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WORTMANN FX 05-188 AIRFOIL (fx05188-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 05-188 AIRFOIL (fx05188-il)
Reynolds number: 500,000
Max Cl/Cd: 99.52 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx05188-il-500000.txt
Download as CSV file: xf-fx05188-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 05-188 AIRFOIL                      
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.2514   0.07289   0.06983  -0.1244   0.8579   0.0415
 -13.500  -0.2907   0.06340   0.06022  -0.1291   0.8548   0.0412
 -13.250  -0.3247   0.05592   0.05260  -0.1322   0.8507   0.0409
 -13.000  -0.3637   0.04951   0.04597  -0.1344   0.8460   0.0412
 -12.750  -0.3917   0.04492   0.04122  -0.1351   0.8408   0.0413
 -12.500  -0.4185   0.04123   0.03736  -0.1347   0.8352   0.0415
 -12.250  -0.6037   0.03618   0.03051  -0.1311   0.8389   0.0259
 -12.000  -0.6006   0.03466   0.02879  -0.1293   0.8325   0.0258
 -11.750  -0.5936   0.03390   0.02786  -0.1278   0.8270   0.0256
 -11.500  -0.5586   0.03116   0.02503  -0.1291   0.8243   0.0251
 -11.250  -0.5403   0.02948   0.02321  -0.1286   0.8203   0.0250
 -11.000  -0.5256   0.02825   0.02181  -0.1276   0.8163   0.0251
 -10.750  -0.5009   0.02692   0.02033  -0.1277   0.8131   0.0251
 -10.500  -0.4785   0.02593   0.01921  -0.1274   0.8097   0.0252
 -10.250  -0.4547   0.02497   0.01817  -0.1271   0.8066   0.0252
 -10.000  -0.4347   0.02425   0.01737  -0.1265   0.8033   0.0254
  -9.750  -0.4121   0.02355   0.01657  -0.1261   0.8000   0.0255
  -9.500  -0.3752   0.02254   0.01556  -0.1267   0.7979   0.0260
  -9.250  -0.3517   0.02189   0.01490  -0.1263   0.7951   0.0264
  -9.000  -0.3327   0.02130   0.01431  -0.1255   0.7922   0.0268
  -8.750  -0.3154   0.02071   0.01373  -0.1245   0.7892   0.0273
  -8.500  -0.2988   0.02012   0.01312  -0.1234   0.7861   0.0279
  -8.250  -0.2827   0.01953   0.01251  -0.1223   0.7833   0.0282
  -8.000  -0.2671   0.01895   0.01188  -0.1211   0.7807   0.0285
  -7.750  -0.2516   0.01838   0.01126  -0.1199   0.7781   0.0292
  -7.500  -0.2377   0.01781   0.01068  -0.1184   0.7756   0.0296
  -7.250  -0.2243   0.01724   0.01009  -0.1168   0.7728   0.0301
  -7.000  -0.2107   0.01669   0.00952  -0.1152   0.7700   0.0304
  -6.750  -0.2019   0.01599   0.00879  -0.1130   0.7672   0.0310
  -6.500  -0.1950   0.01541   0.00819  -0.1103   0.7648   0.0320
  -6.250  -0.1825   0.01501   0.00774  -0.1085   0.7624   0.0329
  -6.000  -0.1666   0.01459   0.00732  -0.1073   0.7599   0.0343
  -5.750  -0.1479   0.01423   0.00694  -0.1064   0.7572   0.0358
  -5.500  -0.1288   0.01381   0.00652  -0.1056   0.7547   0.0384
  -5.250  -0.1070   0.01349   0.00618  -0.1052   0.7524   0.0421
  -5.000  -0.0873   0.01292   0.00574  -0.1046   0.7500   0.0682
  -4.500  -0.0560   0.00978   0.00418  -0.1050   0.7451   0.4364
  -4.250  -0.0281   0.00935   0.00404  -0.1058   0.7426   0.5174
  -4.000   0.0009   0.00920   0.00399  -0.1064   0.7402   0.5554
  -3.750   0.0301   0.00916   0.00404  -0.1068   0.7378   0.5856
  -3.500   0.0599   0.00921   0.00409  -0.1073   0.7354   0.6068
  -3.250   0.0899   0.00934   0.00420  -0.1078   0.7331   0.6227
  -3.000   0.1201   0.00957   0.00439  -0.1083   0.7307   0.6350
  -2.750   0.1486   0.00975   0.00457  -0.1084   0.7282   0.6423
  -2.500   0.1775   0.00992   0.00471  -0.1087   0.7255   0.6505
  -2.250   0.2061   0.01005   0.00484  -0.1088   0.7228   0.6560
  -2.000   0.2348   0.01018   0.00496  -0.1090   0.7201   0.6604
  -1.750   0.2650   0.01024   0.00496  -0.1097   0.7175   0.6650
  -1.500   0.2959   0.01030   0.00492  -0.1105   0.7149   0.6692
  -1.250   0.3240   0.01040   0.00504  -0.1106   0.7121   0.6718
  -1.000   0.3514   0.01046   0.00513  -0.1106   0.7092   0.6749
  -0.750   0.3801   0.01052   0.00518  -0.1110   0.7061   0.6784
  -0.500   0.4101   0.01055   0.00517  -0.1116   0.7032   0.6825
  -0.250   0.4399   0.01057   0.00516  -0.1122   0.7003   0.6859
   0.000   0.4688   0.01069   0.00526  -0.1124   0.6973   0.6888
   0.250   0.4957   0.01079   0.00540  -0.1123   0.6938   0.6921
   0.500   0.5233   0.01081   0.00544  -0.1124   0.6896   0.6960
   0.750   0.5531   0.01082   0.00541  -0.1130   0.6855   0.7001
   1.000   0.5823   0.01080   0.00538  -0.1134   0.6823   0.7028
   1.250   0.6116   0.01091   0.00547  -0.1138   0.6792   0.7050
   1.500   0.6376   0.01092   0.00555  -0.1136   0.6758   0.7074
   1.750   0.6652   0.01094   0.00560  -0.1137   0.6719   0.7100
   2.000   0.6941   0.01094   0.00561  -0.1141   0.6683   0.7130
   2.250   0.7244   0.01096   0.00559  -0.1149   0.6651   0.7163
   2.500   0.7541   0.01100   0.00562  -0.1155   0.6620   0.7189
   2.750   0.7795   0.01100   0.00571  -0.1151   0.6580   0.7210
   3.000   0.8065   0.01101   0.00577  -0.1151   0.6539   0.7230
   3.250   0.8347   0.01100   0.00577  -0.1153   0.6499   0.7251
   3.500   0.8626   0.01099   0.00576  -0.1154   0.6450   0.7275
   3.750   0.8888   0.01096   0.00579  -0.1153   0.6388   0.7301
   4.000   0.9173   0.01094   0.00578  -0.1157   0.6341   0.7329
   4.250   0.9463   0.01096   0.00578  -0.1161   0.6297   0.7353
   4.500   0.9711   0.01095   0.00586  -0.1157   0.6237   0.7371
   4.750   0.9970   0.01093   0.00584  -0.1154   0.6166   0.7388
   5.000   1.0203   0.01093   0.00589  -0.1146   0.6061   0.7406
   5.250   1.0438   0.01096   0.00592  -0.1139   0.5942   0.7426
   5.500   1.0672   0.01106   0.00598  -0.1132   0.5825   0.7447
   5.750   1.0904   0.01117   0.00609  -0.1125   0.5704   0.7472
   6.000   1.1143   0.01130   0.00623  -0.1120   0.5595   0.7495
   6.250   1.1377   0.01147   0.00637  -0.1115   0.5482   0.7514
   6.500   1.1574   0.01163   0.00652  -0.1101   0.5341   0.7530
   6.750   1.1749   0.01185   0.00673  -0.1084   0.5180   0.7546
   7.000   1.1908   0.01210   0.00698  -0.1063   0.5004   0.7564
   7.250   1.2029   0.01237   0.00724  -0.1035   0.4818   0.7583
   7.500   1.2118   0.01275   0.00757  -0.1003   0.4594   0.7604
   7.750   1.2162   0.01336   0.00807  -0.0964   0.4317   0.7627
   8.000   1.2169   0.01419   0.00876  -0.0922   0.4026   0.7650
   8.250   1.2161   0.01520   0.00963  -0.0882   0.3731   0.7672
   8.500   1.2128   0.01642   0.01070  -0.0841   0.3393   0.7690
   8.750   1.2049   0.01798   0.01209  -0.0796   0.2973   0.7708
   9.000   1.1950   0.01987   0.01376  -0.0754   0.2553   0.7725
   9.250   1.1858   0.02191   0.01558  -0.0716   0.2132   0.7744
   9.500   1.1795   0.02393   0.01739  -0.0683   0.1751   0.7762
   9.750   1.1775   0.02580   0.01910  -0.0658   0.1442   0.7780
  10.000   1.1768   0.02769   0.02083  -0.0636   0.1148   0.7796
  10.250   1.1780   0.02952   0.02254  -0.0617   0.0934   0.7812
  10.500   1.1836   0.03114   0.02410  -0.0603   0.0806   0.7828
  10.750   1.1898   0.03277   0.02569  -0.0590   0.0697   0.7841
  11.000   1.1956   0.03443   0.02732  -0.0577   0.0567   0.7853
  11.250   1.2013   0.03614   0.02898  -0.0565   0.0465   0.7865
  11.500   1.2084   0.03781   0.03064  -0.0555   0.0412   0.7878
  11.750   1.2154   0.03952   0.03235  -0.0545   0.0379   0.7891
  12.000   1.2239   0.04117   0.03406  -0.0537   0.0360   0.7907
  12.250   1.2327   0.04284   0.03578  -0.0530   0.0346   0.7924
  12.500   1.2402   0.04468   0.03766  -0.0523   0.0334   0.7939
  12.750   1.2452   0.04681   0.03983  -0.0516   0.0322   0.7954
  13.000   1.2502   0.04901   0.04209  -0.0510   0.0314   0.7969
  13.250   1.2586   0.05093   0.04409  -0.0506   0.0308   0.7983
  13.500   1.2663   0.05298   0.04621  -0.0503   0.0301   0.7997
  13.750   1.2737   0.05503   0.04833  -0.0500   0.0294   0.8011
  14.000   1.2796   0.05728   0.05065  -0.0497   0.0287   0.8026
  14.250   1.2853   0.05960   0.05304  -0.0495   0.0281   0.8041
  14.500   1.2891   0.06219   0.05568  -0.0493   0.0276   0.8056
  14.750   1.2913   0.06500   0.05855  -0.0491   0.0270   0.8073
  15.000   1.2920   0.06799   0.06161  -0.0490   0.0265   0.8091
  15.250   1.3003   0.07020   0.06391  -0.0491   0.0262   0.8112
  15.500   1.3077   0.07258   0.06637  -0.0492   0.0259   0.8133
  15.750   1.3153   0.07496   0.06882  -0.0495   0.0255   0.8151
  16.000   1.3224   0.07737   0.07132  -0.0497   0.0251   0.8170
  16.250   1.3292   0.07982   0.07386  -0.0500   0.0247   0.8189
  16.500   1.3362   0.08227   0.07639  -0.0503   0.0242   0.8210
  16.750   1.3425   0.08484   0.07904  -0.0507   0.0238   0.8233
  17.000   1.3492   0.08737   0.08162  -0.0511   0.0234   0.8257
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