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S1046 17% (Danny Howell) (s1046-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: S1046 17% (Danny Howell) (s1046-il)
Reynolds number: 200,000
Max Cl/Cd: 55.02 at α=8°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s1046-il-200000.txt
Download as CSV file: xf-s1046-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S1046 17% (Danny Howell)                        
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -1.0395   0.08881   0.08308  -0.0218   1.0000   0.0390
 -17.000  -1.0392   0.08569   0.07997  -0.0226   1.0000   0.0409
 -16.750  -1.0424   0.08185   0.07613  -0.0242   1.0000   0.0428
 -16.500  -1.0449   0.07810   0.07230  -0.0257   1.0000   0.0447
 -16.250  -1.0486   0.07413   0.06818  -0.0272   1.0000   0.0469
 -16.000  -1.0528   0.07060   0.06472  -0.0281   1.0000   0.0496
 -15.750  -1.0575   0.06679   0.06087  -0.0295   1.0000   0.0522
 -15.500  -1.0619   0.06300   0.05692  -0.0308   1.0000   0.0556
 -15.250  -1.0702   0.05912   0.05311  -0.0318   1.0000   0.0590
 -15.000  -1.0762   0.05541   0.04934  -0.0330   1.0000   0.0631
 -14.750  -1.0825   0.05189   0.04577  -0.0337   1.0000   0.0676
 -14.500  -1.0903   0.04833   0.04220  -0.0345   1.0000   0.0723
 -14.250  -1.0947   0.04524   0.03902  -0.0350   1.0000   0.0780
 -14.000  -1.1017   0.04205   0.03586  -0.0353   1.0000   0.0834
 -13.750  -1.1041   0.03938   0.03311  -0.0354   1.0000   0.0900
 -13.500  -1.1081   0.03670   0.03045  -0.0353   1.0000   0.0965
 -13.250  -1.1092   0.03440   0.02809  -0.0349   1.0000   0.1035
 -13.000  -1.1093   0.03229   0.02596  -0.0343   1.0000   0.1110
 -12.750  -1.1093   0.03033   0.02399  -0.0335   1.0000   0.1182
 -12.500  -1.1051   0.02876   0.02231  -0.0326   1.0000   0.1270
 -12.250  -1.1050   0.02709   0.02071  -0.0312   1.0000   0.1346
 -12.000  -1.1004   0.02579   0.01935  -0.0298   1.0000   0.1433
 -11.750  -1.0961   0.02462   0.01816  -0.0280   1.0000   0.1522
 -11.500  -1.0918   0.02356   0.01712  -0.0259   1.0000   0.1607
 -11.250  -1.0846   0.02274   0.01622  -0.0238   1.0000   0.1702
 -11.000  -1.0797   0.02195   0.01547  -0.0211   1.0000   0.1791
 -10.750  -1.0736   0.02130   0.01482  -0.0182   1.0000   0.1885
 -10.500  -1.0641   0.02079   0.01422  -0.0157   1.0000   0.1992
 -10.250  -1.0535   0.02025   0.01372  -0.0134   1.0000   0.2099
 -10.000  -1.0410   0.01976   0.01325  -0.0113   1.0000   0.2205
  -9.750  -1.0269   0.01932   0.01277  -0.0093   1.0000   0.2312
  -9.500  -1.0120   0.01893   0.01234  -0.0074   1.0000   0.2413
  -9.250  -0.9964   0.01849   0.01194  -0.0056   1.0000   0.2505
  -9.000  -0.9811   0.01814   0.01151  -0.0036   1.0000   0.2603
  -8.750  -0.9658   0.01778   0.01120  -0.0017   1.0000   0.2693
  -8.500  -0.9514   0.01744   0.01086   0.0005   1.0000   0.2784
  -8.250  -0.9400   0.01721   0.01060   0.0031   1.0000   0.2875
  -8.000  -0.9328   0.01696   0.01040   0.0063   1.0000   0.2950
  -7.750  -0.9136   0.01680   0.01014   0.0070   0.9968   0.3053
  -7.500  -0.8699   0.01647   0.00986   0.0034   0.9882   0.3176
  -7.250  -0.8257   0.01616   0.00954  -0.0003   0.9802   0.3296
  -7.000  -0.7837   0.01583   0.00919  -0.0034   0.9707   0.3415
  -6.750  -0.7424   0.01555   0.00884  -0.0063   0.9610   0.3536
  -6.500  -0.6997   0.01524   0.00854  -0.0094   0.9529   0.3650
  -6.250  -0.6631   0.01495   0.00826  -0.0112   0.9402   0.3754
  -6.000  -0.6288   0.01470   0.00795  -0.0125   0.9267   0.3864
  -5.750  -0.5977   0.01450   0.00773  -0.0130   0.9126   0.3966
  -5.500  -0.5697   0.01430   0.00752  -0.0129   0.8981   0.4060
  -5.250  -0.5445   0.01419   0.00729  -0.0122   0.8835   0.4165
  -5.000  -0.5191   0.01403   0.00716  -0.0114   0.8698   0.4255
  -4.750  -0.4945   0.01390   0.00696  -0.0106   0.8568   0.4353
  -4.500  -0.4701   0.01380   0.00683  -0.0097   0.8429   0.4455
  -4.250  -0.4451   0.01368   0.00669  -0.0090   0.8300   0.4548
  -4.000  -0.4203   0.01359   0.00653  -0.0082   0.8177   0.4656
  -3.750  -0.3948   0.01350   0.00643  -0.0075   0.8066   0.4754
  -3.500  -0.3693   0.01339   0.00631  -0.0069   0.7942   0.4857
  -3.250  -0.3440   0.01334   0.00618  -0.0063   0.7822   0.4970
  -3.000  -0.3178   0.01324   0.00611  -0.0057   0.7714   0.5068
  -2.750  -0.2918   0.01316   0.00600  -0.0051   0.7601   0.5174
  -2.500  -0.2660   0.01312   0.00591  -0.0046   0.7483   0.5291
  -2.250  -0.2395   0.01305   0.00587  -0.0041   0.7375   0.5390
  -2.000  -0.2131   0.01300   0.00579  -0.0036   0.7267   0.5499
  -1.750  -0.1869   0.01297   0.00573  -0.0031   0.7148   0.5618
  -1.500  -0.1602   0.01293   0.00572  -0.0026   0.7042   0.5719
  -1.250  -0.1335   0.01290   0.00566  -0.0022   0.6935   0.5828
  -1.000  -0.1071   0.01289   0.00563  -0.0017   0.6817   0.5946
  -0.750  -0.0803   0.01288   0.00564  -0.0013   0.6711   0.6050
  -0.500  -0.0534   0.01286   0.00561  -0.0008   0.6605   0.6158
  -0.250  -0.0269   0.01286   0.00560  -0.0004   0.6488   0.6275
   0.000   0.0000   0.01286   0.00562   0.0000   0.6381   0.6381
   0.250   0.0269   0.01286   0.00560   0.0004   0.6275   0.6488
   0.500   0.0534   0.01286   0.00561   0.0008   0.6158   0.6605
   0.750   0.0803   0.01288   0.00564   0.0013   0.6050   0.6711
   1.000   0.1071   0.01289   0.00563   0.0017   0.5946   0.6817
   1.250   0.1335   0.01290   0.00566   0.0022   0.5827   0.6935
   1.500   0.1602   0.01293   0.00572   0.0026   0.5719   0.7042
   1.750   0.1869   0.01297   0.00573   0.0031   0.5618   0.7148
   2.000   0.2131   0.01300   0.00579   0.0036   0.5499   0.7267
   2.250   0.2395   0.01305   0.00588   0.0041   0.5391   0.7375
   2.500   0.2660   0.01312   0.00591   0.0046   0.5291   0.7483
   2.750   0.2918   0.01316   0.00600   0.0051   0.5174   0.7601
   3.000   0.3178   0.01324   0.00611   0.0057   0.5068   0.7714
   3.250   0.3439   0.01334   0.00618   0.0063   0.4970   0.7823
   3.500   0.3693   0.01339   0.00631   0.0069   0.4856   0.7942
   3.750   0.3948   0.01350   0.00643   0.0075   0.4754   0.8066
   4.000   0.4203   0.01359   0.00653   0.0082   0.4656   0.8178
   4.250   0.4451   0.01368   0.00669   0.0090   0.4548   0.8299
   4.500   0.4701   0.01380   0.00682   0.0097   0.4454   0.8429
   4.750   0.4946   0.01390   0.00696   0.0106   0.4353   0.8567
   5.000   0.5191   0.01403   0.00716   0.0114   0.4255   0.8698
   5.250   0.5445   0.01419   0.00729   0.0122   0.4166   0.8835
   5.500   0.5697   0.01430   0.00752   0.0129   0.4061   0.8981
   5.750   0.5977   0.01450   0.00774   0.0130   0.3967   0.9126
   6.000   0.6289   0.01470   0.00795   0.0125   0.3865   0.9268
   6.250   0.6631   0.01495   0.00826   0.0112   0.3754   0.9402
   6.750   0.7425   0.01555   0.00883   0.0063   0.3535   0.9611
   7.000   0.7838   0.01583   0.00919   0.0034   0.3414   0.9707
   7.250   0.8257   0.01615   0.00955   0.0003   0.3296   0.9803
   7.500   0.8700   0.01648   0.00986  -0.0034   0.3177   0.9883
   7.750   0.9137   0.01680   0.01013  -0.0070   0.3053   0.9968
   8.000   0.9326   0.01695   0.01039  -0.0062   0.2950   1.0000
   8.250   0.9399   0.01720   0.01060  -0.0030   0.2875   1.0000
   8.500   0.9514   0.01744   0.01086  -0.0005   0.2784   1.0000
   8.750   0.9658   0.01778   0.01120   0.0017   0.2693   1.0000
   9.000   0.9811   0.01814   0.01151   0.0036   0.2603   1.0000
   9.250   0.9964   0.01849   0.01193   0.0056   0.2505   1.0000
   9.500   1.0121   0.01893   0.01234   0.0074   0.2414   1.0000
   9.750   1.0270   0.01932   0.01276   0.0093   0.2312   1.0000
  10.000   1.0412   0.01976   0.01325   0.0113   0.2205   1.0000
  10.250   1.0537   0.02025   0.01372   0.0134   0.2098   1.0000
  10.500   1.0643   0.02079   0.01422   0.0157   0.1991   1.0000
  10.750   1.0738   0.02130   0.01481   0.0182   0.1884   1.0000
  11.000   1.0800   0.02195   0.01547   0.0210   0.1790   1.0000
  11.250   1.0850   0.02274   0.01622   0.0237   0.1702   1.0000
  11.500   1.0922   0.02355   0.01711   0.0258   0.1606   1.0000
  11.750   1.0966   0.02462   0.01816   0.0279   0.1520   1.0000
  12.000   1.1008   0.02579   0.01935   0.0297   0.1432   1.0000
  12.250   1.1056   0.02708   0.02069   0.0311   0.1345   1.0000
  12.500   1.1059   0.02875   0.02230   0.0325   0.1269   1.0000
  12.750   1.1102   0.03030   0.02397   0.0334   0.1182   1.0000
  13.000   1.1102   0.03228   0.02594   0.0342   0.1109   1.0000
  13.250   1.1101   0.03437   0.02807   0.0347   0.1035   1.0000
  13.500   1.1091   0.03669   0.03043   0.0351   0.0963   1.0000
  13.750   1.1051   0.03936   0.03308   0.0352   0.0899   1.0000
  14.000   1.1027   0.04203   0.03584   0.0352   0.0832   1.0000
  14.250   1.0956   0.04524   0.03902   0.0348   0.0778   1.0000
  14.500   1.0915   0.04831   0.04218   0.0344   0.0721   1.0000
  14.750   1.0837   0.05186   0.04572   0.0336   0.0675   1.0000
  15.000   1.0774   0.05541   0.04934   0.0328   0.0628   1.0000
  15.250   1.0714   0.05911   0.05309   0.0316   0.0588   1.0000
  15.500   1.0636   0.06294   0.05687   0.0307   0.0555   1.0000
  15.750   1.0591   0.06674   0.06082   0.0293   0.0520   1.0000
  16.000   1.0543   0.07057   0.06468   0.0280   0.0494   1.0000
  16.250   1.0499   0.07415   0.06821   0.0270   0.0468   1.0000
  16.500   1.0469   0.07799   0.07219   0.0255   0.0447   1.0000
  16.750   1.0434   0.08192   0.07619   0.0239   0.0425   1.0000
  17.000   1.0406   0.08567   0.07994   0.0224   0.0407   1.0000
  17.250   1.0401   0.08898   0.08326   0.0214   0.0388   1.0000
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