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AH 94-156 (ah94156-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: AH 94-156 (ah94156-il)
Reynolds number: 50,000
Max Cl/Cd: 16.74 at α=13°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ah94156-il-50000-n5.txt
Download as CSV file: xf-ah94156-il-50000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 94-156                                       
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.2989   0.14313   0.13662  -0.0580   0.9839   0.1111
 -12.250  -0.3043   0.14038   0.13391  -0.0630   0.9778   0.1125
 -12.000  -0.3034   0.13673   0.13028  -0.0677   0.9730   0.1128
 -11.750  -0.2690   0.13080   0.12427  -0.0669   0.9706   0.1161
 -11.500  -0.2697   0.12216   0.11554  -0.0733   0.9653   0.0683
 -11.000  -0.2669   0.11007   0.10344  -0.0834   0.9578   0.0570
 -10.750  -0.2558   0.10645   0.09980  -0.0850   0.9536   0.0560
 -10.500  -0.2491   0.10235   0.09570  -0.0875   0.9491   0.0548
 -10.250  -0.2453   0.09735   0.09070  -0.0914   0.9452   0.0539
 -10.000  -0.2430   0.09222   0.08557  -0.0956   0.9415   0.0528
  -9.750  -0.2498   0.08731   0.08069  -0.0989   0.9352   0.0518
  -9.500  -0.2599   0.08092   0.07427  -0.1045   0.9300   0.0506
  -9.250  -0.2805   0.07623   0.06952  -0.1067   0.9232   0.0496
  -9.000  -0.3067   0.07246   0.06562  -0.1066   0.9156   0.0487
  -8.750  -0.3351   0.06990   0.06293  -0.1035   0.9081   0.0481
  -8.500  -0.3603   0.06713   0.05991  -0.1003   0.9010   0.0473
  -8.250  -0.3782   0.06447   0.05692  -0.0971   0.8951   0.0469
  -8.000  -0.3929   0.06263   0.05485  -0.0928   0.8886   0.0467
  -7.750  -0.3915   0.06008   0.05210  -0.0911   0.8846   0.0472
  -7.500  -0.3889   0.05816   0.05004  -0.0889   0.8805   0.0480
  -7.250  -0.3945   0.05691   0.04867  -0.0850   0.8746   0.0489
  -7.000  -0.3893   0.05492   0.04642  -0.0830   0.8706   0.0501
  -6.750  -0.3779   0.05257   0.04369  -0.0818   0.8676   0.0515
  -6.500  -0.3864   0.05145   0.04235  -0.0766   0.8616   0.0520
  -6.250  -0.3786   0.04950   0.04002  -0.0742   0.8573   0.0527
  -6.000  -0.3609   0.04726   0.03729  -0.0731   0.8544   0.0537
  -5.750  -0.3368   0.04512   0.03463  -0.0728   0.8521   0.0554
  -5.500  -0.3396   0.04442   0.03365  -0.0679   0.8461   0.0567
  -5.250  -0.3215   0.04304   0.03210  -0.0667   0.8425   0.0595
  -5.000  -0.2959   0.04183   0.03073  -0.0667   0.8398   0.0631
  -4.750  -0.2632   0.04053   0.02913  -0.0673   0.8377   0.0668
  -4.500  -0.2536   0.04005   0.02844  -0.0642   0.8329   0.0704
  -4.250  -0.2358   0.03937   0.02781  -0.0628   0.8289   0.0763
  -4.000  -0.2078   0.03873   0.02693  -0.0626   0.8259   0.0839
  -3.750  -0.1794   0.03802   0.02619  -0.0629   0.8233   0.0961
  -3.500  -0.1663   0.03759   0.02576  -0.0607   0.8192   0.1080
  -3.250  -0.1576   0.03725   0.02545  -0.0579   0.8142   0.1259
  -3.000  -0.1398   0.03637   0.02493  -0.0567   0.8106   0.1743
  -2.750  -0.1291   0.03469   0.02448  -0.0545   0.8077   0.3601
  -2.500  -0.0987   0.03560   0.02711  -0.0490   0.8056   0.7961
  -2.000   0.1439   0.03777   0.02791  -0.0787   0.8077   0.9636
  -1.750   0.2050   0.03771   0.02750  -0.0861   0.8053   0.9792
  -1.500   0.2395   0.03794   0.02753  -0.0892   0.7998   0.9923
  -1.250   0.2801   0.03799   0.02736  -0.0930   0.7961   1.0000
  -1.000   0.3026   0.03812   0.02732  -0.0928   0.7926   1.0000
  -0.750   0.2858   0.03884   0.02800  -0.0863   0.7840   1.0000
  -0.500   0.3005   0.03911   0.02814  -0.0847   0.7791   1.0000
  -0.250   0.3296   0.03921   0.02807  -0.0855   0.7760   1.0000
   0.000   0.3064   0.04000   0.02884  -0.0779   0.7659   1.0000
   0.250   0.3302   0.04017   0.02889  -0.0777   0.7620   1.0000
   0.500   0.3193   0.04082   0.02949  -0.0721   0.7532   1.0000
   0.750   0.3369   0.04108   0.02965  -0.0709   0.7482   1.0000
   1.000   0.3416   0.04153   0.03003  -0.0678   0.7414   1.0000
   1.250   0.3484   0.04193   0.03037  -0.0649   0.7344   1.0000
   1.500   0.3757   0.04207   0.03042  -0.0650   0.7307   1.0000
   1.750   0.3627   0.04277   0.03110  -0.0593   0.7207   1.0000
   2.000   0.3868   0.04294   0.03120  -0.0589   0.7164   1.0000
   2.250   0.3792   0.04358   0.03181  -0.0541   0.7070   1.0000
   2.500   0.4010   0.04376   0.03194  -0.0533   0.7021   1.0000
   2.750   0.3973   0.04435   0.03251  -0.0490   0.6930   1.0000
   3.000   0.4166   0.04456   0.03268  -0.0479   0.6876   1.0000
   3.250   0.4159   0.04512   0.03323  -0.0441   0.6788   1.0000
   3.500   0.4337   0.04535   0.03343  -0.0427   0.6730   1.0000
   3.750   0.4351   0.04590   0.03397  -0.0393   0.6643   1.0000
   4.000   0.4530   0.04612   0.03418  -0.0380   0.6583   1.0000
   4.250   0.4554   0.04672   0.03477  -0.0348   0.6494   1.0000
   4.500   0.4750   0.04695   0.03500  -0.0338   0.6435   1.0000
   4.750   0.4792   0.04765   0.03571  -0.0311   0.6343   1.0000
   5.000   0.5019   0.04785   0.03592  -0.0306   0.6287   1.0000
   5.250   0.5076   0.04868   0.03676  -0.0284   0.6191   1.0000
   5.500   0.5333   0.04882   0.03694  -0.0282   0.6137   1.0000
   5.750   0.5396   0.04977   0.03793  -0.0263   0.6036   1.0000
   6.000   0.5676   0.04984   0.03804  -0.0263   0.5986   1.0000
   6.250   0.5738   0.05093   0.03917  -0.0247   0.5880   1.0000
   6.500   0.6041   0.05089   0.03921  -0.0249   0.5834   1.0000
   6.750   0.6098   0.05212   0.04049  -0.0233   0.5722   1.0000
   7.000   0.6420   0.05193   0.04039  -0.0236   0.5682   1.0000
   7.250   0.6473   0.05328   0.04180  -0.0222   0.5564   1.0000
   7.750   0.6861   0.05439   0.04312  -0.0212   0.5406   1.0000
   8.000   0.6956   0.05565   0.04447  -0.0202   0.5299   1.0000
   8.250   0.7261   0.05540   0.04437  -0.0203   0.5248   1.0000
   8.500   0.7333   0.05690   0.04596  -0.0193   0.5132   1.0000
   8.750   0.7671   0.05628   0.04549  -0.0193   0.5089   1.0000
   9.000   0.7730   0.05792   0.04724  -0.0183   0.4966   1.0000
   9.250   0.7840   0.05920   0.04864  -0.0175   0.4859   1.0000
   9.500   0.8144   0.05869   0.04832  -0.0173   0.4803   1.0000
   9.750   0.8216   0.06034   0.05010  -0.0165   0.4683   1.0000
  10.000   0.8576   0.05911   0.04907  -0.0162   0.4641   1.0000
  10.250   0.8631   0.06093   0.05104  -0.0153   0.4513   1.0000
  10.500   0.8723   0.06243   0.05268  -0.0146   0.4396   1.0000
  10.750   0.9086   0.06090   0.05137  -0.0141   0.4345   1.0000
  11.250   0.9259   0.06392   0.05471  -0.0125   0.4098   1.0000
  11.500   0.9686   0.06139   0.05246  -0.0117   0.4040   1.0000
  12.000   0.9899   0.06352   0.05493  -0.0099   0.3769   1.0000
  12.250   1.0065   0.06374   0.05532  -0.0088   0.3629   1.0000
  12.500   1.0252   0.06356   0.05534  -0.0077   0.3477   1.0000
  12.750   1.0444   0.06323   0.05516  -0.0065   0.3309   1.0000
  13.000   1.0599   0.06332   0.05533  -0.0054   0.3118   1.0000
  13.250   1.0588   0.06570   0.05782  -0.0046   0.2918   1.0000
  13.500   1.0688   0.06649   0.05863  -0.0036   0.2694   1.0000
  13.750   1.0667   0.06919   0.06138  -0.0031   0.2473   1.0000
  14.000   1.0688   0.07125   0.06339  -0.0025   0.2234   1.0000
  14.250   1.0649   0.07441   0.06654  -0.0023   0.1999   1.0000
  14.500   1.0607   0.07773   0.06977  -0.0023   0.1772   1.0000
  14.750   1.0550   0.08139   0.07333  -0.0025   0.1562   1.0000
  15.000   1.0488   0.08530   0.07711  -0.0030   0.1380   1.0000
  15.250   1.0429   0.08938   0.08113  -0.0036   0.1218   1.0000
  15.500   1.0376   0.09347   0.08514  -0.0044   0.1083   1.0000
  15.750   1.0337   0.09742   0.08903  -0.0052   0.0975   1.0000
  16.000   1.0309   0.10124   0.09277  -0.0060   0.0882   1.0000
  16.250   1.0294   0.10513   0.09675  -0.0070   0.0795   1.0000
  16.500   1.0300   0.10859   0.10021  -0.0078   0.0731   1.0000
  16.750   1.0309   0.11217   0.10392  -0.0088   0.0672   1.0000
  17.000   1.0328   0.11550   0.10726  -0.0097   0.0623   1.0000
  17.250   1.0341   0.11928   0.11128  -0.0108   0.0583   1.0000
  17.500   1.0370   0.12248   0.11450  -0.0119   0.0546   1.0000
  17.750   1.0385   0.12621   0.11836  -0.0132   0.0517   1.0000
  18.000   1.0353   0.13118   0.12363  -0.0153   0.0497   1.0000
  18.250   1.0310   0.13642   0.12911  -0.0178   0.0481   1.0000
  18.500   1.0259   0.14184   0.13471  -0.0205   0.0464   1.0000
  18.750   1.0221   0.14703   0.14002  -0.0233   0.0451   1.0000
  19.000   1.0262   0.15017   0.14313  -0.0249   0.0432   1.0000
  19.250   1.0085   0.15923   0.15244  -0.0302   0.0430   1.0000
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