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OAF095 AIRFOIL (oaf095-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: OAF095 AIRFOIL (oaf095-il)
Reynolds number: 1,000,000
Max Cl/Cd: 98.35 at α=2.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-oaf095-il-1000000-n5.txt
Download as CSV file: xf-oaf095-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: OAF095 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.9154   0.08009   0.07765  -0.0300   1.0000   0.0090
 -14.000  -0.9557   0.06946   0.06691  -0.0378   1.0000   0.0089
 -13.750  -1.0096   0.05690   0.05420  -0.0480   1.0000   0.0087
 -13.500  -1.0486   0.03528   0.03217  -0.0787   1.0000   0.0085
 -13.250  -1.0223   0.02606   0.02257  -0.0953   1.0000   0.0087
 -13.000  -0.9957   0.02387   0.02024  -0.0989   1.0000   0.0090
 -12.750  -0.9686   0.02229   0.01854  -0.1013   1.0000   0.0093
 -12.500  -0.9410   0.02101   0.01714  -0.1032   1.0000   0.0096
 -12.250  -0.9131   0.01991   0.01594  -0.1049   1.0000   0.0099
 -12.000  -0.8848   0.01894   0.01487  -0.1063   1.0000   0.0102
 -11.750  -0.8545   0.01807   0.01390  -0.1079   0.9912   0.0105
 -11.500  -0.8232   0.01725   0.01298  -0.1096   0.9823   0.0108
 -11.250  -0.7935   0.01638   0.01201  -0.1109   0.9737   0.0113
 -11.000  -0.7650   0.01571   0.01127  -0.1118   0.9659   0.0119
 -10.750  -0.7374   0.01515   0.01063  -0.1122   0.9581   0.0124
 -10.500  -0.7096   0.01465   0.01006  -0.1126   0.9514   0.0130
 -10.250  -0.6820   0.01420   0.00952  -0.1129   0.9445   0.0135
 -10.000  -0.6538   0.01369   0.00893  -0.1134   0.9386   0.0141
  -9.750  -0.6254   0.01319   0.00837  -0.1138   0.9322   0.0149
  -9.250  -0.5683   0.01240   0.00745  -0.1146   0.9207   0.0164
  -9.000  -0.5395   0.01206   0.00703  -0.1149   0.9148   0.0170
  -8.750  -0.5107   0.01169   0.00659  -0.1153   0.9093   0.0179
  -8.500  -0.4813   0.01133   0.00619  -0.1157   0.9034   0.0191
  -8.250  -0.4523   0.01104   0.00584  -0.1161   0.8974   0.0203
  -8.000  -0.4231   0.01078   0.00551  -0.1164   0.8918   0.0212
  -7.750  -0.3936   0.01046   0.00515  -0.1168   0.8857   0.0226
  -7.500  -0.3644   0.01019   0.00484  -0.1172   0.8797   0.0243
  -7.250  -0.3348   0.00995   0.00456  -0.1175   0.8736   0.0258
  -7.000  -0.3052   0.00972   0.00427  -0.1179   0.8671   0.0273
  -6.750  -0.2756   0.00948   0.00400  -0.1182   0.8609   0.0295
  -6.500  -0.2460   0.00927   0.00376  -0.1186   0.8541   0.0317
  -6.250  -0.2164   0.00908   0.00351  -0.1189   0.8475   0.0344
  -6.000  -0.1866   0.00887   0.00329  -0.1193   0.8403   0.0375
  -5.500  -0.1272   0.00851   0.00287  -0.1199   0.8242   0.0459
  -5.250  -0.0976   0.00837   0.00269  -0.1202   0.8155   0.0508
  -5.000  -0.0677   0.00820   0.00252  -0.1206   0.8065   0.0572
  -4.750  -0.0379   0.00804   0.00235  -0.1209   0.7990   0.0662
  -4.500  -0.0080   0.00790   0.00221  -0.1213   0.7911   0.0745
  -4.250   0.0217   0.00779   0.00208  -0.1216   0.7837   0.0829
  -4.000   0.0516   0.00766   0.00196  -0.1219   0.7760   0.0926
  -3.750   0.0814   0.00755   0.00185  -0.1222   0.7690   0.1023
  -3.500   0.1112   0.00745   0.00176  -0.1226   0.7616   0.1127
  -3.250   0.1409   0.00737   0.00167  -0.1228   0.7544   0.1237
  -3.000   0.1708   0.00728   0.00160  -0.1231   0.7471   0.1370
  -2.500   0.2302   0.00714   0.00149  -0.1237   0.7317   0.1616
  -2.250   0.2598   0.00710   0.00144  -0.1240   0.7236   0.1728
  -2.000   0.2895   0.00705   0.00141  -0.1242   0.7159   0.1828
  -1.500   0.3488   0.00698   0.00135  -0.1247   0.7014   0.2047
  -1.250   0.3783   0.00696   0.00134  -0.1249   0.6938   0.2169
  -1.000   0.4079   0.00693   0.00133  -0.1251   0.6850   0.2301
  -0.750   0.4374   0.00694   0.00133  -0.1253   0.6743   0.2421
  -0.500   0.4668   0.00694   0.00133  -0.1256   0.6629   0.2568
  -0.250   0.4963   0.00693   0.00135  -0.1258   0.6533   0.2716
   0.000   0.5257   0.00694   0.00137  -0.1260   0.6440   0.2867
   0.250   0.5551   0.00696   0.00141  -0.1262   0.6324   0.3031
   0.500   0.5843   0.00701   0.00144  -0.1263   0.6165   0.3184
   0.750   0.6134   0.00709   0.00149  -0.1265   0.5971   0.3310
   1.000   0.6424   0.00717   0.00154  -0.1266   0.5787   0.3422
   1.250   0.6714   0.00726   0.00161  -0.1268   0.5596   0.3554
   1.500   0.7003   0.00739   0.00168  -0.1269   0.5384   0.3679
   1.750   0.7290   0.00753   0.00177  -0.1270   0.5123   0.3796
   2.000   0.7575   0.00775   0.00189  -0.1271   0.4796   0.3909
   2.250   0.7858   0.00799   0.00202  -0.1272   0.4460   0.4026
   2.500   0.8137   0.00834   0.00219  -0.1273   0.3948   0.4152
   2.750   0.8410   0.00880   0.00243  -0.1273   0.3373   0.4302
   3.000   0.8680   0.00931   0.00271  -0.1274   0.2764   0.4477
   3.250   0.8952   0.00976   0.00298  -0.1274   0.2261   0.4693
   3.500   0.9224   0.01016   0.00326  -0.1274   0.1862   0.4922
   3.750   0.9496   0.01053   0.00353  -0.1274   0.1513   0.5143
   4.000   0.9767   0.01089   0.00380  -0.1274   0.1225   0.5400
   4.250   1.0039   0.01121   0.00409  -0.1273   0.0992   0.5713
   4.500   1.0312   0.01147   0.00437  -0.1273   0.0820   0.6132
   4.750   1.0586   0.01169   0.00468  -0.1274   0.0675   0.6849
   5.000   1.0794   0.01141   0.00492  -0.1257   0.0586   1.0000
   5.250   1.1063   0.01173   0.00520  -0.1256   0.0503   1.0000
   5.500   1.1329   0.01207   0.00549  -0.1253   0.0432   1.0000
   5.750   1.1597   0.01237   0.00576  -0.1251   0.0391   1.0000
   6.000   1.1860   0.01270   0.00607  -0.1249   0.0348   1.0000
   6.250   1.2125   0.01301   0.00637  -0.1246   0.0319   1.0000
   6.500   1.2384   0.01338   0.00670  -0.1243   0.0283   1.0000
   6.750   1.2645   0.01369   0.00703  -0.1240   0.0265   1.0000
   7.000   1.2901   0.01406   0.00738  -0.1236   0.0244   1.0000
   7.250   1.3155   0.01444   0.00776  -0.1232   0.0226   1.0000
   7.500   1.3409   0.01479   0.00812  -0.1228   0.0214   1.0000
   7.750   1.3658   0.01518   0.00852  -0.1223   0.0199   1.0000
   8.000   1.3902   0.01563   0.00896  -0.1217   0.0184   1.0000
   8.250   1.4147   0.01603   0.00938  -0.1212   0.0176   1.0000
   8.500   1.4389   0.01644   0.00982  -0.1206   0.0169   1.0000
   8.750   1.4626   0.01688   0.01029  -0.1199   0.0160   1.0000
   9.000   1.4858   0.01737   0.01078  -0.1192   0.0152   1.0000
   9.250   1.5080   0.01793   0.01136  -0.1183   0.0143   1.0000
   9.500   1.5309   0.01839   0.01186  -0.1175   0.0139   1.0000
   9.750   1.5531   0.01888   0.01238  -0.1167   0.0134   1.0000
  10.000   1.5746   0.01941   0.01296  -0.1157   0.0129   1.0000
  10.250   1.5955   0.01997   0.01355  -0.1147   0.0124   1.0000
  10.500   1.6155   0.02057   0.01418  -0.1135   0.0120   1.0000
  10.750   1.6344   0.02125   0.01489  -0.1122   0.0115   1.0000
  11.000   1.6520   0.02199   0.01568  -0.1107   0.0111   1.0000
  11.250   1.6698   0.02263   0.01639  -0.1092   0.0109   1.0000
  11.500   1.6861   0.02331   0.01713  -0.1075   0.0107   1.0000
  11.750   1.7008   0.02401   0.01789  -0.1055   0.0104   1.0000
  12.000   1.7129   0.02475   0.01869  -0.1032   0.0101   1.0000
  12.250   1.7235   0.02558   0.01958  -0.1007   0.0098   1.0000
  12.500   1.7337   0.02652   0.02058  -0.0984   0.0095   1.0000
  12.750   1.7436   0.02755   0.02167  -0.0962   0.0093   1.0000
  13.000   1.7527   0.02870   0.02289  -0.0941   0.0091   1.0000
  13.250   1.7605   0.03001   0.02426  -0.0920   0.0089   1.0000
  13.500   1.7663   0.03155   0.02589  -0.0898   0.0086   1.0000
  13.750   1.7729   0.03307   0.02750  -0.0880   0.0085   1.0000
  14.000   1.7802   0.03458   0.02909  -0.0863   0.0084   1.0000
  14.250   1.7865   0.03624   0.03084  -0.0847   0.0083   1.0000
  14.500   1.7919   0.03802   0.03272  -0.0832   0.0081   1.0000
  14.750   1.7963   0.03998   0.03477  -0.0818   0.0080   1.0000
  15.000   1.7999   0.04208   0.03697  -0.0805   0.0079   1.0000
  15.250   1.8026   0.04432   0.03931  -0.0794   0.0078   1.0000
  15.500   1.8042   0.04674   0.04183  -0.0784   0.0076   1.0000
  15.750   1.8052   0.04932   0.04451  -0.0776   0.0075   1.0000
  16.000   1.8048   0.05212   0.04741  -0.0769   0.0074   1.0000
  16.250   1.8032   0.05513   0.05051  -0.0764   0.0072   1.0000
  16.500   1.8005   0.05838   0.05387  -0.0761   0.0071   1.0000
  16.750   1.7966   0.06194   0.05753  -0.0760   0.0070   1.0000
  17.000   1.7909   0.06586   0.06156  -0.0762   0.0069   1.0000
  17.250   1.7837   0.07012   0.06593  -0.0767   0.0068   1.0000
  17.500   1.7746   0.07484   0.07077  -0.0775   0.0068   1.0000
  17.750   1.7636   0.08000   0.07606  -0.0787   0.0067   1.0000
  18.000   1.7502   0.08567   0.08185  -0.0803   0.0066   1.0000
  18.250   1.7346   0.09190   0.08822  -0.0823   0.0066   1.0000
  18.500   1.7169   0.09870   0.09517  -0.0848   0.0065   1.0000
  18.750   1.6970   0.10610   0.10272  -0.0878   0.0065   1.0000
  19.000   1.6743   0.11421   0.11099  -0.0914   0.0064   1.0000
  19.250   1.6509   0.12280   0.11972  -0.0956   0.0064   1.0000
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