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S9026 (9.5%) (s9026-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: S9026 (9.5%) (s9026-il)
Reynolds number: 1,000,000
Max Cl/Cd: 75.15 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s9026-il-1000000.txt
Download as CSV file: xf-s9026-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S9026 (9.5%)                                    
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -1.0991   0.10861   0.10622   0.0084   1.0000   0.0072
 -17.000  -1.1342   0.09745   0.09494   0.0018   1.0000   0.0071
 -16.750  -1.1829   0.08437   0.08169  -0.0059   1.0000   0.0069
 -16.500  -1.2138   0.07472   0.07190  -0.0117   1.0000   0.0069
 -16.250  -1.2558   0.06329   0.06028  -0.0188   1.0000   0.0067
 -16.000  -1.2897   0.05360   0.05038  -0.0251   1.0000   0.0066
 -15.750  -1.3144   0.04609   0.04267  -0.0299   1.0000   0.0065
 -15.500  -1.3236   0.04157   0.03803  -0.0323   1.0000   0.0067
 -15.250  -1.3257   0.03842   0.03477  -0.0336   1.0000   0.0068
 -15.000  -1.3317   0.03525   0.03148  -0.0342   1.0000   0.0070
 -14.750  -1.3344   0.03280   0.02891  -0.0340   1.0000   0.0072
 -14.500  -1.3340   0.03093   0.02693  -0.0331   1.0000   0.0073
 -14.250  -1.3323   0.02935   0.02525  -0.0316   1.0000   0.0075
 -14.000  -1.3253   0.02828   0.02409  -0.0300   1.0000   0.0077
 -13.750  -1.3195   0.02722   0.02294  -0.0279   1.0000   0.0078
 -13.500  -1.3286   0.02538   0.02095  -0.0238   1.0000   0.0082
 -13.250  -1.3193   0.02423   0.01973  -0.0220   1.0000   0.0087
 -13.000  -1.3036   0.02346   0.01891  -0.0207   1.0000   0.0091
 -12.750  -1.2853   0.02285   0.01826  -0.0197   1.0000   0.0096
 -12.500  -1.2658   0.02231   0.01766  -0.0188   1.0000   0.0101
 -12.250  -1.2462   0.02173   0.01700  -0.0179   1.0000   0.0106
 -12.000  -1.2237   0.02140   0.01663  -0.0173   1.0000   0.0109
 -11.750  -1.2124   0.01990   0.01499  -0.0155   1.0000   0.0118
 -11.500  -1.1923   0.01924   0.01431  -0.0147   1.0000   0.0124
 -11.250  -1.1705   0.01875   0.01378  -0.0140   1.0000   0.0130
 -11.000  -1.1486   0.01823   0.01320  -0.0132   1.0000   0.0136
 -10.750  -1.1260   0.01777   0.01270  -0.0126   1.0000   0.0142
 -10.500  -1.1026   0.01738   0.01224  -0.0120   1.0000   0.0147
 -10.250  -1.0801   0.01687   0.01167  -0.0113   1.0000   0.0150
 -10.000  -1.0624   0.01574   0.01043  -0.0100   1.0000   0.0163
  -9.750  -1.0399   0.01519   0.00986  -0.0093   1.0000   0.0172
  -9.500  -1.0166   0.01473   0.00935  -0.0086   1.0000   0.0179
  -9.250  -0.9930   0.01429   0.00887  -0.0080   1.0000   0.0187
  -9.000  -0.9690   0.01391   0.00844  -0.0074   1.0000   0.0194
  -8.750  -0.9446   0.01358   0.00806  -0.0068   1.0000   0.0199
  -8.500  -0.9227   0.01290   0.00730  -0.0058   1.0000   0.0211
  -8.250  -0.9000   0.01234   0.00672  -0.0049   1.0000   0.0228
  -8.000  -0.8763   0.01194   0.00630  -0.0042   1.0000   0.0241
  -7.750  -0.8523   0.01161   0.00594  -0.0035   1.0000   0.0255
  -7.500  -0.8281   0.01132   0.00561  -0.0028   1.0000   0.0265
  -7.250  -0.8056   0.01080   0.00507  -0.0017   1.0000   0.0302
  -7.000  -0.7820   0.01047   0.00475  -0.0009   1.0000   0.0338
  -6.750  -0.7588   0.01010   0.00440   0.0000   1.0000   0.0395
  -6.500  -0.7348   0.00984   0.00415   0.0009   1.0000   0.0444
  -6.250  -0.7116   0.00951   0.00385   0.0018   1.0000   0.0516
  -6.000  -0.6876   0.00931   0.00364   0.0026   1.0000   0.0561
  -5.750  -0.6645   0.00900   0.00339   0.0036   1.0000   0.0646
  -5.500  -0.6410   0.00878   0.00318   0.0045   1.0000   0.0718
  -5.250  -0.6179   0.00854   0.00297   0.0054   1.0000   0.0806
  -5.000  -0.5950   0.00829   0.00278   0.0064   1.0000   0.0921
  -4.750  -0.5683   0.00806   0.00261   0.0066   0.9994   0.1051
  -4.250  -0.4950   0.00754   0.00228   0.0026   0.9943   0.1453
  -4.000  -0.4597   0.00725   0.00212   0.0010   0.9906   0.1740
  -3.750  -0.4240   0.00699   0.00197  -0.0008   0.9867   0.2004
  -3.500  -0.3873   0.00675   0.00184  -0.0027   0.9836   0.2265
  -3.250  -0.3546   0.00653   0.00171  -0.0037   0.9772   0.2525
  -3.000  -0.3207   0.00628   0.00159  -0.0050   0.9695   0.2843
  -2.750  -0.2902   0.00606   0.00147  -0.0054   0.9560   0.3147
  -2.500  -0.2612   0.00588   0.00137  -0.0055   0.9377   0.3434
  -2.250  -0.2346   0.00573   0.00127  -0.0050   0.9151   0.3724
  -2.000  -0.2091   0.00557   0.00118  -0.0043   0.8921   0.4116
  -1.750  -0.1836   0.00544   0.00110  -0.0036   0.8690   0.4497
  -1.500  -0.1575   0.00535   0.00105  -0.0030   0.8461   0.4816
  -1.250  -0.1315   0.00528   0.00099  -0.0025   0.8208   0.5132
  -1.000  -0.1054   0.00521   0.00095  -0.0019   0.7939   0.5475
  -0.750  -0.0791   0.00516   0.00091  -0.0014   0.7668   0.5801
  -0.500  -0.0526   0.00511   0.00089  -0.0010   0.7409   0.6151
  -0.250  -0.0263   0.00505   0.00088  -0.0005   0.7149   0.6517
   0.000   0.0000   0.00503   0.00087   0.0000   0.6853   0.6853
   0.250   0.0263   0.00505   0.00088   0.0005   0.6518   0.7150
   0.500   0.0526   0.00511   0.00089   0.0010   0.6151   0.7408
   0.750   0.0791   0.00516   0.00091   0.0014   0.5798   0.7667
   1.000   0.1054   0.00521   0.00095   0.0019   0.5475   0.7939
   1.250   0.1314   0.00528   0.00099   0.0025   0.5128   0.8210
   1.500   0.1575   0.00535   0.00105   0.0030   0.4816   0.8461
   1.750   0.1836   0.00544   0.00110   0.0036   0.4500   0.8690
   2.000   0.2091   0.00558   0.00118   0.0043   0.4112   0.8919
   2.250   0.2346   0.00573   0.00127   0.0050   0.3725   0.9151
   2.500   0.2612   0.00588   0.00137   0.0055   0.3433   0.9377
   2.750   0.2902   0.00606   0.00147   0.0054   0.3149   0.9559
   3.000   0.3207   0.00628   0.00159   0.0050   0.2844   0.9695
   3.250   0.3546   0.00653   0.00172   0.0037   0.2524   0.9771
   3.500   0.3873   0.00675   0.00184   0.0027   0.2265   0.9836
   3.750   0.4239   0.00699   0.00197   0.0008   0.2005   0.9866
   4.000   0.4596   0.00725   0.00212  -0.0010   0.1741   0.9906
   4.250   0.4948   0.00754   0.00228  -0.0026   0.1457   0.9943
   4.750   0.5681   0.00806   0.00261  -0.0066   0.1051   0.9993
   5.000   0.5953   0.00829   0.00278  -0.0065   0.0921   1.0000
   5.250   0.6182   0.00854   0.00297  -0.0055   0.0806   1.0000
   5.500   0.6413   0.00878   0.00318  -0.0045   0.0717   1.0000
   5.750   0.6648   0.00900   0.00339  -0.0036   0.0645   1.0000
   6.000   0.6879   0.00931   0.00364  -0.0027   0.0561   1.0000
   6.250   0.7118   0.00951   0.00385  -0.0018   0.0516   1.0000
   6.500   0.7351   0.00984   0.00415  -0.0009   0.0444   1.0000
   6.750   0.7590   0.01010   0.00440  -0.0001   0.0394   1.0000
   7.000   0.7823   0.01047   0.00475   0.0008   0.0337   1.0000
   7.250   0.8058   0.01080   0.00507   0.0017   0.0302   1.0000
   7.500   0.8282   0.01132   0.00561   0.0027   0.0265   1.0000
   7.750   0.8523   0.01161   0.00594   0.0035   0.0255   1.0000
   8.000   0.8763   0.01194   0.00630   0.0042   0.0241   1.0000
   8.250   0.9000   0.01234   0.00671   0.0049   0.0228   1.0000
   8.500   0.9227   0.01290   0.00730   0.0058   0.0211   1.0000
   8.750   0.9444   0.01360   0.00809   0.0068   0.0199   1.0000
   9.000   0.9689   0.01390   0.00843   0.0074   0.0194   1.0000
   9.250   0.9929   0.01429   0.00887   0.0080   0.0187   1.0000
   9.500   1.0164   0.01472   0.00935   0.0086   0.0179   1.0000
   9.750   1.0397   0.01518   0.00985   0.0093   0.0172   1.0000
  10.000   1.0623   0.01572   0.01041   0.0100   0.0163   1.0000
  10.250   1.0800   0.01687   0.01166   0.0113   0.0151   1.0000
  10.500   1.1024   0.01738   0.01224   0.0120   0.0147   1.0000
  10.750   1.1258   0.01776   0.01268   0.0126   0.0142   1.0000
  11.000   1.1481   0.01825   0.01323   0.0133   0.0137   1.0000
  11.250   1.1701   0.01876   0.01379   0.0140   0.0131   1.0000
  11.500   1.1919   0.01924   0.01431   0.0147   0.0124   1.0000
  11.750   1.2118   0.01992   0.01501   0.0156   0.0117   1.0000
  12.000   1.2229   0.02144   0.01667   0.0174   0.0109   1.0000
  12.250   1.2453   0.02177   0.01704   0.0181   0.0106   1.0000
  12.500   1.2654   0.02229   0.01765   0.0189   0.0101   1.0000
  12.750   1.2845   0.02288   0.01828   0.0199   0.0096   1.0000
  13.000   1.3025   0.02350   0.01896   0.0209   0.0092   1.0000
  13.250   1.3184   0.02425   0.01975   0.0221   0.0087   1.0000
  13.500   1.3290   0.02532   0.02088   0.0239   0.0083   1.0000
  13.750   1.3198   0.02717   0.02288   0.0280   0.0078   1.0000
  14.000   1.3241   0.02832   0.02413   0.0302   0.0077   1.0000
  14.250   1.3311   0.02940   0.02530   0.0317   0.0075   1.0000
  14.500   1.3312   0.03109   0.02710   0.0332   0.0074   1.0000
  14.750   1.3292   0.03321   0.02934   0.0341   0.0073   1.0000
  15.000   1.3291   0.03546   0.03170   0.0342   0.0071   1.0000
  15.250   1.3258   0.03836   0.03472   0.0336   0.0069   1.0000
  15.500   1.3192   0.04210   0.03858   0.0320   0.0067   1.0000
  15.750   1.3036   0.04766   0.04430   0.0288   0.0067   1.0000
  16.000   1.2874   0.05394   0.05074   0.0248   0.0066   1.0000
  16.250   1.2686   0.06109   0.05803   0.0202   0.0065   1.0000
  16.500   1.2223   0.07324   0.07039   0.0126   0.0068   1.0000
  16.750   1.1724   0.08625   0.08360   0.0047   0.0071   1.0000
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