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FX 66-S-196 V1 AIRFOIL (fx66196v-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: FX 66-S-196 V1 AIRFOIL (fx66196v-il)
Reynolds number: 200,000
Max Cl/Cd: 61.59 at α=9.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx66196v-il-200000-n5.txt
Download as CSV file: xf-fx66196v-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 66-S-196 V1 AIRFOIL                          
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.4467   0.07790   0.07374  -0.0974   0.9010   0.0150
 -14.250  -0.4702   0.06808   0.06351  -0.1064   0.8824   0.0149
 -14.000  -0.4791   0.06218   0.05732  -0.1117   0.8622   0.0150
 -13.750  -0.4866   0.05755   0.05242  -0.1153   0.8443   0.0150
 -13.500  -0.4888   0.05410   0.04878  -0.1177   0.8274   0.0153
 -13.250  -0.4961   0.05040   0.04480  -0.1194   0.8129   0.0152
 -13.000  -0.4993   0.04762   0.04181  -0.1201   0.7989   0.0154
 -12.750  -0.4998   0.04535   0.03936  -0.1205   0.7855   0.0156
 -12.500  -0.5006   0.04301   0.03683  -0.1206   0.7730   0.0158
 -12.250  -0.4989   0.04103   0.03465  -0.1205   0.7613   0.0161
 -12.000  -0.4960   0.03923   0.03265  -0.1202   0.7507   0.0165
 -11.750  -0.4925   0.03751   0.03073  -0.1197   0.7402   0.0170
 -11.500  -0.4870   0.03584   0.02884  -0.1191   0.7305   0.0174
 -11.250  -0.4804   0.03434   0.02709  -0.1182   0.7216   0.0181
 -11.000  -0.4708   0.03290   0.02543  -0.1174   0.7130   0.0185
 -10.750  -0.4594   0.03156   0.02394  -0.1165   0.7055   0.0189
 -10.500  -0.4470   0.03041   0.02271  -0.1156   0.6973   0.0193
 -10.000  -0.4220   0.02836   0.02048  -0.1138   0.6837   0.0204
  -9.750  -0.4091   0.02741   0.01941  -0.1128   0.6773   0.0211
  -9.500  -0.3961   0.02647   0.01837  -0.1117   0.6714   0.0217
  -9.250  -0.3835   0.02558   0.01736  -0.1105   0.6653   0.0227
  -9.000  -0.3720   0.02476   0.01641  -0.1090   0.6601   0.0235
  -8.750  -0.3651   0.02393   0.01557  -0.1072   0.6547   0.0245
  -8.500  -0.3536   0.02327   0.01485  -0.1058   0.6495   0.0258
  -8.250  -0.3398   0.02260   0.01407  -0.1045   0.6448   0.0270
  -8.000  -0.3250   0.02192   0.01329  -0.1033   0.6400   0.0284
  -7.750  -0.3107   0.02118   0.01248  -0.1021   0.6352   0.0297
  -7.500  -0.2944   0.02054   0.01179  -0.1012   0.6310   0.0319
  -7.250  -0.2758   0.02002   0.01115  -0.1004   0.6272   0.0346
  -7.000  -0.2574   0.01939   0.01048  -0.0997   0.6229   0.0377
  -6.750  -0.2374   0.01884   0.00988  -0.0991   0.6189   0.0416
  -6.500  -0.2166   0.01831   0.00929  -0.0986   0.6154   0.0472
  -6.000  -0.1727   0.01732   0.00824  -0.0980   0.6089   0.0680
  -5.750  -0.1506   0.01675   0.00775  -0.0978   0.6055   0.0915
  -5.500  -0.1291   0.01607   0.00724  -0.0976   0.6024   0.1362
  -5.250  -0.1086   0.01517   0.00667  -0.0975   0.5996   0.2160
  -5.000  -0.0890   0.01412   0.00614  -0.0974   0.5972   0.3434
  -4.750  -0.0640   0.01402   0.00635  -0.0972   0.5944   0.4430
  -4.500  -0.0364   0.01413   0.00640  -0.0973   0.5915   0.4712
  -4.250  -0.0084   0.01426   0.00639  -0.0974   0.5888   0.4911
  -4.000   0.0194   0.01441   0.00643  -0.0975   0.5863   0.5068
  -3.750   0.0471   0.01461   0.00656  -0.0974   0.5841   0.5211
  -3.500   0.0749   0.01485   0.00675  -0.0973   0.5822   0.5341
  -3.250   0.1026   0.01500   0.00683  -0.0974   0.5801   0.5430
  -3.000   0.1305   0.01507   0.00684  -0.0975   0.5777   0.5490
  -2.750   0.1587   0.01508   0.00672  -0.0979   0.5755   0.5539
  -2.500   0.1866   0.01508   0.00667  -0.0981   0.5733   0.5564
  -2.250   0.2147   0.01509   0.00661  -0.0983   0.5711   0.5587
  -2.000   0.2430   0.01509   0.00652  -0.0986   0.5692   0.5610
  -1.750   0.2715   0.01510   0.00643  -0.0990   0.5675   0.5631
  -1.500   0.3002   0.01514   0.00635  -0.0995   0.5659   0.5658
  -1.250   0.3281   0.01517   0.00633  -0.0998   0.5641   0.5687
  -1.000   0.3559   0.01520   0.00633  -0.1001   0.5622   0.5708
  -0.750   0.3837   0.01523   0.00636  -0.1003   0.5604   0.5724
  -0.500   0.4115   0.01528   0.00639  -0.1006   0.5587   0.5744
  -0.250   0.4395   0.01534   0.00642  -0.1009   0.5571   0.5766
   0.000   0.4675   0.01540   0.00645  -0.1012   0.5556   0.5788
   0.250   0.4957   0.01546   0.00647  -0.1016   0.5542   0.5810
   0.500   0.5240   0.01554   0.00650  -0.1020   0.5529   0.5833
   0.750   0.5525   0.01563   0.00653  -0.1024   0.5518   0.5857
   1.000   0.5809   0.01573   0.00661  -0.1028   0.5507   0.5875
   1.250   0.6081   0.01584   0.00676  -0.1030   0.5494   0.5896
   1.500   0.6349   0.01596   0.00694  -0.1032   0.5480   0.5919
   1.750   0.6617   0.01609   0.00711  -0.1033   0.5466   0.5945
   2.000   0.6886   0.01624   0.00728  -0.1035   0.5451   0.5976
   2.250   0.7157   0.01638   0.00744  -0.1037   0.5436   0.6009
   2.500   0.7425   0.01651   0.00761  -0.1039   0.5421   0.6036
   2.750   0.7695   0.01664   0.00780  -0.1040   0.5408   0.6063
   3.000   0.7967   0.01680   0.00799  -0.1043   0.5396   0.6094
   3.250   0.8240   0.01696   0.00818  -0.1045   0.5386   0.6129
   3.500   0.8516   0.01713   0.00837  -0.1049   0.5376   0.6166
   3.750   0.8791   0.01730   0.00859  -0.1051   0.5367   0.6199
   4.000   0.9068   0.01747   0.00881  -0.1055   0.5357   0.6235
   4.250   0.9329   0.01769   0.00910  -0.1055   0.5345   0.6276
   4.500   0.9566   0.01796   0.00948  -0.1052   0.5329   0.6322
   4.750   0.9805   0.01822   0.00986  -0.1050   0.5314   0.6363
   5.000   1.0044   0.01847   0.01023  -0.1047   0.5297   0.6409
   5.250   1.0289   0.01874   0.01061  -0.1045   0.5283   0.6463
   5.500   1.0535   0.01901   0.01099  -0.1044   0.5271   0.6516
   5.750   1.0781   0.01927   0.01135  -0.1042   0.5258   0.6573
   6.000   1.1035   0.01950   0.01168  -0.1042   0.5244   0.6643
   6.250   1.1292   0.01972   0.01201  -0.1042   0.5232   0.6711
   6.500   1.1551   0.01997   0.01235  -0.1043   0.5221   0.6793
   6.750   1.1814   0.02022   0.01272  -0.1044   0.5212   0.6873
   7.000   1.2087   0.02048   0.01306  -0.1047   0.5202   0.6967
   7.250   1.2242   0.02095   0.01375  -0.1031   0.5180   0.7058
   7.500   1.2391   0.02143   0.01442  -0.1015   0.5153   0.7165
   7.750   1.2572   0.02180   0.01498  -0.1003   0.5128   0.7287
   8.000   1.2775   0.02211   0.01545  -0.0994   0.5107   0.7421
   8.250   1.3001   0.02236   0.01585  -0.0989   0.5089   0.7575
   8.500   1.3266   0.02247   0.01609  -0.0990   0.5071   0.7760
   8.750   1.3580   0.02239   0.01614  -0.0997   0.5052   0.7981
   9.000   1.3601   0.02305   0.01707  -0.0959   0.5015   0.8277
   9.250   1.3633   0.02350   0.01779  -0.0923   0.4972   0.8764
   9.500   1.3975   0.02269   0.01707  -0.0931   0.4914   1.0000
   9.750   1.3891   0.02308   0.01755  -0.0876   0.4833   1.0000
  10.000   1.3936   0.02280   0.01726  -0.0840   0.4714   1.0000
  10.250   1.3893   0.02326   0.01775  -0.0799   0.4583   1.0000
  10.500   1.3828   0.02435   0.01888  -0.0763   0.4449   1.0000
  10.750   1.3634   0.02691   0.02159  -0.0725   0.4336   1.0000
  11.000   1.3433   0.03009   0.02490  -0.0694   0.4217   1.0000
  11.250   1.3149   0.03452   0.02946  -0.0666   0.4090   1.0000
  11.500   1.3391   0.03394   0.02863  -0.0660   0.3715   1.0000
  11.750   1.3302   0.03636   0.03077  -0.0638   0.3338   1.0000
  12.000   1.3110   0.03997   0.03417  -0.0615   0.3041   1.0000
  12.250   1.2932   0.04379   0.03784  -0.0596   0.2760   1.0000
  12.500   1.2749   0.04787   0.04176  -0.0581   0.2505   1.0000
  12.750   1.2580   0.05201   0.04576  -0.0568   0.2231   1.0000
  13.000   1.2433   0.05611   0.04971  -0.0559   0.1984   1.0000
  13.250   1.2300   0.06019   0.05365  -0.0551   0.1710   1.0000
  13.500   1.2174   0.06430   0.05759  -0.0545   0.1442   1.0000
  13.750   1.2090   0.06805   0.06121  -0.0541   0.1196   1.0000
  14.000   1.2008   0.07188   0.06490  -0.0538   0.0954   1.0000
  14.250   1.1950   0.07548   0.06836  -0.0537   0.0746   1.0000
  14.500   1.1911   0.07893   0.07171  -0.0536   0.0572   1.0000
  14.750   1.1892   0.08223   0.07493  -0.0536   0.0451   1.0000
  15.250   1.1907   0.08833   0.08102  -0.0538   0.0310   1.0000
  15.500   1.1923   0.09135   0.08408  -0.0540   0.0272   1.0000
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