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WORTMANN FX 05-188 AIRFOIL (fx05188-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 05-188 AIRFOIL (fx05188-il)
Reynolds number: 500,000
Max Cl/Cd: 97.84 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx05188-il-500000-n5.txt
Download as CSV file: xf-fx05188-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 05-188 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
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.6802   0.09838   0.09509  -0.0743   1.0000   0.0137
 -17.000  -0.7046   0.08939   0.08594  -0.0787   0.9821   0.0137
 -16.750  -0.7156   0.08031   0.07660  -0.0878   0.9481   0.0138
 -16.500  -0.7217   0.07192   0.06793  -0.0969   0.9350   0.0138
 -16.250  -0.7154   0.06564   0.06145  -0.1049   0.9234   0.0141
 -16.000  -0.7043   0.05967   0.05518  -0.1135   0.9084   0.0141
 -15.750  -0.6894   0.05542   0.05069  -0.1199   0.8905   0.0142
 -15.500  -0.6808   0.05184   0.04687  -0.1239   0.8750   0.0142
 -15.000  -0.6665   0.04673   0.04141  -0.1278   0.8540   0.0144
 -14.500  -0.6532   0.04249   0.03689  -0.1296   0.8395   0.0147
 -14.250  -0.6459   0.04061   0.03487  -0.1300   0.8330   0.0147
 -13.750  -0.6281   0.03739   0.03140  -0.1304   0.8225   0.0150
 -13.500  -0.6182   0.03597   0.02987  -0.1303   0.8175   0.0151
 -13.250  -0.6071   0.03467   0.02845  -0.1302   0.8129   0.0153
 -13.000  -0.5952   0.03346   0.02713  -0.1300   0.8086   0.0155
 -12.750  -0.5826   0.03230   0.02589  -0.1296   0.8043   0.0156
 -12.500  -0.5691   0.03121   0.02470  -0.1291   0.7998   0.0157
 -12.250  -0.5550   0.03021   0.02360  -0.1287   0.7958   0.0158
 -12.000  -0.5405   0.02928   0.02259  -0.1283   0.7920   0.0161
 -11.750  -0.5256   0.02838   0.02162  -0.1277   0.7877   0.0163
 -11.500  -0.5104   0.02752   0.02068  -0.1271   0.7833   0.0164
 -11.250  -0.4949   0.02673   0.01982  -0.1265   0.7793   0.0166
 -11.000  -0.4790   0.02598   0.01899  -0.1259   0.7756   0.0168
 -10.750  -0.4631   0.02523   0.01818  -0.1253   0.7719   0.0170
 -10.500  -0.4470   0.02455   0.01744  -0.1246   0.7682   0.0171
 -10.250  -0.4322   0.02377   0.01661  -0.1237   0.7647   0.0174
 -10.000  -0.4183   0.02298   0.01579  -0.1228   0.7614   0.0177
  -9.750  -0.4040   0.02223   0.01502  -0.1219   0.7580   0.0180
  -9.500  -0.3890   0.02156   0.01433  -0.1210   0.7547   0.0183
  -9.250  -0.3743   0.02090   0.01364  -0.1200   0.7513   0.0185
  -9.000  -0.3598   0.02025   0.01295  -0.1189   0.7480   0.0187
  -8.750  -0.3450   0.01964   0.01229  -0.1178   0.7450   0.0190
  -8.500  -0.3303   0.01902   0.01165  -0.1167   0.7420   0.0194
  -8.250  -0.3155   0.01844   0.01104  -0.1155   0.7391   0.0196
  -8.000  -0.3008   0.01787   0.01043  -0.1143   0.7363   0.0198
  -7.750  -0.2857   0.01735   0.00986  -0.1131   0.7336   0.0203
  -7.500  -0.2703   0.01685   0.00932  -0.1118   0.7312   0.0207
  -7.250  -0.2550   0.01637   0.00880  -0.1105   0.7290   0.0210
  -7.000  -0.2414   0.01586   0.00827  -0.1089   0.7267   0.0212
  -6.750  -0.2311   0.01534   0.00774  -0.1067   0.7241   0.0218
  -6.500  -0.2197   0.01493   0.00732  -0.1047   0.7217   0.0225
  -6.250  -0.2022   0.01455   0.00691  -0.1037   0.7195   0.0232
  -6.000  -0.1828   0.01420   0.00653  -0.1030   0.7173   0.0241
  -5.750  -0.1616   0.01390   0.00617  -0.1025   0.7151   0.0250
  -5.500  -0.1394   0.01362   0.00584  -0.1021   0.7130   0.0259
  -5.250  -0.1171   0.01331   0.00554  -0.1017   0.7112   0.0274
  -5.000  -0.0937   0.01304   0.00528  -0.1015   0.7093   0.0298
  -4.750  -0.0702   0.01275   0.00501  -0.1013   0.7071   0.0355
  -4.500  -0.0479   0.01229   0.00469  -0.1011   0.7049   0.0672
  -4.250  -0.0266   0.01161   0.00430  -0.1010   0.7026   0.1352
  -4.000  -0.0062   0.01038   0.00367  -0.1016   0.7004   0.2846
  -3.750   0.0207   0.00929   0.00316  -0.1032   0.6984   0.4342
  -3.500   0.0508   0.00892   0.00302  -0.1045   0.6965   0.5084
  -3.250   0.0804   0.00876   0.00298  -0.1052   0.6947   0.5433
  -3.000   0.1098   0.00866   0.00298  -0.1058   0.6925   0.5716
  -2.750   0.1392   0.00863   0.00300  -0.1063   0.6901   0.5887
  -2.500   0.1686   0.00865   0.00305  -0.1067   0.6877   0.6040
  -2.250   0.1980   0.00870   0.00310  -0.1072   0.6854   0.6150
  -2.000   0.2279   0.00874   0.00310  -0.1077   0.6832   0.6231
  -1.750   0.2574   0.00880   0.00314  -0.1082   0.6811   0.6282
  -1.500   0.2874   0.00886   0.00314  -0.1088   0.6790   0.6333
  -1.250   0.3168   0.00887   0.00314  -0.1094   0.6765   0.6381
  -1.000   0.3456   0.00890   0.00319  -0.1097   0.6736   0.6416
  -0.750   0.3749   0.00893   0.00321  -0.1102   0.6708   0.6454
  -0.500   0.4045   0.00896   0.00321  -0.1107   0.6682   0.6499
  -0.250   0.4340   0.00901   0.00323  -0.1112   0.6657   0.6542
   0.000   0.4631   0.00908   0.00328  -0.1116   0.6631   0.6577
   0.250   0.4918   0.00912   0.00334  -0.1119   0.6596   0.6617
   0.500   0.5207   0.00914   0.00336  -0.1124   0.6552   0.6656
   0.750   0.5498   0.00915   0.00334  -0.1128   0.6507   0.6687
   1.000   0.5781   0.00918   0.00336  -0.1130   0.6467   0.6707
   1.250   0.6065   0.00920   0.00343  -0.1133   0.6424   0.6728
   1.500   0.6349   0.00924   0.00348  -0.1136   0.6383   0.6751
   1.750   0.6634   0.00927   0.00352  -0.1139   0.6343   0.6776
   2.000   0.6919   0.00932   0.00355  -0.1143   0.6304   0.6803
   2.250   0.7206   0.00936   0.00360  -0.1147   0.6257   0.6828
   2.500   0.7491   0.00940   0.00365  -0.1150   0.6210   0.6848
   2.750   0.7767   0.00944   0.00370  -0.1151   0.6169   0.6865
   3.000   0.8044   0.00949   0.00378  -0.1153   0.6123   0.6882
   3.250   0.8316   0.00955   0.00387  -0.1154   0.6063   0.6900
   3.500   0.8579   0.00963   0.00393  -0.1152   0.5986   0.6921
   3.750   0.8843   0.00971   0.00402  -0.1151   0.5899   0.6942
   4.000   0.9107   0.00982   0.00412  -0.1151   0.5836   0.6963
   4.250   0.9379   0.00991   0.00423  -0.1152   0.5774   0.6982
   4.500   0.9641   0.01004   0.00434  -0.1151   0.5707   0.6998
   4.750   0.9893   0.01017   0.00447  -0.1149   0.5606   0.7013
   5.000   1.0117   0.01034   0.00462  -0.1140   0.5462   0.7030
   5.250   1.0321   0.01056   0.00481  -0.1128   0.5269   0.7046
   5.500   1.0508   0.01084   0.00502  -0.1113   0.5060   0.7063
   5.750   1.0679   0.01117   0.00528  -0.1095   0.4842   0.7080
   6.000   1.0839   0.01151   0.00556  -0.1075   0.4600   0.7096
   6.250   1.0938   0.01193   0.00588  -0.1044   0.4354   0.7114
   6.500   1.1008   0.01247   0.00630  -0.1009   0.4084   0.7133
   6.750   1.1042   0.01322   0.00691  -0.0969   0.3781   0.7152
   7.000   1.1073   0.01405   0.00760  -0.0932   0.3477   0.7169
   7.250   1.1044   0.01518   0.00854  -0.0888   0.3079   0.7187
   7.500   1.0980   0.01660   0.00976  -0.0842   0.2638   0.7205
   7.750   1.0941   0.01810   0.01108  -0.0804   0.2252   0.7222
   8.000   1.0933   0.01959   0.01241  -0.0772   0.1904   0.7240
   8.250   1.0960   0.02098   0.01369  -0.0747   0.1632   0.7259
   8.500   1.0992   0.02241   0.01500  -0.0724   0.1367   0.7277
   8.750   1.1012   0.02399   0.01643  -0.0700   0.1075   0.7294
   9.000   1.1079   0.02533   0.01769  -0.0683   0.0903   0.7310
   9.250   1.1169   0.02656   0.01888  -0.0668   0.0799   0.7324
   9.500   1.1271   0.02775   0.02006  -0.0656   0.0723   0.7337
  10.000   1.1500   0.03003   0.02236  -0.0635   0.0599   0.7359
  10.250   1.1605   0.03126   0.02359  -0.0624   0.0518   0.7371
  10.500   1.1691   0.03267   0.02498  -0.0612   0.0418   0.7384
  10.750   1.1777   0.03412   0.02641  -0.0601   0.0348   0.7398
  11.000   1.1866   0.03560   0.02790  -0.0591   0.0309   0.7412
  11.250   1.1973   0.03696   0.02930  -0.0583   0.0288   0.7425
  11.500   1.2068   0.03846   0.03083  -0.0575   0.0272   0.7437
  11.750   1.2175   0.03990   0.03232  -0.0567   0.0260   0.7451
  12.000   1.2282   0.04138   0.03386  -0.0561   0.0251   0.7464
  12.250   1.2385   0.04292   0.03545  -0.0555   0.0243   0.7478
  12.500   1.2483   0.04454   0.03712  -0.0549   0.0236   0.7491
  12.750   1.2570   0.04630   0.03892  -0.0544   0.0230   0.7505
  13.250   1.2727   0.05009   0.04284  -0.0533   0.0219   0.7531
  13.500   1.2821   0.05188   0.04471  -0.0529   0.0216   0.7547
  13.750   1.2905   0.05381   0.04672  -0.0526   0.0213   0.7564
  14.000   1.2986   0.05580   0.04879  -0.0523   0.0209   0.7581
  14.250   1.3061   0.05790   0.05097  -0.0521   0.0204   0.7599
  14.500   1.3141   0.06001   0.05315  -0.0520   0.0200   0.7616
  14.750   1.3207   0.06230   0.05551  -0.0519   0.0196   0.7634
  15.000   1.3269   0.06468   0.05796  -0.0519   0.0192   0.7652
  15.250   1.3319   0.06725   0.06059  -0.0520   0.0189   0.7669
  15.500   1.3357   0.07000   0.06341  -0.0521   0.0186   0.7686
  15.750   1.3381   0.07297   0.06646  -0.0523   0.0183   0.7701
  16.000   1.3412   0.07591   0.06949  -0.0525   0.0181   0.7719
  16.250   1.3474   0.07850   0.07218  -0.0529   0.0179   0.7739
  16.500   1.3523   0.08128   0.07505  -0.0533   0.0177   0.7760
  16.750   1.3572   0.08408   0.07795  -0.0538   0.0175   0.7782
  17.000   1.3615   0.08704   0.08099  -0.0544   0.0173   0.7804
  17.250   1.3660   0.08997   0.08401  -0.0550   0.0170   0.7827
  17.500   1.3696   0.09308   0.08720  -0.0558   0.0167   0.7847
  17.750   1.3737   0.09612   0.09034  -0.0566   0.0164   0.7868
  18.000   1.3766   0.09936   0.09368  -0.0575   0.0162   0.7890
  18.250   1.3797   0.10260   0.09701  -0.0585   0.0160   0.7914
  18.500   1.3820   0.10598   0.10048  -0.0596   0.0158   0.7938
  18.750   1.3843   0.10941   0.10400  -0.0609   0.0156   0.7964
  19.000   1.3861   0.11292   0.10758  -0.0622   0.0154   0.7988
  19.250   1.3872   0.11655   0.11129  -0.0636   0.0152   0.8010
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