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FX 73-CL1-152 (fx73cl1152-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX 73-CL1-152 (fx73cl1152-il)
Reynolds number: 1,000,000
Max Cl/Cd: 137.36 at α=9.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx73cl1152-il-1000000.txt
Download as CSV file: xf-fx73cl1152-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 73-CL1-152                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.1324   0.12128   0.11766  -0.0616   0.5733   0.0276
 -12.250  -0.6244   0.02987   0.02638  -0.1260   0.7630   0.0286
 -12.000  -0.6212   0.02752   0.02373  -0.1268   0.7229   0.0287
 -11.500  -0.5956   0.02478   0.02056  -0.1264   0.6677   0.0292
 -11.250  -0.5783   0.02372   0.01932  -0.1261   0.6464   0.0294
 -11.000  -0.5601   0.02267   0.01808  -0.1257   0.6275   0.0297
 -10.750  -0.5403   0.02174   0.01697  -0.1252   0.6102   0.0300
 -10.500  -0.5192   0.02090   0.01597  -0.1248   0.5945   0.0303
 -10.250  -0.4970   0.02013   0.01504  -0.1244   0.5805   0.0306
 -10.000  -0.4738   0.01951   0.01426  -0.1240   0.5670   0.0308
  -9.750  -0.4497   0.01903   0.01362  -0.1235   0.5535   0.0311
  -9.500  -0.4289   0.01777   0.01219  -0.1231   0.5424   0.0316
  -9.250  -0.4050   0.01714   0.01146  -0.1227   0.5309   0.0320
  -9.000  -0.3795   0.01670   0.01096  -0.1223   0.5213   0.0324
  -8.750  -0.3539   0.01635   0.01052  -0.1219   0.5116   0.0327
  -8.500  -0.3278   0.01595   0.01005  -0.1215   0.5037   0.0331
  -8.250  -0.3018   0.01560   0.00959  -0.1211   0.4952   0.0336
  -8.000  -0.2754   0.01520   0.00911  -0.1207   0.4888   0.0340
  -7.750  -0.2488   0.01483   0.00865  -0.1204   0.4823   0.0344
  -7.500  -0.2223   0.01455   0.00825  -0.1200   0.4752   0.0348
  -7.250  -0.1949   0.01427   0.00790  -0.1196   0.4708   0.0352
  -7.000  -0.1692   0.01362   0.00716  -0.1193   0.4657   0.0358
  -6.750  -0.1427   0.01325   0.00673  -0.1189   0.4603   0.0364
  -6.500  -0.1155   0.01305   0.00649  -0.1185   0.4552   0.0370
  -6.250  -0.0876   0.01283   0.00624  -0.1183   0.4521   0.0377
  -6.000  -0.0600   0.01260   0.00596  -0.1180   0.4485   0.0383
  -5.750  -0.0324   0.01239   0.00569  -0.1176   0.4448   0.0390
  -5.500  -0.0048   0.01224   0.00546  -0.1173   0.4409   0.0395
  -5.250   0.0224   0.01199   0.00514  -0.1169   0.4371   0.0401
  -5.000   0.0498   0.01161   0.00475  -0.1166   0.4351   0.0411
  -4.750   0.0779   0.01142   0.00456  -0.1164   0.4327   0.0419
  -4.500   0.1059   0.01127   0.00438  -0.1161   0.4298   0.0428
  -4.250   0.1340   0.01116   0.00422  -0.1158   0.4269   0.0438
  -4.000   0.1620   0.01109   0.00409  -0.1155   0.4239   0.0446
  -3.750   0.1891   0.01085   0.00382  -0.1151   0.4206   0.0459
  -3.500   0.2171   0.01072   0.00368  -0.1148   0.4185   0.0471
  -3.250   0.2455   0.01060   0.00356  -0.1146   0.4170   0.0484
  -3.000   0.2739   0.01051   0.00344  -0.1144   0.4151   0.0496
  -2.750   0.3020   0.01034   0.00326  -0.1141   0.4130   0.0512
  -2.500   0.3302   0.01025   0.00317  -0.1139   0.4107   0.0532
  -2.250   0.3583   0.01020   0.00309  -0.1136   0.4084   0.0552
  -2.000   0.3862   0.01012   0.00299  -0.1133   0.4058   0.0576
  -1.750   0.4138   0.01011   0.00296  -0.1130   0.4025   0.0602
  -1.500   0.4420   0.01007   0.00291  -0.1127   0.4007   0.0630
  -1.250   0.4704   0.00996   0.00283  -0.1125   0.3993   0.0674
  -1.000   0.4987   0.00989   0.00277  -0.1123   0.3977   0.0722
  -0.750   0.5270   0.00983   0.00273  -0.1121   0.3958   0.0777
  -0.500   0.5551   0.00976   0.00269  -0.1118   0.3939   0.0849
  -0.250   0.5832   0.00972   0.00266  -0.1116   0.3918   0.0935
   0.000   0.6110   0.00968   0.00265  -0.1113   0.3898   0.1049
   0.250   0.6386   0.00967   0.00266  -0.1110   0.3876   0.1213
   0.500   0.6657   0.00968   0.00273  -0.1107   0.3848   0.1455
   0.750   0.6936   0.00964   0.00278  -0.1104   0.3834   0.1733
   1.000   0.7217   0.00959   0.00280  -0.1102   0.3821   0.1968
   1.250   0.7498   0.00956   0.00283  -0.1101   0.3806   0.2171
   1.500   0.7778   0.00955   0.00287  -0.1098   0.3788   0.2375
   1.750   0.8057   0.00954   0.00291  -0.1096   0.3771   0.2592
   2.000   0.8334   0.00952   0.00296  -0.1094   0.3753   0.2872
   2.250   0.8608   0.00951   0.00303  -0.1091   0.3735   0.3256
   2.500   0.8878   0.00949   0.00311  -0.1088   0.3714   0.3763
   2.750   0.9140   0.00948   0.00324  -0.1083   0.3689   0.4435
   3.000   0.9396   0.00939   0.00340  -0.1078   0.3668   0.5544
   3.250   0.9617   0.00898   0.00354  -0.1065   0.3657   0.7672
   3.500   1.0057   0.00867   0.00362  -0.1097   0.3639   1.0000
   3.750   1.0336   0.00874   0.00368  -0.1095   0.3621   1.0000
   4.000   1.0613   0.00883   0.00374  -0.1093   0.3602   1.0000
   4.250   1.0889   0.00893   0.00382  -0.1090   0.3582   1.0000
   4.500   1.1162   0.00904   0.00390  -0.1087   0.3562   1.0000
   4.750   1.1430   0.00919   0.00401  -0.1084   0.3538   1.0000
   5.000   1.1691   0.00941   0.00419  -0.1080   0.3507   1.0000
   5.250   1.1969   0.00948   0.00427  -0.1078   0.3496   1.0000
   5.500   1.2244   0.00956   0.00436  -0.1076   0.3480   1.0000
   5.750   1.2517   0.00966   0.00446  -0.1074   0.3461   1.0000
   6.000   1.2789   0.00976   0.00455  -0.1071   0.3439   1.0000
   6.250   1.3057   0.00987   0.00466  -0.1069   0.3415   1.0000
   6.500   1.3321   0.01002   0.00478  -0.1065   0.3389   1.0000
   6.750   1.3575   0.01024   0.00496  -0.1060   0.3358   1.0000
   7.000   1.3840   0.01037   0.00511  -0.1057   0.3339   1.0000
   7.250   1.4109   0.01048   0.00524  -0.1055   0.3321   1.0000
   7.500   1.4375   0.01059   0.00537  -0.1052   0.3299   1.0000
   7.750   1.4637   0.01072   0.00552  -0.1049   0.3274   1.0000
   8.000   1.4894   0.01088   0.00567  -0.1045   0.3248   1.0000
   8.250   1.5141   0.01109   0.00586  -0.1039   0.3218   1.0000
   8.500   1.5388   0.01132   0.00608  -0.1034   0.3188   1.0000
   8.750   1.5649   0.01144   0.00624  -0.1031   0.3168   1.0000
   9.000   1.5905   0.01158   0.00641  -0.1027   0.3145   1.0000
   9.250   1.6154   0.01176   0.00659  -0.1022   0.3118   1.0000
   9.500   1.6396   0.01197   0.00681  -0.1016   0.3091   1.0000
   9.750   1.6624   0.01224   0.00707  -0.1008   0.3060   1.0000
  10.000   1.6859   0.01248   0.00732  -0.1002   0.3034   1.0000
  10.250   1.7105   0.01264   0.00753  -0.0997   0.3012   1.0000
  10.500   1.7344   0.01283   0.00776  -0.0991   0.2988   1.0000
  10.750   1.7572   0.01307   0.00801  -0.0984   0.2962   1.0000
  11.000   1.7787   0.01335   0.00830  -0.0974   0.2932   1.0000
  11.250   1.7978   0.01373   0.00866  -0.0961   0.2893   1.0000
  11.500   1.8214   0.01389   0.00888  -0.0955   0.2866   1.0000
  11.750   1.8429   0.01412   0.00914  -0.0946   0.2823   1.0000
  12.000   1.8596   0.01449   0.00949  -0.0929   0.2778   1.0000
  12.250   1.8750   0.01487   0.00988  -0.0910   0.2741   1.0000
  12.500   1.8949   0.01511   0.01018  -0.0899   0.2711   1.0000
  12.750   1.9122   0.01545   0.01055  -0.0884   0.2680   1.0000
  13.000   1.9265   0.01593   0.01103  -0.0865   0.2638   1.0000
  13.250   1.9401   0.01647   0.01158  -0.0847   0.2591   1.0000
  13.500   1.9577   0.01687   0.01204  -0.0836   0.2547   1.0000
  13.750   1.9706   0.01753   0.01270  -0.0819   0.2501   1.0000
  14.000   1.9813   0.01837   0.01356  -0.0803   0.2454   1.0000
  14.250   1.9982   0.01894   0.01420  -0.0794   0.2423   1.0000
  14.500   2.0115   0.01978   0.01508  -0.0784   0.2382   1.0000
  14.750   2.0204   0.02102   0.01634  -0.0773   0.2338   1.0000
  15.000   2.0317   0.02218   0.01755  -0.0765   0.2299   1.0000
  15.250   2.0428   0.02342   0.01885  -0.0759   0.2255   1.0000
  15.500   2.0458   0.02543   0.02089  -0.0752   0.2201   1.0000
  15.750   2.0503   0.02742   0.02294  -0.0748   0.2154   1.0000
  16.000   2.0512   0.02981   0.02539  -0.0744   0.2094   1.0000
  16.250   2.0423   0.03330   0.02892  -0.0741   0.2035   1.0000
  16.500   2.0345   0.03672   0.03240  -0.0738   0.1968   1.0000
  16.750   2.0115   0.04178   0.03752  -0.0736   0.1902   1.0000
  17.000   1.9911   0.04657   0.04238  -0.0734   0.1840   1.0000
  17.250   1.9551   0.05312   0.04899  -0.0733   0.1778   1.0000
  17.500   1.9292   0.05871   0.05464  -0.0733   0.1716   1.0000
  17.750   1.8904   0.06593   0.06193  -0.0736   0.1658   1.0000
  18.000   1.8620   0.07208   0.06814  -0.0740   0.1588   1.0000
  18.250   1.8258   0.07924   0.07532  -0.0746   0.1520   1.0000
  18.500   1.7987   0.08542   0.08154  -0.0753   0.1452   1.0000
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