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MRC-20 (mrc-20-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: MRC-20 (mrc-20-il)
Reynolds number: 1,000,000
Max Cl/Cd: 114.48 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mrc-20-il-1000000.txt
Download as CSV file: xf-mrc-20-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MRC-20                                          
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.2415   0.08586   0.08406  -0.0997   0.9851   0.0124
 -10.750  -0.2393   0.08135   0.07955  -0.1028   0.9823   0.0125
 -10.500  -0.2402   0.07584   0.07405  -0.1071   0.9785   0.0126
 -10.250  -0.2557   0.06674   0.06490  -0.1157   0.9734   0.0126
 -10.000  -0.2772   0.06103   0.05910  -0.1193   0.9656   0.0126
  -9.750  -0.2956   0.05712   0.05509  -0.1200   0.9587   0.0126
  -9.500  -0.3094   0.05417   0.05206  -0.1190   0.9511   0.0126
  -9.250  -0.3197   0.05179   0.04957  -0.1168   0.9453   0.0127
  -9.000  -0.3212   0.04928   0.04696  -0.1156   0.9398   0.0128
  -8.750  -0.3197   0.04685   0.04441  -0.1143   0.9349   0.0129
  -8.500  -0.3156   0.04440   0.04183  -0.1129   0.9307   0.0131
  -8.250  -0.3091   0.04183   0.03912  -0.1116   0.9258   0.0133
  -8.000  -0.3010   0.03913   0.03627  -0.1101   0.9212   0.0136
  -7.750  -0.2911   0.03628   0.03322  -0.1085   0.9173   0.0140
  -7.500  -0.2837   0.03136   0.02768  -0.1045   0.9121   0.0151
  -7.250  -0.2774   0.02725   0.02337  -0.1028   0.9072   0.0154
  -7.000  -0.2586   0.02587   0.02190  -0.1020   0.9035   0.0156
  -6.750  -0.2532   0.01770   0.01270  -0.0972   0.8989   0.0124
  -6.500  -0.2305   0.01624   0.01109  -0.0965   0.8947   0.0125
  -6.250  -0.2063   0.01516   0.00990  -0.0960   0.8907   0.0126
  -6.000  -0.1812   0.01427   0.00892  -0.0957   0.8871   0.0128
  -5.750  -0.1564   0.01350   0.00807  -0.0953   0.8831   0.0129
  -5.500  -0.1321   0.01282   0.00734  -0.0947   0.8782   0.0130
  -5.250  -0.1075   0.01222   0.00668  -0.0942   0.8737   0.0132
  -5.000  -0.0825   0.01170   0.00610  -0.0938   0.8692   0.0134
  -4.750  -0.0585   0.01129   0.00567  -0.0932   0.8637   0.0138
  -4.500  -0.0339   0.01087   0.00521  -0.0927   0.8583   0.0143
  -4.250  -0.0093   0.01048   0.00475  -0.0921   0.8530   0.0147
  -4.000   0.0150   0.01016   0.00440  -0.0915   0.8467   0.0150
  -3.750   0.0371   0.00959   0.00375  -0.0905   0.8406   0.0156
  -3.500   0.0615   0.00931   0.00347  -0.0899   0.8339   0.0164
  -3.250   0.0868   0.00908   0.00319  -0.0895   0.8270   0.0172
  -3.000   0.1123   0.00888   0.00296  -0.0891   0.8201   0.0179
  -2.750   0.1371   0.00863   0.00266  -0.0886   0.8123   0.0190
  -2.500   0.1628   0.00847   0.00248  -0.0882   0.8049   0.0209
  -2.250   0.1882   0.00830   0.00229  -0.0878   0.7966   0.0235
  -2.000   0.2139   0.00815   0.00212  -0.0874   0.7888   0.0286
  -1.750   0.2381   0.00791   0.00196  -0.0868   0.7800   0.0621
  -1.500   0.2487   0.00650   0.00163  -0.0841   0.7710   0.4159
  -1.250   0.2701   0.00617   0.00158  -0.0830   0.7617   0.5195
  -1.000   0.2950   0.00607   0.00157  -0.0825   0.7521   0.5610
  -0.750   0.3201   0.00603   0.00155  -0.0820   0.7425   0.5881
  -0.500   0.3455   0.00602   0.00155  -0.0816   0.7321   0.6116
  -0.250   0.3700   0.00598   0.00157  -0.0809   0.7217   0.6417
   0.000   0.3950   0.00600   0.00158  -0.0804   0.7110   0.6634
   0.250   0.4204   0.00602   0.00159  -0.0800   0.6998   0.6734
   0.500   0.4462   0.00605   0.00160  -0.0796   0.6887   0.6832
   0.750   0.4715   0.00610   0.00162  -0.0792   0.6776   0.6942
   1.250   0.5217   0.00619   0.00168  -0.0783   0.6541   0.7184
   1.750   0.5710   0.00631   0.00178  -0.0772   0.6305   0.7486
   2.000   0.5952   0.00637   0.00185  -0.0766   0.6182   0.7654
   2.250   0.6199   0.00642   0.00192  -0.0760   0.6060   0.7832
   2.500   0.6441   0.00648   0.00200  -0.0754   0.5940   0.8023
   2.750   0.6675   0.00656   0.00209  -0.0746   0.5814   0.8232
   3.250   0.7141   0.00672   0.00230  -0.0729   0.5554   0.8683
   3.500   0.7373   0.00682   0.00242  -0.0721   0.5425   0.8908
   3.750   0.7599   0.00693   0.00255  -0.0710   0.5294   0.9136
   4.000   0.7828   0.00708   0.00270  -0.0701   0.5162   0.9364
   4.250   0.8075   0.00727   0.00286  -0.0696   0.5023   0.9564
   4.500   0.8363   0.00749   0.00303  -0.0701   0.4874   0.9710
   4.750   0.8693   0.00772   0.00321  -0.0716   0.4723   0.9805
   5.000   0.9029   0.00797   0.00340  -0.0733   0.4572   0.9876
   5.250   0.9367   0.00823   0.00360  -0.0750   0.4416   0.9935
   5.500   0.9721   0.00850   0.00381  -0.0772   0.4257   0.9970
   5.750   1.0028   0.00876   0.00401  -0.0783   0.4102   1.0000
   6.000   1.0099   0.00889   0.00411  -0.0742   0.3988   1.0000
   6.250   1.0220   0.00908   0.00425  -0.0712   0.3869   1.0000
   6.500   1.0373   0.00932   0.00443  -0.0689   0.3742   1.0000
   6.750   1.0551   0.00956   0.00463  -0.0672   0.3609   1.0000
   7.000   1.0742   0.00982   0.00485  -0.0658   0.3477   1.0000
   7.250   1.0933   0.01010   0.00509  -0.0645   0.3343   1.0000
   7.500   1.1124   0.01041   0.00535  -0.0632   0.3200   1.0000
   7.750   1.1314   0.01075   0.00563  -0.0619   0.3047   1.0000
   8.000   1.1498   0.01113   0.00594  -0.0605   0.2886   1.0000
   8.250   1.1677   0.01154   0.00629  -0.0591   0.2717   1.0000
   8.500   1.1858   0.01196   0.00665  -0.0578   0.2556   1.0000
   8.750   1.2032   0.01242   0.00704  -0.0564   0.2395   1.0000
   9.000   1.2199   0.01292   0.00747  -0.0548   0.2231   1.0000
   9.250   1.2364   0.01345   0.00792  -0.0534   0.2068   1.0000
   9.500   1.2523   0.01401   0.00842  -0.0518   0.1908   1.0000
   9.750   1.2679   0.01459   0.00893  -0.0503   0.1755   1.0000
  10.000   1.2832   0.01521   0.00949  -0.0487   0.1603   1.0000
  10.250   1.2974   0.01588   0.01009  -0.0470   0.1454   1.0000
  10.500   1.3115   0.01657   0.01073  -0.0454   0.1317   1.0000
  10.750   1.3248   0.01732   0.01142  -0.0437   0.1185   1.0000
  11.000   1.3373   0.01812   0.01217  -0.0419   0.1056   1.0000
  11.250   1.3491   0.01897   0.01297  -0.0402   0.0935   1.0000
  11.500   1.3606   0.01986   0.01381  -0.0384   0.0827   1.0000
  11.750   1.3714   0.02081   0.01472  -0.0366   0.0730   1.0000
  12.000   1.3818   0.02181   0.01569  -0.0349   0.0642   1.0000
  12.500   1.4011   0.02396   0.01780  -0.0314   0.0497   1.0000
  12.750   1.4107   0.02508   0.01892  -0.0298   0.0439   1.0000
  13.000   1.4190   0.02631   0.02015  -0.0282   0.0390   1.0000
  13.250   1.4265   0.02764   0.02148  -0.0265   0.0350   1.0000
  13.500   1.4360   0.02887   0.02275  -0.0252   0.0320   1.0000
  13.750   1.4421   0.03040   0.02429  -0.0237   0.0292   1.0000
  14.000   1.4511   0.03174   0.02569  -0.0225   0.0274   1.0000
  14.250   1.4576   0.03331   0.02729  -0.0212   0.0256   1.0000
  14.500   1.4624   0.03508   0.02911  -0.0199   0.0239   1.0000
  14.750   1.4705   0.03663   0.03073  -0.0190   0.0228   1.0000
  15.000   1.4758   0.03847   0.03261  -0.0180   0.0216   1.0000
  15.250   1.4773   0.04070   0.03489  -0.0169   0.0205   1.0000
  15.500   1.4812   0.04277   0.03704  -0.0160   0.0198   1.0000
  15.750   1.4864   0.04478   0.03913  -0.0154   0.0192   1.0000
  16.000   1.4900   0.04700   0.04142  -0.0148   0.0185   1.0000
  16.250   1.4915   0.04949   0.04398  -0.0143   0.0179   1.0000
  16.500   1.4896   0.05238   0.04694  -0.0138   0.0173   1.0000
  16.750   1.4829   0.05591   0.05056  -0.0133   0.0167   1.0000
  17.000   1.4856   0.05846   0.05320  -0.0132   0.0164   1.0000
  17.250   1.4863   0.06128   0.05611  -0.0132   0.0160   1.0000
  17.500   1.4854   0.06434   0.05926  -0.0133   0.0156   1.0000
  17.750   1.4829   0.06762   0.06262  -0.0134   0.0152   1.0000
  18.000   1.4789   0.07117   0.06625  -0.0137   0.0149   1.0000
  18.250   1.4732   0.07500   0.07017  -0.0142   0.0146   1.0000
  18.500   1.4651   0.07922   0.07448  -0.0148   0.0143   1.0000
  18.750   1.4540   0.08390   0.07927  -0.0157   0.0141   1.0000
  19.000   1.4393   0.08919   0.08466  -0.0168   0.0138   1.0000
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