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NACA 64(1)-212 MOD B (n64212mb-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: NACA 64(1)-212 MOD B (n64212mb-il)
Reynolds number: 200,000
Max Cl/Cd: 51.26 at α=10.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n64212mb-il-200000-n5.txt
Download as CSV file: xf-n64212mb-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 64(1)-212 MOD B                            
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.6950   0.07408   0.06986  -0.0360   1.0000   0.0208
 -12.000  -0.7156   0.06723   0.06290  -0.0408   1.0000   0.0207
 -11.750  -0.7440   0.06037   0.05584  -0.0452   1.0000   0.0207
 -11.500  -0.7652   0.05536   0.05063  -0.0473   1.0000   0.0206
 -11.250  -0.7845   0.05120   0.04626  -0.0479   1.0000   0.0206
 -11.000  -0.8084   0.04729   0.04204  -0.0469   1.0000   0.0208
 -10.750  -0.8252   0.04415   0.03860  -0.0445   1.0000   0.0209
 -10.500  -0.8209   0.04221   0.03657  -0.0433   1.0000   0.0211
 -10.250  -0.8134   0.04055   0.03481  -0.0421   1.0000   0.0214
 -10.000  -0.8053   0.03865   0.03276  -0.0409   1.0000   0.0216
  -9.750  -0.7960   0.03670   0.03062  -0.0396   1.0000   0.0219
  -9.500  -0.7859   0.03457   0.02826  -0.0382   1.0000   0.0221
  -9.250  -0.7736   0.03260   0.02605  -0.0368   1.0000   0.0223
  -9.000  -0.7599   0.03079   0.02402  -0.0354   1.0000   0.0225
  -8.750  -0.7450   0.02916   0.02219  -0.0339   1.0000   0.0228
  -8.500  -0.7300   0.02768   0.02052  -0.0323   1.0000   0.0232
  -8.250  -0.7152   0.02634   0.01900  -0.0305   1.0000   0.0236
  -8.000  -0.6981   0.02510   0.01760  -0.0290   0.9988   0.0239
  -7.750  -0.6665   0.02370   0.01597  -0.0303   0.9910   0.0245
  -7.500  -0.6337   0.02247   0.01464  -0.0318   0.9847   0.0252
  -7.250  -0.6020   0.02155   0.01374  -0.0332   0.9771   0.0260
  -7.000  -0.5693   0.02069   0.01282  -0.0346   0.9702   0.0270
  -6.750  -0.5374   0.01979   0.01185  -0.0357   0.9625   0.0281
  -6.500  -0.5064   0.01892   0.01091  -0.0366   0.9545   0.0289
  -6.250  -0.4755   0.01804   0.01000  -0.0375   0.9466   0.0300
  -6.000  -0.4472   0.01733   0.00931  -0.0380   0.9373   0.0311
  -5.750  -0.4175   0.01669   0.00865  -0.0386   0.9295   0.0328
  -5.500  -0.3914   0.01616   0.00805  -0.0384   0.9192   0.0346
  -5.250  -0.3648   0.01560   0.00749  -0.0383   0.9106   0.0370
  -5.000  -0.3390   0.01516   0.00702  -0.0380   0.9012   0.0402
  -4.750  -0.3135   0.01469   0.00653  -0.0377   0.8929   0.0436
  -4.500  -0.2878   0.01432   0.00612  -0.0372   0.8841   0.0486
  -4.250  -0.2624   0.01391   0.00572  -0.0368   0.8758   0.0559
  -4.000  -0.2376   0.01349   0.00532  -0.0361   0.8648   0.0685
  -3.750  -0.2138   0.01296   0.00493  -0.0354   0.8516   0.0998
  -3.500  -0.1916   0.01211   0.00448  -0.0347   0.8382   0.1942
  -3.250  -0.1716   0.01087   0.00403  -0.0340   0.8257   0.3829
  -3.000  -0.1478   0.01046   0.00397  -0.0331   0.8127   0.4955
  -2.750  -0.1220   0.01033   0.00390  -0.0323   0.7986   0.5382
  -2.500  -0.0959   0.01025   0.00386  -0.0316   0.7849   0.5766
  -2.250  -0.0708   0.01026   0.00399  -0.0304   0.7729   0.6265
  -2.000  -0.0449   0.01031   0.00408  -0.0295   0.7612   0.6560
  -1.750  -0.0172   0.01029   0.00398  -0.0291   0.7487   0.6661
  -1.500   0.0099   0.01026   0.00389  -0.0286   0.7342   0.6736
  -1.250   0.0377   0.01024   0.00376  -0.0283   0.7180   0.6812
  -1.000   0.0649   0.01022   0.00368  -0.0279   0.7004   0.6868
  -0.750   0.0922   0.01022   0.00359  -0.0275   0.6803   0.6933
  -0.500   0.1196   0.01024   0.00350  -0.0271   0.6589   0.7005
  -0.250   0.1462   0.01027   0.00345  -0.0266   0.6298   0.7068
   0.000   0.1725   0.01038   0.00336  -0.0260   0.5876   0.7141
   0.250   0.1956   0.01072   0.00328  -0.0249   0.4846   0.7205
   0.500   0.2139   0.01175   0.00348  -0.0235   0.3140   0.7275
   0.750   0.2395   0.01207   0.00362  -0.0232   0.2793   0.7355
   1.000   0.2653   0.01230   0.00376  -0.0227   0.2584   0.7428
   1.250   0.2920   0.01251   0.00387  -0.0225   0.2443   0.7514
   1.500   0.3178   0.01271   0.00402  -0.0220   0.2339   0.7583
   1.750   0.3443   0.01289   0.00416  -0.0218   0.2255   0.7668
   2.000   0.3701   0.01310   0.00433  -0.0213   0.2188   0.7744
   2.250   0.3965   0.01328   0.00449  -0.0210   0.2127   0.7835
   2.500   0.4221   0.01348   0.00468  -0.0205   0.2072   0.7918
   2.750   0.4477   0.01373   0.00488  -0.0200   0.2026   0.8015
   3.000   0.4733   0.01390   0.00509  -0.0195   0.1989   0.8100
   3.250   0.4993   0.01411   0.00531  -0.0191   0.1953   0.8197
   3.500   0.5240   0.01432   0.00553  -0.0184   0.1920   0.8288
   3.750   0.5489   0.01459   0.00578  -0.0178   0.1890   0.8392
   4.000   0.5728   0.01488   0.00606  -0.0170   0.1862   0.8497
   4.250   0.5974   0.01507   0.00632  -0.0163   0.1835   0.8603
   4.500   0.6220   0.01528   0.00657  -0.0156   0.1806   0.8719
   4.750   0.6457   0.01551   0.00685  -0.0147   0.1780   0.8842
   5.000   0.6694   0.01575   0.00712  -0.0138   0.1757   0.8973
   5.250   0.6929   0.01603   0.00740  -0.0129   0.1736   0.9121
   5.500   0.7171   0.01637   0.00773  -0.0123   0.1715   0.9286
   5.750   0.7440   0.01669   0.00810  -0.0121   0.1696   0.9473
   6.000   0.7764   0.01697   0.00846  -0.0132   0.1672   0.9693
   6.250   0.8078   0.01731   0.00885  -0.0142   0.1646   1.0000
   6.500   0.8346   0.01769   0.00926  -0.0143   0.1625   1.0000
   6.750   0.8612   0.01809   0.00968  -0.0143   0.1605   1.0000
   7.000   0.8876   0.01851   0.01011  -0.0143   0.1586   1.0000
   7.250   0.9136   0.01898   0.01056  -0.0143   0.1566   1.0000
   7.500   0.9397   0.01955   0.01112  -0.0143   0.1545   1.0000
   7.750   0.9656   0.01994   0.01165  -0.0142   0.1525   1.0000
   8.000   0.9910   0.02032   0.01212  -0.0140   0.1497   1.0000
   8.250   1.0161   0.02066   0.01253  -0.0138   0.1466   1.0000
   8.500   1.0407   0.02098   0.01289  -0.0135   0.1437   1.0000
   8.750   1.0649   0.02142   0.01331  -0.0133   0.1409   1.0000
   9.000   1.0889   0.02182   0.01383  -0.0129   0.1379   1.0000
   9.250   1.1126   0.02214   0.01429  -0.0125   0.1342   1.0000
   9.500   1.1358   0.02244   0.01467  -0.0121   0.1308   1.0000
   9.750   1.1582   0.02276   0.01501  -0.0115   0.1278   1.0000
  10.000   1.1806   0.02319   0.01556  -0.0110   0.1245   1.0000
  10.250   1.2029   0.02357   0.01609  -0.0104   0.1204   1.0000
  10.500   1.2240   0.02388   0.01648  -0.0098   0.1166   1.0000
  10.750   1.2442   0.02427   0.01692  -0.0090   0.1128   1.0000
  11.000   1.2652   0.02470   0.01753  -0.0083   0.1074   1.0000
  11.250   1.2834   0.02508   0.01793  -0.0073   0.1026   1.0000
  11.500   1.3028   0.02561   0.01861  -0.0064   0.0964   1.0000
  11.750   1.3178   0.02615   0.01918  -0.0050   0.0906   1.0000
  12.000   1.3324   0.02683   0.01994  -0.0037   0.0834   1.0000
  12.250   1.3447   0.02767   0.02082  -0.0021   0.0766   1.0000
  12.500   1.3544   0.02870   0.02188  -0.0006   0.0706   1.0000
  12.750   1.3627   0.02991   0.02314   0.0010   0.0649   1.0000
  13.000   1.3691   0.03130   0.02459   0.0025   0.0604   1.0000
  13.250   1.3736   0.03289   0.02626   0.0039   0.0566   1.0000
  13.500   1.3761   0.03467   0.02814   0.0051   0.0536   1.0000
  13.750   1.3783   0.03658   0.03017   0.0062   0.0508   1.0000
  14.000   1.3769   0.03889   0.03257   0.0070   0.0486   1.0000
  14.250   1.3734   0.04152   0.03531   0.0075   0.0468   1.0000
  14.500   1.3709   0.04424   0.03820   0.0076   0.0450   1.0000
  14.750   1.3646   0.04752   0.04162   0.0073   0.0436   1.0000
  15.000   1.3542   0.05152   0.04576   0.0064   0.0424   1.0000
  15.250   1.3398   0.05634   0.05074   0.0048   0.0416   1.0000
  15.500   1.3205   0.06234   0.05691   0.0020   0.0412   1.0000
  15.750   1.2950   0.07004   0.06480  -0.0022   0.0409   1.0000
  16.000   1.2626   0.08019   0.07519  -0.0084   0.0409   1.0000
  16.250   1.2246   0.09207   0.08730  -0.0156   0.0410   1.0000
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