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


Details Polar file
Airfoil: S9032 (9%) (s9032-il)
Reynolds number: 1,000,000
Max Cl/Cd: 74.23 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s9032-il-1000000.txt
Download as CSV file: xf-s9032-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -1.2006   0.08142   0.07872  -0.0047   1.0000   0.0057
 -16.250  -1.2608   0.06640   0.06349  -0.0141   1.0000   0.0055
 -16.000  -1.2980   0.05570   0.05258  -0.0211   1.0000   0.0055
 -15.750  -1.3250   0.04734   0.04404  -0.0269   1.0000   0.0054
 -15.500  -1.3435   0.04127   0.03779  -0.0307   1.0000   0.0054
 -15.250  -1.3493   0.03770   0.03409  -0.0322   1.0000   0.0055
 -15.000  -1.3599   0.03421   0.03045  -0.0329   1.0000   0.0056
 -14.750  -1.3664   0.03171   0.02781  -0.0321   1.0000   0.0058
 -14.500  -1.3751   0.02950   0.02547  -0.0300   1.0000   0.0060
 -14.250  -1.3747   0.02810   0.02401  -0.0276   1.0000   0.0065
 -14.000  -1.3700   0.02705   0.02290  -0.0251   1.0000   0.0068
 -13.750  -1.3579   0.02622   0.02201  -0.0235   1.0000   0.0073
 -13.500  -1.3419   0.02553   0.02126  -0.0224   1.0000   0.0078
 -13.250  -1.3238   0.02494   0.02059  -0.0214   1.0000   0.0082
 -13.000  -1.3089   0.02401   0.01957  -0.0201   1.0000   0.0086
 -12.750  -1.2967   0.02274   0.01821  -0.0186   1.0000   0.0093
 -12.500  -1.2763   0.02222   0.01767  -0.0179   1.0000   0.0098
 -12.250  -1.2555   0.02170   0.01711  -0.0171   1.0000   0.0104
 -12.000  -1.2341   0.02120   0.01656  -0.0164   1.0000   0.0109
 -11.750  -1.2125   0.02071   0.01601  -0.0158   1.0000   0.0113
 -11.500  -1.1894   0.02035   0.01560  -0.0152   1.0000   0.0117
 -11.250  -1.1702   0.01951   0.01464  -0.0142   1.0000   0.0121
 -11.000  -1.1537   0.01826   0.01328  -0.0130   1.0000   0.0129
 -10.750  -1.1320   0.01764   0.01262  -0.0123   1.0000   0.0135
 -10.500  -1.1088   0.01719   0.01215  -0.0117   1.0000   0.0141
 -10.250  -1.0853   0.01676   0.01167  -0.0111   1.0000   0.0148
 -10.000  -1.0618   0.01631   0.01117  -0.0106   1.0000   0.0154
  -9.750  -1.0373   0.01599   0.01081  -0.0101   1.0000   0.0159
  -9.500  -1.0125   0.01569   0.01046  -0.0096   1.0000   0.0162
  -9.250  -0.9925   0.01469   0.00934  -0.0086   1.0000   0.0173
  -9.000  -0.9702   0.01398   0.00858  -0.0078   1.0000   0.0184
  -8.750  -0.9463   0.01353   0.00811  -0.0072   1.0000   0.0194
  -8.500  -0.9221   0.01311   0.00765  -0.0066   1.0000   0.0202
  -8.250  -0.8979   0.01267   0.00716  -0.0059   1.0000   0.0210
  -8.000  -0.8735   0.01227   0.00670  -0.0053   1.0000   0.0217
  -7.750  -0.8489   0.01193   0.00631  -0.0047   1.0000   0.0222
  -7.500  -0.8257   0.01134   0.00565  -0.0038   1.0000   0.0240
  -7.250  -0.8019   0.01089   0.00519  -0.0030   1.0000   0.0265
  -7.000  -0.7775   0.01055   0.00485  -0.0023   1.0000   0.0287
  -6.750  -0.7535   0.01017   0.00444  -0.0015   1.0000   0.0330
  -6.500  -0.7293   0.00985   0.00415  -0.0007   1.0000   0.0387
  -6.250  -0.7053   0.00951   0.00385   0.0001   1.0000   0.0459
  -6.000  -0.6805   0.00930   0.00363   0.0008   1.0000   0.0503
  -5.750  -0.6564   0.00900   0.00337   0.0016   1.0000   0.0577
  -5.500  -0.6318   0.00879   0.00315   0.0023   1.0000   0.0627
  -5.250  -0.6077   0.00851   0.00293   0.0031   1.0000   0.0724
  -5.000  -0.5836   0.00826   0.00273   0.0039   1.0000   0.0832
  -4.750  -0.5595   0.00803   0.00255   0.0047   1.0000   0.0951
  -4.500  -0.5355   0.00780   0.00238   0.0055   1.0000   0.1078
  -4.250  -0.5116   0.00758   0.00221   0.0064   1.0000   0.1222
  -4.000  -0.4879   0.00736   0.00207   0.0072   1.0000   0.1412
  -3.750  -0.4528   0.00709   0.00194   0.0056   0.9977   0.1691
  -3.500  -0.4157   0.00684   0.00181   0.0035   0.9948   0.1979
  -3.250  -0.3799   0.00661   0.00170   0.0018   0.9914   0.2252
  -3.000  -0.3434   0.00639   0.00159   0.0000   0.9865   0.2531
  -2.750  -0.3041   0.00617   0.00148  -0.0025   0.9822   0.2834
  -2.500  -0.2718   0.00596   0.00138  -0.0034   0.9714   0.3133
  -2.250  -0.2388   0.00576   0.00128  -0.0044   0.9572   0.3446
  -2.000  -0.2076   0.00554   0.00118  -0.0049   0.9354   0.3832
  -1.750  -0.1808   0.00537   0.00109  -0.0044   0.9039   0.4260
  -1.500  -0.1558   0.00531   0.00102  -0.0035   0.8653   0.4586
  -1.250  -0.1309   0.00528   0.00096  -0.0026   0.8243   0.4922
  -1.000  -0.1051   0.00525   0.00091  -0.0020   0.7889   0.5248
  -0.750  -0.0788   0.00523   0.00088  -0.0015   0.7572   0.5552
  -0.500  -0.0525   0.00521   0.00086  -0.0010   0.7261   0.5889
  -0.250  -0.0262   0.00516   0.00085  -0.0005   0.6973   0.6280
   0.000   0.0000   0.00513   0.00085   0.0000   0.6667   0.6667
   0.250   0.0262   0.00516   0.00085   0.0005   0.6280   0.6973
   0.500   0.0525   0.00521   0.00086   0.0010   0.5892   0.7259
   0.750   0.0788   0.00523   0.00088   0.0015   0.5552   0.7570
   1.000   0.1051   0.00525   0.00091   0.0020   0.5247   0.7889
   1.250   0.1309   0.00528   0.00096   0.0026   0.4924   0.8243
   1.500   0.1558   0.00531   0.00102   0.0035   0.4584   0.8651
   1.750   0.1808   0.00537   0.00109   0.0044   0.4257   0.9040
   2.000   0.2076   0.00554   0.00118   0.0049   0.3832   0.9355
   2.250   0.2387   0.00576   0.00128   0.0044   0.3447   0.9571
   2.500   0.2717   0.00596   0.00138   0.0034   0.3133   0.9713
   2.750   0.3040   0.00617   0.00148   0.0025   0.2836   0.9822
   3.000   0.3433   0.00639   0.00159   0.0001   0.2530   0.9864
   3.250   0.3797   0.00661   0.00170  -0.0018   0.2253   0.9912
   3.500   0.4155   0.00684   0.00181  -0.0035   0.1981   0.9947
   3.750   0.4526   0.00709   0.00194  -0.0056   0.1698   0.9976
   4.000   0.4886   0.00736   0.00207  -0.0074   0.1405   1.0000
   4.250   0.5123   0.00758   0.00222  -0.0065   0.1220   1.0000
   4.500   0.5362   0.00781   0.00238  -0.0057   0.1076   1.0000
   4.750   0.5602   0.00803   0.00255  -0.0049   0.0950   1.0000
   5.000   0.5843   0.00826   0.00273  -0.0040   0.0831   1.0000
   5.250   0.6084   0.00851   0.00293  -0.0032   0.0724   1.0000
   5.500   0.6325   0.00879   0.00316  -0.0024   0.0625   1.0000
   5.750   0.6571   0.00900   0.00337  -0.0017   0.0576   1.0000
   6.000   0.6811   0.00930   0.00363  -0.0009   0.0503   1.0000
   6.250   0.7059   0.00951   0.00385  -0.0002   0.0459   1.0000
   6.500   0.7299   0.00985   0.00416   0.0006   0.0386   1.0000
   6.750   0.7540   0.01018   0.00446   0.0014   0.0328   1.0000
   7.000   0.7780   0.01055   0.00485   0.0022   0.0287   1.0000
   7.250   0.8023   0.01089   0.00519   0.0029   0.0264   1.0000
   7.500   0.8259   0.01135   0.00565   0.0037   0.0240   1.0000
   7.750   0.8489   0.01194   0.00632   0.0046   0.0222   1.0000
   8.000   0.8735   0.01228   0.00670   0.0053   0.0217   1.0000
   8.250   0.8977   0.01268   0.00717   0.0060   0.0210   1.0000
   8.500   0.9218   0.01310   0.00764   0.0066   0.0202   1.0000
   8.750   0.9459   0.01353   0.00810   0.0072   0.0193   1.0000
   9.000   0.9697   0.01399   0.00859   0.0079   0.0184   1.0000
   9.250   0.9916   0.01472   0.00937   0.0087   0.0171   1.0000
   9.500   1.0118   0.01570   0.01047   0.0098   0.0163   1.0000
   9.750   1.0366   0.01597   0.01079   0.0102   0.0159   1.0000
  10.000   1.0609   0.01632   0.01118   0.0107   0.0154   1.0000
  10.250   1.0847   0.01672   0.01163   0.0113   0.0148   1.0000
  10.500   1.1078   0.01719   0.01214   0.0119   0.0142   1.0000
  10.750   1.1310   0.01764   0.01262   0.0125   0.0135   1.0000
  11.000   1.1528   0.01823   0.01325   0.0132   0.0129   1.0000
  11.250   1.1696   0.01943   0.01455   0.0144   0.0121   1.0000
  11.500   1.1880   0.02036   0.01561   0.0155   0.0117   1.0000
  11.750   1.2110   0.02072   0.01602   0.0160   0.0114   1.0000
  12.000   1.2327   0.02120   0.01657   0.0167   0.0109   1.0000
  12.250   1.2538   0.02171   0.01713   0.0174   0.0104   1.0000
  12.500   1.2746   0.02222   0.01768   0.0182   0.0099   1.0000
  12.750   1.2950   0.02275   0.01823   0.0189   0.0093   1.0000
  13.000   1.3086   0.02387   0.01942   0.0203   0.0086   1.0000
  13.250   1.3212   0.02499   0.02065   0.0218   0.0082   1.0000
  13.500   1.3396   0.02554   0.02127   0.0227   0.0078   1.0000
  13.750   1.3561   0.02618   0.02197   0.0239   0.0073   1.0000
  14.000   1.3684   0.02697   0.02281   0.0255   0.0068   1.0000
  14.250   1.3733   0.02800   0.02391   0.0280   0.0066   1.0000
  14.500   1.3738   0.02940   0.02537   0.0303   0.0061   1.0000
  14.750   1.3657   0.03157   0.02768   0.0324   0.0059   1.0000
  15.000   1.3486   0.03505   0.03133   0.0331   0.0057   1.0000
  15.250   1.3489   0.03750   0.03388   0.0326   0.0055   1.0000
  15.500   1.3389   0.04162   0.03815   0.0307   0.0054   1.0000
  15.750   1.3244   0.04715   0.04384   0.0273   0.0053   1.0000
  16.000   1.2981   0.05537   0.05225   0.0216   0.0055   1.0000
  16.250   1.2500   0.06804   0.06514   0.0131   0.0057   1.0000
  16.500   1.2122   0.07898   0.07625   0.0064   0.0058   1.0000
  16.750   1.1818   0.08859   0.08600   0.0008   0.0061   1.0000
  17.000   1.1369   0.10107   0.09867  -0.0066   0.0065   1.0000
  17.250   1.0874   0.11538   0.11315  -0.0151   0.0067   1.0000
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