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OAF102 AIRFOIL (oaf102-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: OAF102 AIRFOIL (oaf102-il)
Reynolds number: 1,000,000
Max Cl/Cd: 114.04 at α=4°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-oaf102-il-1000000.txt
Download as CSV file: xf-oaf102-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: OAF102 AIRFOIL                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.7973   0.11481   0.11296  -0.0019   1.0000   0.0096
 -14.250  -0.8267   0.10389   0.10194  -0.0078   1.0000   0.0094
 -14.000  -0.8474   0.09520   0.09316  -0.0127   1.0000   0.0094
 -13.750  -0.8643   0.08750   0.08538  -0.0173   1.0000   0.0093
 -13.500  -0.8812   0.08002   0.07782  -0.0220   1.0000   0.0093
 -13.250  -0.8979   0.07293   0.07065  -0.0267   1.0000   0.0093
 -13.000  -0.9224   0.06472   0.06233  -0.0325   1.0000   0.0092
 -12.750  -0.9479   0.05655   0.05405  -0.0387   1.0000   0.0092
 -12.500  -0.9703   0.04841   0.04579  -0.0461   1.0000   0.0092
 -12.250  -0.9698   0.03950   0.03668  -0.0593   1.0000   0.0092
 -12.000  -0.9466   0.02949   0.02624  -0.0782   1.0000   0.0093
 -11.750  -0.9230   0.02477   0.02119  -0.0854   1.0000   0.0097
 -11.500  -0.8958   0.02293   0.01921  -0.0881   1.0000   0.0101
 -11.250  -0.8677   0.02171   0.01790  -0.0900   1.0000   0.0104
 -11.000  -0.8393   0.02073   0.01683  -0.0915   1.0000   0.0108
 -10.750  -0.8104   0.01981   0.01582  -0.0929   1.0000   0.0112
 -10.500  -0.7812   0.01889   0.01479  -0.0943   1.0000   0.0116
 -10.250  -0.7516   0.01801   0.01380  -0.0956   1.0000   0.0119
 -10.000  -0.7219   0.01736   0.01306  -0.0967   1.0000   0.0122
  -9.750  -0.6906   0.01566   0.01120  -0.0991   1.0000   0.0130
  -9.500  -0.6600   0.01495   0.01042  -0.1003   1.0000   0.0137
  -9.250  -0.6295   0.01440   0.00982  -0.1014   1.0000   0.0144
  -9.000  -0.5973   0.01389   0.00925  -0.1028   0.9894   0.0152
  -8.750  -0.5655   0.01353   0.00881  -0.1039   0.9755   0.0158
  -8.500  -0.5359   0.01270   0.00786  -0.1048   0.9627   0.0171
  -8.250  -0.5086   0.01235   0.00746  -0.1049   0.9508   0.0182
  -8.000  -0.4813   0.01209   0.00713  -0.1048   0.9402   0.0194
  -7.750  -0.4535   0.01189   0.00687  -0.1048   0.9299   0.0203
  -7.500  -0.4237   0.01128   0.00617  -0.1055   0.9205   0.0227
  -7.250  -0.3952   0.01103   0.00586  -0.1057   0.9109   0.0245
  -7.000  -0.3661   0.01083   0.00559  -0.1060   0.9010   0.0259
  -6.750  -0.3361   0.01038   0.00508  -0.1066   0.8918   0.0296
  -6.500  -0.3070   0.01020   0.00483  -0.1069   0.8820   0.0322
  -6.250  -0.2767   0.00985   0.00445  -0.1075   0.8722   0.0370
  -6.000  -0.2472   0.00967   0.00421  -0.1078   0.8628   0.0409
  -5.750  -0.2171   0.00938   0.00390  -0.1084   0.8530   0.0490
  -5.500  -0.1869   0.00913   0.00365  -0.1089   0.8433   0.0587
  -5.250  -0.1569   0.00891   0.00342  -0.1094   0.8338   0.0718
  -5.000  -0.1268   0.00868   0.00321  -0.1099   0.8237   0.0887
  -4.750  -0.0966   0.00846   0.00302  -0.1105   0.8140   0.1080
  -4.500  -0.0667   0.00830   0.00286  -0.1110   0.8044   0.1267
  -4.250  -0.0366   0.00814   0.00273  -0.1115   0.7950   0.1449
  -4.000  -0.0066   0.00799   0.00262  -0.1119   0.7867   0.1669
  -3.750   0.0233   0.00790   0.00252  -0.1124   0.7785   0.1840
  -3.500   0.0532   0.00781   0.00244  -0.1128   0.7713   0.1984
  -3.250   0.0831   0.00773   0.00236  -0.1131   0.7639   0.2119
  -3.000   0.1130   0.00766   0.00229  -0.1135   0.7573   0.2256
  -2.750   0.1429   0.00759   0.00223  -0.1139   0.7503   0.2399
  -2.500   0.1727   0.00754   0.00218  -0.1143   0.7438   0.2553
  -2.250   0.2026   0.00747   0.00215  -0.1147   0.7371   0.2712
  -2.000   0.2324   0.00744   0.00211  -0.1150   0.7308   0.2872
  -1.750   0.2622   0.00739   0.00209  -0.1154   0.7250   0.3030
  -1.500   0.2920   0.00736   0.00208  -0.1157   0.7189   0.3177
  -1.250   0.3216   0.00735   0.00207  -0.1160   0.7128   0.3321
  -1.000   0.3514   0.00731   0.00207  -0.1164   0.7062   0.3459
  -0.750   0.3810   0.00732   0.00207  -0.1166   0.7000   0.3586
  -0.500   0.4107   0.00730   0.00208  -0.1169   0.6943   0.3716
  -0.250   0.4403   0.00730   0.00209  -0.1172   0.6883   0.3843
   0.000   0.4699   0.00732   0.00212  -0.1175   0.6828   0.3968
   0.250   0.4996   0.00730   0.00215  -0.1178   0.6771   0.4102
   0.500   0.5291   0.00732   0.00218  -0.1181   0.6712   0.4228
   0.750   0.5586   0.00733   0.00222  -0.1184   0.6657   0.4338
   1.250   0.6176   0.00737   0.00231  -0.1189   0.6539   0.4566
   1.500   0.6472   0.00737   0.00236  -0.1192   0.6480   0.4684
   1.750   0.6767   0.00739   0.00242  -0.1195   0.6415   0.4807
   2.000   0.7061   0.00741   0.00248  -0.1197   0.6322   0.4939
   2.250   0.7351   0.00747   0.00250  -0.1199   0.6101   0.5085
   2.500   0.7643   0.00754   0.00255  -0.1201   0.5859   0.5254
   2.750   0.7934   0.00762   0.00264  -0.1204   0.5661   0.5449
   3.000   0.8226   0.00771   0.00273  -0.1206   0.5466   0.5682
   3.250   0.8517   0.00782   0.00285  -0.1209   0.5209   0.5999
   3.500   0.8807   0.00797   0.00302  -0.1213   0.4880   0.6495
   3.750   0.9091   0.00804   0.00329  -0.1216   0.4426   0.7959
   4.000   0.9294   0.00815   0.00343  -0.1200   0.3742   1.0000
   4.250   0.9550   0.00941   0.00401  -0.1203   0.2395   1.0000
   4.500   0.9804   0.01053   0.00460  -0.1204   0.1345   1.0000
   4.750   1.0069   0.01125   0.00504  -0.1205   0.0816   1.0000
   5.000   1.0340   0.01174   0.00538  -0.1205   0.0577   1.0000
   5.250   1.0613   0.01215   0.00572  -0.1205   0.0450   1.0000
   5.500   1.0885   0.01251   0.00604  -0.1205   0.0386   1.0000
   5.750   1.1157   0.01287   0.00639  -0.1204   0.0338   1.0000
   6.000   1.1424   0.01329   0.00677  -0.1203   0.0293   1.0000
   6.250   1.1692   0.01367   0.00717  -0.1202   0.0269   1.0000
   6.500   1.1959   0.01402   0.00753  -0.1201   0.0249   1.0000
   6.750   1.2213   0.01460   0.00811  -0.1197   0.0223   1.0000
   7.000   1.2473   0.01499   0.00853  -0.1195   0.0211   1.0000
   7.250   1.2733   0.01537   0.00892  -0.1193   0.0199   1.0000
   7.500   1.2987   0.01580   0.00936  -0.1189   0.0187   1.0000
   7.750   1.3220   0.01654   0.01012  -0.1183   0.0173   1.0000
   8.000   1.3456   0.01717   0.01081  -0.1177   0.0166   1.0000
   8.250   1.3700   0.01763   0.01131  -0.1172   0.0160   1.0000
   8.500   1.3937   0.01816   0.01188  -0.1166   0.0153   1.0000
   8.750   1.4170   0.01869   0.01244  -0.1160   0.0146   1.0000
   9.000   1.4396   0.01927   0.01303  -0.1153   0.0140   1.0000
   9.250   1.4564   0.02048   0.01430  -0.1137   0.0131   1.0000
   9.500   1.4761   0.02128   0.01517  -0.1125   0.0128   1.0000
   9.750   1.4968   0.02190   0.01586  -0.1115   0.0124   1.0000
  10.000   1.5162   0.02261   0.01663  -0.1103   0.0121   1.0000
  10.250   1.5342   0.02337   0.01746  -0.1088   0.0117   1.0000
  10.500   1.5512   0.02415   0.01829  -0.1073   0.0113   1.0000
  10.750   1.5669   0.02495   0.01914  -0.1056   0.0110   1.0000
  11.000   1.5810   0.02581   0.02005  -0.1036   0.0107   1.0000
  11.250   1.5924   0.02681   0.02112  -0.1013   0.0105   1.0000
  11.500   1.5956   0.02818   0.02257  -0.0979   0.0102   1.0000
  11.750   1.5931   0.03031   0.02482  -0.0942   0.0099   1.0000
  12.000   1.5929   0.03251   0.02718  -0.0911   0.0097   1.0000
  12.250   1.6038   0.03365   0.02840  -0.0895   0.0096   1.0000
  12.500   1.6125   0.03508   0.02992  -0.0879   0.0094   1.0000
  12.750   1.6207   0.03661   0.03155  -0.0863   0.0093   1.0000
  13.000   1.6268   0.03839   0.03344  -0.0847   0.0091   1.0000
  13.250   1.6315   0.04040   0.03556  -0.0832   0.0089   1.0000
  13.500   1.6353   0.04255   0.03782  -0.0818   0.0088   1.0000
  13.750   1.6384   0.04480   0.04019  -0.0806   0.0086   1.0000
  14.000   1.6406   0.04723   0.04273  -0.0795   0.0085   1.0000
  14.250   1.6420   0.04981   0.04542  -0.0786   0.0084   1.0000
  14.500   1.6421   0.05258   0.04829  -0.0778   0.0082   1.0000
  14.750   1.6415   0.05550   0.05132  -0.0772   0.0081   1.0000
  15.000   1.6392   0.05873   0.05466  -0.0768   0.0080   1.0000
  15.250   1.6359   0.06213   0.05817  -0.0765   0.0079   1.0000
  15.500   1.6316   0.06576   0.06191  -0.0765   0.0078   1.0000
  15.750   1.6256   0.06980   0.06606  -0.0768   0.0078   1.0000
  16.000   1.6179   0.07426   0.07064  -0.0773   0.0077   1.0000
  16.250   1.6072   0.07929   0.07580  -0.0782   0.0076   1.0000
  16.500   1.5944   0.08487   0.08152  -0.0795   0.0075   1.0000
  16.750   1.5797   0.09100   0.08781  -0.0813   0.0075   1.0000
  17.000   1.5626   0.09779   0.09476  -0.0837   0.0075   1.0000
  17.250   1.5421   0.10544   0.10257  -0.0867   0.0074   1.0000
  17.500   1.5214   0.11351   0.11081  -0.0903   0.0074   1.0000
  17.750   1.5019   0.12174   0.11920  -0.0944   0.0074   1.0000
  18.000   1.4785   0.13113   0.12877  -0.0995   0.0073   1.0000
  18.250   1.4586   0.14023   0.13802  -0.1048   0.0074   1.0000
  18.500   1.4381   0.15000   0.14794  -0.1108   0.0074   1.0000
  18.750   1.4146   0.16112   0.15924  -0.1179   0.0074   1.0000
  19.000   1.3824   0.17552   0.17385  -0.1275   0.0075   1.0000
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