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WORTMANN FX 2 AIRFOIL (fx2-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 2 AIRFOIL (fx2-il)
Reynolds number: 500,000
Max Cl/Cd: 50.48 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx2-il-500000-n5.txt
Download as CSV file: xf-fx2-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 2 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.5210   0.09132   0.08647  -0.1598   0.8226   0.0093
 -19.500  -0.5337   0.08567   0.08071  -0.1629   0.8224   0.0094
 -19.250  -0.5449   0.08048   0.07541  -0.1657   0.8221   0.0094
 -19.000  -0.5538   0.07576   0.07057  -0.1682   0.8218   0.0094
 -18.750  -0.5605   0.07145   0.06616  -0.1706   0.8215   0.0096
 -18.500  -0.5660   0.06749   0.06211  -0.1726   0.8212   0.0097
 -18.250  -0.5663   0.06430   0.05883  -0.1743   0.8209   0.0098
 -18.000  -0.5690   0.06095   0.05538  -0.1758   0.8205   0.0099
 -17.750  -0.5700   0.05793   0.05228  -0.1771   0.8202   0.0100
 -17.500  -0.5690   0.05523   0.04949  -0.1781   0.8198   0.0103
 -17.250  -0.5670   0.05276   0.04692  -0.1790   0.8195   0.0104
 -17.000  -0.5628   0.05057   0.04464  -0.1797   0.8191   0.0107
 -16.750  -0.5605   0.04829   0.04227  -0.1803   0.8187   0.0108
 -16.500  -0.5552   0.04637   0.04027  -0.1807   0.8183   0.0110
 -16.250  -0.5482   0.04465   0.03846  -0.1810   0.8180   0.0113
 -16.000  -0.5418   0.04294   0.03666  -0.1812   0.8176   0.0115
 -15.750  -0.5376   0.04111   0.03477  -0.1812   0.8172   0.0118
 -15.500  -0.5309   0.03953   0.03314  -0.1812   0.8168   0.0122
 -15.250  -0.5237   0.03805   0.03161  -0.1811   0.8164   0.0124
 -15.000  -0.5145   0.03675   0.03025  -0.1809   0.8160   0.0127
 -14.750  -0.5038   0.03561   0.02904  -0.1808   0.8156   0.0131
 -14.500  -0.4933   0.03449   0.02786  -0.1805   0.8153   0.0135
 -14.250  -0.4828   0.03339   0.02671  -0.1801   0.8149   0.0139
 -14.000  -0.4703   0.03247   0.02573  -0.1798   0.8145   0.0146
 -13.750  -0.4596   0.03145   0.02465  -0.1793   0.8141   0.0152
 -13.500  -0.4483   0.03050   0.02367  -0.1788   0.8136   0.0158
 -13.250  -0.4362   0.02964   0.02277  -0.1782   0.8131   0.0164
 -13.000  -0.4243   0.02878   0.02187  -0.1776   0.8126   0.0171
 -12.750  -0.4105   0.02806   0.02110  -0.1770   0.8122   0.0181
 -12.500  -0.3970   0.02735   0.02034  -0.1764   0.8118   0.0189
 -12.250  -0.3851   0.02658   0.01956  -0.1755   0.8114   0.0206
 -12.000  -0.3715   0.02593   0.01890  -0.1748   0.8110   0.0219
 -11.750  -0.3573   0.02533   0.01827  -0.1741   0.8106   0.0235
 -11.500  -0.3441   0.02472   0.01766  -0.1732   0.8102   0.0262
 -11.250  -0.3299   0.02418   0.01711  -0.1724   0.8098   0.0286
 -11.000  -0.3152   0.02370   0.01664  -0.1715   0.8094   0.0319
 -10.750  -0.3005   0.02324   0.01619  -0.1706   0.8091   0.0357
 -10.500  -0.2860   0.02279   0.01574  -0.1696   0.8088   0.0386
 -10.250  -0.2711   0.02237   0.01533  -0.1686   0.8084   0.0420
 -10.000  -0.2552   0.02201   0.01495  -0.1677   0.8081   0.0447
  -9.750  -0.2414   0.02158   0.01453  -0.1665   0.8077   0.0474
  -9.500  -0.2270   0.02119   0.01415  -0.1653   0.8073   0.0496
  -9.250  -0.2118   0.02085   0.01380  -0.1642   0.8069   0.0522
  -9.000  -0.1963   0.02053   0.01346  -0.1631   0.8065   0.0540
  -8.750  -0.1837   0.02013   0.01307  -0.1616   0.8059   0.0565
  -8.500  -0.1712   0.01974   0.01268  -0.1600   0.8052   0.0590
  -8.250  -0.1580   0.01938   0.01233  -0.1585   0.8046   0.0614
  -8.000  -0.1441   0.01908   0.01201  -0.1570   0.8040   0.0640
  -7.750  -0.1291   0.01882   0.01174  -0.1557   0.8034   0.0662
  -7.500  -0.1190   0.01842   0.01135  -0.1536   0.8028   0.0697
  -7.250  -0.1086   0.01805   0.01100  -0.1515   0.8021   0.0733
  -7.000  -0.0973   0.01773   0.01068  -0.1495   0.8015   0.0760
  -6.750  -0.0859   0.01743   0.01037  -0.1475   0.8008   0.0791
  -6.500  -0.0763   0.01710   0.01004  -0.1452   0.8001   0.0840
  -6.250  -0.0703   0.01672   0.00970  -0.1422   0.7994   0.0917
  -6.000  -0.0705   0.01635   0.00939  -0.1382   0.7985   0.1046
  -5.750  -0.0789   0.01590   0.00905  -0.1329   0.7975   0.1288
  -5.500  -0.0739   0.01537   0.00861  -0.1301   0.7966   0.1613
  -5.250  -0.0657   0.01486   0.00826  -0.1278   0.7959   0.2026
  -5.000  -0.0566   0.01423   0.00786  -0.1257   0.7953   0.2645
  -4.750  -0.0462   0.01340   0.00738  -0.1241   0.7946   0.3559
  -4.500  -0.0330   0.01259   0.00698  -0.1229   0.7940   0.4551
  -4.250  -0.0272   0.01252   0.00722  -0.1194   0.7925   0.5312
  -4.000  -0.0227   0.01286   0.00764  -0.1154   0.7900   0.5522
  -3.750  -0.0134   0.01313   0.00797  -0.1122   0.7878   0.5702
  -3.500  -0.0005   0.01339   0.00829  -0.1097   0.7861   0.5866
  -3.250   0.0170   0.01362   0.00857  -0.1081   0.7848   0.5995
  -3.000   0.0381   0.01382   0.00880  -0.1071   0.7838   0.6117
  -2.750   0.0637   0.01394   0.00891  -0.1069   0.7831   0.6225
  -2.500   0.0902   0.01411   0.00908  -0.1069   0.7825   0.6298
  -2.250   0.1165   0.01421   0.00911  -0.1071   0.7819   0.6365
  -2.000   0.1435   0.01435   0.00925  -0.1072   0.7814   0.6394
  -1.750   0.1726   0.01444   0.00932  -0.1078   0.7810   0.6430
  -1.500   0.2038   0.01450   0.00932  -0.1089   0.7807   0.6487
  -1.250   0.2361   0.01453   0.00932  -0.1101   0.7803   0.6518
  -1.000   0.2689   0.01453   0.00931  -0.1115   0.7800   0.6531
  -0.750   0.3022   0.01453   0.00929  -0.1130   0.7797   0.6545
   0.750   0.2653   0.01941   0.01418  -0.0788   0.7446   0.6672
   1.000   0.2918   0.01945   0.01422  -0.0789   0.7432   0.6684
   1.250   0.3203   0.01942   0.01420  -0.0794   0.7422   0.6698
   1.500   0.3494   0.01937   0.01415  -0.0800   0.7414   0.6712
   1.750   0.3795   0.01928   0.01407  -0.0807   0.7407   0.6728
   2.000   0.4098   0.01918   0.01397  -0.0815   0.7402   0.6746
   2.250   0.4408   0.01905   0.01384  -0.0825   0.7396   0.6764
   2.500   0.4722   0.01890   0.01368  -0.0835   0.7392   0.6783
   2.750   0.5032   0.01873   0.01350  -0.0844   0.7385   0.6799
   3.500   0.5498   0.01947   0.01434  -0.0793   0.7236   0.6833
   3.750   0.5908   0.01886   0.01376  -0.0817   0.7252   0.6844
   4.250   0.6168   0.01958   0.01454  -0.0775   0.7125   0.6871
   4.750   0.6536   0.01983   0.01483  -0.0751   0.6981   0.6898
   5.000   0.6642   0.02039   0.01540  -0.0727   0.6869   0.6912
   5.250   0.6990   0.01987   0.01490  -0.0741   0.6833   0.6924
   5.500   0.7206   0.01996   0.01499  -0.0734   0.6725   0.6937
   5.750   0.7633   0.01899   0.01398  -0.0759   0.6598   0.6947
   6.000   0.8112   0.01784   0.01276  -0.0791   0.6444   0.6956
   6.250   0.8502   0.01704   0.01183  -0.0809   0.6207   0.6965
   6.500   0.8687   0.01721   0.01191  -0.0796   0.5957   0.6974
   6.750   0.8802   0.01771   0.01230  -0.0773   0.5710   0.6984
   7.000   0.8871   0.01845   0.01292  -0.0743   0.5441   0.6994
   7.250   0.8861   0.01954   0.01384  -0.0701   0.5084   0.7004
   7.500   0.8858   0.02067   0.01480  -0.0662   0.4713   0.7016
   7.750   0.8849   0.02192   0.01586  -0.0624   0.4341   0.7026
   8.000   0.8878   0.02305   0.01683  -0.0592   0.3987   0.7036
   8.250   0.8888   0.02432   0.01787  -0.0559   0.3551   0.7045
   8.500   0.8908   0.02563   0.01894  -0.0528   0.3112   0.7054
   8.750   0.8930   0.02697   0.02001  -0.0499   0.2601   0.7062
   9.000   0.8987   0.02817   0.02097  -0.0475   0.2154   0.7070
   9.250   0.9065   0.02930   0.02191  -0.0455   0.1790   0.7077
   9.500   0.9195   0.03017   0.02270  -0.0442   0.1596   0.7084
   9.750   0.9302   0.03120   0.02358  -0.0426   0.1309   0.7091
  10.000   0.9398   0.03233   0.02453  -0.0410   0.0990   0.7097
  10.250   0.9527   0.03328   0.02539  -0.0398   0.0840   0.7104
  10.500   0.9669   0.03417   0.02625  -0.0388   0.0761   0.7112
  10.750   0.9823   0.03495   0.02706  -0.0379   0.0704   0.7121
  11.000   0.9975   0.03577   0.02790  -0.0370   0.0652   0.7128
  11.250   1.0126   0.03662   0.02876  -0.0361   0.0601   0.7134
  11.500   1.0282   0.03745   0.02961  -0.0354   0.0543   0.7141
  11.750   1.0420   0.03841   0.03058  -0.0345   0.0479   0.7147
  12.000   1.0538   0.03952   0.03165  -0.0334   0.0359   0.7157
  12.250   1.0641   0.04078   0.03283  -0.0322   0.0260   0.7164
  12.500   1.0759   0.04196   0.03402  -0.0312   0.0224   0.7173
  12.750   1.0882   0.04313   0.03522  -0.0302   0.0200   0.7180
  13.000   1.1001   0.04434   0.03648  -0.0293   0.0183   0.7186
  13.250   1.1120   0.04558   0.03775  -0.0285   0.0170   0.7194
  13.500   1.1242   0.04680   0.03906  -0.0277   0.0162   0.7202
  13.750   1.1361   0.04806   0.04038  -0.0269   0.0153   0.7210
  14.000   1.1474   0.04941   0.04177  -0.0261   0.0145   0.7219
  14.250   1.1563   0.05099   0.04340  -0.0253   0.0136   0.7226
  14.500   1.1663   0.05251   0.04499  -0.0245   0.0132   0.7231
  14.750   1.1771   0.05398   0.04653  -0.0239   0.0127   0.7237
  15.000   1.1867   0.05558   0.04819  -0.0232   0.0122   0.7241
  15.250   1.1965   0.05718   0.04987  -0.0227   0.0119   0.7245
  15.500   1.2044   0.05900   0.05176  -0.0221   0.0114   0.7249
  15.750   1.2122   0.06086   0.05368  -0.0215   0.0110   0.7252
  16.000   1.2178   0.06298   0.05586  -0.0210   0.0106   0.7256
  16.250   1.2248   0.06499   0.05794  -0.0206   0.0102   0.7259
  16.500   1.2302   0.06723   0.06027  -0.0202   0.0100   0.7262
  16.750   1.2372   0.06932   0.06246  -0.0199   0.0097   0.7266
  17.250   1.2474   0.07400   0.06732  -0.0196   0.0092   0.7274
  17.500   1.2519   0.07646   0.06987  -0.0195   0.0089   0.7278
  17.750   1.2559   0.07905   0.07255  -0.0196   0.0087   0.7282
  18.000   1.2588   0.08180   0.07539  -0.0197   0.0086   0.7287
  18.250   1.2600   0.08480   0.07849  -0.0200   0.0084   0.7291
  18.500   1.2603   0.08800   0.08178  -0.0203   0.0083   0.7295
  18.750   1.2576   0.09163   0.08550  -0.0209   0.0080   0.7299
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