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WORTMANN FX 05-188 AIRFOIL (fx05188-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 05-188 AIRFOIL (fx05188-il)
Reynolds number: 100,000
Max Cl/Cd: 27.8 at α=11.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx05188-il-100000.txt
Download as CSV file: xf-fx05188-il-100000.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 =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.3603   0.12098   0.11638  -0.0638   0.9812   0.1721
 -11.250  -0.3331   0.11807   0.11342  -0.0646   0.9780   0.1764
 -11.000  -0.3515   0.11244   0.10785  -0.0707   0.9744   0.1881
 -10.750  -0.3201   0.10930   0.10464  -0.0717   0.9721   0.1916
 -10.500  -0.3156   0.10586   0.10121  -0.0733   0.9670   0.1972
 -10.250  -0.3190   0.10106   0.09644  -0.0769   0.9632   0.2069
 -10.000  -0.5987   0.06780   0.06250  -0.0934   0.9467   0.1027
  -9.750  -0.6574   0.06479   0.05902  -0.0861   0.9373   0.0910
  -9.500  -0.6998   0.06062   0.05389  -0.0814   0.9309   0.0813
  -9.250  -0.6912   0.05802   0.05124  -0.0794   0.9269   0.0794
  -9.000  -0.6926   0.05551   0.04861  -0.0765   0.9224   0.0780
  -8.750  -0.6847   0.05254   0.04537  -0.0753   0.9185   0.0757
  -8.500  -0.6703   0.04911   0.04140  -0.0749   0.9152   0.0725
  -8.250  -0.6663   0.04716   0.03884  -0.0722   0.9112   0.0703
  -8.000  -0.6640   0.04620   0.03760  -0.0687   0.9068   0.0696
  -7.750  -0.6457   0.04484   0.03596  -0.0677   0.9028   0.0692
  -7.500  -0.6161   0.04295   0.03384  -0.0685   0.8996   0.0693
  -7.250  -0.5778   0.04090   0.03172  -0.0705   0.8973   0.0705
  -7.000  -0.5688   0.04022   0.03102  -0.0679   0.8933   0.0716
  -6.750  -0.5589   0.03962   0.03039  -0.0654   0.8889   0.0733
  -6.500  -0.5337   0.03878   0.02951  -0.0651   0.8850   0.0752
  -6.250  -0.4987   0.03792   0.02859  -0.0660   0.8818   0.0770
  -6.000  -0.4572   0.03716   0.02778  -0.0679   0.8794   0.0797
  -5.750  -0.4691   0.03724   0.02782  -0.0620   0.8741   0.0804
  -5.500  -0.4581   0.03662   0.02735  -0.0595   0.8696   0.0829
  -5.250  -0.4360   0.03603   0.02686  -0.0592   0.8656   0.0878
  -5.000  -0.4047   0.03528   0.02613  -0.0605   0.8624   0.0972
  -4.750  -0.4109   0.03517   0.02604  -0.0562   0.8576   0.1025
  -4.500  -0.4031   0.03463   0.02557  -0.0542   0.8532   0.1154
  -4.250  -0.3953   0.03118   0.02488  -0.0539   0.8495   0.5217
  -4.000  -0.3712   0.03398   0.02786  -0.0490   0.8455   0.6136
  -3.750  -0.3656   0.03528   0.02903  -0.0452   0.8408   0.6375
  -3.500  -0.3622   0.03696   0.03067  -0.0400   0.8367   0.6542
  -3.250  -0.3524   0.03946   0.03318  -0.0334   0.8321   0.6725
  -3.000  -0.3320   0.04317   0.03689  -0.0257   0.8284   0.6964
  -2.750  -0.3354   0.04507   0.03879  -0.0180   0.8244   0.7123
  -2.500  -0.3365   0.04648   0.04020  -0.0115   0.8208   0.7275
  -2.250  -0.3221   0.04758   0.04123  -0.0076   0.8165   0.7427
  -2.000  -0.2927   0.04795   0.04145  -0.0077   0.8125   0.7551
  -1.750  -0.2767   0.04817   0.04156  -0.0064   0.8087   0.7627
  -1.500  -0.2854   0.04796   0.04131  -0.0025   0.8049   0.7713
  -1.250  -0.2739   0.04802   0.04130  -0.0007   0.8008   0.7783
  -1.000  -0.2484   0.04790   0.04105  -0.0017   0.7967   0.7862
  -0.750  -0.3217   0.05036   0.04374   0.0078   0.8616   0.7939
  -0.500  -0.3255   0.04914   0.04247   0.0110   0.8528   0.8017
  -0.250  -0.2773   0.05051   0.04368   0.0076   0.8441   0.8073
   0.000  -0.2782   0.04953   0.04264   0.0097   0.8357   0.8155
   0.250  -0.2373   0.05049   0.04348   0.0079   0.8264   0.8204
   0.500  -0.2390   0.04998   0.04295   0.0108   0.8208   0.8276
   0.750  -0.1300   0.04821   0.04084   0.0032   0.7589   0.8332
   1.000  -0.1263   0.04841   0.04102   0.0059   0.7542   0.8399
   1.250  -0.0911   0.04851   0.04102   0.0036   0.7485   0.8469
   1.500  -0.0830   0.04860   0.04110   0.0060   0.7414   0.8523
   1.750  -0.0673   0.04885   0.04131   0.0063   0.7360   0.8582
   2.000  -0.0242   0.04896   0.04134   0.0035   0.7310   0.8634
   2.250  -0.0283   0.04923   0.04163   0.0068   0.7231   0.8687
   2.500   0.0018   0.04939   0.04174   0.0055   0.7169   0.8736
   2.750   0.0293   0.04972   0.04202   0.0043   0.7104   0.8785
   3.000   0.0321   0.05011   0.04243   0.0066   0.7039   0.8836
   3.250   0.0695   0.05024   0.04252   0.0048   0.6985   0.8884
   3.500   0.0824   0.05087   0.04314   0.0047   0.6898   0.8929
   3.750   0.1008   0.05112   0.04339   0.0054   0.6840   0.8974
   4.000   0.1422   0.05122   0.04347   0.0035   0.6802   0.9021
   4.250   0.1404   0.05214   0.04442   0.0049   0.6701   0.9070
   4.500   0.1736   0.05225   0.04453   0.0038   0.6651   0.9108
   4.750   0.1836   0.05303   0.04533   0.0046   0.6578   0.9153
   5.000   0.2044   0.05360   0.04591   0.0042   0.6511   0.9201
   5.250   0.2464   0.05356   0.04589   0.0023   0.6474   0.9241
   5.500   0.2410   0.05482   0.04719   0.0041   0.6374   0.9286
   5.750   0.2794   0.05491   0.04731   0.0024   0.6327   0.9327
   6.000   0.2837   0.05614   0.04858   0.0031   0.6237   0.9371
   6.250   0.3146   0.05636   0.04884   0.0022   0.6184   0.9416
   6.500   0.3288   0.05738   0.04991   0.0021   0.6105   0.9461
   6.750   0.3529   0.05801   0.05060   0.0013   0.6040   0.9505
   7.000   0.3999   0.05771   0.05036  -0.0009   0.6005   0.9550
   7.250   0.3973   0.05956   0.05228  -0.0003   0.5890   0.9601
   7.500   0.4448   0.05928   0.05209  -0.0027   0.5852   0.9647
   7.750   0.4473   0.06126   0.05415  -0.0029   0.5736   0.9700
   8.000   0.4967   0.06089   0.05389  -0.0056   0.5694   0.9752
   8.250   0.5043   0.06286   0.05595  -0.0065   0.5574   0.9812
   8.500   0.5585   0.06189   0.05510  -0.0094   0.5530   0.9898
   8.750   0.5631   0.06362   0.05691  -0.0095   0.5401   1.0000
   9.000   0.6206   0.06189   0.05530  -0.0117   0.5361   1.0000
   9.250   0.6300   0.06340   0.05690  -0.0121   0.5226   1.0000
   9.500   0.6761   0.06200   0.05563  -0.0135   0.5153   1.0000
   9.750   0.7164   0.06063   0.05438  -0.0145   0.5053   1.0000
  10.000   0.7927   0.05574   0.04968  -0.0163   0.5029   1.0000
  10.250   0.8108   0.05620   0.05027  -0.0166   0.4891   1.0000
  10.500   0.8830   0.05115   0.04543  -0.0180   0.4874   1.0000
  10.750   1.0166   0.03858   0.03309  -0.0205   0.4855   1.0000
  11.000   1.0143   0.04040   0.03502  -0.0195   0.4634   1.0000
  11.250   1.0565   0.03800   0.03268  -0.0199   0.4388   1.0000
  11.500   1.0716   0.03856   0.03328  -0.0197   0.4091   1.0000
  11.750   1.0860   0.03918   0.03378  -0.0192   0.3678   1.0000
  12.000   1.0838   0.04140   0.03572  -0.0181   0.3103   1.0000
  12.250   1.0713   0.04472   0.03850  -0.0168   0.2454   1.0000
  12.500   1.0557   0.04878   0.04207  -0.0158   0.1969   1.0000
  12.750   1.0463   0.05256   0.04549  -0.0154   0.1621   1.0000
  13.000   1.0427   0.05591   0.04852  -0.0151   0.1366   1.0000
  13.250   1.0472   0.05857   0.05100  -0.0149   0.1163   1.0000
  13.500   1.0609   0.06028   0.05255  -0.0147   0.1031   1.0000
  13.750   1.0853   0.06104   0.05309  -0.0145   0.0936   1.0000
  14.000   1.1084   0.06222   0.05426  -0.0147   0.0865   1.0000
  14.250   1.1448   0.06260   0.05455  -0.0149   0.0807   1.0000
  14.500   1.1737   0.06384   0.05594  -0.0153   0.0770   1.0000
  14.750   1.2091   0.06491   0.05697  -0.0160   0.0735   1.0000
  15.000   1.2504   0.06658   0.05868  -0.0170   0.0701   1.0000
  15.250   1.2597   0.06933   0.06175  -0.0173   0.0685   1.0000
  15.500   1.2709   0.07228   0.06497  -0.0177   0.0671   1.0000
  15.750   1.2797   0.07551   0.06848  -0.0180   0.0661   1.0000
  16.000   1.2835   0.07911   0.07235  -0.0184   0.0653   1.0000
  16.250   1.2832   0.08298   0.07648  -0.0188   0.0647   1.0000
  16.500   1.2798   0.08708   0.08083  -0.0194   0.0641   1.0000
  16.750   1.2755   0.09129   0.08526  -0.0202   0.0634   1.0000
  17.000   1.2730   0.09547   0.08962  -0.0212   0.0627   1.0000
  17.250   1.2597   0.10063   0.09503  -0.0225   0.0624   1.0000
  17.500   1.2101   0.10964   0.10454  -0.0257   0.0635   1.0000
  17.750   1.1548   0.12110   0.11646  -0.0311   0.0652   1.0000
  18.000   1.0998   0.13449   0.13020  -0.0387   0.0671   1.0000
  18.250   1.0492   0.14927   0.14517  -0.0480   0.0692   1.0000
  18.500   1.0215   0.16126   0.15724  -0.0553   0.0706   1.0000
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