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FX 84-W-175 (fx84w175-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 84-W-175 (fx84w175-il)
Reynolds number: 500,000
Max Cl/Cd: 100.07 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx84w175-il-500000-n5.txt
Download as CSV file: xf-fx84w175-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.5965   0.10720   0.10410  -0.0774   0.9663   0.0200
 -17.500  -0.6384   0.09400   0.09066  -0.0867   0.9595   0.0200
 -17.250  -0.6648   0.08371   0.08017  -0.0951   0.9511   0.0201
 -17.000  -0.6850   0.07497   0.07124  -0.1025   0.9407   0.0202
 -16.500  -0.7214   0.06112   0.05704  -0.1128   0.9152   0.0204
 -16.250  -0.7393   0.05521   0.05096  -0.1165   0.9037   0.0205
 -16.000  -0.7530   0.05026   0.04584  -0.1194   0.8936   0.0206
 -15.750  -0.7636   0.04599   0.04143  -0.1218   0.8841   0.0208
 -15.500  -0.7710   0.04241   0.03770  -0.1234   0.8758   0.0209
 -15.250  -0.7765   0.03929   0.03445  -0.1247   0.8675   0.0211
 -15.000  -0.7797   0.03668   0.03170  -0.1253   0.8601   0.0212
 -14.750  -0.7803   0.03442   0.02933  -0.1257   0.8530   0.0214
 -14.500  -0.7798   0.03243   0.02722  -0.1256   0.8463   0.0216
 -14.250  -0.7771   0.03074   0.02541  -0.1252   0.8402   0.0220
 -14.000  -0.7735   0.02919   0.02375  -0.1247   0.8338   0.0221
 -13.750  -0.7684   0.02785   0.02230  -0.1239   0.8277   0.0224
 -13.500  -0.7622   0.02664   0.02098  -0.1229   0.8225   0.0228
 -13.250  -0.7552   0.02550   0.01973  -0.1218   0.8170   0.0231
 -13.000  -0.7465   0.02454   0.01866  -0.1206   0.8114   0.0234
 -12.750  -0.7371   0.02367   0.01766  -0.1192   0.8064   0.0237
 -12.500  -0.7298   0.02269   0.01663  -0.1176   0.8012   0.0240
 -12.250  -0.7196   0.02194   0.01583  -0.1160   0.7961   0.0245
 -12.000  -0.7090   0.02127   0.01508  -0.1142   0.7913   0.0249
 -11.750  -0.6971   0.02074   0.01448  -0.1124   0.7869   0.0254
 -11.500  -0.6836   0.02023   0.01390  -0.1107   0.7821   0.0258
 -11.250  -0.6670   0.01969   0.01328  -0.1095   0.7776   0.0264
 -11.000  -0.6489   0.01919   0.01268  -0.1084   0.7734   0.0270
 -10.750  -0.6297   0.01872   0.01211  -0.1075   0.7695   0.0274
 -10.500  -0.6109   0.01816   0.01152  -0.1065   0.7652   0.0280
 -10.250  -0.5906   0.01768   0.01099  -0.1058   0.7610   0.0287
 -10.000  -0.5690   0.01727   0.01052  -0.1051   0.7571   0.0294
  -9.750  -0.5468   0.01689   0.01007  -0.1045   0.7534   0.0303
  -9.500  -0.5236   0.01651   0.00964  -0.1041   0.7495   0.0312
  -9.250  -0.5006   0.01612   0.00919  -0.1036   0.7452   0.0321
  -9.000  -0.4777   0.01571   0.00876  -0.1031   0.7413   0.0331
  -8.750  -0.4539   0.01538   0.00837  -0.1026   0.7377   0.0341
  -8.500  -0.4295   0.01506   0.00799  -0.1023   0.7341   0.0352
  -8.250  -0.4046   0.01475   0.00764  -0.1020   0.7300   0.0363
  -8.000  -0.3801   0.01441   0.00728  -0.1017   0.7259   0.0378
  -7.750  -0.3551   0.01412   0.00696  -0.1015   0.7222   0.0394
  -7.500  -0.3296   0.01388   0.00664  -0.1012   0.7187   0.0410
  -7.250  -0.3040   0.01359   0.00634  -0.1010   0.7147   0.0426
  -7.000  -0.2782   0.01331   0.00606  -0.1009   0.7106   0.0445
  -6.750  -0.2521   0.01309   0.00579  -0.1007   0.7068   0.0467
  -6.500  -0.2261   0.01286   0.00552  -0.1006   0.7031   0.0492
  -6.250  -0.1998   0.01263   0.00529  -0.1005   0.6994   0.0520
  -6.000  -0.1730   0.01243   0.00506  -0.1004   0.6954   0.0547
  -5.750  -0.1466   0.01221   0.00484  -0.1004   0.6915   0.0582
  -5.500  -0.1197   0.01205   0.00464  -0.1003   0.6877   0.0619
  -5.250  -0.0931   0.01185   0.00444  -0.1002   0.6840   0.0664
  -5.000  -0.0659   0.01168   0.00427  -0.1003   0.6802   0.0709
  -4.750  -0.0389   0.01150   0.00410  -0.1003   0.6763   0.0768
  -4.500  -0.0118   0.01134   0.00394  -0.1003   0.6724   0.0826
  -4.250   0.0153   0.01120   0.00378  -0.1003   0.6686   0.0896
  -4.000   0.0426   0.01104   0.00365  -0.1003   0.6649   0.0977
  -3.750   0.0700   0.01089   0.00352  -0.1004   0.6609   0.1065
  -3.250   0.1245   0.01063   0.00329  -0.1004   0.6530   0.1298
  -3.000   0.1518   0.01049   0.00318  -0.1005   0.6493   0.1448
  -2.750   0.1793   0.01034   0.00310  -0.1006   0.6454   0.1620
  -2.500   0.2066   0.01019   0.00301  -0.1007   0.6413   0.1825
  -2.250   0.2337   0.01005   0.00293  -0.1007   0.6372   0.2079
  -2.000   0.2608   0.00990   0.00285  -0.1008   0.6334   0.2374
  -1.750   0.2880   0.00971   0.00279  -0.1009   0.6295   0.2743
  -1.500   0.3149   0.00950   0.00273  -0.1010   0.6252   0.3214
  -1.250   0.3415   0.00928   0.00267  -0.1010   0.6211   0.3779
  -0.750   0.3947   0.00885   0.00263  -0.1010   0.6133   0.5081
  -0.500   0.4216   0.00870   0.00265  -0.1010   0.6089   0.5623
  -0.250   0.4486   0.00863   0.00268  -0.1010   0.6046   0.6040
   0.000   0.4758   0.00863   0.00272  -0.1009   0.6008   0.6361
   0.250   0.5034   0.00861   0.00278  -0.1009   0.5969   0.6623
   0.500   0.5308   0.00862   0.00284  -0.1009   0.5924   0.6852
   0.750   0.5580   0.00865   0.00290  -0.1008   0.5880   0.7037
   1.000   0.5851   0.00872   0.00295  -0.1007   0.5840   0.7197
   1.250   0.6126   0.00875   0.00303  -0.1007   0.5800   0.7347
   1.500   0.6396   0.00881   0.00311  -0.1006   0.5754   0.7509
   1.750   0.6661   0.00888   0.00319  -0.1004   0.5709   0.7679
   2.000   0.6922   0.00897   0.00329  -0.1000   0.5668   0.7811
   2.250   0.7192   0.00903   0.00337  -0.1000   0.5624   0.7900
   2.500   0.7457   0.00910   0.00346  -0.0998   0.5576   0.7978
   3.000   0.7978   0.00929   0.00364  -0.0993   0.5487   0.8121
   3.250   0.8241   0.00938   0.00374  -0.0992   0.5439   0.8194
   3.500   0.8496   0.00948   0.00384  -0.0989   0.5389   0.8260
   3.750   0.8741   0.00960   0.00395  -0.0983   0.5343   0.8326
   4.000   0.8998   0.00970   0.00408  -0.0981   0.5297   0.8396
   4.250   0.9244   0.00980   0.00420  -0.0976   0.5246   0.8459
   4.500   0.9478   0.00993   0.00433  -0.0969   0.5196   0.8530
   4.750   0.9720   0.01006   0.00447  -0.0964   0.5150   0.8601
   5.000   0.9950   0.01016   0.00462  -0.0956   0.5099   0.8669
   5.250   1.0171   0.01031   0.00477  -0.0947   0.5045   0.8747
   5.500   1.0379   0.01046   0.00494  -0.0935   0.4993   0.8822
   5.750   1.0579   0.01058   0.00510  -0.0922   0.4931   0.8911
   6.000   1.0737   0.01073   0.00527  -0.0900   0.4869   0.9008
   6.250   1.0903   0.01090   0.00547  -0.0880   0.4812   0.9122
   6.500   1.1061   0.01107   0.00568  -0.0859   0.4748   0.9261
   6.750   1.1208   0.01130   0.00593  -0.0837   0.4684   0.9453
   7.000   1.1479   0.01151   0.00618  -0.0841   0.4617   0.9699
   7.250   1.1713   0.01179   0.00646  -0.0839   0.4548   1.0000
   7.500   1.1902   0.01211   0.00678  -0.0828   0.4486   1.0000
   7.750   1.2090   0.01243   0.00711  -0.0817   0.4414   1.0000
   8.000   1.2247   0.01287   0.00752  -0.0802   0.4339   1.0000
   8.250   1.2428   0.01324   0.00791  -0.0791   0.4261   1.0000
   8.500   1.2567   0.01377   0.00841  -0.0773   0.4173   1.0000
   8.750   1.2692   0.01436   0.00898  -0.0755   0.4049   1.0000
   9.000   1.2786   0.01511   0.00969  -0.0733   0.3898   1.0000
   9.250   1.2883   0.01590   0.01043  -0.0712   0.3755   1.0000
   9.500   1.2979   0.01675   0.01123  -0.0692   0.3617   1.0000
   9.750   1.3066   0.01767   0.01211  -0.0672   0.3482   1.0000
  10.000   1.3145   0.01867   0.01308  -0.0652   0.3349   1.0000
  10.250   1.3210   0.01980   0.01416  -0.0632   0.3202   1.0000
  10.500   1.3268   0.02101   0.01532  -0.0611   0.3052   1.0000
  10.750   1.3318   0.02232   0.01657  -0.0591   0.2899   1.0000
  11.000   1.3354   0.02376   0.01796  -0.0571   0.2740   1.0000
  11.250   1.3374   0.02538   0.01951  -0.0550   0.2558   1.0000
  11.500   1.3388   0.02711   0.02118  -0.0530   0.2381   1.0000
  11.750   1.3412   0.02885   0.02286  -0.0513   0.2225   1.0000
  12.000   1.3430   0.03070   0.02465  -0.0496   0.2070   1.0000
  12.250   1.3435   0.03272   0.02661  -0.0480   0.1907   1.0000
  12.500   1.3456   0.03469   0.02853  -0.0466   0.1767   1.0000
  12.750   1.3463   0.03682   0.03060  -0.0452   0.1613   1.0000
  13.000   1.3471   0.03903   0.03276  -0.0440   0.1473   1.0000
  13.250   1.3479   0.04131   0.03500  -0.0429   0.1338   1.0000
  13.500   1.3490   0.04361   0.03726  -0.0419   0.1212   1.0000
  13.750   1.3490   0.04609   0.03969  -0.0409   0.1087   1.0000
  14.000   1.3498   0.04856   0.04214  -0.0402   0.0984   1.0000
  14.250   1.3518   0.05097   0.04453  -0.0395   0.0897   1.0000
  14.500   1.3547   0.05335   0.04691  -0.0390   0.0824   1.0000
  14.750   1.3579   0.05575   0.04932  -0.0386   0.0761   1.0000
  15.000   1.3599   0.05833   0.05189  -0.0383   0.0699   1.0000
  15.250   1.3636   0.06077   0.05437  -0.0381   0.0649   1.0000
  15.500   1.3663   0.06335   0.05695  -0.0379   0.0600   1.0000
  15.750   1.3687   0.06602   0.05965  -0.0378   0.0556   1.0000
  16.000   1.3724   0.06860   0.06225  -0.0378   0.0523   1.0000
  16.250   1.3752   0.07132   0.06501  -0.0379   0.0488   1.0000
  16.500   1.3780   0.07408   0.06781  -0.0380   0.0462   1.0000
  16.750   1.3811   0.07683   0.07061  -0.0382   0.0435   1.0000
  17.000   1.3827   0.07981   0.07362  -0.0385   0.0408   1.0000
  17.250   1.3859   0.08264   0.07651  -0.0389   0.0389   1.0000
  17.500   1.3884   0.08558   0.07950  -0.0393   0.0368   1.0000
  17.750   1.3893   0.08878   0.08274  -0.0399   0.0349   1.0000
  18.000   1.3922   0.09173   0.08576  -0.0404   0.0332   1.0000
  18.250   1.3937   0.09489   0.08897  -0.0411   0.0317   1.0000
  18.750   1.3964   0.10138   0.09558  -0.0427   0.0290   1.0000
  19.000   1.3976   0.10467   0.09894  -0.0436   0.0277   1.0000
  19.250   1.3981   0.10808   0.10240  -0.0445   0.0266   1.0000
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