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FX 84-W-175 (fx84w175-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX 84-W-175 (fx84w175-il)
Reynolds number: 1,000,000
Max Cl/Cd: 135.12 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx84w175-il-1000000.txt
Download as CSV file: xf-fx84w175-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 84-W-175                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -0.7025   0.10200   0.09954  -0.0773   1.0000   0.0195
 -18.250  -0.7355   0.09270   0.09010  -0.0827   1.0000   0.0196
 -18.000  -0.7659   0.08415   0.08142  -0.0879   1.0000   0.0196
 -17.750  -0.7953   0.07607   0.07321  -0.0928   1.0000   0.0197
 -17.500  -0.8177   0.06917   0.06620  -0.0970   1.0000   0.0197
 -17.250  -0.8263   0.06195   0.05883  -0.1043   0.9749   0.0198
 -17.000  -0.8266   0.05502   0.05172  -0.1129   0.9645   0.0199
 -16.750  -0.8188   0.04968   0.04619  -0.1203   0.9509   0.0201
 -16.500  -0.8205   0.04537   0.04168  -0.1243   0.9309   0.0201
 -16.250  -0.8313   0.04151   0.03763  -0.1260   0.9142   0.0202
 -16.000  -0.8465   0.03764   0.03359  -0.1271   0.9011   0.0204
 -15.750  -0.8558   0.03462   0.03043  -0.1276   0.8906   0.0206
 -15.500  -0.8603   0.03220   0.02790  -0.1276   0.8812   0.0209
 -15.250  -0.8616   0.03018   0.02578  -0.1274   0.8733   0.0211
 -15.000  -0.8593   0.02854   0.02405  -0.1268   0.8655   0.0213
 -14.750  -0.8552   0.02716   0.02257  -0.1261   0.8584   0.0215
 -14.500  -0.8506   0.02579   0.02114  -0.1252   0.8521   0.0217
 -14.250  -0.8427   0.02476   0.02002  -0.1242   0.8458   0.0220
 -14.000  -0.8330   0.02387   0.01905  -0.1232   0.8399   0.0224
 -13.750  -0.8248   0.02290   0.01800  -0.1220   0.8342   0.0226
 -13.500  -0.8137   0.02215   0.01716  -0.1207   0.8286   0.0230
 -13.250  -0.8039   0.02138   0.01629  -0.1192   0.8231   0.0233
 -13.000  -0.7919   0.02070   0.01554  -0.1179   0.8183   0.0235
 -12.750  -0.7802   0.02006   0.01482  -0.1163   0.8129   0.0237
 -12.500  -0.7803   0.01900   0.01365  -0.1131   0.8071   0.0242
 -12.250  -0.7719   0.01839   0.01301  -0.1106   0.8027   0.0247
 -12.000  -0.7568   0.01789   0.01247  -0.1091   0.7982   0.0251
 -11.750  -0.7386   0.01744   0.01197  -0.1080   0.7936   0.0255
 -11.500  -0.7193   0.01705   0.01149  -0.1070   0.7889   0.0260
 -11.250  -0.6987   0.01662   0.01102  -0.1062   0.7854   0.0265
 -11.000  -0.6770   0.01623   0.01058  -0.1056   0.7814   0.0270
 -10.750  -0.6541   0.01591   0.01019  -0.1050   0.7772   0.0275
 -10.500  -0.6360   0.01527   0.00948  -0.1039   0.7728   0.0283
 -10.250  -0.6138   0.01485   0.00904  -0.1033   0.7690   0.0291
 -10.000  -0.5899   0.01451   0.00868  -0.1029   0.7654   0.0298
  -9.750  -0.5656   0.01419   0.00832  -0.1026   0.7615   0.0306
  -9.500  -0.5410   0.01391   0.00798  -0.1022   0.7574   0.0314
  -9.250  -0.5167   0.01361   0.00760  -0.1019   0.7531   0.0320
  -9.000  -0.4936   0.01312   0.00711  -0.1014   0.7498   0.0333
  -8.750  -0.4681   0.01283   0.00680  -0.1012   0.7460   0.0343
  -8.500  -0.4423   0.01258   0.00652  -0.1010   0.7421   0.0355
  -8.250  -0.4159   0.01241   0.00628  -0.1009   0.7380   0.0364
  -8.000  -0.3914   0.01201   0.00586  -0.1005   0.7343   0.0381
  -7.750  -0.3650   0.01174   0.00560  -0.1005   0.7307   0.0396
  -7.500  -0.3381   0.01153   0.00536  -0.1004   0.7268   0.0411
  -7.250  -0.3119   0.01128   0.00507  -0.1003   0.7229   0.0428
  -7.000  -0.2857   0.01106   0.00482  -0.1002   0.7187   0.0450
  -6.750  -0.2581   0.01087   0.00463  -0.1002   0.7156   0.0471
  -6.500  -0.2313   0.01061   0.00437  -0.1002   0.7117   0.0498
  -6.250  -0.2041   0.01042   0.00417  -0.1002   0.7078   0.0526
  -6.000  -0.1769   0.01026   0.00397  -0.1002   0.7039   0.0555
  -5.750  -0.1496   0.01006   0.00379  -0.1003   0.7003   0.0595
  -5.500  -0.1218   0.00989   0.00362  -0.1004   0.6967   0.0634
  -5.250  -0.0942   0.00970   0.00345  -0.1004   0.6927   0.0684
  -5.000  -0.0666   0.00955   0.00329  -0.1005   0.6888   0.0736
  -4.750  -0.0390   0.00945   0.00316  -0.1006   0.6847   0.0794
  -4.500  -0.0110   0.00925   0.00302  -0.1007   0.6815   0.0871
  -4.250   0.0171   0.00911   0.00290  -0.1009   0.6776   0.0949
  -4.000   0.0451   0.00898   0.00278  -0.1010   0.6736   0.1035
  -3.750   0.0727   0.00885   0.00267  -0.1011   0.6697   0.1153
  -3.500   0.1008   0.00871   0.00257  -0.1013   0.6660   0.1287
  -3.250   0.1290   0.00855   0.00248  -0.1015   0.6623   0.1448
  -2.750   0.1847   0.00827   0.00231  -0.1018   0.6542   0.1869
  -2.250   0.2405   0.00794   0.00217  -0.1022   0.6466   0.2502
  -2.000   0.2682   0.00772   0.00210  -0.1024   0.6426   0.2946
  -1.750   0.2954   0.00749   0.00204  -0.1026   0.6385   0.3531
  -1.500   0.3222   0.00725   0.00199  -0.1027   0.6340   0.4237
  -1.250   0.3499   0.00698   0.00196  -0.1029   0.6306   0.4971
  -1.000   0.3778   0.00680   0.00195  -0.1031   0.6267   0.5559
  -0.750   0.4059   0.00671   0.00196  -0.1032   0.6226   0.5997
  -0.500   0.4337   0.00669   0.00198  -0.1033   0.6181   0.6323
  -0.250   0.4624   0.00666   0.00202  -0.1035   0.6144   0.6585
   0.000   0.4910   0.00664   0.00205  -0.1037   0.6105   0.6804
   0.250   0.5194   0.00665   0.00208  -0.1039   0.6063   0.6985
   0.500   0.5474   0.00671   0.00212  -0.1040   0.6018   0.7139
   0.750   0.5760   0.00674   0.00217  -0.1042   0.5979   0.7277
   1.000   0.6045   0.00675   0.00222  -0.1044   0.5938   0.7407
   1.250   0.6327   0.00680   0.00227  -0.1045   0.5894   0.7519
   1.500   0.6601   0.00689   0.00233  -0.1045   0.5846   0.7625
   1.750   0.6885   0.00692   0.00239  -0.1047   0.5808   0.7725
   2.000   0.7166   0.00697   0.00246  -0.1048   0.5764   0.7832
   2.250   0.7438   0.00703   0.00253  -0.1047   0.5717   0.7944
   2.500   0.7708   0.00716   0.00262  -0.1047   0.5669   0.8052
   2.750   0.7984   0.00718   0.00270  -0.1047   0.5629   0.8133
   3.000   0.8260   0.00725   0.00277  -0.1047   0.5582   0.8207
   3.250   0.8526   0.00734   0.00285  -0.1046   0.5534   0.8270
   3.500   0.8791   0.00743   0.00295  -0.1045   0.5488   0.8336
   3.750   0.9067   0.00749   0.00303  -0.1046   0.5444   0.8401
   4.000   0.9329   0.00757   0.00312  -0.1044   0.5395   0.8463
   4.250   0.9577   0.00771   0.00324  -0.1039   0.5342   0.8528
   4.500   0.9849   0.00778   0.00333  -0.1040   0.5298   0.8591
   4.750   1.0101   0.00785   0.00343  -0.1036   0.5242   0.8654
   5.000   1.0336   0.00800   0.00356  -0.1029   0.5182   0.8723
   5.250   1.0594   0.00808   0.00367  -0.1027   0.5130   0.8789
   5.500   1.0829   0.00818   0.00379  -0.1020   0.5072   0.8857
   5.750   1.1049   0.00835   0.00394  -0.1010   0.5011   0.8934
   6.000   1.1283   0.00842   0.00407  -0.1003   0.4959   0.9007
   6.250   1.1502   0.00855   0.00421  -0.0993   0.4900   0.9092
   6.500   1.1662   0.00871   0.00437  -0.0972   0.4841   0.9194
   6.750   1.1850   0.00877   0.00450  -0.0955   0.4787   0.9307
   7.000   1.1979   0.00891   0.00467  -0.0927   0.4726   0.9481
   7.250   1.2190   0.00910   0.00489  -0.0917   0.4663   0.9753
   7.500   1.2473   0.00928   0.00508  -0.0924   0.4587   1.0000
   7.750   1.2646   0.00960   0.00537  -0.0910   0.4497   1.0000
   8.000   1.2821   0.00993   0.00566  -0.0896   0.4386   1.0000
   8.250   1.2992   0.01028   0.00599  -0.0881   0.4281   1.0000
   8.500   1.3132   0.01073   0.00640  -0.0862   0.4178   1.0000
   8.750   1.3312   0.01109   0.00675  -0.0850   0.4084   1.0000
   9.000   1.3456   0.01158   0.00721  -0.0833   0.3987   1.0000
   9.250   1.3591   0.01212   0.00773  -0.0815   0.3879   1.0000
   9.500   1.3737   0.01265   0.00824  -0.0799   0.3766   1.0000
   9.750   1.3847   0.01334   0.00888  -0.0778   0.3635   1.0000
  10.000   1.3951   0.01409   0.00959  -0.0758   0.3509   1.0000
  10.250   1.4041   0.01494   0.01038  -0.0736   0.3366   1.0000
  10.500   1.4117   0.01589   0.01128  -0.0714   0.3217   1.0000
  10.750   1.4178   0.01695   0.01228  -0.0691   0.3049   1.0000
  11.000   1.4232   0.01811   0.01337  -0.0668   0.2879   1.0000
  11.250   1.4277   0.01935   0.01454  -0.0645   0.2708   1.0000
  11.500   1.4306   0.02073   0.01585  -0.0621   0.2533   1.0000
  11.750   1.4319   0.02228   0.01732  -0.0598   0.2349   1.0000
  12.000   1.4332   0.02390   0.01886  -0.0576   0.2177   1.0000
  12.250   1.4358   0.02550   0.02040  -0.0556   0.2024   1.0000
  12.500   1.4370   0.02727   0.02210  -0.0536   0.1867   1.0000
  12.750   1.4377   0.02914   0.02391  -0.0518   0.1715   1.0000
  13.000   1.4373   0.03117   0.02586  -0.0500   0.1558   1.0000
  13.250   1.4372   0.03324   0.02787  -0.0484   0.1408   1.0000
  13.500   1.4371   0.03540   0.02996  -0.0468   0.1269   1.0000
  13.750   1.4366   0.03767   0.03217  -0.0455   0.1137   1.0000
  14.000   1.4365   0.03996   0.03442  -0.0442   0.1016   1.0000
  14.250   1.4374   0.04224   0.03666  -0.0432   0.0914   1.0000
  14.500   1.4395   0.04447   0.03888  -0.0423   0.0834   1.0000
  14.750   1.4425   0.04668   0.04108  -0.0415   0.0762   1.0000
  15.000   1.4437   0.04913   0.04351  -0.0408   0.0692   1.0000
  15.250   1.4468   0.05144   0.04582  -0.0403   0.0640   1.0000
  15.500   1.4505   0.05372   0.04811  -0.0398   0.0591   1.0000
  15.750   1.4522   0.05627   0.05066  -0.0394   0.0549   1.0000
  16.000   1.4566   0.05857   0.05299  -0.0391   0.0508   1.0000
  16.250   1.4577   0.06130   0.05573  -0.0389   0.0473   1.0000
  16.500   1.4625   0.06363   0.05809  -0.0388   0.0444   1.0000
  16.750   1.4640   0.06640   0.06088  -0.0387   0.0417   1.0000
  17.000   1.4676   0.06897   0.06349  -0.0387   0.0393   1.0000
  17.250   1.4700   0.07172   0.06627  -0.0388   0.0371   1.0000
  17.500   1.4705   0.07474   0.06933  -0.0390   0.0349   1.0000
  17.750   1.4745   0.07735   0.07199  -0.0393   0.0332   1.0000
  18.000   1.4755   0.08040   0.07507  -0.0396   0.0315   1.0000
  18.250   1.4761   0.08354   0.07825  -0.0400   0.0300   1.0000
  18.500   1.4791   0.08642   0.08119  -0.0405   0.0286   1.0000
  18.750   1.4804   0.08952   0.08433  -0.0411   0.0274   1.0000
  19.000   1.4778   0.09320   0.08806  -0.0418   0.0261   1.0000
  19.250   1.4811   0.09610   0.09102  -0.0425   0.0252   1.0000
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