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WORTMANN FX 73-170 A (fx73170a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 73-170 A (fx73170a-il)
Reynolds number: 1,000,000
Max Cl/Cd: 144.05 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx73170a-il-1000000-n5.txt
Download as CSV file: xf-fx73170a-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 73-170 A                            
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.0157   0.09071   0.08740  -0.1240   0.6837   0.0055
 -11.000  -0.0075   0.08778   0.08446  -0.1261   0.6819   0.0061
 -10.500  -0.3599   0.02357   0.01897  -0.1461   0.6797   0.0047
 -10.250  -0.3522   0.02222   0.01744  -0.1439   0.6775   0.0046
 -10.000  -0.3501   0.02022   0.01517  -0.1410   0.6754   0.0049
  -9.750  -0.3376   0.01906   0.01381  -0.1392   0.6733   0.0049
  -9.500  -0.3133   0.01900   0.01372  -0.1389   0.6716   0.0046
  -9.250  -0.3023   0.01747   0.01198  -0.1369   0.6698   0.0049
  -9.000  -0.2842   0.01663   0.01100  -0.1357   0.6679   0.0050
  -8.750  -0.2617   0.01629   0.01061  -0.1351   0.6659   0.0052
  -8.500  -0.2416   0.01563   0.00984  -0.1342   0.6638   0.0052
  -8.250  -0.2191   0.01525   0.00940  -0.1336   0.6617   0.0054
  -8.000  -0.1991   0.01457   0.00858  -0.1326   0.6595   0.0054
  -7.750  -0.1765   0.01417   0.00810  -0.1319   0.6576   0.0056
  -7.500  -0.1534   0.01373   0.00759  -0.1314   0.6562   0.0058
  -7.250  -0.1302   0.01330   0.00710  -0.1309   0.6546   0.0059
  -7.000  -0.1065   0.01294   0.00669  -0.1304   0.6529   0.0062
  -6.750  -0.0831   0.01255   0.00623  -0.1298   0.6512   0.0062
  -6.500  -0.0588   0.01227   0.00589  -0.1294   0.6494   0.0066
  -6.250  -0.0347   0.01198   0.00554  -0.1290   0.6477   0.0067
  -6.000  -0.0113   0.01163   0.00513  -0.1284   0.6459   0.0067
  -5.750   0.0120   0.01130   0.00475  -0.1278   0.6439   0.0071
  -5.500   0.0363   0.01103   0.00445  -0.1274   0.6423   0.0073
  -5.250   0.0616   0.01081   0.00421  -0.1272   0.6410   0.0078
  -5.000   0.0872   0.01063   0.00402  -0.1270   0.6394   0.0083
  -4.750   0.1123   0.01041   0.00377  -0.1267   0.6379   0.0084
  -4.500   0.1378   0.01023   0.00356  -0.1264   0.6364   0.0090
  -4.250   0.1628   0.01002   0.00333  -0.1261   0.6347   0.0099
  -4.000   0.1883   0.00987   0.00317  -0.1259   0.6332   0.0106
  -3.750   0.2140   0.00974   0.00302  -0.1257   0.6317   0.0119
  -3.500   0.2392   0.00961   0.00285  -0.1254   0.6300   0.0128
  -3.250   0.2646   0.00949   0.00273  -0.1251   0.6284   0.0148
  -3.000   0.2906   0.00936   0.00261  -0.1250   0.6270   0.0176
  -2.750   0.3168   0.00925   0.00250  -0.1249   0.6257   0.0207
  -2.500   0.3428   0.00912   0.00241  -0.1248   0.6243   0.0269
  -2.250   0.3687   0.00901   0.00233  -0.1246   0.6228   0.0353
  -2.000   0.3946   0.00891   0.00225  -0.1245   0.6214   0.0450
  -1.750   0.4196   0.00876   0.00218  -0.1242   0.6200   0.0698
  -1.500   0.4439   0.00857   0.00212  -0.1238   0.6185   0.1125
  -1.250   0.4660   0.00828   0.00206  -0.1230   0.6171   0.1965
  -1.000   0.4864   0.00794   0.00200  -0.1219   0.6156   0.3011
  -0.750   0.5062   0.00761   0.00196  -0.1207   0.6141   0.4076
  -0.500   0.5239   0.00722   0.00193  -0.1190   0.6126   0.5343
  -0.250   0.5388   0.00682   0.00196  -0.1165   0.6114   0.6736
   0.000   0.5603   0.00675   0.00206  -0.1153   0.6100   0.7388
   0.250   0.5854   0.00678   0.00213  -0.1148   0.6087   0.7610
   0.500   0.6109   0.00683   0.00218  -0.1145   0.6073   0.7752
   0.750   0.6366   0.00689   0.00222  -0.1142   0.6059   0.7854
   1.000   0.6623   0.00694   0.00228  -0.1140   0.6044   0.7927
   1.250   0.6881   0.00699   0.00231  -0.1138   0.6029   0.7975
   1.500   0.7141   0.00705   0.00234  -0.1137   0.6014   0.8004
   1.750   0.7404   0.00711   0.00238  -0.1136   0.5999   0.8027
   2.000   0.7667   0.00717   0.00243  -0.1136   0.5984   0.8051
   2.250   0.7934   0.00721   0.00248  -0.1136   0.5974   0.8073
   2.500   0.8199   0.00726   0.00254  -0.1137   0.5962   0.8097
   2.750   0.8462   0.00731   0.00260  -0.1137   0.5950   0.8121
   3.000   0.8723   0.00736   0.00266  -0.1136   0.5935   0.8145
   3.500   0.9242   0.00747   0.00279  -0.1135   0.5903   0.8192
   3.750   0.9501   0.00753   0.00287  -0.1134   0.5888   0.8215
   4.000   0.9757   0.00760   0.00295  -0.1133   0.5874   0.8238
   4.250   1.0012   0.00769   0.00304  -0.1132   0.5859   0.8261
   4.500   1.0264   0.00779   0.00313  -0.1131   0.5839   0.8283
   4.750   1.0519   0.00785   0.00323  -0.1130   0.5826   0.8303
   5.000   1.0763   0.00791   0.00332  -0.1126   0.5807   0.8322
   5.250   1.1006   0.00796   0.00342  -0.1123   0.5778   0.8342
   5.500   1.1242   0.00804   0.00351  -0.1118   0.5744   0.8362
   5.750   1.1482   0.00815   0.00364  -0.1115   0.5714   0.8382
   6.000   1.1724   0.00827   0.00378  -0.1112   0.5680   0.8402
   6.250   1.1974   0.00836   0.00393  -0.1111   0.5633   0.8424
   6.500   1.2215   0.00850   0.00409  -0.1109   0.5588   0.8447
   6.750   1.2444   0.00869   0.00427  -0.1105   0.5540   0.8469
   7.000   1.2705   0.00882   0.00446  -0.1107   0.5488   0.8488
   7.250   1.2961   0.00901   0.00469  -0.1110   0.5430   0.8509
   7.500   1.3207   0.00924   0.00495  -0.1111   0.5343   0.8532
   7.750   1.3406   0.00969   0.00537  -0.1106   0.5162   0.8560
   8.000   1.3563   0.01043   0.00604  -0.1097   0.4925   0.8596
   8.500   1.3503   0.01494   0.01013  -0.1051   0.3941   0.8692
   8.750   1.3371   0.01802   0.01299  -0.1019   0.3463   0.8753
   9.000   1.3270   0.02075   0.01556  -0.0989   0.3065   0.8815
   9.250   1.3338   0.02236   0.01714  -0.0976   0.2896   0.8880
   9.750   1.3357   0.02642   0.02110  -0.0940   0.2438   0.9085
  10.000   1.3419   0.02838   0.02305  -0.0933   0.2230   0.9320
  11.000   1.3444   0.03776   0.03200  -0.0871   0.1256   1.0000
  11.250   1.3381   0.04051   0.03456  -0.0848   0.0949   1.0000
  11.500   1.3388   0.04275   0.03670  -0.0833   0.0771   1.0000
  11.750   1.3506   0.04408   0.03806  -0.0826   0.0728   1.0000
  12.000   1.3542   0.04612   0.04003  -0.0813   0.0589   1.0000
  12.250   1.3590   0.04810   0.04196  -0.0802   0.0478   1.0000
  12.500   1.3661   0.04988   0.04371  -0.0793   0.0399   1.0000
  12.750   1.3715   0.05183   0.04564  -0.0783   0.0326   1.0000
  13.000   1.3807   0.05346   0.04728  -0.0776   0.0296   1.0000
  13.250   1.3906   0.05504   0.04888  -0.0769   0.0269   1.0000
  13.500   1.3971   0.05697   0.05080  -0.0761   0.0231   1.0000
  13.750   1.4067   0.05861   0.05247  -0.0756   0.0216   1.0000
  14.000   1.4164   0.06023   0.05413  -0.0750   0.0198   1.0000
  14.250   1.4233   0.06216   0.05607  -0.0744   0.0175   1.0000
  14.500   1.4322   0.06388   0.05783  -0.0738   0.0164   1.0000
  14.750   1.4418   0.06555   0.05954  -0.0734   0.0158   1.0000
  15.000   1.4481   0.06757   0.06158  -0.0728   0.0135   1.0000
  15.250   1.4560   0.06947   0.06352  -0.0723   0.0131   1.0000
  15.500   1.4633   0.07139   0.06548  -0.0719   0.0109   1.0000
  15.750   1.4699   0.07343   0.06755  -0.0714   0.0099   1.0000
  16.000   1.4752   0.07564   0.06979  -0.0709   0.0082   1.0000
  16.250   1.4782   0.07804   0.07219  -0.0704   0.0058   1.0000
  16.500   1.4830   0.08033   0.07453  -0.0700   0.0052   1.0000
  16.750   1.4879   0.08263   0.07688  -0.0697   0.0046   1.0000
  17.000   1.4940   0.08478   0.07910  -0.0694   0.0045   1.0000
  17.250   1.4963   0.08744   0.08180  -0.0691   0.0039   1.0000
  17.500   1.5004   0.08986   0.08428  -0.0689   0.0037   1.0000
  17.750   1.5043   0.09232   0.08681  -0.0687   0.0033   1.0000
  18.000   1.5073   0.09491   0.08947  -0.0686   0.0031   1.0000
  18.250   1.5114   0.09737   0.09199  -0.0685   0.0030   1.0000
  18.500   1.5125   0.10026   0.09495  -0.0685   0.0029   1.0000
  18.750   1.5151   0.10296   0.09771  -0.0685   0.0028   1.0000
  19.000   1.5151   0.10602   0.10084  -0.0687   0.0026   1.0000
  19.250   1.5178   0.10875   0.10365  -0.0689   0.0026   1.0000
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