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FX S 03-182 AIRFOIL (fxs03182-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX S 03-182 AIRFOIL (fxs03182-il)
Reynolds number: 1,000,000
Max Cl/Cd: 110.82 at α=3.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fxs03182-il-1000000.txt
Download as CSV file: xf-fxs03182-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX S 03-182 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
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.1403   0.12095   0.11886  -0.0960   0.8668   0.0123
 -14.750  -0.1382   0.11777   0.11562  -0.0975   0.8545   0.0130
 -14.500  -0.3149   0.12690   0.12523  -0.0730   0.9609   0.0107
 -10.500  -0.4656   0.02266   0.01717  -0.1245   0.7623   0.0058
 -10.250  -0.4504   0.02207   0.01649  -0.1235   0.7552   0.0057
 -10.000  -0.4380   0.02081   0.01516  -0.1218   0.7494   0.0050
  -9.750  -0.4248   0.01996   0.01421  -0.1205   0.7433   0.0048
  -9.500  -0.4122   0.01917   0.01331  -0.1190   0.7377   0.0047
  -9.250  -0.4005   0.01828   0.01233  -0.1174   0.7325   0.0045
  -9.000  -0.3871   0.01761   0.01158  -0.1160   0.7273   0.0044
  -8.750  -0.3747   0.01691   0.01080  -0.1143   0.7227   0.0043
  -8.500  -0.3618   0.01625   0.01008  -0.1128   0.7182   0.0043
  -8.250  -0.3506   0.01557   0.00934  -0.1110   0.7137   0.0042
  -8.000  -0.3414   0.01494   0.00864  -0.1087   0.7094   0.0042
  -7.750  -0.3344   0.01440   0.00806  -0.1060   0.7057   0.0043
  -7.500  -0.3209   0.01384   0.00744  -0.1044   0.7018   0.0043
  -7.250  -0.3033   0.01342   0.00696  -0.1033   0.6981   0.0043
  -7.000  -0.2844   0.01304   0.00651  -0.1024   0.6945   0.0043
  -6.750  -0.2646   0.01258   0.00601  -0.1016   0.6917   0.0046
  -6.500  -0.2422   0.01225   0.00564  -0.1011   0.6888   0.0046
  -6.250  -0.2199   0.01189   0.00522  -0.1006   0.6859   0.0050
  -6.000  -0.1960   0.01162   0.00488  -0.1004   0.6832   0.0052
  -5.750  -0.1717   0.01137   0.00454  -0.1002   0.6803   0.0058
  -5.500  -0.1459   0.01113   0.00428  -0.1002   0.6783   0.0064
  -5.250  -0.1211   0.01079   0.00398  -0.1002   0.6760   0.0101
  -5.000  -0.0939   0.01067   0.00384  -0.1005   0.6738   0.0147
  -4.750  -0.0671   0.01050   0.00368  -0.1007   0.6716   0.0182
  -4.500  -0.0399   0.01038   0.00353  -0.1010   0.6695   0.0207
  -4.250  -0.0125   0.01028   0.00340  -0.1013   0.6673   0.0228
  -4.000   0.0150   0.01013   0.00326  -0.1016   0.6653   0.0269
  -3.750   0.0426   0.00992   0.00310  -0.1020   0.6635   0.0372
  -3.500   0.0706   0.00978   0.00298  -0.1024   0.6617   0.0461
  -3.250   0.0977   0.00937   0.00277  -0.1030   0.6599   0.1040
  -3.000   0.1237   0.00804   0.00223  -0.1045   0.6581   0.3247
  -2.750   0.1536   0.00700   0.00187  -0.1064   0.6565   0.5198
  -2.500   0.1835   0.00699   0.00191  -0.1071   0.6549   0.5526
  -2.250   0.2133   0.00704   0.00194  -0.1077   0.6532   0.5681
  -2.000   0.2434   0.00714   0.00202  -0.1084   0.6513   0.5820
  -1.750   0.2730   0.00717   0.00206  -0.1090   0.6502   0.5896
  -1.500   0.3028   0.00721   0.00209  -0.1096   0.6489   0.5949
  -1.250   0.3323   0.00724   0.00213  -0.1101   0.6474   0.6000
  -1.000   0.3620   0.00729   0.00218  -0.1107   0.6458   0.6046
  -0.750   0.3918   0.00736   0.00221  -0.1113   0.6443   0.6088
  -0.500   0.4211   0.00740   0.00229  -0.1118   0.6429   0.6148
  -0.250   0.4505   0.00749   0.00237  -0.1123   0.6407   0.6209
   0.000   0.4800   0.00760   0.00241  -0.1129   0.6373   0.6241
   0.250   0.5081   0.00752   0.00237  -0.1131   0.6334   0.6257
   0.500   0.5369   0.00751   0.00238  -0.1135   0.6304   0.6279
   0.750   0.5658   0.00754   0.00242  -0.1139   0.6276   0.6310
   1.000   0.5948   0.00761   0.00247  -0.1144   0.6252   0.6342
   1.250   0.6238   0.00768   0.00252  -0.1149   0.6219   0.6362
   1.500   0.6517   0.00763   0.00249  -0.1151   0.6162   0.6371
   1.750   0.6792   0.00767   0.00247  -0.1152   0.6088   0.6380
   2.000   0.7076   0.00762   0.00246  -0.1156   0.6044   0.6394
   2.250   0.7354   0.00760   0.00246  -0.1158   0.5983   0.6407
   2.500   0.7629   0.00763   0.00248  -0.1160   0.5913   0.6420
   2.750   0.7902   0.00765   0.00249  -0.1161   0.5820   0.6433
   3.000   0.8176   0.00768   0.00253  -0.1163   0.5716   0.6447
   3.250   0.8442   0.00774   0.00257  -0.1163   0.5588   0.6462
   3.500   0.8699   0.00785   0.00263  -0.1161   0.5413   0.6475
   3.750   0.8905   0.00816   0.00277  -0.1150   0.5005   0.6489
   4.000   0.8941   0.00925   0.00337  -0.1108   0.4046   0.6503
   4.250   0.8868   0.01071   0.00423  -0.1048   0.2886   0.6516
   4.500   0.8812   0.01173   0.00487  -0.0990   0.2114   0.6527
   4.750   0.8704   0.01291   0.00569  -0.0924   0.1329   0.6545
   5.000   0.8733   0.01376   0.00635  -0.0885   0.0893   0.6562
   5.250   0.8845   0.01435   0.00688  -0.0861   0.0668   0.6579
   5.500   0.8942   0.01504   0.00750  -0.0836   0.0460   0.6597
   5.750   0.9051   0.01574   0.00812  -0.0814   0.0304   0.6616
   6.000   0.9223   0.01619   0.00859  -0.0802   0.0267   0.6635
   6.250   0.9393   0.01668   0.00909  -0.0791   0.0233   0.6653
   6.500   0.9501   0.01749   0.00987  -0.0771   0.0131   0.6669
   6.750   0.9649   0.01813   0.01052  -0.0757   0.0117   0.6689
   7.000   0.9807   0.01874   0.01116  -0.0746   0.0101   0.6710
   7.250   0.9969   0.01936   0.01181  -0.0735   0.0094   0.6732
   7.500   1.0137   0.01997   0.01244  -0.0726   0.0091   0.6754
   7.750   1.0301   0.02061   0.01311  -0.0717   0.0086   0.6777
   8.000   1.0462   0.02130   0.01382  -0.0707   0.0081   0.6801
   9.000   1.1033   0.02466   0.01731  -0.0666   0.0028   0.6909
   9.250   1.1165   0.02563   0.01832  -0.0655   0.0026   0.6939
   9.500   1.1291   0.02667   0.01940  -0.0644   0.0024   0.6966
   9.750   1.1424   0.02765   0.02045  -0.0635   0.0024   0.6999
  10.000   1.1552   0.02869   0.02156  -0.0625   0.0023   0.7033
  10.250   1.1683   0.02975   0.02267  -0.0617   0.0023   0.7069
  10.500   1.1808   0.03087   0.02384  -0.0608   0.0022   0.7104
  10.750   1.1927   0.03205   0.02509  -0.0599   0.0022   0.7142
  11.000   1.2048   0.03325   0.02635  -0.0590   0.0021   0.7183
  11.250   1.2160   0.03454   0.02771  -0.0582   0.0021   0.7227
  11.500   1.2271   0.03588   0.02911  -0.0574   0.0021   0.7271
  11.750   1.2373   0.03731   0.03062  -0.0565   0.0020   0.7319
  12.000   1.2471   0.03881   0.03221  -0.0557   0.0020   0.7374
  12.250   1.2559   0.04043   0.03391  -0.0549   0.0020   0.7427
  12.500   1.2665   0.04192   0.03549  -0.0543   0.0019   0.7487
  12.750   1.2759   0.04356   0.03720  -0.0536   0.0019   0.7550
  13.000   1.2846   0.04529   0.03902  -0.0530   0.0018   0.7615
  13.250   1.2933   0.04706   0.04088  -0.0524   0.0018   0.7687
  13.500   1.3007   0.04899   0.04291  -0.0518   0.0018   0.7761
  13.750   1.3076   0.05102   0.04503  -0.0513   0.0018   0.7843
  14.000   1.3133   0.05322   0.04735  -0.0508   0.0017   0.7930
  14.250   1.3179   0.05559   0.04982  -0.0504   0.0017   0.8021
  14.500   1.3225   0.05801   0.05236  -0.0500   0.0017   0.8123
  14.750   1.3277   0.06040   0.05488  -0.0498   0.0017   0.8237
  15.000   1.3297   0.06322   0.05783  -0.0495   0.0016   0.8364
  15.250   1.3328   0.06593   0.06068  -0.0494   0.0016   0.8517
  15.500   1.3349   0.06876   0.06365  -0.0492   0.0016   0.8716
  15.750   1.3335   0.07160   0.06671  -0.0485   0.0016   0.9105
  16.000   1.3309   0.07426   0.06954  -0.0476   0.0016   1.0000
  16.250   1.3312   0.07769   0.07306  -0.0480   0.0017   1.0000
  16.500   1.3310   0.08125   0.07673  -0.0485   0.0017   1.0000
  16.750   1.3301   0.08496   0.08054  -0.0491   0.0017   1.0000
  17.000   1.3279   0.08897   0.08466  -0.0499   0.0017   1.0000
  17.250   1.3249   0.09317   0.08897  -0.0509   0.0017   1.0000
  17.500   1.3226   0.09735   0.09326  -0.0520   0.0017   1.0000
  17.750   1.3180   0.10195   0.09798  -0.0534   0.0018   1.0000
  18.000   1.3129   0.10672   0.10288  -0.0549   0.0018   1.0000
  18.250   1.3072   0.11168   0.10796  -0.0567   0.0018   1.0000
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