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WORTMANN FX 05-188 AIRFOIL (fx05188-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 05-188 AIRFOIL (fx05188-il)
Reynolds number: 50,000
Max Cl/Cd: 14.17 at α=13°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx05188-il-50000-n5.txt
Download as CSV file: xf-fx05188-il-50000-n5.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 =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.4142   0.11483   0.10775  -0.0701   1.0000   0.0571
 -12.750  -0.4367   0.11114   0.10416  -0.0691   1.0000   0.0567
 -12.500  -0.4645   0.10694   0.10002  -0.0684   1.0000   0.0561
 -12.250  -0.4874   0.09710   0.09009  -0.0756   0.9937   0.0552
 -12.000  -0.5167   0.08809   0.08090  -0.0824   0.9863   0.0545
 -11.750  -0.5420   0.08121   0.07380  -0.0872   0.9783   0.0539
 -11.500  -0.5624   0.07566   0.06798  -0.0906   0.9711   0.0537
 -11.250  -0.5785   0.07138   0.06345  -0.0925   0.9631   0.0537
 -11.000  -0.5907   0.06769   0.05947  -0.0936   0.9557   0.0538
 -10.750  -0.5984   0.06458   0.05609  -0.0942   0.9484   0.0542
 -10.500  -0.6053   0.06198   0.05321  -0.0937   0.9411   0.0545
 -10.250  -0.6098   0.05969   0.05063  -0.0927   0.9340   0.0551
 -10.000  -0.6038   0.05713   0.04772  -0.0928   0.9291   0.0556
  -9.750  -0.6045   0.05538   0.04572  -0.0905   0.9216   0.0560
  -9.500  -0.5889   0.05306   0.04306  -0.0905   0.9171   0.0566
  -9.250  -0.5622   0.05077   0.04038  -0.0917   0.9142   0.0574
  -9.000  -0.5477   0.04942   0.03875  -0.0901   0.9090   0.0581
  -8.750  -0.5123   0.04789   0.03709  -0.0909   0.9060   0.0594
  -8.500  -0.4677   0.04658   0.03577  -0.0930   0.9041   0.0627
  -8.250  -0.4162   0.04560   0.03456  -0.0953   0.9027   0.0669
  -8.000  -0.3669   0.04488   0.03379  -0.0970   0.9012   0.0709
  -7.750  -0.3336   0.04411   0.03297  -0.0978   0.8986   0.0748
  -7.500  -0.3130   0.04346   0.03220  -0.0972   0.8946   0.0794
  -7.250  -0.3147   0.04309   0.03186  -0.0935   0.8874   0.0828
  -7.000  -0.3023   0.04222   0.03099  -0.0926   0.8827   0.0892
  -6.750  -0.2890   0.04106   0.02987  -0.0921   0.8791   0.0993
  -6.500  -0.3104   0.04110   0.02993  -0.0852   0.8699   0.1026
  -6.250  -0.3097   0.04013   0.02904  -0.0826   0.8647   0.1144
  -6.000  -0.3227   0.03953   0.02853  -0.0776   0.8581   0.1271
  -5.750  -0.3380   0.03882   0.02798  -0.0724   0.8506   0.1466
  -5.500  -0.3461   0.03683   0.02665  -0.0697   0.8457   0.2233
  -5.250  -0.3691   0.03619   0.02655  -0.0630   0.8377   0.2885
  -5.000  -0.3530   0.03771   0.02920  -0.0573   0.8334   0.4855
  -4.750  -0.3314   0.03990   0.03137  -0.0536   0.8295   0.5703
  -4.500  -0.2792   0.04576   0.03704  -0.0489   0.8277   0.6339
  -4.250  -0.2905   0.04673   0.03797  -0.0421   0.8197   0.6481
  -4.000  -0.2684   0.04735   0.03839  -0.0404   0.8154   0.6616
  -3.750  -0.2467   0.04717   0.03797  -0.0400   0.8120   0.6723
  -3.500  -0.2613   0.04703   0.03777  -0.0346   0.8047   0.6837
  -3.250  -0.2426   0.04722   0.03780  -0.0331   0.7999   0.6897
  -3.000  -0.2269   0.04676   0.03714  -0.0325   0.7960   0.7002
  -2.750  -0.2112   0.04691   0.03716  -0.0307   0.7914   0.7058
  -2.500  -0.2131   0.04689   0.03705  -0.0270   0.7849   0.7145
  -2.250  -0.1930   0.04672   0.03672  -0.0265   0.7809   0.7214
  -2.000  -0.1633   0.04663   0.03645  -0.0271   0.7782   0.7277
  -1.750  -0.1772   0.04664   0.03643  -0.0220   0.7701   0.7367
  -1.500  -0.1564   0.04671   0.03638  -0.0212   0.7661   0.7423
  -1.250  -0.1340   0.04642   0.03592  -0.0216   0.7628   0.7509
  -1.000  -0.1328   0.04671   0.03618  -0.0180   0.7560   0.7566
  -0.750  -0.1180   0.04673   0.03610  -0.0168   0.7513   0.7639
  -0.500  -0.0942   0.04664   0.03588  -0.0169   0.7479   0.7707
  -0.250  -0.0842   0.04684   0.03602  -0.0149   0.7425   0.7769
   0.000  -0.0750   0.04688   0.03598  -0.0135   0.7365   0.7848
   0.250  -0.0509   0.04692   0.03594  -0.0132   0.7328   0.7895
   0.500  -0.0218   0.04687   0.03578  -0.0140   0.7300   0.7954
   0.750  -0.0254   0.04722   0.03612  -0.0109   0.7217   0.8020
   1.000  -0.0033   0.04730   0.03613  -0.0106   0.7173   0.8068
   1.250   0.0258   0.04728   0.03602  -0.0116   0.7142   0.8123
   1.750   0.0484   0.04786   0.03654  -0.0088   0.7014   0.8228
   2.000   0.0771   0.04790   0.03652  -0.0097   0.6979   0.8280
   2.500   0.1023   0.04860   0.03719  -0.0074   0.6849   0.8380
   2.750   0.1307   0.04872   0.03728  -0.0082   0.6812   0.8429
   3.250   0.1581   0.04961   0.03817  -0.0065   0.6684   0.8524
   3.500   0.1864   0.04977   0.03831  -0.0072   0.6645   0.8571
   4.000   0.2155   0.05084   0.03942  -0.0060   0.6516   0.8664
   4.250   0.2443   0.05101   0.03960  -0.0067   0.6479   0.8709
   4.500   0.2524   0.05189   0.04052  -0.0058   0.6397   0.8759
   4.750   0.2750   0.05226   0.04092  -0.0060   0.6346   0.8802
   5.000   0.3050   0.05239   0.04108  -0.0066   0.6313   0.8846
   5.250   0.3083   0.05352   0.04228  -0.0054   0.6218   0.8895
   5.500   0.3365   0.05382   0.04263  -0.0063   0.6176   0.8939
   5.750   0.3463   0.05473   0.04359  -0.0053   0.6099   0.8986
   6.000   0.3677   0.05528   0.04421  -0.0056   0.6040   0.9032
   6.250   0.3999   0.05549   0.04449  -0.0068   0.6006   0.9078
   6.500   0.4021   0.05681   0.04591  -0.0055   0.5906   0.9126
   6.750   0.4303   0.05712   0.04630  -0.0063   0.5862   0.9173
   7.000   0.4404   0.05836   0.04763  -0.0060   0.5776   0.9224
   7.250   0.4634   0.05887   0.04825  -0.0063   0.5717   0.9275
   7.500   0.4976   0.05890   0.04839  -0.0075   0.5682   0.9326
   7.750   0.4992   0.06069   0.05029  -0.0069   0.5569   0.9379
   8.000   0.5328   0.06074   0.05049  -0.0080   0.5526   0.9434
   8.250   0.5380   0.06250   0.05237  -0.0078   0.5417   0.9496
   8.500   0.5714   0.06265   0.05268  -0.0092   0.5367   0.9559
   8.750   0.5807   0.06437   0.05455  -0.0096   0.5258   0.9635
   9.000   0.6153   0.06444   0.05479  -0.0112   0.5202   0.9736
   9.500   0.6600   0.06576   0.05643  -0.0129   0.5031   1.0000
   9.750   0.6688   0.06756   0.05836  -0.0133   0.4904   1.0000
  10.000   0.7105   0.06677   0.05775  -0.0146   0.4852   1.0000
  10.250   0.7208   0.06843   0.05956  -0.0151   0.4719   1.0000
  10.750   0.7591   0.07003   0.06151  -0.0161   0.4475   1.0000
  11.000   0.8063   0.06725   0.05894  -0.0162   0.4374   1.0000
  11.500   0.8548   0.06594   0.05800  -0.0159   0.4056   1.0000
  11.750   0.8749   0.06615   0.05840  -0.0159   0.3897   1.0000
  12.000   0.8969   0.06616   0.05862  -0.0160   0.3729   1.0000
  12.250   0.9112   0.06712   0.05974  -0.0161   0.3521   1.0000
  12.500   0.9266   0.06791   0.06067  -0.0161   0.3267   1.0000
  12.750   0.9497   0.06741   0.06013  -0.0156   0.2901   1.0000
  13.000   0.9637   0.06803   0.06039  -0.0151   0.2420   1.0000
  13.250   0.9658   0.07057   0.06256  -0.0151   0.2019   1.0000
  13.500   0.9656   0.07374   0.06545  -0.0155   0.1735   1.0000
  13.750   0.9658   0.07707   0.06857  -0.0161   0.1528   1.0000
  14.000   0.9668   0.08041   0.07178  -0.0168   0.1364   1.0000
  14.250   0.9700   0.08359   0.07489  -0.0175   0.1229   1.0000
  14.500   0.9750   0.08662   0.07790  -0.0183   0.1114   1.0000
  14.750   0.9813   0.08948   0.08074  -0.0190   0.1019   1.0000
  15.000   0.9892   0.09205   0.08320  -0.0197   0.0947   1.0000
  15.250   1.0011   0.09428   0.08556  -0.0201   0.0882   1.0000
  15.500   1.0146   0.09604   0.08718  -0.0204   0.0830   1.0000
  15.750   1.0267   0.09845   0.08987  -0.0210   0.0781   1.0000
  16.000   1.0399   0.10053   0.09203  -0.0216   0.0740   1.0000
  16.250   1.0604   0.10158   0.09303  -0.0215   0.0707   1.0000
  16.500   1.0708   0.10448   0.09628  -0.0223   0.0684   1.0000
  16.750   1.0783   0.10773   0.09979  -0.0234   0.0662   1.0000
  17.000   1.0840   0.11116   0.10342  -0.0247   0.0642   1.0000
  17.250   1.0910   0.11426   0.10666  -0.0260   0.0623   1.0000
  17.500   1.1030   0.11665   0.10905  -0.0269   0.0604   1.0000
  17.750   1.0901   0.12310   0.11586  -0.0302   0.0597   1.0000
  18.000   1.0737   0.13043   0.12350  -0.0342   0.0592   1.0000
  18.250   1.0523   0.13907   0.13244  -0.0393   0.0590   1.0000
  18.500   1.0235   0.14999   0.14361  -0.0462   0.0590   1.0000
  18.750   0.9856   0.16451   0.15834  -0.0555   0.0593   1.0000
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