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RONCZ 1082T VOYAGER TIP OUTER AFT WING AIRFOIL (r1082t-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: RONCZ 1082T VOYAGER TIP OUTER AFT WING AIRFOIL (r1082t-il)
Reynolds number: 500,000
Max Cl/Cd: 101.58 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-r1082t-il-500000-n5.txt
Download as CSV file: xf-r1082t-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.6094   0.06931   0.06660  -0.0711   1.0000   0.0086
 -13.250  -0.6530   0.05716   0.05417  -0.0799   1.0000   0.0086
 -13.000  -0.6544   0.05306   0.04999  -0.0828   0.9872   0.0087
 -12.750  -0.6634   0.04253   0.03887  -0.0966   0.9349   0.0086
 -12.500  -0.6265   0.03708   0.03292  -0.1094   0.8950   0.0087
 -12.250  -0.6172   0.03502   0.03047  -0.1108   0.8444   0.0089
 -12.000  -0.6203   0.03335   0.02852  -0.1087   0.8136   0.0090
 -11.750  -0.6214   0.03190   0.02682  -0.1064   0.7907   0.0091
 -11.500  -0.6232   0.03028   0.02495  -0.1039   0.7735   0.0092
 -11.250  -0.6221   0.02880   0.02323  -0.1013   0.7588   0.0092
 -11.000  -0.6189   0.02743   0.02163  -0.0987   0.7466   0.0093
 -10.750  -0.6130   0.02620   0.02018  -0.0963   0.7360   0.0094
 -10.500  -0.6052   0.02503   0.01883  -0.0940   0.7264   0.0095
 -10.250  -0.5956   0.02400   0.01761  -0.0917   0.7179   0.0096
 -10.000  -0.5843   0.02304   0.01648  -0.0896   0.7098   0.0097
  -9.750  -0.5719   0.02222   0.01550  -0.0875   0.7028   0.0098
  -9.500  -0.5576   0.02144   0.01458  -0.0856   0.6959   0.0100
  -9.250  -0.5417   0.02065   0.01364  -0.0840   0.6895   0.0101
  -9.000  -0.5239   0.01999   0.01285  -0.0827   0.6839   0.0103
  -8.750  -0.5053   0.01938   0.01213  -0.0814   0.6780   0.0104
  -8.250  -0.4686   0.01801   0.01057  -0.0789   0.6676   0.0106
  -8.000  -0.4509   0.01728   0.00978  -0.0775   0.6626   0.0109
  -7.750  -0.4315   0.01678   0.00921  -0.0764   0.6581   0.0111
  -7.500  -0.4113   0.01630   0.00868  -0.0753   0.6542   0.0114
  -7.250  -0.3904   0.01586   0.00819  -0.0744   0.6503   0.0117
  -7.000  -0.3694   0.01542   0.00769  -0.0734   0.6464   0.0119
  -6.750  -0.3480   0.01503   0.00724  -0.0724   0.6429   0.0123
  -6.500  -0.3262   0.01467   0.00681  -0.0715   0.6397   0.0127
  -6.250  -0.3034   0.01434   0.00643  -0.0708   0.6367   0.0131
  -6.000  -0.2809   0.01397   0.00602  -0.0701   0.6335   0.0136
  -5.750  -0.2587   0.01359   0.00561  -0.0693   0.6305   0.0144
  -5.500  -0.2355   0.01331   0.00528  -0.0686   0.6275   0.0149
  -5.250  -0.2119   0.01306   0.00497  -0.0679   0.6248   0.0156
  -5.000  -0.1877   0.01281   0.00468  -0.0674   0.6222   0.0164
  -4.750  -0.1637   0.01253   0.00439  -0.0669   0.6195   0.0180
  -4.500  -0.1392   0.01231   0.00414  -0.0664   0.6170   0.0201
  -4.250  -0.1150   0.01205   0.00390  -0.0659   0.6146   0.0257
  -4.000  -0.0920   0.01171   0.00366  -0.0652   0.6124   0.0483
  -3.750  -0.0684   0.01143   0.00347  -0.0646   0.6103   0.0740
  -3.250  -0.0204   0.01089   0.00315  -0.0637   0.6066   0.1372
  -3.000   0.0032   0.01055   0.00300  -0.0632   0.6047   0.1860
  -2.750   0.0248   0.01006   0.00282  -0.0625   0.6028   0.2692
  -2.500   0.0442   0.00940   0.00262  -0.0614   0.6008   0.3914
  -2.250   0.0617   0.00862   0.00240  -0.0599   0.5987   0.5405
  -2.000   0.0819   0.00819   0.00243  -0.0585   0.5968   0.6623
  -1.750   0.1082   0.00822   0.00253  -0.0581   0.5950   0.7070
  -1.500   0.1360   0.00828   0.00255  -0.0582   0.5934   0.7253
  -1.250   0.1640   0.00835   0.00259  -0.0582   0.5919   0.7379
  -1.000   0.1920   0.00841   0.00264  -0.0583   0.5904   0.7481
  -0.750   0.2200   0.00848   0.00269  -0.0583   0.5888   0.7593
  -0.500   0.2477   0.00858   0.00278  -0.0583   0.5872   0.7709
  -0.250   0.2753   0.00867   0.00288  -0.0582   0.5856   0.7790
   0.000   0.3033   0.00874   0.00293  -0.0582   0.5838   0.7854
   0.250   0.3316   0.00880   0.00294  -0.0585   0.5820   0.7898
   0.500   0.3596   0.00884   0.00298  -0.0586   0.5805   0.7926
   0.750   0.3879   0.00890   0.00302  -0.0588   0.5791   0.7953
   1.000   0.4162   0.00897   0.00306  -0.0590   0.5777   0.7980
   1.250   0.4447   0.00904   0.00310  -0.0593   0.5762   0.8007
   1.500   0.4730   0.00907   0.00314  -0.0595   0.5746   0.8031
   1.750   0.5014   0.00911   0.00318  -0.0598   0.5729   0.8052
   2.000   0.5296   0.00915   0.00322  -0.0601   0.5712   0.8068
   2.250   0.5576   0.00918   0.00328  -0.0603   0.5692   0.8082
   2.500   0.5856   0.00922   0.00333  -0.0605   0.5672   0.8097
   2.750   0.6135   0.00927   0.00338  -0.0607   0.5650   0.8112
   3.000   0.6416   0.00933   0.00343  -0.0609   0.5627   0.8126
   3.250   0.6695   0.00940   0.00350  -0.0611   0.5603   0.8141
   3.500   0.6970   0.00943   0.00358  -0.0612   0.5576   0.8159
   3.750   0.7244   0.00946   0.00365  -0.0613   0.5544   0.8177
   4.000   0.7518   0.00950   0.00371  -0.0614   0.5512   0.8193
   4.250   0.7792   0.00956   0.00376  -0.0616   0.5477   0.8208
   4.500   0.8064   0.00962   0.00383  -0.0616   0.5441   0.8222
   4.750   0.8328   0.00963   0.00393  -0.0616   0.5396   0.8235
   5.000   0.8590   0.00966   0.00400  -0.0614   0.5345   0.8250
   5.250   0.8849   0.00973   0.00407  -0.0612   0.5294   0.8267
   5.500   0.9108   0.00975   0.00418  -0.0610   0.5229   0.8286
   5.750   0.9359   0.00981   0.00425  -0.0606   0.5158   0.8303
   6.000   0.9615   0.00986   0.00436  -0.0604   0.5079   0.8321
   6.250   0.9858   0.00994   0.00446  -0.0599   0.4987   0.8340
   6.500   1.0097   0.01003   0.00457  -0.0594   0.4864   0.8359
   6.750   1.0320   0.01016   0.00469  -0.0586   0.4692   0.8378
   7.000   1.0497   0.01039   0.00486  -0.0568   0.4414   0.8398
   7.250   1.0593   0.01090   0.00519  -0.0536   0.4007   0.8424
   7.500   1.0647   0.01156   0.00567  -0.0498   0.3614   0.8458
   7.750   1.0682   0.01216   0.00615  -0.0456   0.3295   0.8494
   8.000   1.0714   0.01287   0.00672  -0.0415   0.2990   0.8530
   8.250   1.0748   0.01358   0.00735  -0.0376   0.2725   0.8564
   8.500   1.0779   0.01432   0.00803  -0.0339   0.2479   0.8604
   8.750   1.0794   0.01519   0.00881  -0.0301   0.2232   0.8653
   9.000   1.0828   0.01606   0.00963  -0.0269   0.2039   0.8701
   9.250   1.0843   0.01704   0.01058  -0.0235   0.1855   0.8758
   9.500   1.0875   0.01806   0.01158  -0.0207   0.1693   0.8829
   9.750   1.0885   0.01926   0.01275  -0.0178   0.1512   0.8910
  10.250   1.0930   0.02179   0.01528  -0.0129   0.1211   0.9146
  10.500   1.0998   0.02318   0.01668  -0.0117   0.1068   0.9364
  10.750   1.1172   0.02490   0.01836  -0.0134   0.0897   0.9880
  11.000   1.1216   0.02636   0.01978  -0.0117   0.0793   1.0000
  11.250   1.1286   0.02780   0.02122  -0.0107   0.0706   1.0000
  11.500   1.1359   0.02926   0.02266  -0.0096   0.0635   1.0000
  11.750   1.1425   0.03078   0.02416  -0.0086   0.0572   1.0000
  12.000   1.1512   0.03217   0.02557  -0.0078   0.0523   1.0000
  12.250   1.1583   0.03370   0.02710  -0.0069   0.0476   1.0000
  12.500   1.1664   0.03518   0.02861  -0.0062   0.0435   1.0000
  13.000   1.1813   0.03834   0.03180  -0.0048   0.0359   1.0000
  13.250   1.1878   0.04006   0.03352  -0.0041   0.0324   1.0000
  13.500   1.1960   0.04165   0.03515  -0.0036   0.0294   1.0000
  13.750   1.2025   0.04344   0.03696  -0.0031   0.0266   1.0000
  14.000   1.2102   0.04514   0.03870  -0.0027   0.0240   1.0000
  14.250   1.2157   0.04709   0.04067  -0.0023   0.0212   1.0000
  14.500   1.2230   0.04890   0.04252  -0.0019   0.0190   1.0000
  14.750   1.2282   0.05094   0.04460  -0.0016   0.0170   1.0000
  15.000   1.2345   0.05292   0.04662  -0.0014   0.0153   1.0000
  15.250   1.2386   0.05516   0.04890  -0.0012   0.0137   1.0000
  15.500   1.2444   0.05728   0.05107  -0.0011   0.0126   1.0000
  15.750   1.2486   0.05959   0.05344  -0.0011   0.0117   1.0000
  16.000   1.2523   0.06200   0.05591  -0.0011   0.0111   1.0000
  16.250   1.2564   0.06444   0.05842  -0.0012   0.0105   1.0000
  16.500   1.2608   0.06687   0.06093  -0.0014   0.0100   1.0000
  16.750   1.2637   0.06953   0.06367  -0.0017   0.0096   1.0000
  17.000   1.2659   0.07229   0.06650  -0.0020   0.0091   1.0000
  17.250   1.2663   0.07537   0.06966  -0.0025   0.0088   1.0000
  17.500   1.2673   0.07843   0.07279  -0.0031   0.0086   1.0000
  17.750   1.2674   0.08169   0.07615  -0.0038   0.0083   1.0000
  18.000   1.2674   0.08501   0.07957  -0.0046   0.0081   1.0000
  18.250   1.2675   0.08836   0.08303  -0.0055   0.0080   1.0000
  18.500   1.2664   0.09196   0.08673  -0.0066   0.0078   1.0000
  18.750   1.2648   0.09571   0.09058  -0.0078   0.0077   1.0000
  19.000   1.2617   0.09975   0.09473  -0.0092   0.0075   1.0000
  19.250   1.2584   0.10388   0.09896  -0.0108   0.0074   1.0000
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