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FX 75-VG-166/22 (fx75vg166-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 75-VG-166/22 (fx75vg166-il)
Reynolds number: 1,000,000
Max Cl/Cd: 103.32 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx75vg166-il-1000000-n5.txt
Download as CSV file: xf-fx75vg166-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.8954   0.07154   0.06765  -0.0818   0.7266   0.0059
 -17.500  -0.9123   0.06438   0.06031  -0.0867   0.7263   0.0057
 -17.250  -0.9272   0.05797   0.05375  -0.0910   0.7260   0.0058
 -17.000  -0.9408   0.05235   0.04795  -0.0945   0.7256   0.0058
 -16.750  -0.9447   0.04837   0.04385  -0.0967   0.7252   0.0059
 -16.500  -0.9442   0.04518   0.04052  -0.0984   0.7246   0.0059
 -16.250  -0.9400   0.04271   0.03796  -0.0994   0.7243   0.0061
 -16.000  -0.9425   0.03978   0.03488  -0.0999   0.7241   0.0059
 -15.750  -0.9385   0.03766   0.03266  -0.1001   0.7238   0.0059
 -15.500  -0.9372   0.03541   0.03028  -0.0999   0.7235   0.0059
 -15.250  -0.9292   0.03386   0.02865  -0.0997   0.7231   0.0060
 -15.000  -0.9220   0.03226   0.02696  -0.0993   0.7226   0.0062
 -14.750  -0.9076   0.03130   0.02595  -0.0992   0.7221   0.0063
 -14.500  -0.9022   0.02960   0.02413  -0.0983   0.7216   0.0062
 -14.250  -0.8904   0.02846   0.02290  -0.0978   0.7211   0.0064
 -14.000  -0.8745   0.02763   0.02201  -0.0975   0.7206   0.0067
 -13.750  -0.8618   0.02658   0.02088  -0.0969   0.7202   0.0066
 -13.500  -0.8463   0.02573   0.01996  -0.0964   0.7196   0.0068
 -13.250  -0.8325   0.02475   0.01889  -0.0956   0.7190   0.0070
 -13.000  -0.8175   0.02389   0.01796  -0.0949   0.7185   0.0070
 -12.750  -0.8016   0.02310   0.01708  -0.0942   0.7180   0.0071
 -12.500  -0.7843   0.02241   0.01632  -0.0936   0.7174   0.0072
 -12.250  -0.7686   0.02164   0.01549  -0.0928   0.7167   0.0073
 -12.000  -0.7511   0.02100   0.01479  -0.0921   0.7161   0.0072
 -11.750  -0.7365   0.02014   0.01386  -0.0909   0.7152   0.0076
 -11.500  -0.7178   0.01959   0.01328  -0.0902   0.7146   0.0078
 -11.250  -0.6995   0.01901   0.01265  -0.0894   0.7139   0.0078
 -11.000  -0.6794   0.01857   0.01218  -0.0888   0.7132   0.0083
 -10.750  -0.6592   0.01812   0.01170  -0.0882   0.7126   0.0087
 -10.500  -0.6409   0.01754   0.01105  -0.0873   0.7120   0.0084
 -10.250  -0.6199   0.01717   0.01065  -0.0868   0.7114   0.0090
 -10.000  -0.5986   0.01682   0.01026  -0.0863   0.7106   0.0094
  -9.750  -0.5790   0.01638   0.00978  -0.0854   0.7102   0.0095
  -9.500  -0.5597   0.01592   0.00930  -0.0844   0.7098   0.0098
  -9.250  -0.5395   0.01554   0.00892  -0.0836   0.7093   0.0104
  -9.000  -0.5194   0.01517   0.00853  -0.0828   0.7087   0.0107
  -8.750  -0.4980   0.01489   0.00824  -0.0821   0.7081   0.0114
  -8.500  -0.4777   0.01454   0.00788  -0.0812   0.7075   0.0117
  -8.250  -0.4572   0.01422   0.00753  -0.0803   0.7068   0.0122
  -8.000  -0.4367   0.01390   0.00720  -0.0794   0.7061   0.0127
  -7.750  -0.4168   0.01357   0.00687  -0.0783   0.7054   0.0134
  -7.500  -0.3966   0.01327   0.00657  -0.0773   0.7047   0.0141
  -7.250  -0.3766   0.01300   0.00628  -0.0763   0.7040   0.0148
  -7.000  -0.3563   0.01278   0.00606  -0.0752   0.7033   0.0156
  -6.750  -0.3384   0.01251   0.00577  -0.0737   0.7025   0.0164
  -6.500  -0.3204   0.01228   0.00553  -0.0722   0.7018   0.0171
  -6.250  -0.3009   0.01207   0.00532  -0.0709   0.7011   0.0182
  -6.000  -0.2790   0.01187   0.00511  -0.0701   0.7004   0.0192
  -5.750  -0.2569   0.01166   0.00488  -0.0692   0.6997   0.0202
  -5.500  -0.2348   0.01144   0.00467  -0.0684   0.6990   0.0219
  -5.250  -0.2118   0.01126   0.00447  -0.0678   0.6984   0.0233
  -5.000  -0.1887   0.01106   0.00429  -0.0672   0.6977   0.0262
  -4.750  -0.1650   0.01090   0.00413  -0.0666   0.6970   0.0296
  -4.500  -0.1416   0.01071   0.00398  -0.0661   0.6964   0.0352
  -4.250  -0.1179   0.01053   0.00384  -0.0656   0.6957   0.0421
  -4.000  -0.0941   0.01034   0.00370  -0.0651   0.6949   0.0519
  -3.750  -0.0709   0.01010   0.00356  -0.0645   0.6940   0.0704
  -3.250  -0.0245   0.00960   0.00328  -0.0633   0.6918   0.1249
  -3.000  -0.0019   0.00928   0.00313  -0.0627   0.6906   0.1695
  -2.750   0.0180   0.00881   0.00294  -0.0616   0.6896   0.2465
  -2.500   0.0392   0.00838   0.00277  -0.0608   0.6886   0.3184
  -2.250   0.0584   0.00781   0.00255  -0.0597   0.6875   0.4174
  -2.000   0.0756   0.00708   0.00226  -0.0582   0.6864   0.5403
  -1.750   0.0894   0.00635   0.00209  -0.0557   0.6854   0.6873
  -1.500   0.1165   0.00640   0.00226  -0.0555   0.6845   0.7285
  -1.250   0.1469   0.00672   0.00263  -0.0559   0.6837   0.7438
  -1.000   0.1763   0.00689   0.00273  -0.0563   0.6826   0.7635
  -0.750   0.2059   0.00709   0.00295  -0.0567   0.6814   0.7677
  -0.500   0.2351   0.00719   0.00306  -0.0570   0.6798   0.7709
  -0.250   0.2639   0.00725   0.00309  -0.0574   0.6782   0.7740
   0.000   0.2924   0.00725   0.00306  -0.0577   0.6768   0.7760
   0.250   0.3211   0.00725   0.00306  -0.0580   0.6754   0.7771
   0.500   0.3501   0.00725   0.00306  -0.0584   0.6737   0.7779
   0.750   0.3790   0.00725   0.00305  -0.0587   0.6720   0.7788
   1.000   0.4078   0.00724   0.00302  -0.0591   0.6702   0.7795
   1.250   0.4365   0.00726   0.00303  -0.0594   0.6683   0.7803
   1.500   0.4649   0.00728   0.00309  -0.0597   0.6660   0.7812
   1.750   0.4934   0.00730   0.00313  -0.0600   0.6637   0.7821
   2.000   0.5218   0.00731   0.00315  -0.0603   0.6609   0.7831
   2.250   0.5501   0.00730   0.00314  -0.0606   0.6580   0.7841
   2.500   0.5783   0.00729   0.00311  -0.0608   0.6550   0.7850
   2.750   0.6064   0.00730   0.00313  -0.0611   0.6521   0.7859
   3.000   0.6344   0.00730   0.00316  -0.0613   0.6479   0.7867
   3.250   0.6617   0.00727   0.00311  -0.0613   0.6399   0.7876
   3.500   0.6887   0.00727   0.00310  -0.0614   0.6288   0.7884
   3.750   0.7139   0.00732   0.00308  -0.0610   0.6132   0.7892
   4.000   0.7392   0.00740   0.00312  -0.0607   0.6005   0.7898
   4.250   0.7645   0.00749   0.00318  -0.0604   0.5899   0.7904
   4.500   0.7873   0.00762   0.00326  -0.0595   0.5661   0.7912
   4.750   0.8081   0.00784   0.00340  -0.0584   0.5434   0.7919
   5.000   0.8277   0.00812   0.00360  -0.0570   0.5184   0.7926
   5.250   0.8429   0.00854   0.00388  -0.0548   0.4837   0.7931
   5.500   0.8459   0.00932   0.00438  -0.0503   0.4226   0.7939
   5.750   0.8510   0.00996   0.00482  -0.0463   0.3773   0.7946
   6.000   0.8501   0.01068   0.00532  -0.0412   0.3312   0.7954
   6.250   0.8537   0.01108   0.00565  -0.0368   0.3079   0.7961
   6.500   0.8527   0.01167   0.00612  -0.0317   0.2825   0.7971
   6.750   0.8495   0.01245   0.00679  -0.0267   0.2541   0.7981
   7.000   0.8421   0.01378   0.00799  -0.0220   0.2228   0.7990
   7.250   0.8405   0.01499   0.00908  -0.0185   0.1979   0.7997
   7.500   0.8483   0.01579   0.00983  -0.0161   0.1829   0.8003
   7.750   0.8482   0.01693   0.01080  -0.0128   0.1534   0.8009
   8.000   0.8601   0.01761   0.01143  -0.0112   0.1414   0.8013
   8.250   0.8645   0.01863   0.01231  -0.0086   0.1157   0.8018
   8.500   0.8815   0.01913   0.01283  -0.0077   0.1138   0.8021
   8.750   0.8922   0.01992   0.01355  -0.0061   0.0986   0.8024
   9.000   0.9041   0.02070   0.01426  -0.0047   0.0847   0.8027
   9.250   0.9133   0.02164   0.01509  -0.0031   0.0684   0.8029
   9.500   0.9266   0.02239   0.01580  -0.0020   0.0591   0.8032
   9.750   0.9394   0.02320   0.01656  -0.0008   0.0481   0.8034
  10.000   0.9515   0.02408   0.01738   0.0003   0.0383   0.8035
  10.250   0.9655   0.02487   0.01816   0.0012   0.0332   0.8037
  10.500   0.9784   0.02575   0.01900   0.0021   0.0265   0.8038
  10.750   0.9945   0.02646   0.01972   0.0027   0.0246   0.8040
  11.000   1.0085   0.02731   0.02056   0.0035   0.0212   0.8041
  11.250   1.0238   0.02815   0.02141   0.0040   0.0198   0.8042
  11.500   1.0393   0.02901   0.02229   0.0045   0.0185   0.8043
  11.750   1.0552   0.02986   0.02315   0.0049   0.0171   0.8044
  12.000   1.0715   0.03070   0.02403   0.0052   0.0162   0.8044
  12.250   1.0867   0.03166   0.02501   0.0055   0.0155   0.8045
  12.500   1.1006   0.03271   0.02607   0.0059   0.0143   0.8045
  12.750   1.1167   0.03363   0.02703   0.0061   0.0134   0.8046
  13.000   1.1322   0.03460   0.02804   0.0064   0.0131   0.8046
  13.250   1.1463   0.03570   0.02916   0.0066   0.0123   0.8047
  13.500   1.1600   0.03685   0.03035   0.0069   0.0119   0.8047
  13.750   1.1731   0.03807   0.03159   0.0072   0.0109   0.8047
  14.000   1.1872   0.03923   0.03280   0.0073   0.0105   0.8048
  14.250   1.1999   0.04050   0.03411   0.0075   0.0103   0.8049
  14.500   1.2126   0.04178   0.03544   0.0077   0.0100   0.8050
  14.750   1.2241   0.04315   0.03683   0.0080   0.0092   0.8051
  15.000   1.2353   0.04464   0.03839   0.0081   0.0093   0.8051
  15.250   1.2464   0.04617   0.03994   0.0082   0.0085   0.8052
  15.500   1.2555   0.04789   0.04172   0.0083   0.0084   0.8052
  15.750   1.2669   0.04945   0.04334   0.0083   0.0083   0.8053
  16.000   1.2764   0.05122   0.04517   0.0082   0.0081   0.8054
  16.250   1.2867   0.05296   0.04698   0.0080   0.0080   0.8056
  16.500   1.2945   0.05490   0.04898   0.0080   0.0076   0.8056
  16.750   1.3024   0.05694   0.05110   0.0078   0.0076   0.8059
  17.000   1.3104   0.05897   0.05319   0.0075   0.0074   0.8061
  17.250   1.3143   0.06140   0.05570   0.0074   0.0073   0.8061
  17.500   1.3202   0.06367   0.05804   0.0071   0.0073   0.8062
  17.750   1.3255   0.06608   0.06051   0.0067   0.0071   0.8063
  18.000   1.3290   0.06869   0.06319   0.0064   0.0069   0.8063
  18.250   1.3316   0.07143   0.06601   0.0059   0.0069   0.8063
  18.500   1.3323   0.07446   0.06911   0.0054   0.0067   0.8064
  18.750   1.3342   0.07732   0.07206   0.0048   0.0067   0.8064
  19.000   1.3301   0.08101   0.07584   0.0040   0.0065   0.8064
  19.250   1.3272   0.08463   0.07955   0.0032   0.0064   0.8065
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