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FX 75-VG-166/22 (fx75vg166-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: FX 75-VG-166/22 (fx75vg166-il)
Reynolds number: 200,000
Max Cl/Cd: 44.99 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx75vg166-il-200000-n5.txt
Download as CSV file: xf-fx75vg166-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 75-VG-166/22                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.4164   0.07837   0.07332  -0.1033   0.7682   0.0156
 -13.250  -0.4508   0.06868   0.06346  -0.1097   0.7679   0.0155
 -13.000  -0.4705   0.06329   0.05794  -0.1124   0.7673   0.0154
 -12.750  -0.4986   0.05778   0.05220  -0.1138   0.7667   0.0154
 -12.500  -0.5203   0.05362   0.04783  -0.1136   0.7659   0.0154
 -12.250  -0.5389   0.05003   0.04404  -0.1124   0.7650   0.0154
 -12.000  -0.5502   0.04727   0.04108  -0.1107   0.7641   0.0153
 -11.750  -0.5703   0.04371   0.03717  -0.1077   0.7629   0.0155
 -11.500  -0.5774   0.04131   0.03451  -0.1052   0.7617   0.0156
 -11.250  -0.5808   0.03911   0.03201  -0.1027   0.7605   0.0157
 -11.000  -0.5786   0.03727   0.03002  -0.1005   0.7596   0.0160
 -10.750  -0.5715   0.03622   0.02891  -0.0988   0.7586   0.0165
 -10.500  -0.5633   0.03445   0.02691  -0.0969   0.7575   0.0165
 -10.250  -0.5542   0.03368   0.02606  -0.0951   0.7565   0.0172
 -10.000  -0.5440   0.03279   0.02503  -0.0932   0.7554   0.0180
  -9.750  -0.5300   0.03146   0.02346  -0.0917   0.7545   0.0186
  -9.500  -0.5126   0.03006   0.02175  -0.0905   0.7537   0.0194
  -9.250  -0.4923   0.02890   0.02048  -0.0899   0.7531   0.0201
  -9.000  -0.4730   0.02802   0.01957  -0.0891   0.7521   0.0207
  -8.750  -0.4532   0.02723   0.01872  -0.0884   0.7511   0.0215
  -8.500  -0.4319   0.02643   0.01785  -0.0877   0.7500   0.0222
  -8.250  -0.4106   0.02570   0.01701  -0.0870   0.7489   0.0234
  -8.000  -0.3909   0.02506   0.01632  -0.0861   0.7478   0.0249
  -7.750  -0.3724   0.02454   0.01581  -0.0851   0.7467   0.0262
  -7.500  -0.3531   0.02397   0.01520  -0.0840   0.7456   0.0276
  -7.250  -0.3343   0.02344   0.01460  -0.0828   0.7445   0.0290
  -7.000  -0.3174   0.02290   0.01403  -0.0814   0.7433   0.0302
  -6.750  -0.3007   0.02249   0.01362  -0.0800   0.7422   0.0324
  -6.500  -0.2839   0.02210   0.01318  -0.0784   0.7411   0.0346
  -6.250  -0.2688   0.02168   0.01271  -0.0765   0.7401   0.0366
  -6.000  -0.2545   0.02131   0.01233  -0.0746   0.7392   0.0391
  -5.750  -0.2396   0.02107   0.01206  -0.0727   0.7380   0.0429
  -5.500  -0.2260   0.02078   0.01182  -0.0706   0.7363   0.0470
  -5.250  -0.2097   0.02056   0.01160  -0.0690   0.7346   0.0526
  -5.000  -0.1938   0.02029   0.01138  -0.0673   0.7330   0.0630
  -4.750  -0.1778   0.02000   0.01117  -0.0656   0.7315   0.0791
  -4.500  -0.1627   0.01962   0.01095  -0.0639   0.7300   0.1113
  -4.250  -0.1494   0.01911   0.01071  -0.0618   0.7285   0.1713
  -4.000  -0.1396   0.01843   0.01045  -0.0593   0.7272   0.2625
  -3.750  -0.1342   0.01756   0.01016  -0.0561   0.7260   0.3920
  -3.500  -0.1294   0.01670   0.01012  -0.0521   0.7249   0.5566
  -3.250  -0.0897   0.01894   0.01299  -0.0497   0.7242   0.6869
  -3.000  -0.0765   0.01926   0.01329  -0.0476   0.7204   0.7164
  -2.750  -0.0533   0.01990   0.01387  -0.0465   0.7182   0.7376
  -2.500  -0.0296   0.02068   0.01458  -0.0453   0.7164   0.7582
  -2.250  -0.0100   0.02123   0.01505  -0.0437   0.7149   0.7768
  -2.000   0.0203   0.02189   0.01565  -0.0431   0.7139   0.7821
  -1.750   0.0410   0.02199   0.01567  -0.0421   0.7127   0.7909
  -1.500   0.0691   0.02218   0.01580  -0.0419   0.7118   0.7933
  -1.250   0.0966   0.02230   0.01585  -0.0416   0.7110   0.7965
  -1.000   0.1066   0.02263   0.01620  -0.0393   0.7062   0.8032
  -0.750   0.1260   0.02274   0.01627  -0.0382   0.7037   0.8066
  -0.500   0.1498   0.02285   0.01636  -0.0376   0.7020   0.8086
  -0.250   0.1742   0.02290   0.01637  -0.0371   0.7005   0.8114
   0.000   0.1987   0.02284   0.01627  -0.0367   0.6992   0.8145
   0.250   0.2233   0.02268   0.01604  -0.0366   0.6980   0.8184
   0.500   0.2498   0.02251   0.01582  -0.0366   0.6970   0.8208
   0.750   0.2556   0.02304   0.01643  -0.0335   0.6896   0.8228
   1.000   0.2788   0.02305   0.01643  -0.0330   0.6876   0.8246
   1.250   0.3034   0.02301   0.01638  -0.0327   0.6861   0.8265
   1.500   0.3296   0.02290   0.01625  -0.0326   0.6849   0.8287
   1.750   0.3569   0.02275   0.01607  -0.0328   0.6838   0.8309
   2.250   0.3830   0.02331   0.01671  -0.0292   0.6736   0.8362
   2.500   0.4109   0.02307   0.01647  -0.0293   0.6718   0.8370
   2.750   0.4399   0.02282   0.01622  -0.0296   0.6705   0.8379
   3.000   0.4687   0.02261   0.01603  -0.0299   0.6695   0.8388
   3.500   0.4914   0.02331   0.01682  -0.0259   0.6578   0.8422
   3.750   0.5219   0.02298   0.01651  -0.0264   0.6562   0.8431
   4.000   0.5541   0.02256   0.01612  -0.0271   0.6550   0.8442
   4.250   0.5864   0.02214   0.01573  -0.0279   0.6540   0.8454
   4.750   0.6119   0.02267   0.01635  -0.0244   0.6409   0.8486
   5.000   0.6441   0.02220   0.01594  -0.0251   0.6397   0.8493
   5.500   0.6629   0.02230   0.01616  -0.0194   0.6260   0.8522
   6.000   0.6980   0.02188   0.01585  -0.0163   0.6110   0.8548
   6.250   0.7022   0.02243   0.01644  -0.0134   0.5986   0.8561
   6.500   0.7452   0.02121   0.01526  -0.0150   0.5938   0.8564
   6.750   0.7462   0.02211   0.01621  -0.0119   0.5799   0.8577
   7.000   0.7588   0.02251   0.01666  -0.0103   0.5677   0.8587
   7.250   0.7854   0.02219   0.01639  -0.0101   0.5573   0.8594
   7.500   0.8230   0.02130   0.01552  -0.0110   0.5452   0.8598
   7.750   0.8574   0.02057   0.01479  -0.0114   0.5273   0.8602
   8.000   0.8877   0.01999   0.01411  -0.0113   0.4979   0.8608
   8.250   0.9033   0.02008   0.01392  -0.0093   0.4533   0.8620
   8.500   0.9053   0.02094   0.01455  -0.0061   0.4139   0.8631
   8.750   0.9048   0.02204   0.01545  -0.0030   0.3781   0.8640
   9.250   0.8929   0.02489   0.01781   0.0040   0.2982   0.8655
   9.500   0.8891   0.02636   0.01907   0.0070   0.2594   0.8662
   9.750   0.8890   0.02775   0.02028   0.0094   0.2271   0.8668
  10.000   0.8904   0.02915   0.02152   0.0115   0.1978   0.8673
  10.250   0.8974   0.03033   0.02262   0.0129   0.1757   0.8678
  10.500   0.9037   0.03162   0.02382   0.0142   0.1551   0.8683
  10.750   0.9125   0.03282   0.02496   0.0153   0.1374   0.8687
  11.000   0.9219   0.03406   0.02614   0.0162   0.1192   0.8690
  11.250   0.9319   0.03531   0.02736   0.0169   0.1050   0.8694
  11.500   0.9415   0.03661   0.02862   0.0177   0.0892   0.8698
  11.750   0.9490   0.03810   0.03001   0.0185   0.0717   0.8701
  12.000   0.9576   0.03957   0.03144   0.0193   0.0595   0.8704
  12.250   0.9663   0.04108   0.03292   0.0199   0.0497   0.8708
  12.500   0.9748   0.04264   0.03447   0.0205   0.0429   0.8713
  12.750   0.9834   0.04424   0.03609   0.0210   0.0378   0.8717
  13.000   0.9924   0.04583   0.03773   0.0214   0.0348   0.8723
  13.250   1.0001   0.04756   0.03952   0.0218   0.0321   0.8727
  13.500   1.0084   0.04929   0.04135   0.0222   0.0304   0.8730
  13.750   1.0152   0.05120   0.04329   0.0224   0.0278   0.8732
  14.000   1.0218   0.05319   0.04535   0.0226   0.0267   0.8735
  14.250   1.0289   0.05517   0.04745   0.0228   0.0257   0.8740
  14.500   1.0351   0.05730   0.04967   0.0228   0.0246   0.8745
  14.750   1.0409   0.05950   0.05196   0.0228   0.0234   0.8753
  15.000   1.0453   0.06188   0.05441   0.0227   0.0228   0.8757
  15.250   1.0479   0.06452   0.05710   0.0226   0.0221   0.8760
  15.500   1.0536   0.06687   0.05958   0.0223   0.0214   0.8761
  15.750   1.0590   0.06932   0.06215   0.0220   0.0209   0.8762
  16.000   1.0639   0.07186   0.06480   0.0216   0.0201   0.8763
  16.250   1.0688   0.07445   0.06749   0.0210   0.0195   0.8764
  16.500   1.0714   0.07739   0.07050   0.0202   0.0185   0.8765
  16.750   1.0744   0.08027   0.07346   0.0196   0.0182   0.8766
  17.000   1.0773   0.08314   0.07639   0.0189   0.0179   0.8767
  17.250   1.0806   0.08611   0.07950   0.0182   0.0174   0.8768
  17.500   1.0844   0.08900   0.08251   0.0174   0.0173   0.8769
  17.750   1.0864   0.09223   0.08592   0.0163   0.0169   0.8771
  18.000   1.0876   0.09562   0.08945   0.0152   0.0165   0.8772
  18.250   1.0887   0.09907   0.09305   0.0139   0.0163   0.8773
  18.500   1.0885   0.10279   0.09692   0.0125   0.0159   0.8774
  18.750   1.0882   0.10655   0.10083   0.0109   0.0158   0.8775
  19.000   1.0855   0.11077   0.10520   0.0090   0.0155   0.8776
  19.250   1.0825   0.11510   0.10967   0.0069   0.0153   0.8777
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