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FX 84-W-218 (fx84w218-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: FX 84-W-218 (fx84w218-il)
Reynolds number: 100,000
Max Cl/Cd: 24.66 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx84w218-il-100000-n5.txt
Download as CSV file: xf-fx84w218-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 84-W-218                                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.6350   0.07318   0.06643  -0.1013   0.9806   0.0777
 -15.500  -0.6604   0.06562   0.05852  -0.1075   0.9704   0.0788
 -15.250  -0.6405   0.06371   0.05663  -0.1102   0.9629   0.0801
 -15.000  -0.6352   0.06031   0.05311  -0.1136   0.9544   0.0816
 -14.750  -0.6361   0.05642   0.04901  -0.1171   0.9463   0.0833
 -14.500  -0.6400   0.05271   0.04502  -0.1197   0.9374   0.0849
 -14.250  -0.6390   0.04991   0.04201  -0.1214   0.9287   0.0866
 -14.000  -0.6255   0.04850   0.04060  -0.1221   0.9206   0.0881
 -13.750  -0.6187   0.04678   0.03879  -0.1224   0.9123   0.0898
 -13.500  -0.6158   0.04493   0.03679  -0.1224   0.9036   0.0917
 -13.250  -0.6154   0.04301   0.03462  -0.1221   0.8957   0.0938
 -13.000  -0.6059   0.04185   0.03344  -0.1215   0.8879   0.0956
 -12.750  -0.5966   0.04072   0.03228  -0.1209   0.8816   0.0976
 -12.500  -0.5899   0.03953   0.03100  -0.1201   0.8738   0.0999
 -12.250  -0.5841   0.03824   0.02953  -0.1191   0.8667   0.1024
 -12.000  -0.5740   0.03725   0.02848  -0.1181   0.8612   0.1047
 -11.750  -0.5637   0.03637   0.02761  -0.1173   0.8541   0.1072
 -11.500  -0.5540   0.03541   0.02656  -0.1162   0.8477   0.1102
 -11.250  -0.5438   0.03444   0.02544  -0.1150   0.8425   0.1132
 -11.000  -0.5324   0.03371   0.02474  -0.1140   0.8361   0.1160
 -10.750  -0.5217   0.03295   0.02394  -0.1127   0.8297   0.1194
 -10.500  -0.5102   0.03216   0.02298  -0.1113   0.8246   0.1233
 -10.250  -0.4980   0.03146   0.02231  -0.1099   0.8201   0.1264
 -10.000  -0.4867   0.03087   0.02170  -0.1086   0.8133   0.1304
  -9.750  -0.4742   0.03023   0.02096  -0.1072   0.8075   0.1350
  -9.500  -0.4622   0.02959   0.02034  -0.1056   0.8029   0.1390
  -9.250  -0.4493   0.02900   0.01968  -0.1040   0.7987   0.1440
  -9.000  -0.4374   0.02855   0.01923  -0.1024   0.7921   0.1489
  -8.750  -0.4264   0.02807   0.01875  -0.1005   0.7865   0.1540
  -8.500  -0.4126   0.02759   0.01815  -0.0987   0.7821   0.1603
  -8.250  -0.4010   0.02709   0.01768  -0.0966   0.7786   0.1658
  -8.000  -0.3917   0.02694   0.01751  -0.0943   0.7719   0.1723
  -7.750  -0.3805   0.02661   0.01721  -0.0921   0.7664   0.1786
  -7.500  -0.3660   0.02622   0.01678  -0.0903   0.7620   0.1866
  -7.250  -0.3497   0.02576   0.01631  -0.0886   0.7587   0.1947
  -7.000  -0.3367   0.02559   0.01613  -0.0867   0.7531   0.2036
  -6.750  -0.3242   0.02538   0.01597  -0.0847   0.7473   0.2122
  -6.500  -0.3072   0.02508   0.01562  -0.0831   0.7429   0.2232
  -6.250  -0.2898   0.02465   0.01524  -0.0816   0.7393   0.2341
  -6.000  -0.2693   0.02423   0.01479  -0.0804   0.7366   0.2467
  -5.750  -0.2597   0.02432   0.01493  -0.0780   0.7292   0.2585
  -5.500  -0.2443   0.02408   0.01476  -0.0762   0.7243   0.2718
  -5.250  -0.2251   0.02375   0.01446  -0.0749   0.7205   0.2874
  -5.000  -0.2033   0.02336   0.01408  -0.0739   0.7175   0.3048
  -4.750  -0.1875   0.02325   0.01402  -0.0722   0.7127   0.3223
  -4.500  -0.1755   0.02328   0.01413  -0.0699   0.7063   0.3400
  -4.250  -0.1566   0.02306   0.01397  -0.0685   0.7021   0.3609
  -4.000  -0.1342   0.02273   0.01372  -0.0675   0.6988   0.3841
  -3.750  -0.1093   0.02238   0.01343  -0.0668   0.6963   0.4093
  -3.500  -0.0997   0.02261   0.01377  -0.0642   0.6896   0.4303
  -3.250  -0.0838   0.02264   0.01390  -0.0623   0.6842   0.4539
  -3.000  -0.0608   0.02249   0.01380  -0.0613   0.6805   0.4795
  -2.750  -0.0342   0.02227   0.01361  -0.0608   0.6777   0.5053
  -2.500  -0.0050   0.02205   0.01339  -0.0607   0.6754   0.5306
  -2.250  -0.0025   0.02265   0.01412  -0.0569   0.6670   0.5479
  -2.000   0.0181   0.02273   0.01424  -0.0556   0.6625   0.5687
  -1.750   0.0451   0.02266   0.01417  -0.0551   0.6593   0.5890
  -1.500   0.0754   0.02253   0.01403  -0.0550   0.6568   0.6082
  -1.250   0.0938   0.02276   0.01428  -0.0534   0.6521   0.6248
  -1.000   0.0995   0.02327   0.01482  -0.0501   0.6447   0.6405
  -0.750   0.1248   0.02333   0.01488  -0.0493   0.6410   0.6554
  -0.500   0.1549   0.02325   0.01478  -0.0491   0.6382   0.6700
  -0.250   0.1877   0.02309   0.01454  -0.0495   0.6361   0.6856
   0.000   0.1807   0.02401   0.01558  -0.0444   0.6271   0.6964
   0.250   0.2002   0.02417   0.01571  -0.0429   0.6224   0.7097
   0.500   0.2293   0.02412   0.01564  -0.0426   0.6195   0.7223
   0.750   0.2626   0.02398   0.01545  -0.0429   0.6172   0.7343
   1.250   0.2644   0.02519   0.01674  -0.0348   0.6033   0.7573
   1.500   0.2935   0.02509   0.01660  -0.0345   0.6003   0.7690
   1.750   0.3284   0.02490   0.01637  -0.0351   0.5981   0.7788
   2.000   0.3666   0.02468   0.01609  -0.0362   0.5963   0.7885
   2.250   0.3196   0.02646   0.01802  -0.0260   0.5834   0.8013
   2.500   0.3493   0.02627   0.01780  -0.0257   0.5807   0.8113
   2.750   0.3844   0.02592   0.01739  -0.0263   0.5786   0.8207
   3.000   0.4236   0.02556   0.01698  -0.0274   0.5770   0.8285
   3.500   0.4094   0.02764   0.01918  -0.0184   0.5609   0.8526
   3.750   0.4453   0.02718   0.01866  -0.0191   0.5591   0.8617
   4.000   0.4856   0.02666   0.01810  -0.0202   0.5576   0.8692
   4.500   0.4739   0.02901   0.02057  -0.0125   0.5412   0.8967
   4.750   0.5140   0.02843   0.01996  -0.0137   0.5396   0.9046
   5.250   0.5217   0.03097   0.02262  -0.0100   0.5235   0.9330
   5.500   0.5678   0.03039   0.02201  -0.0124   0.5218   0.9404
   5.750   0.6147   0.02968   0.02127  -0.0147   0.5203   0.9488
   6.250   0.6538   0.03243   0.02415  -0.0175   0.5044   0.9729
   6.500   0.7043   0.03168   0.02337  -0.0205   0.5026   0.9804
   6.750   0.7584   0.03076   0.02241  -0.0239   0.5009   0.9871
   7.250   0.7394   0.03377   0.02543  -0.0179   0.4842   1.0000
   7.500   0.7798   0.03281   0.02442  -0.0189   0.4825   1.0000
   8.000   0.7726   0.03619   0.02781  -0.0146   0.4658   1.0000
   8.250   0.8146   0.03511   0.02668  -0.0155   0.4640   1.0000
   8.750   0.8127   0.03870   0.03030  -0.0122   0.4474   1.0000
   9.000   0.8547   0.03754   0.02910  -0.0130   0.4456   1.0000
   9.500   0.8536   0.04136   0.03298  -0.0101   0.4290   1.0000
   9.750   0.8963   0.04004   0.03162  -0.0108   0.4270   1.0000
  10.250   0.8952   0.04406   0.03572  -0.0082   0.4105   1.0000
  10.500   0.9385   0.04260   0.03423  -0.0088   0.4084   1.0000
  11.000   0.9386   0.04670   0.03841  -0.0066   0.3919   1.0000
  11.500   0.9429   0.05078   0.04257  -0.0050   0.3757   1.0000
  11.750   0.9839   0.04924   0.04099  -0.0052   0.3731   1.0000
  12.250   0.9873   0.05352   0.04536  -0.0038   0.3568   1.0000
  12.750   0.9936   0.05779   0.04971  -0.0028   0.3409   1.0000
  13.000   1.0331   0.05617   0.04805  -0.0028   0.3377   1.0000
  13.250   1.0040   0.06179   0.05379  -0.0022   0.3255   1.0000
  13.500   1.0378   0.06067   0.05264  -0.0020   0.3214   1.0000
  13.750   1.0213   0.06516   0.05722  -0.0018   0.3111   1.0000
  14.000   1.0451   0.06511   0.05716  -0.0016   0.3055   1.0000
  14.250   1.0564   0.06651   0.05858  -0.0015   0.2987   1.0000
  14.500   1.0539   0.06955   0.06167  -0.0014   0.2899   1.0000
  14.750   1.0915   0.06781   0.05986  -0.0011   0.2856   1.0000
  15.000   1.0647   0.07388   0.06608  -0.0015   0.2749   1.0000
  15.250   1.0952   0.07293   0.06506  -0.0012   0.2699   1.0000
  15.500   1.0779   0.07804   0.07029  -0.0017   0.2605   1.0000
  15.750   1.0983   0.07833   0.07056  -0.0016   0.2546   1.0000
  16.000   1.0938   0.08191   0.07420  -0.0020   0.2467   1.0000
  16.250   1.1016   0.08388   0.07619  -0.0022   0.2398   1.0000
  16.500   1.1132   0.08535   0.07766  -0.0024   0.2336   1.0000
  16.750   1.1061   0.08942   0.08182  -0.0032   0.2256   1.0000
  17.000   1.1354   0.08842   0.08071  -0.0028   0.2207   1.0000
  17.250   1.1113   0.09497   0.08745  -0.0043   0.2120   1.0000
  17.500   1.1331   0.09498   0.08738  -0.0042   0.2067   1.0000
  17.750   1.1176   0.10045   0.09299  -0.0056   0.1990   1.0000
  18.000   1.1296   0.10189   0.09441  -0.0060   0.1931   1.0000
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