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SD7084 (9.6%) (sd7084-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: SD7084 (9.6%) (sd7084-il)
Reynolds number: 1,000,000
Max Cl/Cd: 98.85 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sd7084-il-1000000-n5.txt
Download as CSV file: xf-sd7084-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SD7084 (9.6%)                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.9462   0.03782   0.03566  -0.0665   1.0000   0.0044
 -12.750  -0.9728   0.03412   0.03174  -0.0639   1.0000   0.0045
 -12.500  -0.9797   0.03102   0.02841  -0.0624   1.0000   0.0046
 -12.250  -0.9713   0.02932   0.02658  -0.0612   1.0000   0.0047
 -12.000  -0.9589   0.02802   0.02517  -0.0601   1.0000   0.0049
 -11.750  -0.9426   0.02722   0.02431  -0.0591   1.0000   0.0050
 -11.500  -0.9284   0.02634   0.02336  -0.0577   1.0000   0.0051
 -11.250  -0.9045   0.02525   0.02217  -0.0583   0.9960   0.0053
 -11.000  -0.8799   0.02400   0.02076  -0.0591   0.9918   0.0054
 -10.750  -0.8528   0.02329   0.01997  -0.0599   0.9886   0.0057
 -10.500  -0.8267   0.02213   0.01866  -0.0607   0.9854   0.0059
 -10.250  -0.8005   0.02093   0.01730  -0.0616   0.9826   0.0062
 -10.000  -0.7764   0.02000   0.01623  -0.0616   0.9777   0.0064
  -9.750  -0.7519   0.01901   0.01509  -0.0617   0.9733   0.0067
  -9.500  -0.7268   0.01830   0.01426  -0.0617   0.9692   0.0068
  -9.250  -0.7036   0.01774   0.01360  -0.0612   0.9636   0.0070
  -9.000  -0.6820   0.01685   0.01255  -0.0604   0.9582   0.0072
  -8.750  -0.6602   0.01605   0.01164  -0.0597   0.9532   0.0076
  -8.500  -0.6362   0.01568   0.01122  -0.0591   0.9482   0.0079
  -8.250  -0.6119   0.01536   0.01085  -0.0585   0.9439   0.0081
  -8.000  -0.5877   0.01490   0.01031  -0.0580   0.9396   0.0084
  -7.750  -0.5634   0.01441   0.00975  -0.0575   0.9347   0.0087
  -7.500  -0.5394   0.01392   0.00917  -0.0568   0.9301   0.0090
  -7.250  -0.5145   0.01347   0.00861  -0.0563   0.9254   0.0094
  -7.000  -0.4897   0.01299   0.00805  -0.0558   0.9202   0.0097
  -6.750  -0.4645   0.01263   0.00761  -0.0553   0.9156   0.0101
  -6.500  -0.4388   0.01222   0.00713  -0.0549   0.9108   0.0104
  -6.250  -0.4134   0.01177   0.00660  -0.0545   0.9055   0.0106
  -5.750  -0.3620   0.01100   0.00568  -0.0536   0.8945   0.0108
  -5.500  -0.3369   0.01047   0.00506  -0.0531   0.8882   0.0111
  -5.250  -0.3122   0.00982   0.00432  -0.0525   0.8820   0.0119
  -5.000  -0.2861   0.00949   0.00394  -0.0521   0.8752   0.0125
  -4.750  -0.2595   0.00921   0.00361  -0.0518   0.8684   0.0130
  -4.500  -0.2330   0.00895   0.00329  -0.0515   0.8604   0.0135
  -4.250  -0.2061   0.00872   0.00301  -0.0512   0.8520   0.0140
  -4.000  -0.1794   0.00851   0.00273  -0.0509   0.8424   0.0145
  -3.750  -0.1525   0.00832   0.00248  -0.0506   0.8312   0.0149
  -3.500  -0.1255   0.00816   0.00226  -0.0503   0.8187   0.0153
  -3.250  -0.0986   0.00802   0.00204  -0.0501   0.8045   0.0156
  -3.000  -0.0717   0.00791   0.00185  -0.0498   0.7882   0.0160
  -2.750  -0.0449   0.00780   0.00165  -0.0494   0.7686   0.0177
  -2.500  -0.0183   0.00771   0.00150  -0.0491   0.7465   0.0210
  -2.250   0.0082   0.00762   0.00136  -0.0488   0.7232   0.0321
  -2.000   0.0346   0.00752   0.00125  -0.0484   0.7007   0.0529
  -1.750   0.0611   0.00743   0.00116  -0.0482   0.6781   0.0761
  -1.500   0.0875   0.00733   0.00108  -0.0479   0.6562   0.1097
  -1.250   0.1135   0.00718   0.00101  -0.0476   0.6341   0.1606
  -1.000   0.1396   0.00702   0.00096  -0.0473   0.6123   0.2197
  -0.750   0.1655   0.00688   0.00092  -0.0471   0.5911   0.2813
  -0.500   0.1910   0.00666   0.00089  -0.0467   0.5702   0.3702
  -0.250   0.2159   0.00641   0.00089  -0.0463   0.5494   0.4758
   0.000   0.2409   0.00621   0.00091  -0.0459   0.5295   0.5696
   0.250   0.2666   0.00614   0.00093  -0.0454   0.5096   0.6290
   0.500   0.2919   0.00607   0.00096  -0.0449   0.4898   0.6900
   1.000   0.3425   0.00601   0.00105  -0.0438   0.4521   0.7885
   1.250   0.3668   0.00598   0.00111  -0.0429   0.4341   0.8416
   1.500   0.3913   0.00596   0.00118  -0.0420   0.4160   0.8937
   1.750   0.4216   0.00602   0.00127  -0.0424   0.3975   0.9389
   2.250   0.4981   0.00635   0.00143  -0.0471   0.3579   0.9787
   2.500   0.5321   0.00652   0.00151  -0.0486   0.3391   0.9861
   2.750   0.5652   0.00669   0.00161  -0.0498   0.3223   0.9926
   3.000   0.5996   0.00686   0.00170  -0.0514   0.3053   0.9971
   3.250   0.6338   0.00703   0.00179  -0.0529   0.2905   1.0000
   3.500   0.6582   0.00719   0.00190  -0.0522   0.2778   1.0000
   4.000   0.7073   0.00751   0.00214  -0.0509   0.2542   1.0000
   4.250   0.7318   0.00768   0.00226  -0.0503   0.2429   1.0000
   4.500   0.7564   0.00785   0.00240  -0.0497   0.2326   1.0000
   4.750   0.7808   0.00805   0.00256  -0.0491   0.2216   1.0000
   5.000   0.8053   0.00823   0.00271  -0.0484   0.2108   1.0000
   5.250   0.8298   0.00843   0.00287  -0.0478   0.1999   1.0000
   5.500   0.8541   0.00864   0.00305  -0.0472   0.1883   1.0000
   5.750   0.8777   0.00893   0.00325  -0.0465   0.1707   1.0000
   6.000   0.9011   0.00925   0.00349  -0.0457   0.1524   1.0000
   6.250   0.9245   0.00957   0.00374  -0.0450   0.1339   1.0000
   6.500   0.9471   0.00998   0.00403  -0.0442   0.1130   1.0000
   6.750   0.9688   0.01048   0.00438  -0.0433   0.0871   1.0000
   7.000   0.9902   0.01101   0.00478  -0.0423   0.0635   1.0000
   7.250   1.0122   0.01148   0.00518  -0.0414   0.0468   1.0000
   7.500   1.0334   0.01203   0.00563  -0.0404   0.0300   1.0000
   7.750   1.0547   0.01258   0.00611  -0.0394   0.0176   1.0000
   8.000   1.0756   0.01315   0.00663  -0.0384   0.0087   1.0000
   8.250   1.0976   0.01360   0.00708  -0.0375   0.0061   1.0000
   8.500   1.1196   0.01404   0.00754  -0.0367   0.0047   1.0000
   8.750   1.1418   0.01443   0.00799  -0.0358   0.0043   1.0000
   9.000   1.1635   0.01487   0.00847  -0.0349   0.0040   1.0000
   9.250   1.1847   0.01532   0.00896  -0.0340   0.0037   1.0000
   9.500   1.2052   0.01583   0.00951  -0.0329   0.0033   1.0000
   9.750   1.2249   0.01637   0.01011  -0.0318   0.0031   1.0000
  10.000   1.2437   0.01697   0.01078  -0.0305   0.0030   1.0000
  10.250   1.2596   0.01776   0.01167  -0.0288   0.0027   1.0000
  10.500   1.2765   0.01842   0.01241  -0.0273   0.0027   1.0000
  10.750   1.2934   0.01902   0.01308  -0.0257   0.0026   1.0000
  11.000   1.3086   0.01964   0.01376  -0.0240   0.0025   1.0000
  11.250   1.3212   0.02027   0.01446  -0.0217   0.0024   1.0000
  11.500   1.3314   0.02100   0.01526  -0.0192   0.0024   1.0000
  11.750   1.3419   0.02174   0.01608  -0.0169   0.0023   1.0000
  12.000   1.3494   0.02270   0.01713  -0.0143   0.0023   1.0000
  12.250   1.3575   0.02366   0.01817  -0.0120   0.0022   1.0000
  12.500   1.3642   0.02474   0.01935  -0.0098   0.0022   1.0000
  12.750   1.3709   0.02588   0.02059  -0.0077   0.0021   1.0000
  13.000   1.3750   0.02724   0.02206  -0.0056   0.0021   1.0000
  13.250   1.3780   0.02877   0.02368  -0.0037   0.0020   1.0000
  13.500   1.3795   0.03052   0.02554  -0.0020   0.0020   1.0000
  13.750   1.3822   0.03228   0.02741  -0.0006   0.0019   1.0000
  14.000   1.3826   0.03438   0.02960   0.0005   0.0019   1.0000
  14.250   1.3818   0.03675   0.03208   0.0012   0.0018   1.0000
  14.500   1.3761   0.03984   0.03530   0.0016   0.0019   1.0000
  14.750   1.3725   0.04294   0.03852   0.0015   0.0018   1.0000
  15.000   1.3677   0.04644   0.04214   0.0009   0.0018   1.0000
  15.250   1.3596   0.05059   0.04642  -0.0002   0.0018   1.0000
  15.500   1.3512   0.05507   0.05103  -0.0018   0.0018   1.0000
  15.750   1.3387   0.06042   0.05651  -0.0039   0.0018   1.0000
  16.000   1.3279   0.06575   0.06196  -0.0063   0.0017   1.0000
  16.250   1.3122   0.07209   0.06845  -0.0092   0.0017   1.0000
  16.500   1.2953   0.07885   0.07534  -0.0125   0.0017   1.0000
  16.750   1.2789   0.08574   0.08236  -0.0159   0.0017   1.0000
  17.000   1.2602   0.09319   0.08994  -0.0196   0.0017   1.0000
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