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NACA M12 (nacam12-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA M12 (nacam12-il)
Reynolds number: 1,000,000
Max Cl/Cd: 71.69 at α=9.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-nacam12-il-1000000-n5.txt
Download as CSV file: xf-nacam12-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA M12                                        
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -1.3828   0.04723   0.04422  -0.0581   1.0000   0.0127
 -17.500  -1.3936   0.04362   0.04048  -0.0584   1.0000   0.0128
 -17.250  -1.3973   0.04098   0.03772  -0.0580   1.0000   0.0131
 -17.000  -1.3962   0.03889   0.03554  -0.0572   1.0000   0.0133
 -16.750  -1.3922   0.03712   0.03369  -0.0562   1.0000   0.0136
 -16.500  -1.3872   0.03550   0.03197  -0.0549   1.0000   0.0139
 -16.250  -1.3816   0.03400   0.03038  -0.0534   1.0000   0.0142
 -16.000  -1.3756   0.03263   0.02890  -0.0516   1.0000   0.0145
 -15.750  -1.3685   0.03137   0.02754  -0.0497   1.0000   0.0147
 -15.500  -1.3605   0.03022   0.02628  -0.0477   1.0000   0.0149
 -15.250  -1.3508   0.02918   0.02513  -0.0457   1.0000   0.0151
 -15.000  -1.3372   0.02818   0.02407  -0.0443   1.0000   0.0154
 -14.750  -1.3203   0.02740   0.02323  -0.0432   1.0000   0.0157
 -14.500  -1.3018   0.02675   0.02255  -0.0423   1.0000   0.0160
 -14.250  -1.2822   0.02618   0.02195  -0.0414   1.0000   0.0163
 -14.000  -1.2621   0.02565   0.02138  -0.0406   1.0000   0.0166
 -13.750  -1.2419   0.02510   0.02079  -0.0398   1.0000   0.0170
 -13.500  -1.2219   0.02453   0.02016  -0.0390   1.0000   0.0173
 -13.250  -1.2021   0.02390   0.01946  -0.0381   1.0000   0.0176
 -13.000  -1.1823   0.02326   0.01874  -0.0372   1.0000   0.0179
 -12.750  -1.1621   0.02262   0.01803  -0.0363   1.0000   0.0182
 -12.500  -1.1415   0.02202   0.01735  -0.0354   1.0000   0.0185
 -12.250  -1.1201   0.02149   0.01675  -0.0346   1.0000   0.0187
 -12.000  -1.0981   0.02103   0.01623  -0.0338   1.0000   0.0188
 -11.750  -1.0797   0.02020   0.01532  -0.0326   1.0000   0.0192
 -11.500  -1.0592   0.01963   0.01470  -0.0316   1.0000   0.0195
 -11.250  -1.0380   0.01915   0.01420  -0.0307   1.0000   0.0198
 -11.000  -1.0167   0.01876   0.01378  -0.0297   1.0000   0.0201
 -10.750  -0.9956   0.01841   0.01341  -0.0286   1.0000   0.0203
 -10.500  -0.9697   0.01801   0.01297  -0.0285   0.9985   0.0207
 -10.250  -0.9398   0.01752   0.01242  -0.0294   0.9959   0.0210
 -10.000  -0.9094   0.01704   0.01191  -0.0303   0.9931   0.0214
  -9.750  -0.8807   0.01661   0.01142  -0.0308   0.9881   0.0218
  -9.500  -0.8507   0.01611   0.01086  -0.0316   0.9834   0.0221
  -9.250  -0.8224   0.01564   0.01033  -0.0320   0.9763   0.0224
  -9.000  -0.7931   0.01524   0.00988  -0.0325   0.9686   0.0227
  -8.750  -0.7653   0.01488   0.00946  -0.0326   0.9579   0.0229
  -8.500  -0.7393   0.01451   0.00903  -0.0324   0.9448   0.0231
  -8.250  -0.7143   0.01417   0.00861  -0.0318   0.9304   0.0232
  -8.000  -0.6910   0.01364   0.00799  -0.0310   0.9161   0.0235
  -7.750  -0.6674   0.01313   0.00739  -0.0303   0.9029   0.0239
  -7.250  -0.6172   0.01244   0.00657  -0.0293   0.8783   0.0247
  -7.000  -0.5914   0.01215   0.00623  -0.0289   0.8669   0.0250
  -6.750  -0.5656   0.01188   0.00589  -0.0285   0.8552   0.0253
  -6.500  -0.5393   0.01162   0.00556  -0.0282   0.8433   0.0256
  -6.250  -0.5130   0.01137   0.00526  -0.0279   0.8319   0.0259
  -6.000  -0.4865   0.01114   0.00496  -0.0276   0.8201   0.0262
  -5.750  -0.4598   0.01092   0.00468  -0.0274   0.8081   0.0266
  -5.500  -0.4330   0.01071   0.00441  -0.0272   0.7963   0.0269
  -5.250  -0.4061   0.01051   0.00416  -0.0270   0.7850   0.0273
  -5.000  -0.3790   0.01034   0.00393  -0.0268   0.7732   0.0277
  -4.750  -0.3517   0.01017   0.00370  -0.0267   0.7621   0.0280
  -4.500  -0.3244   0.01002   0.00350  -0.0266   0.7514   0.0283
  -4.250  -0.2969   0.00988   0.00333  -0.0265   0.7403   0.0286
  -4.000  -0.2697   0.00969   0.00308  -0.0264   0.7302   0.0295
  -3.750  -0.2424   0.00953   0.00289  -0.0262   0.7196   0.0302
  -3.500  -0.2147   0.00939   0.00272  -0.0262   0.7093   0.0310
  -3.250  -0.1871   0.00927   0.00256  -0.0261   0.6992   0.0319
  -3.000  -0.1594   0.00915   0.00242  -0.0261   0.6885   0.0328
  -2.750  -0.1316   0.00905   0.00229  -0.0261   0.6782   0.0338
  -2.500  -0.1038   0.00897   0.00217  -0.0260   0.6676   0.0352
  -2.250  -0.0760   0.00885   0.00205  -0.0260   0.6564   0.0393
  -2.000  -0.0486   0.00870   0.00194  -0.0260   0.6453   0.0510
  -1.750  -0.0212   0.00856   0.00183  -0.0259   0.6338   0.0705
  -1.500   0.0074   0.00861   0.00203  -0.0261   0.6216   0.1088
  -1.250   0.0362   0.00869   0.00208  -0.0262   0.6097   0.1152
  -1.000   0.0645   0.00871   0.00204  -0.0263   0.5975   0.1180
  -0.500   0.1217   0.00885   0.00212  -0.0265   0.5724   0.1209
  -0.250   0.1502   0.00890   0.00215  -0.0266   0.5604   0.1222
   0.000   0.1784   0.00894   0.00214  -0.0267   0.5487   0.1232
   0.250   0.2066   0.00898   0.00215  -0.0267   0.5367   0.1245
   0.500   0.2351   0.00904   0.00218  -0.0269   0.5258   0.1260
   0.750   0.2633   0.00909   0.00220  -0.0269   0.5145   0.1273
   1.000   0.2913   0.00910   0.00219  -0.0270   0.5031   0.1281
   1.250   0.3193   0.00910   0.00218  -0.0270   0.4918   0.1285
   1.500   0.3471   0.00915   0.00219  -0.0271   0.4782   0.1292
   1.750   0.3747   0.00919   0.00219  -0.0271   0.4610   0.1296
   2.000   0.4023   0.00922   0.00219  -0.0271   0.4471   0.1297
   2.250   0.4300   0.00924   0.00219  -0.0271   0.4357   0.1298
   2.500   0.4578   0.00926   0.00219  -0.0271   0.4240   0.1299
   2.750   0.4855   0.00930   0.00221  -0.0272   0.4134   0.1301
   3.000   0.5131   0.00935   0.00225  -0.0272   0.4014   0.1303
   3.250   0.5407   0.00940   0.00228  -0.0272   0.3888   0.1306
   3.500   0.5683   0.00946   0.00233  -0.0272   0.3776   0.1308
   3.750   0.5953   0.00958   0.00240  -0.0271   0.3578   0.1311
   4.000   0.6213   0.00981   0.00250  -0.0269   0.3252   0.1314
   4.250   0.6473   0.01004   0.00262  -0.0268   0.2960   0.1317
   4.500   0.6728   0.01032   0.00277  -0.0265   0.2628   0.1320
   4.750   0.6984   0.01059   0.00293  -0.0263   0.2341   0.1324
   5.000   0.7243   0.01083   0.00309  -0.0261   0.2115   0.1327
   5.250   0.7499   0.01109   0.00328  -0.0258   0.1898   0.1331
   5.500   0.7756   0.01134   0.00346  -0.0256   0.1709   0.1334
   5.750   0.8012   0.01159   0.00366  -0.0253   0.1536   0.1337
   6.000   0.8266   0.01186   0.00388  -0.0251   0.1363   0.1341
   6.250   0.8511   0.01221   0.00413  -0.0247   0.1149   0.1344
   6.500   0.8753   0.01258   0.00441  -0.0242   0.0925   0.1347
   6.750   0.8991   0.01298   0.00473  -0.0238   0.0739   0.1349
   7.000   0.9235   0.01330   0.00501  -0.0233   0.0620   0.1355
   7.250   0.9481   0.01358   0.00528  -0.0230   0.0549   0.1361
   7.500   0.9729   0.01385   0.00556  -0.0226   0.0496   0.1367
   7.750   0.9972   0.01415   0.00586  -0.0222   0.0449   0.1373
   8.000   1.0217   0.01442   0.00615  -0.0218   0.0417   0.1380
   8.250   1.0460   0.01470   0.00644  -0.0214   0.0392   0.1388
   8.500   1.0697   0.01502   0.00677  -0.0208   0.0365   0.1396
   8.750   1.0936   0.01531   0.00710  -0.0204   0.0348   0.1405
   9.000   1.1174   0.01559   0.00742  -0.0199   0.0335   0.1414
   9.250   1.1406   0.01591   0.00776  -0.0193   0.0320   0.1423
   9.500   1.1631   0.01627   0.00813  -0.0187   0.0302   0.1432
   9.750   1.1851   0.01664   0.00854  -0.0179   0.0288   0.1447
  10.000   1.2077   0.01695   0.00890  -0.0173   0.0280   0.1465
  10.250   1.2296   0.01729   0.00929  -0.0166   0.0268   0.1480
  10.500   1.2505   0.01768   0.00970  -0.0157   0.0255   0.1496
  10.750   1.2703   0.01812   0.01017  -0.0147   0.0240   0.1512
  11.000   1.2901   0.01853   0.01063  -0.0137   0.0231   0.1533
  11.250   1.3095   0.01894   0.01109  -0.0126   0.0221   0.1567
  11.750   1.3398   0.01977   0.01212  -0.0090   0.0197   0.2886
  12.000   1.3547   0.01916   0.01290  -0.0076   0.0187   0.9015
  12.500   1.3851   0.02029   0.01423  -0.0046   0.0165   1.0000
  12.750   1.3980   0.02105   0.01501  -0.0030   0.0155   1.0000
  13.000   1.4111   0.02184   0.01585  -0.0016   0.0148   1.0000
  13.250   1.4237   0.02270   0.01676  -0.0002   0.0141   1.0000
  13.500   1.4355   0.02366   0.01777   0.0011   0.0134   1.0000
  13.750   1.4461   0.02474   0.01890   0.0024   0.0128   1.0000
  14.000   1.4556   0.02596   0.02016   0.0036   0.0122   1.0000
  14.250   1.4651   0.02724   0.02150   0.0047   0.0117   1.0000
  14.500   1.4746   0.02857   0.02289   0.0056   0.0113   1.0000
  14.750   1.4830   0.03005   0.02444   0.0064   0.0109   1.0000
  15.000   1.4901   0.03168   0.02615   0.0071   0.0105   1.0000
  15.250   1.4962   0.03349   0.02802   0.0077   0.0102   1.0000
  15.500   1.5008   0.03549   0.03009   0.0082   0.0098   1.0000
  15.750   1.5039   0.03771   0.03238   0.0085   0.0095   1.0000
  16.000   1.5055   0.04017   0.03492   0.0088   0.0092   1.0000
  16.250   1.5074   0.04265   0.03748   0.0088   0.0090   1.0000
  16.500   1.5087   0.04526   0.04018   0.0088   0.0089   1.0000
  16.750   1.5088   0.04808   0.04309   0.0085   0.0087   1.0000
  17.000   1.5075   0.05116   0.04627   0.0081   0.0086   1.0000
  17.250   1.5048   0.05448   0.04969   0.0075   0.0084   1.0000
  17.500   1.5012   0.05803   0.05334   0.0068   0.0083   1.0000
  17.750   1.4960   0.06190   0.05731   0.0058   0.0082   1.0000
  18.000   1.4894   0.06601   0.06152   0.0046   0.0080   1.0000
  18.250   1.4816   0.07038   0.06599   0.0033   0.0079   1.0000
  18.500   1.4721   0.07511   0.07083   0.0018   0.0078   1.0000
  18.750   1.4613   0.08009   0.07591   0.0000   0.0077   1.0000
  19.000   1.4493   0.08533   0.08125  -0.0019   0.0076   1.0000
  19.250   1.4354   0.09098   0.08702  -0.0040   0.0075   1.0000
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