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S9032 (9%) (s9032-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: S9032 (9%) (s9032-il)
Reynolds number: 500,000
Max Cl/Cd: 61.02 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s9032-il-500000-n5.txt
Download as CSV file: xf-s9032-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S9032 (9%)                                      
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -1.0599   0.10032   0.09736   0.0080   1.0000   0.0083
 -15.750  -1.1028   0.08790   0.08481   0.0006   1.0000   0.0080
 -15.500  -1.1488   0.07518   0.07194  -0.0071   1.0000   0.0076
 -15.250  -1.1786   0.06556   0.06216  -0.0132   1.0000   0.0076
 -15.000  -1.2110   0.05566   0.05208  -0.0199   1.0000   0.0073
 -14.750  -1.2281   0.04893   0.04517  -0.0246   1.0000   0.0074
 -14.500  -1.2411   0.04356   0.03962  -0.0280   1.0000   0.0075
 -14.250  -1.2468   0.03986   0.03576  -0.0298   1.0000   0.0078
 -14.000  -1.2543   0.03655   0.03228  -0.0305   1.0000   0.0079
 -13.750  -1.2590   0.03406   0.02963  -0.0300   1.0000   0.0081
 -13.500  -1.2570   0.03243   0.02787  -0.0288   1.0000   0.0084
 -13.250  -1.2588   0.03073   0.02607  -0.0266   1.0000   0.0087
 -13.000  -1.2542   0.02954   0.02480  -0.0245   1.0000   0.0091
 -12.750  -1.2444   0.02846   0.02362  -0.0228   1.0000   0.0095
 -12.500  -1.2295   0.02762   0.02270  -0.0217   1.0000   0.0100
 -12.250  -1.2156   0.02659   0.02155  -0.0204   1.0000   0.0104
 -12.000  -1.1995   0.02569   0.02053  -0.0193   1.0000   0.0110
 -11.750  -1.1825   0.02480   0.01952  -0.0183   1.0000   0.0114
 -11.500  -1.1642   0.02399   0.01859  -0.0173   1.0000   0.0117
 -11.250  -1.1485   0.02285   0.01730  -0.0161   1.0000   0.0122
 -11.000  -1.1303   0.02191   0.01630  -0.0152   1.0000   0.0129
 -10.750  -1.1097   0.02124   0.01557  -0.0144   1.0000   0.0136
 -10.500  -1.0882   0.02064   0.01491  -0.0137   1.0000   0.0143
 -10.250  -1.0666   0.02002   0.01420  -0.0130   1.0000   0.0151
 -10.000  -1.0447   0.01939   0.01347  -0.0123   1.0000   0.0157
  -9.750  -1.0225   0.01879   0.01277  -0.0116   1.0000   0.0161
  -9.500  -1.0015   0.01799   0.01186  -0.0107   1.0000   0.0167
  -9.250  -0.9806   0.01713   0.01093  -0.0098   1.0000   0.0177
  -9.000  -0.9582   0.01649   0.01023  -0.0091   1.0000   0.0184
  -8.750  -0.9352   0.01591   0.00959  -0.0084   1.0000   0.0192
  -8.500  -0.9117   0.01539   0.00900  -0.0078   1.0000   0.0201
  -8.250  -0.8879   0.01491   0.00845  -0.0071   1.0000   0.0211
  -8.000  -0.8640   0.01445   0.00791  -0.0065   1.0000   0.0220
  -7.750  -0.8404   0.01393   0.00733  -0.0057   1.0000   0.0231
  -7.500  -0.8167   0.01341   0.00679  -0.0050   1.0000   0.0252
  -7.250  -0.7925   0.01299   0.00635  -0.0044   1.0000   0.0275
  -7.000  -0.7680   0.01263   0.00595  -0.0037   1.0000   0.0298
  -6.750  -0.7440   0.01221   0.00553  -0.0031   1.0000   0.0342
  -6.500  -0.7195   0.01189   0.00520  -0.0024   1.0000   0.0385
  -6.250  -0.6952   0.01154   0.00485  -0.0017   1.0000   0.0436
  -6.000  -0.6708   0.01124   0.00456  -0.0010   1.0000   0.0492
  -5.750  -0.6466   0.01093   0.00426  -0.0003   1.0000   0.0551
  -5.500  -0.6223   0.01065   0.00398   0.0005   1.0000   0.0611
  -5.250  -0.5980   0.01037   0.00372   0.0012   1.0000   0.0682
  -5.000  -0.5737   0.01012   0.00348   0.0019   1.0000   0.0762
  -4.750  -0.5495   0.00985   0.00326   0.0027   1.0000   0.0876
  -4.250  -0.5017   0.00929   0.00284   0.0043   1.0000   0.1178
  -4.000  -0.4734   0.00902   0.00266   0.0041   0.9983   0.1360
  -3.750  -0.4375   0.00878   0.00249   0.0023   0.9936   0.1557
  -3.500  -0.4030   0.00855   0.00232   0.0009   0.9869   0.1742
  -3.250  -0.3678   0.00832   0.00217  -0.0007   0.9792   0.1952
  -3.000  -0.3337   0.00809   0.00204  -0.0020   0.9690   0.2178
  -2.750  -0.3005   0.00785   0.00190  -0.0031   0.9551   0.2464
  -2.500  -0.2661   0.00761   0.00177  -0.0045   0.9355   0.2790
  -2.250  -0.2332   0.00737   0.00164  -0.0054   0.9057   0.3175
  -2.000  -0.2059   0.00725   0.00152  -0.0049   0.8684   0.3476
  -1.750  -0.1805   0.00718   0.00143  -0.0042   0.8316   0.3764
  -1.500  -0.1550   0.00714   0.00135  -0.0034   0.7979   0.4025
  -1.250  -0.1292   0.00709   0.00129  -0.0028   0.7668   0.4315
  -1.000  -0.1036   0.00703   0.00123  -0.0022   0.7353   0.4647
  -0.750  -0.0780   0.00698   0.00120  -0.0016   0.7000   0.5040
  -0.500  -0.0525   0.00695   0.00117  -0.0010   0.6643   0.5424
  -0.250  -0.0263   0.00694   0.00115  -0.0005   0.6330   0.5720
   0.000   0.0000   0.00693   0.00114   0.0000   0.6023   0.6024
   0.250   0.0263   0.00694   0.00115   0.0005   0.5719   0.6329
   0.500   0.0525   0.00695   0.00117   0.0010   0.5422   0.6643
   0.750   0.0780   0.00698   0.00120   0.0016   0.5037   0.7000
   1.000   0.1036   0.00704   0.00123   0.0022   0.4643   0.7351
   1.250   0.1292   0.00709   0.00129   0.0028   0.4312   0.7669
   1.500   0.1550   0.00713   0.00135   0.0035   0.4026   0.7980
   1.750   0.1805   0.00718   0.00143   0.0042   0.3765   0.8316
   2.000   0.2059   0.00725   0.00152   0.0049   0.3479   0.8681
   2.250   0.2332   0.00738   0.00164   0.0054   0.3171   0.9058
   2.500   0.2661   0.00761   0.00177   0.0045   0.2786   0.9356
   2.750   0.3005   0.00785   0.00190   0.0031   0.2468   0.9550
   3.250   0.3678   0.00832   0.00218   0.0007   0.1952   0.9790
   3.500   0.4028   0.00855   0.00232  -0.0008   0.1742   0.9867
   3.750   0.4373   0.00878   0.00249  -0.0023   0.1558   0.9935
   4.000   0.4732   0.00902   0.00266  -0.0041   0.1360   0.9981
   4.250   0.5023   0.00929   0.00284  -0.0044   0.1174   1.0000
   4.500   0.5261   0.00957   0.00304  -0.0036   0.1016   1.0000
   4.750   0.5501   0.00985   0.00326  -0.0028   0.0876   1.0000
   5.000   0.5742   0.01012   0.00349  -0.0021   0.0760   1.0000
   5.250   0.5986   0.01037   0.00372  -0.0013   0.0681   1.0000
   5.500   0.6228   0.01065   0.00398  -0.0006   0.0611   1.0000
   5.750   0.6471   0.01093   0.00426   0.0002   0.0549   1.0000
   6.000   0.6713   0.01124   0.00456   0.0009   0.0492   1.0000
   6.250   0.6956   0.01154   0.00485   0.0016   0.0436   1.0000
   6.500   0.7198   0.01189   0.00520   0.0023   0.0385   1.0000
   6.750   0.7442   0.01221   0.00554   0.0030   0.0341   1.0000
   7.000   0.7682   0.01263   0.00595   0.0037   0.0298   1.0000
   7.250   0.7926   0.01299   0.00635   0.0044   0.0274   1.0000
   7.500   0.8166   0.01341   0.00680   0.0050   0.0252   1.0000
   7.750   0.8403   0.01392   0.00732   0.0058   0.0232   1.0000
   8.000   0.8637   0.01445   0.00791   0.0065   0.0219   1.0000
   8.250   0.8876   0.01491   0.00846   0.0072   0.0211   1.0000
   8.500   0.9113   0.01539   0.00900   0.0078   0.0201   1.0000
   8.750   0.9347   0.01591   0.00958   0.0085   0.0192   1.0000
   9.000   0.9576   0.01648   0.01022   0.0092   0.0185   1.0000
   9.250   0.9799   0.01713   0.01093   0.0100   0.0177   1.0000
   9.500   1.0008   0.01797   0.01184   0.0109   0.0168   1.0000
   9.750   1.0216   0.01879   0.01277   0.0118   0.0162   1.0000
  10.000   1.0438   0.01937   0.01346   0.0125   0.0157   1.0000
  10.250   1.0656   0.02000   0.01418   0.0132   0.0151   1.0000
  10.500   1.0874   0.02059   0.01485   0.0139   0.0143   1.0000
  10.750   1.1086   0.02123   0.01556   0.0147   0.0136   1.0000
  11.000   1.1292   0.02189   0.01628   0.0154   0.0129   1.0000
  11.250   1.1474   0.02280   0.01726   0.0164   0.0123   1.0000
  11.500   1.1626   0.02401   0.01860   0.0176   0.0117   1.0000
  11.750   1.1810   0.02479   0.01951   0.0186   0.0114   1.0000
  12.000   1.1981   0.02566   0.02050   0.0196   0.0110   1.0000
  12.250   1.2135   0.02661   0.02158   0.0208   0.0105   1.0000
  12.500   1.2284   0.02754   0.02261   0.0220   0.0100   1.0000
  12.750   1.2426   0.02843   0.02359   0.0232   0.0095   1.0000
  13.000   1.2537   0.02941   0.02465   0.0247   0.0090   1.0000
  13.250   1.2563   0.03073   0.02607   0.0271   0.0088   1.0000
  13.500   1.2553   0.03239   0.02783   0.0291   0.0084   1.0000
  13.750   1.2570   0.03405   0.02961   0.0304   0.0081   1.0000
  14.000   1.2547   0.03633   0.03205   0.0309   0.0079   1.0000
  14.250   1.2463   0.03969   0.03559   0.0301   0.0078   1.0000
  14.500   1.2381   0.04373   0.03979   0.0281   0.0077   1.0000
  14.750   1.2234   0.04941   0.04565   0.0244   0.0076   1.0000
  15.000   1.2009   0.05714   0.05359   0.0190   0.0076   1.0000
  15.250   1.1818   0.06470   0.06130   0.0139   0.0075   1.0000
  15.500   1.1433   0.07593   0.07270   0.0068   0.0078   1.0000
  15.750   1.1028   0.08767   0.08459  -0.0004   0.0080   1.0000
  16.000   1.0616   0.09978   0.09681  -0.0076   0.0083   1.0000
  16.250   1.0278   0.11103   0.10820  -0.0141   0.0085   1.0000
  16.500   0.9956   0.12275   0.12005  -0.0208   0.0086   1.0000
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