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RONCZ 1082 VOYAGER ROOT OUTER AFT WING AIRFOIL (r1082-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: RONCZ 1082 VOYAGER ROOT OUTER AFT WING AIRFOIL (r1082-il)
Reynolds number: 1,000,000
Max Cl/Cd: 127.14 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-r1082-il-1000000-n5.txt
Download as CSV file: xf-r1082-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.000  -0.7019   0.11051   0.10807  -0.0577   1.0000   0.0070
 -17.750  -0.7481   0.09801   0.09539  -0.0641   1.0000   0.0070
 -17.500  -0.7894   0.08665   0.08386  -0.0701   1.0000   0.0069
 -17.250  -0.8181   0.07763   0.07467  -0.0750   1.0000   0.0068
 -17.000  -0.8402   0.06923   0.06612  -0.0806   0.9998   0.0068
 -16.750  -0.8577   0.06083   0.05753  -0.0874   0.9988   0.0069
 -16.500  -0.8762   0.05530   0.05187  -0.0891   0.9924   0.0068
 -16.250  -0.8697   0.04962   0.04602  -0.0962   0.9516   0.0069
 -16.000  -0.8159   0.04295   0.03906  -0.1143   0.9225   0.0070
 -15.750  -0.7757   0.03800   0.03360  -0.1273   0.8591   0.0070
 -15.500  -0.7713   0.03628   0.03161  -0.1273   0.8144   0.0071
 -15.250  -0.7691   0.03457   0.02973  -0.1267   0.7892   0.0072
 -15.000  -0.7712   0.03261   0.02759  -0.1258   0.7704   0.0071
 -14.750  -0.7667   0.03121   0.02605  -0.1248   0.7545   0.0072
 -14.500  -0.7628   0.02982   0.02454  -0.1237   0.7410   0.0073
 -14.250  -0.7593   0.02844   0.02303  -0.1223   0.7288   0.0073
 -14.000  -0.7525   0.02730   0.02179  -0.1210   0.7188   0.0073
 -13.500  -0.7357   0.02535   0.01963  -0.1183   0.6985   0.0075
 -13.250  -0.7261   0.02448   0.01866  -0.1169   0.6902   0.0076
 -13.000  -0.7181   0.02349   0.01758  -0.1152   0.6833   0.0076
 -12.750  -0.7072   0.02271   0.01670  -0.1137   0.6762   0.0076
 -12.500  -0.6950   0.02200   0.01592  -0.1123   0.6704   0.0078
 -12.250  -0.6824   0.02132   0.01517  -0.1108   0.6644   0.0079
 -12.000  -0.6713   0.02057   0.01433  -0.1091   0.6587   0.0080
 -11.750  -0.6579   0.01995   0.01364  -0.1076   0.6540   0.0080
 -11.500  -0.6439   0.01935   0.01297  -0.1061   0.6491   0.0081
 -11.250  -0.6302   0.01876   0.01231  -0.1045   0.6442   0.0082
 -10.750  -0.5990   0.01778   0.01120  -0.1016   0.6363   0.0085
 -10.500  -0.5843   0.01724   0.01060  -0.1000   0.6323   0.0085
 -10.250  -0.5682   0.01678   0.01008  -0.0985   0.6284   0.0086
 -10.000  -0.5517   0.01638   0.00962  -0.0970   0.6248   0.0087
  -9.750  -0.5350   0.01597   0.00916  -0.0955   0.6215   0.0088
  -9.500  -0.5199   0.01546   0.00860  -0.0937   0.6185   0.0090
  -9.250  -0.5040   0.01504   0.00814  -0.0920   0.6151   0.0092
  -9.000  -0.4881   0.01464   0.00769  -0.0902   0.6119   0.0094
  -8.750  -0.4715   0.01434   0.00736  -0.0884   0.6088   0.0097
  -8.500  -0.4551   0.01407   0.00705  -0.0865   0.6061   0.0099
  -8.250  -0.4375   0.01380   0.00675  -0.0849   0.6041   0.0101
  -8.000  -0.4177   0.01353   0.00646  -0.0836   0.6018   0.0103
  -7.750  -0.3973   0.01326   0.00615  -0.0825   0.5995   0.0105
  -7.500  -0.3762   0.01301   0.00587  -0.0814   0.5972   0.0108
  -7.250  -0.3547   0.01278   0.00560  -0.0805   0.5949   0.0111
  -7.000  -0.3328   0.01256   0.00535  -0.0796   0.5927   0.0113
  -6.500  -0.2892   0.01206   0.00481  -0.0777   0.5889   0.0123
  -6.250  -0.2661   0.01185   0.00459  -0.0770   0.5874   0.0128
  -6.000  -0.2427   0.01165   0.00438  -0.0763   0.5857   0.0135
  -5.750  -0.2189   0.01147   0.00418  -0.0757   0.5839   0.0142
  -5.500  -0.1956   0.01126   0.00397  -0.0751   0.5819   0.0158
  -5.250  -0.1717   0.01109   0.00379  -0.0745   0.5799   0.0176
  -5.000  -0.1484   0.01088   0.00360  -0.0738   0.5781   0.0226
  -4.750  -0.1254   0.01066   0.00342  -0.0731   0.5764   0.0339
  -4.500  -0.1020   0.01045   0.00326  -0.0724   0.5747   0.0456
  -4.250  -0.0779   0.01028   0.00312  -0.0719   0.5732   0.0570
  -4.000  -0.0534   0.01008   0.00299  -0.0715   0.5722   0.0700
  -3.750  -0.0286   0.00990   0.00287  -0.0711   0.5711   0.0854
  -3.500  -0.0044   0.00968   0.00274  -0.0706   0.5699   0.1083
  -3.250   0.0199   0.00946   0.00263  -0.0702   0.5686   0.1348
  -3.000   0.0436   0.00921   0.00251  -0.0696   0.5673   0.1717
  -2.750   0.0674   0.00895   0.00239  -0.0691   0.5660   0.2139
  -2.500   0.0902   0.00862   0.00227  -0.0685   0.5647   0.2719
  -2.250   0.1122   0.00823   0.00214  -0.0677   0.5633   0.3484
  -2.000   0.1344   0.00784   0.00201  -0.0670   0.5619   0.4279
  -1.750   0.1572   0.00748   0.00190  -0.0664   0.5605   0.5040
  -1.500   0.1801   0.00713   0.00179  -0.0657   0.5590   0.5826
  -1.250   0.2037   0.00686   0.00178  -0.0650   0.5575   0.6622
  -1.000   0.2311   0.00683   0.00183  -0.0651   0.5566   0.6937
  -0.750   0.2595   0.00685   0.00187  -0.0653   0.5558   0.7102
  -0.500   0.2880   0.00687   0.00190  -0.0655   0.5549   0.7213
  -0.250   0.3168   0.00692   0.00193  -0.0658   0.5539   0.7318
   0.000   0.3451   0.00696   0.00199  -0.0660   0.5528   0.7412
   0.250   0.3738   0.00702   0.00203  -0.0663   0.5517   0.7490
   0.500   0.4020   0.00706   0.00209  -0.0664   0.5504   0.7548
   0.750   0.4305   0.00711   0.00214  -0.0667   0.5491   0.7590
   1.000   0.4590   0.00716   0.00217  -0.0670   0.5479   0.7623
   1.250   0.4876   0.00721   0.00220  -0.0673   0.5467   0.7649
   1.500   0.5159   0.00725   0.00224  -0.0675   0.5455   0.7672
   1.750   0.5439   0.00730   0.00228  -0.0677   0.5440   0.7695
   2.000   0.5719   0.00736   0.00234  -0.0679   0.5424   0.7716
   2.250   0.6001   0.00742   0.00239  -0.0682   0.5408   0.7732
   2.500   0.6286   0.00744   0.00243  -0.0685   0.5394   0.7746
   2.750   0.6569   0.00747   0.00247  -0.0688   0.5376   0.7759
   3.000   0.6852   0.00750   0.00251  -0.0691   0.5356   0.7772
   3.250   0.7132   0.00754   0.00256  -0.0693   0.5334   0.7784
   3.500   0.7410   0.00758   0.00260  -0.0695   0.5311   0.7795
   3.750   0.7684   0.00763   0.00265  -0.0697   0.5286   0.7805
   4.000   0.7954   0.00771   0.00270  -0.0697   0.5258   0.7815
   4.250   0.8233   0.00775   0.00277  -0.0699   0.5235   0.7825
   4.500   0.8510   0.00777   0.00283  -0.0701   0.5206   0.7838
   4.750   0.8782   0.00781   0.00288  -0.0702   0.5171   0.7850
   5.000   0.9045   0.00786   0.00295  -0.0702   0.5132   0.7861
   5.250   0.9303   0.00793   0.00302  -0.0700   0.5092   0.7873
   5.500   0.9575   0.00797   0.00310  -0.0701   0.5046   0.7884
   5.750   0.9831   0.00803   0.00318  -0.0699   0.4983   0.7896
   6.000   1.0081   0.00811   0.00327  -0.0696   0.4925   0.7908
   6.250   1.0332   0.00819   0.00336  -0.0693   0.4837   0.7920
   6.500   1.0565   0.00831   0.00347  -0.0687   0.4731   0.7934
   6.750   1.0778   0.00848   0.00360  -0.0677   0.4582   0.7949
   7.000   1.0937   0.00877   0.00381  -0.0656   0.4348   0.7966
   7.250   1.1020   0.00918   0.00409  -0.0621   0.4063   0.7982
   7.500   1.1096   0.00966   0.00445  -0.0585   0.3806   0.7996
   7.750   1.1158   0.01021   0.00490  -0.0548   0.3554   0.8014
   8.000   1.1210   0.01079   0.00539  -0.0509   0.3299   0.8034
   8.250   1.1247   0.01143   0.00593  -0.0470   0.3061   0.8055
   8.500   1.1270   0.01213   0.00655  -0.0430   0.2829   0.8077
   8.750   1.1285   0.01290   0.00724  -0.0390   0.2623   0.8101
   9.000   1.1307   0.01371   0.00799  -0.0354   0.2436   0.8125
   9.250   1.1339   0.01457   0.00880  -0.0322   0.2282   0.8150
   9.750   1.1356   0.01675   0.01089  -0.0257   0.1957   0.8202
  10.000   1.1383   0.01789   0.01202  -0.0231   0.1832   0.8230
  10.250   1.1394   0.01921   0.01331  -0.0205   0.1695   0.8260
  10.500   1.1413   0.02058   0.01465  -0.0181   0.1573   0.8291
  10.750   1.1427   0.02206   0.01609  -0.0159   0.1449   0.8321
  11.000   1.1464   0.02345   0.01747  -0.0140   0.1343   0.8351
  11.250   1.1493   0.02492   0.01894  -0.0121   0.1238   0.8386
  11.500   1.1500   0.02655   0.02055  -0.0102   0.1118   0.8425
  11.750   1.1545   0.02802   0.02202  -0.0087   0.1047   0.8465
  12.000   1.1562   0.02972   0.02368  -0.0071   0.0939   0.8505
  12.250   1.1639   0.03100   0.02501  -0.0059   0.0891   0.8555
  12.500   1.1655   0.03275   0.02673  -0.0044   0.0789   0.8614
  13.000   1.1749   0.03591   0.02992  -0.0020   0.0650   0.8749
  13.500   1.1865   0.03896   0.03304   0.0000   0.0550   0.8957
  13.750   1.1912   0.04057   0.03473   0.0011   0.0502   0.9175
  14.000   1.2126   0.04233   0.03660  -0.0014   0.0456   0.9518
  15.000   1.2537   0.04948   0.04380  -0.0026   0.0330   1.0000
  15.250   1.2612   0.05121   0.04555  -0.0022   0.0306   1.0000
  15.500   1.2676   0.05308   0.04743  -0.0019   0.0280   1.0000
  15.750   1.2742   0.05496   0.04934  -0.0017   0.0265   1.0000
  16.000   1.2823   0.05671   0.05112  -0.0015   0.0246   1.0000
  16.250   1.2863   0.05891   0.05332  -0.0013   0.0219   1.0000
  16.500   1.2926   0.06089   0.05533  -0.0012   0.0199   1.0000
  16.750   1.2983   0.06295   0.05742  -0.0011   0.0184   1.0000
  17.000   1.3031   0.06515   0.05966  -0.0011   0.0167   1.0000
  17.250   1.3072   0.06746   0.06199  -0.0011   0.0145   1.0000
  17.500   1.3107   0.06987   0.06442  -0.0012   0.0130   1.0000
  17.750   1.3150   0.07223   0.06682  -0.0014   0.0120   1.0000
  18.000   1.3185   0.07469   0.06932  -0.0016   0.0108   1.0000
  18.250   1.3216   0.07726   0.07194  -0.0019   0.0102   1.0000
  18.500   1.3248   0.07983   0.07456  -0.0023   0.0093   1.0000
  18.750   1.3274   0.08255   0.07734  -0.0027   0.0090   1.0000
  19.000   1.3298   0.08530   0.08014  -0.0033   0.0084   1.0000
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