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FX 84-W-175 (fx84w175-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 84-W-175 (fx84w175-il)
Reynolds number: 1,000,000
Max Cl/Cd: 123.97 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx84w175-il-1000000-n5.txt
Download as CSV file: xf-fx84w175-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -0.7410   0.08784   0.08486  -0.0949   0.9353   0.0160
 -18.250  -0.7943   0.07571   0.07249  -0.1028   0.9223   0.0159
 -18.000  -0.8467   0.06449   0.06101  -0.1096   0.9091   0.0159
 -17.750  -0.8860   0.05553   0.05183  -0.1151   0.8968   0.0158
 -17.500  -0.9083   0.04935   0.04546  -0.1187   0.8867   0.0159
 -17.250  -0.9246   0.04443   0.04036  -0.1213   0.8768   0.0159
 -17.000  -0.9345   0.04057   0.03637  -0.1232   0.8681   0.0160
 -16.500  -0.9453   0.03467   0.03021  -0.1250   0.8528   0.0163
 -16.250  -0.9472   0.03237   0.02779  -0.1252   0.8451   0.0164
 -16.000  -0.9458   0.03048   0.02579  -0.1251   0.8388   0.0165
 -15.750  -0.9434   0.02876   0.02397  -0.1248   0.8322   0.0167
 -15.500  -0.9386   0.02735   0.02245  -0.1242   0.8261   0.0168
 -15.250  -0.9330   0.02604   0.02105  -0.1234   0.8208   0.0169
 -15.000  -0.9274   0.02479   0.01972  -0.1225   0.8148   0.0171
 -14.750  -0.9225   0.02360   0.01844  -0.1212   0.8088   0.0174
 -14.500  -0.9152   0.02258   0.01735  -0.1199   0.8039   0.0176
 -14.250  -0.9057   0.02171   0.01643  -0.1187   0.7990   0.0180
 -14.000  -0.8954   0.02095   0.01560  -0.1173   0.7937   0.0182
 -13.500  -0.8727   0.01961   0.01413  -0.1142   0.7842   0.0188
 -13.250  -0.8611   0.01900   0.01346  -0.1125   0.7794   0.0190
 -13.000  -0.8491   0.01849   0.01288  -0.1106   0.7745   0.0193
 -12.750  -0.8365   0.01806   0.01238  -0.1086   0.7700   0.0195
 -12.500  -0.8196   0.01762   0.01188  -0.1073   0.7660   0.0198
 -12.250  -0.8005   0.01720   0.01140  -0.1063   0.7616   0.0201
 -12.000  -0.7819   0.01673   0.01086  -0.1053   0.7573   0.0204
 -11.750  -0.7622   0.01628   0.01037  -0.1044   0.7531   0.0209
 -11.500  -0.7408   0.01588   0.00993  -0.1037   0.7494   0.0213
 -11.250  -0.7188   0.01550   0.00952  -0.1031   0.7455   0.0218
 -11.000  -0.6961   0.01515   0.00912  -0.1026   0.7415   0.0223
 -10.750  -0.6729   0.01484   0.00875  -0.1021   0.7375   0.0229
 -10.500  -0.6490   0.01452   0.00839  -0.1017   0.7339   0.0234
 -10.250  -0.6251   0.01419   0.00802  -0.1013   0.7300   0.0239
 -10.000  -0.6011   0.01384   0.00764  -0.1009   0.7260   0.0245
  -9.750  -0.5766   0.01354   0.00731  -0.1006   0.7222   0.0253
  -9.500  -0.5518   0.01327   0.00700  -0.1003   0.7185   0.0260
  -9.250  -0.5262   0.01300   0.00669  -0.1001   0.7149   0.0267
  -9.000  -0.5004   0.01275   0.00641  -0.0999   0.7109   0.0273
  -8.750  -0.4748   0.01248   0.00611  -0.0997   0.7070   0.0283
  -8.500  -0.4491   0.01223   0.00584  -0.0996   0.7031   0.0293
  -8.250  -0.4228   0.01200   0.00558  -0.0995   0.6996   0.0304
  -8.000  -0.3961   0.01179   0.00534  -0.0994   0.6958   0.0314
  -7.750  -0.3696   0.01157   0.00510  -0.0993   0.6918   0.0324
  -7.500  -0.3432   0.01135   0.00486  -0.0992   0.6878   0.0338
  -7.250  -0.3164   0.01116   0.00465  -0.0992   0.6840   0.0352
  -7.000  -0.2890   0.01099   0.00445  -0.0993   0.6805   0.0366
  -6.750  -0.2620   0.01077   0.00424  -0.0993   0.6768   0.0386
  -6.500  -0.2348   0.01060   0.00405  -0.0993   0.6726   0.0405
  -6.250  -0.2075   0.01046   0.00388  -0.0993   0.6687   0.0423
  -6.000  -0.1800   0.01028   0.00370  -0.0993   0.6653   0.0448
  -5.750  -0.1522   0.01013   0.00355  -0.0995   0.6617   0.0475
  -5.500  -0.1247   0.00997   0.00339  -0.0995   0.6577   0.0507
  -5.250  -0.0970   0.00985   0.00325  -0.0996   0.6535   0.0538
  -5.000  -0.0694   0.00971   0.00311  -0.0997   0.6498   0.0574
  -4.750  -0.0412   0.00958   0.00299  -0.0999   0.6464   0.0616
  -4.500  -0.0133   0.00944   0.00287  -0.1000   0.6424   0.0666
  -4.250   0.0146   0.00934   0.00275  -0.1001   0.6382   0.0712
  -3.750   0.0706   0.00911   0.00255  -0.1004   0.6308   0.0841
  -3.500   0.0989   0.00901   0.00246  -0.1006   0.6268   0.0909
  -3.250   0.1268   0.00890   0.00238  -0.1007   0.6226   0.1002
  -3.000   0.1546   0.00881   0.00230  -0.1008   0.6183   0.1097
  -2.750   0.1829   0.00871   0.00223  -0.1010   0.6148   0.1205
  -2.500   0.2111   0.00860   0.00217  -0.1013   0.6108   0.1342
  -2.250   0.2391   0.00850   0.00211  -0.1014   0.6065   0.1502
  -2.000   0.2669   0.00841   0.00206  -0.1016   0.6022   0.1681
  -1.750   0.2949   0.00831   0.00201  -0.1017   0.5986   0.1897
  -1.500   0.3231   0.00820   0.00197  -0.1020   0.5947   0.2143
  -1.250   0.3509   0.00807   0.00194  -0.1022   0.5901   0.2452
  -1.000   0.3785   0.00796   0.00191  -0.1023   0.5860   0.2792
  -0.750   0.4062   0.00782   0.00189  -0.1025   0.5823   0.3217
  -0.500   0.4340   0.00765   0.00187  -0.1027   0.5783   0.3708
  -0.250   0.4615   0.00748   0.00186  -0.1029   0.5737   0.4297
   0.000   0.4888   0.00733   0.00186  -0.1030   0.5695   0.4880
   0.250   0.5163   0.00722   0.00189  -0.1032   0.5656   0.5394
   0.500   0.5445   0.00714   0.00192  -0.1034   0.5615   0.5801
   0.750   0.5723   0.00711   0.00196  -0.1035   0.5568   0.6112
   1.000   0.5998   0.00712   0.00201  -0.1035   0.5523   0.6398
   1.250   0.6277   0.00713   0.00207  -0.1037   0.5483   0.6622
   1.500   0.6558   0.00714   0.00213  -0.1038   0.5438   0.6805
   1.750   0.6833   0.00719   0.00220  -0.1039   0.5389   0.6975
   2.000   0.7102   0.00726   0.00228  -0.1038   0.5342   0.7140
   2.250   0.7380   0.00729   0.00235  -0.1039   0.5301   0.7328
   2.500   0.7654   0.00735   0.00244  -0.1039   0.5252   0.7491
   2.750   0.7919   0.00742   0.00253  -0.1038   0.5201   0.7599
   3.250   0.8460   0.00758   0.00270  -0.1037   0.5109   0.7751
   3.500   0.8725   0.00768   0.00280  -0.1036   0.5056   0.7826
   3.750   0.8980   0.00780   0.00291  -0.1033   0.5007   0.7891
   4.000   0.9247   0.00787   0.00301  -0.1032   0.4963   0.7958
   4.250   0.9507   0.00798   0.00312  -0.1030   0.4909   0.8025
   4.500   0.9750   0.00812   0.00325  -0.1025   0.4852   0.8085
   4.750   1.0003   0.00822   0.00337  -0.1022   0.4797   0.8151
   5.000   1.0244   0.00836   0.00350  -0.1017   0.4727   0.8216
   5.250   1.0470   0.00852   0.00366  -0.1009   0.4663   0.8278
   5.500   1.0705   0.00865   0.00380  -0.1002   0.4597   0.8345
   5.750   1.0910   0.00883   0.00397  -0.0990   0.4528   0.8413
   6.000   1.1108   0.00896   0.00413  -0.0976   0.4469   0.8481
   6.250   1.1292   0.00913   0.00432  -0.0960   0.4400   0.8559
   6.500   1.1460   0.00936   0.00455  -0.0942   0.4337   0.8638
   6.750   1.1649   0.00955   0.00477  -0.0927   0.4269   0.8724
   7.000   1.1801   0.00984   0.00506  -0.0906   0.4193   0.8816
   7.250   1.1982   0.01006   0.00531  -0.0891   0.4125   0.8919
   7.500   1.2117   0.01039   0.00565  -0.0868   0.4037   0.9041
   7.750   1.2259   0.01070   0.00599  -0.0847   0.3940   0.9195
   8.000   1.2358   0.01113   0.00643  -0.0819   0.3804   0.9468
   8.250   1.2540   0.01176   0.00700  -0.0812   0.3600   1.0000
   8.500   1.2642   0.01246   0.00762  -0.0790   0.3427   1.0000
   8.750   1.2749   0.01318   0.00827  -0.0769   0.3268   1.0000
   9.000   1.2860   0.01391   0.00894  -0.0749   0.3124   1.0000
   9.250   1.2952   0.01475   0.00972  -0.0727   0.2968   1.0000
   9.500   1.3031   0.01569   0.01059  -0.0705   0.2802   1.0000
   9.750   1.3102   0.01672   0.01153  -0.0683   0.2631   1.0000
  10.000   1.3167   0.01781   0.01255  -0.0661   0.2465   1.0000
  10.250   1.3206   0.01908   0.01374  -0.0637   0.2287   1.0000
  10.500   1.3245   0.02042   0.01499  -0.0614   0.2110   1.0000
  10.750   1.3292   0.02174   0.01624  -0.0593   0.1948   1.0000
  11.000   1.3349   0.02308   0.01752  -0.0575   0.1812   1.0000
  11.250   1.3373   0.02467   0.01903  -0.0554   0.1640   1.0000
  11.500   1.3433   0.02609   0.02041  -0.0538   0.1522   1.0000
  11.750   1.3467   0.02773   0.02199  -0.0521   0.1375   1.0000
  12.000   1.3465   0.02970   0.02387  -0.0502   0.1200   1.0000
  12.250   1.3516   0.03136   0.02549  -0.0488   0.1098   1.0000
  12.500   1.3554   0.03316   0.02725  -0.0474   0.0985   1.0000
  12.750   1.3599   0.03496   0.02902  -0.0463   0.0901   1.0000
  13.000   1.3653   0.03673   0.03078  -0.0452   0.0820   1.0000
  13.250   1.3709   0.03855   0.03258  -0.0442   0.0747   1.0000
  13.500   1.3755   0.04050   0.03451  -0.0433   0.0681   1.0000
  13.750   1.3822   0.04229   0.03631  -0.0425   0.0631   1.0000
  14.000   1.3876   0.04426   0.03828  -0.0418   0.0580   1.0000
  14.250   1.3927   0.04627   0.04029  -0.0412   0.0532   1.0000
  14.500   1.3989   0.04824   0.04227  -0.0406   0.0496   1.0000
  14.750   1.4045   0.05031   0.04434  -0.0401   0.0459   1.0000
  15.000   1.4102   0.05239   0.04645  -0.0397   0.0429   1.0000
  15.250   1.4158   0.05451   0.04859  -0.0393   0.0404   1.0000
  15.500   1.4217   0.05666   0.05077  -0.0391   0.0380   1.0000
  15.750   1.4274   0.05883   0.05297  -0.0388   0.0359   1.0000
  16.000   1.4319   0.06122   0.05539  -0.0387   0.0335   1.0000
  16.250   1.4373   0.06349   0.05769  -0.0386   0.0316   1.0000
  16.500   1.4409   0.06603   0.06026  -0.0386   0.0299   1.0000
  16.750   1.4469   0.06831   0.06258  -0.0386   0.0286   1.0000
  17.000   1.4504   0.07095   0.06526  -0.0387   0.0271   1.0000
  17.250   1.4544   0.07353   0.06788  -0.0389   0.0258   1.0000
  17.500   1.4584   0.07617   0.07056  -0.0391   0.0247   1.0000
  17.750   1.4624   0.07880   0.07324  -0.0394   0.0234   1.0000
  18.000   1.4639   0.08182   0.07630  -0.0398   0.0224   1.0000
  18.250   1.4683   0.08448   0.07901  -0.0402   0.0216   1.0000
  18.500   1.4704   0.08749   0.08207  -0.0407   0.0205   1.0000
  18.750   1.4736   0.09036   0.08499  -0.0413   0.0198   1.0000
  19.000   1.4737   0.09368   0.08836  -0.0420   0.0189   1.0000
  19.250   1.4769   0.09659   0.09133  -0.0427   0.0183   1.0000
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