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FX S 02-196 AIRFOIL (fxs02196-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX S 02-196 AIRFOIL (fxs02196-il)
Reynolds number: 1,000,000
Max Cl/Cd: 54.86 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fxs02196-il-1000000-n5.txt
Download as CSV file: xf-fxs02196-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.8158   0.10885   0.10603  -0.0564   1.0000   0.0053
 -19.500  -0.8410   0.10058   0.09762  -0.0610   1.0000   0.0054
 -19.250  -0.8594   0.09366   0.09058  -0.0648   1.0000   0.0054
 -19.000  -0.8719   0.08798   0.08479  -0.0679   1.0000   0.0054
 -18.750  -0.8821   0.08273   0.07943  -0.0708   1.0000   0.0054
 -18.500  -0.8921   0.07766   0.07426  -0.0735   1.0000   0.0054
 -18.250  -0.8978   0.07339   0.06990  -0.0757   1.0000   0.0054
 -18.000  -0.9010   0.06940   0.06583  -0.0779   0.9999   0.0054
 -17.750  -0.9103   0.06591   0.06227  -0.0776   0.9812   0.0055
 -17.500  -0.8734   0.06058   0.05678  -0.0895   0.9471   0.0056
 -17.250  -0.8268   0.05576   0.05178  -0.1022   0.9309   0.0057
 -17.000  -0.7927   0.05214   0.04789  -0.1109   0.8901   0.0059
 -16.750  -0.7886   0.05003   0.04554  -0.1115   0.8517   0.0059
 -16.500  -0.7857   0.04795   0.04331  -0.1118   0.8287   0.0060
 -16.250  -0.7818   0.04600   0.04123  -0.1120   0.8093   0.0061
 -16.000  -0.7767   0.04420   0.03930  -0.1122   0.7927   0.0061
 -15.500  -0.7633   0.04085   0.03576  -0.1125   0.7665   0.0062
 -15.250  -0.7547   0.03943   0.03425  -0.1125   0.7524   0.0064
 -15.000  -0.7428   0.03825   0.03301  -0.1126   0.7401   0.0066
 -14.750  -0.7351   0.03681   0.03147  -0.1125   0.7297   0.0066
 -14.500  -0.7206   0.03588   0.03052  -0.1127   0.7191   0.0070
 -14.250  -0.7064   0.03503   0.02963  -0.1127   0.7050   0.0073
 -14.000  -0.6918   0.03416   0.02875  -0.1129   0.6961   0.0077
 -13.750  -0.6790   0.03325   0.02778  -0.1128   0.6828   0.0080
 -13.500  -0.6708   0.03204   0.02645  -0.1123   0.6677   0.0079
 -13.250  -0.6595   0.03098   0.02531  -0.1120   0.6594   0.0095
 -13.000  -0.6498   0.02993   0.02412  -0.1114   0.6406   0.0100
 -12.750  -0.6388   0.02884   0.02295  -0.1109   0.6387   0.0106
 -12.500  -0.6291   0.02781   0.02182  -0.1102   0.6241   0.0106
 -12.250  -0.6152   0.02699   0.02093  -0.1099   0.6184   0.0111
 -12.000  -0.6023   0.02615   0.02001  -0.1093   0.6106   0.0115
 -11.750  -0.5905   0.02523   0.01903  -0.1087   0.6058   0.0115
 -11.500  -0.5762   0.02446   0.01819  -0.1082   0.5993   0.0120
 -11.250  -0.5615   0.02374   0.01740  -0.1077   0.5948   0.0124
 -11.000  -0.5486   0.02297   0.01655  -0.1070   0.5871   0.0125
 -10.750  -0.5326   0.02236   0.01585  -0.1065   0.5785   0.0128
 -10.500  -0.5171   0.02177   0.01516  -0.1060   0.5714   0.0130
 -10.250  -0.5033   0.02108   0.01441  -0.1052   0.5669   0.0132
 -10.000  -0.4903   0.02032   0.01363  -0.1042   0.5632   0.0132
  -9.750  -0.4778   0.01959   0.01287  -0.1031   0.5588   0.0134
  -9.500  -0.4667   0.01884   0.01209  -0.1017   0.5554   0.0134
  -9.250  -0.4572   0.01825   0.01147  -0.1000   0.5505   0.0136
  -8.750  -0.4311   0.01722   0.01036  -0.0974   0.5430   0.0139
  -8.500  -0.4121   0.01679   0.00990  -0.0967   0.5386   0.0142
  -8.250  -0.3926   0.01637   0.00943  -0.0960   0.5322   0.0142
  -8.000  -0.3716   0.01602   0.00902  -0.0955   0.5243   0.0145
  -7.750  -0.3494   0.01565   0.00861  -0.0951   0.5203   0.0147
  -7.500  -0.3267   0.01528   0.00821  -0.0948   0.5147   0.0149
  -7.250  -0.3032   0.01498   0.00785  -0.0946   0.5082   0.0151
  -7.000  -0.2789   0.01470   0.00752  -0.0944   0.5030   0.0153
  -6.750  -0.2536   0.01447   0.00724  -0.0944   0.4972   0.0155
  -6.500  -0.2270   0.01442   0.00711  -0.0944   0.4887   0.0157
  -6.250  -0.2047   0.01388   0.00654  -0.0942   0.4811   0.0160
  -6.000  -0.1818   0.01341   0.00601  -0.0940   0.4697   0.0165
  -5.750  -0.1563   0.01309   0.00566  -0.0941   0.4617   0.0169
  -5.500  -0.1308   0.01288   0.00536  -0.0942   0.4444   0.0172
  -5.250  -0.1139   0.01348   0.00544  -0.0928   0.3113   0.0173
  -5.000  -0.0909   0.01362   0.00536  -0.0924   0.2473   0.0175
  -4.750  -0.0654   0.01357   0.00521  -0.0924   0.2220   0.0175
  -4.500  -0.0400   0.01358   0.00509  -0.0924   0.1778   0.0176
  -4.250  -0.0129   0.01347   0.00493  -0.0926   0.1672   0.0177
  -4.000   0.0148   0.01333   0.00477  -0.0928   0.1625   0.0178
  -3.750   0.0415   0.01332   0.00467  -0.0929   0.1305   0.0179
  -3.500   0.0692   0.01324   0.00455  -0.0932   0.1262   0.0180
  -3.250   0.0971   0.01316   0.00445  -0.0935   0.1226   0.0181
  -3.000   0.1251   0.01308   0.00435  -0.0938   0.1206   0.0181
  -2.750   0.1532   0.01302   0.00427  -0.0941   0.1177   0.0182
  -2.500   0.1802   0.01306   0.00423  -0.0942   0.0905   0.0183
  -2.250   0.2080   0.01305   0.00419  -0.0944   0.0853   0.0183
  -2.000   0.2358   0.01304   0.00416  -0.0947   0.0821   0.0184
  -1.750   0.2636   0.01304   0.00414  -0.0949   0.0794   0.0184
  -1.500   0.2916   0.01303   0.00411  -0.0952   0.0780   0.0187
  -1.250   0.3190   0.01307   0.00410  -0.0953   0.0603   0.0189
  -0.750   0.3738   0.01315   0.00414  -0.0957   0.0542   0.0193
  -0.500   0.4012   0.01320   0.00417  -0.0958   0.0534   0.0194
  -0.250   0.4285   0.01325   0.00422  -0.0959   0.0525   0.0195
   0.000   0.4556   0.01332   0.00427  -0.0961   0.0518   0.0197
   0.250   0.4825   0.01340   0.00435  -0.0961   0.0507   0.0200
   0.500   0.5093   0.01347   0.00441  -0.0962   0.0499   0.0204
   1.000   0.5625   0.01364   0.00459  -0.0963   0.0488   0.0310
   1.250   0.5887   0.01375   0.00470  -0.0962   0.0478   0.0332
   1.500   0.6147   0.01386   0.00481  -0.0962   0.0467   0.0347
   1.750   0.6403   0.01398   0.00493  -0.0960   0.0454   0.0359
   2.000   0.6657   0.01410   0.00505  -0.0959   0.0444   0.0371
   2.250   0.6909   0.01422   0.00517  -0.0957   0.0432   0.0394
   2.500   0.7149   0.01439   0.00531  -0.0953   0.0321   0.0412
   2.750   0.7386   0.01456   0.00546  -0.0949   0.0313   0.0438
   3.000   0.7618   0.01473   0.00565  -0.0944   0.0303   0.0617
   3.250   0.7845   0.01491   0.00584  -0.0938   0.0299   0.0667
   3.500   0.8061   0.01510   0.00604  -0.0930   0.0295   0.0698
   3.750   0.8248   0.01527   0.00624  -0.0916   0.0292   0.0738
   4.000   0.8422   0.01547   0.00646  -0.0901   0.0288   0.0955
   4.250   0.8598   0.01572   0.00674  -0.0886   0.0286   0.1012
   4.500   0.8774   0.01602   0.00706  -0.0873   0.0285   0.1066
   4.750   0.8953   0.01632   0.00742  -0.0861   0.0284   0.1415
   5.000   0.9121   0.01669   0.00782  -0.0847   0.0283   0.1500
   5.250   0.9291   0.01704   0.00826  -0.0836   0.0282   0.1931
   5.500   0.9452   0.01748   0.00875  -0.0823   0.0282   0.2064
   5.750   0.9615   0.01790   0.00927  -0.0813   0.0281   0.2569
   6.250   0.9955   0.01864   0.01048  -0.0799   0.0279   0.4372
   6.500   1.0096   0.01931   0.01121  -0.0787   0.0279   0.4509
   6.750   1.0232   0.02004   0.01200  -0.0775   0.0278   0.4606
   7.000   1.0367   0.02082   0.01286  -0.0764   0.0277   0.4780
   7.250   1.0497   0.02167   0.01376  -0.0753   0.0276   0.4868
   7.500   1.0619   0.02262   0.01475  -0.0742   0.0276   0.4955
   7.750   1.0738   0.02363   0.01580  -0.0731   0.0275   0.5011
   8.000   1.0857   0.02467   0.01690  -0.0722   0.0274   0.5099
   8.250   1.0971   0.02578   0.01807  -0.0712   0.0273   0.5166
   8.750   1.1183   0.02822   0.02062  -0.0694   0.0272   0.5292
   9.000   1.1280   0.02956   0.02202  -0.0685   0.0271   0.5374
   9.250   1.1375   0.03094   0.02346  -0.0676   0.0270   0.5434
   9.500   1.1468   0.03236   0.02494  -0.0668   0.0268   0.5555
   9.750   1.1548   0.03393   0.02655  -0.0660   0.0267   0.5588
  10.000   1.1640   0.03543   0.02811  -0.0653   0.0266   0.5654
  10.250   1.1713   0.03715   0.02989  -0.0646   0.0264   0.5729
  10.500   1.1783   0.03892   0.03171  -0.0639   0.0261   0.5786
  10.750   1.1851   0.04076   0.03362  -0.0633   0.0259   0.5831
  11.000   1.1937   0.04247   0.03538  -0.0629   0.0258   0.5884
  11.250   1.2002   0.04444   0.03742  -0.0624   0.0257   0.5948
  11.500   1.2074   0.04633   0.03938  -0.0620   0.0255   0.6026
  11.750   1.2129   0.04848   0.04159  -0.0616   0.0254   0.6090
  12.000   1.2169   0.05080   0.04397  -0.0612   0.0251   0.6164
  12.250   1.2263   0.05262   0.04584  -0.0610   0.0250   0.6210
  12.500   1.2384   0.05420   0.04749  -0.0610   0.0248   0.6315
  12.750   1.2504   0.05577   0.04913  -0.0610   0.0245   0.6427
  13.000   1.2609   0.05752   0.05096  -0.0610   0.0243   0.6533
  13.250   1.2705   0.05942   0.05297  -0.0611   0.0239   0.6769
  13.500   1.2793   0.06144   0.05507  -0.0611   0.0237   0.6934
  13.750   1.2885   0.06340   0.05713  -0.0612   0.0236   0.7085
  14.000   1.2987   0.06526   0.05910  -0.0613   0.0231   0.7333
  14.250   1.3064   0.06749   0.06143  -0.0615   0.0229   0.7534
  14.500   1.3159   0.06948   0.06352  -0.0617   0.0224   0.7780
  14.750   1.3248   0.07150   0.06568  -0.0619   0.0222   0.8146
  15.000   1.3287   0.07325   0.06779  -0.0611   0.0219   1.0000
  15.250   1.3348   0.07578   0.07036  -0.0614   0.0217   1.0000
  15.500   1.3407   0.07834   0.07296  -0.0618   0.0215   1.0000
  15.750   1.3479   0.08074   0.07540  -0.0622   0.0213   1.0000
  16.000   1.3586   0.08276   0.07747  -0.0626   0.0211   1.0000
  16.250   1.3667   0.08513   0.07989  -0.0631   0.0210   1.0000
  16.500   1.3777   0.08710   0.08190  -0.0636   0.0207   1.0000
  16.750   1.3879   0.08915   0.08400  -0.0641   0.0204   1.0000
  17.000   1.3988   0.09112   0.08601  -0.0646   0.0198   1.0000
  17.250   1.4061   0.09364   0.08859  -0.0652   0.0194   1.0000
  17.500   1.4143   0.09602   0.09101  -0.0659   0.0190   1.0000
  17.750   1.4233   0.09829   0.09332  -0.0665   0.0185   1.0000
  18.000   1.4335   0.10039   0.09546  -0.0671   0.0181   1.0000
  18.250   1.4416   0.10279   0.09790  -0.0679   0.0178   1.0000
  18.500   1.4461   0.10573   0.10090  -0.0688   0.0175   1.0000
  18.750   1.4529   0.10833   0.10356  -0.0696   0.0169   1.0000
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