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NACA 25112 (naca25112-jf) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 25112 (naca25112-jf)
Reynolds number: 1,000,000
Max Cl/Cd: 109.42 at α=7.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca25112-jf-1000000.txt
Download as CSV file: xf-naca25112-jf-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 25112                                      
  
 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  -1.1781   0.04652   0.04375  -0.0398   1.0000   0.0139
 -15.000  -1.1937   0.04219   0.03925  -0.0406   1.0000   0.0140
 -14.750  -1.2025   0.03917   0.03609  -0.0398   1.0000   0.0141
 -14.500  -1.2061   0.03692   0.03371  -0.0382   1.0000   0.0142
 -14.250  -1.2070   0.03504   0.03171  -0.0361   1.0000   0.0143
 -14.000  -1.2046   0.03350   0.03006  -0.0338   1.0000   0.0144
 -13.750  -1.1998   0.03218   0.02864  -0.0313   1.0000   0.0146
 -13.500  -1.1913   0.03093   0.02728  -0.0292   1.0000   0.0148
 -13.250  -1.1797   0.02969   0.02592  -0.0275   1.0000   0.0150
 -13.000  -1.1667   0.02847   0.02458  -0.0259   1.0000   0.0152
 -12.750  -1.1523   0.02730   0.02328  -0.0244   1.0000   0.0155
 -12.500  -1.1366   0.02617   0.02201  -0.0230   1.0000   0.0157
 -12.250  -1.1194   0.02516   0.02087  -0.0217   1.0000   0.0159
 -12.000  -1.1005   0.02428   0.01987  -0.0206   1.0000   0.0160
 -11.750  -1.0865   0.02268   0.01809  -0.0189   1.0000   0.0163
 -11.500  -1.0703   0.02134   0.01663  -0.0174   1.0000   0.0167
 -11.250  -1.0495   0.02058   0.01582  -0.0164   1.0000   0.0170
 -11.000  -1.0274   0.01996   0.01515  -0.0155   1.0000   0.0173
 -10.750  -1.0048   0.01937   0.01451  -0.0147   1.0000   0.0176
 -10.500  -0.9820   0.01877   0.01384  -0.0139   1.0000   0.0180
 -10.250  -0.9590   0.01817   0.01317  -0.0131   1.0000   0.0184
 -10.000  -0.9357   0.01760   0.01251  -0.0123   1.0000   0.0187
  -9.750  -0.9119   0.01708   0.01193  -0.0116   1.0000   0.0191
  -9.500  -0.8878   0.01662   0.01140  -0.0109   1.0000   0.0194
  -9.250  -0.8676   0.01560   0.01032  -0.0097   1.0000   0.0201
  -9.000  -0.8437   0.01518   0.00988  -0.0089   1.0000   0.0206
  -8.750  -0.8198   0.01479   0.00947  -0.0081   1.0000   0.0211
  -8.500  -0.7963   0.01439   0.00904  -0.0072   1.0000   0.0217
  -8.250  -0.7735   0.01401   0.00861  -0.0062   1.0000   0.0222
  -8.000  -0.7440   0.01364   0.00819  -0.0065   0.9974   0.0227
  -7.750  -0.7105   0.01292   0.00742  -0.0079   0.9902   0.0236
  -7.500  -0.6765   0.01247   0.00697  -0.0092   0.9790   0.0245
  -7.250  -0.6441   0.01217   0.00666  -0.0101   0.9619   0.0254
  -7.000  -0.6168   0.01193   0.00636  -0.0097   0.9368   0.0264
  -6.750  -0.5927   0.01176   0.00607  -0.0086   0.9071   0.0270
  -6.500  -0.5700   0.01129   0.00550  -0.0073   0.8776   0.0282
  -6.250  -0.5451   0.01110   0.00522  -0.0065   0.8492   0.0293
  -6.000  -0.5195   0.01095   0.00495  -0.0059   0.8213   0.0304
  -5.750  -0.4931   0.01082   0.00471  -0.0054   0.7952   0.0315
  -5.500  -0.4678   0.01052   0.00431  -0.0047   0.7704   0.0332
  -5.250  -0.4411   0.01037   0.00410  -0.0043   0.7461   0.0348
  -5.000  -0.4142   0.01026   0.00388  -0.0040   0.7232   0.0364
  -4.750  -0.3878   0.01006   0.00359  -0.0035   0.7019   0.0383
  -4.500  -0.3609   0.00989   0.00338  -0.0032   0.6810   0.0406
  -4.250  -0.3334   0.00981   0.00322  -0.0030   0.6609   0.0428
  -4.000  -0.3066   0.00962   0.00298  -0.0027   0.6424   0.0459
  -3.750  -0.2793   0.00952   0.00283  -0.0024   0.6242   0.0488
  -3.500  -0.2519   0.00940   0.00265  -0.0022   0.6072   0.0523
  -3.250  -0.2245   0.00929   0.00251  -0.0020   0.5917   0.0568
  -3.000  -0.1970   0.00919   0.00236  -0.0018   0.5769   0.0612
  -2.750  -0.1695   0.00909   0.00224  -0.0016   0.5628   0.0671
  -2.500  -0.1420   0.00900   0.00212  -0.0014   0.5497   0.0742
  -2.250  -0.1141   0.00892   0.00203  -0.0013   0.5377   0.0811
  -2.000  -0.0865   0.00882   0.00193  -0.0012   0.5264   0.0918
  -1.750  -0.0589   0.00873   0.00185  -0.0010   0.5157   0.1047
  -1.500  -0.0311   0.00863   0.00178  -0.0009   0.5061   0.1203
  -1.250  -0.0036   0.00853   0.00172  -0.0008   0.4968   0.1421
  -1.000   0.0239   0.00840   0.00166  -0.0007   0.4877   0.1721
  -0.750   0.0507   0.00819   0.00160  -0.0005   0.4798   0.2252
  -0.500   0.0728   0.00740   0.00147   0.0004   0.4721   0.4316
  -0.250   0.0883   0.00628   0.00137   0.0027   0.4652   0.7327
   0.000   0.1111   0.00598   0.00140   0.0041   0.4583   0.8315
   0.250   0.1368   0.00595   0.00147   0.0049   0.4509   0.8792
   0.500   0.1637   0.00597   0.00153   0.0055   0.4444   0.9073
   0.750   0.1907   0.00604   0.00159   0.0060   0.4372   0.9261
   1.000   0.2179   0.00613   0.00167   0.0064   0.4308   0.9402
   1.250   0.2465   0.00623   0.00175   0.0066   0.4239   0.9501
   1.500   0.2743   0.00637   0.00183   0.0069   0.4168   0.9590
   1.750   0.3051   0.00648   0.00193   0.0065   0.4109   0.9659
   2.000   0.3354   0.00662   0.00202   0.0062   0.4038   0.9720
   2.250   0.3748   0.00678   0.00215   0.0038   0.3970   0.9752
   2.500   0.4184   0.00698   0.00229   0.0006   0.3893   0.9786
   2.750   0.4496   0.00712   0.00239   0.0000   0.3827   0.9831
   3.000   0.4852   0.00718   0.00243  -0.0017   0.3759   0.9838
   3.250   0.5202   0.00730   0.00249  -0.0033   0.3683   0.9847
   3.500   0.5551   0.00735   0.00254  -0.0049   0.3620   0.9856
   3.750   0.5893   0.00746   0.00260  -0.0063   0.3545   0.9868
   4.000   0.6232   0.00754   0.00267  -0.0076   0.3479   0.9882
   4.250   0.6563   0.00764   0.00274  -0.0088   0.3404   0.9897
   4.500   0.6888   0.00774   0.00282  -0.0099   0.3335   0.9914
   4.750   0.7202   0.00785   0.00291  -0.0107   0.3259   0.9932
   5.000   0.7533   0.00796   0.00300  -0.0120   0.3183   0.9943
   5.250   0.7871   0.00806   0.00308  -0.0134   0.3101   0.9952
   5.500   0.8205   0.00818   0.00317  -0.0147   0.3019   0.9961
   5.750   0.8534   0.00832   0.00328  -0.0160   0.2922   0.9972
   6.000   0.8862   0.00844   0.00339  -0.0172   0.2832   0.9983
   6.250   0.9185   0.00861   0.00352  -0.0183   0.2729   0.9993
   6.500   0.9491   0.00878   0.00365  -0.0191   0.2622   1.0000
   6.750   0.9733   0.00893   0.00379  -0.0186   0.2527   1.0000
   7.000   0.9971   0.00913   0.00395  -0.0179   0.2423   1.0000
   7.250   1.0205   0.00934   0.00413  -0.0172   0.2312   1.0000
   7.500   1.0439   0.00954   0.00431  -0.0165   0.2205   1.0000
   7.750   1.0667   0.00979   0.00452  -0.0157   0.2088   1.0000
   8.000   1.0890   0.01007   0.00476  -0.0149   0.1964   1.0000
   8.250   1.1109   0.01038   0.00502  -0.0139   0.1833   1.0000
   8.500   1.1321   0.01072   0.00530  -0.0129   0.1694   1.0000
   8.750   1.1528   0.01110   0.00562  -0.0118   0.1551   1.0000
   9.000   1.1728   0.01152   0.00597  -0.0106   0.1401   1.0000
   9.250   1.1922   0.01197   0.00635  -0.0093   0.1253   1.0000
   9.500   1.2109   0.01246   0.00677  -0.0079   0.1109   1.0000
   9.750   1.2288   0.01299   0.00723  -0.0064   0.0968   1.0000
  10.000   1.2464   0.01354   0.00771  -0.0049   0.0845   1.0000
  10.250   1.2640   0.01408   0.00820  -0.0034   0.0741   1.0000
  10.500   1.2814   0.01462   0.00870  -0.0019   0.0651   1.0000
  10.750   1.2986   0.01518   0.00923  -0.0004   0.0574   1.0000
  11.000   1.3156   0.01575   0.00978   0.0011   0.0509   1.0000
  11.250   1.3320   0.01638   0.01039   0.0026   0.0453   1.0000
  11.500   1.3495   0.01695   0.01096   0.0039   0.0413   1.0000
  11.750   1.3661   0.01758   0.01160   0.0052   0.0376   1.0000
  12.000   1.3819   0.01824   0.01227   0.0066   0.0345   1.0000
  12.250   1.3970   0.01893   0.01299   0.0080   0.0320   1.0000
  12.500   1.4104   0.01961   0.01370   0.0097   0.0300   1.0000
  12.750   1.4175   0.02053   0.01464   0.0121   0.0281   1.0000
  13.000   1.4286   0.02133   0.01551   0.0138   0.0269   1.0000
  13.250   1.4385   0.02232   0.01655   0.0152   0.0256   1.0000
  13.500   1.4453   0.02365   0.01792   0.0165   0.0244   1.0000
  13.750   1.4499   0.02533   0.01967   0.0174   0.0232   1.0000
  14.000   1.4593   0.02677   0.02119   0.0178   0.0224   1.0000
  14.250   1.4662   0.02858   0.02307   0.0180   0.0216   1.0000
  14.500   1.4701   0.03084   0.02539   0.0178   0.0208   1.0000
  14.750   1.4698   0.03371   0.02834   0.0173   0.0201   1.0000
  15.000   1.4664   0.03707   0.03179   0.0165   0.0195   1.0000
  15.250   1.4684   0.03985   0.03467   0.0158   0.0191   1.0000
  15.500   1.4674   0.04304   0.03796   0.0149   0.0187   1.0000
  15.750   1.4639   0.04652   0.04153   0.0140   0.0183   1.0000
  16.000   1.4583   0.05031   0.04541   0.0129   0.0179   1.0000
  16.250   1.4498   0.05442   0.04962   0.0118   0.0176   1.0000
  16.500   1.4392   0.05885   0.05414   0.0105   0.0173   1.0000
  16.750   1.4266   0.06360   0.05898   0.0091   0.0170   1.0000
  17.000   1.4120   0.06876   0.06424   0.0075   0.0168   1.0000
  17.250   1.3962   0.07423   0.06980   0.0056   0.0165   1.0000
  17.500   1.3781   0.08011   0.07579   0.0036   0.0163   1.0000
  17.750   1.3672   0.08509   0.08087   0.0018   0.0161   1.0000
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