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


Details Polar file
Airfoil: S9032 (9%) (s9032-il)
Reynolds number: 500,000
Max Cl/Cd: 60.21 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s9032-il-500000.txt
Download as CSV file: xf-s9032-il-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -1.0419   0.08051   0.07761  -0.0050   1.0000   0.0123
 -14.500  -1.0644   0.07188   0.06882  -0.0107   1.0000   0.0122
 -14.250  -1.0827   0.06433   0.06114  -0.0160   1.0000   0.0123
 -14.000  -1.1027   0.05684   0.05346  -0.0212   1.0000   0.0122
 -13.750  -1.1209   0.05025   0.04667  -0.0256   1.0000   0.0122
 -13.500  -1.1347   0.04514   0.04143  -0.0288   1.0000   0.0125
 -13.250  -1.1424   0.04147   0.03764  -0.0304   1.0000   0.0128
 -13.000  -1.1419   0.03928   0.03540  -0.0309   1.0000   0.0131
 -12.750  -1.1445   0.03711   0.03312  -0.0305   1.0000   0.0135
 -12.500  -1.1387   0.03605   0.03201  -0.0294   1.0000   0.0140
 -12.250  -1.1409   0.03434   0.03017  -0.0273   1.0000   0.0145
 -12.000  -1.1368   0.03319   0.02889  -0.0251   1.0000   0.0151
 -11.750  -1.1278   0.03194   0.02747  -0.0235   1.0000   0.0157
 -11.500  -1.1141   0.03107   0.02645  -0.0222   1.0000   0.0162
 -11.250  -1.1124   0.02817   0.02326  -0.0202   1.0000   0.0168
 -11.000  -1.1024   0.02625   0.02121  -0.0187   1.0000   0.0178
 -10.750  -1.0837   0.02558   0.02050  -0.0178   1.0000   0.0186
 -10.500  -1.0641   0.02493   0.01978  -0.0170   1.0000   0.0196
 -10.250  -1.0444   0.02414   0.01888  -0.0161   1.0000   0.0206
 -10.000  -1.0235   0.02349   0.01812  -0.0154   1.0000   0.0215
  -9.750  -1.0017   0.02292   0.01742  -0.0146   1.0000   0.0221
  -9.500  -0.9862   0.02089   0.01518  -0.0132   1.0000   0.0230
  -9.250  -0.9686   0.01938   0.01356  -0.0120   1.0000   0.0242
  -9.000  -0.9470   0.01860   0.01273  -0.0112   1.0000   0.0253
  -8.750  -0.9247   0.01790   0.01196  -0.0104   1.0000   0.0264
  -8.500  -0.9025   0.01714   0.01112  -0.0096   1.0000   0.0274
  -8.250  -0.8799   0.01643   0.01031  -0.0087   1.0000   0.0284
  -8.000  -0.8564   0.01587   0.00966  -0.0080   1.0000   0.0295
  -7.750  -0.8351   0.01495   0.00864  -0.0069   1.0000   0.0310
  -7.500  -0.8136   0.01409   0.00775  -0.0059   1.0000   0.0335
  -7.250  -0.7898   0.01359   0.00722  -0.0052   1.0000   0.0361
  -7.000  -0.7655   0.01318   0.00674  -0.0045   1.0000   0.0389
  -6.750  -0.7433   0.01244   0.00599  -0.0035   1.0000   0.0448
  -6.500  -0.7187   0.01212   0.00563  -0.0028   1.0000   0.0502
  -6.250  -0.6957   0.01156   0.00512  -0.0019   1.0000   0.0592
  -6.000  -0.6717   0.01118   0.00474  -0.0012   1.0000   0.0671
  -5.750  -0.6473   0.01090   0.00445  -0.0004   1.0000   0.0749
  -5.500  -0.6236   0.01050   0.00410   0.0004   1.0000   0.0855
  -5.250  -0.5997   0.01016   0.00380   0.0012   1.0000   0.0971
  -5.000  -0.5757   0.00983   0.00352   0.0020   1.0000   0.1109
  -4.750  -0.5518   0.00952   0.00328   0.0028   1.0000   0.1282
  -4.500  -0.5282   0.00919   0.00305   0.0036   1.0000   0.1505
  -4.250  -0.5045   0.00888   0.00285   0.0044   1.0000   0.1747
  -4.000  -0.4808   0.00860   0.00266   0.0052   1.0000   0.2003
  -3.750  -0.4572   0.00832   0.00250   0.0061   1.0000   0.2277
  -3.500  -0.4337   0.00807   0.00235   0.0069   1.0000   0.2547
  -3.250  -0.4103   0.00783   0.00222   0.0078   1.0000   0.2832
  -3.000  -0.3871   0.00761   0.00212   0.0087   1.0000   0.3134
  -2.750  -0.3641   0.00741   0.00204   0.0097   1.0000   0.3449
  -2.500  -0.3293   0.00718   0.00197   0.0080   0.9967   0.3870
  -2.250  -0.2894   0.00692   0.00192   0.0054   0.9911   0.4359
  -2.000  -0.2491   0.00666   0.00186   0.0027   0.9843   0.4882
  -1.750  -0.2107   0.00642   0.00179   0.0006   0.9758   0.5340
  -1.500  -0.1731   0.00620   0.00173  -0.0014   0.9659   0.5758
  -1.250  -0.1386   0.00600   0.00167  -0.0025   0.9511   0.6145
  -1.000  -0.1048   0.00580   0.00161  -0.0034   0.9309   0.6544
  -0.750  -0.0745   0.00565   0.00155  -0.0035   0.9010   0.6948
  -0.500  -0.0490   0.00557   0.00151  -0.0024   0.8650   0.7317
  -0.250  -0.0244   0.00555   0.00148  -0.0012   0.8300   0.7638
   0.000   0.0000   0.00554   0.00147   0.0000   0.7965   0.7965
   0.250   0.0244   0.00555   0.00148   0.0012   0.7638   0.8299
   0.500   0.0490   0.00557   0.00151   0.0024   0.7316   0.8650
   0.750   0.0745   0.00565   0.00155   0.0035   0.6947   0.9010
   1.000   0.1048   0.00581   0.00161   0.0035   0.6541   0.9308
   1.250   0.1386   0.00600   0.00167   0.0025   0.6142   0.9511
   1.500   0.1731   0.00620   0.00173   0.0013   0.5759   0.9658
   1.750   0.2107   0.00642   0.00179  -0.0006   0.5340   0.9757
   2.000   0.2489   0.00666   0.00186  -0.0027   0.4882   0.9842
   2.250   0.2894   0.00692   0.00192  -0.0054   0.4353   0.9910
   2.500   0.3292   0.00718   0.00197  -0.0080   0.3871   0.9966
   2.750   0.3646   0.00741   0.00204  -0.0097   0.3449   1.0000
   3.000   0.3876   0.00762   0.00212  -0.0088   0.3131   1.0000
   3.250   0.4108   0.00783   0.00222  -0.0079   0.2829   1.0000
   3.500   0.4342   0.00807   0.00235  -0.0070   0.2545   1.0000
   3.750   0.4578   0.00832   0.00250  -0.0062   0.2275   1.0000
   4.250   0.5050   0.00889   0.00285  -0.0045   0.1743   1.0000
   4.500   0.5287   0.00919   0.00305  -0.0037   0.1502   1.0000
   4.750   0.5524   0.00953   0.00328  -0.0029   0.1281   1.0000
   5.000   0.5763   0.00983   0.00353  -0.0021   0.1107   1.0000
   5.250   0.6002   0.01016   0.00380  -0.0013   0.0969   1.0000
   5.500   0.6241   0.01050   0.00410  -0.0005   0.0854   1.0000
   5.750   0.6478   0.01090   0.00445   0.0003   0.0748   1.0000
   6.000   0.6721   0.01119   0.00474   0.0011   0.0671   1.0000
   6.250   0.6960   0.01156   0.00512   0.0018   0.0591   1.0000
   6.500   0.7190   0.01212   0.00563   0.0027   0.0502   1.0000
   6.750   0.7435   0.01244   0.00599   0.0034   0.0447   1.0000
   7.000   0.7656   0.01318   0.00675   0.0045   0.0389   1.0000
   7.250   0.7899   0.01359   0.00721   0.0052   0.0361   1.0000
   7.500   0.8135   0.01409   0.00775   0.0060   0.0335   1.0000
   7.750   0.8351   0.01493   0.00862   0.0070   0.0311   1.0000
   8.000   0.8560   0.01589   0.00967   0.0081   0.0295   1.0000
   8.250   0.8795   0.01643   0.01032   0.0088   0.0284   1.0000
   8.500   0.9020   0.01714   0.01111   0.0097   0.0274   1.0000
   8.750   0.9242   0.01789   0.01196   0.0105   0.0263   1.0000
   9.000   0.9463   0.01861   0.01274   0.0114   0.0253   1.0000
   9.250   0.9679   0.01937   0.01355   0.0122   0.0242   1.0000
   9.500   0.9857   0.02084   0.01512   0.0134   0.0231   1.0000
   9.750   1.0003   0.02302   0.01753   0.0148   0.0222   1.0000
  10.000   1.0227   0.02344   0.01807   0.0155   0.0215   1.0000
  10.250   1.0434   0.02411   0.01886   0.0164   0.0206   1.0000
  10.500   1.0634   0.02481   0.01966   0.0172   0.0196   1.0000
  10.750   1.0825   0.02556   0.02048   0.0181   0.0187   1.0000
  11.000   1.1010   0.02623   0.02119   0.0189   0.0178   1.0000
  11.250   1.1119   0.02801   0.02309   0.0204   0.0169   1.0000
  11.500   1.1116   0.03119   0.02658   0.0226   0.0162   1.0000
  11.750   1.1255   0.03201   0.02754   0.0239   0.0157   1.0000
  12.000   1.1352   0.03313   0.02883   0.0254   0.0152   1.0000
  12.250   1.1371   0.03450   0.03034   0.0278   0.0146   1.0000
  12.500   1.1378   0.03593   0.03188   0.0297   0.0141   1.0000
  12.750   1.1424   0.03712   0.03314   0.0308   0.0135   1.0000
  13.000   1.1469   0.03853   0.03458   0.0312   0.0131   1.0000
  13.250   1.1366   0.04199   0.03821   0.0306   0.0129   1.0000
  13.500   1.1324   0.04524   0.04153   0.0290   0.0126   1.0000
  13.750   1.1223   0.04982   0.04623   0.0261   0.0122   1.0000
  14.000   1.0982   0.05732   0.05394   0.0210   0.0120   1.0000
  14.250   1.0860   0.06351   0.06029   0.0167   0.0123   1.0000
  14.500   1.0636   0.07182   0.06878   0.0109   0.0123   1.0000
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