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FX 73-CL1-152 (fx73cl1152-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 73-CL1-152 (fx73cl1152-il)
Reynolds number: 1,000,000
Max Cl/Cd: 136.82 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx73cl1152-il-1000000-n5.txt
Download as CSV file: xf-fx73cl1152-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.5360   0.07146   0.06766  -0.0876   0.6324   0.0239
 -13.750  -0.8022   0.02964   0.02547  -0.1256   0.6854   0.0236
 -13.500  -0.7991   0.02660   0.02218  -0.1274   0.6644   0.0237
 -13.250  -0.7871   0.02496   0.02035  -0.1276   0.6448   0.0237
 -13.000  -0.7736   0.02346   0.01868  -0.1274   0.6275   0.0239
 -12.500  -0.7373   0.02134   0.01629  -0.1268   0.5961   0.0244
 -12.250  -0.7163   0.02058   0.01542  -0.1264   0.5814   0.0246
 -12.000  -0.6944   0.01989   0.01461  -0.1259   0.5675   0.0248
 -11.750  -0.6715   0.01929   0.01390  -0.1255   0.5536   0.0250
 -11.500  -0.6480   0.01871   0.01322  -0.1251   0.5425   0.0252
 -11.250  -0.6239   0.01821   0.01262  -0.1247   0.5316   0.0255
 -11.000  -0.5993   0.01772   0.01204  -0.1243   0.5225   0.0258
 -10.500  -0.5491   0.01684   0.01096  -0.1235   0.5052   0.0264
 -10.250  -0.5238   0.01642   0.01044  -0.1231   0.4968   0.0266
 -10.000  -0.4981   0.01601   0.00994  -0.1227   0.4899   0.0269
  -9.750  -0.4721   0.01562   0.00947  -0.1223   0.4825   0.0271
  -9.250  -0.4200   0.01484   0.00851  -0.1215   0.4688   0.0276
  -9.000  -0.3938   0.01445   0.00806  -0.1212   0.4628   0.0279
  -8.500  -0.3402   0.01385   0.00734  -0.1205   0.4529   0.0286
  -8.250  -0.3130   0.01359   0.00703  -0.1202   0.4486   0.0290
  -8.000  -0.2857   0.01334   0.00672  -0.1198   0.4441   0.0293
  -7.750  -0.2585   0.01310   0.00642  -0.1195   0.4397   0.0297
  -7.500  -0.2310   0.01288   0.00614  -0.1192   0.4362   0.0302
  -7.250  -0.2033   0.01267   0.00588  -0.1189   0.4333   0.0306
  -7.000  -0.1755   0.01248   0.00563  -0.1186   0.4297   0.0310
  -6.750  -0.1481   0.01224   0.00534  -0.1183   0.4260   0.0314
  -6.500  -0.1206   0.01202   0.00507  -0.1179   0.4221   0.0320
  -6.250  -0.0928   0.01184   0.00486  -0.1176   0.4189   0.0325
  -6.000  -0.0648   0.01165   0.00465  -0.1174   0.4169   0.0330
  -5.750  -0.0367   0.01150   0.00446  -0.1171   0.4147   0.0336
  -5.500  -0.0086   0.01135   0.00427  -0.1168   0.4122   0.0341
  -5.250   0.0194   0.01121   0.00409  -0.1165   0.4098   0.0347
  -5.000   0.0475   0.01109   0.00393  -0.1163   0.4073   0.0352
  -4.750   0.0754   0.01094   0.00375  -0.1160   0.4047   0.0360
  -4.250   0.1317   0.01070   0.00348  -0.1154   0.4001   0.0377
  -4.000   0.1600   0.01059   0.00335  -0.1152   0.3984   0.0385
  -3.750   0.1884   0.01049   0.00323  -0.1150   0.3965   0.0393
  -3.500   0.2167   0.01040   0.00311  -0.1147   0.3946   0.0401
  -3.250   0.2449   0.01029   0.00299  -0.1145   0.3927   0.0412
  -3.000   0.2731   0.01021   0.00290  -0.1142   0.3907   0.0424
  -2.750   0.3013   0.01015   0.00282  -0.1139   0.3885   0.0438
  -2.500   0.3294   0.01011   0.00275  -0.1137   0.3860   0.0452
  -2.250   0.3575   0.01005   0.00268  -0.1134   0.3837   0.0469
  -2.000   0.3859   0.00998   0.00262  -0.1132   0.3825   0.0488
  -1.750   0.4144   0.00992   0.00256  -0.1130   0.3808   0.0506
  -1.500   0.4427   0.00987   0.00251  -0.1128   0.3788   0.0533
  -1.250   0.4710   0.00983   0.00247  -0.1125   0.3768   0.0562
  -1.000   0.4991   0.00979   0.00244  -0.1123   0.3747   0.0600
  -0.750   0.5273   0.00977   0.00242  -0.1121   0.3726   0.0636
  -0.500   0.5553   0.00976   0.00240  -0.1118   0.3704   0.0680
  -0.250   0.5832   0.00976   0.00240  -0.1115   0.3679   0.0726
   0.250   0.6396   0.00970   0.00240  -0.1111   0.3653   0.0861
   0.500   0.6677   0.00967   0.00240  -0.1109   0.3640   0.0949
   0.750   0.6958   0.00964   0.00241  -0.1107   0.3624   0.1070
   1.000   0.7237   0.00962   0.00243  -0.1105   0.3605   0.1222
   1.250   0.7515   0.00959   0.00246  -0.1102   0.3584   0.1422
   1.500   0.7792   0.00958   0.00250  -0.1100   0.3562   0.1656
   1.750   0.8069   0.00960   0.00255  -0.1097   0.3542   0.1844
   2.000   0.8344   0.00962   0.00261  -0.1094   0.3521   0.2040
   2.250   0.8619   0.00965   0.00268  -0.1092   0.3504   0.2234
   2.500   0.8898   0.00965   0.00274  -0.1090   0.3492   0.2417
   2.750   0.9176   0.00966   0.00280  -0.1088   0.3478   0.2610
   3.000   0.9453   0.00968   0.00287  -0.1085   0.3461   0.2825
   3.250   0.9726   0.00968   0.00295  -0.1083   0.3441   0.3164
   3.500   0.9996   0.00964   0.00305  -0.1080   0.3418   0.3749
   3.750   1.0260   0.00958   0.00317  -0.1076   0.3394   0.4558
   4.000   1.0513   0.00947   0.00331  -0.1071   0.3370   0.5771
   4.250   1.0739   0.00924   0.00348  -0.1059   0.3348   0.7490
   4.750   1.1436   0.00903   0.00370  -0.1086   0.3315   1.0000
   5.000   1.1709   0.00914   0.00380  -0.1083   0.3295   1.0000
   5.250   1.1981   0.00925   0.00390  -0.1081   0.3272   1.0000
   5.500   1.2250   0.00938   0.00401  -0.1078   0.3248   1.0000
   5.750   1.2517   0.00953   0.00413  -0.1074   0.3224   1.0000
   6.000   1.2780   0.00969   0.00427  -0.1071   0.3195   1.0000
   6.250   1.3050   0.00981   0.00439  -0.1068   0.3177   1.0000
   6.500   1.3318   0.00993   0.00452  -0.1065   0.3153   1.0000
   6.750   1.3583   0.01007   0.00466  -0.1062   0.3126   1.0000
   7.000   1.3845   0.01023   0.00480  -0.1059   0.3099   1.0000
   7.250   1.4103   0.01040   0.00496  -0.1055   0.3072   1.0000
   7.500   1.4356   0.01060   0.00514  -0.1050   0.3043   1.0000
   7.750   1.4618   0.01074   0.00530  -0.1047   0.3025   1.0000
   8.000   1.4877   0.01089   0.00547  -0.1043   0.3002   1.0000
   8.250   1.5132   0.01106   0.00565  -0.1039   0.2974   1.0000
   8.500   1.5382   0.01126   0.00584  -0.1034   0.2943   1.0000
   8.750   1.5625   0.01149   0.00606  -0.1028   0.2911   1.0000
   9.000   1.5870   0.01169   0.00627  -0.1023   0.2886   1.0000
   9.250   1.6120   0.01187   0.00647  -0.1018   0.2865   1.0000
   9.500   1.6364   0.01207   0.00669  -0.1013   0.2841   1.0000
   9.750   1.6603   0.01229   0.00692  -0.1006   0.2816   1.0000
  10.000   1.6835   0.01254   0.00718  -0.0999   0.2788   1.0000
  10.250   1.7057   0.01282   0.00747  -0.0991   0.2758   1.0000
  10.500   1.7287   0.01306   0.00773  -0.0984   0.2736   1.0000
  10.750   1.7517   0.01328   0.00798  -0.0976   0.2717   1.0000
  11.000   1.7739   0.01353   0.00826  -0.0968   0.2692   1.0000
  11.250   1.7948   0.01383   0.00857  -0.0958   0.2659   1.0000
  11.500   1.8128   0.01424   0.00897  -0.0944   0.2611   1.0000
  11.750   1.8320   0.01453   0.00929  -0.0931   0.2566   1.0000
  12.000   1.8474   0.01493   0.00969  -0.0912   0.2509   1.0000
  12.250   1.8607   0.01544   0.01018  -0.0890   0.2461   1.0000
  12.500   1.8783   0.01578   0.01056  -0.0876   0.2425   1.0000
  12.750   1.8944   0.01620   0.01102  -0.0860   0.2388   1.0000
  13.000   1.9071   0.01681   0.01162  -0.0841   0.2341   1.0000
  13.250   1.9203   0.01744   0.01227  -0.0825   0.2282   1.0000
  13.500   1.9301   0.01832   0.01314  -0.0806   0.2204   1.0000
  13.750   1.9402   0.01929   0.01413  -0.0791   0.2129   1.0000
  14.000   1.9442   0.02082   0.01563  -0.0775   0.2023   1.0000
  14.250   1.9487   0.02252   0.01734  -0.0764   0.1931   1.0000
  14.500   1.9498   0.02471   0.01954  -0.0756   0.1837   1.0000
  14.750   1.9439   0.02774   0.02259  -0.0750   0.1742   1.0000
  15.000   1.9313   0.03169   0.02656  -0.0748   0.1649   1.0000
  15.250   1.9157   0.03609   0.03102  -0.0747   0.1566   1.0000
  15.500   1.8900   0.04163   0.03662  -0.0747   0.1489   1.0000
  15.750   1.8623   0.04741   0.04248  -0.0746   0.1429   1.0000
  16.000   1.8362   0.05302   0.04817  -0.0746   0.1385   1.0000
  16.250   1.8040   0.05943   0.05466  -0.0747   0.1329   1.0000
  16.500   1.7734   0.06584   0.06113  -0.0751   0.1276   1.0000
  16.750   1.7500   0.07150   0.06686  -0.0754   0.1229   1.0000
  17.000   1.7256   0.07739   0.07280  -0.0759   0.1187   1.0000
  17.250   1.7036   0.08303   0.07850  -0.0764   0.1136   1.0000
  17.500   1.6761   0.08947   0.08497  -0.0772   0.1073   1.0000
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