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RONCZ 1082T VOYAGER TIP OUTER AFT WING AIRFOIL (r1082t-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: RONCZ 1082T VOYAGER TIP OUTER AFT WING AIRFOIL (r1082t-il)
Reynolds number: 1,000,000
Max Cl/Cd: 122.39 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-r1082t-il-1000000-n5.txt
Download as CSV file: xf-r1082t-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RONCZ 1082T VOYAGER TIP OUTER 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
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.7438   0.07664   0.07433  -0.0653   1.0000   0.0063
 -15.250  -0.7971   0.06143   0.05882  -0.0755   1.0000   0.0063
 -15.000  -0.8341   0.05187   0.04900  -0.0816   1.0000   0.0062
 -14.750  -0.8451   0.04750   0.04450  -0.0835   1.0000   0.0062
 -14.500  -0.8467   0.04311   0.03996  -0.0871   0.9982   0.0062
 -14.250  -0.8545   0.03901   0.03567  -0.0886   0.9577   0.0062
 -14.000  -0.7974   0.03466   0.03103  -0.1031   0.9331   0.0064
 -13.750  -0.7501   0.03144   0.02731  -0.1140   0.8619   0.0064
 -13.250  -0.7496   0.02879   0.02417  -0.1100   0.7900   0.0066
 -13.000  -0.7437   0.02777   0.02300  -0.1083   0.7716   0.0066
 -12.750  -0.7452   0.02617   0.02119  -0.1058   0.7543   0.0066
 -12.500  -0.7394   0.02508   0.01996  -0.1039   0.7409   0.0066
 -12.250  -0.7305   0.02424   0.01899  -0.1021   0.7294   0.0067
 -12.000  -0.7214   0.02339   0.01802  -0.1002   0.7190   0.0068
 -11.750  -0.7110   0.02260   0.01712  -0.0984   0.7094   0.0069
 -11.500  -0.7003   0.02183   0.01623  -0.0965   0.7011   0.0070
 -11.250  -0.6902   0.02098   0.01527  -0.0945   0.6930   0.0070
 -11.000  -0.6784   0.02026   0.01444  -0.0925   0.6860   0.0072
 -10.750  -0.6662   0.01955   0.01363  -0.0905   0.6792   0.0072
 -10.500  -0.6535   0.01891   0.01287  -0.0885   0.6728   0.0074
 -10.250  -0.6400   0.01832   0.01220  -0.0864   0.6672   0.0074
 -10.000  -0.6267   0.01777   0.01156  -0.0843   0.6612   0.0075
  -9.750  -0.6120   0.01732   0.01101  -0.0823   0.6556   0.0076
  -9.500  -0.5939   0.01687   0.01049  -0.0809   0.6506   0.0077
  -9.250  -0.5762   0.01633   0.00987  -0.0795   0.6455   0.0077
  -8.750  -0.5357   0.01557   0.00898  -0.0774   0.6372   0.0079
  -8.500  -0.5178   0.01495   0.00829  -0.0760   0.6333   0.0081
  -8.250  -0.4983   0.01445   0.00773  -0.0748   0.6294   0.0082
  -8.000  -0.4780   0.01401   0.00723  -0.0737   0.6258   0.0084
  -7.750  -0.4562   0.01366   0.00683  -0.0728   0.6227   0.0086
  -7.500  -0.4336   0.01333   0.00648  -0.0721   0.6197   0.0088
  -7.250  -0.4106   0.01304   0.00615  -0.0714   0.6166   0.0090
  -7.000  -0.3878   0.01272   0.00579  -0.0707   0.6136   0.0091
  -6.750  -0.3644   0.01246   0.00549  -0.0701   0.6106   0.0094
  -6.500  -0.3409   0.01219   0.00518  -0.0694   0.6078   0.0096
  -6.250  -0.3168   0.01193   0.00488  -0.0689   0.6054   0.0099
  -6.000  -0.2925   0.01168   0.00461  -0.0684   0.6028   0.0101
  -5.750  -0.2678   0.01147   0.00436  -0.0680   0.6002   0.0104
  -5.500  -0.2433   0.01124   0.00410  -0.0675   0.5977   0.0107
  -5.250  -0.2190   0.01100   0.00384  -0.0670   0.5954   0.0113
  -5.000  -0.1942   0.01081   0.00363  -0.0666   0.5932   0.0120
  -4.750  -0.1687   0.01063   0.00343  -0.0663   0.5914   0.0128
  -4.500  -0.1428   0.01046   0.00325  -0.0660   0.5897   0.0133
  -4.250  -0.1172   0.01028   0.00306  -0.0657   0.5879   0.0144
  -4.000  -0.0914   0.01012   0.00289  -0.0655   0.5860   0.0164
  -3.750  -0.0659   0.00992   0.00273  -0.0652   0.5842   0.0226
  -3.500  -0.0412   0.00968   0.00256  -0.0648   0.5823   0.0425
  -3.250  -0.0162   0.00945   0.00242  -0.0644   0.5805   0.0652
  -3.000   0.0087   0.00923   0.00230  -0.0641   0.5785   0.0939
  -2.750   0.0335   0.00900   0.00218  -0.0637   0.5766   0.1289
  -2.500   0.0588   0.00875   0.00207  -0.0635   0.5753   0.1681
  -2.250   0.0838   0.00847   0.00197  -0.0632   0.5740   0.2183
  -2.000   0.1078   0.00810   0.00185  -0.0628   0.5726   0.2933
  -1.750   0.1292   0.00750   0.00170  -0.0621   0.5711   0.4217
  -1.500   0.1506   0.00688   0.00154  -0.0613   0.5696   0.5568
  -1.250   0.1744   0.00651   0.00149  -0.0607   0.5682   0.6506
  -1.000   0.2014   0.00645   0.00153  -0.0606   0.5667   0.6943
  -0.750   0.2294   0.00646   0.00156  -0.0607   0.5653   0.7133
  -0.500   0.2577   0.00650   0.00158  -0.0609   0.5638   0.7265
  -0.250   0.2859   0.00655   0.00162  -0.0610   0.5621   0.7378
   0.000   0.3141   0.00660   0.00168  -0.0611   0.5606   0.7481
   0.250   0.3429   0.00665   0.00171  -0.0614   0.5596   0.7566
   0.500   0.3713   0.00667   0.00177  -0.0616   0.5584   0.7626
   0.750   0.4000   0.00671   0.00181  -0.0619   0.5571   0.7671
   1.000   0.4287   0.00675   0.00183  -0.0622   0.5557   0.7707
   1.250   0.4575   0.00680   0.00186  -0.0625   0.5541   0.7734
   1.500   0.4859   0.00682   0.00190  -0.0627   0.5525   0.7761
   1.750   0.5142   0.00686   0.00194  -0.0629   0.5507   0.7786
   2.000   0.5423   0.00691   0.00198  -0.0631   0.5485   0.7807
   2.250   0.5703   0.00698   0.00202  -0.0633   0.5459   0.7823
   2.500   0.5989   0.00700   0.00206  -0.0636   0.5439   0.7839
   2.750   0.6275   0.00703   0.00210  -0.0639   0.5414   0.7853
   3.000   0.6559   0.00706   0.00214  -0.0642   0.5385   0.7866
   3.250   0.6840   0.00710   0.00218  -0.0644   0.5354   0.7878
   3.500   0.7117   0.00716   0.00223  -0.0646   0.5320   0.7890
   3.750   0.7396   0.00721   0.00229  -0.0648   0.5288   0.7903
   4.000   0.7677   0.00723   0.00234  -0.0650   0.5249   0.7917
   4.250   0.7953   0.00727   0.00240  -0.0651   0.5200   0.7929
   4.500   0.8220   0.00734   0.00246  -0.0651   0.5147   0.7942
   4.750   0.8499   0.00737   0.00254  -0.0653   0.5087   0.7954
   5.000   0.8763   0.00745   0.00261  -0.0652   0.5010   0.7968
   5.250   0.9032   0.00752   0.00269  -0.0652   0.4919   0.7982
   5.500   0.9290   0.00762   0.00279  -0.0650   0.4803   0.7999
   5.750   0.9534   0.00779   0.00290  -0.0646   0.4617   0.8015
   6.000   0.9740   0.00810   0.00309  -0.0634   0.4302   0.8030
   6.250   0.9910   0.00859   0.00340  -0.0617   0.3923   0.8046
   6.500   1.0050   0.00920   0.00381  -0.0594   0.3503   0.8061
   6.750   1.0186   0.00977   0.00421  -0.0571   0.3120   0.8080
   7.000   1.0316   0.01031   0.00462  -0.0546   0.2788   0.8100
   7.250   1.0433   0.01082   0.00501  -0.0519   0.2502   0.8120
   7.500   1.0523   0.01128   0.00538  -0.0487   0.2268   0.8144
   7.750   1.0611   0.01180   0.00581  -0.0455   0.2042   0.8171
   8.000   1.0701   0.01234   0.00627  -0.0424   0.1850   0.8198
   8.500   1.0880   0.01345   0.00727  -0.0366   0.1512   0.8248
   8.750   1.0897   0.01428   0.00800  -0.0327   0.1289   0.8280
   9.000   1.0950   0.01505   0.00872  -0.0296   0.1129   0.8314
   9.250   1.1019   0.01583   0.00947  -0.0270   0.1010   0.8348
   9.500   1.1084   0.01670   0.01032  -0.0245   0.0901   0.8382
   9.750   1.1161   0.01756   0.01118  -0.0222   0.0811   0.8420
  10.000   1.1224   0.01855   0.01217  -0.0200   0.0714   0.8466
  10.250   1.1292   0.01960   0.01320  -0.0180   0.0633   0.8516
  10.500   1.1356   0.02072   0.01432  -0.0161   0.0560   0.8567
  10.750   1.1432   0.02180   0.01543  -0.0144   0.0497   0.8627
  11.000   1.1515   0.02290   0.01655  -0.0128   0.0452   0.8689
  11.250   1.1595   0.02402   0.01771  -0.0113   0.0411   0.8765
  11.750   1.1750   0.02632   0.02011  -0.0084   0.0344   0.8986
  12.000   1.1817   0.02750   0.02138  -0.0068   0.0312   0.9216
  12.250   1.2043   0.02885   0.02284  -0.0088   0.0275   0.9607
  12.750   1.2250   0.03173   0.02574  -0.0081   0.0216   1.0000
  13.000   1.2341   0.03310   0.02713  -0.0074   0.0194   1.0000
  13.250   1.2410   0.03467   0.02871  -0.0065   0.0168   1.0000
  13.500   1.2483   0.03624   0.03029  -0.0058   0.0144   1.0000
  13.750   1.2546   0.03793   0.03200  -0.0051   0.0119   1.0000
  14.000   1.2619   0.03957   0.03367  -0.0045   0.0109   1.0000
  14.250   1.2694   0.04122   0.03535  -0.0039   0.0096   1.0000
  14.500   1.2762   0.04297   0.03713  -0.0034   0.0089   1.0000
  14.750   1.2837   0.04468   0.03888  -0.0030   0.0082   1.0000
  15.000   1.2908   0.04647   0.04072  -0.0026   0.0078   1.0000
  15.250   1.2980   0.04828   0.04257  -0.0023   0.0073   1.0000
  15.500   1.3036   0.05027   0.04461  -0.0020   0.0069   1.0000
  15.750   1.3093   0.05228   0.04666  -0.0018   0.0066   1.0000
  16.000   1.3149   0.05436   0.04880  -0.0016   0.0064   1.0000
  16.250   1.3215   0.05635   0.05085  -0.0016   0.0063   1.0000
  16.500   1.3277   0.05843   0.05299  -0.0015   0.0061   1.0000
  16.750   1.3326   0.06066   0.05528  -0.0016   0.0060   1.0000
  17.000   1.3372   0.06297   0.05765  -0.0017   0.0058   1.0000
  17.250   1.3411   0.06542   0.06018  -0.0018   0.0057   1.0000
  17.500   1.3453   0.06785   0.06267  -0.0021   0.0056   1.0000
  17.750   1.3473   0.07061   0.06550  -0.0024   0.0054   1.0000
  18.000   1.3495   0.07337   0.06833  -0.0028   0.0053   1.0000
  18.250   1.3515   0.07621   0.07124  -0.0033   0.0053   1.0000
  18.500   1.3516   0.07937   0.07447  -0.0040   0.0051   1.0000
  18.750   1.3517   0.08258   0.07775  -0.0047   0.0050   1.0000
  19.000   1.3476   0.08646   0.08172  -0.0057   0.0048   1.0000
  19.250   1.3465   0.08995   0.08530  -0.0067   0.0048   1.0000
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