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NACA 2414 (n2414-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 2414 (n2414-il)
Reynolds number: 1,000,000
Max Cl/Cd: 90.04 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n2414-il-1000000-n5.txt
Download as CSV file: xf-n2414-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 2414                                       
  
 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  -1.1513   0.08637   0.08297  -0.0417   1.0000   0.0159
 -18.250  -1.2034   0.07478   0.07120  -0.0481   1.0000   0.0158
 -18.000  -1.2484   0.06428   0.06051  -0.0541   1.0000   0.0157
 -17.750  -1.2803   0.05571   0.05176  -0.0592   1.0000   0.0157
 -17.500  -1.3010   0.04887   0.04476  -0.0636   1.0000   0.0158
 -17.250  -1.3131   0.04353   0.03927  -0.0670   1.0000   0.0158
 -17.000  -1.3192   0.03930   0.03491  -0.0696   1.0000   0.0159
 -16.750  -1.3211   0.03592   0.03142  -0.0714   1.0000   0.0160
 -16.500  -1.3213   0.03305   0.02844  -0.0725   1.0000   0.0161
 -16.250  -1.3213   0.03053   0.02582  -0.0729   1.0000   0.0163
 -16.000  -1.3186   0.02855   0.02375  -0.0726   1.0000   0.0165
 -15.750  -1.3135   0.02697   0.02209  -0.0719   1.0000   0.0168
 -15.500  -1.3068   0.02568   0.02074  -0.0707   1.0000   0.0170
 -15.250  -1.2990   0.02460   0.01960  -0.0692   1.0000   0.0173
 -15.000  -1.2907   0.02368   0.01863  -0.0672   1.0000   0.0176
 -14.750  -1.2830   0.02291   0.01779  -0.0648   1.0000   0.0178
 -14.500  -1.2746   0.02223   0.01706  -0.0622   1.0000   0.0181
 -14.250  -1.2633   0.02160   0.01637  -0.0600   1.0000   0.0184
 -14.000  -1.2520   0.02102   0.01574  -0.0576   1.0000   0.0186
 -13.750  -1.2402   0.02049   0.01515  -0.0552   1.0000   0.0188
 -13.500  -1.2287   0.01998   0.01459  -0.0527   1.0000   0.0191
 -13.250  -1.2118   0.01934   0.01392  -0.0513   0.9994   0.0195
 -13.000  -1.1853   0.01870   0.01325  -0.0518   0.9979   0.0200
 -12.750  -1.1579   0.01812   0.01264  -0.0523   0.9962   0.0205
 -12.500  -1.1297   0.01758   0.01206  -0.0530   0.9948   0.0211
 -12.250  -1.1005   0.01708   0.01151  -0.0538   0.9936   0.0217
 -12.000  -1.0732   0.01663   0.01101  -0.0541   0.9916   0.0222
 -11.750  -1.0457   0.01611   0.01047  -0.0546   0.9893   0.0229
 -11.500  -1.0168   0.01563   0.00998  -0.0552   0.9873   0.0238
 -11.250  -0.9871   0.01519   0.00952  -0.0560   0.9855   0.0246
 -11.000  -0.9570   0.01479   0.00908  -0.0567   0.9837   0.0254
 -10.750  -0.9275   0.01440   0.00865  -0.0574   0.9815   0.0261
 -10.500  -0.9016   0.01399   0.00824  -0.0572   0.9769   0.0271
 -10.250  -0.8735   0.01362   0.00785  -0.0575   0.9732   0.0281
 -10.000  -0.8441   0.01328   0.00749  -0.0580   0.9701   0.0292
  -9.750  -0.8182   0.01297   0.00715  -0.0577   0.9650   0.0301
  -9.500  -0.7916   0.01262   0.00680  -0.0576   0.9598   0.0316
  -9.250  -0.7639   0.01232   0.00647  -0.0577   0.9554   0.0330
  -9.000  -0.7381   0.01206   0.00619  -0.0573   0.9488   0.0342
  -8.750  -0.7118   0.01175   0.00587  -0.0570   0.9423   0.0358
  -8.500  -0.6856   0.01149   0.00559  -0.0567   0.9353   0.0375
  -8.250  -0.6592   0.01126   0.00533  -0.0563   0.9266   0.0390
  -8.000  -0.6331   0.01099   0.00505  -0.0560   0.9179   0.0412
  -7.750  -0.6067   0.01077   0.00480  -0.0556   0.9085   0.0436
  -7.500  -0.5800   0.01055   0.00456  -0.0554   0.8994   0.0459
  -7.250  -0.5534   0.01034   0.00432  -0.0551   0.8902   0.0486
  -7.000  -0.5263   0.01015   0.00411  -0.0549   0.8808   0.0512
  -6.750  -0.4996   0.00994   0.00389  -0.0546   0.8712   0.0550
  -6.500  -0.4725   0.00977   0.00369  -0.0544   0.8608   0.0585
  -6.250  -0.4455   0.00958   0.00349  -0.0542   0.8506   0.0631
  -6.000  -0.4183   0.00943   0.00331  -0.0539   0.8394   0.0672
  -5.750  -0.3910   0.00926   0.00314  -0.0538   0.8282   0.0725
  -5.500  -0.3639   0.00911   0.00297  -0.0536   0.8169   0.0779
  -5.250  -0.3365   0.00899   0.00282  -0.0534   0.8045   0.0833
  -5.000  -0.3091   0.00884   0.00267  -0.0532   0.7921   0.0905
  -4.750  -0.2817   0.00872   0.00253  -0.0530   0.7797   0.0973
  -4.500  -0.2544   0.00861   0.00240  -0.0529   0.7664   0.1049
  -4.250  -0.2269   0.00849   0.00227  -0.0527   0.7527   0.1140
  -4.000  -0.1993   0.00839   0.00216  -0.0526   0.7395   0.1235
  -3.750  -0.1718   0.00830   0.00206  -0.0524   0.7258   0.1340
  -3.500  -0.1445   0.00820   0.00196  -0.0523   0.7115   0.1468
  -3.000  -0.0895   0.00802   0.00179  -0.0520   0.6823   0.1733
  -2.750  -0.0619   0.00795   0.00172  -0.0519   0.6675   0.1869
  -2.500  -0.0342   0.00789   0.00166  -0.0517   0.6533   0.2016
  -2.250  -0.0067   0.00783   0.00161  -0.0516   0.6386   0.2174
  -2.000   0.0208   0.00778   0.00156  -0.0515   0.6241   0.2350
  -1.750   0.0485   0.00773   0.00152  -0.0514   0.6095   0.2522
  -1.500   0.0763   0.00768   0.00149  -0.0513   0.5957   0.2705
  -1.250   0.1040   0.00764   0.00146  -0.0512   0.5822   0.2892
  -1.000   0.1316   0.00761   0.00145  -0.0511   0.5687   0.3098
  -0.500   0.1871   0.00755   0.00143  -0.0510   0.5419   0.3529
  -0.250   0.2147   0.00751   0.00143  -0.0509   0.5296   0.3775
   0.000   0.2422   0.00748   0.00144  -0.0508   0.5171   0.4054
   0.250   0.2696   0.00742   0.00145  -0.0506   0.5047   0.4399
   0.500   0.2971   0.00736   0.00147  -0.0505   0.4936   0.4756
   0.750   0.3245   0.00733   0.00150  -0.0504   0.4826   0.5113
   1.000   0.3520   0.00729   0.00154  -0.0503   0.4717   0.5459
   1.250   0.3795   0.00727   0.00158  -0.0502   0.4615   0.5780
   1.500   0.4068   0.00728   0.00163  -0.0500   0.4504   0.6090
   1.750   0.4343   0.00726   0.00169  -0.0499   0.4399   0.6410
   2.000   0.4615   0.00727   0.00175  -0.0497   0.4283   0.6721
   2.250   0.4883   0.00730   0.00183  -0.0494   0.4153   0.7038
   2.500   0.5154   0.00731   0.00190  -0.0492   0.4026   0.7353
   2.750   0.5421   0.00734   0.00199  -0.0489   0.3900   0.7675
   3.000   0.5683   0.00739   0.00209  -0.0484   0.3764   0.8003
   3.250   0.5943   0.00746   0.00220  -0.0479   0.3613   0.8313
   3.500   0.6197   0.00755   0.00233  -0.0473   0.3456   0.8621
   3.750   0.6447   0.00768   0.00246  -0.0466   0.3278   0.8900
   4.000   0.6696   0.00784   0.00261  -0.0459   0.3098   0.9157
   4.500   0.7222   0.00825   0.00293  -0.0451   0.2738   0.9565
   4.750   0.7531   0.00854   0.00313  -0.0458   0.2522   0.9735
   5.000   0.7854   0.00885   0.00333  -0.0468   0.2321   0.9844
   5.250   0.8170   0.00913   0.00353  -0.0478   0.2139   0.9904
   5.500   0.8478   0.00943   0.00374  -0.0486   0.1959   0.9942
   5.750   0.8797   0.00977   0.00397  -0.0497   0.1766   0.9968
   6.000   0.9105   0.01014   0.00423  -0.0506   0.1574   0.9997
   6.250   0.9324   0.01045   0.00446  -0.0495   0.1424   1.0000
   6.500   0.9533   0.01075   0.00469  -0.0482   0.1297   1.0000
   6.750   0.9748   0.01104   0.00492  -0.0470   0.1187   1.0000
   7.000   0.9969   0.01133   0.00517  -0.0459   0.1088   1.0000
   7.250   1.0190   0.01166   0.00543  -0.0449   0.0990   1.0000
   7.500   1.0412   0.01199   0.00571  -0.0440   0.0902   1.0000
   7.750   1.0636   0.01232   0.00600  -0.0430   0.0825   1.0000
   8.000   1.0863   0.01264   0.00629  -0.0422   0.0758   1.0000
   8.250   1.1086   0.01299   0.00660  -0.0413   0.0697   1.0000
   8.500   1.1307   0.01334   0.00693  -0.0404   0.0641   1.0000
   8.750   1.1529   0.01368   0.00725  -0.0395   0.0594   1.0000
   9.000   1.1744   0.01407   0.00761  -0.0385   0.0548   1.0000
   9.250   1.1961   0.01442   0.00795  -0.0375   0.0511   1.0000
   9.500   1.2171   0.01481   0.00833  -0.0365   0.0478   1.0000
   9.750   1.2379   0.01519   0.00870  -0.0354   0.0448   1.0000
  10.000   1.2576   0.01561   0.00912  -0.0342   0.0421   1.0000
  10.250   1.2764   0.01599   0.00950  -0.0327   0.0399   1.0000
  10.500   1.2938   0.01643   0.00994  -0.0311   0.0378   1.0000
  10.750   1.3114   0.01687   0.01040  -0.0296   0.0362   1.0000
  11.000   1.3289   0.01733   0.01087  -0.0281   0.0345   1.0000
  11.250   1.3453   0.01786   0.01141  -0.0265   0.0328   1.0000
  11.500   1.3619   0.01839   0.01196  -0.0250   0.0314   1.0000
  11.750   1.3783   0.01894   0.01254  -0.0235   0.0300   1.0000
  12.000   1.3935   0.01957   0.01319  -0.0220   0.0287   1.0000
  12.250   1.4083   0.02025   0.01388  -0.0204   0.0276   1.0000
  12.500   1.4236   0.02091   0.01458  -0.0191   0.0267   1.0000
  12.750   1.4379   0.02165   0.01535  -0.0176   0.0258   1.0000
  13.000   1.4510   0.02248   0.01621  -0.0162   0.0249   1.0000
  13.250   1.4631   0.02341   0.01717  -0.0147   0.0240   1.0000
  13.500   1.4762   0.02430   0.01812  -0.0135   0.0234   1.0000
  13.750   1.4884   0.02528   0.01914  -0.0122   0.0227   1.0000
  14.000   1.4995   0.02639   0.02029  -0.0110   0.0219   1.0000
  14.250   1.5094   0.02762   0.02156  -0.0098   0.0212   1.0000
  14.500   1.5179   0.02900   0.02298  -0.0087   0.0206   1.0000
  14.750   1.5274   0.03035   0.02440  -0.0077   0.0201   1.0000
  15.000   1.5361   0.03182   0.02593  -0.0069   0.0196   1.0000
  15.250   1.5437   0.03343   0.02760  -0.0061   0.0192   1.0000
  15.500   1.5501   0.03520   0.02943  -0.0054   0.0187   1.0000
  15.750   1.5552   0.03716   0.03145  -0.0048   0.0183   1.0000
  16.000   1.5590   0.03932   0.03367  -0.0043   0.0178   1.0000
  16.250   1.5610   0.04171   0.03612  -0.0039   0.0174   1.0000
  16.500   1.5637   0.04411   0.03861  -0.0038   0.0172   1.0000
  16.750   1.5661   0.04663   0.04121  -0.0037   0.0169   1.0000
  17.000   1.5671   0.04937   0.04404  -0.0038   0.0166   1.0000
  17.250   1.5666   0.05235   0.04710  -0.0041   0.0164   1.0000
  17.500   1.5649   0.05557   0.05039  -0.0045   0.0161   1.0000
  17.750   1.5620   0.05900   0.05391  -0.0051   0.0158   1.0000
  18.000   1.5577   0.06265   0.05765  -0.0058   0.0156   1.0000
  18.250   1.5517   0.06659   0.06168  -0.0067   0.0154   1.0000
  18.500   1.5442   0.07083   0.06601  -0.0077   0.0151   1.0000
  18.750   1.5353   0.07534   0.07061  -0.0090   0.0149   1.0000
  19.000   1.5245   0.08014   0.07550  -0.0104   0.0147   1.0000
  19.250   1.5127   0.08519   0.08065  -0.0120   0.0146   1.0000
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