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NACA 25112 (naca25112-jf) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 25112 (naca25112-jf)
Reynolds number: 1,000,000
Max Cl/Cd: 98.11 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca25112-jf-1000000-n5.txt
Download as CSV file: xf-naca25112-jf-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -1.2923   0.05073   0.04779  -0.0392   1.0000   0.0105
 -16.500  -1.3204   0.04425   0.04108  -0.0420   1.0000   0.0105
 -16.250  -1.3344   0.04041   0.03707  -0.0419   1.0000   0.0105
 -16.000  -1.3418   0.03763   0.03413  -0.0407   1.0000   0.0106
 -15.750  -1.3450   0.03543   0.03179  -0.0389   1.0000   0.0106
 -15.500  -1.3446   0.03363   0.02985  -0.0368   1.0000   0.0107
 -15.250  -1.3467   0.03176   0.02785  -0.0341   1.0000   0.0108
 -15.000  -1.3440   0.03026   0.02624  -0.0314   1.0000   0.0110
 -14.750  -1.3364   0.02898   0.02487  -0.0291   1.0000   0.0111
 -14.500  -1.3241   0.02783   0.02363  -0.0274   1.0000   0.0113
 -14.250  -1.3097   0.02678   0.02250  -0.0259   1.0000   0.0115
 -14.000  -1.2938   0.02582   0.02145  -0.0245   1.0000   0.0116
 -13.750  -1.2768   0.02490   0.02045  -0.0232   1.0000   0.0118
 -13.500  -1.2589   0.02404   0.01950  -0.0220   1.0000   0.0120
 -13.250  -1.2401   0.02322   0.01859  -0.0208   1.0000   0.0121
 -13.000  -1.2206   0.02243   0.01772  -0.0197   1.0000   0.0123
 -12.750  -1.2004   0.02168   0.01689  -0.0187   1.0000   0.0125
 -12.500  -1.1796   0.02097   0.01610  -0.0177   1.0000   0.0127
 -12.250  -1.1582   0.02030   0.01534  -0.0168   1.0000   0.0129
 -12.000  -1.1363   0.01966   0.01462  -0.0159   1.0000   0.0130
 -11.750  -1.1138   0.01907   0.01396  -0.0151   1.0000   0.0132
 -11.500  -1.0921   0.01837   0.01319  -0.0142   1.0000   0.0134
 -11.250  -1.0696   0.01773   0.01250  -0.0134   1.0000   0.0138
 -11.000  -1.0463   0.01719   0.01192  -0.0126   1.0000   0.0140
 -10.750  -1.0225   0.01669   0.01138  -0.0119   1.0000   0.0143
 -10.500  -0.9985   0.01622   0.01087  -0.0113   1.0000   0.0146
 -10.250  -0.9743   0.01578   0.01039  -0.0106   1.0000   0.0150
 -10.000  -0.9499   0.01537   0.00993  -0.0100   1.0000   0.0154
  -9.750  -0.9254   0.01497   0.00948  -0.0093   1.0000   0.0157
  -9.500  -0.8980   0.01457   0.00904  -0.0093   0.9947   0.0160
  -9.250  -0.8669   0.01406   0.00849  -0.0101   0.9787   0.0165
  -9.000  -0.8359   0.01364   0.00803  -0.0107   0.9562   0.0170
  -8.750  -0.8105   0.01333   0.00765  -0.0101   0.9252   0.0175
  -8.500  -0.7871   0.01308   0.00729  -0.0090   0.8926   0.0179
  -8.250  -0.7630   0.01286   0.00693  -0.0080   0.8613   0.0184
  -8.000  -0.7381   0.01264   0.00658  -0.0073   0.8328   0.0189
  -7.500  -0.6870   0.01217   0.00590  -0.0061   0.7794   0.0201
  -7.250  -0.6610   0.01196   0.00560  -0.0057   0.7556   0.0209
  -7.000  -0.6346   0.01177   0.00531  -0.0053   0.7327   0.0216
  -6.750  -0.6081   0.01159   0.00504  -0.0049   0.7105   0.0223
  -6.500  -0.5813   0.01142   0.00477  -0.0045   0.6900   0.0229
  -6.250  -0.5548   0.01120   0.00449  -0.0042   0.6703   0.0240
  -6.000  -0.5280   0.01103   0.00425  -0.0039   0.6511   0.0250
  -5.750  -0.5009   0.01088   0.00403  -0.0036   0.6336   0.0262
  -5.500  -0.4737   0.01075   0.00382  -0.0034   0.6168   0.0272
  -5.250  -0.4468   0.01057   0.00360  -0.0031   0.6002   0.0286
  -5.000  -0.4195   0.01043   0.00341  -0.0028   0.5850   0.0301
  -4.750  -0.3920   0.01031   0.00323  -0.0026   0.5711   0.0314
  -4.500  -0.3647   0.01016   0.00305  -0.0024   0.5575   0.0333
  -4.250  -0.3373   0.01004   0.00289  -0.0022   0.5448   0.0354
  -4.000  -0.3096   0.00995   0.00274  -0.0021   0.5330   0.0371
  -3.750  -0.2821   0.00981   0.00259  -0.0019   0.5217   0.0398
  -3.500  -0.2544   0.00972   0.00246  -0.0017   0.5113   0.0426
  -3.250  -0.2268   0.00961   0.00234  -0.0016   0.5013   0.0458
  -3.000  -0.1989   0.00951   0.00222  -0.0014   0.4926   0.0492
  -2.500  -0.1433   0.00934   0.00202  -0.0012   0.4753   0.0579
  -2.250  -0.1154   0.00926   0.00193  -0.0011   0.4673   0.0631
  -2.000  -0.0874   0.00918   0.00185  -0.0010   0.4599   0.0688
  -1.750  -0.0596   0.00910   0.00178  -0.0009   0.4522   0.0767
  -1.500  -0.0315   0.00903   0.00171  -0.0009   0.4459   0.0845
  -1.250  -0.0035   0.00896   0.00166  -0.0008   0.4387   0.0942
  -1.000   0.0244   0.00890   0.00161  -0.0007   0.4318   0.1062
  -0.750   0.0524   0.00882   0.00157  -0.0007   0.4257   0.1212
  -0.500   0.0803   0.00876   0.00153  -0.0006   0.4188   0.1390
  -0.250   0.1081   0.00866   0.00150  -0.0005   0.4129   0.1644
   0.000   0.1357   0.00854   0.00147  -0.0004   0.4065   0.2001
   0.250   0.1626   0.00836   0.00145  -0.0003   0.4003   0.2596
   0.500   0.1801   0.00710   0.00131   0.0013   0.3953   0.6115
   0.750   0.2029   0.00668   0.00130   0.0024   0.3891   0.7374
   1.000   0.2271   0.00647   0.00134   0.0034   0.3834   0.8150
   1.500   0.2801   0.00641   0.00146   0.0045   0.3711   0.8903
   1.750   0.3076   0.00646   0.00153   0.0048   0.3657   0.9113
   2.000   0.3353   0.00652   0.00160   0.0050   0.3594   0.9271
   2.250   0.3627   0.00663   0.00169   0.0053   0.3530   0.9413
   2.500   0.3910   0.00672   0.00179   0.0055   0.3475   0.9541
   2.750   0.4210   0.00685   0.00189   0.0052   0.3406   0.9617
   3.000   0.4502   0.00695   0.00196   0.0050   0.3348   0.9655
   3.250   0.4780   0.00704   0.00202   0.0050   0.3285   0.9696
   3.500   0.5085   0.00716   0.00210   0.0045   0.3214   0.9717
   3.750   0.5399   0.00725   0.00218   0.0037   0.3154   0.9734
   4.000   0.5710   0.00738   0.00227   0.0030   0.3079   0.9753
   4.250   0.6019   0.00750   0.00236   0.0023   0.3016   0.9774
   4.500   0.6319   0.00763   0.00246   0.0018   0.2939   0.9797
   4.750   0.6600   0.00776   0.00257   0.0017   0.2872   0.9825
   5.000   0.6916   0.00790   0.00268   0.0009   0.2788   0.9837
   5.250   0.7240   0.00805   0.00280  -0.0002   0.2710   0.9845
   5.500   0.7561   0.00822   0.00294  -0.0013   0.2617   0.9854
   5.750   0.7878   0.00838   0.00307  -0.0023   0.2526   0.9863
   6.000   0.8190   0.00858   0.00323  -0.0032   0.2419   0.9875
   6.500   0.8797   0.00903   0.00358  -0.0047   0.2177   0.9902
   6.750   0.9092   0.00928   0.00378  -0.0053   0.2050   0.9917
   7.000   0.9377   0.00956   0.00401  -0.0057   0.1915   0.9933
   7.250   0.9674   0.00986   0.00425  -0.0064   0.1773   0.9943
   7.500   0.9976   0.01020   0.00452  -0.0072   0.1625   0.9951
   7.750   1.0271   0.01057   0.00482  -0.0080   0.1475   0.9961
   8.000   1.0560   0.01099   0.00515  -0.0087   0.1316   0.9972
   8.250   1.0847   0.01141   0.00551  -0.0094   0.1168   0.9983
   8.500   1.1130   0.01187   0.00589  -0.0100   0.1024   0.9993
   8.750   1.1391   0.01233   0.00629  -0.0101   0.0894   1.0000
   9.000   1.1583   0.01277   0.00668  -0.0088   0.0787   1.0000
   9.250   1.1770   0.01322   0.00709  -0.0074   0.0694   1.0000
   9.500   1.1956   0.01368   0.00751  -0.0059   0.0615   1.0000
   9.750   1.2140   0.01413   0.00793  -0.0045   0.0544   1.0000
  10.000   1.2328   0.01456   0.00835  -0.0032   0.0489   1.0000
  10.250   1.2511   0.01502   0.00880  -0.0018   0.0443   1.0000
  10.500   1.2693   0.01548   0.00925  -0.0004   0.0401   1.0000
  10.750   1.2876   0.01594   0.00972   0.0010   0.0367   1.0000
  11.000   1.3051   0.01647   0.01024   0.0023   0.0332   1.0000
  11.250   1.3236   0.01695   0.01074   0.0035   0.0309   1.0000
  11.500   1.3411   0.01750   0.01130   0.0048   0.0286   1.0000
  11.750   1.3588   0.01804   0.01187   0.0060   0.0267   1.0000
  12.000   1.3755   0.01864   0.01249   0.0072   0.0249   1.0000
  12.250   1.3906   0.01930   0.01317   0.0086   0.0232   1.0000
  12.500   1.4041   0.01991   0.01382   0.0103   0.0221   1.0000
  12.750   1.4149   0.02064   0.01459   0.0123   0.0210   1.0000
  13.000   1.4247   0.02154   0.01553   0.0140   0.0199   1.0000
  13.250   1.4352   0.02250   0.01655   0.0153   0.0192   1.0000
  13.500   1.4455   0.02360   0.01770   0.0163   0.0184   1.0000
  13.750   1.4542   0.02492   0.01908   0.0171   0.0176   1.0000
  14.000   1.4614   0.02652   0.02073   0.0176   0.0168   1.0000
  14.250   1.4674   0.02838   0.02266   0.0178   0.0161   1.0000
  14.500   1.4745   0.03029   0.02465   0.0177   0.0157   1.0000
  14.750   1.4797   0.03249   0.02692   0.0174   0.0152   1.0000
  15.000   1.4830   0.03500   0.02952   0.0169   0.0147   1.0000
  15.250   1.4842   0.03782   0.03242   0.0162   0.0143   1.0000
  15.500   1.4832   0.04096   0.03564   0.0154   0.0139   1.0000
  15.750   1.4797   0.04442   0.03919   0.0145   0.0136   1.0000
  16.000   1.4739   0.04820   0.04305   0.0134   0.0133   1.0000
  16.250   1.4689   0.05187   0.04683   0.0124   0.0131   1.0000
  16.500   1.4619   0.05580   0.05085   0.0113   0.0129   1.0000
  16.750   1.4537   0.05990   0.05505   0.0102   0.0128   1.0000
  17.000   1.4442   0.06426   0.05951   0.0089   0.0126   1.0000
  17.250   1.4343   0.06880   0.06414   0.0074   0.0124   1.0000
  17.500   1.4239   0.07348   0.06892   0.0059   0.0122   1.0000
  17.750   1.4130   0.07829   0.07382   0.0043   0.0120   1.0000
  18.000   1.4019   0.08323   0.07885   0.0025   0.0119   1.0000
  18.250   1.3904   0.08829   0.08400   0.0007   0.0117   1.0000
  18.500   1.3784   0.09347   0.08927  -0.0012   0.0115   1.0000
  18.750   1.3663   0.09877   0.09465  -0.0033   0.0114   1.0000
  19.000   1.3541   0.10415   0.10012  -0.0054   0.0112   1.0000
  19.250   1.3416   0.10959   0.10564  -0.0076   0.0110   1.0000
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