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AH 94-156 (ah94156-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: AH 94-156 (ah94156-il)
Reynolds number: 500,000
Max Cl/Cd: 103.2 at α=7.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ah94156-il-500000.txt
Download as CSV file: xf-ah94156-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.1628   0.08889   0.08598  -0.0796   0.8001   0.0245
 -11.000  -0.1600   0.08532   0.08241  -0.0810   0.7983   0.0250
 -10.750  -0.1592   0.08136   0.07845  -0.0825   0.7965   0.0256
 -10.500  -0.1620   0.07667   0.07375  -0.0845   0.7949   0.0258
 -10.250  -0.1677   0.07140   0.06849  -0.0869   0.7934   0.0269
 -10.000  -0.1776   0.06528   0.06237  -0.0899   0.7920   0.0274
  -9.750  -0.1941   0.05771   0.05482  -0.0945   0.7906   0.0274
  -9.500  -0.2307   0.04796   0.04503  -0.1019   0.7889   0.0266
  -9.250  -0.2608   0.04265   0.03962  -0.1031   0.7865   0.0262
  -9.000  -0.2854   0.03890   0.03576  -0.1017   0.7837   0.0262
  -8.750  -0.3070   0.03606   0.03279  -0.0985   0.7809   0.0268
  -8.500  -0.4150   0.03313   0.02835  -0.0907   0.7819   0.0182
  -8.250  -0.4113   0.02982   0.02471  -0.0883   0.7797   0.0180
  -8.000  -0.4020   0.02705   0.02158  -0.0861   0.7776   0.0178
  -7.750  -0.3877   0.02486   0.01903  -0.0844   0.7756   0.0179
  -7.500  -0.3687   0.02336   0.01728  -0.0833   0.7736   0.0182
  -7.250  -0.3495   0.02146   0.01508  -0.0822   0.7715   0.0188
  -7.000  -0.3267   0.01992   0.01344  -0.0818   0.7695   0.0193
  -6.750  -0.3025   0.01894   0.01237  -0.0814   0.7674   0.0198
  -6.500  -0.2778   0.01812   0.01144  -0.0811   0.7653   0.0204
  -6.250  -0.2527   0.01731   0.01053  -0.0808   0.7635   0.0209
  -6.000  -0.2275   0.01668   0.00981  -0.0805   0.7619   0.0219
  -5.750  -0.2024   0.01610   0.00915  -0.0801   0.7602   0.0227
  -5.500  -0.1780   0.01548   0.00847  -0.0797   0.7581   0.0237
  -5.250  -0.1554   0.01475   0.00776  -0.0791   0.7558   0.0253
  -5.000  -0.1307   0.01435   0.00735  -0.0788   0.7536   0.0269
  -4.750  -0.1060   0.01395   0.00691  -0.0784   0.7516   0.0285
  -4.500  -0.0824   0.01343   0.00633  -0.0778   0.7496   0.0305
  -4.250  -0.0577   0.01304   0.00592  -0.0774   0.7478   0.0338
  -4.000  -0.0320   0.01278   0.00561  -0.0772   0.7461   0.0380
  -3.750  -0.0074   0.01246   0.00532  -0.0768   0.7441   0.0452
  -3.500   0.0170   0.01209   0.00501  -0.0764   0.7417   0.0602
  -3.250   0.0399   0.01159   0.00478  -0.0759   0.7394   0.1154
  -3.000   0.0615   0.01096   0.00458  -0.0753   0.7372   0.2227
  -2.750   0.0815   0.01022   0.00438  -0.0744   0.7351   0.3686
  -2.500   0.0991   0.00932   0.00415  -0.0731   0.7330   0.5523
  -2.250   0.1151   0.00875   0.00435  -0.0705   0.7311   0.7412
  -2.000   0.1402   0.00922   0.00491  -0.0693   0.7289   0.8018
  -1.750   0.1669   0.00952   0.00517  -0.0689   0.7263   0.8235
  -1.500   0.1931   0.00985   0.00547  -0.0682   0.7237   0.8355
  -1.250   0.2187   0.01019   0.00578  -0.0673   0.7211   0.8474
  -1.000   0.2450   0.01046   0.00598  -0.0666   0.7188   0.8584
  -0.750   0.2707   0.01066   0.00614  -0.0655   0.7166   0.8636
  -0.500   0.2968   0.01087   0.00629  -0.0650   0.7141   0.8717
  -0.250   0.3196   0.01099   0.00644  -0.0635   0.7109   0.8777
   0.000   0.3442   0.01112   0.00655  -0.0626   0.7079   0.8855
   0.250   0.3691   0.01112   0.00652  -0.0617   0.7052   0.8908
   0.500   0.3955   0.01114   0.00649  -0.0612   0.7027   0.8962
   0.750   0.4223   0.01118   0.00645  -0.0611   0.7004   0.9021
   1.000   0.4461   0.01111   0.00642  -0.0601   0.6971   0.9056
   1.250   0.4711   0.01108   0.00639  -0.0596   0.6937   0.9097
   1.500   0.4970   0.01105   0.00633  -0.0594   0.6905   0.9141
   1.750   0.5235   0.01092   0.00617  -0.0593   0.6878   0.9170
   2.000   0.5521   0.01086   0.00606  -0.0595   0.6852   0.9191
   2.250   0.5759   0.01080   0.00605  -0.0589   0.6813   0.9217
   2.500   0.6015   0.01074   0.00599  -0.0587   0.6776   0.9242
   2.750   0.6283   0.01065   0.00589  -0.0587   0.6741   0.9265
   3.000   0.6566   0.01062   0.00580  -0.0591   0.6709   0.9284
   3.250   0.6800   0.01051   0.00575  -0.0586   0.6664   0.9301
   3.500   0.7055   0.01040   0.00566  -0.0583   0.6619   0.9316
   3.750   0.7331   0.01030   0.00554  -0.0585   0.6580   0.9329
   4.000   0.7593   0.01025   0.00550  -0.0584   0.6536   0.9343
   4.250   0.7837   0.01018   0.00548  -0.0580   0.6478   0.9358
   4.500   0.8108   0.01010   0.00538  -0.0582   0.6428   0.9368
   4.750   0.8355   0.01007   0.00538  -0.0579   0.6370   0.9383
   5.000   0.8607   0.01002   0.00536  -0.0578   0.6305   0.9393
   5.250   0.8867   0.00999   0.00533  -0.0577   0.6239   0.9402
   5.500   0.9109   0.00998   0.00535  -0.0574   0.6159   0.9413
   5.750   0.9364   0.00999   0.00537  -0.0573   0.6085   0.9420
   6.000   0.9607   0.00999   0.00540  -0.0570   0.5994   0.9426
   6.250   0.9832   0.00999   0.00543  -0.0564   0.5894   0.9435
   6.500   1.0050   0.01001   0.00545  -0.0555   0.5790   0.9447
   6.750   1.0265   0.01008   0.00552  -0.0547   0.5677   0.9455
   7.000   1.0464   0.01018   0.00564  -0.0536   0.5548   0.9463
   7.250   1.0650   0.01032   0.00578  -0.0523   0.5412   0.9473
   7.500   1.0793   0.01050   0.00593  -0.0501   0.5257   0.9488
   7.750   1.0885   0.01074   0.00613  -0.0470   0.5081   0.9504
   8.000   1.0978   0.01111   0.00646  -0.0442   0.4888   0.9518
   8.250   1.1063   0.01157   0.00687  -0.0414   0.4698   0.9532
   8.500   1.1137   0.01214   0.00739  -0.0386   0.4510   0.9547
   8.750   1.1208   0.01279   0.00798  -0.0359   0.4326   0.9567
   9.000   1.1303   0.01346   0.00863  -0.0338   0.4147   0.9583
   9.250   1.1382   0.01427   0.00940  -0.0317   0.3947   0.9602
   9.500   1.1448   0.01524   0.01029  -0.0295   0.3737   0.9624
   9.750   1.1542   0.01618   0.01119  -0.0279   0.3531   0.9645
  10.000   1.1626   0.01733   0.01227  -0.0265   0.3298   0.9670
  10.250   1.1734   0.01855   0.01342  -0.0257   0.3047   0.9696
  10.500   1.1836   0.01997   0.01475  -0.0252   0.2771   0.9736
  10.750   1.1943   0.02149   0.01615  -0.0249   0.2491   0.9788
  11.000   1.1984   0.02303   0.01757  -0.0234   0.2225   1.0000
  11.250   1.2013   0.02461   0.01902  -0.0217   0.1966   1.0000
  11.500   1.2041   0.02626   0.02055  -0.0200   0.1700   1.0000
  11.750   1.2043   0.02816   0.02227  -0.0183   0.1409   1.0000
  12.000   1.2072   0.02994   0.02393  -0.0169   0.1167   1.0000
  12.250   1.2079   0.03195   0.02581  -0.0154   0.0922   1.0000
  12.500   1.2096   0.03395   0.02770  -0.0141   0.0727   1.0000
  12.750   1.2121   0.03596   0.02963  -0.0129   0.0568   1.0000
  13.000   1.2137   0.03812   0.03171  -0.0119   0.0437   1.0000
  13.250   1.2164   0.04024   0.03379  -0.0109   0.0340   1.0000
  13.500   1.2176   0.04258   0.03612  -0.0100   0.0275   1.0000
  13.750   1.2244   0.04447   0.03806  -0.0096   0.0242   1.0000
  14.000   1.2249   0.04701   0.04062  -0.0088   0.0212   1.0000
  14.250   1.2309   0.04909   0.04280  -0.0085   0.0195   1.0000
  14.500   1.2336   0.05155   0.04530  -0.0081   0.0179   1.0000
  14.750   1.2305   0.05469   0.04852  -0.0076   0.0166   1.0000
  15.000   1.2354   0.05704   0.05097  -0.0075   0.0158   1.0000
  15.250   1.2386   0.05964   0.05364  -0.0075   0.0149   1.0000
  15.500   1.2405   0.06243   0.05652  -0.0076   0.0144   1.0000
  15.750   1.2422   0.06531   0.05945  -0.0078   0.0137   1.0000
  16.000   1.2340   0.06943   0.06366  -0.0079   0.0131   1.0000
  16.250   1.2333   0.07273   0.06705  -0.0083   0.0126   1.0000
  16.500   1.2363   0.07566   0.07009  -0.0088   0.0121   1.0000
  16.750   1.2372   0.07887   0.07341  -0.0094   0.0120   1.0000
  17.000   1.2376   0.08224   0.07686  -0.0101   0.0115   1.0000
  17.250   1.2374   0.08569   0.08040  -0.0108   0.0112   1.0000
  17.500   1.2373   0.08920   0.08398  -0.0117   0.0108   1.0000
  17.750   1.2364   0.09284   0.08770  -0.0128   0.0105   1.0000
  18.000   1.2353   0.09650   0.09144  -0.0137   0.0104   1.0000
  18.250   1.2336   0.10026   0.09526  -0.0148   0.0102   1.0000
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