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WORTMANN FX 05-191 AIRFOIL (fx05191-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 05-191 AIRFOIL (fx05191-il)
Reynolds number: 100,000
Max Cl/Cd: 29.24 at α=8.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx05191-il-100000-n5.txt
Download as CSV file: xf-fx05191-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 05-191 AIRFOIL                      
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.4619   0.09360   0.08805  -0.1019   0.9726   0.0357
 -14.000  -0.4884   0.08517   0.07943  -0.1076   0.9686   0.0355
 -13.750  -0.5135   0.07798   0.07203  -0.1124   0.9646   0.0354
 -13.500  -0.5321   0.07202   0.06582  -0.1164   0.9614   0.0353
 -13.250  -0.5477   0.06677   0.06030  -0.1197   0.9588   0.0353
 -13.000  -0.5639   0.06275   0.05603  -0.1207   0.9541   0.0353
 -12.750  -0.5764   0.05884   0.05180  -0.1219   0.9504   0.0354
 -12.500  -0.5832   0.05532   0.04794  -0.1229   0.9475   0.0355
 -12.250  -0.5875   0.05249   0.04479  -0.1228   0.9439   0.0357
 -12.000  -0.5860   0.05034   0.04250  -0.1219   0.9392   0.0360
 -11.750  -0.5759   0.04843   0.04046  -0.1221   0.9360   0.0366
 -11.500  -0.5639   0.04670   0.03858  -0.1224   0.9336   0.0374
 -11.250  -0.5535   0.04522   0.03696  -0.1221   0.9308   0.0383
 -11.000  -0.5542   0.04407   0.03566  -0.1192   0.9252   0.0388
 -10.750  -0.5432   0.04258   0.03395  -0.1184   0.9217   0.0398
 -10.500  -0.5237   0.04087   0.03198  -0.1186   0.9195   0.0406
 -10.250  -0.4970   0.03914   0.02997  -0.1195   0.9180   0.0415
 -10.000  -0.4897   0.03838   0.02905  -0.1165   0.9126   0.0420
  -9.750  -0.4637   0.03715   0.02769  -0.1166   0.9096   0.0430
  -9.500  -0.4347   0.03606   0.02662  -0.1175   0.9072   0.0445
  -9.250  -0.4064   0.03509   0.02560  -0.1184   0.9050   0.0464
  -9.000  -0.3749   0.03413   0.02454  -0.1196   0.9033   0.0488
  -8.750  -0.3685   0.03385   0.02419  -0.1163   0.8976   0.0501
  -8.500  -0.3489   0.03320   0.02353  -0.1152   0.8939   0.0517
  -8.250  -0.3278   0.03243   0.02278  -0.1149   0.8910   0.0537
  -8.000  -0.3046   0.03165   0.02197  -0.1151   0.8886   0.0564
  -7.750  -0.3059   0.03148   0.02177  -0.1108   0.8824   0.0586
  -7.500  -0.2992   0.03101   0.02128  -0.1080   0.8773   0.0617
  -7.250  -0.2846   0.03027   0.02053  -0.1069   0.8739   0.0660
  -7.000  -0.2833   0.02993   0.02014  -0.1032   0.8685   0.0697
  -6.750  -0.2901   0.02971   0.01988  -0.0980   0.8612   0.0726
  -6.500  -0.2804   0.02894   0.01912  -0.0959   0.8575   0.0793
  -6.250  -0.2988   0.02901   0.01915  -0.0885   0.8485   0.0824
  -6.000  -0.2924   0.02832   0.01852  -0.0858   0.8434   0.0943
  -5.750  -0.2774   0.02732   0.01768  -0.0848   0.8404   0.1234
  -5.500  -0.2980   0.02730   0.01776  -0.0769   0.8298   0.1396
  -5.250  -0.2939   0.02571   0.01679  -0.0746   0.8256   0.2449
  -5.000  -0.3096   0.02488   0.01659  -0.0683   0.8167   0.3525
  -4.750  -0.2987   0.02435   0.01669  -0.0656   0.8115   0.4888
  -4.500  -0.2709   0.02433   0.01684  -0.0652   0.8089   0.5550
  -4.250  -0.2382   0.02478   0.01735  -0.0649   0.8071   0.5988
  -4.000  -0.2464   0.02536   0.01798  -0.0585   0.7961   0.6195
  -3.750  -0.2181   0.02648   0.01910  -0.0565   0.7933   0.6470
  -3.500  -0.1847   0.02738   0.01991  -0.0558   0.7913   0.6635
  -3.000  -0.1612   0.02789   0.02026  -0.0502   0.7775   0.6781
  -2.750  -0.1290   0.02740   0.01960  -0.0518   0.7754   0.6873
  -2.500  -0.1286   0.02800   0.02018  -0.0470   0.7655   0.6908
  -2.250  -0.1021   0.02801   0.02009  -0.0467   0.7618   0.6955
  -2.000  -0.0696   0.02757   0.01950  -0.0483   0.7596   0.7038
  -1.500  -0.0413   0.02815   0.01998  -0.0438   0.7463   0.7128
  -1.250  -0.0085   0.02777   0.01947  -0.0453   0.7441   0.7202
  -1.000  -0.0036   0.02836   0.02005  -0.0416   0.7348   0.7243
  -0.750   0.0221   0.02831   0.01994  -0.0414   0.7311   0.7299
  -0.500   0.0545   0.02799   0.01952  -0.0427   0.7289   0.7366
  -0.250   0.0613   0.02858   0.02011  -0.0395   0.7202   0.7409
   0.000   0.0868   0.02853   0.01999  -0.0394   0.7162   0.7467
   0.250   0.1191   0.02824   0.01962  -0.0406   0.7139   0.7530
   0.500   0.1488   0.02805   0.01939  -0.0406   0.7123   0.7565
   0.750   0.1522   0.02882   0.02016  -0.0376   0.7016   0.7630
   1.000   0.1843   0.02855   0.01984  -0.0388   0.6992   0.7692
   1.250   0.2133   0.02830   0.01956  -0.0386   0.6975   0.7726
   1.750   0.2505   0.02892   0.02015  -0.0374   0.6849   0.7849
   2.000   0.2777   0.02868   0.01990  -0.0368   0.6830   0.7883
   2.250   0.3090   0.02834   0.01954  -0.0372   0.6815   0.7927
   2.500   0.3162   0.02934   0.02055  -0.0357   0.6709   0.7998
   2.750   0.3430   0.02913   0.02035  -0.0354   0.6686   0.8035
   3.000   0.3727   0.02882   0.02004  -0.0354   0.6669   0.8075
   3.500   0.4087   0.02967   0.02093  -0.0340   0.6544   0.8181
   3.750   0.4362   0.02942   0.02071  -0.0337   0.6523   0.8218
   4.000   0.4691   0.02905   0.02035  -0.0345   0.6507   0.8261
   4.500   0.4992   0.03015   0.02154  -0.0322   0.6376   0.8357
   4.750   0.5302   0.02981   0.02124  -0.0325   0.6357   0.8397
   5.000   0.5661   0.02939   0.02086  -0.0338   0.6342   0.8440
   5.500   0.5901   0.03071   0.02231  -0.0305   0.6204   0.8529
   5.750   0.6241   0.03027   0.02193  -0.0313   0.6186   0.8569
   6.000   0.6632   0.02975   0.02147  -0.0331   0.6172   0.8608
   6.500   0.6821   0.03122   0.02310  -0.0291   0.6026   0.8692
   6.750   0.7197   0.03062   0.02258  -0.0303   0.6010   0.8728
   7.250   0.7443   0.03216   0.02430  -0.0277   0.5863   0.8808
   7.500   0.7656   0.03233   0.02458  -0.0270   0.5814   0.8845
   7.750   0.7725   0.03342   0.02577  -0.0253   0.5719   0.8887
   8.000   0.8237   0.03171   0.02415  -0.0275   0.5689   0.8915
   8.250   0.8253   0.03284   0.02536  -0.0250   0.5563   0.8954
   8.500   0.8552   0.03190   0.02451  -0.0247   0.5464   0.8987
   8.750   0.8939   0.03057   0.02322  -0.0253   0.5357   0.9017
   9.000   0.8993   0.03149   0.02423  -0.0232   0.5217   0.9058
   9.250   0.9103   0.03217   0.02501  -0.0218   0.5080   0.9095
   9.500   0.9217   0.03261   0.02554  -0.0201   0.4939   0.9130
   9.750   0.9360   0.03306   0.02607  -0.0189   0.4799   0.9167
  10.000   0.9503   0.03366   0.02676  -0.0180   0.4650   0.9205
  10.250   0.9600   0.03451   0.02770  -0.0166   0.4481   0.9240
  10.500   0.9678   0.03540   0.02867  -0.0150   0.4279   0.9277
  10.750   0.9800   0.03607   0.02934  -0.0138   0.4033   0.9317
  11.000   0.9896   0.03699   0.03019  -0.0125   0.3696   0.9356
  11.250   0.9950   0.03797   0.03095  -0.0105   0.3264   0.9396
  11.500   0.9927   0.03988   0.03258  -0.0085   0.2798   0.9435
  11.750   0.9857   0.04243   0.03486  -0.0067   0.2360   0.9477
  12.000   0.9775   0.04517   0.03740  -0.0050   0.2006   0.9527
  12.250   0.9727   0.04791   0.03998  -0.0040   0.1707   0.9583
  12.500   0.9722   0.05049   0.04245  -0.0035   0.1472   0.9648
  13.000   0.9769   0.05513   0.04701  -0.0033   0.1169   1.0000
  13.250   0.9838   0.05752   0.04938  -0.0037   0.1071   1.0000
  13.500   0.9902   0.05999   0.05181  -0.0041   0.0991   1.0000
  13.750   1.0003   0.06210   0.05400  -0.0046   0.0924   1.0000
  14.000   1.0077   0.06449   0.05638  -0.0050   0.0867   1.0000
  14.250   1.0189   0.06650   0.05846  -0.0055   0.0817   1.0000
  14.500   1.0292   0.06865   0.06067  -0.0061   0.0767   1.0000
  14.750   1.0388   0.07078   0.06275  -0.0065   0.0726   1.0000
  15.000   1.0519   0.07267   0.06481  -0.0071   0.0684   1.0000
  15.250   1.0629   0.07477   0.06696  -0.0077   0.0646   1.0000
  15.500   1.0743   0.07674   0.06889  -0.0081   0.0615   1.0000
  15.750   1.0867   0.07880   0.07115  -0.0088   0.0582   1.0000
  16.000   1.0984   0.08091   0.07335  -0.0094   0.0554   1.0000
  16.250   1.1090   0.08311   0.07558  -0.0102   0.0531   1.0000
  16.500   1.1205   0.08524   0.07780  -0.0108   0.0509   1.0000
  16.750   1.1299   0.08774   0.08051  -0.0117   0.0485   1.0000
  17.000   1.1381   0.09036   0.08324  -0.0127   0.0465   1.0000
  17.250   1.1465   0.09291   0.08585  -0.0137   0.0448   1.0000
  17.500   1.1556   0.09535   0.08831  -0.0147   0.0433   1.0000
  17.750   1.1595   0.09872   0.09196  -0.0159   0.0417   1.0000
  18.000   1.1629   0.10212   0.09557  -0.0173   0.0401   1.0000
  18.250   1.1659   0.10554   0.09915  -0.0189   0.0388   1.0000
  18.500   1.1698   0.10881   0.10251  -0.0205   0.0377   1.0000
  18.750   1.1762   0.11163   0.10535  -0.0220   0.0367   1.0000
  19.000   1.1730   0.11619   0.11015  -0.0242   0.0357   1.0000
  19.250   1.1659   0.12149   0.11575  -0.0269   0.0348   1.0000
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