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RONCZ 1046 VOYAGER CANARD AIRFOIL (r1046-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: RONCZ 1046 VOYAGER CANARD AIRFOIL (r1046-il)
Reynolds number: 1,000,000
Max Cl/Cd: 149.63 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-r1046-il-1000000-n5.txt
Download as CSV file: xf-r1046-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.4784   0.03932   0.03505  -0.1392   0.5920   0.0062
 -13.250  -0.5062   0.03336   0.02891  -0.1434   0.5904   0.0062
 -12.750  -0.5331   0.02814   0.02340  -0.1421   0.5871   0.0063
 -12.500  -0.5355   0.02677   0.02193  -0.1397   0.5857   0.0063
 -12.250  -0.5407   0.02552   0.02057  -0.1363   0.5842   0.0063
 -12.000  -0.5342   0.02450   0.01943  -0.1342   0.5826   0.0064
 -11.750  -0.5229   0.02357   0.01838  -0.1326   0.5810   0.0065
 -11.500  -0.5128   0.02245   0.01712  -0.1309   0.5792   0.0065
 -11.250  -0.4967   0.02169   0.01625  -0.1297   0.5774   0.0065
 -11.000  -0.4805   0.02088   0.01532  -0.1286   0.5755   0.0066
 -10.750  -0.4623   0.02019   0.01452  -0.1276   0.5735   0.0066
 -10.500  -0.4454   0.01934   0.01354  -0.1264   0.5716   0.0067
 -10.250  -0.4272   0.01852   0.01261  -0.1254   0.5705   0.0068
 -10.000  -0.4074   0.01780   0.01181  -0.1245   0.5694   0.0069
  -9.750  -0.3862   0.01718   0.01110  -0.1238   0.5681   0.0071
  -9.500  -0.3636   0.01669   0.01055  -0.1232   0.5668   0.0072
  -9.250  -0.3406   0.01620   0.00999  -0.1227   0.5655   0.0072
  -9.000  -0.3174   0.01573   0.00944  -0.1221   0.5641   0.0074
  -8.750  -0.2932   0.01534   0.00899  -0.1217   0.5628   0.0075
  -8.500  -0.2690   0.01495   0.00854  -0.1213   0.5614   0.0077
  -8.250  -0.2447   0.01456   0.00808  -0.1208   0.5600   0.0078
  -8.000  -0.2200   0.01422   0.00767  -0.1205   0.5587   0.0080
  -7.750  -0.1953   0.01387   0.00725  -0.1201   0.5573   0.0082
  -7.500  -0.1702   0.01357   0.00689  -0.1197   0.5558   0.0084
  -7.250  -0.1446   0.01326   0.00653  -0.1195   0.5549   0.0086
  -7.000  -0.1187   0.01297   0.00619  -0.1193   0.5539   0.0087
  -6.750  -0.0929   0.01267   0.00585  -0.1190   0.5529   0.0089
  -6.500  -0.0673   0.01234   0.00549  -0.1187   0.5518   0.0093
  -6.250  -0.0411   0.01209   0.00521  -0.1186   0.5508   0.0096
  -6.000  -0.0146   0.01187   0.00497  -0.1184   0.5497   0.0101
  -5.750   0.0121   0.01168   0.00475  -0.1183   0.5486   0.0105
  -5.500   0.0387   0.01148   0.00452  -0.1182   0.5475   0.0110
  -5.250   0.0654   0.01129   0.00429  -0.1181   0.5465   0.0113
  -5.000   0.0919   0.01109   0.00407  -0.1179   0.5454   0.0120
  -4.750   0.1187   0.01093   0.00389  -0.1179   0.5443   0.0127
  -4.500   0.1457   0.01079   0.00372  -0.1178   0.5432   0.0137
  -4.250   0.1725   0.01065   0.00357  -0.1177   0.5421   0.0148
  -4.000   0.1994   0.01054   0.00344  -0.1176   0.5407   0.0161
  -3.750   0.2265   0.01043   0.00331  -0.1176   0.5395   0.0180
  -3.500   0.2540   0.01031   0.00320  -0.1176   0.5388   0.0205
  -3.250   0.2815   0.01019   0.00309  -0.1177   0.5380   0.0232
  -3.000   0.3089   0.01008   0.00299  -0.1177   0.5373   0.0260
  -2.750   0.3364   0.00998   0.00290  -0.1178   0.5364   0.0292
  -2.500   0.3640   0.00989   0.00282  -0.1179   0.5356   0.0335
  -2.250   0.3914   0.00979   0.00274  -0.1179   0.5347   0.0403
  -2.000   0.4186   0.00968   0.00267  -0.1180   0.5337   0.0520
  -1.750   0.4458   0.00956   0.00262  -0.1180   0.5328   0.0687
  -1.500   0.4728   0.00945   0.00257  -0.1180   0.5317   0.0904
  -1.250   0.4997   0.00933   0.00252  -0.1180   0.5306   0.1179
  -1.000   0.5265   0.00920   0.00249  -0.1180   0.5295   0.1509
  -0.750   0.5528   0.00905   0.00247  -0.1180   0.5284   0.1995
  -0.500   0.5792   0.00892   0.00246  -0.1179   0.5275   0.2503
  -0.250   0.6046   0.00870   0.00246  -0.1178   0.5264   0.3314
   0.000   0.6292   0.00844   0.00249  -0.1175   0.5253   0.4360
   0.250   0.6553   0.00835   0.00253  -0.1174   0.5243   0.4935
   0.500   0.6821   0.00827   0.00257  -0.1174   0.5237   0.5404
   0.750   0.7086   0.00818   0.00261  -0.1174   0.5230   0.5876
   1.000   0.7346   0.00808   0.00266  -0.1172   0.5221   0.6402
   1.250   0.7601   0.00797   0.00271  -0.1169   0.5212   0.6963
   1.750   0.8107   0.00783   0.00283  -0.1162   0.5193   0.7890
   2.000   0.8348   0.00774   0.00291  -0.1155   0.5184   0.8431
   2.250   0.8592   0.00769   0.00303  -0.1148   0.5175   0.9113
   2.500   0.8927   0.00776   0.00314  -0.1161   0.5165   0.9546
   2.750   0.9296   0.00786   0.00323  -0.1183   0.5155   0.9723
   3.000   0.9659   0.00795   0.00331  -0.1204   0.5144   0.9804
   3.250   1.0008   0.00804   0.00338  -0.1222   0.5132   0.9847
   3.500   1.0366   0.00814   0.00346  -0.1243   0.5121   0.9876
   3.750   1.0705   0.00825   0.00355  -0.1260   0.5110   0.9909
   4.000   1.1030   0.00837   0.00365  -0.1273   0.5099   0.9939
   4.250   1.1374   0.00847   0.00375  -0.1292   0.5089   0.9966
   4.500   1.1713   0.00855   0.00385  -0.1309   0.5081   0.9988
   4.750   1.2017   0.00863   0.00394  -0.1318   0.5072   1.0000
   5.000   1.2233   0.00870   0.00404  -0.1308   0.5061   1.0000
   5.250   1.2451   0.00878   0.00413  -0.1299   0.5051   1.0000
   5.500   1.2669   0.00885   0.00422  -0.1290   0.5040   1.0000
   5.750   1.2886   0.00893   0.00432  -0.1281   0.5027   1.0000
   6.000   1.3102   0.00901   0.00442  -0.1272   0.5012   1.0000
   6.250   1.3313   0.00910   0.00452  -0.1262   0.4997   1.0000
   6.500   1.3523   0.00920   0.00463  -0.1252   0.4982   1.0000
   6.750   1.3727   0.00931   0.00474  -0.1240   0.4964   1.0000
   7.000   1.3928   0.00945   0.00488  -0.1229   0.4944   1.0000
   7.250   1.4130   0.00953   0.00500  -0.1217   0.4931   1.0000
   7.500   1.4331   0.00963   0.00514  -0.1206   0.4917   1.0000
   7.750   1.4530   0.00973   0.00529  -0.1194   0.4898   1.0000
   8.000   1.4724   0.00984   0.00543  -0.1181   0.4873   1.0000
   8.250   1.4905   0.00998   0.00559  -0.1167   0.4842   1.0000
   8.500   1.5065   0.01017   0.00577  -0.1149   0.4808   1.0000
   8.750   1.5259   0.01031   0.00596  -0.1138   0.4764   1.0000
   9.000   1.5434   0.01050   0.00618  -0.1123   0.4711   1.0000
   9.250   1.5567   0.01080   0.00646  -0.1102   0.4657   1.0000
   9.500   1.5757   0.01101   0.00673  -0.1092   0.4605   1.0000
   9.750   1.5858   0.01144   0.00714  -0.1066   0.4517   1.0000
  10.000   1.5988   0.01186   0.00758  -0.1047   0.4420   1.0000
  10.250   1.6058   0.01251   0.00821  -0.1020   0.4307   1.0000
  10.500   1.6080   0.01343   0.00910  -0.0987   0.4170   1.0000
  10.750   1.6101   0.01448   0.01014  -0.0957   0.4054   1.0000
  11.000   1.6035   0.01612   0.01173  -0.0920   0.3878   1.0000
  11.250   1.5991   0.01785   0.01345  -0.0888   0.3744   1.0000
  11.500   1.5761   0.02096   0.01648  -0.0843   0.3522   1.0000
  11.750   1.5597   0.02390   0.01939  -0.0808   0.3364   1.0000
  12.000   1.5412   0.02714   0.02261  -0.0775   0.3212   1.0000
  12.250   1.5245   0.03038   0.02583  -0.0745   0.3057   1.0000
  12.500   1.5026   0.03417   0.02957  -0.0714   0.2888   1.0000
  13.000   1.4733   0.04091   0.03625  -0.0667   0.2613   1.0000
  13.250   1.4637   0.04396   0.03928  -0.0649   0.2478   1.0000
  13.500   1.4496   0.04745   0.04271  -0.0629   0.2310   1.0000
  13.750   1.4422   0.05044   0.04567  -0.0614   0.2184   1.0000
  14.000   1.4360   0.05336   0.04853  -0.0600   0.2045   1.0000
  14.250   1.4318   0.05612   0.05127  -0.0588   0.1923   1.0000
  14.500   1.4310   0.05858   0.05370  -0.0578   0.1814   1.0000
  14.750   1.4262   0.06152   0.05659  -0.0568   0.1690   1.0000
  15.000   1.4249   0.06410   0.05913  -0.0559   0.1574   1.0000
  15.250   1.4184   0.06726   0.06222  -0.0549   0.1421   1.0000
  15.500   1.4196   0.06966   0.06461  -0.0543   0.1337   1.0000
  15.750   1.4182   0.07237   0.06726  -0.0536   0.1216   1.0000
  16.000   1.4160   0.07524   0.07009  -0.0530   0.1105   1.0000
  16.250   1.4168   0.07780   0.07260  -0.0526   0.1001   1.0000
  16.500   1.4178   0.08034   0.07513  -0.0522   0.0915   1.0000
  16.750   1.4160   0.08327   0.07802  -0.0518   0.0814   1.0000
  17.000   1.4181   0.08577   0.08049  -0.0516   0.0742   1.0000
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