0.6657   0.03492   0.03009  -0.1174   0.8174   0.0121
 -13.750  -0.6649   0.03338   0.02831  -0.1171   0.7976   0.0127
 -13.500  -0.6611   0.03202   0.02676  -0.1166   0.7786   0.0129
 -13.250  -0.6583   0.03064   0.02523  -0.1161   0.7654   0.0133
 -13.000  -0.6459   0.02979   0.02430  -0.1154   0.7446   0.0135
 -12.750  -0.6329   0.02897   0.02348  -0.1149   0.7357   0.0140
 -12.500  -0.6214   0.02801   0.02243  -0.1142   0.7219   0.0141
 -12.000  -0.6083   0.02604   0.02021  -0.1129   0.7015   0.0152
 -11.500  -0.6097   0.02435   0.01818  -0.1098   0.6825   0.0157
 -11.250  -0.5648   0.02356   0.01754  -0.1104   0.6732   0.0167
 -11.000  -0.5486   0.02286   0.01681  -0.1097   0.6642   0.0170
 -10.750  -0.5347   0.02216   0.01602  -0.1087   0.6533   0.0175
 -10.500  -0.5233   0.02147   0.01523  -0.1078   0.6457   0.0179
 -10.250  -0.5213   0.02086   0.01447  -0.1059   0.6388   0.0183
 -10.000  -0.5223   0.02048   0.01395  -0.1029   0.6314   0.0184
  -9.750  -0.4791   0.01918   0.01282  -0.1043   0.6248   0.0192
  -9.500  -0.4670   0.01847   0.01208  -0.1028   0.6194   0.0193
  -9.250  -0.4620   0.01774   0.01134  -0.1004   0.6131   0.0198
  -9.000  -0.4502   0.01715   0.01070  -0.0989   0.6074   0.0201
  -8.750  -0.4331   0.01662   0.01013  -0.0980   0.6027   0.0204
  -8.500  -0.4141   0.01618   0.00963  -0.0972   0.5971   0.0207
  -8.250  -0.3947   0.01575   0.00913  -0.0965   0.5903   0.0207
  -8.000  -0.3723   0.01542   0.00875  -0.0961   0.5840   0.0209
  -7.750  -0.3518   0.01489   0.00818  -0.0956   0.5792   0.0211
  -7.500  -0.3305   0.01440   0.00764  -0.0951   0.5739   0.0211
  -7.250  -0.3090   0.01388   0.00707  -0.0947   0.5683   0.0213
  -7.000  -0.2854   0.01343   0.00658  -0.0946   0.5642   0.0215
  -6.750  -0.2609   0.01301   0.00613  -0.0946   0.5597   0.0217
  -6.500  -0.2362   0.01260   0.00568  -0.0946   0.5543   0.0220
  -6.250  -0.2107   0.01229   0.00531  -0.0946   0.5471   0.0223
  -6.000  -0.1840   0.01197   0.00495  -0.0948   0.5414   0.0227
  -5.750  -0.1570   0.01171   0.00464  -0.0950   0.5347   0.0231
  -5.500  -0.1299   0.01150   0.00437  -0.0952   0.5279   0.0234
  -5.250  -0.1019   0.01131   0.00414  -0.0955   0.5236   0.0236
  -5.000  -0.0736   0.01113   0.00394  -0.0959   0.5176   0.0236
  -4.750  -0.0456   0.01101   0.00376  -0.0961   0.5089   0.0237
  -4.500  -0.0174   0.01090   0.00360  -0.0964   0.5002   0.0238
  -4.250   0.0106   0.01083   0.00346  -0.0967   0.4907   0.0240
  -4.000   0.0390   0.01075   0.00334  -0.0970   0.4835   0.0242
  -3.750   0.0676   0.01067   0.00323  -0.0973   0.4772   0.0244
  -3.500   0.0958   0.01063   0.00314  -0.0976   0.4690   0.0247
  -3.250   0.1246   0.01056   0.00306  -0.0980   0.4636   0.0251
  -3.000   0.1534   0.01050   0.00300  -0.0983   0.4547   0.0257
  -2.750   0.1792   0.01067   0.00302  -0.0983   0.4170   0.0262
  -2.500   0.1954   0.01163   0.00343  -0.0967   0.2921   0.0306
  -2.250   0.2175   0.01211   0.00365  -0.0961   0.2238   0.0317
  -2.000   0.2423   0.01239   0.00377  -0.0958   0.1763   0.0323
  -1.750   0.2696   0.01247   0.00381  -0.0959   0.1655   0.0328
  -1.500   0.2955   0.01265   0.00389  -0.0959   0.1311   0.0337
  -1.250   0.3228   0.01272   0.00394  -0.0960   0.1242   0.0347
  -1.000   0.3505   0.01277   0.00397  -0.0962   0.1197   0.0356
  -0.750   0.3766   0.01293   0.00405  -0.0961   0.0932   0.0361
  -0.500   0.4037   0.01301   0.00410  -0.0962   0.0885   0.0362
  -0.250   0.4311   0.01306   0.00415  -0.0964   0.0859   0.0365
   0.000   0.4584   0.01312   0.00420  -0.0965   0.0841   0.0370
   0.250   0.4853   0.01321   0.00427  -0.0966   0.0810   0.0375
   0.500   0.5122   0.01328   0.00434  -0.0967   0.0789   0.0384
   0.750   0.5392   0.01335   0.00440  -0.0968   0.0767   0.0395
   1.000   0.5647   0.01351   0.00451  -0.0966   0.0599   0.0406
   1.250   0.5905   0.01363   0.00460  -0.0966   0.0577   0.0428
   1.500   0.6164   0.01374   0.00471  -0.0965   0.0561   0.0450
   1.750   0.6422   0.01384   0.00484  -0.0964   0.0551   0.0607
   2.000   0.6677   0.01397   0.00498  -0.0962   0.0544   0.0650
   2.250   0.6928   0.01410   0.00512  -0.0960   0.0537   0.0714
   2.500   0.7177   0.01421   0.00528  -0.0958   0.0531   0.1001
   2.750   0.7418   0.01437   0.00545  -0.0955   0.0524   0.1081
   3.000   0.7657   0.01449   0.00563  -0.0951   0.0518   0.1421
   3.250   0.7896   0.01456   0.00581  -0.0949   0.0514   0.1926
   3.500   0.8131   0.01462   0.00599  -0.0946   0.0509   0.2505
   3.750   0.8355   0.01462   0.00617  -0.0942   0.0504   0.3233
   4.000   0.8575   0.01452   0.00637  -0.0938   0.0498   0.4305
   4.250   0.8760   0.01471   0.00660  -0.0924   0.0496   0.4475
   4.500   0.8951   0.01492   0.00691  -0.0913   0.0493   0.4737
   4.750   0.9132   0.01519   0.00724  -0.0900   0.0490   0.4911
   5.000   0.9308   0.01552   0.00759  -0.0887   0.0485   0.5007
   5.250   0.9481   0.01587   0.00797  -0.0874   0.0481   0.5078
   5.500   0.9649   0.01626   0.00839  -0.0861   0.0476   0.5138
   5.750   0.9811   0.01670   0.00886  -0.0848   0.0471   0.5187
   6.000   0.9973   0.01717   0.00938  -0.0836   0.0465   0.5292
   6.250   1.0129   0.01769   0.00994  -0.0823   0.0460   0.5376
   6.500   1.0280   0.01828   0.01056  -0.0811   0.0455   0.5439
   6.750   1.0426   0.01892   0.01124  -0.0799   0.0449   0.5496
   7.000   1.0578   0.01957   0.01192  -0.0788   0.0446   0.5567
   7.250   1.0725   0.02028   0.01267  -0.0778   0.0442   0.5626
   7.500   1.0870   0.02103   0.01347  -0.0768   0.0436   0.5692
   7.750   1.1011   0.02183   0.01432  -0.0758   0.0423   0.5767
   8.000   1.1135   0.02277   0.01529  -0.0747   0.0359   0.5852
   8.250   1.1251   0.02381   0.01637  -0.0737   0.0357   0.5931
   8.500   1.1364   0.02490   0.01749  -0.0726   0.0354   0.6000
   8.750   1.1470   0.02607   0.01869  -0.0717   0.0349   0.6086
   9.000   1.1573   0.02732   0.01997  -0.0707   0.0344   0.6177
   9.250   1.1678   0.02857   0.02128  -0.0698   0.0341   0.6256
   9.500   1.1774   0.02991   0.02267  -0.0689   0.0335   0.6362
   9.750   1.1869   0.03131   0.02412  -0.0681   0.0331   0.6439
  10.000   1.1970   0.03267   0.02556  -0.0674   0.0329   0.6538
  10.250   1.2060   0.03416   0.02712  -0.0666   0.0326   0.6655
  10.500   1.2155   0.03564   0.02866  -0.0660   0.0324   0.6784
  10.750   1.2237   0.03727   0.03039  -0.0653   0.0322   0.6900
  11.000   1.2325   0.03889   0.03207  -0.0648   0.0321   0.7019
  11.250   1.2405   0.04061   0.03389  -0.0642   0.0319   0.7172
  11.500   1.2488   0.04231   0.03570  -0.0637   0.0318   0.7373
  11.750   1.2550   0.04427   0.03776  -0.0632   0.0315   0.7562
  12.000   1.2613   0.04618   0.03981  -0.0627   0.0311   0.7843
  12.250   1.2677   0.04809   0.04187  -0.0622   0.0310   0.8222
  12.500   1.2690   0.04985   0.04400  -0.0608   0.0306   1.0000
  12.750   1.2724   0.05231   0.04651  -0.0605   0.0302   1.0000
  13.000   1.2780   0.05457   0.04881  -0.0603   0.0300   1.0000
  13.250   1.2820   0.05703   0.05131  -0.0602   0.0296   1.0000
  13.500   1.2853   0.05966   0.05399  -0.0601   0.0293   1.0000
  13.750   1.2901   0.06214   0.05651  -0.0601   0.0291   1.0000
  14.000   1.2939   0.06474   0.05918  -0.0601   0.0287   1.0000
  14.250   1.3010   0.06707   0.06155  -0.0603   0.0285   1.0000
  14.500   1.3091   0.06927   0.06380  -0.0605   0.0280   1.0000
  14.750   1.3161   0.07161   0.06619  -0.0607   0.0277   1.0000
  15.000   1.3207   0.07430   0.06892  -0.0610   0.0273   1.0000
  15.250   1.3261   0.07692   0.07159  -0.0613   0.0270   1.0000
  15.500   1.3316   0.07952   0.07424  -0.0616   0.0267   1.0000
  15.750   1.3355   0.08237   0.07713  -0.0621   0.0263   1.0000
  16.000   1.3376   0.08552   0.08031  -0.0626   0.0260   1.0000
  16.250   1.3409   0.08845   0.08327  -0.0630   0.0257   1.0000
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