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S9032 (9%) (s9032-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: S9032 (9%) (s9032-il)
Reynolds number: 1,000,000
Max Cl/Cd: 74.13 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s9032-il-1000000-n5.txt
Download as CSV file: xf-s9032-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -1.1576   0.10163   0.09905   0.0067   1.0000   0.0039
 -17.000  -1.2333   0.08311   0.08029  -0.0045   1.0000   0.0035
 -16.750  -1.2874   0.06913   0.06609  -0.0131   1.0000   0.0033
 -16.500  -1.3293   0.05768   0.05442  -0.0207   1.0000   0.0032
 -16.250  -1.3534   0.04980   0.04636  -0.0260   1.0000   0.0032
 -16.000  -1.3731   0.04340   0.03979  -0.0301   1.0000   0.0033
 -15.750  -1.3846   0.03892   0.03516  -0.0323   1.0000   0.0033
 -15.500  -1.3930   0.03546   0.03157  -0.0332   1.0000   0.0034
 -15.250  -1.3989   0.03281   0.02878  -0.0330   1.0000   0.0035
 -15.000  -1.4024   0.03075   0.02661  -0.0318   1.0000   0.0035
 -14.750  -1.4040   0.02911   0.02485  -0.0298   1.0000   0.0037
 -14.500  -1.4034   0.02778   0.02343  -0.0273   1.0000   0.0038
 -14.250  -1.4011   0.02658   0.02213  -0.0245   1.0000   0.0042
 -14.000  -1.3916   0.02547   0.02094  -0.0227   1.0000   0.0044
 -13.750  -1.3790   0.02444   0.01984  -0.0212   1.0000   0.0048
 -13.500  -1.3643   0.02352   0.01884  -0.0200   1.0000   0.0052
 -13.250  -1.3480   0.02266   0.01790  -0.0188   1.0000   0.0056
 -13.000  -1.3306   0.02184   0.01701  -0.0177   1.0000   0.0061
 -12.750  -1.3120   0.02110   0.01621  -0.0168   1.0000   0.0066
 -12.500  -1.2923   0.02043   0.01550  -0.0159   1.0000   0.0072
 -12.250  -1.2719   0.01979   0.01479  -0.0151   1.0000   0.0076
 -12.000  -1.2507   0.01921   0.01414  -0.0144   1.0000   0.0080
 -11.750  -1.2291   0.01865   0.01350  -0.0136   1.0000   0.0083
 -11.500  -1.2079   0.01800   0.01280  -0.0129   1.0000   0.0087
 -11.250  -1.1861   0.01740   0.01215  -0.0122   1.0000   0.0092
 -11.000  -1.1635   0.01688   0.01158  -0.0115   1.0000   0.0097
 -10.750  -1.1405   0.01638   0.01103  -0.0109   1.0000   0.0102
 -10.500  -1.1171   0.01593   0.01054  -0.0103   1.0000   0.0107
 -10.250  -1.0934   0.01550   0.01006  -0.0098   1.0000   0.0111
 -10.000  -1.0694   0.01509   0.00960  -0.0092   1.0000   0.0115
  -9.750  -1.0449   0.01476   0.00923  -0.0088   1.0000   0.0118
  -9.500  -1.0220   0.01415   0.00856  -0.0081   1.0000   0.0127
  -9.250  -0.9981   0.01370   0.00809  -0.0075   1.0000   0.0137
  -9.000  -0.9738   0.01331   0.00768  -0.0070   1.0000   0.0144
  -8.750  -0.9492   0.01295   0.00729  -0.0064   1.0000   0.0152
  -8.500  -0.9246   0.01259   0.00688  -0.0059   1.0000   0.0157
  -8.250  -0.8999   0.01224   0.00649  -0.0053   1.0000   0.0160
  -8.000  -0.8750   0.01192   0.00612  -0.0048   1.0000   0.0163
  -7.750  -0.8508   0.01150   0.00567  -0.0041   1.0000   0.0177
  -7.500  -0.8263   0.01115   0.00531  -0.0034   1.0000   0.0191
  -7.250  -0.8018   0.01083   0.00499  -0.0028   1.0000   0.0204
  -7.000  -0.7771   0.01055   0.00468  -0.0021   1.0000   0.0217
  -6.750  -0.7525   0.01027   0.00438  -0.0014   1.0000   0.0240
  -6.500  -0.7283   0.00996   0.00410  -0.0007   1.0000   0.0275
  -6.250  -0.7038   0.00970   0.00384   0.0000   1.0000   0.0312
  -6.000  -0.6795   0.00942   0.00360   0.0007   1.0000   0.0368
  -5.750  -0.6548   0.00921   0.00339   0.0015   1.0000   0.0401
  -5.500  -0.6305   0.00896   0.00316   0.0022   1.0000   0.0456
  -5.250  -0.6004   0.00875   0.00296   0.0017   0.9985   0.0501
  -5.000  -0.5667   0.00850   0.00276   0.0004   0.9954   0.0581
  -4.750  -0.5333   0.00829   0.00258  -0.0008   0.9921   0.0653
  -4.500  -0.5006   0.00808   0.00240  -0.0018   0.9870   0.0747
  -4.250  -0.4667   0.00785   0.00223  -0.0031   0.9803   0.0873
  -4.000  -0.4343   0.00758   0.00206  -0.0041   0.9694   0.1056
  -3.750  -0.4019   0.00734   0.00189  -0.0050   0.9528   0.1240
  -3.250  -0.3450   0.00708   0.00160  -0.0048   0.8897   0.1542
  -3.000  -0.3200   0.00705   0.00148  -0.0040   0.8486   0.1682
  -2.750  -0.2945   0.00703   0.00137  -0.0033   0.8088   0.1832
  -2.500  -0.2683   0.00699   0.00127  -0.0028   0.7743   0.1995
  -2.250  -0.2418   0.00693   0.00118  -0.0024   0.7435   0.2190
  -2.000  -0.2152   0.00684   0.00109  -0.0021   0.7166   0.2456
  -1.750  -0.1887   0.00671   0.00102  -0.0018   0.6904   0.2813
  -1.500  -0.1619   0.00666   0.00095  -0.0015   0.6589   0.3069
  -1.250  -0.1352   0.00665   0.00090  -0.0012   0.6213   0.3325
  -1.000  -0.1082   0.00664   0.00086  -0.0009   0.5892   0.3560
  -0.500  -0.0538   0.00660   0.00080  -0.0005   0.5335   0.4038
  -0.250  -0.0268   0.00654   0.00078  -0.0002   0.5078   0.4405
   0.000   0.0000   0.00649   0.00078   0.0000   0.4793   0.4793
   0.250   0.0269   0.00654   0.00078   0.0002   0.4406   0.5078
   0.500   0.0539   0.00660   0.00080   0.0005   0.4043   0.5331
   0.750   0.0810   0.00662   0.00082   0.0007   0.3769   0.5612
   1.000   0.1082   0.00664   0.00086   0.0009   0.3558   0.5890
   1.250   0.1352   0.00665   0.00090   0.0012   0.3329   0.6214
   1.500   0.1619   0.00667   0.00095   0.0015   0.3066   0.6585
   1.750   0.1887   0.00671   0.00102   0.0018   0.2809   0.6906
   2.000   0.2152   0.00684   0.00109   0.0021   0.2458   0.7167
   2.250   0.2418   0.00693   0.00118   0.0024   0.2192   0.7433
   2.500   0.2683   0.00699   0.00127   0.0028   0.1995   0.7743
   2.750   0.2945   0.00703   0.00137   0.0033   0.1833   0.8089
   3.000   0.3200   0.00705   0.00148   0.0040   0.1682   0.8489
   3.250   0.3450   0.00708   0.00160   0.0048   0.1542   0.8892
   3.750   0.4018   0.00734   0.00189   0.0050   0.1240   0.9528
   4.000   0.4341   0.00759   0.00206   0.0041   0.1047   0.9693
   4.250   0.4666   0.00785   0.00223   0.0031   0.0874   0.9802
   4.500   0.5003   0.00808   0.00240   0.0019   0.0747   0.9868
   4.750   0.5330   0.00829   0.00258   0.0008   0.0655   0.9920
   5.000   0.5662   0.00851   0.00276  -0.0003   0.0580   0.9952
   5.250   0.6000   0.00875   0.00297  -0.0017   0.0502   0.9982
   5.500   0.6312   0.00896   0.00316  -0.0024   0.0455   1.0000
   5.750   0.6554   0.00921   0.00339  -0.0016   0.0400   1.0000
   6.000   0.6801   0.00942   0.00360  -0.0009   0.0368   1.0000
   6.250   0.7044   0.00970   0.00384  -0.0001   0.0312   1.0000
   6.500   0.7288   0.00996   0.00410   0.0006   0.0275   1.0000
   6.750   0.7530   0.01027   0.00438   0.0013   0.0239   1.0000
   7.000   0.7775   0.01055   0.00468   0.0020   0.0217   1.0000
   7.250   0.8021   0.01083   0.00499   0.0027   0.0204   1.0000
   7.500   0.8266   0.01115   0.00531   0.0034   0.0191   1.0000
   7.750   0.8510   0.01150   0.00567   0.0041   0.0178   1.0000
   8.000   0.8750   0.01193   0.00613   0.0048   0.0163   1.0000
   8.250   0.8997   0.01224   0.00650   0.0053   0.0160   1.0000
   8.500   0.9244   0.01259   0.00688   0.0059   0.0156   1.0000
   8.750   0.9489   0.01295   0.00729   0.0065   0.0152   1.0000
   9.000   0.9734   0.01331   0.00769   0.0071   0.0145   1.0000
   9.250   0.9977   0.01369   0.00808   0.0076   0.0135   1.0000
   9.500   1.0215   0.01415   0.00856   0.0082   0.0128   1.0000
   9.750   1.0443   0.01475   0.00922   0.0089   0.0118   1.0000
  10.000   1.0687   0.01509   0.00961   0.0094   0.0115   1.0000
  10.250   1.0927   0.01548   0.01004   0.0099   0.0111   1.0000
  10.500   1.1163   0.01592   0.01053   0.0105   0.0107   1.0000
  10.750   1.1396   0.01637   0.01103   0.0111   0.0102   1.0000
  11.000   1.1626   0.01686   0.01156   0.0117   0.0097   1.0000
  11.250   1.1851   0.01739   0.01214   0.0124   0.0092   1.0000
  11.500   1.2068   0.01799   0.01278   0.0131   0.0087   1.0000
  11.750   1.2279   0.01864   0.01350   0.0139   0.0083   1.0000
  12.000   1.2494   0.01920   0.01413   0.0146   0.0080   1.0000
  12.250   1.2705   0.01979   0.01479   0.0154   0.0077   1.0000
  12.500   1.2908   0.02041   0.01548   0.0162   0.0072   1.0000
  12.750   1.3105   0.02108   0.01620   0.0171   0.0066   1.0000
  13.000   1.3290   0.02182   0.01698   0.0181   0.0060   1.0000
  13.250   1.3463   0.02264   0.01788   0.0191   0.0056   1.0000
  13.500   1.3625   0.02349   0.01881   0.0203   0.0053   1.0000
  13.750   1.3772   0.02441   0.01981   0.0216   0.0048   1.0000
  14.000   1.3895   0.02544   0.02091   0.0231   0.0044   1.0000
  14.250   1.3990   0.02652   0.02208   0.0249   0.0042   1.0000
  14.500   1.4012   0.02772   0.02337   0.0277   0.0038   1.0000
  14.750   1.4021   0.02905   0.02479   0.0302   0.0037   1.0000
  15.000   1.4006   0.03070   0.02656   0.0321   0.0036   1.0000
  15.250   1.3972   0.03276   0.02873   0.0333   0.0035   1.0000
  15.500   1.3915   0.03540   0.03150   0.0336   0.0034   1.0000
  15.750   1.3822   0.03897   0.03521   0.0326   0.0033   1.0000
  16.000   1.3727   0.04319   0.03957   0.0304   0.0033   1.0000
  16.250   1.3559   0.04913   0.04568   0.0267   0.0033   1.0000
  16.500   1.3311   0.05706   0.05379   0.0213   0.0033   1.0000
  16.750   1.2926   0.06793   0.06487   0.0141   0.0034   1.0000
  17.000   1.2368   0.08218   0.07934   0.0052   0.0036   1.0000
  17.250   1.1664   0.09959   0.09698  -0.0053   0.0039   1.0000
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