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OAF102 AIRFOIL (oaf102-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: OAF102 AIRFOIL (oaf102-il)
Reynolds number: 1,000,000
Max Cl/Cd: 92 at α=2.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-oaf102-il-1000000-n5.txt
Download as CSV file: xf-oaf102-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.9627   0.07975   0.07728  -0.0225   1.0000   0.0066
 -14.000  -1.0014   0.06940   0.06683  -0.0294   1.0000   0.0066
 -13.750  -1.0457   0.05845   0.05575  -0.0372   1.0000   0.0065
 -13.500  -1.0869   0.04592   0.04304  -0.0496   1.0000   0.0064
 -13.250  -1.0848   0.03291   0.02970  -0.0702   1.0000   0.0065
 -13.000  -1.0582   0.02789   0.02441  -0.0796   1.0000   0.0066
 -12.750  -1.0326   0.02574   0.02209  -0.0830   1.0000   0.0067
 -12.500  -1.0061   0.02411   0.02032  -0.0854   1.0000   0.0067
 -12.250  -0.9792   0.02232   0.01838  -0.0880   1.0000   0.0070
 -12.000  -0.9514   0.02094   0.01688  -0.0900   1.0000   0.0073
 -11.750  -0.9232   0.01990   0.01574  -0.0915   1.0000   0.0076
 -11.500  -0.8946   0.01902   0.01479  -0.0928   1.0000   0.0078
 -11.250  -0.8657   0.01821   0.01390  -0.0940   1.0000   0.0081
 -10.750  -0.8054   0.01677   0.01226  -0.0967   0.9678   0.0087
 -10.500  -0.7777   0.01620   0.01157  -0.0972   0.9548   0.0090
 -10.250  -0.7503   0.01568   0.01095  -0.0976   0.9432   0.0092
 -10.000  -0.7220   0.01503   0.01020  -0.0983   0.9334   0.0097
  -9.750  -0.6938   0.01450   0.00958  -0.0988   0.9240   0.0102
  -9.500  -0.6653   0.01405   0.00905  -0.0993   0.9141   0.0107
  -9.250  -0.6364   0.01364   0.00856  -0.0998   0.9048   0.0113
  -9.000  -0.6076   0.01327   0.00810  -0.1002   0.8958   0.0118
  -8.750  -0.5783   0.01293   0.00767  -0.1008   0.8863   0.0123
  -8.500  -0.5488   0.01250   0.00717  -0.1014   0.8770   0.0132
  -8.250  -0.5194   0.01217   0.00677  -0.1019   0.8670   0.0142
  -8.000  -0.4898   0.01189   0.00641  -0.1024   0.8576   0.0153
  -7.750  -0.4602   0.01162   0.00606  -0.1029   0.8485   0.0162
  -7.500  -0.4302   0.01130   0.00569  -0.1035   0.8387   0.0177
  -7.250  -0.4004   0.01104   0.00537  -0.1041   0.8293   0.0192
  -7.000  -0.3707   0.01084   0.00509  -0.1045   0.8198   0.0203
  -6.750  -0.3406   0.01056   0.00478  -0.1051   0.8108   0.0229
  -6.500  -0.3106   0.01036   0.00451  -0.1056   0.8021   0.0252
  -6.250  -0.2806   0.01015   0.00426  -0.1061   0.7930   0.0279
  -6.000  -0.2505   0.00994   0.00402  -0.1067   0.7849   0.0314
  -5.750  -0.2205   0.00976   0.00379  -0.1072   0.7766   0.0355
  -5.500  -0.1904   0.00957   0.00358  -0.1077   0.7688   0.0401
  -5.250  -0.1602   0.00940   0.00338  -0.1082   0.7605   0.0465
  -5.000  -0.1301   0.00921   0.00319  -0.1087   0.7526   0.0548
  -4.750  -0.0999   0.00905   0.00301  -0.1093   0.7442   0.0650
  -4.500  -0.0697   0.00886   0.00284  -0.1098   0.7358   0.0786
  -4.250  -0.0395   0.00871   0.00270  -0.1103   0.7282   0.0923
  -4.000  -0.0093   0.00855   0.00256  -0.1109   0.7210   0.1080
  -3.750   0.0208   0.00841   0.00244  -0.1114   0.7147   0.1240
  -3.500   0.0509   0.00828   0.00234  -0.1119   0.7094   0.1407
  -3.250   0.0810   0.00815   0.00225  -0.1123   0.7037   0.1589
  -3.000   0.1110   0.00806   0.00218  -0.1128   0.6984   0.1756
  -2.750   0.1409   0.00799   0.00212  -0.1132   0.6933   0.1885
  -2.500   0.1708   0.00792   0.00206  -0.1136   0.6877   0.2010
  -2.250   0.2007   0.00786   0.00202  -0.1139   0.6824   0.2141
  -2.000   0.2306   0.00779   0.00198  -0.1143   0.6770   0.2272
  -1.750   0.2604   0.00774   0.00194  -0.1147   0.6718   0.2404
  -1.500   0.2902   0.00770   0.00192  -0.1151   0.6671   0.2528
  -1.250   0.3200   0.00766   0.00191  -0.1154   0.6614   0.2661
  -1.000   0.3497   0.00764   0.00189  -0.1158   0.6549   0.2796
  -0.750   0.3795   0.00761   0.00189  -0.1161   0.6490   0.2925
  -0.250   0.4388   0.00759   0.00191  -0.1167   0.6378   0.3206
   0.000   0.4685   0.00757   0.00193  -0.1171   0.6323   0.3334
   0.250   0.4981   0.00756   0.00196  -0.1174   0.6266   0.3482
   0.500   0.5277   0.00756   0.00199  -0.1177   0.6211   0.3612
   0.750   0.5573   0.00757   0.00203  -0.1179   0.6152   0.3708
   1.000   0.5868   0.00760   0.00207  -0.1182   0.6091   0.3805
   1.250   0.6163   0.00761   0.00212  -0.1185   0.6033   0.3897
   1.750   0.6752   0.00767   0.00223  -0.1190   0.5899   0.4086
   2.000   0.7044   0.00774   0.00229  -0.1193   0.5767   0.4178
   2.250   0.7332   0.00797   0.00237  -0.1195   0.5320   0.4280
   2.500   0.7616   0.00837   0.00252  -0.1198   0.4674   0.4393
   2.750   0.7900   0.00873   0.00270  -0.1201   0.4177   0.4509
   3.000   0.8182   0.00919   0.00294  -0.1204   0.3578   0.4633
   3.250   0.8455   0.00991   0.00329  -0.1207   0.2711   0.4774
   3.500   0.8727   0.01064   0.00369  -0.1210   0.1893   0.4926
   4.000   0.9274   0.01173   0.00440  -0.1214   0.0843   0.5308
   4.250   0.9552   0.01205   0.00467  -0.1215   0.0636   0.5507
   4.500   0.9832   0.01230   0.00494  -0.1217   0.0515   0.5740
   4.750   1.0111   0.01254   0.00520  -0.1218   0.0428   0.6037
   5.000   1.0391   0.01276   0.00549  -0.1220   0.0356   0.6495
   5.250   1.0672   0.01280   0.00582  -0.1222   0.0316   0.7665
   5.500   1.0878   0.01263   0.00602  -0.1205   0.0279   1.0000
   5.750   1.1152   0.01291   0.00630  -0.1205   0.0256   1.0000
   6.000   1.1422   0.01326   0.00661  -0.1205   0.0226   1.0000
   6.250   1.1693   0.01356   0.00692  -0.1204   0.0209   1.0000
   6.500   1.1960   0.01389   0.00725  -0.1203   0.0193   1.0000
   6.750   1.2224   0.01426   0.00761  -0.1201   0.0178   1.0000
   7.000   1.2487   0.01463   0.00799  -0.1199   0.0166   1.0000
   7.250   1.2749   0.01498   0.00836  -0.1198   0.0156   1.0000
   7.500   1.3007   0.01536   0.00874  -0.1195   0.0146   1.0000
   7.750   1.3260   0.01579   0.00918  -0.1192   0.0137   1.0000
   8.000   1.3508   0.01627   0.00967  -0.1188   0.0129   1.0000
   8.250   1.3757   0.01668   0.01012  -0.1184   0.0124   1.0000
   8.500   1.4003   0.01712   0.01060  -0.1180   0.0119   1.0000
   8.750   1.4243   0.01759   0.01109  -0.1175   0.0114   1.0000
   9.000   1.4479   0.01809   0.01161  -0.1169   0.0109   1.0000
   9.250   1.4708   0.01863   0.01217  -0.1162   0.0104   1.0000
   9.500   1.4922   0.01932   0.01289  -0.1153   0.0097   1.0000
   9.750   1.5146   0.01983   0.01345  -0.1146   0.0095   1.0000
  10.000   1.5362   0.02039   0.01407  -0.1137   0.0092   1.0000
  10.250   1.5569   0.02100   0.01473  -0.1127   0.0090   1.0000
  10.500   1.5767   0.02163   0.01541  -0.1116   0.0087   1.0000
  10.750   1.5956   0.02229   0.01611  -0.1103   0.0084   1.0000
  11.000   1.6133   0.02298   0.01686  -0.1089   0.0081   1.0000
  11.250   1.6297   0.02372   0.01765  -0.1072   0.0079   1.0000
  11.500   1.6442   0.02454   0.01852  -0.1053   0.0077   1.0000
  11.750   1.6562   0.02549   0.01953  -0.1031   0.0074   1.0000
  12.000   1.6614   0.02668   0.02080  -0.0999   0.0072   1.0000
  12.250   1.6691   0.02780   0.02200  -0.0973   0.0071   1.0000
  12.500   1.6781   0.02895   0.02324  -0.0951   0.0070   1.0000
  12.750   1.6872   0.03018   0.02455  -0.0931   0.0069   1.0000
  13.000   1.6962   0.03149   0.02595  -0.0913   0.0068   1.0000
  13.250   1.7042   0.03295   0.02750  -0.0896   0.0066   1.0000
  13.500   1.7119   0.03449   0.02913  -0.0880   0.0065   1.0000
  13.750   1.7191   0.03613   0.03085  -0.0865   0.0064   1.0000
  14.000   1.7251   0.03793   0.03275  -0.0851   0.0062   1.0000
  14.250   1.7306   0.03986   0.03476  -0.0838   0.0061   1.0000
  14.500   1.7352   0.04192   0.03692  -0.0826   0.0060   1.0000
  14.750   1.7388   0.04413   0.03922  -0.0815   0.0059   1.0000
  15.000   1.7412   0.04653   0.04171  -0.0805   0.0058   1.0000
  15.250   1.7430   0.04905   0.04433  -0.0797   0.0057   1.0000
  15.500   1.7435   0.05177   0.04715  -0.0789   0.0057   1.0000
  15.750   1.7425   0.05472   0.05020  -0.0783   0.0056   1.0000
  16.000   1.7401   0.05791   0.05349  -0.0778   0.0055   1.0000
  16.250   1.7359   0.06142   0.05712  -0.0775   0.0054   1.0000
  16.500   1.7300   0.06528   0.06110  -0.0775   0.0053   1.0000
  16.750   1.7230   0.06944   0.06538  -0.0777   0.0053   1.0000
  17.000   1.7135   0.07414   0.07021  -0.0782   0.0052   1.0000
  17.250   1.7015   0.07937   0.07557  -0.0792   0.0051   1.0000
  17.500   1.6871   0.08513   0.08148  -0.0805   0.0051   1.0000
  17.750   1.6729   0.09112   0.08760  -0.0822   0.0051   1.0000
  18.000   1.6612   0.09687   0.09350  -0.0841   0.0050   1.0000
  18.250   1.6464   0.10329   0.10006  -0.0864   0.0050   1.0000
  18.500   1.6302   0.11015   0.10706  -0.0891   0.0050   1.0000
  18.750   1.6118   0.11768   0.11474  -0.0925   0.0050   1.0000
  19.000   1.5919   0.12576   0.12297  -0.0964   0.0050   1.0000
  19.250   1.5702   0.13449   0.13185  -0.1010   0.0050   1.0000
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