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N-13 (n13-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: N-13 (n13-il)
Reynolds number: 1,000,000
Max Cl/Cd: 70.98 at α=8.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n13-il-1000000-n5.txt
Download as CSV file: xf-n13-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: N-13                                            
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -1.0384   0.11417   0.11144  -0.0156   1.0000   0.0045
 -18.250  -1.0816   0.10212   0.09924  -0.0216   1.0000   0.0044
 -18.000  -1.1260   0.09007   0.08701  -0.0277   1.0000   0.0043
 -17.750  -1.1691   0.07861   0.07535  -0.0337   1.0000   0.0043
 -17.500  -1.1951   0.07061   0.06720  -0.0378   1.0000   0.0042
 -17.250  -1.2118   0.06438   0.06083  -0.0409   1.0000   0.0043
 -17.000  -1.2327   0.05782   0.05412  -0.0441   1.0000   0.0042
 -16.750  -1.2477   0.05252   0.04867  -0.0464   1.0000   0.0043
 -16.500  -1.2530   0.04882   0.04487  -0.0476   1.0000   0.0044
 -16.250  -1.2604   0.04507   0.04100  -0.0486   1.0000   0.0044
 -16.000  -1.2670   0.04164   0.03745  -0.0491   1.0000   0.0044
 -15.750  -1.2661   0.03922   0.03495  -0.0492   1.0000   0.0046
 -15.500  -1.2664   0.03682   0.03244  -0.0489   1.0000   0.0046
 -15.250  -1.2729   0.03400   0.02949  -0.0482   1.0000   0.0046
 -15.000  -1.2708   0.03217   0.02756  -0.0472   1.0000   0.0047
 -14.750  -1.2663   0.03064   0.02595  -0.0460   1.0000   0.0048
 -14.500  -1.2617   0.02923   0.02445  -0.0445   1.0000   0.0049
 -14.250  -1.2578   0.02787   0.02299  -0.0427   1.0000   0.0049
 -14.000  -1.2547   0.02655   0.02158  -0.0405   1.0000   0.0050
 -13.750  -1.2488   0.02549   0.02044  -0.0383   1.0000   0.0050
 -13.500  -1.2441   0.02442   0.01929  -0.0357   1.0000   0.0051
 -13.250  -1.2397   0.02340   0.01819  -0.0329   1.0000   0.0053
 -13.000  -1.2340   0.02252   0.01723  -0.0300   1.0000   0.0054
 -12.750  -1.2275   0.02175   0.01639  -0.0269   1.0000   0.0055
 -12.500  -1.2197   0.02111   0.01571  -0.0239   1.0000   0.0058
 -12.250  -1.2126   0.02053   0.01506  -0.0206   1.0000   0.0058
 -12.000  -1.2067   0.01997   0.01444  -0.0169   1.0000   0.0060
 -11.750  -1.1992   0.01946   0.01388  -0.0134   1.0000   0.0061
 -11.500  -1.1868   0.01895   0.01333  -0.0108   1.0000   0.0063
 -11.250  -1.1741   0.01842   0.01274  -0.0083   1.0000   0.0065
 -11.000  -1.1604   0.01793   0.01220  -0.0059   1.0000   0.0067
 -10.750  -1.1360   0.01741   0.01163  -0.0058   0.9993   0.0069
 -10.500  -1.1078   0.01688   0.01105  -0.0065   0.9980   0.0071
 -10.250  -1.0803   0.01620   0.01031  -0.0071   0.9962   0.0077
 -10.000  -1.0512   0.01566   0.00974  -0.0080   0.9945   0.0083
  -9.750  -1.0253   0.01517   0.00922  -0.0080   0.9923   0.0087
  -9.500  -0.9989   0.01471   0.00872  -0.0081   0.9898   0.0092
  -9.250  -0.9711   0.01431   0.00828  -0.0085   0.9874   0.0097
  -8.750  -0.9226   0.01340   0.00731  -0.0077   0.9794   0.0115
  -8.250  -0.8792   0.01268   0.00654  -0.0056   0.9618   0.0134
  -8.000  -0.8538   0.01224   0.00610  -0.0053   0.9536   0.0165
  -7.750  -0.8248   0.01174   0.00566  -0.0060   0.9486   0.0243
  -7.500  -0.7934   0.01136   0.00534  -0.0071   0.9449   0.0320
  -7.250  -0.7598   0.01107   0.00506  -0.0085   0.9419   0.0359
  -6.750  -0.6866   0.01048   0.00444  -0.0129   0.9360   0.0413
  -6.500  -0.6490   0.01021   0.00417  -0.0153   0.9333   0.0439
  -6.250  -0.6108   0.00999   0.00392  -0.0178   0.9311   0.0456
  -6.000  -0.5728   0.00978   0.00369  -0.0203   0.9282   0.0468
  -5.750  -0.5354   0.00954   0.00341  -0.0226   0.9246   0.0499
  -5.500  -0.5008   0.00928   0.00316  -0.0243   0.9203   0.0541
  -5.250  -0.4680   0.00909   0.00295  -0.0256   0.9154   0.0568
  -5.000  -0.4372   0.00890   0.00275  -0.0264   0.9109   0.0640
  -4.750  -0.4105   0.00864   0.00261  -0.0264   0.9067   0.0896
  -4.500  -0.3836   0.00853   0.00250  -0.0262   0.9026   0.0945
  -4.250  -0.3562   0.00841   0.00238  -0.0262   0.8979   0.0991
  -4.000  -0.3291   0.00833   0.00228  -0.0261   0.8924   0.1029
  -3.750  -0.3038   0.00826   0.00219  -0.0255   0.8855   0.1055
  -3.500  -0.2769   0.00820   0.00210  -0.0253   0.8796   0.1072
  -3.250  -0.2528   0.00810   0.00201  -0.0245   0.8730   0.1110
  -3.000  -0.2272   0.00802   0.00192  -0.0239   0.8668   0.1133
  -2.750  -0.2025   0.00793   0.00184  -0.0232   0.8596   0.1159
  -2.500  -0.1774   0.00785   0.00175  -0.0226   0.8513   0.1185
  -2.250  -0.1531   0.00777   0.00167  -0.0218   0.8400   0.1213
  -2.000  -0.1299   0.00767   0.00158  -0.0207   0.8208   0.1296
  -1.750  -0.1119   0.00762   0.00144  -0.0184   0.7669   0.1500
  -1.500  -0.0954   0.00749   0.00133  -0.0160   0.7280   0.2039
  -1.250  -0.0748   0.00738   0.00127  -0.0145   0.7064   0.2398
  -1.000  -0.0545   0.00714   0.00119  -0.0130   0.6907   0.2976
  -0.750  -0.0327   0.00700   0.00115  -0.0117   0.6748   0.3420
  -0.500  -0.0118   0.00687   0.00111  -0.0103   0.6548   0.3891
  -0.250   0.0100   0.00673   0.00108  -0.0090   0.6359   0.4300
   0.000   0.0319   0.00660   0.00105  -0.0077   0.6186   0.4715
   0.250   0.0541   0.00648   0.00104  -0.0066   0.6038   0.5120
   0.500   0.0764   0.00640   0.00104  -0.0053   0.5858   0.5494
   0.750   0.0981   0.00635   0.00105  -0.0040   0.5640   0.5853
   1.000   0.1199   0.00640   0.00107  -0.0027   0.5294   0.6086
   1.250   0.1406   0.00654   0.00111  -0.0011   0.4817   0.6277
   1.500   0.1609   0.00676   0.00118   0.0004   0.4300   0.6440
   1.750   0.1823   0.00691   0.00126   0.0018   0.3934   0.6625
   2.000   0.2040   0.00705   0.00133   0.0031   0.3564   0.6818
   2.250   0.2264   0.00718   0.00140   0.0042   0.3254   0.6976
   2.500   0.2490   0.00730   0.00147   0.0053   0.2961   0.7123
   2.750   0.2713   0.00744   0.00155   0.0065   0.2677   0.7276
   3.000   0.2935   0.00755   0.00164   0.0077   0.2427   0.7443
   3.500   0.3354   0.00778   0.00185   0.0106   0.1925   0.7914
   3.750   0.3560   0.00784   0.00198   0.0122   0.1727   0.8241
   4.000   0.3779   0.00793   0.00216   0.0135   0.1533   0.8716
   4.250   0.4064   0.00812   0.00240   0.0134   0.1360   0.9108
   4.500   0.4342   0.00835   0.00261   0.0134   0.1190   0.9314
   4.750   0.4627   0.00862   0.00282   0.0132   0.1014   0.9440
   5.000   0.4946   0.00890   0.00305   0.0122   0.0880   0.9501
   5.250   0.5231   0.00916   0.00327   0.0120   0.0780   0.9565
   5.500   0.5483   0.00936   0.00346   0.0125   0.0714   0.9609
   5.750   0.5808   0.00961   0.00369   0.0113   0.0649   0.9627
   6.000   0.6118   0.00986   0.00392   0.0104   0.0595   0.9647
   6.250   0.6418   0.01013   0.00417   0.0098   0.0537   0.9668
   6.500   0.6703   0.01035   0.00439   0.0095   0.0500   0.9693
   6.750   0.6930   0.01060   0.00462   0.0105   0.0458   0.9731
   7.000   0.7244   0.01087   0.00489   0.0095   0.0425   0.9741
   7.250   0.7550   0.01113   0.00515   0.0087   0.0394   0.9751
   7.500   0.7846   0.01143   0.00544   0.0081   0.0365   0.9764
   7.750   0.8133   0.01173   0.00574   0.0077   0.0338   0.9779
   8.000   0.8418   0.01201   0.00602   0.0073   0.0313   0.9798
   8.250   0.8676   0.01234   0.00634   0.0075   0.0282   0.9826
   8.500   0.8944   0.01265   0.00667   0.0075   0.0260   0.9848
   8.750   0.9242   0.01302   0.00703   0.0067   0.0222   0.9859
   9.000   0.9526   0.01343   0.00742   0.0062   0.0183   0.9871
   9.250   0.9798   0.01389   0.00787   0.0059   0.0149   0.9887
   9.500   1.0064   0.01434   0.00833   0.0057   0.0130   0.9904
   9.750   1.0316   0.01481   0.00883   0.0058   0.0115   0.9923
  10.000   1.0559   0.01523   0.00929   0.0062   0.0108   0.9940
  10.250   1.0831   0.01571   0.00980   0.0058   0.0099   0.9954
  10.500   1.1102   0.01623   0.01036   0.0054   0.0093   0.9969
  10.750   1.1366   0.01687   0.01104   0.0051   0.0085   0.9984
  11.000   1.1638   0.01738   0.01161   0.0047   0.0082   0.9996
  11.250   1.1814   0.01784   0.01212   0.0062   0.0078   1.0000
  11.500   1.1907   0.01827   0.01260   0.0095   0.0075   1.0000
  11.750   1.1970   0.01871   0.01309   0.0134   0.0073   1.0000
  12.000   1.2001   0.01911   0.01353   0.0178   0.0069   1.0000
  12.250   1.2040   0.01962   0.01409   0.0220   0.0067   1.0000
  12.500   1.2099   0.02017   0.01470   0.0257   0.0065   1.0000
  12.750   1.2162   0.02083   0.01541   0.0290   0.0062   1.0000
  13.000   1.2236   0.02151   0.01617   0.0321   0.0061   1.0000
  13.250   1.2333   0.02213   0.01686   0.0346   0.0060   1.0000
  13.500   1.2415   0.02290   0.01769   0.0371   0.0058   1.0000
  13.750   1.2496   0.02371   0.01859   0.0395   0.0057   1.0000
  14.000   1.2567   0.02465   0.01961   0.0418   0.0056   1.0000
  14.250   1.2632   0.02569   0.02073   0.0439   0.0055   1.0000
  14.500   1.2699   0.02677   0.02188   0.0458   0.0054   1.0000
  14.750   1.2747   0.02804   0.02324   0.0477   0.0052   1.0000
  15.000   1.2800   0.02934   0.02462   0.0492   0.0052   1.0000
  15.250   1.2820   0.03098   0.02636   0.0508   0.0051   1.0000
  15.500   1.2832   0.03281   0.02828   0.0520   0.0049   1.0000
  15.750   1.2853   0.03469   0.03025   0.0528   0.0048   1.0000
  16.000   1.2835   0.03712   0.03279   0.0532   0.0047   1.0000
  16.250   1.2800   0.03991   0.03568   0.0532   0.0046   1.0000
  16.500   1.2741   0.04319   0.03908   0.0528   0.0047   1.0000
  16.750   1.2654   0.04702   0.04303   0.0517   0.0045   1.0000
  17.000   1.2528   0.05166   0.04782   0.0500   0.0046   1.0000
  17.250   1.2385   0.05693   0.05322   0.0475   0.0045   1.0000
  17.500   1.2175   0.06369   0.06014   0.0439   0.0044   1.0000
  17.750   1.1923   0.07162   0.06824   0.0395   0.0045   1.0000
  18.000   1.1609   0.08073   0.07752   0.0346   0.0045   1.0000
  18.250   1.1261   0.09066   0.08762   0.0294   0.0046   1.0000
  18.500   1.0756   0.10368   0.10083   0.0226   0.0046   1.0000
  18.750   1.0233   0.11736   0.11469   0.0156   0.0048   1.0000
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