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WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX L V-152 AIRFOIL (fxlv152-il)
Reynolds number: 200,000
Max Cl/Cd: 45.32 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fxlv152-il-200000-n5.txt
Download as CSV file: xf-fxlv152-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX L V-152 AIRFOIL                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -0.9371   0.16719   0.16355   0.0487   1.0005   0.0109
 -18.250  -0.9634   0.15511   0.15133   0.0415   1.0005   0.0108
 -18.000  -0.9840   0.14520   0.14127   0.0356   1.0005   0.0107
 -17.750  -1.0030   0.13601   0.13195   0.0302   1.0005   0.0107
 -17.500  -1.0211   0.12741   0.12320   0.0253   1.0005   0.0107
 -17.250  -1.0384   0.11925   0.11489   0.0207   1.0005   0.0106
 -17.000  -1.0548   0.11154   0.10703   0.0165   1.0005   0.0106
 -16.750  -1.0697   0.10437   0.09970   0.0127   1.0005   0.0107
 -16.500  -1.0831   0.09766   0.09283   0.0092   1.0005   0.0107
 -16.250  -1.0949   0.09145   0.08647   0.0061   1.0005   0.0108
 -16.000  -1.1051   0.08575   0.08062   0.0034   1.0005   0.0109
 -15.750  -1.1138   0.08047   0.07519   0.0010   1.0005   0.0111
 -15.500  -1.1210   0.07560   0.07017  -0.0011   1.0005   0.0113
 -15.250  -1.1269   0.07110   0.06552  -0.0029   1.0005   0.0115
 -15.000  -1.1318   0.06690   0.06118  -0.0044   1.0005   0.0118
 -14.750  -1.1353   0.06308   0.05723  -0.0057   1.0005   0.0121
 -14.500  -1.1372   0.05962   0.05364  -0.0067   1.0005   0.0124
 -14.250  -1.1382   0.05640   0.05030  -0.0075   1.0005   0.0130
 -14.000  -1.1381   0.05340   0.04714  -0.0081   1.0005   0.0136
 -13.500  -1.1341   0.04796   0.04144  -0.0089   1.0005   0.0151
 -13.250  -1.1304   0.04550   0.03885  -0.0092   1.0005   0.0160
 -13.000  -1.1239   0.04338   0.03656  -0.0093   1.0005   0.0170
 -12.750  -1.1203   0.04098   0.03407  -0.0095   1.0005   0.0177
 -12.500  -1.1140   0.03889   0.03187  -0.0095   1.0005   0.0187
 -12.250  -1.1057   0.03702   0.02987  -0.0095   1.0005   0.0198
 -12.000  -1.0991   0.03501   0.02779  -0.0094   1.0005   0.0206
 -11.750  -1.0899   0.03327   0.02596  -0.0093   1.0005   0.0216
 -11.500  -1.0795   0.03168   0.02429  -0.0091   1.0005   0.0227
 -11.250  -1.0690   0.03012   0.02269  -0.0089   1.0005   0.0240
 -11.000  -1.0566   0.02877   0.02128  -0.0087   1.0005   0.0252
 -10.750  -1.0435   0.02751   0.01999  -0.0084   1.0005   0.0266
 -10.500  -1.0294   0.02639   0.01882  -0.0080   1.0005   0.0286
 -10.250  -1.0147   0.02536   0.01776  -0.0076   1.0005   0.0312
 -10.000  -0.9993   0.02444   0.01680  -0.0070   1.0005   0.0341
  -9.750  -0.9826   0.02362   0.01592  -0.0063   1.0005   0.0369
  -9.500  -0.9641   0.02282   0.01507  -0.0059   1.0005   0.0401
  -9.250  -0.9454   0.02199   0.01425  -0.0055   1.0005   0.0438
  -9.000  -0.9193   0.02129   0.01347  -0.0064   0.9138   0.0482
  -8.750  -0.8984   0.02071   0.01279  -0.0059   0.8737   0.0530
  -8.500  -0.8781   0.02021   0.01217  -0.0051   0.8503   0.0588
  -8.000  -0.8347   0.01919   0.01095  -0.0040   0.8160   0.0713
  -7.750  -0.8128   0.01864   0.01036  -0.0036   0.8024   0.0791
  -7.500  -0.7912   0.01804   0.00977  -0.0031   0.7902   0.0917
  -7.250  -0.7690   0.01746   0.00922  -0.0028   0.7789   0.1093
  -7.000  -0.7461   0.01692   0.00870  -0.0025   0.7697   0.1277
  -6.750  -0.7225   0.01643   0.00819  -0.0022   0.7619   0.1454
  -6.500  -0.6983   0.01597   0.00770  -0.0020   0.7545   0.1618
  -6.250  -0.6747   0.01541   0.00720  -0.0018   0.7465   0.1830
  -6.000  -0.6522   0.01477   0.00667  -0.0015   0.7399   0.2259
  -5.750  -0.6293   0.01403   0.00620  -0.0013   0.7327   0.2813
  -5.500  -0.6055   0.01347   0.00578  -0.0011   0.7266   0.3236
  -5.000  -0.5563   0.01263   0.00531  -0.0006   0.7157   0.4195
  -4.750  -0.5297   0.01245   0.00518  -0.0005   0.7105   0.4536
  -4.500  -0.5028   0.01234   0.00510  -0.0003   0.7059   0.4801
  -4.250  -0.4754   0.01232   0.00509  -0.0002   0.7018   0.5020
  -4.000  -0.4474   0.01233   0.00508  -0.0002   0.6969   0.5216
  -3.750  -0.4193   0.01236   0.00503  -0.0002   0.6922   0.5383
  -3.500  -0.3914   0.01239   0.00503  -0.0001   0.6879   0.5516
  -3.000  -0.3349   0.01242   0.00494  -0.0002   0.6805   0.5702
  -2.750  -0.3063   0.01240   0.00483  -0.0004   0.6766   0.5773
  -2.500  -0.2779   0.01241   0.00484  -0.0004   0.6729   0.5832
  -2.250  -0.2496   0.01244   0.00480  -0.0004   0.6693   0.5908
  -1.750  -0.1926   0.01246   0.00476  -0.0006   0.6620   0.6021
  -1.500  -0.1639   0.01246   0.00474  -0.0008   0.6582   0.6072
  -1.250  -0.1351   0.01246   0.00468  -0.0010   0.6546   0.6122
  -1.000  -0.1065   0.01246   0.00465  -0.0012   0.6511   0.6163
  -0.750  -0.0780   0.01249   0.00465  -0.0012   0.6478   0.6205
  -0.500  -0.0493   0.01249   0.00467  -0.0014   0.6434   0.6256
  -0.250  -0.0206   0.01251   0.00467  -0.0016   0.6388   0.6315
   0.000   0.0079   0.01250   0.00468  -0.0017   0.6345   0.6358
   0.250   0.0363   0.01250   0.00468  -0.0018   0.6305   0.6399
   0.500   0.0650   0.01251   0.00468  -0.0020   0.6266   0.6439
   0.750   0.0938   0.01250   0.00470  -0.0022   0.6215   0.6477
   1.000   0.1226   0.01250   0.00468  -0.0025   0.6165   0.6514
   1.250   0.1510   0.01246   0.00469  -0.0025   0.6120   0.6545
   1.500   0.1794   0.01247   0.00472  -0.0026   0.6074   0.6581
   1.750   0.2080   0.01246   0.00479  -0.0028   0.6015   0.6620
   2.000   0.2365   0.01244   0.00478  -0.0029   0.5954   0.6658
   2.250   0.2651   0.01244   0.00474  -0.0030   0.5897   0.6697
   2.500   0.2933   0.01241   0.00484  -0.0030   0.5820   0.6729
   2.750   0.3214   0.01240   0.00488  -0.0030   0.5754   0.6766
   3.000   0.3496   0.01241   0.00493  -0.0030   0.5688   0.6806
   3.250   0.3780   0.01241   0.00501  -0.0031   0.5597   0.6847
   3.500   0.4061   0.01241   0.00502  -0.0031   0.5501   0.6885
   3.750   0.4338   0.01237   0.00507  -0.0030   0.5363   0.6920
   4.000   0.4616   0.01234   0.00513  -0.0030   0.5199   0.6961
   4.250   0.4892   0.01232   0.00512  -0.0028   0.4988   0.7007
   4.500   0.5163   0.01238   0.00511  -0.0027   0.4765   0.7060
   4.750   0.5427   0.01248   0.00522  -0.0024   0.4494   0.7105
   5.000   0.5686   0.01268   0.00535  -0.0021   0.4122   0.7158
   5.250   0.5928   0.01308   0.00554  -0.0018   0.3587   0.7216
   5.500   0.6157   0.01364   0.00588  -0.0013   0.3109   0.7272
   5.750   0.6389   0.01419   0.00630  -0.0010   0.2656   0.7335
   6.000   0.6611   0.01490   0.00679  -0.0006   0.2173   0.7405
   6.250   0.6838   0.01550   0.00728  -0.0003   0.1805   0.7466
   6.500   0.7067   0.01603   0.00777   0.0001   0.1600   0.7536
   6.750   0.7300   0.01655   0.00828   0.0004   0.1420   0.7614
   7.000   0.7528   0.01702   0.00878   0.0009   0.1232   0.7692
   7.250   0.7752   0.01757   0.00930   0.0013   0.1056   0.7784
   7.500   0.7967   0.01812   0.00985   0.0018   0.0902   0.7887
   7.750   0.8181   0.01869   0.01042   0.0024   0.0786   0.8005
   8.000   0.8393   0.01924   0.01101   0.0030   0.0707   0.8144
   8.250   0.8601   0.01974   0.01161   0.0037   0.0646   0.8301
   8.500   0.8806   0.02024   0.01221   0.0045   0.0585   0.8498
   8.750   0.8995   0.02073   0.01283   0.0056   0.0528   0.8740
   9.000   0.9190   0.02129   0.01350   0.0064   0.0482   0.9151
   9.250   0.9445   0.02199   0.01426   0.0056   0.0439   0.9995
   9.500   0.9626   0.02280   0.01507   0.0061   0.0402   0.9995
   9.750   0.9794   0.02363   0.01593   0.0068   0.0366   0.9995
  10.000   0.9951   0.02445   0.01680   0.0076   0.0332   0.9995
  10.250   1.0104   0.02537   0.01776   0.0082   0.0302   0.9995
  10.500   1.0249   0.02640   0.01883   0.0087   0.0279   0.9995
  10.750   1.0386   0.02754   0.02001   0.0091   0.0263   0.9995
  11.000   1.0516   0.02877   0.02129   0.0094   0.0251   0.9995
  11.250   1.0636   0.03011   0.02269   0.0097   0.0241   0.9995
  11.500   1.0739   0.03165   0.02426   0.0100   0.0230   0.9995
  11.750   1.0841   0.03321   0.02591   0.0102   0.0217   0.9995
  12.000   1.0924   0.03496   0.02774   0.0104   0.0207   0.9995
  12.250   1.0993   0.03688   0.02973   0.0106   0.0199   0.9995
  12.500   1.1070   0.03873   0.03171   0.0107   0.0190   0.9995
  12.750   1.1125   0.04083   0.03391   0.0108   0.0180   0.9995
  13.000   1.1159   0.04316   0.03633   0.0107   0.0173   0.9995
  13.250   1.1218   0.04526   0.03859   0.0107   0.0163   0.9995
  13.500   1.1251   0.04767   0.04113   0.0106   0.0155   0.9995
  13.750   1.1265   0.05031   0.04388   0.0103   0.0148   0.9995
  14.000   1.1282   0.05297   0.04669   0.0100   0.0141   0.9995
  14.250   1.1282   0.05588   0.04975   0.0096   0.0134   0.9995
  14.500   1.1266   0.05903   0.05303   0.0090   0.0129   0.9995
  14.750   1.1243   0.06240   0.05653   0.0081   0.0125   0.9995
  15.000   1.1209   0.06607   0.06032   0.0070   0.0121   0.9995
  15.250   1.1159   0.07011   0.06451   0.0057   0.0118   0.9995
  15.500   1.1098   0.07446   0.06901   0.0041   0.0116   0.9995
  15.750   1.1024   0.07914   0.07383   0.0022   0.0114   0.9995
  16.000   1.0937   0.08422   0.07906   0.0001   0.0112   0.9995
  16.250   1.0834   0.08971   0.08469  -0.0024   0.0111   0.9995
  16.500   1.0717   0.09562   0.09074  -0.0052   0.0110   0.9995
  16.750   1.0584   0.10204   0.09731  -0.0083   0.0109   0.9995
  17.000   1.0436   0.10886   0.10429  -0.0118   0.0109   0.9995
  17.250   1.0274   0.11621   0.11178  -0.0156   0.0109   0.9995
  17.500   1.0101   0.12398   0.11970  -0.0198   0.0109   0.9995
  17.750   0.9919   0.13219   0.12805  -0.0242   0.0109   0.9995
  18.000   0.9731   0.14087   0.13687  -0.0291   0.0110   0.9995
  18.250   0.9530   0.15019   0.14632  -0.0344   0.0110   0.9995
  18.500   0.9294   0.16084   0.15711  -0.0406   0.0111   0.9995
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