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FX S 02-196 AIRFOIL (fxs02196-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: FX S 02-196 AIRFOIL (fxs02196-il)
Reynolds number: 200,000
Max Cl/Cd: 68.41 at α=7.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fxs02196-il-200000.txt
Download as CSV file: xf-fxs02196-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.1357   0.10846   0.10489  -0.0856   0.8546   0.0760
 -12.750  -0.2202   0.10739   0.10403  -0.0838   0.9294   0.0726
 -12.500  -0.4830   0.05727   0.05283  -0.1165   0.9246   0.0362
 -12.250  -0.4798   0.05263   0.04791  -0.1205   0.9030   0.0360
 -12.000  -0.4881   0.04902   0.04400  -0.1216   0.8807   0.0358
 -11.750  -0.4992   0.04618   0.04089  -0.1207   0.8610   0.0357
 -11.500  -0.5169   0.04366   0.03803  -0.1185   0.8432   0.0358
 -11.250  -0.5396   0.04170   0.03569  -0.1147   0.8277   0.0360
 -11.000  -0.5573   0.03975   0.03320  -0.1111   0.8154   0.0363
 -10.750  -0.5259   0.03845   0.03216  -0.1120   0.8044   0.0382
 -10.500  -0.5300   0.03665   0.02988  -0.1094   0.7947   0.0395
 -10.250  -0.5215   0.03467   0.02766  -0.1080   0.7842   0.0407
 -10.000  -0.5027   0.03324   0.02608  -0.1074   0.7758   0.0418
  -9.750  -0.4867   0.03163   0.02421  -0.1064   0.7668   0.0426
  -9.500  -0.4704   0.03021   0.02247  -0.1053   0.7583   0.0434
  -9.250  -0.4481   0.02892   0.02104  -0.1049   0.7512   0.0448
  -9.000  -0.4252   0.02801   0.02012  -0.1046   0.7429   0.0462
  -8.750  -0.4051   0.02710   0.01895  -0.1038   0.7361   0.0477
  -8.500  -0.3799   0.02614   0.01794  -0.1037   0.7301   0.0489
  -8.250  -0.3536   0.02520   0.01697  -0.1034   0.7231   0.0492
  -8.000  -0.3269   0.02434   0.01605  -0.1030   0.7172   0.0493
  -7.750  -0.3015   0.02363   0.01526  -0.1025   0.7122   0.0496
  -7.500  -0.2789   0.02298   0.01464  -0.1018   0.7064   0.0500
  -7.250  -0.2581   0.02237   0.01403  -0.1009   0.7007   0.0505
  -7.000  -0.2384   0.02179   0.01341  -0.1000   0.6958   0.0511
  -6.750  -0.2192   0.02125   0.01280  -0.0991   0.6916   0.0517
  -6.500  -0.2009   0.02072   0.01227  -0.0983   0.6870   0.0525
  -6.250  -0.1818   0.02021   0.01179  -0.0976   0.6822   0.0535
  -6.000  -0.1611   0.01974   0.01128  -0.0972   0.6779   0.0550
  -5.750  -0.1389   0.01931   0.01075  -0.0968   0.6741   0.0570
  -5.500  -0.1160   0.01892   0.01028  -0.0967   0.6707   0.0601
  -5.250  -0.0934   0.01851   0.00984  -0.0965   0.6668   0.0650
  -5.000  -0.0710   0.01791   0.00921  -0.0964   0.6624   0.0735
  -4.750  -0.0474   0.01729   0.00873  -0.0966   0.6583   0.1032
  -4.500  -0.0244   0.01628   0.00808  -0.0972   0.6549   0.1975
  -4.250  -0.0014   0.01499   0.00760  -0.0982   0.6518   0.3856
  -4.000   0.0272   0.01512   0.00776  -0.0985   0.6486   0.4454
  -3.750   0.0548   0.01523   0.00789  -0.0986   0.6448   0.4631
  -3.500   0.0830   0.01534   0.00795  -0.0988   0.6408   0.4767
  -3.250   0.1118   0.01541   0.00792  -0.0991   0.6371   0.4863
  -3.000   0.1411   0.01548   0.00788  -0.0994   0.6337   0.4958
  -2.750   0.1707   0.01557   0.00783  -0.0998   0.6300   0.5048
  -2.500   0.1979   0.01566   0.00791  -0.0997   0.6251   0.5112
  -2.250   0.2258   0.01565   0.00783  -0.0999   0.6194   0.5177
  -2.000   0.2548   0.01559   0.00767  -0.1000   0.6141   0.5229
  -1.750   0.2841   0.01561   0.00758  -0.1002   0.6094   0.5277
  -1.500   0.3117   0.01572   0.00767  -0.1003   0.6053   0.5334
  -1.250   0.3397   0.01580   0.00771  -0.1006   0.6013   0.5394
  -1.000   0.3673   0.01590   0.00783  -0.1006   0.5977   0.5454
  -0.750   0.3959   0.01605   0.00796  -0.1008   0.5945   0.5558
  -0.500   0.4246   0.01617   0.00803  -0.1010   0.5918   0.5631
  -0.250   0.4533   0.01632   0.00815  -0.1012   0.5891   0.5695
   0.000   0.4818   0.01651   0.00830  -0.1015   0.5864   0.5758
   0.250   0.5085   0.01660   0.00843  -0.1015   0.5832   0.5813
   0.500   0.5344   0.01670   0.00862  -0.1011   0.5787   0.5886
   1.000   0.5901   0.01680   0.00868  -0.1009   0.5699   0.6065
   1.250   0.6187   0.01687   0.00870  -0.1012   0.5660   0.6114
   1.500   0.6452   0.01694   0.00881  -0.1013   0.5626   0.6159
   1.750   0.6726   0.01700   0.00889  -0.1015   0.5593   0.6205
   2.000   0.6987   0.01706   0.00902  -0.1012   0.5559   0.6261
   2.250   0.7262   0.01713   0.00909  -0.1011   0.5521   0.6353
   2.500   0.7541   0.01713   0.00905  -0.1010   0.5478   0.6441
   2.750   0.7785   0.01722   0.00923  -0.1004   0.5430   0.6515
   3.000   0.8045   0.01727   0.00932  -0.1004   0.5379   0.6586
   3.250   0.8308   0.01722   0.00931  -0.1003   0.5337   0.6629
   3.500   0.8577   0.01721   0.00933  -0.1002   0.5303   0.6669
   3.750   0.8861   0.01725   0.00934  -0.1005   0.5274   0.6711
   4.000   0.9136   0.01733   0.00944  -0.1008   0.5245   0.6754
   4.250   0.9394   0.01744   0.00962  -0.1010   0.5213   0.6795
   4.500   0.9647   0.01750   0.00978  -0.1009   0.5182   0.6829
   4.750   0.9901   0.01756   0.00994  -0.1007   0.5152   0.6865
   5.000   1.0162   0.01762   0.01005  -0.1007   0.5121   0.6909
   5.250   1.0434   0.01766   0.01012  -0.1009   0.5092   0.6958
   5.500   1.0722   0.01773   0.01016  -0.1014   0.5065   0.7009
   5.750   1.0955   0.01784   0.01041  -0.1010   0.5036   0.7054
   6.000   1.1179   0.01798   0.01070  -0.1004   0.4999   0.7107
   6.250   1.1411   0.01807   0.01088  -0.0999   0.4951   0.7170
   6.500   1.1658   0.01809   0.01095  -0.0997   0.4907   0.7234
   6.750   1.1912   0.01811   0.01101  -0.0994   0.4872   0.7298
   7.000   1.2126   0.01830   0.01133  -0.0987   0.4832   0.7377
   7.250   1.2313   0.01848   0.01167  -0.0976   0.4778   0.7457
   7.500   1.2506   0.01858   0.01187  -0.0964   0.4720   0.7545
   7.750   1.2732   0.01861   0.01191  -0.0957   0.4663   0.7649
   8.000   1.2845   0.01891   0.01245  -0.0933   0.4596   0.7756
   8.250   1.2949   0.01913   0.01282  -0.0907   0.4521   0.7886
   8.500   1.3063   0.01937   0.01317  -0.0883   0.4451   0.8045
   8.750   1.3122   0.01980   0.01381  -0.0852   0.4369   0.8222
   9.000   1.3188   0.02017   0.01430  -0.0822   0.4276   0.8466
   9.250   1.3183   0.02061   0.01492  -0.0780   0.4173   0.8869
   9.500   1.3214   0.02109   0.01549  -0.0751   0.4042   1.0000
   9.750   1.3269   0.02220   0.01654  -0.0735   0.3801   1.0000
  10.000   1.3193   0.02399   0.01810  -0.0706   0.3542   1.0000
  10.250   1.3101   0.02619   0.02017  -0.0679   0.3349   1.0000
  10.500   1.3028   0.02854   0.02246  -0.0658   0.3087   1.0000
  10.750   1.2899   0.03144   0.02524  -0.0635   0.2918   1.0000
  11.000   1.2830   0.03408   0.02784  -0.0619   0.2788   1.0000
  11.250   1.2751   0.03695   0.03068  -0.0605   0.2495   1.0000
  11.500   1.2575   0.04076   0.03434  -0.0588   0.2330   1.0000
  11.750   1.2483   0.04404   0.03754  -0.0578   0.2200   1.0000
  12.000   1.2467   0.04678   0.04027  -0.0571   0.1907   1.0000
  12.250   1.2362   0.05044   0.04380  -0.0564   0.1795   1.0000
  12.500   1.2333   0.05346   0.04679  -0.0559   0.1672   1.0000
  12.750   1.2330   0.05630   0.04961  -0.0556   0.1411   1.0000
  13.000   1.2254   0.05998   0.05314  -0.0553   0.1313   1.0000
  13.250   1.2227   0.06323   0.05638  -0.0552   0.1211   1.0000
  13.500   1.2264   0.06584   0.05898  -0.0552   0.0996   1.0000
  13.750   1.2216   0.06948   0.06250  -0.0553   0.0920   1.0000
  14.000   1.2157   0.07333   0.06629  -0.0554   0.0868   1.0000
  14.250   1.2186   0.07619   0.06923  -0.0555   0.0805   1.0000
  14.500   1.2249   0.07872   0.07186  -0.0558   0.0742   1.0000
  14.750   1.2312   0.08125   0.07443  -0.0561   0.0696   1.0000
  15.000   1.2367   0.08390   0.07708  -0.0564   0.0665   1.0000
  15.250   1.2406   0.08678   0.07996  -0.0569   0.0644   1.0000
  15.500   1.2437   0.08977   0.08295  -0.0574   0.0627   1.0000
  15.750   1.2464   0.09280   0.08594  -0.0579   0.0612   1.0000
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