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RONCZ 1080 VOYAGER INNER AFT WING AIRFOIL (r1080-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: RONCZ 1080 VOYAGER INNER AFT WING AIRFOIL (r1080-il)
Reynolds number: 1,000,000
Max Cl/Cd: 127.05 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-r1080-il-1000000-n5.txt
Download as CSV file: xf-r1080-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RONCZ 1080 VOYAGER INNER AFT WING AIRFOIL       
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -0.5683   0.11590   0.11250  -0.0791   0.7430   0.0065
 -18.250  -0.6040   0.10484   0.10128  -0.0848   0.7407   0.0063
 -18.000  -0.6296   0.09608   0.09240  -0.0895   0.7367   0.0063
 -17.750  -0.6656   0.08577   0.08194  -0.0952   0.7338   0.0063
 -17.500  -0.6962   0.07649   0.07250  -0.1005   0.7296   0.0063
 -17.250  -0.7190   0.06875   0.06459  -0.1051   0.7241   0.0063
 -17.000  -0.7363   0.06221   0.05790  -0.1091   0.7187   0.0063
 -16.750  -0.7540   0.05616   0.05169  -0.1125   0.7133   0.0063
 -16.500  -0.7624   0.05183   0.04722  -0.1146   0.7072   0.0063
 -16.250  -0.7752   0.04739   0.04263  -0.1164   0.7020   0.0063
 -16.000  -0.7790   0.04430   0.03941  -0.1172   0.6969   0.0063
 -15.750  -0.7917   0.04063   0.03559  -0.1176   0.6920   0.0064
 -15.500  -0.7953   0.03813   0.03297  -0.1174   0.6870   0.0063
 -15.250  -0.7924   0.03632   0.03106  -0.1170   0.6828   0.0063
 -15.000  -0.8019   0.03367   0.02828  -0.1160   0.6789   0.0065
 -14.750  -0.8034   0.03176   0.02625  -0.1148   0.6746   0.0065
 -14.500  -0.7993   0.03034   0.02473  -0.1136   0.6704   0.0065
 -14.250  -0.7974   0.02880   0.02309  -0.1121   0.6672   0.0065
 -14.000  -0.7905   0.02764   0.02186  -0.1109   0.6639   0.0066
 -13.750  -0.7822   0.02658   0.02074  -0.1096   0.6607   0.0067
 -13.500  -0.7745   0.02553   0.01960  -0.1081   0.6572   0.0068
 -13.250  -0.7629   0.02474   0.01874  -0.1069   0.6540   0.0068
 -13.000  -0.7556   0.02369   0.01759  -0.1051   0.6508   0.0069
 -12.750  -0.7433   0.02294   0.01679  -0.1038   0.6485   0.0070
 -12.500  -0.7320   0.02213   0.01591  -0.1022   0.6458   0.0070
 -12.250  -0.7185   0.02147   0.01520  -0.1009   0.6432   0.0071
 -12.000  -0.7051   0.02081   0.01448  -0.0995   0.6406   0.0072
 -11.750  -0.6927   0.02010   0.01369  -0.0978   0.6384   0.0072
 -11.500  -0.6775   0.01957   0.01310  -0.0965   0.6361   0.0074
 -11.250  -0.6632   0.01897   0.01243  -0.0950   0.6339   0.0075
 -11.000  -0.6484   0.01838   0.01179  -0.0935   0.6325   0.0075
 -10.750  -0.6321   0.01788   0.01125  -0.0921   0.6308   0.0077
 -10.500  -0.6153   0.01742   0.01074  -0.0908   0.6291   0.0077
 -10.250  -0.5992   0.01691   0.01018  -0.0893   0.6274   0.0079
 -10.000  -0.5826   0.01645   0.00967  -0.0878   0.6256   0.0080
  -9.750  -0.5653   0.01603   0.00921  -0.0864   0.6240   0.0080
  -9.500  -0.5477   0.01565   0.00878  -0.0850   0.6224   0.0082
  -9.250  -0.5306   0.01525   0.00833  -0.0835   0.6207   0.0083
  -9.000  -0.5126   0.01492   0.00795  -0.0820   0.6191   0.0084
  -8.500  -0.4802   0.01416   0.00713  -0.0784   0.6165   0.0089
  -8.250  -0.4626   0.01386   0.00681  -0.0767   0.6154   0.0091
  -8.000  -0.4429   0.01359   0.00652  -0.0755   0.6142   0.0095
  -7.750  -0.4217   0.01332   0.00624  -0.0745   0.6128   0.0097
  -7.500  -0.4002   0.01306   0.00595  -0.0735   0.6115   0.0100
  -7.250  -0.3783   0.01281   0.00567  -0.0726   0.6102   0.0104
  -7.000  -0.3558   0.01258   0.00542  -0.0718   0.6090   0.0107
  -6.750  -0.3334   0.01234   0.00516  -0.0710   0.6078   0.0110
  -6.500  -0.3110   0.01209   0.00489  -0.0702   0.6067   0.0116
  -6.250  -0.2879   0.01187   0.00466  -0.0695   0.6055   0.0123
  -6.000  -0.2643   0.01168   0.00445  -0.0689   0.6044   0.0129
  -5.750  -0.2407   0.01149   0.00425  -0.0683   0.6032   0.0139
  -5.500  -0.2169   0.01131   0.00406  -0.0677   0.6020   0.0153
  -5.250  -0.1929   0.01114   0.00388  -0.0671   0.6008   0.0176
  -5.000  -0.1687   0.01093   0.00370  -0.0666   0.6002   0.0220
  -4.750  -0.1447   0.01070   0.00352  -0.0661   0.5995   0.0301
  -4.500  -0.1204   0.01049   0.00336  -0.0656   0.5987   0.0399
  -4.250  -0.0960   0.01029   0.00321  -0.0652   0.5979   0.0520
  -4.000  -0.0714   0.01009   0.00308  -0.0647   0.5971   0.0652
  -3.750  -0.0464   0.00991   0.00295  -0.0644   0.5961   0.0803
  -3.500  -0.0219   0.00970   0.00283  -0.0640   0.5951   0.1005
  -3.250   0.0024   0.00946   0.00270  -0.0635   0.5941   0.1283
  -3.000   0.0258   0.00918   0.00258  -0.0630   0.5931   0.1705
  -2.750   0.0485   0.00884   0.00244  -0.0623   0.5922   0.2269
  -2.500   0.0701   0.00843   0.00230  -0.0615   0.5913   0.3025
  -2.250   0.0921   0.00802   0.00216  -0.0607   0.5904   0.3799
  -2.000   0.1140   0.00759   0.00202  -0.0599   0.5895   0.4644
  -1.750   0.1367   0.00721   0.00189  -0.0592   0.5887   0.5446
  -1.500   0.1595   0.00684   0.00181  -0.0585   0.5878   0.6273
  -1.250   0.1854   0.00674   0.00186  -0.0582   0.5868   0.6813
  -1.000   0.2135   0.00676   0.00190  -0.0584   0.5858   0.7020
  -0.750   0.2423   0.00681   0.00194  -0.0587   0.5847   0.7135
  -0.500   0.2711   0.00685   0.00197  -0.0590   0.5840   0.7243
  -0.250   0.2998   0.00688   0.00202  -0.0592   0.5833   0.7336
   0.000   0.3287   0.00693   0.00207  -0.0595   0.5826   0.7422
   0.250   0.3574   0.00697   0.00213  -0.0598   0.5819   0.7489
   0.500   0.3862   0.00703   0.00219  -0.0601   0.5811   0.7547
   0.750   0.4152   0.00707   0.00223  -0.0605   0.5802   0.7585
   1.000   0.4442   0.00711   0.00225  -0.0609   0.5791   0.7606
   1.250   0.4732   0.00714   0.00227  -0.0613   0.5780   0.7623
   1.500   0.5020   0.00715   0.00229  -0.0617   0.5767   0.7642
   1.750   0.5307   0.00716   0.00231  -0.0620   0.5751   0.7658
   2.000   0.5592   0.00719   0.00234  -0.0623   0.5732   0.7672
   2.250   0.5877   0.00723   0.00236  -0.0626   0.5714   0.7685
   2.500   0.6161   0.00728   0.00240  -0.0629   0.5693   0.7698
   2.750   0.6446   0.00731   0.00244  -0.0633   0.5675   0.7711
   3.000   0.6730   0.00732   0.00248  -0.0636   0.5653   0.7722
   3.250   0.7015   0.00734   0.00251  -0.0639   0.5629   0.7733
   3.500   0.7297   0.00735   0.00254  -0.0642   0.5601   0.7744
   3.750   0.7576   0.00738   0.00256  -0.0644   0.5569   0.7755
   4.000   0.7849   0.00744   0.00260  -0.0645   0.5533   0.7767
   4.250   0.8130   0.00746   0.00265  -0.0648   0.5501   0.7778
   4.500   0.8410   0.00748   0.00270  -0.0651   0.5457   0.7787
   4.750   0.8682   0.00752   0.00274  -0.0652   0.5411   0.7797
   5.000   0.8949   0.00756   0.00279  -0.0652   0.5366   0.7809
   5.250   0.9223   0.00759   0.00286  -0.0653   0.5308   0.7820
   5.500   0.9480   0.00766   0.00292  -0.0651   0.5232   0.7832
   5.750   0.9737   0.00773   0.00301  -0.0650   0.5126   0.7844
   6.000   0.9973   0.00785   0.00310  -0.0644   0.4976   0.7857
   6.250   1.0152   0.00814   0.00328  -0.0628   0.4696   0.7871
   6.500   1.0276   0.00861   0.00360  -0.0601   0.4362   0.7889
   6.750   1.0376   0.00913   0.00398  -0.0571   0.4051   0.7908
   7.000   1.0423   0.00964   0.00436  -0.0530   0.3755   0.7926
   7.250   1.0465   0.01016   0.00478  -0.0488   0.3515   0.7944
   7.500   1.0511   0.01073   0.00525  -0.0449   0.3278   0.7960
   7.750   1.0548   0.01133   0.00578  -0.0410   0.3071   0.7979
   8.000   1.0563   0.01203   0.00640  -0.0369   0.2861   0.8002
   8.250   1.0572   0.01282   0.00713  -0.0329   0.2663   0.8025
   8.500   1.0597   0.01366   0.00793  -0.0295   0.2501   0.8049
   8.750   1.0613   0.01464   0.00887  -0.0263   0.2339   0.8074
   9.000   1.0636   0.01572   0.00990  -0.0234   0.2190   0.8102
   9.250   1.0654   0.01693   0.01106  -0.0206   0.2036   0.8127
   9.500   1.0697   0.01808   0.01219  -0.0183   0.1916   0.8153
   9.750   1.0743   0.01926   0.01336  -0.0162   0.1806   0.8182
  10.000   1.0786   0.02051   0.01458  -0.0141   0.1683   0.8212
  10.250   1.0847   0.02170   0.01576  -0.0123   0.1579   0.8242
  10.500   1.0910   0.02291   0.01695  -0.0106   0.1488   0.8274
  11.000   1.1044   0.02532   0.01935  -0.0075   0.1307   0.8339
  11.250   1.1100   0.02661   0.02063  -0.0059   0.1219   0.8379
  11.500   1.1174   0.02782   0.02183  -0.0045   0.1141   0.8421
  11.750   1.1256   0.02904   0.02306  -0.0033   0.1074   0.8465
  12.000   1.1326   0.03031   0.02433  -0.0020   0.0998   0.8512
  12.250   1.1413   0.03151   0.02556  -0.0009   0.0940   0.8572
  12.500   1.1494   0.03278   0.02683   0.0002   0.0883   0.8639
  12.750   1.1578   0.03400   0.02810   0.0013   0.0821   0.8724
  13.000   1.1638   0.03541   0.02952   0.0025   0.0754   0.8836
  13.250   1.1724   0.03659   0.03076   0.0036   0.0703   0.9005
  13.500   1.1851   0.03803   0.03231   0.0033   0.0645   0.9378
  13.750   1.2141   0.04001   0.03431  -0.0011   0.0570   0.9648
  14.250   1.2359   0.04288   0.03719  -0.0007   0.0503   1.0000
  14.750   1.2551   0.04576   0.04010   0.0003   0.0448   1.0000
  15.250   1.2730   0.04885   0.04324   0.0010   0.0409   1.0000
  15.750   1.2891   0.05215   0.04656   0.0017   0.0357   1.0000
  16.000   1.2975   0.05382   0.04826   0.0020   0.0342   1.0000
  16.250   1.3061   0.05548   0.04995   0.0022   0.0327   1.0000
  16.500   1.3126   0.05735   0.05184   0.0025   0.0306   1.0000
  16.750   1.3202   0.05918   0.05371   0.0026   0.0293   1.0000
  17.000   1.3275   0.06103   0.05559   0.0027   0.0276   1.0000
  17.250   1.3325   0.06313   0.05771   0.0028   0.0257   1.0000
  17.500   1.3389   0.06514   0.05977   0.0028   0.0245   1.0000
  17.750   1.3451   0.06718   0.06185   0.0028   0.0232   1.0000
  18.000   1.3485   0.06958   0.06428   0.0027   0.0214   1.0000
  18.250   1.3534   0.07184   0.06658   0.0025   0.0198   1.0000
  18.500   1.3560   0.07438   0.06915   0.0023   0.0184   1.0000
  18.750   1.3596   0.07685   0.07167   0.0020   0.0171   1.0000
  19.000   1.3620   0.07950   0.07437   0.0017   0.0159   1.0000
  19.250   1.3633   0.08234   0.07725   0.0012   0.0145   1.0000
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