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RONCZ 1082 VOYAGER ROOT OUTER AFT WING AIRFOIL (r1082-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: RONCZ 1082 VOYAGER ROOT OUTER AFT WING AIRFOIL (r1082-il)
Reynolds number: 500,000
Max Cl/Cd: 102.23 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-r1082-il-500000-n5.txt
Download as CSV file: xf-r1082-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.6409   0.08889   0.08582  -0.0705   1.0000   0.0093
 -15.750  -0.6960   0.07391   0.07047  -0.0796   1.0000   0.0091
 -15.500  -0.7149   0.06681   0.06321  -0.0840   1.0000   0.0091
 -15.250  -0.7293   0.06043   0.05667  -0.0884   0.9995   0.0091
 -15.000  -0.7433   0.05468   0.05075  -0.0910   0.9691   0.0091
 -14.750  -0.7192   0.04825   0.04405  -0.1032   0.9343   0.0092
 -14.500  -0.6721   0.04232   0.03775  -0.1188   0.9057   0.0093
 -14.250  -0.6473   0.03862   0.03360  -0.1263   0.8525   0.0094
 -14.000  -0.6453   0.03681   0.03151  -0.1260   0.8167   0.0094
 -13.500  -0.6436   0.03358   0.02789  -0.1236   0.7758   0.0096
 -13.250  -0.6406   0.03217   0.02631  -0.1222   0.7609   0.0097
 -13.000  -0.6374   0.03072   0.02469  -0.1207   0.7484   0.0097
 -12.750  -0.6314   0.02955   0.02337  -0.1192   0.7373   0.0098
 -12.500  -0.6245   0.02846   0.02214  -0.1177   0.7268   0.0100
 -12.250  -0.6169   0.02737   0.02092  -0.1161   0.7176   0.0101
 -12.000  -0.6088   0.02632   0.01973  -0.1144   0.7089   0.0102
 -11.750  -0.5987   0.02541   0.01870  -0.1128   0.7011   0.0102
 -11.500  -0.5879   0.02456   0.01773  -0.1113   0.6936   0.0104
 -11.250  -0.5769   0.02369   0.01675  -0.1096   0.6874   0.0106
 -11.000  -0.5635   0.02300   0.01595  -0.1082   0.6814   0.0108
 -10.750  -0.5493   0.02240   0.01522  -0.1067   0.6757   0.0111
 -10.500  -0.5365   0.02163   0.01436  -0.1051   0.6707   0.0111
 -10.250  -0.5219   0.02099   0.01363  -0.1036   0.6657   0.0114
 -10.000  -0.5089   0.02027   0.01285  -0.1019   0.6610   0.0115
  -9.750  -0.4966   0.01955   0.01206  -0.1000   0.6568   0.0118
  -9.500  -0.4821   0.01893   0.01140  -0.0984   0.6529   0.0120
  -9.250  -0.4666   0.01840   0.01081  -0.0968   0.6489   0.0122
  -9.000  -0.4511   0.01790   0.01025  -0.0951   0.6450   0.0124
  -8.750  -0.4355   0.01743   0.00971  -0.0934   0.6415   0.0127
  -8.500  -0.4196   0.01698   0.00920  -0.0917   0.6383   0.0130
  -8.250  -0.4036   0.01656   0.00873  -0.0899   0.6349   0.0133
  -8.000  -0.3875   0.01621   0.00833  -0.0881   0.6315   0.0136
  -7.750  -0.3713   0.01588   0.00794  -0.0863   0.6283   0.0138
  -7.500  -0.3538   0.01557   0.00756  -0.0846   0.6255   0.0142
  -7.250  -0.3357   0.01519   0.00714  -0.0832   0.6229   0.0148
  -7.000  -0.3156   0.01487   0.00679  -0.0820   0.6207   0.0152
  -6.750  -0.2950   0.01457   0.00646  -0.0809   0.6183   0.0160
  -6.500  -0.2738   0.01430   0.00616  -0.0799   0.6158   0.0171
  -6.250  -0.2529   0.01401   0.00585  -0.0789   0.6136   0.0183
  -6.000  -0.2314   0.01375   0.00556  -0.0779   0.6113   0.0202
  -5.750  -0.2101   0.01349   0.00528  -0.0769   0.6092   0.0231
  -5.500  -0.1887   0.01323   0.00503  -0.0759   0.6073   0.0291
  -5.250  -0.1669   0.01296   0.00479  -0.0750   0.6056   0.0387
  -5.000  -0.1447   0.01270   0.00458  -0.0742   0.6037   0.0505
  -4.750  -0.1220   0.01246   0.00439  -0.0735   0.6018   0.0639
  -4.500  -0.0995   0.01221   0.00421  -0.0727   0.5997   0.0798
  -4.250  -0.0766   0.01198   0.00405  -0.0720   0.5977   0.0982
  -4.000  -0.0542   0.01172   0.00388  -0.0713   0.5959   0.1229
  -3.750  -0.0322   0.01144   0.00372  -0.0705   0.5943   0.1563
  -3.500  -0.0113   0.01109   0.00355  -0.0695   0.5927   0.2058
  -3.250   0.0092   0.01070   0.00338  -0.0685   0.5912   0.2667
  -3.000   0.0284   0.01023   0.00320  -0.0673   0.5898   0.3477
  -2.750   0.0483   0.00976   0.00302  -0.0662   0.5885   0.4273
  -2.500   0.0676   0.00924   0.00285  -0.0649   0.5871   0.5192
  -2.250   0.0873   0.00878   0.00278  -0.0636   0.5857   0.6147
  -2.000   0.1114   0.00870   0.00292  -0.0628   0.5843   0.6819
  -1.750   0.1387   0.00876   0.00300  -0.0627   0.5829   0.7071
  -1.500   0.1665   0.00882   0.00304  -0.0627   0.5813   0.7217
  -1.250   0.1945   0.00888   0.00304  -0.0628   0.5797   0.7328
  -1.000   0.2223   0.00897   0.00311  -0.0628   0.5782   0.7421
  -0.750   0.2502   0.00907   0.00317  -0.0629   0.5769   0.7520
  -0.500   0.2780   0.00920   0.00328  -0.0629   0.5757   0.7623
  -0.250   0.3058   0.00933   0.00339  -0.0629   0.5744   0.7699
   0.000   0.3340   0.00945   0.00349  -0.0630   0.5732   0.7754
   0.250   0.3621   0.00950   0.00353  -0.0632   0.5721   0.7796
   0.500   0.3904   0.00955   0.00355  -0.0635   0.5710   0.7830
   0.750   0.4183   0.00959   0.00360  -0.0637   0.5696   0.7852
   1.000   0.4463   0.00964   0.00365  -0.0638   0.5681   0.7874
   1.250   0.4743   0.00969   0.00371  -0.0640   0.5666   0.7896
   1.500   0.5025   0.00974   0.00376  -0.0643   0.5654   0.7918
   1.750   0.5306   0.00979   0.00380  -0.0645   0.5641   0.7939
   2.000   0.5588   0.00984   0.00384  -0.0648   0.5626   0.7957
   2.250   0.5870   0.00989   0.00387  -0.0651   0.5612   0.7974
   2.500   0.6153   0.00996   0.00391  -0.0655   0.5597   0.7989
   2.750   0.6439   0.01003   0.00396  -0.0659   0.5582   0.8002
   3.000   0.6718   0.01009   0.00403  -0.0661   0.5566   0.8015
   3.250   0.6988   0.01013   0.00411  -0.0662   0.5548   0.8027
   3.500   0.7258   0.01017   0.00419  -0.0662   0.5527   0.8039
   3.750   0.7529   0.01021   0.00427  -0.0663   0.5504   0.8051
   4.000   0.7799   0.01025   0.00433  -0.0664   0.5481   0.8063
   4.250   0.8068   0.01030   0.00440  -0.0664   0.5458   0.8078
   4.500   0.8340   0.01036   0.00446  -0.0665   0.5433   0.8093
   4.750   0.8613   0.01044   0.00454  -0.0667   0.5407   0.8108
   5.000   0.8868   0.01048   0.00464  -0.0665   0.5378   0.8122
   5.250   0.9125   0.01051   0.00473  -0.0663   0.5344   0.8136
   5.500   0.9381   0.01056   0.00480  -0.0662   0.5308   0.8150
   5.750   0.9637   0.01061   0.00485  -0.0660   0.5271   0.8163
   6.000   0.9886   0.01066   0.00495  -0.0657   0.5231   0.8176
   6.250   1.0124   0.01069   0.00506  -0.0651   0.5179   0.8189
   6.500   1.0356   0.01074   0.00514  -0.0644   0.5125   0.8205
   6.750   1.0588   0.01080   0.00525  -0.0638   0.5070   0.8222
   7.000   1.0810   0.01086   0.00537  -0.0629   0.4998   0.8238
   7.250   1.1020   0.01095   0.00548  -0.0619   0.4926   0.8255
   7.500   1.1222   0.01104   0.00562  -0.0606   0.4828   0.8273
   7.750   1.1388   0.01114   0.00574  -0.0587   0.4711   0.8293
   8.000   1.1516   0.01131   0.00589  -0.0560   0.4557   0.8315
   8.250   1.1585   0.01166   0.00617  -0.0524   0.4345   0.8338
   8.500   1.1609   0.01217   0.00660  -0.0480   0.4094   0.8363
   8.750   1.1591   0.01287   0.00721  -0.0432   0.3849   0.8393
   9.000   1.1553   0.01373   0.00798  -0.0383   0.3601   0.8430
   9.250   1.1503   0.01475   0.00892  -0.0336   0.3365   0.8469
   9.500   1.1470   0.01586   0.00996  -0.0296   0.3158   0.8504
   9.750   1.1407   0.01719   0.01125  -0.0254   0.2955   0.8542
  10.000   1.1357   0.01863   0.01265  -0.0218   0.2756   0.8585
  10.250   1.1323   0.02017   0.01415  -0.0188   0.2579   0.8632
  10.500   1.1296   0.02179   0.01574  -0.0160   0.2413   0.8678
  10.750   1.1264   0.02349   0.01743  -0.0133   0.2250   0.8733
  11.000   1.1249   0.02519   0.01912  -0.0110   0.2103   0.8795
  11.250   1.1240   0.02689   0.02082  -0.0089   0.1965   0.8866
  11.500   1.1231   0.02863   0.02256  -0.0069   0.1828   0.8961
  11.750   1.1228   0.03041   0.02435  -0.0051   0.1692   0.9083
  12.000   1.1273   0.03219   0.02615  -0.0043   0.1567   0.9260
  12.250   1.1409   0.03439   0.02834  -0.0060   0.1391   0.9498
  12.500   1.1515   0.03614   0.03010  -0.0065   0.1306   1.0000
  12.750   1.1543   0.03807   0.03199  -0.0055   0.1187   1.0000
  13.000   1.1599   0.03981   0.03371  -0.0048   0.1091   1.0000
  13.250   1.1637   0.04174   0.03561  -0.0040   0.0993   1.0000
  13.500   1.1678   0.04367   0.03749  -0.0033   0.0900   1.0000
  13.750   1.1723   0.04560   0.03940  -0.0027   0.0820   1.0000
  14.000   1.1785   0.04742   0.04120  -0.0023   0.0745   1.0000
  14.250   1.1834   0.04939   0.04317  -0.0018   0.0680   1.0000
  14.500   1.1897   0.05125   0.04502  -0.0014   0.0626   1.0000
  14.750   1.1963   0.05312   0.04691  -0.0011   0.0580   1.0000
  15.000   1.2020   0.05511   0.04891  -0.0009   0.0536   1.0000
  15.250   1.2088   0.05702   0.05083  -0.0007   0.0497   1.0000
  15.500   1.2150   0.05902   0.05287  -0.0005   0.0464   1.0000
  15.750   1.2201   0.06116   0.05502  -0.0004   0.0428   1.0000
  16.000   1.2269   0.06313   0.05703  -0.0004   0.0401   1.0000
  16.250   1.2309   0.06546   0.05938  -0.0003   0.0373   1.0000
  16.500   1.2373   0.06755   0.06152  -0.0004   0.0348   1.0000
  16.750   1.2415   0.06993   0.06392  -0.0005   0.0321   1.0000
  17.000   1.2466   0.07223   0.06627  -0.0007   0.0302   1.0000
  17.250   1.2512   0.07461   0.06869  -0.0009   0.0279   1.0000
  17.500   1.2541   0.07723   0.07136  -0.0013   0.0259   1.0000
  17.750   1.2585   0.07970   0.07388  -0.0016   0.0241   1.0000
  18.000   1.2600   0.08259   0.07681  -0.0021   0.0221   1.0000
  18.250   1.2638   0.08522   0.07951  -0.0026   0.0206   1.0000
  18.500   1.2641   0.08832   0.08265  -0.0032   0.0186   1.0000
  18.750   1.2665   0.09118   0.08558  -0.0039   0.0173   1.0000
  19.000   1.2664   0.09444   0.08889  -0.0047   0.0159   1.0000
  19.250   1.2673   0.09760   0.09212  -0.0056   0.0148   1.0000
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