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NACA M6 (nacam6-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA M6 (nacam6-il)
Reynolds number: 1,000,000
Max Cl/Cd: 81 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-nacam6-il-1000000-n5.txt
Download as CSV file: xf-nacam6-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA M6                                         
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -1.0670   0.05371   0.05117  -0.0565   1.0000   0.0176
 -15.500  -1.1037   0.04543   0.04263  -0.0617   1.0000   0.0176
 -15.250  -1.1172   0.04165   0.03869  -0.0621   1.0000   0.0177
 -15.000  -1.1232   0.03905   0.03595  -0.0614   1.0000   0.0179
 -14.750  -1.1266   0.03690   0.03366  -0.0600   1.0000   0.0180
 -14.500  -1.1273   0.03514   0.03177  -0.0583   1.0000   0.0181
 -14.250  -1.1288   0.03342   0.02992  -0.0560   1.0000   0.0182
 -14.000  -1.1267   0.03203   0.02840  -0.0536   1.0000   0.0183
 -13.750  -1.1229   0.03082   0.02707  -0.0510   1.0000   0.0183
 -13.500  -1.1195   0.02961   0.02575  -0.0482   1.0000   0.0185
 -13.250  -1.1190   0.02824   0.02425  -0.0449   1.0000   0.0187
 -13.000  -1.1130   0.02726   0.02319  -0.0419   1.0000   0.0189
 -12.750  -1.1053   0.02645   0.02230  -0.0390   1.0000   0.0190
 -12.500  -1.0954   0.02585   0.02166  -0.0362   1.0000   0.0191
 -12.250  -1.0866   0.02519   0.02093  -0.0331   1.0000   0.0192
 -12.000  -1.0763   0.02465   0.02034  -0.0302   1.0000   0.0193
 -11.750  -1.0626   0.02421   0.01986  -0.0279   1.0000   0.0195
 -11.500  -1.0487   0.02366   0.01924  -0.0256   1.0000   0.0196
 -11.250  -1.0350   0.02305   0.01857  -0.0232   1.0000   0.0198
 -11.000  -1.0203   0.02252   0.01798  -0.0210   1.0000   0.0199
 -10.750  -1.0067   0.02184   0.01721  -0.0185   1.0000   0.0201
 -10.500  -0.9873   0.02116   0.01646  -0.0173   0.9890   0.0203
 -10.250  -0.9560   0.02030   0.01549  -0.0186   0.9750   0.0205
 -10.000  -0.9146   0.01945   0.01455  -0.0221   0.9636   0.0208
  -9.750  -0.8692   0.01857   0.01355  -0.0265   0.9508   0.0211
  -9.500  -0.8239   0.01772   0.01258  -0.0308   0.9327   0.0214
  -9.250  -0.7905   0.01709   0.01178  -0.0323   0.9068   0.0216
  -9.000  -0.7685   0.01659   0.01113  -0.0313   0.8828   0.0218
  -8.750  -0.7484   0.01618   0.01059  -0.0298   0.8629   0.0219
  -8.500  -0.7281   0.01583   0.01011  -0.0283   0.8443   0.0221
  -8.250  -0.7079   0.01541   0.00957  -0.0268   0.8256   0.0222
  -8.000  -0.6870   0.01510   0.00915  -0.0254   0.8075   0.0223
  -7.750  -0.6657   0.01481   0.00876  -0.0241   0.7902   0.0224
  -7.500  -0.6440   0.01452   0.00837  -0.0228   0.7736   0.0225
  -7.250  -0.6241   0.01378   0.00752  -0.0213   0.7589   0.0230
  -7.000  -0.6027   0.01334   0.00699  -0.0201   0.7459   0.0232
  -6.750  -0.5806   0.01299   0.00658  -0.0189   0.7334   0.0234
  -6.500  -0.5578   0.01269   0.00622  -0.0178   0.7219   0.0236
  -6.250  -0.5349   0.01241   0.00587  -0.0168   0.7113   0.0238
  -6.000  -0.5117   0.01214   0.00554  -0.0158   0.7012   0.0240
  -5.750  -0.4881   0.01188   0.00523  -0.0149   0.6919   0.0242
  -5.500  -0.4646   0.01164   0.00493  -0.0140   0.6824   0.0245
  -5.250  -0.4406   0.01141   0.00466  -0.0131   0.6741   0.0247
  -4.750  -0.3925   0.01097   0.00413  -0.0114   0.6574   0.0252
  -4.500  -0.3684   0.01078   0.00389  -0.0106   0.6493   0.0255
  -4.250  -0.3438   0.01058   0.00366  -0.0098   0.6418   0.0257
  -4.000  -0.3194   0.01040   0.00344  -0.0090   0.6342   0.0260
  -3.750  -0.2947   0.01023   0.00323  -0.0083   0.6270   0.0262
  -3.500  -0.2699   0.01007   0.00304  -0.0076   0.6198   0.0266
  -3.250  -0.2449   0.00995   0.00289  -0.0069   0.6131   0.0270
  -3.000  -0.2197   0.00983   0.00274  -0.0062   0.6057   0.0272
  -2.750  -0.1950   0.00970   0.00258  -0.0055   0.5990   0.0276
  -2.500  -0.1701   0.00952   0.00238  -0.0048   0.5918   0.0282
  -2.250  -0.1453   0.00940   0.00222  -0.0041   0.5846   0.0288
  -2.000  -0.1200   0.00928   0.00210  -0.0034   0.5784   0.0294
  -1.750  -0.0948   0.00918   0.00198  -0.0028   0.5714   0.0301
  -1.500  -0.0696   0.00910   0.00188  -0.0021   0.5650   0.0308
  -1.250  -0.0441   0.00901   0.00179  -0.0015   0.5582   0.0318
  -1.000  -0.0188   0.00896   0.00171  -0.0009   0.5517   0.0327
  -0.750   0.0068   0.00889   0.00163  -0.0004   0.5452   0.0342
  -0.500   0.0320   0.00881   0.00156   0.0003   0.5380   0.0382
  -0.250   0.0559   0.00863   0.00150   0.0011   0.5320   0.0699
   0.000   0.0803   0.00848   0.00144   0.0019   0.5254   0.1000
   0.250   0.1042   0.00835   0.00141   0.0028   0.5181   0.1370
   0.500   0.1290   0.00824   0.00139   0.0034   0.5117   0.1644
   0.750   0.1528   0.00810   0.00137   0.0043   0.5049   0.2094
   1.000   0.1762   0.00793   0.00135   0.0052   0.4986   0.2668
   1.250   0.1876   0.00702   0.00126   0.0084   0.4918   0.5251
   1.500   0.1783   0.00584   0.00119   0.0167   0.4864   0.8462
   1.750   0.2413   0.00576   0.00122   0.0087   0.4747   0.8925
   2.000   0.3372   0.00621   0.00166  -0.0065   0.4528   0.9222
   2.250   0.3746   0.00648   0.00189  -0.0084   0.4409   0.9300
   2.500   0.3981   0.00663   0.00201  -0.0073   0.4319   0.9392
   3.000   0.4601   0.00698   0.00229  -0.0086   0.4152   0.9450
   3.250   0.4788   0.00711   0.00238  -0.0065   0.4048   0.9520
   3.500   0.5094   0.00726   0.00248  -0.0072   0.3918   0.9529
   3.750   0.5396   0.00741   0.00258  -0.0077   0.3784   0.9539
   4.000   0.5692   0.00756   0.00269  -0.0082   0.3663   0.9552
   4.250   0.5977   0.00773   0.00280  -0.0084   0.3514   0.9568
   4.500   0.6235   0.00796   0.00294  -0.0081   0.3314   0.9595
   4.750   0.6425   0.00815   0.00308  -0.0062   0.3169   0.9642
   5.000   0.6722   0.00836   0.00323  -0.0068   0.2997   0.9650
   5.250   0.7007   0.00866   0.00341  -0.0072   0.2732   0.9660
   5.500   0.7282   0.00899   0.00362  -0.0074   0.2470   0.9673
   5.750   0.7541   0.00936   0.00386  -0.0073   0.2189   0.9692
   6.000   0.7755   0.00973   0.00412  -0.0061   0.1960   0.9726
   6.250   0.7975   0.01008   0.00438  -0.0051   0.1767   0.9751
   6.500   0.8262   0.01041   0.00463  -0.0056   0.1572   0.9759
   6.750   0.8536   0.01081   0.00492  -0.0060   0.1338   0.9769
   7.000   0.8786   0.01138   0.00531  -0.0059   0.0995   0.9782
   7.250   0.9033   0.01187   0.00569  -0.0057   0.0803   0.9799
   7.500   0.9276   0.01222   0.00601  -0.0053   0.0713   0.9819
   7.750   0.9468   0.01262   0.00637  -0.0038   0.0621   0.9848
   8.000   0.9751   0.01301   0.00670  -0.0044   0.0514   0.9854
   8.250   1.0026   0.01343   0.00706  -0.0049   0.0423   0.9862
   8.500   1.0299   0.01378   0.00740  -0.0052   0.0380   0.9871
   8.750   1.0563   0.01416   0.00776  -0.0054   0.0344   0.9881
   9.000   1.0824   0.01449   0.00811  -0.0055   0.0324   0.9893
   9.250   1.1072   0.01486   0.00848  -0.0054   0.0305   0.9906
   9.500   1.1303   0.01528   0.00890  -0.0050   0.0285   0.9920
   9.750   1.1526   0.01567   0.00931  -0.0044   0.0272   0.9935
  10.000   1.1773   0.01604   0.00971  -0.0043   0.0258   0.9945
  10.250   1.2031   0.01644   0.01013  -0.0046   0.0245   0.9953
  10.500   1.2270   0.01690   0.01060  -0.0045   0.0228   0.9962
  10.750   1.2506   0.01728   0.01101  -0.0044   0.0220   0.9972
  11.000   1.2729   0.01772   0.01148  -0.0040   0.0207   0.9982
  11.250   1.2939   0.01821   0.01198  -0.0035   0.0195   0.9992
  11.500   1.3117   0.01870   0.01249  -0.0024   0.0183   1.0000
  11.750   1.3138   0.01913   0.01297   0.0019   0.0178   1.0000
  12.000   1.3175   0.01966   0.01355   0.0057   0.0171   1.0000
  12.250   1.3222   0.02030   0.01423   0.0089   0.0165   1.0000
  12.500   1.3269   0.02107   0.01503   0.0119   0.0157   1.0000
  12.750   1.3316   0.02197   0.01596   0.0146   0.0149   1.0000
  13.000   1.3381   0.02287   0.01691   0.0168   0.0145   1.0000
  13.250   1.3445   0.02386   0.01796   0.0188   0.0141   1.0000
  13.500   1.3504   0.02498   0.01913   0.0207   0.0135   1.0000
  13.750   1.3559   0.02621   0.02043   0.0224   0.0131   1.0000
  14.000   1.3606   0.02760   0.02186   0.0239   0.0126   1.0000
  14.250   1.3646   0.02914   0.02344   0.0253   0.0121   1.0000
  14.500   1.3682   0.03078   0.02514   0.0264   0.0118   1.0000
  14.750   1.3734   0.03238   0.02681   0.0274   0.0115   1.0000
  15.000   1.3770   0.03417   0.02867   0.0283   0.0112   1.0000
  15.250   1.3800   0.03607   0.03063   0.0290   0.0109   1.0000
  15.500   1.3829   0.03804   0.03267   0.0297   0.0106   1.0000
  15.750   1.3837   0.04026   0.03497   0.0302   0.0104   1.0000
  16.000   1.3839   0.04260   0.03738   0.0306   0.0101   1.0000
  16.250   1.3832   0.04508   0.03992   0.0309   0.0098   1.0000
  16.500   1.3817   0.04774   0.04265   0.0311   0.0097   1.0000
  16.750   1.3779   0.05073   0.04571   0.0310   0.0093   1.0000
  17.000   1.3761   0.05360   0.04866   0.0309   0.0094   1.0000
  17.250   1.3721   0.05682   0.05196   0.0306   0.0091   1.0000
  17.500   1.3696   0.05992   0.05514   0.0302   0.0090   1.0000
  17.750   1.3663   0.06318   0.05849   0.0296   0.0089   1.0000
  18.000   1.3597   0.06699   0.06239   0.0289   0.0088   1.0000
  18.250   1.3554   0.07055   0.06604   0.0281   0.0086   1.0000
  18.500   1.3499   0.07433   0.06991   0.0271   0.0084   1.0000
  18.750   1.3426   0.07843   0.07411   0.0260   0.0084   1.0000
  19.000   1.3346   0.08273   0.07850   0.0248   0.0083   1.0000
  19.250   1.3262   0.08715   0.08301   0.0234   0.0082   1.0000
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