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NACA 64(1)-212 MOD B (n64212mb-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 64(1)-212 MOD B (n64212mb-il)
Reynolds number: 500,000
Max Cl/Cd: 76.46 at α=9.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n64212mb-il-500000-n5.txt
Download as CSV file: xf-n64212mb-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.8813   0.06298   0.05973  -0.0414   1.0000   0.0133
 -13.750  -0.9140   0.05486   0.05135  -0.0464   1.0000   0.0133
 -13.500  -0.9352   0.04920   0.04545  -0.0491   1.0000   0.0133
 -13.250  -0.9501   0.04481   0.04085  -0.0505   1.0000   0.0134
 -13.000  -0.9621   0.04110   0.03693  -0.0509   1.0000   0.0134
 -12.750  -0.9693   0.03810   0.03374  -0.0507   1.0000   0.0135
 -12.500  -0.9744   0.03549   0.03092  -0.0498   1.0000   0.0135
 -12.250  -0.9757   0.03338   0.02864  -0.0485   1.0000   0.0137
 -12.000  -0.9760   0.03145   0.02652  -0.0468   1.0000   0.0138
 -11.750  -0.9737   0.02991   0.02482  -0.0446   1.0000   0.0139
 -11.500  -0.9672   0.02843   0.02316  -0.0426   1.0000   0.0140
 -11.250  -0.9558   0.02707   0.02165  -0.0412   1.0000   0.0141
 -11.000  -0.9420   0.02587   0.02031  -0.0399   1.0000   0.0142
 -10.750  -0.9266   0.02474   0.01903  -0.0387   1.0000   0.0143
 -10.500  -0.9111   0.02354   0.01772  -0.0374   1.0000   0.0145
 -10.250  -0.8938   0.02261   0.01674  -0.0364   1.0000   0.0148
 -10.000  -0.8752   0.02182   0.01591  -0.0353   1.0000   0.0149
  -9.750  -0.8561   0.02112   0.01517  -0.0343   1.0000   0.0151
  -9.500  -0.8370   0.02045   0.01446  -0.0332   1.0000   0.0154
  -9.250  -0.8143   0.01970   0.01365  -0.0328   0.9969   0.0156
  -9.000  -0.7834   0.01886   0.01274  -0.0340   0.9850   0.0158
  -8.750  -0.7518   0.01807   0.01188  -0.0354   0.9745   0.0161
  -8.500  -0.7202   0.01732   0.01106  -0.0366   0.9639   0.0165
  -8.250  -0.6899   0.01662   0.01028  -0.0375   0.9527   0.0168
  -8.000  -0.6618   0.01601   0.00959  -0.0379   0.9406   0.0170
  -7.750  -0.6359   0.01548   0.00898  -0.0377   0.9281   0.0173
  -7.500  -0.6124   0.01492   0.00836  -0.0371   0.9154   0.0176
  -7.250  -0.5888   0.01443   0.00784  -0.0364   0.9041   0.0180
  -7.000  -0.5646   0.01403   0.00738  -0.0358   0.8938   0.0184
  -6.750  -0.5401   0.01365   0.00696  -0.0352   0.8835   0.0189
  -6.500  -0.5152   0.01328   0.00654  -0.0347   0.8743   0.0195
  -6.250  -0.4900   0.01295   0.00615  -0.0342   0.8654   0.0202
  -6.000  -0.4644   0.01263   0.00577  -0.0338   0.8570   0.0210
  -5.750  -0.4389   0.01227   0.00540  -0.0334   0.8483   0.0220
  -5.500  -0.4128   0.01198   0.00508  -0.0330   0.8405   0.0231
  -5.250  -0.3865   0.01172   0.00476  -0.0327   0.8315   0.0244
  -5.000  -0.3604   0.01143   0.00443  -0.0323   0.8194   0.0259
  -4.750  -0.3343   0.01120   0.00414  -0.0319   0.8055   0.0278
  -4.500  -0.3078   0.01100   0.00387  -0.0315   0.7925   0.0299
  -4.250  -0.2810   0.01076   0.00362  -0.0312   0.7800   0.0328
  -4.000  -0.2539   0.01057   0.00338  -0.0310   0.7676   0.0362
  -3.750  -0.2269   0.01038   0.00316  -0.0307   0.7548   0.0415
  -3.500  -0.1999   0.01017   0.00295  -0.0305   0.7408   0.0508
  -3.250  -0.1729   0.00990   0.00274  -0.0303   0.7280   0.0719
  -3.000  -0.1464   0.00952   0.00251  -0.0302   0.7139   0.1202
  -2.750  -0.1206   0.00896   0.00224  -0.0301   0.6992   0.2098
  -2.500  -0.0955   0.00818   0.00193  -0.0301   0.6849   0.3472
  -2.250  -0.0694   0.00771   0.00180  -0.0300   0.6694   0.4596
  -2.000  -0.0418   0.00760   0.00175  -0.0299   0.6520   0.4992
  -1.750  -0.0142   0.00752   0.00171  -0.0297   0.6334   0.5347
  -1.500   0.0127   0.00746   0.00174  -0.0294   0.6092   0.5860
  -1.250   0.0397   0.00756   0.00175  -0.0291   0.5730   0.6125
  -1.000   0.0657   0.00781   0.00174  -0.0286   0.5006   0.6224
  -0.750   0.0875   0.00877   0.00194  -0.0279   0.3074   0.6297
  -0.250   0.1426   0.00913   0.00204  -0.0277   0.2477   0.6415
   0.000   0.1706   0.00927   0.00208  -0.0277   0.2311   0.6478
   0.250   0.1985   0.00937   0.00213  -0.0276   0.2187   0.6542
   0.500   0.2266   0.00947   0.00218  -0.0276   0.2096   0.6612
   0.750   0.2546   0.00959   0.00225  -0.0276   0.2021   0.6674
   1.000   0.2826   0.00967   0.00232  -0.0275   0.1957   0.6742
   1.250   0.3106   0.00980   0.00239  -0.0275   0.1895   0.6812
   1.500   0.3385   0.00990   0.00249  -0.0274   0.1851   0.6878
   1.750   0.3665   0.00999   0.00258  -0.0273   0.1816   0.6953
   2.000   0.3944   0.01010   0.00268  -0.0273   0.1780   0.7027
   2.250   0.4220   0.01022   0.00280  -0.0272   0.1745   0.7107
   2.500   0.4496   0.01038   0.00293  -0.0271   0.1712   0.7183
   2.750   0.4773   0.01048   0.00307  -0.0270   0.1691   0.7259
   3.000   0.5051   0.01060   0.00320  -0.0269   0.1669   0.7339
   3.250   0.5325   0.01071   0.00334  -0.0267   0.1643   0.7414
   3.500   0.5600   0.01085   0.00349  -0.0266   0.1617   0.7497
   3.750   0.5871   0.01100   0.00366  -0.0264   0.1595   0.7577
   4.000   0.6140   0.01118   0.00384  -0.0263   0.1573   0.7668
   4.250   0.6405   0.01139   0.00406  -0.0260   0.1549   0.7753
   4.500   0.6677   0.01153   0.00425  -0.0258   0.1538   0.7844
   4.750   0.6945   0.01167   0.00445  -0.0256   0.1525   0.7928
   5.000   0.7214   0.01183   0.00465  -0.0254   0.1509   0.8019
   5.250   0.7479   0.01198   0.00486  -0.0251   0.1490   0.8109
   5.750   0.8003   0.01234   0.00529  -0.0244   0.1454   0.8305
   6.000   0.8261   0.01255   0.00554  -0.0241   0.1438   0.8404
   6.250   0.8512   0.01279   0.00581  -0.0236   0.1421   0.8513
   6.500   0.8755   0.01308   0.00614  -0.0229   0.1402   0.8621
   6.750   0.9009   0.01323   0.00638  -0.0224   0.1391   0.8738
   7.000   0.9257   0.01339   0.00662  -0.0218   0.1377   0.8867
   7.250   0.9498   0.01352   0.00683  -0.0211   0.1355   0.9008
   7.500   0.9735   0.01364   0.00701  -0.0202   0.1326   0.9170
   7.750   0.9964   0.01379   0.00720  -0.0193   0.1300   0.9360
   8.250   1.0524   0.01420   0.00769  -0.0197   0.1244   1.0000
   8.500   1.0788   0.01443   0.00796  -0.0196   0.1219   1.0000
   8.750   1.1048   0.01467   0.00822  -0.0195   0.1190   1.0000
   9.000   1.1302   0.01494   0.00849  -0.0193   0.1159   1.0000
   9.250   1.1553   0.01524   0.00881  -0.0190   0.1130   1.0000
   9.500   1.1808   0.01549   0.00912  -0.0188   0.1094   1.0000
   9.750   1.2057   0.01577   0.00941  -0.0185   0.1047   1.0000
  10.000   1.2300   0.01610   0.00975  -0.0182   0.1002   1.0000
  10.250   1.2539   0.01645   0.01010  -0.0178   0.0937   1.0000
  10.500   1.2770   0.01685   0.01051  -0.0173   0.0870   1.0000
  10.750   1.2988   0.01737   0.01099  -0.0167   0.0782   1.0000
  11.000   1.3193   0.01799   0.01157  -0.0159   0.0690   1.0000
  11.250   1.3384   0.01870   0.01225  -0.0150   0.0607   1.0000
  11.500   1.3566   0.01946   0.01300  -0.0140   0.0545   1.0000
  11.750   1.3748   0.02016   0.01373  -0.0130   0.0496   1.0000
  12.000   1.3916   0.02091   0.01450  -0.0118   0.0459   1.0000
  12.250   1.4061   0.02165   0.01528  -0.0102   0.0424   1.0000
  12.500   1.4190   0.02245   0.01612  -0.0085   0.0397   1.0000
  12.750   1.4315   0.02325   0.01698  -0.0068   0.0372   1.0000
  13.000   1.4417   0.02423   0.01799  -0.0050   0.0349   1.0000
  13.250   1.4531   0.02512   0.01896  -0.0034   0.0332   1.0000
  13.500   1.4628   0.02616   0.02006  -0.0019   0.0315   1.0000
  13.750   1.4706   0.02737   0.02133  -0.0003   0.0301   1.0000
  14.000   1.4782   0.02862   0.02267   0.0011   0.0290   1.0000
  14.250   1.4857   0.02992   0.02407   0.0023   0.0279   1.0000
  14.500   1.4914   0.03143   0.02566   0.0035   0.0269   1.0000
  14.750   1.4950   0.03317   0.02749   0.0045   0.0260   1.0000
  15.000   1.4952   0.03530   0.02970   0.0054   0.0250   1.0000
  15.250   1.4975   0.03734   0.03185   0.0060   0.0243   1.0000
  15.500   1.4984   0.03962   0.03425   0.0064   0.0237   1.0000
  15.750   1.4966   0.04229   0.03704   0.0064   0.0231   1.0000
  16.000   1.4920   0.04544   0.04030   0.0061   0.0226   1.0000
  16.250   1.4834   0.04924   0.04424   0.0053   0.0221   1.0000
  16.500   1.4712   0.05381   0.04896   0.0038   0.0217   1.0000
  16.750   1.4525   0.05970   0.05501   0.0013   0.0215   1.0000
  17.000   1.4264   0.06752   0.06304  -0.0029   0.0215   1.0000
  17.250   1.3834   0.08003   0.07584  -0.0105   0.0218   1.0000
  17.500   1.3243   0.09586   0.09196  -0.0197   0.0222   1.0000
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