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NACA 63(2)-215 MOD B (n63215b-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 63(2)-215 MOD B (n63215b-il)
Reynolds number: 1,000,000
Max Cl/Cd: 83.93 at α=10°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n63215b-il-1000000-n5.txt
Download as CSV file: xf-n63215b-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63(2)-215 MOD B                            
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.1811   0.09145   0.08766  -0.0311   1.0000   0.0083
 -19.500  -1.1948   0.08553   0.08164  -0.0342   1.0000   0.0084
 -19.250  -1.2090   0.07974   0.07572  -0.0372   1.0000   0.0083
 -19.000  -1.2213   0.07437   0.07024  -0.0399   1.0000   0.0084
 -18.750  -1.2263   0.07023   0.06602  -0.0418   1.0000   0.0084
 -18.500  -1.2315   0.06616   0.06187  -0.0436   1.0000   0.0086
 -18.250  -1.2382   0.06197   0.05757  -0.0454   1.0000   0.0085
 -18.000  -1.2420   0.05831   0.05383  -0.0468   1.0000   0.0086
 -17.750  -1.2424   0.05518   0.05062  -0.0479   1.0000   0.0086
 -17.500  -1.2452   0.05181   0.04717  -0.0490   1.0000   0.0086
 -17.250  -1.2439   0.04903   0.04430  -0.0499   1.0000   0.0088
 -17.000  -1.2432   0.04625   0.04145  -0.0506   1.0000   0.0088
 -16.750  -1.2405   0.04378   0.03890  -0.0511   1.0000   0.0088
 -16.500  -1.2371   0.04151   0.03656  -0.0514   1.0000   0.0089
 -16.250  -1.2323   0.03942   0.03441  -0.0516   1.0000   0.0090
 -16.000  -1.2291   0.03721   0.03215  -0.0518   1.0000   0.0092
 -15.750  -1.2237   0.03527   0.03015  -0.0518   1.0000   0.0092
 -15.500  -1.2173   0.03348   0.02830  -0.0516   1.0000   0.0094
 -15.250  -1.2102   0.03180   0.02659  -0.0514   1.0000   0.0097
 -15.000  -1.2026   0.03019   0.02493  -0.0511   1.0000   0.0098
 -14.750  -1.1936   0.02876   0.02346  -0.0506   1.0000   0.0100
 -14.500  -1.1842   0.02740   0.02206  -0.0501   1.0000   0.0103
 -14.250  -1.1743   0.02612   0.02072  -0.0495   1.0000   0.0103
 -14.000  -1.1634   0.02496   0.01953  -0.0488   1.0000   0.0103
 -13.750  -1.1522   0.02386   0.01839  -0.0480   1.0000   0.0106
 -13.500  -1.1405   0.02284   0.01734  -0.0472   1.0000   0.0109
 -13.250  -1.1286   0.02187   0.01634  -0.0462   1.0000   0.0110
 -13.000  -1.1165   0.02098   0.01541  -0.0451   1.0000   0.0112
 -12.750  -1.1041   0.02016   0.01456  -0.0439   1.0000   0.0115
 -12.500  -1.0921   0.01937   0.01375  -0.0425   1.0000   0.0119
 -12.250  -1.0800   0.01867   0.01304  -0.0410   1.0000   0.0124
 -12.000  -1.0615   0.01800   0.01235  -0.0405   0.9767   0.0128
 -11.750  -1.0210   0.01732   0.01160  -0.0441   0.9372   0.0135
 -11.500  -1.0089   0.01691   0.01106  -0.0419   0.9042   0.0139
 -11.250  -0.9954   0.01654   0.01059  -0.0398   0.8845   0.0144
 -11.000  -0.9782   0.01614   0.01015  -0.0382   0.8696   0.0151
 -10.750  -0.9592   0.01579   0.00975  -0.0370   0.8569   0.0159
 -10.500  -0.9387   0.01545   0.00936  -0.0359   0.8458   0.0167
 -10.250  -0.9174   0.01512   0.00896  -0.0349   0.8362   0.0172
 -10.000  -0.8955   0.01478   0.00859  -0.0341   0.8273   0.0178
  -9.750  -0.8729   0.01445   0.00823  -0.0333   0.8198   0.0188
  -9.500  -0.8498   0.01412   0.00788  -0.0326   0.8122   0.0193
  -9.250  -0.8259   0.01384   0.00755  -0.0320   0.8055   0.0200
  -9.000  -0.8014   0.01355   0.00723  -0.0315   0.7982   0.0206
  -8.750  -0.7764   0.01332   0.00695  -0.0311   0.7911   0.0212
  -8.500  -0.7518   0.01299   0.00661  -0.0306   0.7839   0.0220
  -8.250  -0.7268   0.01271   0.00630  -0.0301   0.7769   0.0228
  -8.000  -0.7011   0.01244   0.00602  -0.0298   0.7709   0.0236
  -7.750  -0.6751   0.01220   0.00575  -0.0295   0.7646   0.0243
  -7.250  -0.6223   0.01174   0.00524  -0.0289   0.7532   0.0260
  -7.000  -0.5959   0.01148   0.00498  -0.0287   0.7471   0.0274
  -6.750  -0.5691   0.01127   0.00474  -0.0284   0.7414   0.0285
  -6.500  -0.5419   0.01106   0.00452  -0.0283   0.7353   0.0297
  -6.250  -0.5146   0.01087   0.00431  -0.0281   0.7288   0.0308
  -6.000  -0.4874   0.01065   0.00409  -0.0280   0.7229   0.0327
  -5.750  -0.4597   0.01045   0.00388  -0.0279   0.7172   0.0348
  -5.500  -0.4322   0.01028   0.00369  -0.0277   0.7100   0.0372
  -5.250  -0.4045   0.01008   0.00349  -0.0276   0.7002   0.0411
  -5.000  -0.3773   0.00986   0.00328  -0.0275   0.6891   0.0495
  -4.750  -0.3499   0.00962   0.00307  -0.0274   0.6779   0.0637
  -4.500  -0.3224   0.00936   0.00288  -0.0274   0.6681   0.0823
  -4.250  -0.2948   0.00910   0.00269  -0.0273   0.6580   0.1032
  -4.000  -0.2667   0.00887   0.00253  -0.0273   0.6509   0.1237
  -3.750  -0.2389   0.00861   0.00235  -0.0274   0.6432   0.1529
  -3.500  -0.2111   0.00830   0.00216  -0.0274   0.6341   0.1896
  -3.250  -0.1835   0.00795   0.00198  -0.0275   0.6255   0.2385
  -3.000  -0.1558   0.00755   0.00179  -0.0276   0.6154   0.2991
  -2.750  -0.1279   0.00720   0.00163  -0.0278   0.6021   0.3613
  -2.500  -0.0995   0.00704   0.00154  -0.0279   0.5844   0.3968
  -2.250  -0.0710   0.00692   0.00148  -0.0280   0.5676   0.4331
  -2.000  -0.0421   0.00683   0.00145  -0.0281   0.5535   0.4629
  -1.750  -0.0133   0.00684   0.00143  -0.0282   0.5330   0.4813
  -1.500   0.0150   0.00692   0.00143  -0.0282   0.4966   0.4987
  -1.250   0.0402   0.00745   0.00155  -0.0278   0.3704   0.5134
  -1.000   0.0682   0.00764   0.00162  -0.0279   0.3405   0.5244
  -0.750   0.0969   0.00774   0.00167  -0.0279   0.3212   0.5326
  -0.500   0.1257   0.00786   0.00171  -0.0280   0.3029   0.5403
  -0.250   0.1545   0.00796   0.00175  -0.0281   0.2841   0.5466
   0.000   0.1831   0.00809   0.00180  -0.0281   0.2637   0.5528
   0.250   0.2118   0.00822   0.00185  -0.0282   0.2457   0.5581
   0.500   0.2405   0.00832   0.00190  -0.0283   0.2330   0.5635
   0.750   0.2693   0.00842   0.00195  -0.0283   0.2224   0.5698
   1.250   0.3269   0.00861   0.00208  -0.0285   0.2062   0.5809
   1.500   0.3558   0.00869   0.00215  -0.0286   0.2001   0.5863
   1.750   0.3845   0.00880   0.00222  -0.0287   0.1930   0.5912
   2.000   0.4131   0.00889   0.00230  -0.0287   0.1868   0.5965
   2.250   0.4418   0.00899   0.00239  -0.0288   0.1800   0.6024
   2.750   0.4988   0.00922   0.00258  -0.0289   0.1679   0.6153
   3.000   0.5271   0.00935   0.00269  -0.0289   0.1619   0.6222
   3.250   0.5553   0.00948   0.00280  -0.0289   0.1560   0.6279
   3.500   0.5836   0.00960   0.00292  -0.0289   0.1511   0.6343
   3.750   0.6117   0.00975   0.00305  -0.0289   0.1461   0.6404
   4.000   0.6397   0.00989   0.00318  -0.0289   0.1418   0.6469
   4.250   0.6679   0.01001   0.00331  -0.0289   0.1391   0.6543
   4.500   0.6958   0.01015   0.00346  -0.0289   0.1353   0.6607
   4.750   0.7233   0.01032   0.00362  -0.0288   0.1302   0.6672
   5.000   0.7509   0.01048   0.00377  -0.0288   0.1265   0.6730
   5.250   0.7787   0.01062   0.00393  -0.0287   0.1237   0.6787
   5.500   0.8061   0.01078   0.00410  -0.0287   0.1205   0.6851
   5.750   0.8332   0.01098   0.00428  -0.0286   0.1167   0.6909
   6.000   0.8602   0.01117   0.00447  -0.0284   0.1130   0.6972
   6.250   0.8874   0.01133   0.00465  -0.0283   0.1110   0.7043
   6.500   0.9144   0.01150   0.00485  -0.0282   0.1083   0.7111
   6.750   0.9409   0.01171   0.00506  -0.0280   0.1049   0.7186
   7.000   0.9670   0.01194   0.00528  -0.0278   0.1009   0.7257
   7.250   0.9934   0.01214   0.00551  -0.0276   0.0980   0.7332
   7.500   1.0193   0.01238   0.00574  -0.0273   0.0941   0.7399
   7.750   1.0444   0.01266   0.00600  -0.0269   0.0891   0.7463
   8.000   1.0699   0.01291   0.00626  -0.0266   0.0864   0.7531
   8.250   1.0951   0.01316   0.00652  -0.0263   0.0836   0.7593
   8.500   1.1198   0.01343   0.00680  -0.0259   0.0812   0.7663
   9.000   1.1685   0.01398   0.00740  -0.0250   0.0776   0.7814
   9.250   1.1924   0.01428   0.00771  -0.0244   0.0757   0.7894
   9.500   1.2163   0.01453   0.00802  -0.0239   0.0746   0.7974
   9.750   1.2401   0.01479   0.00832  -0.0234   0.0736   0.8054
  10.000   1.2632   0.01505   0.00864  -0.0227   0.0724   0.8142
  10.250   1.2854   0.01535   0.00897  -0.0220   0.0706   0.8250
  10.500   1.3066   0.01568   0.00934  -0.0211   0.0685   0.8375
  10.750   1.3267   0.01603   0.00973  -0.0200   0.0666   0.8505
  11.000   1.3456   0.01639   0.01014  -0.0187   0.0645   0.8638
  11.250   1.3622   0.01669   0.01051  -0.0170   0.0633   0.8803
  11.500   1.3759   0.01700   0.01090  -0.0148   0.0618   0.9033
  11.750   1.3851   0.01725   0.01129  -0.0117   0.0605   0.9704
  12.000   1.4018   0.01771   0.01177  -0.0104   0.0590   1.0000
  12.250   1.4172   0.01825   0.01232  -0.0090   0.0574   1.0000
  12.500   1.4321   0.01884   0.01291  -0.0076   0.0556   1.0000
  12.750   1.4468   0.01946   0.01354  -0.0063   0.0537   1.0000
  13.000   1.4620   0.02007   0.01419  -0.0052   0.0530   1.0000
  13.250   1.4771   0.02071   0.01486  -0.0040   0.0525   1.0000
  13.500   1.4914   0.02141   0.01560  -0.0029   0.0516   1.0000
  13.750   1.5033   0.02230   0.01648  -0.0017   0.0493   1.0000
  14.000   1.5159   0.02317   0.01737  -0.0006   0.0483   1.0000
  14.250   1.5276   0.02411   0.01835   0.0004   0.0470   1.0000
  14.500   1.5391   0.02511   0.01937   0.0014   0.0453   1.0000
  14.750   1.5510   0.02609   0.02040   0.0023   0.0444   1.0000
  15.000   1.5612   0.02723   0.02157   0.0032   0.0425   1.0000
  15.250   1.5734   0.02826   0.02267   0.0039   0.0430   1.0000
  15.500   1.5735   0.03027   0.02463   0.0050   0.0368   1.0000
  15.750   1.5834   0.03155   0.02596   0.0056   0.0367   1.0000
  16.000   1.5865   0.03343   0.02787   0.0063   0.0332   1.0000
  16.250   1.5827   0.03600   0.03044   0.0069   0.0284   1.0000
  16.500   1.5850   0.03812   0.03261   0.0073   0.0268   1.0000
  16.750   1.5621   0.04281   0.03732   0.0074   0.0190   1.0000
  17.000   1.5799   0.04359   0.03818   0.0073   0.0226   1.0000
  17.250   1.5742   0.04688   0.04154   0.0070   0.0208   1.0000
  17.500   1.5295   0.05504   0.04980   0.0049   0.0121   1.0000
  17.750   1.5271   0.05854   0.05339   0.0037   0.0124   1.0000
  18.000   1.5112   0.06403   0.05901   0.0015   0.0111   1.0000
  18.250   1.4877   0.07110   0.06623  -0.0019   0.0098   1.0000
  18.500   1.4464   0.08181   0.07716  -0.0077   0.0080   1.0000
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