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AH 82-150 A (ah82150a-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: AH 82-150 A (ah82150a-il)
Reynolds number: 500,000
Max Cl/Cd: 107.42 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ah82150a-il-500000-n5.txt
Download as CSV file: xf-ah82150a-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 82-150 A                                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.5723   0.04752   0.04439  -0.1210   0.8878   0.0085
 -13.250  -0.6025   0.04118   0.03768  -0.1239   0.8689   0.0082
 -12.750  -0.6276   0.03475   0.03072  -0.1231   0.8452   0.0085
 -12.500  -0.6339   0.03238   0.02812  -0.1217   0.8364   0.0085
 -12.250  -0.6377   0.03029   0.02578  -0.1200   0.8284   0.0087
 -12.000  -0.6368   0.02861   0.02388  -0.1184   0.8215   0.0088
 -11.750  -0.6352   0.02696   0.02200  -0.1164   0.8151   0.0090
 -11.500  -0.6289   0.02571   0.02054  -0.1146   0.8100   0.0091
 -11.250  -0.6224   0.02447   0.01912  -0.1127   0.8048   0.0093
 -11.000  -0.6172   0.02323   0.01770  -0.1103   0.8000   0.0095
 -10.750  -0.6099   0.02223   0.01655  -0.1080   0.7957   0.0097
 -10.500  -0.5960   0.02140   0.01561  -0.1066   0.7914   0.0100
 -10.250  -0.5790   0.02076   0.01488  -0.1055   0.7874   0.0103
 -10.000  -0.5607   0.02017   0.01418  -0.1046   0.7841   0.0108
  -9.750  -0.5419   0.01951   0.01341  -0.1037   0.7810   0.0111
  -9.500  -0.5223   0.01886   0.01264  -0.1029   0.7777   0.0116
  -9.250  -0.5018   0.01827   0.01195  -0.1022   0.7743   0.0122
  -9.000  -0.4805   0.01775   0.01130  -0.1016   0.7711   0.0128
  -8.500  -0.4385   0.01658   0.00998  -0.1003   0.7655   0.0142
  -8.250  -0.4155   0.01618   0.00954  -0.0999   0.7626   0.0150
  -8.000  -0.3925   0.01577   0.00906  -0.0994   0.7597   0.0158
  -7.750  -0.3694   0.01535   0.00854  -0.0990   0.7570   0.0167
  -7.500  -0.3456   0.01499   0.00808  -0.0986   0.7545   0.0175
  -7.250  -0.3231   0.01447   0.00752  -0.0981   0.7518   0.0186
  -7.000  -0.2986   0.01418   0.00722  -0.0979   0.7491   0.0200
  -6.750  -0.2738   0.01390   0.00691  -0.0977   0.7465   0.0215
  -6.500  -0.2488   0.01364   0.00659  -0.0975   0.7439   0.0230
  -6.250  -0.2238   0.01337   0.00623  -0.0973   0.7414   0.0239
  -5.750  -0.1746   0.01269   0.00552  -0.0968   0.7367   0.0280
  -5.500  -0.1491   0.01243   0.00522  -0.0967   0.7342   0.0298
  -5.250  -0.1233   0.01220   0.00494  -0.0966   0.7315   0.0314
  -5.000  -0.0978   0.01192   0.00462  -0.0965   0.7290   0.0336
  -4.750  -0.0720   0.01165   0.00433  -0.0965   0.7268   0.0365
  -4.250  -0.0189   0.01128   0.00388  -0.0965   0.7223   0.0420
  -4.000   0.0074   0.01104   0.00366  -0.0966   0.7197   0.0472
  -3.750   0.0342   0.01086   0.00347  -0.0967   0.7171   0.0530
  -3.500   0.0610   0.01066   0.00329  -0.0968   0.7148   0.0624
  -3.250   0.0879   0.01046   0.00312  -0.0969   0.7126   0.0797
  -3.000   0.1143   0.01017   0.00295  -0.0971   0.7105   0.1185
  -2.750   0.1404   0.00979   0.00280  -0.0973   0.7080   0.1819
  -2.500   0.1667   0.00939   0.00265  -0.0976   0.7055   0.2563
  -2.250   0.1925   0.00878   0.00245  -0.0980   0.7029   0.3783
  -2.000   0.2167   0.00779   0.00235  -0.0983   0.7004   0.6258
  -1.750   0.2449   0.00785   0.00245  -0.0984   0.6981   0.6710
  -1.250   0.3011   0.00820   0.00281  -0.0984   0.6934   0.7219
  -1.000   0.3293   0.00831   0.00291  -0.0985   0.6906   0.7312
  -0.750   0.3574   0.00841   0.00299  -0.0986   0.6877   0.7377
  -0.500   0.3860   0.00848   0.00301  -0.0989   0.6850   0.7435
  -0.250   0.4144   0.00852   0.00301  -0.0991   0.6824   0.7456
   0.000   0.4428   0.00852   0.00301  -0.0994   0.6790   0.7468
   0.250   0.4711   0.00852   0.00300  -0.0997   0.6751   0.7479
   0.500   0.4996   0.00853   0.00297  -0.1001   0.6711   0.7489
   0.750   0.5281   0.00855   0.00294  -0.1004   0.6676   0.7499
   1.000   0.5564   0.00855   0.00296  -0.1007   0.6636   0.7511
   1.250   0.5847   0.00857   0.00297  -0.1010   0.6595   0.7524
   1.500   0.6131   0.00860   0.00298  -0.1014   0.6559   0.7536
   1.750   0.6416   0.00863   0.00298  -0.1017   0.6526   0.7547
   2.000   0.6698   0.00865   0.00302  -0.1021   0.6483   0.7557
   2.250   0.6980   0.00868   0.00306  -0.1024   0.6439   0.7567
   2.500   0.7260   0.00872   0.00308  -0.1026   0.6399   0.7575
   2.750   0.7537   0.00875   0.00314  -0.1028   0.6352   0.7585
   3.000   0.7812   0.00878   0.00321  -0.1030   0.6302   0.7595
   3.250   0.8086   0.00883   0.00328  -0.1031   0.6254   0.7605
   3.500   0.8361   0.00888   0.00337  -0.1033   0.6200   0.7615
   3.750   0.8632   0.00894   0.00345  -0.1034   0.6143   0.7625
   4.000   0.8902   0.00900   0.00354  -0.1035   0.6086   0.7635
   4.250   0.9171   0.00907   0.00365  -0.1035   0.6017   0.7646
   4.500   0.9435   0.00915   0.00375  -0.1035   0.5945   0.7657
   4.750   0.9697   0.00924   0.00387  -0.1034   0.5857   0.7669
   5.000   0.9955   0.00934   0.00401  -0.1032   0.5762   0.7681
   5.250   1.0194   0.00949   0.00414  -0.1027   0.5602   0.7694
   5.500   1.0396   0.00975   0.00430  -0.1014   0.5327   0.7709
   5.750   1.0536   0.01023   0.00458  -0.0991   0.4888   0.7723
   6.000   1.0605   0.01096   0.00504  -0.0954   0.4342   0.7737
   6.250   1.0637   0.01181   0.00562  -0.0913   0.3809   0.7751
   6.500   1.0634   0.01260   0.00618  -0.0864   0.3337   0.7767
   6.750   1.0628   0.01352   0.00686  -0.0818   0.2866   0.7785
   7.000   1.0602   0.01462   0.00771  -0.0771   0.2365   0.7805
   7.250   1.0578   0.01585   0.00869  -0.0729   0.1868   0.7825
   7.500   1.0539   0.01729   0.00985  -0.0687   0.1354   0.7845
   7.750   1.0504   0.01886   0.01116  -0.0649   0.0858   0.7864
   8.000   1.0478   0.02048   0.01255  -0.0615   0.0408   0.7882
   8.250   1.0511   0.02187   0.01382  -0.0589   0.0179   0.7901
   8.500   1.0636   0.02275   0.01475  -0.0574   0.0144   0.7920
   8.750   1.0751   0.02372   0.01575  -0.0559   0.0122   0.7940
   9.000   1.0889   0.02456   0.01667  -0.0547   0.0114   0.7959
   9.250   1.1017   0.02550   0.01767  -0.0535   0.0106   0.7980
   9.500   1.1140   0.02650   0.01872  -0.0522   0.0100   0.7999
   9.750   1.1250   0.02760   0.01988  -0.0509   0.0094   0.8018
  10.000   1.1342   0.02884   0.02122  -0.0495   0.0089   0.8037
  10.250   1.1426   0.03018   0.02264  -0.0480   0.0084   0.8059
  10.500   1.1537   0.03134   0.02388  -0.0469   0.0082   0.8082
  10.750   1.1636   0.03263   0.02525  -0.0458   0.0078   0.8106
  11.000   1.1731   0.03398   0.02667  -0.0447   0.0075   0.8131
  11.500   1.1913   0.03684   0.02967  -0.0427   0.0068   0.8183
  11.750   1.1987   0.03846   0.03138  -0.0416   0.0066   0.8213
  12.000   1.2054   0.04020   0.03322  -0.0407   0.0064   0.8247
  12.250   1.2108   0.04213   0.03523  -0.0397   0.0062   0.8281
  12.500   1.2135   0.04436   0.03755  -0.0387   0.0060   0.8314
  12.750   1.2144   0.04682   0.04012  -0.0377   0.0058   0.8349
  13.000   1.2204   0.04885   0.04225  -0.0370   0.0058   0.8390
  13.250   1.2272   0.05085   0.04436  -0.0365   0.0056   0.8434
  13.500   1.2318   0.05311   0.04673  -0.0359   0.0055   0.8481
  13.750   1.2368   0.05537   0.04911  -0.0355   0.0054   0.8537
  14.250   1.2454   0.06016   0.05415  -0.0347   0.0052   0.8678
  14.500   1.2488   0.06267   0.05680  -0.0343   0.0051   0.8780
  14.750   1.2525   0.06511   0.05941  -0.0339   0.0049   0.8953
  15.000   1.2550   0.06759   0.06209  -0.0337   0.0049   0.9906
  15.250   1.2589   0.07032   0.06492  -0.0338   0.0048   1.0000
  15.500   1.2621   0.07326   0.06796  -0.0340   0.0046   1.0000
  15.750   1.2655   0.07622   0.07102  -0.0344   0.0045   1.0000
  16.000   1.2689   0.07924   0.07414  -0.0350   0.0044   1.0000
  16.250   1.2711   0.08248   0.07747  -0.0357   0.0043   1.0000
  16.500   1.2724   0.08590   0.08100  -0.0364   0.0043   1.0000
  16.750   1.2737   0.08941   0.08459  -0.0375   0.0042   1.0000
  17.000   1.2739   0.09313   0.08841  -0.0385   0.0041   1.0000
  17.250   1.2730   0.09703   0.09242  -0.0398   0.0040   1.0000
  17.500   1.2708   0.10124   0.09674  -0.0412   0.0039   1.0000
  17.750   1.2664   0.10582   0.10146  -0.0427   0.0039   1.0000
  18.000   1.2592   0.11096   0.10679  -0.0445   0.0038   1.0000
  18.250   1.2552   0.11576   0.11173  -0.0466   0.0038   1.0000
  18.500   1.2503   0.12078   0.11690  -0.0489   0.0037   1.0000
  18.750   1.2444   0.12606   0.12234  -0.0515   0.0037   1.0000
  19.000   1.2378   0.13160   0.12803  -0.0544   0.0037   1.0000
  19.250   1.2302   0.13744   0.13403  -0.0576   0.0037   1.0000
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