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NACA M2 (nacam2-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA M2 (nacam2-il)
Reynolds number: 1,000,000
Max Cl/Cd: 70.46 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-nacam2-il-1000000-n5.txt
Download as CSV file: xf-nacam2-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA M2                                         
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -1.2791   0.05164   0.04918  -0.0184   1.0000   0.0034
 -14.750  -1.3007   0.04505   0.04237  -0.0224   1.0000   0.0034
 -14.500  -1.3149   0.04075   0.03789  -0.0234   1.0000   0.0034
 -14.250  -1.3243   0.03765   0.03463  -0.0225   1.0000   0.0034
 -14.000  -1.3300   0.03529   0.03211  -0.0204   1.0000   0.0035
 -13.750  -1.3328   0.03336   0.03002  -0.0177   1.0000   0.0035
 -13.500  -1.3275   0.03156   0.02807  -0.0159   1.0000   0.0036
 -13.250  -1.3187   0.02990   0.02624  -0.0144   1.0000   0.0037
 -13.000  -1.3071   0.02840   0.02458  -0.0130   1.0000   0.0038
 -12.750  -1.2935   0.02700   0.02303  -0.0118   1.0000   0.0039
 -12.500  -1.2782   0.02570   0.02158  -0.0106   1.0000   0.0040
 -12.250  -1.2615   0.02451   0.02024  -0.0096   1.0000   0.0041
 -12.000  -1.2435   0.02340   0.01900  -0.0087   1.0000   0.0042
 -11.750  -1.2244   0.02239   0.01785  -0.0079   1.0000   0.0043
 -11.500  -1.2043   0.02146   0.01679  -0.0071   1.0000   0.0044
 -11.250  -1.1838   0.02054   0.01575  -0.0064   1.0000   0.0045
 -11.000  -1.1639   0.01944   0.01452  -0.0056   1.0000   0.0048
 -10.750  -1.1424   0.01859   0.01355  -0.0049   1.0000   0.0050
 -10.500  -1.1198   0.01785   0.01274  -0.0044   1.0000   0.0053
 -10.250  -1.0968   0.01718   0.01199  -0.0039   1.0000   0.0055
 -10.000  -1.0732   0.01656   0.01129  -0.0035   1.0000   0.0058
  -9.750  -1.0493   0.01598   0.01064  -0.0031   1.0000   0.0061
  -9.500  -1.0250   0.01545   0.01002  -0.0027   1.0000   0.0064
  -9.250  -1.0010   0.01483   0.00933  -0.0022   1.0000   0.0069
  -9.000  -0.9767   0.01425   0.00869  -0.0018   1.0000   0.0075
  -8.750  -0.9519   0.01375   0.00813  -0.0015   1.0000   0.0081
  -8.500  -0.9268   0.01329   0.00762  -0.0012   1.0000   0.0087
  -8.250  -0.9014   0.01288   0.00715  -0.0009   1.0000   0.0092
  -8.000  -0.8761   0.01244   0.00668  -0.0006   1.0000   0.0104
  -7.750  -0.8504   0.01207   0.00632  -0.0003   1.0000   0.0119
  -7.500  -0.8245   0.01174   0.00597  -0.0001   1.0000   0.0133
  -7.250  -0.7984   0.01146   0.00571   0.0001   1.0000   0.0155
  -7.000  -0.7719   0.01125   0.00551   0.0002   1.0000   0.0175
  -6.750  -0.7455   0.01105   0.00530   0.0004   1.0000   0.0187
  -6.500  -0.7189   0.01089   0.00512   0.0006   1.0000   0.0194
  -6.250  -0.6931   0.01058   0.00478   0.0009   1.0000   0.0207
  -6.000  -0.6673   0.01029   0.00447   0.0012   1.0000   0.0221
  -5.750  -0.6413   0.01006   0.00425   0.0015   1.0000   0.0233
  -5.500  -0.6156   0.00986   0.00404   0.0019   1.0000   0.0245
  -5.250  -0.5901   0.00966   0.00382   0.0023   1.0000   0.0256
  -5.000  -0.5649   0.00946   0.00361   0.0028   1.0000   0.0266
  -4.750  -0.5399   0.00929   0.00342   0.0034   1.0000   0.0275
  -4.500  -0.5089   0.00911   0.00323   0.0026   0.9982   0.0280
  -4.250  -0.4760   0.00893   0.00305   0.0013   0.9959   0.0284
  -4.000  -0.4436   0.00867   0.00275   0.0002   0.9932   0.0294
  -3.750  -0.4121   0.00843   0.00248  -0.0006   0.9889   0.0307
  -3.500  -0.3797   0.00823   0.00227  -0.0017   0.9849   0.0319
  -3.250  -0.3490   0.00806   0.00210  -0.0023   0.9788   0.0330
  -3.000  -0.3181   0.00791   0.00194  -0.0030   0.9724   0.0342
  -2.750  -0.2881   0.00777   0.00181  -0.0035   0.9642   0.0355
  -2.500  -0.2596   0.00764   0.00169  -0.0036   0.9538   0.0371
  -2.250  -0.2319   0.00754   0.00158  -0.0035   0.9418   0.0403
  -2.000  -0.2057   0.00734   0.00146  -0.0030   0.9251   0.0650
  -1.750  -0.1804   0.00713   0.00133  -0.0024   0.9016   0.1023
  -1.500  -0.1551   0.00687   0.00120  -0.0018   0.8761   0.1602
  -1.250  -0.1294   0.00649   0.00108  -0.0015   0.8546   0.2495
  -1.000  -0.1030   0.00632   0.00100  -0.0012   0.8277   0.3015
  -0.750  -0.0776   0.00623   0.00092  -0.0008   0.7748   0.3573
  -0.500  -0.0517   0.00607   0.00085  -0.0005   0.7248   0.4384
  -0.250  -0.0255   0.00587   0.00081  -0.0003   0.6828   0.5256
   0.000   0.0000   0.00577   0.00080   0.0000   0.6160   0.6157
   0.250   0.0256   0.00585   0.00081   0.0003   0.5286   0.6832
   0.500   0.0517   0.00607   0.00085   0.0005   0.4377   0.7248
   0.750   0.0773   0.00623   0.00092   0.0008   0.3549   0.7781
   1.000   0.1030   0.00630   0.00100   0.0013   0.3043   0.8290
   1.250   0.1293   0.00649   0.00108   0.0015   0.2487   0.8544
   1.500   0.1551   0.00686   0.00120   0.0018   0.1614   0.8761
   1.750   0.1803   0.00713   0.00133   0.0024   0.1017   0.9018
   2.000   0.2056   0.00735   0.00146   0.0030   0.0633   0.9251
   2.250   0.2319   0.00754   0.00158   0.0035   0.0400   0.9418
   2.500   0.2596   0.00764   0.00169   0.0036   0.0371   0.9538
   2.750   0.2881   0.00777   0.00181   0.0035   0.0355   0.9642
   3.000   0.3181   0.00791   0.00194   0.0030   0.0342   0.9725
   3.250   0.3490   0.00806   0.00210   0.0023   0.0330   0.9788
   3.500   0.3797   0.00823   0.00227   0.0017   0.0319   0.9849
   3.750   0.4121   0.00843   0.00248   0.0006   0.0307   0.9889
   4.000   0.4436   0.00867   0.00275  -0.0002   0.0294   0.9932
   4.250   0.4760   0.00893   0.00305  -0.0013   0.0284   0.9959
   4.500   0.5089   0.00911   0.00323  -0.0026   0.0281   0.9982
   4.750   0.5399   0.00929   0.00342  -0.0034   0.0275   1.0000
   5.000   0.5649   0.00947   0.00361  -0.0028   0.0267   1.0000
   5.250   0.5901   0.00965   0.00382  -0.0023   0.0256   1.0000
   5.500   0.6155   0.00986   0.00404  -0.0019   0.0245   1.0000
   5.750   0.6413   0.01006   0.00425  -0.0015   0.0233   1.0000
   6.000   0.6672   0.01029   0.00447  -0.0012   0.0221   1.0000
   6.250   0.6931   0.01058   0.00478  -0.0009   0.0207   1.0000
   6.500   0.7189   0.01089   0.00512  -0.0006   0.0194   1.0000
   6.750   0.7455   0.01105   0.00530  -0.0004   0.0187   1.0000
   7.000   0.7719   0.01125   0.00551  -0.0002   0.0175   1.0000
   7.250   0.7984   0.01146   0.00571  -0.0001   0.0155   1.0000
   7.500   0.8245   0.01174   0.00597   0.0001   0.0132   1.0000
   7.750   0.8504   0.01207   0.00631   0.0003   0.0119   1.0000
   8.000   0.8761   0.01244   0.00668   0.0006   0.0104   1.0000
   8.250   0.9014   0.01288   0.00714   0.0009   0.0092   1.0000
   8.500   0.9268   0.01329   0.00762   0.0012   0.0087   1.0000
   8.750   0.9519   0.01375   0.00812   0.0015   0.0080   1.0000
   9.000   0.9768   0.01424   0.00867   0.0018   0.0075   1.0000
   9.250   1.0010   0.01483   0.00933   0.0022   0.0069   1.0000
   9.500   1.0251   0.01545   0.01002   0.0027   0.0064   1.0000
   9.750   1.0494   0.01598   0.01063   0.0030   0.0061   1.0000
  10.000   1.0733   0.01656   0.01129   0.0035   0.0058   1.0000
  10.250   1.0968   0.01718   0.01199   0.0039   0.0055   1.0000
  10.500   1.1199   0.01785   0.01273   0.0044   0.0053   1.0000
  10.750   1.1424   0.01858   0.01355   0.0049   0.0050   1.0000
  11.000   1.1639   0.01945   0.01453   0.0056   0.0048   1.0000
  11.250   1.1838   0.02055   0.01577   0.0064   0.0045   1.0000
  11.500   1.2044   0.02145   0.01679   0.0071   0.0044   1.0000
  11.750   1.2245   0.02239   0.01785   0.0079   0.0043   1.0000
  12.000   1.2436   0.02340   0.01899   0.0087   0.0042   1.0000
  12.250   1.2616   0.02451   0.02024   0.0096   0.0041   1.0000
  12.500   1.2784   0.02570   0.02158   0.0106   0.0040   1.0000
  12.750   1.2937   0.02699   0.02302   0.0117   0.0039   1.0000
  13.000   1.3073   0.02840   0.02457   0.0130   0.0038   1.0000
  13.250   1.3189   0.02991   0.02626   0.0143   0.0037   1.0000
  13.500   1.3278   0.03156   0.02806   0.0158   0.0036   1.0000
  13.750   1.3331   0.03336   0.03002   0.0176   0.0035   1.0000
  14.000   1.3307   0.03528   0.03210   0.0203   0.0035   1.0000
  14.250   1.3250   0.03766   0.03463   0.0224   0.0034   1.0000
  14.500   1.3155   0.04076   0.03791   0.0232   0.0034   1.0000
  14.750   1.3017   0.04502   0.04235   0.0223   0.0034   1.0000
  15.000   1.2798   0.05169   0.04923   0.0182   0.0034   1.0000
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