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NACA 24112 (naca24112-jf) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 24112 (naca24112-jf)
Reynolds number: 1,000,000
Max Cl/Cd: 105.5 at α=7.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca24112-jf-1000000.txt
Download as CSV file: xf-naca24112-jf-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 24112                                      
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -1.1278   0.05373   0.05113  -0.0340   1.0000   0.0138
 -15.000  -1.1540   0.04708   0.04425  -0.0374   1.0000   0.0138
 -14.750  -1.1738   0.04238   0.03935  -0.0380   1.0000   0.0139
 -14.500  -1.1869   0.03896   0.03576  -0.0370   1.0000   0.0139
 -14.250  -1.1929   0.03652   0.03318  -0.0352   1.0000   0.0141
 -14.000  -1.1934   0.03471   0.03126  -0.0331   1.0000   0.0142
 -13.750  -1.1896   0.03333   0.02980  -0.0308   1.0000   0.0143
 -13.500  -1.1828   0.03222   0.02861  -0.0285   1.0000   0.0145
 -13.250  -1.1732   0.03122   0.02755  -0.0264   1.0000   0.0146
 -13.000  -1.1608   0.03014   0.02637  -0.0248   1.0000   0.0148
 -12.750  -1.1473   0.02904   0.02516  -0.0232   1.0000   0.0150
 -12.500  -1.1336   0.02782   0.02382  -0.0216   1.0000   0.0153
 -12.250  -1.1191   0.02658   0.02245  -0.0200   1.0000   0.0155
 -12.000  -1.1029   0.02544   0.02117  -0.0186   1.0000   0.0157
 -11.750  -1.0855   0.02438   0.01997  -0.0173   1.0000   0.0160
 -11.500  -1.0668   0.02343   0.01889  -0.0161   1.0000   0.0162
 -11.250  -1.0466   0.02261   0.01796  -0.0150   1.0000   0.0164
 -11.000  -1.0265   0.02174   0.01697  -0.0139   1.0000   0.0165
 -10.750  -1.0120   0.01995   0.01501  -0.0122   1.0000   0.0170
 -10.500  -0.9906   0.01923   0.01424  -0.0112   1.0000   0.0173
 -10.250  -0.9680   0.01868   0.01365  -0.0104   1.0000   0.0177
 -10.000  -0.9450   0.01815   0.01308  -0.0095   1.0000   0.0180
  -9.750  -0.9220   0.01762   0.01250  -0.0087   1.0000   0.0184
  -9.500  -0.8990   0.01707   0.01189  -0.0078   1.0000   0.0188
  -9.250  -0.8758   0.01657   0.01132  -0.0069   1.0000   0.0192
  -9.000  -0.8522   0.01618   0.01087  -0.0061   1.0000   0.0196
  -8.750  -0.8297   0.01565   0.01027  -0.0050   1.0000   0.0199
  -8.500  -0.8103   0.01475   0.00933  -0.0035   1.0000   0.0206
  -8.250  -0.7886   0.01435   0.00891  -0.0022   1.0000   0.0211
  -8.000  -0.7669   0.01400   0.00855  -0.0010   1.0000   0.0216
  -7.750  -0.7456   0.01366   0.00819   0.0004   1.0000   0.0221
  -7.500  -0.7147   0.01326   0.00776  -0.0002   0.9981   0.0228
  -7.250  -0.6789   0.01289   0.00734  -0.0019   0.9951   0.0234
  -7.000  -0.6457   0.01218   0.00661  -0.0032   0.9911   0.0243
  -6.750  -0.6116   0.01182   0.00626  -0.0045   0.9848   0.0253
  -6.500  -0.5788   0.01153   0.00597  -0.0055   0.9759   0.0264
  -6.250  -0.5473   0.01124   0.00565  -0.0061   0.9631   0.0273
  -6.000  -0.5194   0.01093   0.00528  -0.0059   0.9450   0.0281
  -5.750  -0.4955   0.01053   0.00483  -0.0049   0.9229   0.0294
  -5.500  -0.4708   0.01035   0.00460  -0.0039   0.8970   0.0306
  -5.250  -0.4457   0.01022   0.00437  -0.0031   0.8697   0.0318
  -5.000  -0.4201   0.01010   0.00414  -0.0023   0.8420   0.0329
  -4.750  -0.3952   0.00982   0.00378  -0.0016   0.8148   0.0349
  -4.500  -0.3690   0.00972   0.00358  -0.0010   0.7864   0.0366
  -4.250  -0.3423   0.00965   0.00340  -0.0006   0.7583   0.0381
  -4.000  -0.3163   0.00944   0.00311  -0.0001   0.7324   0.0407
  -3.750  -0.2894   0.00937   0.00296   0.0003   0.7060   0.0432
  -3.500  -0.2622   0.00932   0.00281   0.0006   0.6797   0.0452
  -3.250  -0.2357   0.00917   0.00260   0.0010   0.6542   0.0491
  -3.000  -0.2082   0.00913   0.00248   0.0012   0.6307   0.0523
  -2.750  -0.1813   0.00902   0.00231   0.0015   0.6066   0.0572
  -2.500  -0.1538   0.00899   0.00220   0.0017   0.5829   0.0614
  -2.250  -0.1265   0.00890   0.00207   0.0019   0.5602   0.0683
  -2.000  -0.0990   0.00886   0.00197   0.0021   0.5390   0.0754
  -1.750  -0.0715   0.00882   0.00189   0.0022   0.5182   0.0844
  -1.500  -0.0441   0.00875   0.00181   0.0024   0.4980   0.0979
  -1.250  -0.0167   0.00867   0.00174   0.0026   0.4793   0.1181
  -1.000   0.0103   0.00854   0.00167   0.0028   0.4624   0.1542
  -0.750   0.0294   0.00739   0.00145   0.0039   0.4477   0.4488
  -0.500   0.0507   0.00674   0.00137   0.0051   0.4333   0.6298
   0.000   0.0984   0.00623   0.00139   0.0071   0.4084   0.8048
   0.250   0.1242   0.00619   0.00144   0.0079   0.3974   0.8484
   0.500   0.1506   0.00623   0.00150   0.0084   0.3864   0.8791
   0.750   0.1776   0.00626   0.00156   0.0089   0.3777   0.9011
   1.000   0.2044   0.00636   0.00163   0.0094   0.3691   0.9188
   1.250   0.2317   0.00644   0.00170   0.0098   0.3614   0.9324
   1.500   0.2585   0.00657   0.00178   0.0103   0.3534   0.9444
   1.750   0.2847   0.00666   0.00187   0.0110   0.3474   0.9558
   2.000   0.3148   0.00683   0.00199   0.0108   0.3401   0.9642
   2.250   0.3449   0.00697   0.00211   0.0105   0.3339   0.9721
   2.500   0.3794   0.00710   0.00219   0.0092   0.3274   0.9744
   2.750   0.4132   0.00724   0.00228   0.0079   0.3207   0.9766
   3.000   0.4474   0.00733   0.00235   0.0066   0.3151   0.9789
   3.250   0.4783   0.00746   0.00244   0.0060   0.3090   0.9823
   3.500   0.5133   0.00758   0.00253   0.0044   0.3032   0.9837
   3.750   0.5494   0.00767   0.00260   0.0026   0.2972   0.9846
   4.000   0.5846   0.00782   0.00270   0.0010   0.2906   0.9858
   4.250   0.6197   0.00790   0.00278  -0.0006   0.2854   0.9871
   4.500   0.6540   0.00802   0.00287  -0.0021   0.2795   0.9887
   4.750   0.6875   0.00816   0.00298  -0.0034   0.2732   0.9906
   5.000   0.7204   0.00826   0.00307  -0.0045   0.2679   0.9926
   5.250   0.7532   0.00840   0.00319  -0.0057   0.2615   0.9941
   5.500   0.7878   0.00851   0.00329  -0.0073   0.2556   0.9951
   5.750   0.8221   0.00862   0.00339  -0.0088   0.2492   0.9962
   6.000   0.8557   0.00878   0.00352  -0.0102   0.2425   0.9974
   6.250   0.8893   0.00889   0.00363  -0.0115   0.2361   0.9986
   6.500   0.9223   0.00908   0.00378  -0.0128   0.2282   0.9997
   6.750   0.9494   0.00919   0.00390  -0.0128   0.2221   1.0000
   7.000   0.9726   0.00938   0.00406  -0.0121   0.2142   1.0000
   7.250   0.9963   0.00951   0.00420  -0.0114   0.2081   1.0000
   7.500   1.0191   0.00973   0.00438  -0.0105   0.1999   1.0000
   7.750   1.0423   0.00988   0.00455  -0.0097   0.1932   1.0000
   8.000   1.0646   0.01013   0.00476  -0.0088   0.1848   1.0000
   8.250   1.0873   0.01033   0.00496  -0.0079   0.1772   1.0000
   8.500   1.1093   0.01059   0.00519  -0.0070   0.1688   1.0000
   8.750   1.1310   0.01088   0.00544  -0.0060   0.1594   1.0000
   9.000   1.1528   0.01115   0.00570  -0.0050   0.1506   1.0000
   9.250   1.1739   0.01148   0.00600  -0.0039   0.1409   1.0000
   9.500   1.1945   0.01186   0.00634  -0.0028   0.1301   1.0000
   9.750   1.2148   0.01226   0.00669  -0.0017   0.1194   1.0000
  10.000   1.2350   0.01269   0.00708  -0.0005   0.1086   1.0000
  10.250   1.2548   0.01315   0.00750   0.0006   0.0979   1.0000
  10.500   1.2742   0.01364   0.00795   0.0019   0.0879   1.0000
  10.750   1.2931   0.01418   0.00845   0.0031   0.0780   1.0000
  11.000   1.3119   0.01476   0.00898   0.0043   0.0687   1.0000
  11.250   1.3305   0.01536   0.00955   0.0054   0.0606   1.0000
  11.500   1.3487   0.01601   0.01016   0.0066   0.0535   1.0000
  11.750   1.3669   0.01664   0.01079   0.0077   0.0477   1.0000
  12.000   1.3852   0.01725   0.01140   0.0088   0.0430   1.0000
  12.250   1.4020   0.01797   0.01211   0.0100   0.0386   1.0000
  12.500   1.4188   0.01864   0.01280   0.0112   0.0354   1.0000
  12.750   1.4340   0.01938   0.01357   0.0126   0.0326   1.0000
  13.000   1.4486   0.02009   0.01432   0.0140   0.0304   1.0000
  13.250   1.4562   0.02104   0.01529   0.0164   0.0282   1.0000
  13.500   1.4678   0.02180   0.01611   0.0181   0.0269   1.0000
  13.750   1.4767   0.02279   0.01715   0.0198   0.0255   1.0000
  14.000   1.4817   0.02416   0.01857   0.0214   0.0241   1.0000
  14.250   1.4887   0.02554   0.02003   0.0225   0.0231   1.0000
  14.500   1.4960   0.02703   0.02160   0.0231   0.0222   1.0000
  14.750   1.5004   0.02894   0.02358   0.0235   0.0214   1.0000
  15.000   1.5014   0.03140   0.02612   0.0234   0.0206   1.0000
  15.250   1.4968   0.03477   0.02958   0.0226   0.0199   1.0000
  15.500   1.4956   0.03796   0.03288   0.0216   0.0194   1.0000
  15.750   1.4937   0.04139   0.03643   0.0203   0.0190   1.0000
  16.000   1.4878   0.04541   0.04056   0.0188   0.0186   1.0000
  16.250   1.4785   0.04997   0.04523   0.0170   0.0183   1.0000
  16.500   1.4651   0.05507   0.05046   0.0150   0.0181   1.0000
  16.750   1.4483   0.06067   0.05618   0.0129   0.0178   1.0000
  17.000   1.4289   0.06659   0.06222   0.0107   0.0177   1.0000
  17.250   1.4084   0.07276   0.06850   0.0084   0.0175   1.0000
  17.500   1.3877   0.07908   0.07494   0.0059   0.0174   1.0000
  17.750   1.3673   0.08550   0.08146   0.0034   0.0172   1.0000
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