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FX 75-VG-166/22 (fx75vg166-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 75-VG-166/22 (fx75vg166-il)
Reynolds number: 500,000
Max Cl/Cd: 84.02 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx75vg166-il-500000-n5.txt
Download as CSV file: xf-fx75vg166-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.6227   0.07247   0.06830  -0.0964   0.7387   0.0084
 -15.250  -0.6583   0.06204   0.05761  -0.1034   0.7384   0.0083
 -15.000  -0.6897   0.05414   0.04946  -0.1077   0.7380   0.0084
 -14.750  -0.6974   0.05026   0.04542  -0.1094   0.7376   0.0085
 -14.500  -0.7087   0.04636   0.04134  -0.1102   0.7371   0.0085
 -14.250  -0.7189   0.04294   0.03771  -0.1102   0.7366   0.0087
 -14.000  -0.7212   0.04047   0.03507  -0.1099   0.7361   0.0089
 -13.750  -0.7237   0.03805   0.03249  -0.1091   0.7356   0.0087
 -13.500  -0.7233   0.03596   0.03021  -0.1081   0.7349   0.0090
 -13.250  -0.7210   0.03405   0.02811  -0.1069   0.7343   0.0092
 -13.000  -0.7154   0.03245   0.02637  -0.1058   0.7337   0.0092
 -12.750  -0.7080   0.03099   0.02475  -0.1046   0.7331   0.0094
 -12.500  -0.6979   0.02978   0.02339  -0.1034   0.7325   0.0096
 -12.250  -0.6875   0.02858   0.02206  -0.1022   0.7319   0.0096
 -12.000  -0.6755   0.02756   0.02094  -0.1011   0.7312   0.0096
 -11.750  -0.6653   0.02638   0.01969  -0.0997   0.7305   0.0100
 -11.500  -0.6512   0.02556   0.01881  -0.0986   0.7297   0.0102
 -11.250  -0.6368   0.02475   0.01790  -0.0974   0.7288   0.0102
 -11.000  -0.6203   0.02417   0.01728  -0.0964   0.7279   0.0106
 -10.750  -0.6039   0.02350   0.01653  -0.0954   0.7272   0.0111
 -10.500  -0.5888   0.02264   0.01558  -0.0941   0.7264   0.0110
 -10.250  -0.5710   0.02208   0.01495  -0.0932   0.7258   0.0116
 -10.000  -0.5528   0.02153   0.01430  -0.0922   0.7252   0.0121
  -9.750  -0.5353   0.02093   0.01362  -0.0912   0.7245   0.0123
  -9.500  -0.5190   0.02026   0.01291  -0.0898   0.7239   0.0127
  -9.250  -0.5011   0.01976   0.01241  -0.0888   0.7232   0.0132
  -9.000  -0.4833   0.01926   0.01188  -0.0876   0.7224   0.0136
  -8.750  -0.4635   0.01892   0.01152  -0.0868   0.7216   0.0144
  -8.500  -0.4448   0.01848   0.01105  -0.0857   0.7208   0.0150
  -8.250  -0.4260   0.01807   0.01059  -0.0846   0.7200   0.0157
  -8.000  -0.4086   0.01758   0.01009  -0.0833   0.7191   0.0165
  -7.750  -0.3895   0.01721   0.00971  -0.0822   0.7182   0.0173
  -7.500  -0.3710   0.01681   0.00929  -0.0809   0.7174   0.0183
  -7.250  -0.3520   0.01646   0.00890  -0.0797   0.7166   0.0192
  -7.000  -0.3332   0.01613   0.00853  -0.0785   0.7158   0.0197
  -6.750  -0.3161   0.01573   0.00815  -0.0770   0.7150   0.0213
  -6.500  -0.2979   0.01545   0.00785  -0.0756   0.7143   0.0226
  -6.250  -0.2800   0.01519   0.00756  -0.0741   0.7136   0.0238
  -6.000  -0.2629   0.01491   0.00727  -0.0725   0.7129   0.0252
  -5.750  -0.2448   0.01467   0.00701  -0.0710   0.7121   0.0273
  -5.500  -0.2242   0.01446   0.00677  -0.0700   0.7114   0.0295
  -5.250  -0.2038   0.01422   0.00654  -0.0689   0.7108   0.0326
  -5.000  -0.1832   0.01402   0.00635  -0.0678   0.7099   0.0372
  -4.750  -0.1628   0.01382   0.00619  -0.0668   0.7087   0.0428
  -4.500  -0.1424   0.01360   0.00604  -0.0657   0.7075   0.0531
  -4.250  -0.1221   0.01336   0.00589  -0.0646   0.7063   0.0708
  -4.000  -0.1018   0.01309   0.00574  -0.0636   0.7052   0.0959
  -3.750  -0.0819   0.01277   0.00557  -0.0625   0.7041   0.1335
  -3.500  -0.0638   0.01234   0.00539  -0.0612   0.7030   0.1949
  -3.250  -0.0470   0.01180   0.00518  -0.0597   0.7020   0.2775
  -3.000  -0.0316   0.01114   0.00492  -0.0580   0.7010   0.3810
  -2.750  -0.0185   0.01025   0.00454  -0.0560   0.6999   0.5126
  -2.500  -0.0058   0.00952   0.00450  -0.0532   0.6989   0.6690
  -2.250   0.0220   0.00998   0.00513  -0.0526   0.6981   0.7210
  -2.000   0.0524   0.01048   0.00563  -0.0526   0.6974   0.7378
  -1.750   0.0812   0.01082   0.00594  -0.0528   0.6962   0.7557
  -1.500   0.1087   0.01125   0.00636  -0.0527   0.6946   0.7679
  -1.250   0.1358   0.01145   0.00653  -0.0527   0.6930   0.7749
  -1.000   0.1634   0.01161   0.00667  -0.0527   0.6916   0.7779
  -0.750   0.1915   0.01176   0.00682  -0.0527   0.6902   0.7795
  -0.500   0.2196   0.01182   0.00686  -0.0528   0.6889   0.7811
  -0.250   0.2478   0.01183   0.00685  -0.0530   0.6878   0.7827
   0.000   0.2760   0.01182   0.00681  -0.0533   0.6868   0.7845
   0.250   0.3045   0.01176   0.00672  -0.0536   0.6857   0.7868
   0.500   0.3330   0.01165   0.00656  -0.0541   0.6848   0.7897
   0.750   0.3618   0.01158   0.00647  -0.0545   0.6839   0.7909
   1.000   0.3892   0.01160   0.00650  -0.0545   0.6824   0.7917
   1.250   0.4150   0.01167   0.00661  -0.0543   0.6798   0.7925
   1.500   0.4419   0.01167   0.00664  -0.0544   0.6776   0.7934
   1.750   0.4696   0.01163   0.00662  -0.0545   0.6755   0.7942
   2.000   0.4977   0.01156   0.00655  -0.0547   0.6736   0.7952
   2.250   0.5262   0.01148   0.00647  -0.0550   0.6721   0.7962
   2.500   0.5549   0.01137   0.00637  -0.0554   0.6706   0.7970
   2.750   0.5840   0.01125   0.00623  -0.0558   0.6691   0.7979
   3.000   0.6091   0.01128   0.00632  -0.0556   0.6650   0.7989
   3.250   0.6359   0.01124   0.00633  -0.0557   0.6617   0.8000
   3.500   0.6638   0.01115   0.00625  -0.0559   0.6587   0.8010
   3.750   0.6921   0.01103   0.00615  -0.0562   0.6562   0.8022
   4.000   0.7195   0.01093   0.00606  -0.0564   0.6510   0.8035
   4.250   0.7465   0.01075   0.00589  -0.0564   0.6412   0.8046
   4.500   0.7727   0.01064   0.00579  -0.0562   0.6301   0.8054
   4.750   0.7988   0.01053   0.00568  -0.0560   0.6201   0.8060
   5.000   0.8245   0.01048   0.00564  -0.0557   0.6113   0.8067
   5.250   0.8492   0.01050   0.00567  -0.0552   0.6009   0.8075
   5.500   0.8724   0.01054   0.00570  -0.0545   0.5854   0.8082
   5.750   0.8940   0.01064   0.00576  -0.0535   0.5649   0.8088
   6.000   0.9097   0.01087   0.00587  -0.0513   0.5351   0.8096
   6.250   0.9139   0.01144   0.00619  -0.0470   0.4867   0.8106
   6.500   0.9147   0.01206   0.00664  -0.0423   0.4481   0.8118
   6.750   0.9051   0.01274   0.00715  -0.0357   0.4102   0.8131
   7.000   0.8912   0.01364   0.00788  -0.0287   0.3747   0.8146
   7.500   0.8771   0.01617   0.01020  -0.0196   0.3236   0.8175
   7.750   0.8689   0.01757   0.01143  -0.0152   0.2897   0.8185
   8.000   0.8661   0.01879   0.01248  -0.0116   0.2588   0.8193
   8.250   0.8616   0.02013   0.01361  -0.0079   0.2219   0.8199
   8.500   0.8665   0.02108   0.01444  -0.0055   0.1994   0.8204
   8.750   0.8702   0.02213   0.01536  -0.0030   0.1715   0.8209
   9.000   0.8790   0.02300   0.01615  -0.0012   0.1549   0.8213
   9.250   0.8888   0.02385   0.01693   0.0004   0.1375   0.8217
   9.500   0.8997   0.02467   0.01771   0.0018   0.1240   0.8221
  10.000   0.9209   0.02646   0.01938   0.0046   0.0957   0.8227
  10.250   0.9310   0.02743   0.02026   0.0059   0.0784   0.8230
  10.500   0.9390   0.02855   0.02128   0.0073   0.0612   0.8233
  10.750   0.9516   0.02946   0.02217   0.0082   0.0528   0.8236
  11.000   0.9607   0.03065   0.02327   0.0093   0.0406   0.8238
  11.250   0.9740   0.03159   0.02423   0.0101   0.0351   0.8240
  11.500   0.9863   0.03265   0.02528   0.0108   0.0302   0.8242
  11.750   0.9987   0.03373   0.02636   0.0115   0.0265   0.8244
  12.000   1.0123   0.03475   0.02741   0.0120   0.0243   0.8246
  12.250   1.0246   0.03590   0.02857   0.0126   0.0227   0.8248
  12.500   1.0374   0.03702   0.02975   0.0131   0.0211   0.8249
  12.750   1.0499   0.03820   0.03097   0.0136   0.0194   0.8251
  13.000   1.0623   0.03941   0.03223   0.0140   0.0189   0.8254
  13.250   1.0724   0.04084   0.03369   0.0145   0.0177   0.8255
  13.500   1.0846   0.04213   0.03504   0.0148   0.0170   0.8256
  13.750   1.0963   0.04348   0.03645   0.0151   0.0158   0.8257
  14.000   1.1071   0.04492   0.03795   0.0154   0.0150   0.8260
  14.250   1.1167   0.04651   0.03960   0.0157   0.0147   0.8263
  14.500   1.1231   0.04842   0.04156   0.0160   0.0141   0.8267
  14.750   1.1337   0.04996   0.04318   0.0162   0.0135   0.8273
  15.000   1.1416   0.05179   0.04510   0.0164   0.0132   0.8275
  15.250   1.1503   0.05359   0.04697   0.0165   0.0127   0.8278
  15.500   1.1582   0.05551   0.04897   0.0164   0.0124   0.8280
  15.750   1.1658   0.05751   0.05104   0.0163   0.0121   0.8280
  16.000   1.1711   0.05978   0.05337   0.0162   0.0116   0.8280
  16.250   1.1771   0.06201   0.05566   0.0160   0.0113   0.8281
  16.500   1.1771   0.06495   0.05868   0.0158   0.0110   0.8281
  16.750   1.1799   0.06763   0.06147   0.0155   0.0109   0.8281
  17.000   1.1872   0.06988   0.06381   0.0150   0.0106   0.8282
  17.250   1.1859   0.07316   0.06719   0.0145   0.0104   0.8282
  17.500   1.1903   0.07579   0.06991   0.0139   0.0103   0.8282
  17.750   1.1915   0.07888   0.07312   0.0132   0.0101   0.8282
  18.000   1.1924   0.08205   0.07639   0.0123   0.0098   0.8283
  18.250   1.1916   0.08551   0.07995   0.0114   0.0098   0.8283
  18.500   1.1917   0.08891   0.08345   0.0103   0.0095   0.8283
  18.750   1.1917   0.09238   0.08701   0.0091   0.0095   0.8283
  19.000   1.1889   0.09626   0.09099   0.0077   0.0093   0.8283
  19.250   1.1861   0.10021   0.09504   0.0062   0.0092   0.8284
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