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NACA 64(1)-112 (naca641112-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 64(1)-112 (naca641112-il)
Reynolds number: 1,000,000
Max Cl/Cd: 69.63 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca641112-il-1000000-n5.txt
Download as CSV file: xf-naca641112-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 64(1)-112                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -1.1281   0.08548   0.08302  -0.0178   1.0000   0.0070
 -17.250  -1.1591   0.07526   0.07261  -0.0242   1.0000   0.0070
 -17.000  -1.1801   0.06775   0.06494  -0.0286   1.0000   0.0070
 -16.750  -1.1947   0.06183   0.05888  -0.0319   1.0000   0.0070
 -16.500  -1.2057   0.05689   0.05382  -0.0344   1.0000   0.0071
 -16.250  -1.2161   0.05232   0.04912  -0.0364   1.0000   0.0071
 -16.000  -1.2210   0.04870   0.04538  -0.0378   1.0000   0.0072
 -15.750  -1.2202   0.04592   0.04252  -0.0387   1.0000   0.0073
 -15.500  -1.2239   0.04274   0.03922  -0.0395   1.0000   0.0073
 -15.250  -1.2236   0.04015   0.03653  -0.0399   1.0000   0.0075
 -15.000  -1.2233   0.03765   0.03391  -0.0401   1.0000   0.0075
 -14.750  -1.2199   0.03558   0.03175  -0.0400   1.0000   0.0076
 -14.500  -1.2166   0.03360   0.02966  -0.0397   1.0000   0.0077
 -14.250  -1.2124   0.03177   0.02773  -0.0392   1.0000   0.0078
 -14.000  -1.2058   0.03024   0.02611  -0.0386   1.0000   0.0080
 -13.750  -1.2005   0.02865   0.02442  -0.0377   1.0000   0.0081
 -13.500  -1.1925   0.02736   0.02304  -0.0367   1.0000   0.0082
 -13.250  -1.1830   0.02627   0.02186  -0.0356   1.0000   0.0084
 -13.000  -1.1737   0.02520   0.02070  -0.0344   1.0000   0.0085
 -12.750  -1.1651   0.02415   0.01956  -0.0328   1.0000   0.0086
 -12.500  -1.1543   0.02334   0.01866  -0.0312   1.0000   0.0087
 -12.250  -1.1443   0.02254   0.01778  -0.0292   1.0000   0.0088
 -12.000  -1.1323   0.02173   0.01688  -0.0275   1.0000   0.0090
 -11.750  -1.1197   0.02067   0.01575  -0.0260   1.0000   0.0092
 -11.500  -1.1030   0.01989   0.01490  -0.0250   1.0000   0.0095
 -11.250  -1.0844   0.01921   0.01417  -0.0241   1.0000   0.0097
 -11.000  -1.0644   0.01863   0.01355  -0.0234   1.0000   0.0099
 -10.500  -1.0231   0.01746   0.01227  -0.0220   1.0000   0.0103
 -10.250  -1.0014   0.01694   0.01170  -0.0214   1.0000   0.0105
 -10.000  -0.9746   0.01637   0.01108  -0.0219   0.9800   0.0108
  -9.750  -0.9413   0.01581   0.01045  -0.0238   0.9574   0.0112
  -9.500  -0.9164   0.01537   0.00991  -0.0236   0.9361   0.0114
  -9.250  -0.8948   0.01495   0.00937  -0.0228   0.9180   0.0116
  -9.000  -0.8727   0.01455   0.00888  -0.0220   0.9026   0.0118
  -8.500  -0.8287   0.01353   0.00768  -0.0205   0.8760   0.0125
  -8.250  -0.8049   0.01315   0.00724  -0.0200   0.8648   0.0129
  -8.000  -0.7805   0.01282   0.00685  -0.0196   0.8541   0.0134
  -7.750  -0.7557   0.01251   0.00648  -0.0193   0.8436   0.0138
  -7.500  -0.7306   0.01219   0.00609  -0.0190   0.8336   0.0142
  -7.250  -0.7053   0.01188   0.00572  -0.0187   0.8242   0.0146
  -7.000  -0.6796   0.01160   0.00537  -0.0185   0.8145   0.0150
  -6.750  -0.6536   0.01133   0.00504  -0.0184   0.8056   0.0154
  -6.500  -0.6279   0.01102   0.00467  -0.0181   0.7968   0.0162
  -6.250  -0.6015   0.01074   0.00437  -0.0180   0.7882   0.0173
  -6.000  -0.5750   0.01051   0.00410  -0.0180   0.7802   0.0183
  -5.750  -0.5481   0.01030   0.00385  -0.0179   0.7715   0.0195
  -5.500  -0.5212   0.01009   0.00360  -0.0179   0.7633   0.0210
  -5.250  -0.4943   0.00987   0.00336  -0.0178   0.7548   0.0233
  -5.000  -0.4670   0.00969   0.00315  -0.0179   0.7473   0.0251
  -4.750  -0.4396   0.00953   0.00295  -0.0179   0.7394   0.0268
  -4.500  -0.4123   0.00933   0.00275  -0.0179   0.7323   0.0302
  -4.250  -0.3847   0.00917   0.00257  -0.0180   0.7245   0.0332
  -4.000  -0.3571   0.00901   0.00239  -0.0180   0.7172   0.0383
  -3.750  -0.3295   0.00883   0.00222  -0.0181   0.7091   0.0469
  -3.250  -0.2752   0.00827   0.00186  -0.0182   0.6942   0.1049
  -3.000  -0.2485   0.00790   0.00166  -0.0183   0.6877   0.1585
  -2.750  -0.2219   0.00743   0.00145  -0.0184   0.6807   0.2321
  -2.500  -0.1954   0.00698   0.00125  -0.0185   0.6742   0.3119
  -2.250  -0.1689   0.00647   0.00107  -0.0187   0.6677   0.4050
  -2.000  -0.1416   0.00619   0.00099  -0.0188   0.6611   0.4710
  -1.750  -0.1135   0.00605   0.00095  -0.0189   0.6549   0.5075
  -1.500  -0.0854   0.00592   0.00092  -0.0191   0.6479   0.5445
  -1.250  -0.0571   0.00585   0.00091  -0.0192   0.6416   0.5714
  -1.000  -0.0284   0.00582   0.00089  -0.0194   0.6352   0.5833
  -0.500   0.0292   0.00580   0.00087  -0.0198   0.6238   0.5981
  -0.250   0.0580   0.00580   0.00086  -0.0200   0.6180   0.6046
   0.000   0.0868   0.00581   0.00086  -0.0202   0.6127   0.6110
   0.250   0.1157   0.00581   0.00087  -0.0204   0.6070   0.6165
   0.500   0.1444   0.00583   0.00088  -0.0206   0.6004   0.6222
   0.750   0.1732   0.00584   0.00090  -0.0208   0.5934   0.6282
   1.000   0.2019   0.00587   0.00092  -0.0210   0.5859   0.6338
   1.250   0.2306   0.00588   0.00096  -0.0212   0.5790   0.6402
   1.750   0.2874   0.00600   0.00103  -0.0214   0.5473   0.6536
   2.000   0.3148   0.00617   0.00107  -0.0215   0.5099   0.6606
   2.500   0.3696   0.00656   0.00123  -0.0215   0.4315   0.6742
   2.750   0.3947   0.00708   0.00143  -0.0213   0.3443   0.6807
   3.000   0.4201   0.00759   0.00167  -0.0212   0.2697   0.6880
   3.250   0.4450   0.00815   0.00194  -0.0210   0.1913   0.6947
   3.500   0.4707   0.00858   0.00219  -0.0209   0.1366   0.7024
   3.750   0.4965   0.00898   0.00242  -0.0208   0.0922   0.7099
   4.000   0.5225   0.00934   0.00266  -0.0207   0.0596   0.7182
   4.250   0.5491   0.00961   0.00288  -0.0206   0.0428   0.7258
   4.500   0.5760   0.00983   0.00309  -0.0205   0.0349   0.7339
   4.750   0.6029   0.01003   0.00329  -0.0205   0.0311   0.7412
   5.000   0.6297   0.01024   0.00352  -0.0204   0.0275   0.7493
   5.250   0.6566   0.01042   0.00374  -0.0204   0.0258   0.7568
   5.500   0.6832   0.01064   0.00397  -0.0203   0.0236   0.7656
   5.750   0.7093   0.01089   0.00425  -0.0201   0.0211   0.7740
   6.000   0.7359   0.01110   0.00450  -0.0200   0.0200   0.7829
   6.250   0.7619   0.01133   0.00477  -0.0198   0.0184   0.7914
   6.500   0.7876   0.01161   0.00506  -0.0196   0.0169   0.8003
   6.750   0.8129   0.01190   0.00540  -0.0193   0.0159   0.8098
   7.000   0.8384   0.01217   0.00573  -0.0190   0.0152   0.8192
   7.250   0.8635   0.01246   0.00607  -0.0187   0.0145   0.8295
   7.500   0.8881   0.01276   0.00643  -0.0183   0.0138   0.8398
   7.750   0.9122   0.01310   0.00680  -0.0179   0.0131   0.8506
   8.000   0.9354   0.01352   0.00729  -0.0173   0.0125   0.8621
   8.250   0.9583   0.01391   0.00776  -0.0166   0.0122   0.8748
   8.500   0.9809   0.01427   0.00820  -0.0158   0.0120   0.8886
   8.750   1.0025   0.01465   0.00868  -0.0149   0.0118   0.9043
   9.000   1.0231   0.01504   0.00915  -0.0138   0.0115   0.9223
   9.250   1.0428   0.01542   0.00964  -0.0125   0.0113   0.9455
   9.500   1.0701   0.01591   0.01022  -0.0130   0.0111   1.0000
   9.750   1.0918   0.01645   0.01079  -0.0124   0.0108   1.0000
  10.000   1.1135   0.01693   0.01131  -0.0117   0.0106   1.0000
  10.250   1.1345   0.01745   0.01186  -0.0110   0.0103   1.0000
  10.500   1.1545   0.01802   0.01248  -0.0102   0.0101   1.0000
  10.750   1.1731   0.01867   0.01317  -0.0091   0.0099   1.0000
  11.000   1.1900   0.01939   0.01395  -0.0079   0.0097   1.0000
  11.250   1.2039   0.02021   0.01483  -0.0063   0.0095   1.0000
  11.500   1.2122   0.02120   0.01590  -0.0038   0.0093   1.0000
  11.750   1.2237   0.02197   0.01675  -0.0019   0.0092   1.0000
  12.000   1.2356   0.02277   0.01762  -0.0002   0.0091   1.0000
  12.250   1.2469   0.02366   0.01858   0.0014   0.0090   1.0000
  12.500   1.2588   0.02453   0.01954   0.0028   0.0089   1.0000
  12.750   1.2686   0.02560   0.02070   0.0043   0.0088   1.0000
  13.000   1.2795   0.02662   0.02180   0.0055   0.0086   1.0000
  13.250   1.2898   0.02772   0.02298   0.0066   0.0085   1.0000
  13.500   1.2987   0.02899   0.02433   0.0076   0.0084   1.0000
  13.750   1.3066   0.03039   0.02581   0.0086   0.0082   1.0000
  14.000   1.3136   0.03192   0.02743   0.0095   0.0081   1.0000
  14.250   1.3197   0.03358   0.02919   0.0102   0.0080   1.0000
  14.500   1.3251   0.03536   0.03106   0.0108   0.0079   1.0000
  14.750   1.3288   0.03739   0.03319   0.0113   0.0078   1.0000
  15.000   1.3346   0.03924   0.03513   0.0115   0.0077   1.0000
  15.250   1.3378   0.04146   0.03744   0.0116   0.0076   1.0000
  15.500   1.3384   0.04403   0.04012   0.0116   0.0075   1.0000
  15.750   1.3386   0.04675   0.04293   0.0112   0.0074   1.0000
  16.000   1.3385   0.04961   0.04589   0.0107   0.0074   1.0000
  16.250   1.3357   0.05292   0.04930   0.0099   0.0073   1.0000
  16.500   1.3312   0.05660   0.05309   0.0088   0.0072   1.0000
  16.750   1.3286   0.06023   0.05681   0.0074   0.0071   1.0000
  17.000   1.3180   0.06518   0.06188   0.0053   0.0070   1.0000
  17.250   1.3053   0.07076   0.06761   0.0027   0.0070   1.0000
  17.500   1.2892   0.07728   0.07427  -0.0007   0.0069   1.0000
  17.750   1.2709   0.08460   0.08174  -0.0048   0.0069   1.0000
  18.000   1.2476   0.09344   0.09075  -0.0100   0.0068   1.0000
  18.250   1.2262   0.10241   0.09988  -0.0154   0.0069   1.0000
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