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RONCZ 1046 VOYAGER CANARD AIRFOIL (r1046-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: RONCZ 1046 VOYAGER CANARD AIRFOIL (r1046-il)
Reynolds number: 500,000
Max Cl/Cd: 108.12 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-r1046-il-500000-n5.txt
Download as CSV file: xf-r1046-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RONCZ 1046 VOYAGER CANARD 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
  ------ -------- --------- --------- -------- -------- --------
 -12.000   0.0175   0.10628   0.10171  -0.1068   0.5955   0.0098
 -11.500  -0.2825   0.04248   0.03783  -0.1365   0.6005   0.0086
 -11.250  -0.3163   0.03604   0.03116  -0.1411   0.5992   0.0086
 -11.000  -0.3378   0.03289   0.02781  -0.1400   0.5977   0.0086
 -10.750  -0.3535   0.03083   0.02556  -0.1366   0.5960   0.0086
 -10.500  -0.3575   0.02890   0.02337  -0.1341   0.5944   0.0087
 -10.250  -0.3542   0.02720   0.02145  -0.1322   0.5927   0.0087
 -10.000  -0.3463   0.02569   0.01970  -0.1304   0.5910   0.0089
  -9.750  -0.3364   0.02426   0.01807  -0.1288   0.5893   0.0090
  -9.500  -0.3207   0.02329   0.01695  -0.1277   0.5876   0.0091
  -9.250  -0.3030   0.02239   0.01593  -0.1268   0.5862   0.0092
  -9.000  -0.2845   0.02151   0.01493  -0.1258   0.5848   0.0094
  -8.750  -0.2638   0.02084   0.01416  -0.1251   0.5833   0.0096
  -8.500  -0.2430   0.02014   0.01335  -0.1244   0.5818   0.0098
  -8.250  -0.2218   0.01943   0.01252  -0.1237   0.5803   0.0100
  -8.000  -0.1997   0.01880   0.01176  -0.1231   0.5789   0.0102
  -7.750  -0.1773   0.01819   0.01102  -0.1224   0.5775   0.0105
  -7.500  -0.1540   0.01767   0.01038  -0.1219   0.5761   0.0109
  -7.250  -0.1304   0.01718   0.00975  -0.1214   0.5748   0.0112
  -7.000  -0.1075   0.01663   0.00913  -0.1208   0.5735   0.0116
  -6.750  -0.0834   0.01625   0.00868  -0.1204   0.5722   0.0120
  -6.500  -0.0588   0.01585   0.00823  -0.1200   0.5710   0.0123
  -6.250  -0.0340   0.01546   0.00778  -0.1196   0.5698   0.0127
  -6.000  -0.0090   0.01508   0.00734  -0.1193   0.5685   0.0132
  -5.750   0.0161   0.01472   0.00692  -0.1189   0.5671   0.0137
  -5.500   0.0412   0.01437   0.00653  -0.1186   0.5659   0.0143
  -5.250   0.0669   0.01409   0.00622  -0.1184   0.5647   0.0149
  -5.000   0.0928   0.01385   0.00594  -0.1181   0.5636   0.0158
  -4.750   0.1188   0.01361   0.00564  -0.1179   0.5624   0.0167
  -4.500   0.1449   0.01339   0.00541  -0.1177   0.5612   0.0182
  -4.250   0.1713   0.01322   0.00519  -0.1176   0.5601   0.0199
  -4.000   0.1974   0.01302   0.00497  -0.1174   0.5591   0.0216
  -3.750   0.2239   0.01286   0.00476  -0.1173   0.5580   0.0239
  -3.500   0.2504   0.01271   0.00459  -0.1172   0.5568   0.0267
  -3.250   0.2770   0.01259   0.00444  -0.1171   0.5555   0.0301
  -3.000   0.3037   0.01244   0.00430  -0.1170   0.5546   0.0344
  -2.750   0.3304   0.01230   0.00418  -0.1170   0.5536   0.0402
  -2.500   0.3572   0.01217   0.00408  -0.1169   0.5525   0.0489
  -2.250   0.3837   0.01202   0.00399  -0.1168   0.5515   0.0640
  -2.000   0.4102   0.01187   0.00392  -0.1168   0.5505   0.0854
  -1.750   0.4367   0.01173   0.00385  -0.1167   0.5494   0.1118
  -1.500   0.4629   0.01157   0.00380  -0.1167   0.5484   0.1487
  -1.250   0.4888   0.01137   0.00376  -0.1166   0.5474   0.2018
  -1.000   0.5144   0.01116   0.00373  -0.1165   0.5463   0.2678
  -0.750   0.5394   0.01089   0.00372  -0.1163   0.5452   0.3537
  -0.500   0.5630   0.01056   0.00374  -0.1158   0.5441   0.4738
  -0.250   0.5881   0.01041   0.00377  -0.1155   0.5430   0.5463
   0.000   0.6140   0.01035   0.00381  -0.1153   0.5420   0.5951
   0.250   0.6396   0.01028   0.00386  -0.1150   0.5410   0.6449
   0.500   0.6646   0.01021   0.00394  -0.1146   0.5400   0.7039
   0.750   0.6878   0.01008   0.00403  -0.1137   0.5392   0.7734
   1.000   0.7114   0.00998   0.00415  -0.1127   0.5384   0.8421
   1.250   0.7415   0.00999   0.00429  -0.1131   0.5374   0.9007
   1.500   0.7796   0.01010   0.00442  -0.1154   0.5363   0.9394
   1.750   0.8174   0.01021   0.00451  -0.1177   0.5351   0.9606
   2.000   0.8572   0.01033   0.00461  -0.1205   0.5339   0.9750
   2.250   0.8961   0.01045   0.00471  -0.1231   0.5328   0.9839
   2.500   0.9350   0.01056   0.00479  -0.1258   0.5318   0.9885
   2.750   0.9709   0.01067   0.00488  -0.1279   0.5308   0.9933
   3.000   1.0080   0.01077   0.00496  -0.1303   0.5298   0.9972
   3.250   1.0425   0.01088   0.00504  -0.1321   0.5288   1.0000
   3.500   1.0644   0.01097   0.00512  -0.1312   0.5277   1.0000
   3.750   1.0867   0.01108   0.00521  -0.1304   0.5266   1.0000
   4.000   1.1095   0.01121   0.00531  -0.1297   0.5255   1.0000
   4.250   1.1330   0.01135   0.00544  -0.1292   0.5245   1.0000
   4.500   1.1547   0.01148   0.00559  -0.1283   0.5236   1.0000
   4.750   1.1759   0.01161   0.00575  -0.1273   0.5227   1.0000
   5.000   1.1971   0.01173   0.00590  -0.1264   0.5215   1.0000
   5.250   1.2184   0.01186   0.00607  -0.1254   0.5202   1.0000
   5.500   1.2397   0.01199   0.00622  -0.1245   0.5188   1.0000
   5.750   1.2616   0.01213   0.00639  -0.1237   0.5176   1.0000
   6.000   1.2836   0.01226   0.00655  -0.1229   0.5164   1.0000
   6.250   1.3058   0.01240   0.00671  -0.1222   0.5151   1.0000
   6.500   1.3279   0.01252   0.00685  -0.1215   0.5138   1.0000
   6.750   1.3505   0.01266   0.00702  -0.1208   0.5126   1.0000
   7.000   1.3736   0.01279   0.00716  -0.1203   0.5113   1.0000
   7.250   1.3977   0.01294   0.00730  -0.1200   0.5098   1.0000
   7.500   1.4174   0.01311   0.00753  -0.1189   0.5081   1.0000
   7.750   1.4345   0.01328   0.00778  -0.1173   0.5062   1.0000
   8.000   1.4511   0.01346   0.00802  -0.1156   0.5044   1.0000
   8.250   1.4672   0.01363   0.00825  -0.1138   0.5024   1.0000
   8.500   1.4839   0.01381   0.00848  -0.1121   0.5005   1.0000
   8.750   1.5008   0.01397   0.00868  -0.1106   0.4984   1.0000
   9.000   1.5193   0.01409   0.00881  -0.1093   0.4957   1.0000
   9.250   1.5320   0.01435   0.00912  -0.1071   0.4925   1.0000
   9.500   1.5418   0.01467   0.00954  -0.1045   0.4887   1.0000
   9.750   1.5530   0.01498   0.00989  -0.1022   0.4843   1.0000
  10.000   1.5675   0.01524   0.01015  -0.1005   0.4802   1.0000
  10.250   1.5749   0.01581   0.01084  -0.0979   0.4751   1.0000
  10.500   1.5838   0.01638   0.01145  -0.0957   0.4697   1.0000
  10.750   1.5914   0.01704   0.01215  -0.0934   0.4637   1.0000
  11.000   1.5950   0.01800   0.01318  -0.0909   0.4556   1.0000
  11.250   1.5982   0.01910   0.01431  -0.0884   0.4474   1.0000
  11.500   1.5982   0.02048   0.01571  -0.0859   0.4380   1.0000
  11.750   1.5975   0.02207   0.01734  -0.0835   0.4279   1.0000
  12.000   1.5941   0.02392   0.01921  -0.0811   0.4176   1.0000
  12.250   1.5823   0.02646   0.02173  -0.0781   0.4033   1.0000
  12.500   1.5715   0.02906   0.02433  -0.0754   0.3907   1.0000
  12.750   1.5522   0.03242   0.02765  -0.0722   0.3736   1.0000
  13.000   1.5355   0.03574   0.03094  -0.0695   0.3581   1.0000
  13.250   1.5144   0.03955   0.03469  -0.0668   0.3406   1.0000
  13.500   1.4975   0.04317   0.03826  -0.0645   0.3250   1.0000
  13.750   1.4819   0.04677   0.04181  -0.0624   0.3082   1.0000
  14.000   1.4649   0.05061   0.04558  -0.0604   0.2908   1.0000
  14.250   1.4520   0.05418   0.04910  -0.0588   0.2754   1.0000
  14.500   1.4404   0.05772   0.05258  -0.0574   0.2590   1.0000
  14.750   1.4345   0.06076   0.05558  -0.0563   0.2451   1.0000
  15.000   1.4262   0.06412   0.05889  -0.0553   0.2305   1.0000
  15.250   1.4206   0.06725   0.06197  -0.0544   0.2159   1.0000
  15.500   1.4155   0.07040   0.06509  -0.0537   0.2031   1.0000
  15.750   1.4112   0.07351   0.06814  -0.0530   0.1887   1.0000
  16.000   1.4092   0.07643   0.07104  -0.0526   0.1769   1.0000
  16.250   1.4079   0.07928   0.07387  -0.0521   0.1651   1.0000
  16.500   1.4050   0.08238   0.07693  -0.0518   0.1528   1.0000
  16.750   1.4025   0.08546   0.07998  -0.0515   0.1407   1.0000
  17.000   1.4014   0.08843   0.08291  -0.0513   0.1294   1.0000
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