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MRC-16 (mrc-16-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MRC-16 (mrc-16-il)
Reynolds number: 1,000,000
Max Cl/Cd: 110.31 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mrc-16-il-1000000-n5.txt
Download as CSV file: xf-mrc-16-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MRC-16                                          
  
 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  -0.9601   0.05714   0.05446  -0.0703   1.0000   0.0073
 -15.500  -0.9949   0.04632   0.04339  -0.0794   1.0000   0.0073
 -15.250  -1.0103   0.04045   0.03733  -0.0838   1.0000   0.0073
 -15.000  -1.0184   0.03654   0.03327  -0.0859   1.0000   0.0073
 -14.750  -1.0224   0.03366   0.03026  -0.0866   1.0000   0.0074
 -14.500  -1.0239   0.03144   0.02792  -0.0862   1.0000   0.0075
 -14.250  -1.0240   0.02966   0.02603  -0.0849   1.0000   0.0075
 -14.000  -1.0251   0.02824   0.02450  -0.0826   1.0000   0.0076
 -13.750  -1.0147   0.02685   0.02300  -0.0820   0.9950   0.0077
 -13.500  -0.9979   0.02553   0.02156  -0.0821   0.9870   0.0078
 -13.250  -0.9789   0.02435   0.02025  -0.0823   0.9799   0.0079
 -13.000  -0.9592   0.02327   0.01905  -0.0823   0.9720   0.0080
 -12.750  -0.9406   0.02231   0.01798  -0.0817   0.9633   0.0081
 -12.500  -0.9217   0.02146   0.01701  -0.0811   0.9549   0.0082
 -12.250  -0.9034   0.02068   0.01612  -0.0801   0.9458   0.0083
 -12.000  -0.8841   0.01996   0.01528  -0.0792   0.9377   0.0084
 -11.750  -0.8642   0.01930   0.01452  -0.0783   0.9293   0.0085
 -11.500  -0.8449   0.01851   0.01361  -0.0774   0.9216   0.0086
 -11.250  -0.8251   0.01775   0.01275  -0.0765   0.9137   0.0089
 -11.000  -0.8034   0.01714   0.01206  -0.0758   0.9069   0.0091
 -10.750  -0.7808   0.01661   0.01145  -0.0752   0.8996   0.0093
 -10.500  -0.7577   0.01613   0.01089  -0.0747   0.8930   0.0095
 -10.250  -0.7340   0.01567   0.01036  -0.0742   0.8862   0.0097
 -10.000  -0.7101   0.01525   0.00986  -0.0738   0.8794   0.0099
  -9.750  -0.6856   0.01484   0.00938  -0.0734   0.8731   0.0102
  -9.500  -0.6610   0.01444   0.00891  -0.0730   0.8661   0.0105
  -9.250  -0.6362   0.01406   0.00845  -0.0727   0.8599   0.0108
  -9.000  -0.6112   0.01369   0.00800  -0.0723   0.8529   0.0110
  -8.750  -0.5866   0.01327   0.00751  -0.0719   0.8464   0.0112
  -8.500  -0.5617   0.01284   0.00702  -0.0715   0.8394   0.0116
  -8.250  -0.5364   0.01251   0.00663  -0.0712   0.8325   0.0120
  -8.000  -0.5105   0.01220   0.00628  -0.0710   0.8257   0.0124
  -7.750  -0.4846   0.01191   0.00594  -0.0707   0.8186   0.0129
  -7.500  -0.4585   0.01164   0.00561  -0.0705   0.8119   0.0133
  -7.250  -0.4323   0.01139   0.00529  -0.0703   0.8045   0.0137
  -7.000  -0.4061   0.01113   0.00498  -0.0701   0.7975   0.0142
  -6.750  -0.3801   0.01084   0.00466  -0.0698   0.7897   0.0150
  -6.500  -0.3536   0.01063   0.00441  -0.0696   0.7827   0.0158
  -6.250  -0.3269   0.01043   0.00417  -0.0695   0.7749   0.0167
  -6.000  -0.3003   0.01025   0.00393  -0.0693   0.7677   0.0174
  -5.750  -0.2738   0.01002   0.00367  -0.0691   0.7597   0.0186
  -5.500  -0.2471   0.00984   0.00346  -0.0689   0.7522   0.0198
  -5.250  -0.2201   0.00968   0.00326  -0.0688   0.7441   0.0211
  -5.000  -0.1934   0.00951   0.00306  -0.0686   0.7366   0.0228
  -4.750  -0.1664   0.00936   0.00289  -0.0685   0.7282   0.0251
  -4.500  -0.1395   0.00922   0.00272  -0.0683   0.7205   0.0274
  -4.250  -0.1125   0.00908   0.00257  -0.0682   0.7121   0.0305
  -4.000  -0.0856   0.00896   0.00242  -0.0681   0.7044   0.0340
  -3.750  -0.0585   0.00884   0.00229  -0.0680   0.6958   0.0387
  -3.500  -0.0316   0.00871   0.00216  -0.0678   0.6880   0.0456
  -3.250  -0.0047   0.00860   0.00205  -0.0677   0.6793   0.0536
  -3.000   0.0223   0.00847   0.00194  -0.0676   0.6713   0.0648
  -2.750   0.0491   0.00836   0.00184  -0.0674   0.6626   0.0786
  -2.500   0.0759   0.00822   0.00175  -0.0673   0.6545   0.0981
  -2.250   0.1022   0.00808   0.00166  -0.0671   0.6458   0.1264
  -2.000   0.1286   0.00789   0.00157  -0.0669   0.6374   0.1649
  -1.750   0.1544   0.00771   0.00150  -0.0666   0.6289   0.2111
  -1.500   0.1801   0.00747   0.00144  -0.0664   0.6200   0.2704
  -1.250   0.2058   0.00728   0.00139  -0.0661   0.6116   0.3293
  -1.000   0.2313   0.00707   0.00135  -0.0658   0.6025   0.3938
  -0.750   0.2569   0.00689   0.00132  -0.0654   0.5941   0.4556
  -0.500   0.2822   0.00672   0.00131  -0.0651   0.5848   0.5185
  -0.250   0.3075   0.00653   0.00131  -0.0646   0.5762   0.5864
   0.000   0.3323   0.00640   0.00132  -0.0641   0.5672   0.6502
   0.250   0.3579   0.00630   0.00135  -0.0637   0.5580   0.7000
   0.500   0.3837   0.00626   0.00139  -0.0632   0.5490   0.7382
   0.750   0.4099   0.00626   0.00143  -0.0629   0.5393   0.7681
   1.250   0.4625   0.00630   0.00153  -0.0623   0.5202   0.8165
   1.500   0.4891   0.00634   0.00159  -0.0620   0.5101   0.8371
   1.750   0.5155   0.00639   0.00165  -0.0617   0.5002   0.8558
   2.000   0.5418   0.00647   0.00173  -0.0614   0.4901   0.8731
   2.250   0.5683   0.00654   0.00180  -0.0611   0.4797   0.8891
   2.500   0.5946   0.00663   0.00188  -0.0608   0.4699   0.9036
   2.750   0.6209   0.00674   0.00198  -0.0605   0.4594   0.9168
   3.000   0.6476   0.00684   0.00207  -0.0603   0.4489   0.9289
   3.250   0.6744   0.00696   0.00217  -0.0602   0.4385   0.9407
   3.500   0.7018   0.00711   0.00228  -0.0602   0.4277   0.9515
   3.750   0.7310   0.00726   0.00240  -0.0606   0.4164   0.9603
   4.000   0.7594   0.00741   0.00251  -0.0609   0.4051   0.9689
   4.250   0.7910   0.00759   0.00265  -0.0619   0.3932   0.9740
   4.500   0.8211   0.00778   0.00279  -0.0626   0.3809   0.9797
   4.750   0.8515   0.00798   0.00293  -0.0634   0.3681   0.9843
   5.000   0.8835   0.00818   0.00309  -0.0646   0.3552   0.9876
   5.250   0.9147   0.00839   0.00325  -0.0657   0.3419   0.9910
   5.500   0.9452   0.00862   0.00343  -0.0665   0.3281   0.9942
   5.750   0.9771   0.00887   0.00362  -0.0678   0.3139   0.9964
   6.000   1.0082   0.00914   0.00383  -0.0689   0.2989   0.9989
   6.250   1.0324   0.00939   0.00403  -0.0685   0.2848   1.0000
   6.500   1.0507   0.00964   0.00422  -0.0668   0.2718   1.0000
   6.750   1.0689   0.00991   0.00443  -0.0651   0.2580   1.0000
   7.000   1.0874   0.01019   0.00466  -0.0634   0.2439   1.0000
   7.250   1.1064   0.01051   0.00491  -0.0619   0.2292   1.0000
   7.500   1.1256   0.01084   0.00519  -0.0606   0.2146   1.0000
   7.750   1.1447   0.01121   0.00548  -0.0592   0.1989   1.0000
   8.000   1.1634   0.01161   0.00581  -0.0578   0.1826   1.0000
   8.250   1.1813   0.01205   0.00617  -0.0563   0.1656   1.0000
   8.500   1.1975   0.01253   0.00656  -0.0545   0.1493   1.0000
   8.750   1.2131   0.01301   0.00697  -0.0525   0.1339   1.0000
   9.000   1.2287   0.01352   0.00741  -0.0507   0.1195   1.0000
   9.250   1.2439   0.01408   0.00790  -0.0489   0.1053   1.0000
   9.500   1.2588   0.01467   0.00843  -0.0472   0.0921   1.0000
   9.750   1.2735   0.01530   0.00900  -0.0454   0.0802   1.0000
  10.000   1.2877   0.01596   0.00961  -0.0437   0.0695   1.0000
  10.250   1.3016   0.01666   0.01028  -0.0420   0.0600   1.0000
  10.500   1.3148   0.01742   0.01100  -0.0403   0.0512   1.0000
  10.750   1.3280   0.01820   0.01176  -0.0387   0.0439   1.0000
  11.000   1.3418   0.01897   0.01252  -0.0372   0.0383   1.0000
  11.250   1.3548   0.01981   0.01335  -0.0358   0.0335   1.0000
  11.500   1.3666   0.02074   0.01427  -0.0342   0.0288   1.0000
  11.750   1.3789   0.02167   0.01522  -0.0328   0.0252   1.0000
  12.000   1.3908   0.02265   0.01621  -0.0315   0.0222   1.0000
  12.250   1.4017   0.02373   0.01731  -0.0301   0.0196   1.0000
  12.500   1.4133   0.02478   0.01840  -0.0289   0.0178   1.0000
  12.750   1.4237   0.02596   0.01960  -0.0277   0.0161   1.0000
  13.000   1.4337   0.02718   0.02087  -0.0265   0.0148   1.0000
  13.250   1.4436   0.02845   0.02217  -0.0254   0.0136   1.0000
  13.500   1.4520   0.02987   0.02364  -0.0243   0.0125   1.0000
  13.750   1.4603   0.03133   0.02514  -0.0233   0.0117   1.0000
  14.000   1.4683   0.03285   0.02672  -0.0224   0.0109   1.0000
  14.250   1.4748   0.03453   0.02845  -0.0215   0.0102   1.0000
  14.500   1.4800   0.03639   0.03036  -0.0206   0.0095   1.0000
  14.750   1.4863   0.03819   0.03223  -0.0199   0.0091   1.0000
  15.000   1.4917   0.04013   0.03424  -0.0192   0.0086   1.0000
  15.250   1.4960   0.04224   0.03641  -0.0187   0.0082   1.0000
  15.500   1.4992   0.04451   0.03874  -0.0182   0.0078   1.0000
  15.750   1.5011   0.04697   0.04126  -0.0178   0.0075   1.0000
  16.000   1.5023   0.04957   0.04394  -0.0175   0.0072   1.0000
  16.250   1.5043   0.05214   0.04659  -0.0173   0.0070   1.0000
  16.500   1.5055   0.05488   0.04941  -0.0173   0.0068   1.0000
  16.750   1.5055   0.05778   0.05240  -0.0173   0.0066   1.0000
  17.000   1.5044   0.06087   0.05557  -0.0175   0.0064   1.0000
  17.250   1.5024   0.06414   0.05893  -0.0177   0.0063   1.0000
  17.500   1.4993   0.06761   0.06247  -0.0181   0.0061   1.0000
  17.750   1.4952   0.07126   0.06622  -0.0186   0.0059   1.0000
  18.000   1.4897   0.07514   0.07018  -0.0192   0.0058   1.0000
  18.250   1.4831   0.07924   0.07437  -0.0200   0.0057   1.0000
  18.500   1.4751   0.08362   0.07885  -0.0209   0.0055   1.0000
  18.750   1.4660   0.08822   0.08354  -0.0220   0.0054   1.0000
  19.000   1.4583   0.09263   0.08805  -0.0232   0.0053   1.0000
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