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WORTMANN FX 05-191 AIRFOIL (fx05191-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 05-191 AIRFOIL (fx05191-il)
Reynolds number: 1,000,000
Max Cl/Cd: 112.63 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx05191-il-1000000-n5.txt
Download as CSV file: xf-fx05191-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 05-191 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  -0.8280   0.08299   0.07932  -0.1100   0.8752   0.0116
 -19.500  -0.8325   0.07806   0.07425  -0.1136   0.8702   0.0117
 -19.250  -0.8373   0.07340   0.06946  -0.1168   0.8663   0.0117
 -19.000  -0.8380   0.06941   0.06535  -0.1195   0.8626   0.0118
 -18.750  -0.8398   0.06538   0.06120  -0.1223   0.8590   0.0119
 -18.250  -0.8351   0.05886   0.05445  -0.1266   0.8532   0.0121
 -18.000  -0.8317   0.05594   0.05144  -0.1283   0.8507   0.0122
 -17.750  -0.8276   0.05318   0.04858  -0.1299   0.8483   0.0123
 -17.500  -0.8233   0.05051   0.04581  -0.1314   0.8462   0.0124
 -17.250  -0.8159   0.04821   0.04341  -0.1328   0.8440   0.0126
 -17.000  -0.8052   0.04633   0.04145  -0.1340   0.8420   0.0127
 -16.500  -0.7905   0.04213   0.03707  -0.1360   0.8385   0.0128
 -16.250  -0.7813   0.04036   0.03522  -0.1366   0.8371   0.0130
 -16.000  -0.7684   0.03896   0.03375  -0.1373   0.8357   0.0131
 -15.750  -0.7588   0.03732   0.03204  -0.1378   0.8341   0.0132
 -15.500  -0.7467   0.03592   0.03057  -0.1382   0.8326   0.0133
 -15.250  -0.7389   0.03422   0.02880  -0.1384   0.8311   0.0134
 -15.000  -0.7304   0.03262   0.02714  -0.1385   0.8296   0.0137
 -14.750  -0.7193   0.03128   0.02574  -0.1386   0.8281   0.0137
 -14.500  -0.7071   0.03006   0.02447  -0.1387   0.8266   0.0139
 -14.250  -0.6946   0.02890   0.02324  -0.1387   0.8249   0.0141
 -13.750  -0.6657   0.02697   0.02123  -0.1386   0.8221   0.0145
 -13.500  -0.6514   0.02605   0.02028  -0.1383   0.8211   0.0147
 -13.250  -0.6378   0.02513   0.01931  -0.1379   0.8199   0.0148
 -13.000  -0.6224   0.02435   0.01850  -0.1376   0.8188   0.0150
 -12.750  -0.6064   0.02363   0.01775  -0.1373   0.8176   0.0152
 -12.500  -0.5922   0.02283   0.01690  -0.1367   0.8164   0.0154
 -12.250  -0.5774   0.02209   0.01612  -0.1361   0.8152   0.0156
 -12.000  -0.5612   0.02144   0.01544  -0.1356   0.8140   0.0159
 -11.750  -0.5441   0.02086   0.01482  -0.1351   0.8128   0.0161
 -11.500  -0.5282   0.02023   0.01415  -0.1345   0.8114   0.0163
 -11.250  -0.5117   0.01966   0.01353  -0.1338   0.8097   0.0165
 -11.000  -0.4952   0.01910   0.01292  -0.1331   0.8076   0.0166
 -10.750  -0.4811   0.01844   0.01223  -0.1321   0.8056   0.0169
 -10.500  -0.4663   0.01783   0.01160  -0.1311   0.8042   0.0171
 -10.250  -0.4516   0.01724   0.01099  -0.1300   0.8026   0.0176
 -10.000  -0.4351   0.01674   0.01048  -0.1290   0.8010   0.0178
  -9.750  -0.4184   0.01626   0.00999  -0.1281   0.7993   0.0182
  -9.500  -0.4012   0.01583   0.00954  -0.1271   0.7973   0.0186
  -9.250  -0.3843   0.01539   0.00907  -0.1261   0.7952   0.0189
  -9.000  -0.3669   0.01498   0.00863  -0.1251   0.7934   0.0192
  -8.750  -0.3493   0.01460   0.00821  -0.1241   0.7913   0.0197
  -8.500  -0.3310   0.01424   0.00783  -0.1232   0.7896   0.0200
  -8.250  -0.3128   0.01388   0.00746  -0.1221   0.7883   0.0203
  -8.000  -0.2960   0.01349   0.00707  -0.1209   0.7865   0.0211
  -7.750  -0.2791   0.01311   0.00669  -0.1197   0.7847   0.0218
  -7.500  -0.2617   0.01275   0.00634  -0.1184   0.7826   0.0226
  -7.250  -0.2442   0.01243   0.00600  -0.1172   0.7804   0.0234
  -7.000  -0.2266   0.01212   0.00568  -0.1159   0.7784   0.0242
  -6.750  -0.2097   0.01185   0.00538  -0.1144   0.7764   0.0250
  -6.500  -0.1958   0.01159   0.00512  -0.1124   0.7741   0.0264
  -6.250  -0.1802   0.01135   0.00488  -0.1107   0.7722   0.0282
  -6.000  -0.1606   0.01110   0.00464  -0.1097   0.7700   0.0305
  -5.750  -0.1400   0.01084   0.00441  -0.1090   0.7676   0.0346
  -5.500  -0.1187   0.01059   0.00419  -0.1083   0.7650   0.0413
  -5.250  -0.0965   0.01035   0.00397  -0.1077   0.7623   0.0499
  -5.000  -0.0738   0.01011   0.00377  -0.1073   0.7597   0.0610
  -4.750  -0.0507   0.00986   0.00357  -0.1069   0.7573   0.0751
  -4.250  -0.0051   0.00916   0.00314  -0.1062   0.7510   0.1408
  -4.000   0.0170   0.00866   0.00286  -0.1059   0.7473   0.2012
  -3.750   0.0385   0.00791   0.00249  -0.1058   0.7436   0.3062
  -3.500   0.0640   0.00725   0.00220  -0.1064   0.7400   0.4041
  -3.250   0.0926   0.00683   0.00203  -0.1074   0.7355   0.4743
  -3.000   0.1218   0.00659   0.00192  -0.1082   0.7303   0.5184
  -2.750   0.1513   0.00643   0.00184  -0.1089   0.7251   0.5504
  -2.500   0.1810   0.00634   0.00179  -0.1096   0.7186   0.5700
  -2.250   0.2097   0.00629   0.00173  -0.1101   0.7119   0.5801
  -2.000   0.2388   0.00628   0.00170  -0.1106   0.7036   0.5868
  -1.750   0.2669   0.00628   0.00166  -0.1109   0.6941   0.5931
  -1.500   0.2949   0.00630   0.00164  -0.1112   0.6834   0.5998
  -1.250   0.3228   0.00633   0.00163  -0.1114   0.6738   0.6062
  -1.000   0.3505   0.00637   0.00163  -0.1117   0.6649   0.6130
  -0.750   0.3787   0.00641   0.00165  -0.1120   0.6565   0.6196
  -0.500   0.4062   0.00647   0.00167  -0.1122   0.6486   0.6260
  -0.250   0.4346   0.00651   0.00170  -0.1126   0.6414   0.6332
   0.000   0.4621   0.00658   0.00174  -0.1128   0.6346   0.6396
   0.250   0.4908   0.00662   0.00179  -0.1132   0.6293   0.6462
   0.500   0.5191   0.00667   0.00183  -0.1136   0.6235   0.6532
   0.750   0.5465   0.00675   0.00190  -0.1138   0.6176   0.6597
   1.000   0.5751   0.00679   0.00196  -0.1142   0.6124   0.6665
   1.250   0.6031   0.00686   0.00202  -0.1145   0.6069   0.6722
   1.500   0.6305   0.00694   0.00210  -0.1147   0.6018   0.6783
   1.750   0.6586   0.00700   0.00218  -0.1150   0.5972   0.6847
   2.000   0.6865   0.00707   0.00225  -0.1153   0.5920   0.6898
   2.250   0.7134   0.00717   0.00235  -0.1154   0.5866   0.6950
   2.500   0.7403   0.00726   0.00244  -0.1154   0.5806   0.6999
   2.750   0.7667   0.00736   0.00253  -0.1154   0.5728   0.7043
   3.000   0.7921   0.00749   0.00266  -0.1152   0.5663   0.7087
   3.250   0.8190   0.00758   0.00276  -0.1153   0.5601   0.7130
   3.750   0.8682   0.00785   0.00299  -0.1146   0.5424   0.7201
   4.000   0.8912   0.00801   0.00314  -0.1138   0.5343   0.7231
   4.250   0.9157   0.00813   0.00328  -0.1135   0.5262   0.7265
   4.500   0.9356   0.00831   0.00343  -0.1121   0.5162   0.7301
   4.750   0.9537   0.00852   0.00359  -0.1105   0.5029   0.7334
   5.000   0.9715   0.00878   0.00379  -0.1088   0.4872   0.7360
   5.250   0.9870   0.00910   0.00406  -0.1067   0.4689   0.7384
   5.500   1.0029   0.00944   0.00435  -0.1047   0.4507   0.7411
   5.750   1.0191   0.00978   0.00466  -0.1029   0.4343   0.7440
   6.000   1.0333   0.01022   0.00501  -0.1008   0.4136   0.7468
   6.250   1.0391   0.01095   0.00557  -0.0973   0.3779   0.7494
   6.500   1.0395   0.01195   0.00633  -0.0931   0.3320   0.7518
   6.750   1.0394   0.01305   0.00722  -0.0890   0.2855   0.7542
   7.000   1.0365   0.01438   0.00828  -0.0847   0.2323   0.7566
   7.250   1.0399   0.01551   0.00923  -0.0815   0.1930   0.7590
   7.500   1.0461   0.01657   0.01013  -0.0789   0.1612   0.7614
   7.750   1.0528   0.01765   0.01106  -0.0764   0.1314   0.7639
   8.000   1.0601   0.01874   0.01201  -0.0741   0.1037   0.7663
   8.250   1.0711   0.01967   0.01286  -0.0724   0.0879   0.7682
   8.500   1.0862   0.02037   0.01356  -0.0712   0.0809   0.7702
   8.750   1.1004   0.02113   0.01432  -0.0699   0.0752   0.7720
   9.000   1.1166   0.02181   0.01501  -0.0688   0.0709   0.7737
   9.250   1.1321   0.02253   0.01575  -0.0678   0.0673   0.7754
   9.500   1.1463   0.02334   0.01656  -0.0666   0.0635   0.7770
   9.750   1.1626   0.02406   0.01729  -0.0657   0.0609   0.7786
  10.000   1.1784   0.02481   0.01806  -0.0648   0.0583   0.7802
  10.250   1.1924   0.02568   0.01895  -0.0638   0.0549   0.7816
  10.500   1.2068   0.02657   0.01983  -0.0628   0.0516   0.7830
  10.750   1.2214   0.02745   0.02073  -0.0619   0.0485   0.7841
  11.000   1.2338   0.02850   0.02177  -0.0608   0.0443   0.7855
  11.250   1.2476   0.02946   0.02276  -0.0599   0.0410   0.7868
  11.500   1.2588   0.03063   0.02392  -0.0588   0.0372   0.7881
  11.750   1.2714   0.03173   0.02505  -0.0578   0.0340   0.7894
  12.000   1.2820   0.03301   0.02632  -0.0568   0.0307   0.7905
  12.250   1.2941   0.03421   0.02755  -0.0559   0.0285   0.7918
  12.500   1.3059   0.03546   0.02883  -0.0551   0.0270   0.7931
  12.750   1.3165   0.03685   0.03024  -0.0542   0.0252   0.7942
  13.000   1.3286   0.03813   0.03156  -0.0535   0.0241   0.7953
  13.250   1.3395   0.03956   0.03302  -0.0528   0.0231   0.7963
  13.500   1.3502   0.04103   0.03452  -0.0522   0.0221   0.7974
  13.750   1.3597   0.04265   0.03616  -0.0515   0.0210   0.7985
  14.000   1.3712   0.04411   0.03767  -0.0510   0.0204   0.7994
  14.250   1.3815   0.04571   0.03932  -0.0505   0.0197   0.8002
  14.500   1.3915   0.04736   0.04102  -0.0501   0.0189   0.8011
  14.750   1.4004   0.04916   0.04286  -0.0496   0.0182   0.8021
  15.000   1.4089   0.05103   0.04477  -0.0492   0.0175   0.8030
  15.250   1.4179   0.05287   0.04667  -0.0489   0.0170   0.8039
  15.500   1.4274   0.05468   0.04855  -0.0487   0.0166   0.8048
  15.750   1.4360   0.05661   0.05054  -0.0485   0.0161   0.8058
  16.000   1.4443   0.05862   0.05260  -0.0483   0.0155   0.8069
  16.250   1.4516   0.06076   0.05479  -0.0482   0.0148   0.8079
  16.500   1.4583   0.06300   0.05708  -0.0482   0.0143   0.8089
  16.750   1.4649   0.06528   0.05941  -0.0482   0.0138   0.8098
  17.000   1.4723   0.06750   0.06170  -0.0483   0.0134   0.8106
  17.250   1.4791   0.06982   0.06409  -0.0484   0.0129   0.8115
  17.500   1.4851   0.07228   0.06660  -0.0486   0.0124   0.8123
  17.750   1.4907   0.07480   0.06918  -0.0489   0.0120   0.8131
  18.000   1.4952   0.07752   0.07195  -0.0492   0.0115   0.8138
  18.250   1.4993   0.08028   0.07477  -0.0496   0.0111   0.8145
  18.500   1.5038   0.08306   0.07762  -0.0501   0.0108   0.8152
  18.750   1.5086   0.08579   0.08042  -0.0506   0.0105   0.8158
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