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


Details Polar file
Airfoil: NACA 64(1)-212 MOD B (n64212mb-il)
Reynolds number: 1,000,000
Max Cl/Cd: 95.02 at α=9.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n64212mb-il-1000000-n5.txt
Download as CSV file: xf-n64212mb-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -1.0230   0.08491   0.08230  -0.0278   1.0000   0.0104
 -16.750  -1.0583   0.07373   0.07091  -0.0352   1.0000   0.0104
 -16.500  -1.0893   0.06453   0.06149  -0.0411   1.0000   0.0103
 -16.250  -1.0986   0.05953   0.05639  -0.0440   1.0000   0.0104
 -16.000  -1.1148   0.05395   0.05065  -0.0470   1.0000   0.0104
 -15.750  -1.1197   0.05016   0.04675  -0.0488   1.0000   0.0105
 -15.500  -1.1260   0.04641   0.04289  -0.0504   1.0000   0.0106
 -15.250  -1.1305   0.04308   0.03943  -0.0514   1.0000   0.0106
 -15.000  -1.1345   0.03997   0.03619  -0.0522   1.0000   0.0106
 -14.750  -1.1357   0.03730   0.03340  -0.0525   1.0000   0.0107
 -14.500  -1.1357   0.03488   0.03087  -0.0525   1.0000   0.0107
 -14.250  -1.1336   0.03280   0.02868  -0.0522   1.0000   0.0108
 -14.000  -1.1294   0.03101   0.02679  -0.0516   1.0000   0.0108
 -13.750  -1.1247   0.02935   0.02503  -0.0508   1.0000   0.0109
 -13.500  -1.1186   0.02790   0.02348  -0.0498   1.0000   0.0110
 -13.250  -1.1122   0.02655   0.02204  -0.0485   1.0000   0.0110
 -13.000  -1.1053   0.02535   0.02076  -0.0470   1.0000   0.0111
 -12.750  -1.0985   0.02428   0.01959  -0.0451   1.0000   0.0111
 -12.500  -1.0918   0.02332   0.01854  -0.0428   1.0000   0.0112
 -12.250  -1.0791   0.02250   0.01765  -0.0411   1.0000   0.0113
 -12.000  -1.0643   0.02164   0.01671  -0.0398   1.0000   0.0114
 -11.750  -1.0476   0.02088   0.01588  -0.0386   1.0000   0.0114
 -11.500  -1.0300   0.02013   0.01506  -0.0374   1.0000   0.0115
 -11.250  -1.0116   0.01941   0.01427  -0.0364   1.0000   0.0116
 -11.000  -0.9920   0.01880   0.01360  -0.0354   1.0000   0.0116
 -10.750  -0.9722   0.01815   0.01290  -0.0344   1.0000   0.0117
 -10.500  -0.9543   0.01730   0.01200  -0.0332   1.0000   0.0119
 -10.250  -0.9272   0.01656   0.01120  -0.0338   0.9874   0.0121
 -10.000  -0.8938   0.01590   0.01051  -0.0355   0.9743   0.0123
  -9.750  -0.8609   0.01536   0.00993  -0.0370   0.9610   0.0125
  -9.500  -0.8324   0.01490   0.00941  -0.0374   0.9452   0.0127
  -9.250  -0.8082   0.01448   0.00892  -0.0369   0.9292   0.0129
  -9.000  -0.7849   0.01408   0.00845  -0.0362   0.9149   0.0130
  -8.750  -0.7611   0.01371   0.00802  -0.0355   0.9023   0.0132
  -8.500  -0.7371   0.01335   0.00758  -0.0349   0.8911   0.0134
  -8.250  -0.7128   0.01299   0.00716  -0.0343   0.8804   0.0136
  -8.000  -0.6878   0.01264   0.00676  -0.0338   0.8706   0.0138
  -7.750  -0.6626   0.01233   0.00638  -0.0334   0.8613   0.0140
  -7.500  -0.6369   0.01201   0.00602  -0.0330   0.8525   0.0141
  -7.250  -0.6111   0.01173   0.00567  -0.0326   0.8443   0.0143
  -7.000  -0.5852   0.01139   0.00530  -0.0323   0.8359   0.0146
  -6.750  -0.5592   0.01109   0.00496  -0.0319   0.8278   0.0150
  -6.500  -0.5324   0.01083   0.00467  -0.0317   0.8204   0.0154
  -6.250  -0.5057   0.01059   0.00440  -0.0315   0.8129   0.0159
  -6.000  -0.4786   0.01037   0.00415  -0.0313   0.8045   0.0164
  -5.750  -0.4518   0.01018   0.00390  -0.0310   0.7926   0.0170
  -5.500  -0.4248   0.00999   0.00366  -0.0308   0.7781   0.0177
  -5.250  -0.3977   0.00980   0.00343  -0.0306   0.7630   0.0187
  -5.000  -0.3703   0.00964   0.00324  -0.0304   0.7508   0.0201
  -4.750  -0.3428   0.00948   0.00304  -0.0303   0.7404   0.0216
  -4.500  -0.3152   0.00933   0.00286  -0.0302   0.7272   0.0236
  -4.250  -0.2876   0.00921   0.00269  -0.0300   0.7107   0.0254
  -4.000  -0.2599   0.00909   0.00253  -0.0299   0.6948   0.0279
  -3.750  -0.2322   0.00898   0.00238  -0.0298   0.6785   0.0304
  -3.500  -0.2043   0.00888   0.00224  -0.0297   0.6622   0.0339
  -3.250  -0.1764   0.00876   0.00210  -0.0296   0.6487   0.0388
  -3.000  -0.1484   0.00865   0.00198  -0.0296   0.6333   0.0472
  -2.750  -0.1208   0.00852   0.00185  -0.0295   0.6138   0.0638
  -2.500  -0.0934   0.00831   0.00171  -0.0295   0.5917   0.1001
  -2.250  -0.0667   0.00796   0.00155  -0.0295   0.5648   0.1764
  -2.000  -0.0410   0.00761   0.00138  -0.0294   0.5144   0.2785
  -1.750  -0.0196   0.00802   0.00141  -0.0290   0.3105   0.3738
  -1.500   0.0073   0.00789   0.00139  -0.0290   0.2730   0.4498
  -1.250   0.0350   0.00785   0.00139  -0.0290   0.2475   0.4964
  -1.000   0.0627   0.00777   0.00142  -0.0290   0.2291   0.5493
  -0.750   0.0908   0.00779   0.00145  -0.0290   0.2159   0.5796
  -0.500   0.1192   0.00784   0.00148  -0.0290   0.2052   0.5930
  -0.250   0.1478   0.00789   0.00150  -0.0290   0.1979   0.6003
   0.000   0.1764   0.00796   0.00154  -0.0291   0.1907   0.6070
   0.250   0.2050   0.00804   0.00157  -0.0291   0.1847   0.6124
   0.500   0.2336   0.00809   0.00161  -0.0291   0.1796   0.6180
   0.750   0.2621   0.00817   0.00165  -0.0292   0.1748   0.6246
   1.250   0.3191   0.00830   0.00176  -0.0292   0.1683   0.6371
   1.500   0.3477   0.00837   0.00183  -0.0293   0.1657   0.6435
   1.750   0.3761   0.00845   0.00190  -0.0293   0.1631   0.6495
   2.000   0.4045   0.00853   0.00197  -0.0293   0.1603   0.6563
   2.250   0.4327   0.00863   0.00206  -0.0293   0.1571   0.6630
   2.500   0.4610   0.00872   0.00215  -0.0293   0.1545   0.6695
   2.750   0.4894   0.00879   0.00224  -0.0293   0.1532   0.6769
   3.000   0.5176   0.00887   0.00234  -0.0293   0.1517   0.6842
   3.250   0.5458   0.00896   0.00245  -0.0293   0.1500   0.6922
   3.750   0.6019   0.00916   0.00267  -0.0293   0.1463   0.7072
   4.000   0.6298   0.00928   0.00280  -0.0292   0.1444   0.7148
   4.250   0.6575   0.00941   0.00294  -0.0292   0.1422   0.7221
   4.500   0.6850   0.00956   0.00310  -0.0291   0.1401   0.7301
   4.750   0.7130   0.00965   0.00323  -0.0291   0.1392   0.7375
   5.000   0.7407   0.00976   0.00338  -0.0290   0.1382   0.7460
   5.250   0.7683   0.00988   0.00353  -0.0289   0.1371   0.7542
   5.500   0.7958   0.01000   0.00370  -0.0288   0.1358   0.7633
   5.750   0.8232   0.01013   0.00386  -0.0287   0.1343   0.7716
   6.000   0.8504   0.01027   0.00403  -0.0286   0.1328   0.7805
   6.250   0.8775   0.01042   0.00420  -0.0285   0.1309   0.7886
   6.500   0.9042   0.01059   0.00440  -0.0283   0.1283   0.7980
   6.750   0.9310   0.01075   0.00460  -0.0281   0.1259   0.8071
   7.000   0.9581   0.01086   0.00476  -0.0280   0.1240   0.8171
   7.250   0.9849   0.01100   0.00492  -0.0278   0.1210   0.8266
   7.500   1.0113   0.01117   0.00511  -0.0276   0.1182   0.8368
   7.750   1.0372   0.01135   0.00533  -0.0273   0.1154   0.8475
   8.000   1.0631   0.01153   0.00555  -0.0270   0.1134   0.8583
   8.250   1.0890   0.01168   0.00577  -0.0266   0.1112   0.8702
   8.500   1.1141   0.01185   0.00599  -0.0262   0.1081   0.8834
   8.750   1.1384   0.01206   0.00622  -0.0256   0.1037   0.8975
   9.000   1.1622   0.01225   0.00646  -0.0248   0.1000   0.9137
   9.250   1.1849   0.01247   0.00671  -0.0239   0.0945   0.9320
   9.500   1.2071   0.01271   0.00697  -0.0229   0.0886   0.9590
   9.750   1.2341   0.01311   0.00733  -0.0232   0.0793   1.0000
  10.000   1.2570   0.01363   0.00779  -0.0227   0.0688   1.0000
  10.250   1.2795   0.01419   0.00829  -0.0221   0.0601   1.0000
  10.500   1.3017   0.01475   0.00882  -0.0215   0.0535   1.0000
  10.750   1.3238   0.01530   0.00936  -0.0209   0.0481   1.0000
  11.000   1.3462   0.01579   0.00985  -0.0203   0.0441   1.0000
  11.250   1.3675   0.01637   0.01042  -0.0196   0.0401   1.0000
  11.500   1.3887   0.01691   0.01097  -0.0189   0.0366   1.0000
  11.750   1.4093   0.01748   0.01155  -0.0181   0.0338   1.0000
  12.000   1.4296   0.01803   0.01211  -0.0172   0.0315   1.0000
  12.250   1.4486   0.01865   0.01275  -0.0163   0.0294   1.0000
  12.500   1.4679   0.01919   0.01333  -0.0153   0.0280   1.0000
  12.750   1.4854   0.01980   0.01397  -0.0141   0.0264   1.0000
  13.000   1.4996   0.02046   0.01466  -0.0124   0.0250   1.0000
  13.250   1.5136   0.02106   0.01531  -0.0106   0.0240   1.0000
  13.500   1.5262   0.02173   0.01603  -0.0088   0.0229   1.0000
  13.750   1.5373   0.02252   0.01686  -0.0070   0.0218   1.0000
  14.000   1.5474   0.02340   0.01778  -0.0052   0.0208   1.0000
  14.250   1.5587   0.02422   0.01867  -0.0036   0.0202   1.0000
  14.500   1.5688   0.02517   0.01968  -0.0021   0.0195   1.0000
  14.750   1.5775   0.02624   0.02081  -0.0006   0.0188   1.0000
  15.000   1.5844   0.02749   0.02211   0.0009   0.0180   1.0000
  15.250   1.5904   0.02887   0.02355   0.0022   0.0175   1.0000
  15.500   1.5973   0.03022   0.02498   0.0033   0.0170   1.0000
  15.750   1.6028   0.03175   0.02659   0.0043   0.0165   1.0000
  16.000   1.6069   0.03346   0.02839   0.0052   0.0161   1.0000
  16.250   1.6087   0.03547   0.03048   0.0059   0.0156   1.0000
  16.500   1.6089   0.03772   0.03281   0.0064   0.0152   1.0000
  16.750   1.6064   0.04037   0.03554   0.0066   0.0148   1.0000
  17.000   1.6021   0.04336   0.03864   0.0065   0.0145   1.0000
  17.250   1.5957   0.04677   0.04216   0.0060   0.0143   1.0000
  17.500   1.5883   0.05051   0.04603   0.0051   0.0141   1.0000
  17.750   1.5760   0.05515   0.05081   0.0035   0.0140   1.0000
  18.000   1.5563   0.06130   0.05712   0.0007   0.0139   1.0000
  18.250   1.5223   0.07058   0.06662  -0.0044   0.0139   1.0000
  18.500   1.4092   0.09700   0.09354  -0.0203   0.0148   1.0000
  18.750   1.3156   0.11876   0.11563  -0.0333   0.0155   1.0000
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