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NACA 2414 (n2414-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 2414 (n2414-il)
Reynolds number: 1,000,000
Max Cl/Cd: 103.69 at α=5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-n2414-il-1000000.txt
Download as CSV file: xf-n2414-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -1.1298   0.08491   0.08162  -0.0429   1.0000   0.0199
 -18.000  -1.1553   0.07749   0.07409  -0.0469   1.0000   0.0199
 -17.750  -1.1815   0.07006   0.06653  -0.0510   1.0000   0.0199
 -17.500  -1.2057   0.06285   0.05919  -0.0551   1.0000   0.0200
 -17.250  -1.2260   0.05617   0.05238  -0.0590   1.0000   0.0200
 -17.000  -1.2413   0.05018   0.04627  -0.0627   1.0000   0.0201
 -16.750  -1.2517   0.04505   0.04101  -0.0660   1.0000   0.0202
 -16.500  -1.2577   0.04071   0.03656  -0.0687   1.0000   0.0204
 -16.250  -1.2599   0.03715   0.03289  -0.0707   1.0000   0.0206
 -16.000  -1.2595   0.03419   0.02983  -0.0721   1.0000   0.0208
 -15.750  -1.2572   0.03174   0.02728  -0.0728   1.0000   0.0210
 -15.500  -1.2531   0.02972   0.02516  -0.0729   1.0000   0.0212
 -15.250  -1.2475   0.02806   0.02341  -0.0724   1.0000   0.0215
 -15.000  -1.2401   0.02672   0.02199  -0.0715   1.0000   0.0217
 -14.750  -1.2315   0.02560   0.02079  -0.0702   1.0000   0.0220
 -14.500  -1.2211   0.02473   0.01984  -0.0687   1.0000   0.0222
 -14.250  -1.2229   0.02346   0.01850  -0.0654   1.0000   0.0226
 -14.000  -1.2227   0.02251   0.01749  -0.0617   1.0000   0.0229
 -13.750  -1.2157   0.02176   0.01670  -0.0588   1.0000   0.0233
 -13.500  -1.2065   0.02114   0.01604  -0.0561   1.0000   0.0237
 -13.250  -1.1965   0.02060   0.01546  -0.0533   1.0000   0.0241
 -13.000  -1.1862   0.02009   0.01490  -0.0505   1.0000   0.0245
 -12.750  -1.1752   0.01961   0.01438  -0.0478   1.0000   0.0249
 -12.500  -1.1634   0.01916   0.01387  -0.0452   1.0000   0.0253
 -12.250  -1.1503   0.01876   0.01342  -0.0427   1.0000   0.0257
 -12.000  -1.1298   0.01801   0.01262  -0.0420   0.9993   0.0263
 -11.750  -1.1006   0.01731   0.01189  -0.0430   0.9979   0.0272
 -11.500  -1.0696   0.01680   0.01136  -0.0441   0.9965   0.0281
 -11.250  -1.0377   0.01637   0.01089  -0.0453   0.9952   0.0290
 -11.000  -1.0047   0.01601   0.01048  -0.0467   0.9942   0.0298
 -10.750  -0.9748   0.01528   0.00974  -0.0477   0.9927   0.0312
 -10.500  -0.9448   0.01484   0.00929  -0.0485   0.9904   0.0324
 -10.250  -0.9130   0.01447   0.00888  -0.0495   0.9885   0.0336
 -10.000  -0.8807   0.01403   0.00841  -0.0507   0.9868   0.0348
  -9.750  -0.8481   0.01354   0.00792  -0.0521   0.9853   0.0365
  -9.500  -0.8139   0.01319   0.00756  -0.0536   0.9842   0.0382
  -9.250  -0.7794   0.01282   0.00716  -0.0552   0.9833   0.0399
  -9.000  -0.7448   0.01239   0.00675  -0.0568   0.9824   0.0422
  -8.750  -0.7166   0.01211   0.00645  -0.0569   0.9782   0.0440
  -8.500  -0.6857   0.01172   0.00606  -0.0577   0.9749   0.0464
  -8.250  -0.6538   0.01138   0.00573  -0.0586   0.9719   0.0491
  -8.000  -0.6238   0.01110   0.00543  -0.0590   0.9682   0.0515
  -7.750  -0.5983   0.01077   0.00513  -0.0586   0.9618   0.0550
  -7.500  -0.5699   0.01055   0.00488  -0.0586   0.9570   0.0579
  -7.250  -0.5442   0.01023   0.00459  -0.0581   0.9509   0.0622
  -7.000  -0.5176   0.01003   0.00437  -0.0577   0.9444   0.0658
  -6.750  -0.4910   0.00974   0.00411  -0.0574   0.9385   0.0714
  -6.500  -0.4648   0.00953   0.00390  -0.0570   0.9308   0.0765
  -6.250  -0.4379   0.00930   0.00368  -0.0567   0.9241   0.0826
  -6.000  -0.4114   0.00908   0.00348  -0.0563   0.9160   0.0895
  -5.750  -0.3843   0.00890   0.00329  -0.0560   0.9082   0.0964
  -5.500  -0.3574   0.00869   0.00311  -0.0558   0.8996   0.1052
  -5.250  -0.3303   0.00850   0.00293  -0.0555   0.8909   0.1145
  -5.000  -0.3031   0.00832   0.00278  -0.0553   0.8815   0.1248
  -4.750  -0.2758   0.00817   0.00262  -0.0550   0.8722   0.1358
  -4.500  -0.2483   0.00801   0.00248  -0.0548   0.8617   0.1477
  -4.250  -0.2210   0.00785   0.00235  -0.0546   0.8514   0.1620
  -4.000  -0.1937   0.00770   0.00223  -0.0544   0.8403   0.1770
  -3.750  -0.1661   0.00756   0.00212  -0.0543   0.8288   0.1932
  -3.500  -0.1387   0.00744   0.00201  -0.0541   0.8170   0.2105
  -3.250  -0.1112   0.00733   0.00192  -0.0539   0.8043   0.2281
  -3.000  -0.0837   0.00721   0.00183  -0.0537   0.7913   0.2472
  -2.750  -0.0562   0.00711   0.00175  -0.0536   0.7780   0.2670
  -2.500  -0.0288   0.00702   0.00168  -0.0534   0.7642   0.2883
  -2.250  -0.0015   0.00694   0.00162  -0.0532   0.7497   0.3106
  -1.750   0.0536   0.00677   0.00152  -0.0528   0.7200   0.3593
  -1.500   0.0810   0.00670   0.00148  -0.0527   0.7051   0.3869
  -1.250   0.1081   0.00661   0.00145  -0.0525   0.6899   0.4184
  -1.000   0.1351   0.00652   0.00143  -0.0522   0.6746   0.4569
  -0.750   0.1620   0.00644   0.00142  -0.0520   0.6591   0.4984
  -0.500   0.1889   0.00637   0.00142  -0.0517   0.6435   0.5383
  -0.250   0.2161   0.00631   0.00142  -0.0515   0.6282   0.5765
   0.000   0.2432   0.00625   0.00144  -0.0512   0.6131   0.6137
   0.250   0.2702   0.00622   0.00147  -0.0510   0.5983   0.6508
   0.500   0.2972   0.00620   0.00150  -0.0507   0.5840   0.6851
   0.750   0.3240   0.00619   0.00154  -0.0503   0.5698   0.7191
   1.000   0.3507   0.00618   0.00158  -0.0500   0.5559   0.7535
   1.250   0.3775   0.00616   0.00164  -0.0496   0.5428   0.7869
   1.500   0.4040   0.00617   0.00171  -0.0491   0.5303   0.8186
   1.750   0.4303   0.00620   0.00178  -0.0486   0.5179   0.8493
   2.000   0.4563   0.00624   0.00186  -0.0480   0.5052   0.8781
   2.250   0.4823   0.00630   0.00195  -0.0473   0.4931   0.9041
   2.500   0.5081   0.00639   0.00204  -0.0467   0.4812   0.9262
   2.750   0.5347   0.00650   0.00214  -0.0462   0.4691   0.9447
   3.000   0.5634   0.00661   0.00223  -0.0461   0.4573   0.9595
   3.250   0.5934   0.00675   0.00232  -0.0465   0.4448   0.9709
   3.500   0.6256   0.00692   0.00243  -0.0473   0.4312   0.9796
   4.000   0.6973   0.00727   0.00266  -0.0508   0.3996   0.9885
   4.250   0.7327   0.00747   0.00278  -0.0525   0.3830   0.9926
   4.500   0.7713   0.00769   0.00291  -0.0549   0.3636   0.9952
   4.750   0.8116   0.00792   0.00306  -0.0577   0.3427   0.9983
   5.000   0.8451   0.00815   0.00321  -0.0590   0.3225   1.0000
   5.250   0.8660   0.00836   0.00334  -0.0577   0.3049   1.0000
   5.500   0.8866   0.00860   0.00349  -0.0563   0.2862   1.0000
   5.750   0.9070   0.00887   0.00367  -0.0548   0.2669   1.0000
   6.000   0.9274   0.00916   0.00386  -0.0534   0.2477   1.0000
   6.250   0.9481   0.00944   0.00405  -0.0520   0.2288   1.0000
   6.500   0.9688   0.00975   0.00427  -0.0506   0.2104   1.0000
   6.750   0.9896   0.01006   0.00450  -0.0493   0.1931   1.0000
   7.000   1.0106   0.01041   0.00475  -0.0481   0.1757   1.0000
   7.250   1.0316   0.01078   0.00503  -0.0468   0.1586   1.0000
   7.500   1.0532   0.01116   0.00532  -0.0457   0.1434   1.0000
   7.750   1.0749   0.01154   0.00563  -0.0447   0.1294   1.0000
   8.000   1.0966   0.01192   0.00594  -0.0437   0.1166   1.0000
   8.250   1.1184   0.01231   0.00627  -0.0427   0.1053   1.0000
   8.500   1.1401   0.01270   0.00661  -0.0417   0.0954   1.0000
   8.750   1.1616   0.01310   0.00696  -0.0407   0.0864   1.0000
   9.000   1.1828   0.01351   0.00733  -0.0396   0.0786   1.0000
   9.250   1.2032   0.01396   0.00773  -0.0385   0.0715   1.0000
   9.500   1.2244   0.01435   0.00811  -0.0375   0.0663   1.0000
   9.750   1.2446   0.01478   0.00852  -0.0363   0.0614   1.0000
  10.000   1.2640   0.01524   0.00896  -0.0350   0.0569   1.0000
  10.250   1.2830   0.01565   0.00937  -0.0336   0.0535   1.0000
  10.500   1.2998   0.01612   0.00984  -0.0319   0.0503   1.0000
  10.750   1.3165   0.01661   0.01033  -0.0302   0.0475   1.0000
  11.000   1.3335   0.01709   0.01082  -0.0286   0.0451   1.0000
  11.250   1.3477   0.01774   0.01146  -0.0266   0.0424   1.0000
  11.500   1.3654   0.01820   0.01197  -0.0253   0.0407   1.0000
  11.750   1.3809   0.01881   0.01258  -0.0237   0.0388   1.0000
  12.000   1.3935   0.01959   0.01338  -0.0218   0.0369   1.0000
  12.250   1.4099   0.02017   0.01400  -0.0204   0.0357   1.0000
  12.500   1.4244   0.02088   0.01474  -0.0189   0.0343   1.0000
  12.750   1.4365   0.02176   0.01564  -0.0173   0.0330   1.0000
  13.000   1.4478   0.02272   0.01664  -0.0156   0.0318   1.0000
  13.250   1.4617   0.02354   0.01751  -0.0144   0.0309   1.0000
  13.500   1.4738   0.02450   0.01852  -0.0130   0.0298   1.0000
  13.750   1.4837   0.02567   0.01971  -0.0116   0.0288   1.0000
  14.000   1.4897   0.02717   0.02125  -0.0101   0.0277   1.0000
  14.250   1.5016   0.02828   0.02243  -0.0091   0.0271   1.0000
  14.500   1.5116   0.02957   0.02378  -0.0081   0.0263   1.0000
  14.750   1.5197   0.03106   0.02533  -0.0071   0.0256   1.0000
  15.000   1.5256   0.03282   0.02713  -0.0062   0.0250   1.0000
  15.250   1.5271   0.03503   0.02940  -0.0053   0.0243   1.0000
  15.500   1.5299   0.03723   0.03168  -0.0046   0.0237   1.0000
  15.750   1.5359   0.03918   0.03371  -0.0042   0.0233   1.0000
  16.000   1.5399   0.04137   0.03598  -0.0039   0.0228   1.0000
  16.250   1.5426   0.04378   0.03847  -0.0037   0.0224   1.0000
  16.500   1.5437   0.04646   0.04122  -0.0037   0.0220   1.0000
  16.750   1.5428   0.04943   0.04426  -0.0038   0.0216   1.0000
  17.000   1.5388   0.05286   0.04777  -0.0041   0.0212   1.0000
  17.250   1.5312   0.05684   0.05183  -0.0047   0.0209   1.0000
  17.500   1.5180   0.06166   0.05676  -0.0057   0.0205   1.0000
  17.750   1.5153   0.06519   0.06038  -0.0064   0.0203   1.0000
  18.000   1.5119   0.06888   0.06417  -0.0073   0.0200   1.0000
  18.250   1.5058   0.07299   0.06838  -0.0084   0.0198   1.0000
  18.500   1.4989   0.07728   0.07278  -0.0096   0.0196   1.0000
  18.750   1.4897   0.08192   0.07751  -0.0110   0.0193   1.0000
  19.000   1.4802   0.08669   0.08238  -0.0125   0.0191   1.0000
  19.250   1.4697   0.09170   0.08748  -0.0143   0.0189   1.0000
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