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FX 66-S-196 V1 AIRFOIL (fx66196v-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: FX 66-S-196 V1 AIRFOIL (fx66196v-il)
Reynolds number: 500,000
Max Cl/Cd: 110.08 at α=9.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx66196v-il-500000.txt
Download as CSV file: xf-fx66196v-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.4647   0.08409   0.08159  -0.0858   0.9469   0.0153
 -14.500  -0.3926   0.08427   0.08178  -0.0953   0.9217   0.0159
 -14.250  -0.4857   0.06180   0.05859  -0.1126   0.9137   0.0145
 -14.000  -0.4939   0.05453   0.05089  -0.1218   0.8837   0.0146
 -13.750  -0.5036   0.05027   0.04629  -0.1248   0.8560   0.0146
 -13.500  -0.5192   0.04636   0.04206  -0.1260   0.8340   0.0147
 -13.250  -0.5245   0.04418   0.03965  -0.1264   0.8155   0.0148
 -13.000  -0.5334   0.04109   0.03632  -0.1262   0.8001   0.0147
 -12.750  -0.5478   0.03751   0.03244  -0.1257   0.7860   0.0150
 -12.500  -0.5481   0.03521   0.02995  -0.1249   0.7726   0.0152
 -12.250  -0.5437   0.03348   0.02808  -0.1241   0.7605   0.0154
 -12.000  -0.5378   0.03211   0.02659  -0.1234   0.7485   0.0157
 -11.500  -0.5236   0.02947   0.02367  -0.1216   0.7272   0.0162
 -11.250  -0.5142   0.02833   0.02239  -0.1206   0.7178   0.0166
 -11.000  -0.5033   0.02708   0.02099  -0.1194   0.7085   0.0168
 -10.750  -0.4919   0.02602   0.01980  -0.1184   0.7003   0.0173
 -10.500  -0.4787   0.02496   0.01859  -0.1172   0.6923   0.0175
 -10.250  -0.4658   0.02403   0.01753  -0.1160   0.6849   0.0180
 -10.000  -0.4526   0.02317   0.01654  -0.1148   0.6775   0.0183
  -9.750  -0.4405   0.02248   0.01572  -0.1134   0.6709   0.0187
  -9.500  -0.4279   0.02110   0.01428  -0.1117   0.6645   0.0193
  -9.250  -0.4205   0.02031   0.01343  -0.1095   0.6587   0.0198
  -9.000  -0.4084   0.01973   0.01283  -0.1079   0.6527   0.0205
  -8.750  -0.3927   0.01921   0.01224  -0.1068   0.6472   0.0214
  -8.500  -0.3755   0.01872   0.01165  -0.1057   0.6421   0.0225
  -8.250  -0.3568   0.01821   0.01108  -0.1048   0.6369   0.0232
  -8.000  -0.3446   0.01725   0.01004  -0.1032   0.6322   0.0243
  -7.750  -0.3270   0.01666   0.00939  -0.1023   0.6278   0.0255
  -7.500  -0.3061   0.01618   0.00889  -0.1017   0.6234   0.0271
  -7.250  -0.2842   0.01575   0.00839  -0.1012   0.6190   0.0287
  -7.000  -0.2650   0.01508   0.00766  -0.1005   0.6151   0.0312
  -6.750  -0.2417   0.01473   0.00724  -0.1002   0.6114   0.0343
  -6.500  -0.2188   0.01421   0.00670  -0.0999   0.6078   0.0383
  -6.250  -0.1945   0.01382   0.00628  -0.0997   0.6042   0.0438
  -6.000  -0.1705   0.01337   0.00583  -0.0996   0.6009   0.0538
  -5.750  -0.1469   0.01286   0.00537  -0.0995   0.5978   0.0766
  -5.500  -0.1238   0.01217   0.00493  -0.0995   0.5950   0.1304
  -5.250  -0.1017   0.01125   0.00441  -0.0995   0.5921   0.2282
  -4.750  -0.0539   0.01000   0.00393  -0.0996   0.5866   0.4532
  -4.500  -0.0252   0.01012   0.00395  -0.0999   0.5840   0.4757
  -4.250   0.0037   0.01029   0.00400  -0.1002   0.5813   0.4905
  -4.000   0.0322   0.01034   0.00406  -0.1004   0.5790   0.5008
  -3.750   0.0608   0.01041   0.00408  -0.1006   0.5766   0.5100
  -3.500   0.0895   0.01053   0.00416  -0.1009   0.5742   0.5190
  -3.250   0.1181   0.01064   0.00422  -0.1011   0.5721   0.5273
  -3.000   0.1468   0.01083   0.00435  -0.1013   0.5700   0.5366
  -2.750   0.1753   0.01095   0.00444  -0.1015   0.5680   0.5436
  -2.500   0.2044   0.01114   0.00455  -0.1018   0.5659   0.5494
  -2.250   0.2331   0.01121   0.00456  -0.1022   0.5644   0.5536
  -2.000   0.2616   0.01115   0.00451  -0.1025   0.5627   0.5564
  -1.750   0.2903   0.01115   0.00450  -0.1029   0.5610   0.5586
  -1.500   0.3191   0.01117   0.00450  -0.1032   0.5592   0.5609
  -1.250   0.3480   0.01119   0.00447  -0.1036   0.5576   0.5628
  -1.000   0.3769   0.01121   0.00445  -0.1041   0.5560   0.5645
  -0.750   0.4058   0.01125   0.00444  -0.1045   0.5545   0.5666
  -0.500   0.4349   0.01132   0.00445  -0.1050   0.5531   0.5688
  -0.250   0.4640   0.01140   0.00447  -0.1055   0.5517   0.5705
   0.000   0.4931   0.01148   0.00453  -0.1060   0.5502   0.5723
   0.250   0.5214   0.01149   0.00458  -0.1064   0.5492   0.5743
   0.500   0.5498   0.01153   0.00463  -0.1067   0.5480   0.5761
   0.750   0.5783   0.01157   0.00469  -0.1071   0.5468   0.5780
   1.000   0.6068   0.01163   0.00476  -0.1075   0.5456   0.5801
   1.250   0.6353   0.01170   0.00482  -0.1079   0.5443   0.5822
   1.500   0.6639   0.01177   0.00488  -0.1083   0.5429   0.5843
   1.750   0.6925   0.01183   0.00494  -0.1087   0.5417   0.5864
   2.000   0.7209   0.01188   0.00503  -0.1091   0.5406   0.5887
   2.250   0.7495   0.01196   0.00513  -0.1095   0.5396   0.5910
   2.500   0.7782   0.01206   0.00524  -0.1100   0.5386   0.5936
   2.750   0.8070   0.01218   0.00537  -0.1105   0.5377   0.5964
   3.000   0.8359   0.01234   0.00552  -0.1110   0.5367   0.5994
   3.250   0.8648   0.01255   0.00573  -0.1116   0.5356   0.6024
   3.500   0.8925   0.01267   0.00593  -0.1119   0.5346   0.6056
   3.750   0.9195   0.01275   0.00609  -0.1120   0.5335   0.6090
   4.000   0.9468   0.01286   0.00626  -0.1122   0.5324   0.6127
   4.250   0.9743   0.01300   0.00645  -0.1125   0.5314   0.6165
   4.500   1.0016   0.01313   0.00665  -0.1127   0.5304   0.6203
   4.750   1.0288   0.01326   0.00686  -0.1130   0.5294   0.6245
   5.000   1.0562   0.01340   0.00707  -0.1132   0.5283   0.6292
   5.250   1.0837   0.01355   0.00726  -0.1135   0.5272   0.6342
   5.500   1.1109   0.01368   0.00749  -0.1138   0.5262   0.6392
   5.750   1.1385   0.01384   0.00772  -0.1141   0.5253   0.6451
   6.000   1.1662   0.01399   0.00793  -0.1144   0.5242   0.6513
   6.250   1.1942   0.01412   0.00813  -0.1148   0.5230   0.6580
   6.500   1.2229   0.01431   0.00836  -0.1153   0.5217   0.6657
   6.750   1.2512   0.01463   0.00875  -0.1158   0.5200   0.6735
   7.000   1.2753   0.01473   0.00898  -0.1155   0.5187   0.6826
   7.250   1.2989   0.01483   0.00924  -0.1151   0.5168   0.6923
   7.500   1.3229   0.01494   0.00949  -0.1147   0.5148   0.7031
   7.750   1.3475   0.01504   0.00971  -0.1145   0.5127   0.7156
   8.000   1.3740   0.01491   0.00965  -0.1144   0.5093   0.7298
   8.250   1.3963   0.01455   0.00935  -0.1134   0.5016   0.7461
   8.500   1.4141   0.01399   0.00883  -0.1113   0.4918   0.7654
   8.750   1.4261   0.01376   0.00877  -0.1085   0.4829   0.7897
   9.000   1.4417   0.01357   0.00867  -0.1062   0.4755   0.8202
   9.250   1.4527   0.01353   0.00887  -0.1032   0.4697   0.8661
   9.500   1.4751   0.01340   0.00896  -0.1026   0.4620   1.0000
   9.750   1.4871   0.01358   0.00920  -0.1001   0.4544   1.0000
  10.000   1.4974   0.01383   0.00945  -0.0974   0.4455   1.0000
  10.250   1.5056   0.01422   0.00990  -0.0946   0.4320   1.0000
  10.500   1.5089   0.01486   0.01054  -0.0913   0.4061   1.0000
  10.750   1.4904   0.01663   0.01210  -0.0856   0.3690   1.0000
  11.000   1.4666   0.01938   0.01467  -0.0805   0.3328   1.0000
  11.250   1.4446   0.02262   0.01778  -0.0767   0.3041   1.0000
  11.500   1.4198   0.02652   0.02156  -0.0734   0.2734   1.0000
  11.750   1.3967   0.03062   0.02557  -0.0708   0.2488   1.0000
  12.000   1.3750   0.03482   0.02968  -0.0686   0.2247   1.0000
  12.250   1.3512   0.03942   0.03417  -0.0666   0.1994   1.0000
  12.500   1.3311   0.04382   0.03847  -0.0650   0.1737   1.0000
  12.750   1.3137   0.04808   0.04261  -0.0637   0.1500   1.0000
  13.000   1.2969   0.05236   0.04676  -0.0625   0.1242   1.0000
  13.250   1.2821   0.05649   0.05075  -0.0614   0.0987   1.0000
  13.500   1.2676   0.06069   0.05476  -0.0605   0.0718   1.0000
  13.750   1.2589   0.06432   0.05827  -0.0598   0.0522   1.0000
  14.000   1.2501   0.06805   0.06189  -0.0591   0.0364   1.0000
  14.250   1.2483   0.07111   0.06491  -0.0587   0.0283   1.0000
  14.500   1.2463   0.07427   0.06805  -0.0584   0.0234   1.0000
  14.750   1.2498   0.07681   0.07064  -0.0582   0.0211   1.0000
  15.000   1.2502   0.07973   0.07358  -0.0580   0.0191   1.0000
  15.250   1.2516   0.08260   0.07651  -0.0579   0.0176   1.0000
  15.500   1.2555   0.08520   0.07916  -0.0579   0.0167   1.0000
  15.750   1.2579   0.08800   0.08202  -0.0579   0.0158   1.0000
  16.000   1.2579   0.09109   0.08515  -0.0579   0.0150   1.0000
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