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RONCZ 1082T VOYAGER TIP OUTER AFT WING AIRFOIL (r1082t-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: RONCZ 1082T VOYAGER TIP OUTER AFT WING AIRFOIL (r1082t-il)
Reynolds number: 500,000
Max Cl/Cd: 107.57 at α=8.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-r1082t-il-500000.txt
Download as CSV file: xf-r1082t-il-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.500  -0.4042   0.05251   0.04916  -0.1129   0.8394   0.0305
 -10.250  -0.4283   0.05083   0.04717  -0.1088   0.8093   0.0306
  -9.000  -0.5070   0.02883   0.02320  -0.0867   0.7458   0.0200
  -8.750  -0.4974   0.02615   0.02019  -0.0844   0.7376   0.0192
  -8.500  -0.4850   0.02253   0.01594  -0.0820   0.7303   0.0175
  -8.250  -0.4642   0.02128   0.01444  -0.0809   0.7232   0.0173
  -8.000  -0.4417   0.02003   0.01305  -0.0803   0.7170   0.0175
  -7.750  -0.4190   0.01905   0.01196  -0.0797   0.7108   0.0176
  -7.500  -0.3966   0.01823   0.01104  -0.0790   0.7054   0.0180
  -7.250  -0.3741   0.01751   0.01026  -0.0783   0.7003   0.0184
  -7.000  -0.3519   0.01680   0.00948  -0.0775   0.6952   0.0186
  -6.750  -0.3301   0.01622   0.00882  -0.0766   0.6908   0.0192
  -6.500  -0.3085   0.01568   0.00820  -0.0756   0.6866   0.0195
  -6.250  -0.2870   0.01515   0.00762  -0.0747   0.6825   0.0200
  -6.000  -0.2653   0.01471   0.00712  -0.0737   0.6784   0.0204
  -5.750  -0.2454   0.01414   0.00649  -0.0725   0.6747   0.0213
  -5.500  -0.2239   0.01373   0.00604  -0.0716   0.6712   0.0225
  -5.250  -0.2012   0.01336   0.00566  -0.0708   0.6679   0.0237
  -5.000  -0.1781   0.01304   0.00529  -0.0700   0.6646   0.0249
  -4.750  -0.1557   0.01263   0.00486  -0.0691   0.6616   0.0277
  -4.500  -0.1320   0.01235   0.00454  -0.0685   0.6589   0.0321
  -4.250  -0.1117   0.01179   0.00417  -0.0674   0.6562   0.0714
  -4.000  -0.0909   0.01128   0.00395  -0.0664   0.6538   0.1315
  -3.750  -0.0694   0.01083   0.00375  -0.0656   0.6512   0.1919
  -3.500  -0.0489   0.01030   0.00354  -0.0647   0.6487   0.2755
  -3.250  -0.0315   0.00956   0.00330  -0.0633   0.6463   0.4048
  -3.000  -0.0158   0.00874   0.00307  -0.0614   0.6439   0.5586
  -2.750   0.0037   0.00844   0.00325  -0.0597   0.6417   0.6947
  -2.500   0.0306   0.00863   0.00344  -0.0593   0.6395   0.7334
  -2.250   0.0575   0.00880   0.00359  -0.0589   0.6376   0.7561
  -2.000   0.0848   0.00897   0.00375  -0.0586   0.6356   0.7688
  -1.750   0.1124   0.00911   0.00387  -0.0585   0.6335   0.7782
  -1.500   0.1402   0.00924   0.00396  -0.0584   0.6316   0.7866
  -1.250   0.1680   0.00936   0.00405  -0.0583   0.6297   0.7932
  -1.000   0.1958   0.00952   0.00417  -0.0582   0.6279   0.8001
  -0.750   0.2234   0.00968   0.00428  -0.0580   0.6260   0.8081
  -0.500   0.2507   0.00996   0.00455  -0.0576   0.6240   0.8161
  -0.250   0.2773   0.01007   0.00466  -0.0573   0.6226   0.8235
   0.000   0.3039   0.01019   0.00481  -0.0569   0.6209   0.8282
   0.250   0.3314   0.01027   0.00488  -0.0569   0.6192   0.8325
   0.500   0.3594   0.01032   0.00491  -0.0571   0.6173   0.8365
   0.750   0.3872   0.01034   0.00491  -0.0573   0.6153   0.8394
   1.000   0.4149   0.01038   0.00495  -0.0573   0.6136   0.8417
   1.250   0.4430   0.01044   0.00499  -0.0575   0.6120   0.8440
   1.500   0.4715   0.01051   0.00504  -0.0578   0.6103   0.8465
   1.750   0.5004   0.01065   0.00514  -0.0583   0.6083   0.8491
   2.000   0.5280   0.01068   0.00519  -0.0585   0.6066   0.8516
   2.250   0.5560   0.01070   0.00523  -0.0588   0.6046   0.8538
   2.500   0.5830   0.01069   0.00525  -0.0588   0.6023   0.8555
   2.750   0.6104   0.01071   0.00529  -0.0589   0.5999   0.8572
   3.000   0.6383   0.01074   0.00532  -0.0591   0.5976   0.8589
   3.250   0.6669   0.01077   0.00535  -0.0595   0.5953   0.8605
   3.500   0.6960   0.01090   0.00544  -0.0599   0.5928   0.8623
   3.750   0.7224   0.01091   0.00552  -0.0599   0.5901   0.8644
   4.000   0.7493   0.01091   0.00557  -0.0600   0.5871   0.8663
   4.250   0.7771   0.01091   0.00558  -0.0602   0.5836   0.8680
   4.500   0.8058   0.01091   0.00557  -0.0607   0.5803   0.8696
   4.750   0.8343   0.01097   0.00562  -0.0610   0.5768   0.8712
   5.000   0.8584   0.01091   0.00566  -0.0604   0.5728   0.8731
   5.250   0.8843   0.01086   0.00566  -0.0602   0.5682   0.8748
   5.500   0.9115   0.01082   0.00563  -0.0602   0.5637   0.8766
   5.750   0.9377   0.01084   0.00568  -0.0601   0.5589   0.8785
   6.000   0.9624   0.01079   0.00570  -0.0597   0.5535   0.8807
   6.250   0.9888   0.01075   0.00568  -0.0596   0.5481   0.8829
   6.500   1.0143   0.01076   0.00574  -0.0594   0.5425   0.8851
   6.750   1.0373   0.01069   0.00576  -0.0586   0.5357   0.8873
   7.000   1.0614   0.01067   0.00577  -0.0580   0.5289   0.8895
   7.250   1.0832   0.01062   0.00582  -0.0569   0.5197   0.8920
   7.500   1.1056   0.01062   0.00588  -0.0561   0.5099   0.8948
   7.750   1.1272   0.01064   0.00594  -0.0551   0.4980   0.8978
   8.000   1.1477   0.01070   0.00604  -0.0539   0.4820   0.9008
   8.250   1.1628   0.01081   0.00614  -0.0516   0.4581   0.9044
   8.500   1.1704   0.01114   0.00636  -0.0480   0.4243   0.9095
   8.750   1.1688   0.01169   0.00675  -0.0427   0.3878   0.9161
   9.000   1.1639   0.01237   0.00732  -0.0370   0.3547   0.9239
   9.250   1.1593   0.01316   0.00800  -0.0317   0.3232   0.9342
   9.500   1.1530   0.01409   0.00884  -0.0265   0.2919   0.9509
   9.750   1.1614   0.01551   0.01012  -0.0255   0.2510   0.9799
  10.000   1.1617   0.01699   0.01144  -0.0232   0.2203   1.0000
  10.250   1.1598   0.01863   0.01293  -0.0206   0.1928   1.0000
  10.500   1.1596   0.02028   0.01447  -0.0184   0.1716   1.0000
  10.750   1.1598   0.02199   0.01608  -0.0164   0.1501   1.0000
  11.000   1.1605   0.02374   0.01775  -0.0146   0.1325   1.0000
  11.250   1.1629   0.02544   0.01939  -0.0130   0.1179   1.0000
  11.500   1.1666   0.02710   0.02100  -0.0116   0.1055   1.0000
  11.750   1.1708   0.02876   0.02263  -0.0103   0.0944   1.0000
  12.000   1.1754   0.03041   0.02426  -0.0092   0.0850   1.0000
  12.250   1.1794   0.03214   0.02596  -0.0080   0.0769   1.0000
  12.500   1.1844   0.03383   0.02765  -0.0070   0.0692   1.0000
  12.750   1.1904   0.03548   0.02930  -0.0062   0.0627   1.0000
  13.000   1.1942   0.03735   0.03115  -0.0053   0.0568   1.0000
  13.250   1.2022   0.03892   0.03276  -0.0046   0.0521   1.0000
  13.500   1.2054   0.04092   0.03474  -0.0039   0.0470   1.0000
  13.750   1.2135   0.04254   0.03641  -0.0034   0.0431   1.0000
  14.000   1.2168   0.04463   0.03850  -0.0027   0.0387   1.0000
  14.250   1.2235   0.04645   0.04035  -0.0023   0.0345   1.0000
  14.500   1.2271   0.04861   0.04253  -0.0019   0.0303   1.0000
  14.750   1.2281   0.05107   0.04498  -0.0014   0.0265   1.0000
  15.000   1.2323   0.05327   0.04723  -0.0011   0.0233   1.0000
  15.250   1.2315   0.05605   0.05003  -0.0008   0.0209   1.0000
  15.500   1.2361   0.05831   0.05236  -0.0007   0.0192   1.0000
  15.750   1.2362   0.06111   0.05520  -0.0006   0.0179   1.0000
  16.000   1.2346   0.06418   0.05833  -0.0007   0.0170   1.0000
  16.250   1.2389   0.06665   0.06089  -0.0008   0.0162   1.0000
  16.500   1.2415   0.06936   0.06369  -0.0011   0.0155   1.0000
  16.750   1.2424   0.07231   0.06671  -0.0015   0.0150   1.0000
  17.000   1.2411   0.07563   0.07008  -0.0020   0.0144   1.0000
  17.250   1.2351   0.07960   0.07413  -0.0026   0.0139   1.0000
  17.500   1.2329   0.08316   0.07777  -0.0033   0.0137   1.0000
  17.750   1.2337   0.08641   0.08114  -0.0041   0.0134   1.0000
  18.000   1.2334   0.08986   0.08468  -0.0050   0.0131   1.0000
  18.250   1.2330   0.09335   0.08827  -0.0060   0.0129   1.0000
  18.500   1.2318   0.09705   0.09207  -0.0072   0.0126   1.0000
  18.750   1.2307   0.10078   0.09589  -0.0084   0.0123   1.0000
  19.000   1.2288   0.10466   0.09986  -0.0098   0.0120   1.0000
  19.250   1.2275   0.10846   0.10374  -0.0113   0.0119   1.0000
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