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S1012 (s1012-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: S1012 (s1012-il)
Reynolds number: 1,000,000
Max Cl/Cd: 69.92 at α=9.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s1012-il-1000000.txt
Download as CSV file: xf-s1012-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S1012                                           
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -1.1658   0.09878   0.09587  -0.0210   1.0000   0.0132
 -18.750  -1.2005   0.08828   0.08521  -0.0272   1.0000   0.0131
 -18.500  -1.2320   0.07843   0.07518  -0.0331   1.0000   0.0131
 -18.250  -1.2574   0.06992   0.06651  -0.0382   1.0000   0.0131
 -18.000  -1.2810   0.06217   0.05860  -0.0427   1.0000   0.0132
 -17.750  -1.2987   0.05598   0.05225  -0.0460   1.0000   0.0132
 -17.500  -1.3127   0.05086   0.04700  -0.0481   1.0000   0.0133
 -17.250  -1.3231   0.04667   0.04270  -0.0494   1.0000   0.0136
 -17.000  -1.3292   0.04336   0.03928  -0.0498   1.0000   0.0137
 -16.750  -1.3332   0.04051   0.03633  -0.0498   1.0000   0.0139
 -16.500  -1.3351   0.03805   0.03377  -0.0494   1.0000   0.0140
 -16.250  -1.3319   0.03617   0.03182  -0.0488   1.0000   0.0143
 -16.000  -1.3289   0.03434   0.02991  -0.0480   1.0000   0.0145
 -15.750  -1.3249   0.03267   0.02815  -0.0470   1.0000   0.0149
 -15.500  -1.3180   0.03128   0.02669  -0.0460   1.0000   0.0151
 -15.250  -1.3114   0.02992   0.02524  -0.0449   1.0000   0.0154
 -15.000  -1.3019   0.02879   0.02403  -0.0437   1.0000   0.0157
 -14.750  -1.2918   0.02773   0.02288  -0.0426   1.0000   0.0159
 -14.500  -1.2925   0.02597   0.02103  -0.0404   1.0000   0.0164
 -14.250  -1.2866   0.02471   0.01969  -0.0386   1.0000   0.0167
 -14.000  -1.2776   0.02367   0.01861  -0.0370   1.0000   0.0172
 -13.750  -1.2662   0.02279   0.01769  -0.0355   1.0000   0.0177
 -13.500  -1.2535   0.02202   0.01686  -0.0340   1.0000   0.0181
 -13.250  -1.2395   0.02133   0.01612  -0.0326   1.0000   0.0187
 -13.000  -1.2239   0.02076   0.01549  -0.0314   1.0000   0.0192
 -12.750  -1.2080   0.02020   0.01487  -0.0301   1.0000   0.0195
 -12.500  -1.1990   0.01923   0.01384  -0.0278   1.0000   0.0204
 -12.250  -1.1856   0.01851   0.01310  -0.0261   1.0000   0.0212
 -12.000  -1.1698   0.01795   0.01252  -0.0246   1.0000   0.0219
 -11.750  -1.1441   0.01742   0.01195  -0.0251   0.9758   0.0229
 -11.500  -1.1125   0.01695   0.01138  -0.0266   0.9487   0.0238
 -11.250  -1.1006   0.01642   0.01073  -0.0240   0.9246   0.0250
 -11.000  -1.0867   0.01597   0.01022  -0.0217   0.9121   0.0264
 -10.750  -1.0689   0.01563   0.00983  -0.0202   0.9041   0.0276
 -10.500  -1.0489   0.01534   0.00947  -0.0190   0.8978   0.0288
 -10.250  -1.0295   0.01490   0.00897  -0.0177   0.8926   0.0304
 -10.000  -1.0091   0.01448   0.00855  -0.0167   0.8879   0.0325
  -9.750  -0.9870   0.01419   0.00823  -0.0158   0.8839   0.0343
  -9.500  -0.9639   0.01399   0.00796  -0.0151   0.8802   0.0355
  -9.250  -0.9432   0.01350   0.00747  -0.0141   0.8771   0.0386
  -9.000  -0.9200   0.01319   0.00716  -0.0135   0.8741   0.0408
  -8.750  -0.8958   0.01297   0.00689  -0.0130   0.8712   0.0425
  -8.500  -0.8733   0.01261   0.00651  -0.0122   0.8683   0.0454
  -8.250  -0.8498   0.01233   0.00623  -0.0115   0.8657   0.0483
  -8.000  -0.8251   0.01213   0.00600  -0.0111   0.8634   0.0507
  -7.750  -0.8008   0.01183   0.00570  -0.0106   0.8615   0.0537
  -7.500  -0.7765   0.01154   0.00543  -0.0101   0.8594   0.0573
  -7.250  -0.7512   0.01133   0.00521  -0.0097   0.8575   0.0602
  -7.000  -0.7263   0.01109   0.00496  -0.0093   0.8556   0.0639
  -6.750  -0.7014   0.01083   0.00473  -0.0089   0.8538   0.0688
  -6.500  -0.6755   0.01067   0.00455  -0.0086   0.8521   0.0722
  -6.250  -0.6507   0.01041   0.00431  -0.0082   0.8504   0.0786
  -6.000  -0.6249   0.01024   0.00414  -0.0079   0.8485   0.0835
  -5.750  -0.5991   0.01002   0.00395  -0.0076   0.8470   0.0900
  -5.500  -0.5730   0.00983   0.00378  -0.0073   0.8455   0.0968
  -5.250  -0.5471   0.00961   0.00361  -0.0071   0.8441   0.1051
  -5.000  -0.5206   0.00944   0.00346  -0.0069   0.8427   0.1129
  -4.750  -0.4946   0.00923   0.00330  -0.0067   0.8412   0.1242
  -4.500  -0.4684   0.00903   0.00316  -0.0064   0.8398   0.1363
  -4.250  -0.4422   0.00883   0.00302  -0.0062   0.8383   0.1505
  -4.000  -0.4161   0.00863   0.00288  -0.0060   0.8368   0.1676
  -3.750  -0.3898   0.00844   0.00276  -0.0057   0.8354   0.1867
  -3.500  -0.3641   0.00821   0.00265  -0.0054   0.8341   0.2130
  -3.250  -0.3386   0.00799   0.00255  -0.0051   0.8325   0.2473
  -3.000  -0.3134   0.00768   0.00243  -0.0048   0.8312   0.2897
  -2.750  -0.2889   0.00731   0.00230  -0.0043   0.8297   0.3475
  -2.500  -0.2653   0.00687   0.00216  -0.0037   0.8281   0.4223
  -2.250  -0.2425   0.00636   0.00200  -0.0030   0.8262   0.5106
  -2.000  -0.2218   0.00573   0.00184  -0.0018   0.8242   0.6292
  -1.750  -0.1974   0.00549   0.00186  -0.0009   0.8215   0.7077
  -1.500  -0.1701   0.00550   0.00188  -0.0006   0.8163   0.7313
  -1.250  -0.1423   0.00541   0.00180  -0.0003   0.8084   0.7457
  -1.000  -0.1144   0.00541   0.00173   0.0000   0.8004   0.7558
  -0.750  -0.0859   0.00538   0.00172   0.0000   0.7953   0.7639
  -0.500  -0.0572   0.00537   0.00169   0.0000   0.7905   0.7699
  -0.250  -0.0288   0.00537   0.00170   0.0001   0.7859   0.7759
   0.000   0.0000   0.00539   0.00172   0.0000   0.7816   0.7815
   0.250   0.0288   0.00537   0.00170   0.0000   0.7759   0.7860
   0.500   0.0572   0.00537   0.00169   0.0000   0.7700   0.7905
   0.750   0.0859   0.00538   0.00173   0.0000   0.7639   0.7954
   1.000   0.1144   0.00541   0.00173   0.0000   0.7558   0.8004
   1.250   0.1423   0.00541   0.00180   0.0003   0.7456   0.8084
   1.500   0.1701   0.00550   0.00188   0.0006   0.7312   0.8163
   1.750   0.1974   0.00549   0.00186   0.0009   0.7077   0.8215
   2.250   0.2425   0.00636   0.00200   0.0030   0.5105   0.8262
   2.500   0.2653   0.00687   0.00216   0.0037   0.4226   0.8281
   2.750   0.2888   0.00732   0.00231   0.0044   0.3463   0.8298
   3.000   0.3134   0.00768   0.00243   0.0048   0.2896   0.8312
   3.250   0.3386   0.00799   0.00256   0.0051   0.2469   0.8324
   3.500   0.3641   0.00822   0.00265   0.0054   0.2125   0.8341
   3.750   0.3898   0.00844   0.00276   0.0057   0.1867   0.8354
   4.000   0.4161   0.00863   0.00288   0.0060   0.1675   0.8368
   4.250   0.4422   0.00883   0.00302   0.0062   0.1506   0.8383
   4.500   0.4684   0.00903   0.00316   0.0064   0.1362   0.8398
   4.750   0.4946   0.00923   0.00330   0.0067   0.1243   0.8412
   5.000   0.5206   0.00944   0.00346   0.0069   0.1129   0.8427
   5.250   0.5471   0.00961   0.00361   0.0071   0.1051   0.8441
   5.500   0.5730   0.00983   0.00378   0.0074   0.0967   0.8455
   5.750   0.5992   0.01002   0.00395   0.0076   0.0901   0.8470
   6.000   0.6249   0.01024   0.00414   0.0079   0.0835   0.8485
   6.250   0.6507   0.01041   0.00431   0.0082   0.0786   0.8504
   6.500   0.6754   0.01067   0.00455   0.0086   0.0722   0.8521
   6.750   0.7014   0.01083   0.00473   0.0089   0.0689   0.8538
   7.000   0.7262   0.01109   0.00496   0.0093   0.0638   0.8556
   7.250   0.7512   0.01133   0.00521   0.0097   0.0602   0.8575
   7.500   0.7765   0.01154   0.00544   0.0101   0.0573   0.8594
   7.750   0.8009   0.01183   0.00570   0.0106   0.0537   0.8615
   8.000   0.8251   0.01213   0.00600   0.0111   0.0507   0.8633
   8.250   0.8499   0.01232   0.00623   0.0115   0.0483   0.8657
   8.500   0.8733   0.01261   0.00651   0.0122   0.0454   0.8683
   8.750   0.8958   0.01297   0.00690   0.0130   0.0425   0.8712
   9.000   0.9200   0.01319   0.00716   0.0135   0.0408   0.8741
   9.250   0.9432   0.01349   0.00746   0.0141   0.0385   0.8771
   9.500   0.9639   0.01398   0.00795   0.0151   0.0356   0.8802
   9.750   0.9870   0.01420   0.00823   0.0158   0.0344   0.8839
  10.000   1.0090   0.01448   0.00855   0.0167   0.0325   0.8879
  10.250   1.0295   0.01490   0.00897   0.0177   0.0304   0.8926
  10.500   1.0489   0.01533   0.00946   0.0190   0.0288   0.8978
  10.750   1.0690   0.01563   0.00984   0.0202   0.0276   0.9041
  11.000   1.0868   0.01598   0.01023   0.0217   0.0264   0.9122
  11.250   1.1010   0.01641   0.01072   0.0239   0.0251   0.9246
  11.500   1.1124   0.01697   0.01141   0.0266   0.0239   0.9492
  11.750   1.1443   0.01743   0.01195   0.0250   0.0229   0.9758
  12.000   1.1699   0.01795   0.01252   0.0246   0.0220   1.0000
  12.250   1.1859   0.01851   0.01309   0.0261   0.0212   1.0000
  12.500   1.1989   0.01925   0.01385   0.0278   0.0203   1.0000
  12.750   1.2084   0.02019   0.01486   0.0300   0.0195   1.0000
  13.000   1.2238   0.02078   0.01551   0.0314   0.0192   1.0000
  13.250   1.2398   0.02133   0.01612   0.0326   0.0186   1.0000
  13.500   1.2535   0.02204   0.01688   0.0340   0.0181   1.0000
  13.750   1.2655   0.02286   0.01776   0.0356   0.0178   1.0000
  14.000   1.2780   0.02366   0.01860   0.0370   0.0173   1.0000
  14.250   1.2875   0.02466   0.01966   0.0385   0.0169   1.0000
  14.500   1.2926   0.02599   0.02105   0.0404   0.0163   1.0000
  14.750   1.2908   0.02783   0.02298   0.0426   0.0159   1.0000
  15.000   1.3024   0.02878   0.02402   0.0437   0.0157   1.0000
  15.250   1.3104   0.03002   0.02534   0.0449   0.0154   1.0000
  15.500   1.3198   0.03118   0.02658   0.0459   0.0151   1.0000
  15.750   1.3224   0.03290   0.02839   0.0471   0.0149   1.0000
  16.000   1.3274   0.03450   0.03008   0.0480   0.0147   1.0000
  16.250   1.3322   0.03617   0.03182   0.0488   0.0143   1.0000
  16.500   1.3340   0.03819   0.03392   0.0494   0.0141   1.0000
  16.750   1.3337   0.04050   0.03632   0.0497   0.0139   1.0000
  17.000   1.3309   0.04323   0.03914   0.0498   0.0137   1.0000
  17.250   1.3246   0.04656   0.04257   0.0493   0.0135   1.0000
  17.500   1.3146   0.05068   0.04681   0.0481   0.0133   1.0000
  17.750   1.3009   0.05573   0.05200   0.0460   0.0132   1.0000
  18.000   1.2797   0.06247   0.05890   0.0424   0.0131   1.0000
  18.250   1.2588   0.06980   0.06639   0.0381   0.0131   1.0000
  18.500   1.2348   0.07807   0.07482   0.0332   0.0131   1.0000
  18.750   1.2001   0.08847   0.08540   0.0270   0.0131   1.0000
  19.000   1.1660   0.09888   0.09597   0.0209   0.0132   1.0000
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