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MRC-16 (mrc-16-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: MRC-16 (mrc-16-il)
Reynolds number: 1,000,000
Max Cl/Cd: 124.12 at α=5.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mrc-16-il-1000000.txt
Download as CSV file: xf-mrc-16-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.6052   0.09237   0.09059  -0.0484   1.0000   0.0114
 -13.500  -0.7693   0.05125   0.04891  -0.0771   1.0000   0.0107
 -13.250  -0.7949   0.04343   0.04086  -0.0838   1.0000   0.0107
 -13.000  -0.8130   0.03870   0.03594  -0.0861   1.0000   0.0107
 -12.750  -0.8294   0.03560   0.03267  -0.0852   1.0000   0.0107
 -12.500  -0.8519   0.03397   0.03093  -0.0804   0.9996   0.0108
 -12.250  -0.8408   0.03133   0.02806  -0.0820   0.9951   0.0109
 -12.000  -0.8241   0.02925   0.02577  -0.0831   0.9905   0.0110
 -11.750  -0.8023   0.02766   0.02400  -0.0843   0.9865   0.0110
 -11.500  -0.7958   0.02392   0.01987  -0.0843   0.9798   0.0113
 -11.250  -0.7785   0.02220   0.01799  -0.0840   0.9729   0.0115
 -11.000  -0.7587   0.02119   0.01688  -0.0835   0.9658   0.0118
 -10.750  -0.7387   0.02039   0.01600  -0.0826   0.9583   0.0120
 -10.500  -0.7188   0.01969   0.01520  -0.0817   0.9507   0.0122
 -10.250  -0.6986   0.01898   0.01439  -0.0807   0.9433   0.0125
 -10.000  -0.6778   0.01828   0.01359  -0.0798   0.9361   0.0127
  -9.750  -0.6565   0.01761   0.01280  -0.0790   0.9289   0.0131
  -9.500  -0.6344   0.01696   0.01204  -0.0782   0.9222   0.0134
  -9.250  -0.6115   0.01639   0.01137  -0.0775   0.9152   0.0137
  -9.000  -0.5874   0.01599   0.01086  -0.0770   0.9090   0.0139
  -8.750  -0.5675   0.01486   0.00961  -0.0760   0.9017   0.0145
  -8.500  -0.5444   0.01428   0.00896  -0.0753   0.8952   0.0150
  -8.250  -0.5197   0.01384   0.00848  -0.0749   0.8888   0.0154
  -8.000  -0.4950   0.01344   0.00801  -0.0745   0.8821   0.0159
  -7.750  -0.4700   0.01303   0.00754  -0.0741   0.8759   0.0164
  -7.500  -0.4446   0.01265   0.00709  -0.0737   0.8691   0.0169
  -7.250  -0.4189   0.01236   0.00671  -0.0733   0.8628   0.0174
  -7.000  -0.3956   0.01166   0.00595  -0.0727   0.8558   0.0182
  -6.750  -0.3702   0.01132   0.00556  -0.0723   0.8491   0.0190
  -6.500  -0.3439   0.01104   0.00526  -0.0721   0.8425   0.0199
  -6.250  -0.3174   0.01082   0.00498  -0.0719   0.8355   0.0209
  -6.000  -0.2916   0.01049   0.00458  -0.0715   0.8289   0.0220
  -5.750  -0.2659   0.01014   0.00422  -0.0712   0.8216   0.0236
  -5.500  -0.2393   0.00994   0.00396  -0.0710   0.8149   0.0250
  -5.250  -0.2122   0.00976   0.00375  -0.0708   0.8074   0.0263
  -5.000  -0.1866   0.00944   0.00339  -0.0704   0.8005   0.0292
  -4.750  -0.1594   0.00928   0.00321  -0.0703   0.7928   0.0317
  -4.500  -0.1332   0.00904   0.00294  -0.0700   0.7856   0.0359
  -4.250  -0.1061   0.00887   0.00275  -0.0699   0.7779   0.0401
  -4.000  -0.0795   0.00869   0.00257  -0.0697   0.7704   0.0466
  -3.750  -0.0527   0.00849   0.00240  -0.0695   0.7627   0.0563
  -3.500  -0.0262   0.00832   0.00224  -0.0693   0.7550   0.0705
  -3.250   0.0004   0.00811   0.00210  -0.0691   0.7470   0.0920
  -3.000   0.0263   0.00790   0.00196  -0.0688   0.7391   0.1248
  -2.750   0.0521   0.00760   0.00184  -0.0686   0.7311   0.1732
  -2.500   0.0770   0.00730   0.00172  -0.0681   0.7231   0.2387
  -2.250   0.1020   0.00695   0.00162  -0.0678   0.7149   0.3176
  -2.000   0.1265   0.00665   0.00154  -0.0673   0.7069   0.3990
  -1.750   0.1515   0.00636   0.00148  -0.0668   0.6985   0.4759
  -1.500   0.1760   0.00611   0.00143  -0.0662   0.6904   0.5535
  -1.250   0.2010   0.00591   0.00141  -0.0657   0.6818   0.6192
  -1.000   0.2260   0.00576   0.00140  -0.0651   0.6736   0.6766
  -0.750   0.2515   0.00566   0.00140  -0.0646   0.6649   0.7221
  -0.500   0.2774   0.00561   0.00142  -0.0641   0.6566   0.7601
  -0.250   0.3032   0.00558   0.00144  -0.0636   0.6477   0.7941
   0.000   0.3293   0.00555   0.00147  -0.0632   0.6391   0.8249
   0.500   0.3818   0.00557   0.00155  -0.0623   0.6213   0.8714
   0.750   0.4081   0.00563   0.00159  -0.0619   0.6125   0.8892
   1.000   0.4347   0.00567   0.00164  -0.0615   0.6030   0.9049
   1.250   0.4612   0.00574   0.00169  -0.0612   0.5939   0.9187
   1.750   0.5147   0.00590   0.00181  -0.0606   0.5746   0.9423
   2.000   0.5413   0.00600   0.00188  -0.0602   0.5652   0.9531
   2.250   0.5710   0.00611   0.00195  -0.0606   0.5550   0.9608
   2.500   0.5986   0.00622   0.00203  -0.0606   0.5452   0.9697
   2.750   0.6325   0.00636   0.00212  -0.0620   0.5349   0.9740
   3.000   0.6656   0.00649   0.00221  -0.0633   0.5239   0.9789
   3.250   0.6985   0.00662   0.00229  -0.0645   0.5132   0.9834
   3.500   0.7361   0.00676   0.00239  -0.0668   0.5021   0.9852
   3.750   0.7726   0.00692   0.00249  -0.0689   0.4903   0.9875
   4.000   0.8080   0.00706   0.00260  -0.0708   0.4784   0.9903
   4.250   0.8417   0.00721   0.00271  -0.0723   0.4663   0.9934
   4.500   0.8773   0.00736   0.00281  -0.0742   0.4540   0.9952
   4.750   0.9126   0.00752   0.00293  -0.0761   0.4413   0.9971
   5.000   0.9473   0.00770   0.00306  -0.0779   0.4278   0.9990
   5.250   0.9756   0.00788   0.00319  -0.0784   0.4148   1.0000
   5.500   0.9954   0.00802   0.00331  -0.0769   0.4030   1.0000
   5.750   1.0145   0.00819   0.00344  -0.0753   0.3909   1.0000
   6.000   1.0333   0.00838   0.00359  -0.0737   0.3786   1.0000
   6.250   1.0518   0.00858   0.00375  -0.0720   0.3658   1.0000
   6.500   1.0703   0.00881   0.00392  -0.0703   0.3523   1.0000
   6.750   1.0891   0.00904   0.00411  -0.0686   0.3385   1.0000
   7.000   1.1080   0.00928   0.00430  -0.0670   0.3243   1.0000
   7.250   1.1269   0.00955   0.00452  -0.0655   0.3094   1.0000
   7.500   1.1461   0.00984   0.00476  -0.0640   0.2940   1.0000
   7.750   1.1653   0.01017   0.00502  -0.0626   0.2775   1.0000
   8.000   1.1848   0.01051   0.00529  -0.0613   0.2607   1.0000
   8.250   1.2040   0.01089   0.00560  -0.0599   0.2431   1.0000
   8.500   1.2227   0.01130   0.00593  -0.0585   0.2255   1.0000
   8.750   1.2405   0.01174   0.00629  -0.0570   0.2082   1.0000
   9.000   1.2565   0.01220   0.00668  -0.0551   0.1915   1.0000
   9.250   1.2721   0.01269   0.00710  -0.0533   0.1753   1.0000
   9.500   1.2877   0.01321   0.00755  -0.0515   0.1592   1.0000
   9.750   1.3028   0.01377   0.00804  -0.0497   0.1437   1.0000
  10.000   1.3172   0.01439   0.00859  -0.0478   0.1285   1.0000
  10.250   1.3307   0.01507   0.00920  -0.0460   0.1136   1.0000
  10.500   1.3434   0.01582   0.00988  -0.0441   0.0995   1.0000
  10.750   1.3557   0.01660   0.01060  -0.0422   0.0869   1.0000
  11.000   1.3678   0.01743   0.01138  -0.0404   0.0755   1.0000
  11.250   1.3793   0.01831   0.01222  -0.0386   0.0652   1.0000
  11.500   1.3901   0.01927   0.01315  -0.0368   0.0558   1.0000
  11.750   1.4003   0.02029   0.01414  -0.0351   0.0475   1.0000
  12.000   1.4101   0.02137   0.01520  -0.0334   0.0406   1.0000
  12.250   1.4190   0.02254   0.01636  -0.0317   0.0347   1.0000
  12.500   1.4277   0.02377   0.01758  -0.0301   0.0300   1.0000
  12.750   1.4372   0.02499   0.01882  -0.0288   0.0264   1.0000
  13.000   1.4445   0.02639   0.02024  -0.0273   0.0231   1.0000
  13.250   1.4527   0.02777   0.02165  -0.0260   0.0208   1.0000
  13.500   1.4587   0.02937   0.02328  -0.0247   0.0187   1.0000
  13.750   1.4665   0.03086   0.02483  -0.0236   0.0172   1.0000
  14.000   1.4704   0.03271   0.02671  -0.0224   0.0157   1.0000
  14.250   1.4761   0.03447   0.02854  -0.0214   0.0147   1.0000
  14.500   1.4821   0.03626   0.03039  -0.0205   0.0138   1.0000
  14.750   1.4853   0.03835   0.03253  -0.0197   0.0130   1.0000
  15.000   1.4836   0.04101   0.03526  -0.0188   0.0121   1.0000
  15.250   1.4884   0.04309   0.03743  -0.0183   0.0117   1.0000
  15.500   1.4916   0.04540   0.03982  -0.0178   0.0112   1.0000
  15.750   1.4934   0.04790   0.04239  -0.0175   0.0108   1.0000
  16.000   1.4935   0.05066   0.04522  -0.0172   0.0104   1.0000
  16.250   1.4910   0.05378   0.04842  -0.0171   0.0100   1.0000
  16.500   1.4844   0.05748   0.05221  -0.0171   0.0096   1.0000
  16.750   1.4775   0.06131   0.05614  -0.0172   0.0094   1.0000
  17.000   1.4762   0.06453   0.05945  -0.0175   0.0092   1.0000
  17.250   1.4731   0.06804   0.06306  -0.0179   0.0090   1.0000
  17.500   1.4687   0.07177   0.06690  -0.0185   0.0088   1.0000
  17.750   1.4630   0.07571   0.07093  -0.0191   0.0087   1.0000
  18.000   1.4564   0.07985   0.07517  -0.0199   0.0085   1.0000
  18.250   1.4491   0.08417   0.07958  -0.0209   0.0083   1.0000
  18.500   1.4410   0.08866   0.08417  -0.0219   0.0082   1.0000
  18.750   1.4316   0.09339   0.08899  -0.0232   0.0080   1.0000
  19.000   1.4210   0.09836   0.09406  -0.0246   0.0079   1.0000
  19.250   1.4093   0.10362   0.09942  -0.0263   0.0078   1.0000
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