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RONCZ 1082 VOYAGER ROOT OUTER AFT WING AIRFOIL (r1082-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: RONCZ 1082 VOYAGER ROOT OUTER AFT WING AIRFOIL (r1082-il)
Reynolds number: 1,000,000
Max Cl/Cd: 136.76 at α=8.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-r1082-il-1000000.txt
Download as CSV file: xf-r1082-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RONCZ 1082 VOYAGER ROOT 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.4827   0.07980   0.07775  -0.0802   0.9579   0.0109
 -15.250  -0.6426   0.07654   0.07431  -0.0771   1.0000   0.0106
 -15.000  -0.6837   0.06516   0.06270  -0.0845   1.0000   0.0103
 -14.750  -0.7106   0.05776   0.05512  -0.0888   1.0000   0.0103
 -14.500  -0.7274   0.05074   0.04787  -0.0944   0.9987   0.0103
 -14.250  -0.7487   0.04545   0.04237  -0.0956   0.9671   0.0102
 -14.000  -0.7190   0.03937   0.03593  -0.1080   0.9401   0.0103
 -13.750  -0.6592   0.03393   0.03000  -0.1251   0.9076   0.0107
 -13.500  -0.6439   0.03169   0.02727  -0.1278   0.8392   0.0107
 -13.250  -0.6443   0.03032   0.02564  -0.1258   0.8067   0.0108
 -13.000  -0.6444   0.02873   0.02383  -0.1236   0.7845   0.0107
 -12.750  -0.6399   0.02761   0.02253  -0.1217   0.7670   0.0108
 -12.500  -0.6339   0.02666   0.02141  -0.1198   0.7523   0.0110
 -12.250  -0.6271   0.02569   0.02028  -0.1178   0.7395   0.0111
 -12.000  -0.6194   0.02455   0.01899  -0.1159   0.7281   0.0111
 -11.750  -0.6090   0.02372   0.01805  -0.1142   0.7183   0.0112
 -11.500  -0.5981   0.02307   0.01726  -0.1124   0.7087   0.0113
 -11.250  -0.5862   0.02211   0.01620  -0.1107   0.7008   0.0113
 -11.000  -0.5741   0.02134   0.01530  -0.1089   0.6931   0.0114
 -10.750  -0.5629   0.02000   0.01385  -0.1071   0.6867   0.0116
 -10.500  -0.5491   0.01924   0.01301  -0.1055   0.6801   0.0116
 -10.250  -0.5375   0.01838   0.01207  -0.1035   0.6738   0.0119
 -10.000  -0.5224   0.01779   0.01143  -0.1019   0.6691   0.0119
  -9.750  -0.5082   0.01717   0.01075  -0.1001   0.6636   0.0121
  -9.500  -0.4936   0.01665   0.01017  -0.0983   0.6585   0.0124
  -9.250  -0.4777   0.01617   0.00965  -0.0966   0.6542   0.0125
  -9.000  -0.4624   0.01567   0.00910  -0.0948   0.6502   0.0127
  -8.750  -0.4467   0.01524   0.00862  -0.0930   0.6462   0.0130
  -8.500  -0.4316   0.01485   0.00816  -0.0910   0.6424   0.0133
  -8.250  -0.4168   0.01451   0.00776  -0.0889   0.6388   0.0135
  -8.000  -0.3991   0.01424   0.00747  -0.0872   0.6361   0.0139
  -7.750  -0.3802   0.01396   0.00715  -0.0858   0.6331   0.0141
  -7.500  -0.3647   0.01342   0.00655  -0.0838   0.6302   0.0145
  -7.250  -0.3465   0.01303   0.00612  -0.0823   0.6273   0.0151
  -7.000  -0.3262   0.01276   0.00581  -0.0811   0.6242   0.0155
  -6.750  -0.3049   0.01249   0.00550  -0.0801   0.6219   0.0161
  -6.500  -0.2827   0.01222   0.00522  -0.0792   0.6198   0.0168
  -6.250  -0.2600   0.01199   0.00497  -0.0784   0.6177   0.0172
  -6.000  -0.2389   0.01166   0.00462  -0.0774   0.6153   0.0185
  -5.750  -0.2161   0.01144   0.00437  -0.0766   0.6130   0.0201
  -5.500  -0.1937   0.01119   0.00412  -0.0757   0.6107   0.0231
  -5.250  -0.1719   0.01093   0.00389  -0.0748   0.6083   0.0315
  -5.000  -0.1510   0.01060   0.00367  -0.0737   0.6061   0.0559
  -4.750  -0.1281   0.01033   0.00349  -0.0730   0.6048   0.0757
  -4.500  -0.1048   0.01007   0.00334  -0.0724   0.6033   0.0961
  -4.250  -0.0809   0.00985   0.00320  -0.0718   0.6017   0.1172
  -4.000  -0.0573   0.00962   0.00306  -0.0713   0.6001   0.1440
  -3.750  -0.0340   0.00935   0.00292  -0.0706   0.5985   0.1789
  -3.500  -0.0123   0.00899   0.00277  -0.0698   0.5969   0.2332
  -3.250   0.0084   0.00856   0.00261  -0.0688   0.5954   0.3087
  -3.000   0.0274   0.00802   0.00243  -0.0676   0.5938   0.4113
  -2.750   0.0466   0.00747   0.00226  -0.0663   0.5919   0.5228
  -2.500   0.0660   0.00697   0.00218  -0.0650   0.5898   0.6444
  -2.250   0.0919   0.00689   0.00226  -0.0646   0.5888   0.7022
  -2.000   0.1201   0.00693   0.00232  -0.0647   0.5877   0.7217
  -1.750   0.1488   0.00698   0.00234  -0.0650   0.5865   0.7332
  -1.500   0.1773   0.00704   0.00240  -0.0651   0.5852   0.7415
  -1.250   0.2062   0.00712   0.00243  -0.0654   0.5840   0.7488
  -1.000   0.2348   0.00716   0.00249  -0.0656   0.5827   0.7542
  -0.750   0.2635   0.00724   0.00255  -0.0659   0.5814   0.7597
  -0.500   0.2923   0.00733   0.00259  -0.0662   0.5802   0.7650
  -0.250   0.3207   0.00739   0.00266  -0.0663   0.5789   0.7704
   0.000   0.3492   0.00751   0.00278  -0.0665   0.5775   0.7765
   0.250   0.3779   0.00767   0.00289  -0.0667   0.5758   0.7820
   0.500   0.4067   0.00777   0.00299  -0.0670   0.5741   0.7864
   0.750   0.4355   0.00786   0.00309  -0.0673   0.5730   0.7897
   1.000   0.4640   0.00791   0.00315  -0.0676   0.5722   0.7925
   1.250   0.4925   0.00795   0.00320  -0.0679   0.5711   0.7951
   1.500   0.5211   0.00799   0.00324  -0.0682   0.5698   0.7973
   1.750   0.5498   0.00804   0.00328  -0.0685   0.5685   0.7991
   2.000   0.5782   0.00806   0.00329  -0.0689   0.5670   0.8009
   2.250   0.6064   0.00805   0.00329  -0.0691   0.5653   0.8029
   2.500   0.6347   0.00808   0.00332  -0.0694   0.5636   0.8045
   2.750   0.6629   0.00811   0.00336  -0.0697   0.5619   0.8059
   3.000   0.6914   0.00818   0.00341  -0.0700   0.5599   0.8073
   3.250   0.7208   0.00832   0.00353  -0.0706   0.5574   0.8086
   3.500   0.7483   0.00831   0.00356  -0.0708   0.5559   0.8098
   3.750   0.7758   0.00832   0.00359  -0.0709   0.5542   0.8112
   4.000   0.8033   0.00833   0.00362  -0.0711   0.5520   0.8126
   4.250   0.8309   0.00834   0.00365  -0.0712   0.5496   0.8138
   4.500   0.8585   0.00835   0.00367  -0.0714   0.5472   0.8149
   4.750   0.8859   0.00839   0.00370  -0.0716   0.5446   0.8159
   5.000   0.9143   0.00852   0.00380  -0.0720   0.5411   0.8167
   5.250   0.9402   0.00847   0.00381  -0.0718   0.5388   0.8182
   5.500   0.9662   0.00844   0.00383  -0.0717   0.5356   0.8198
   5.750   0.9922   0.00843   0.00385  -0.0715   0.5321   0.8211
   6.000   1.0182   0.00845   0.00389  -0.0714   0.5286   0.8224
   6.250   1.0440   0.00853   0.00397  -0.0713   0.5245   0.8236
   6.500   1.0694   0.00852   0.00403  -0.0710   0.5206   0.8250
   6.750   1.0946   0.00853   0.00408  -0.0707   0.5159   0.8264
   7.000   1.1185   0.00860   0.00414  -0.0702   0.5107   0.8278
   7.250   1.1436   0.00862   0.00423  -0.0699   0.5054   0.8293
   7.500   1.1675   0.00867   0.00431  -0.0694   0.4987   0.8308
   7.750   1.1902   0.00875   0.00440  -0.0687   0.4908   0.8324
   8.000   1.2100   0.00887   0.00450  -0.0673   0.4792   0.8337
   8.250   1.2267   0.00897   0.00460  -0.0654   0.4646   0.8359
   8.500   1.2387   0.00920   0.00479  -0.0626   0.4429   0.8381
   8.750   1.2433   0.00967   0.00515  -0.0584   0.4156   0.8406
   9.000   1.2453   0.01027   0.00564  -0.0539   0.3890   0.8432
   9.250   1.2445   0.01099   0.00624  -0.0491   0.3601   0.8462
   9.500   1.2456   0.01170   0.00686  -0.0449   0.3375   0.8490
   9.750   1.2433   0.01254   0.00762  -0.0403   0.3136   0.8523
  10.000   1.2393   0.01350   0.00851  -0.0357   0.2915   0.8564
  10.250   1.2362   0.01456   0.00952  -0.0316   0.2712   0.8608
  10.500   1.2294   0.01592   0.01080  -0.0274   0.2501   0.8653
  10.750   1.2246   0.01733   0.01217  -0.0237   0.2314   0.8702
  11.000   1.2203   0.01884   0.01365  -0.0204   0.2139   0.8758
  11.250   1.2168   0.02046   0.01522  -0.0174   0.1972   0.8820
  11.500   1.2120   0.02218   0.01693  -0.0145   0.1809   0.8895
  11.750   1.2110   0.02378   0.01853  -0.0121   0.1686   0.8988
  12.000   1.2052   0.02564   0.02038  -0.0093   0.1522   0.9142
  12.250   1.2119   0.02725   0.02209  -0.0087   0.1409   0.9464
  12.500   1.2296   0.02956   0.02435  -0.0116   0.1225   1.0000
  12.750   1.2312   0.03145   0.02619  -0.0103   0.1108   1.0000
  13.000   1.2350   0.03320   0.02791  -0.0092   0.1019   1.0000
  13.250   1.2381   0.03506   0.02972  -0.0082   0.0934   1.0000
  13.500   1.2443   0.03670   0.03136  -0.0074   0.0866   1.0000
  13.750   1.2485   0.03852   0.03316  -0.0065   0.0795   1.0000
  14.000   1.2544   0.04024   0.03488  -0.0058   0.0738   1.0000
  14.250   1.2600   0.04201   0.03664  -0.0052   0.0679   1.0000
  14.500   1.2652   0.04383   0.03844  -0.0045   0.0627   1.0000
  14.750   1.2713   0.04562   0.04023  -0.0040   0.0580   1.0000
  15.000   1.2771   0.04744   0.04206  -0.0035   0.0537   1.0000
  15.250   1.2832   0.04930   0.04393  -0.0031   0.0500   1.0000
  15.500   1.2888   0.05119   0.04582  -0.0026   0.0460   1.0000
  15.750   1.2946   0.05311   0.04775  -0.0023   0.0432   1.0000
  16.000   1.3008   0.05501   0.04968  -0.0021   0.0402   1.0000
  16.250   1.3057   0.05706   0.05172  -0.0018   0.0369   1.0000
  16.500   1.3114   0.05909   0.05378  -0.0016   0.0344   1.0000
  16.750   1.3152   0.06131   0.05602  -0.0015   0.0316   1.0000
  17.000   1.3216   0.06329   0.05804  -0.0014   0.0295   1.0000
  17.250   1.3236   0.06578   0.06053  -0.0014   0.0264   1.0000
  17.500   1.3287   0.06797   0.06274  -0.0014   0.0238   1.0000
  17.750   1.3307   0.07054   0.06535  -0.0015   0.0216   1.0000
  18.000   1.3319   0.07325   0.06805  -0.0016   0.0187   1.0000
  18.250   1.3346   0.07581   0.07067  -0.0019   0.0172   1.0000
  18.500   1.3337   0.07884   0.07373  -0.0022   0.0149   1.0000
  18.750   1.3351   0.08169   0.07663  -0.0026   0.0139   1.0000
  19.000   1.3346   0.08479   0.07977  -0.0031   0.0129   1.0000
  19.250   1.3346   0.08791   0.08295  -0.0037   0.0122   1.0000
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