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AH 93-W-257 (ah93w257-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: AH 93-W-257 (ah93w257-il)
Reynolds number: 200,000
Max Cl/Cd: 58.29 at α=9.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ah93w257-il-200000-n5.txt
Download as CSV file: xf-ah93w257-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 93-W-257                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.9749   0.09562   0.08945  -0.0295   1.0000   0.1231
 -17.250  -0.9722   0.09282   0.08669  -0.0305   1.0000   0.1269
 -17.000  -0.9715   0.08972   0.08359  -0.0316   1.0000   0.1316
 -16.750  -0.9698   0.08680   0.08067  -0.0326   1.0000   0.1364
 -16.500  -0.9699   0.08370   0.07760  -0.0336   1.0000   0.1418
 -16.250  -0.9691   0.08068   0.07457  -0.0345   1.0000   0.1475
 -16.000  -0.9695   0.07761   0.07154  -0.0355   1.0000   0.1536
 -15.750  -0.9693   0.07458   0.06850  -0.0364   1.0000   0.1602
 -15.500  -0.9699   0.07156   0.06553  -0.0373   1.0000   0.1673
 -15.250  -0.9701   0.06855   0.06253  -0.0382   1.0000   0.1746
 -15.000  -0.9700   0.06565   0.05966  -0.0390   1.0000   0.1826
 -14.750  -0.9697   0.06282   0.05685  -0.0398   1.0000   0.1901
 -14.500  -0.9686   0.06007   0.05410  -0.0406   1.0000   0.1982
 -14.250  -0.9604   0.05751   0.05142  -0.0428   0.8691   0.2063
 -14.000  -0.9589   0.05499   0.04866  -0.0432   0.8207   0.2141
 -13.750  -0.9538   0.05301   0.04661  -0.0435   0.7937   0.2213
 -13.500  -0.9517   0.05057   0.04403  -0.0439   0.7745   0.2290
 -13.250  -0.9447   0.04881   0.04223  -0.0441   0.7590   0.2358
 -13.000  -0.9414   0.04660   0.03991  -0.0445   0.7456   0.2432
 -12.750  -0.9334   0.04492   0.03819  -0.0447   0.7341   0.2498
 -12.500  -0.9274   0.04304   0.03623  -0.0450   0.7234   0.2570
 -12.250  -0.9204   0.04122   0.03433  -0.0454   0.7143   0.2636
 -12.000  -0.9107   0.03975   0.03284  -0.0456   0.7051   0.2703
 -11.750  -0.9067   0.03769   0.03063  -0.0460   0.6970   0.2774
 -11.500  -0.8925   0.03672   0.02967  -0.0460   0.6897   0.2834
 -11.250  -0.8848   0.03509   0.02800  -0.0463   0.6827   0.2903
 -11.000  -0.8767   0.03358   0.02639  -0.0465   0.6764   0.2966
 -10.750  -0.8630   0.03264   0.02543  -0.0465   0.6708   0.3027
 -10.500  -0.8569   0.03092   0.02362  -0.0467   0.6659   0.3098
 -10.250  -0.8421   0.03000   0.02271  -0.0468   0.6605   0.3156
 -10.000  -0.8292   0.02894   0.02162  -0.0470   0.6554   0.3223
  -9.750  -0.8243   0.02727   0.01983  -0.0471   0.6507   0.3297
  -9.500  -0.8077   0.02684   0.01942  -0.0466   0.6462   0.3363
  -9.250  -0.8017   0.02523   0.01771  -0.0473   0.6419   0.3447
  -9.000  -0.7793   0.02477   0.01729  -0.0478   0.6372   0.3506
  -8.750  -0.7572   0.02415   0.01664  -0.0487   0.6328   0.3562
  -8.500  -0.7370   0.02285   0.01518  -0.0511   0.6289   0.3629
  -8.250  -0.7104   0.02258   0.01489  -0.0518   0.6252   0.3671
  -8.000  -0.6833   0.02234   0.01461  -0.0525   0.6219   0.3714
  -7.750  -0.6557   0.02161   0.01381  -0.0547   0.6185   0.3771
  -7.500  -0.6262   0.02077   0.01286  -0.0575   0.6147   0.3827
  -7.250  -0.5976   0.02073   0.01286  -0.0578   0.6109   0.3862
  -7.000  -0.5681   0.02048   0.01258  -0.0590   0.6072   0.3906
  -6.750  -0.5369   0.01995   0.01194  -0.0613   0.6037   0.3961
  -6.500  -0.5057   0.01950   0.01136  -0.0633   0.6007   0.4009
  -6.250  -0.4766   0.01953   0.01138  -0.0636   0.5979   0.4042
  -6.000  -0.4462   0.01940   0.01128  -0.0646   0.5952   0.4083
  -5.750  -0.4145   0.01911   0.01094  -0.0663   0.5922   0.4132
  -5.500  -0.3813   0.01867   0.01038  -0.0687   0.5891   0.4183
  -5.250  -0.3520   0.01870   0.01046  -0.0689   0.5859   0.4213
  -5.000  -0.3218   0.01869   0.01045  -0.0695   0.5828   0.4249
  -4.750  -0.2903   0.01856   0.01027  -0.0707   0.5800   0.4293
  -4.500  -0.2574   0.01832   0.00990  -0.0726   0.5774   0.4343
  -4.250  -0.2258   0.01824   0.00975  -0.0738   0.5751   0.4382
  -4.000  -0.1958   0.01829   0.00988  -0.0742   0.5727   0.4413
  -3.750  -0.1647   0.01828   0.00989  -0.0750   0.5701   0.4450
  -3.500  -0.1325   0.01817   0.00976  -0.0764   0.5673   0.4495
  -3.250  -0.0983   0.01792   0.00940  -0.0785   0.5643   0.4547
  -3.000  -0.0685   0.01798   0.00950  -0.0788   0.5616   0.4575
  -2.750  -0.0383   0.01804   0.00958  -0.0793   0.5590   0.4604
  -2.500  -0.0071   0.01807   0.00959  -0.0801   0.5568   0.4640
  -2.250   0.0253   0.01804   0.00949  -0.0813   0.5547   0.4684
  -2.000   0.0595   0.01790   0.00923  -0.0832   0.5526   0.4732
  -1.750   0.0896   0.01796   0.00937  -0.0837   0.5503   0.4758
  -1.500   0.1195   0.01806   0.00955  -0.0841   0.5476   0.4785
  -1.250   0.1502   0.01813   0.00965  -0.0847   0.5448   0.4817
  -1.000   0.1818   0.01815   0.00966  -0.0857   0.5421   0.4855
  -0.750   0.2149   0.01807   0.00954  -0.0871   0.5398   0.4898
  -0.500   0.2475   0.01802   0.00945  -0.0884   0.5376   0.4935
  -0.250   0.2770   0.01816   0.00963  -0.0886   0.5356   0.4959
   0.000   0.3072   0.01830   0.00977  -0.0890   0.5336   0.4986
   0.250   0.3381   0.01842   0.00987  -0.0897   0.5315   0.5018
   0.500   0.3693   0.01846   0.00996  -0.0906   0.5290   0.5052
   0.750   0.4019   0.01844   0.00994  -0.0919   0.5264   0.5093
   1.000   0.4338   0.01846   0.00997  -0.0930   0.5239   0.5129
   1.250   0.4629   0.01863   0.01022  -0.0932   0.5215   0.5151
   1.500   0.4925   0.01878   0.01041  -0.0935   0.5192   0.5175
   1.750   0.5227   0.01888   0.01055  -0.0940   0.5169   0.5202
   2.000   0.5536   0.01894   0.01060  -0.0947   0.5147   0.5233
   2.250   0.5856   0.01898   0.01060  -0.0957   0.5126   0.5269
   2.500   0.6196   0.01900   0.01052  -0.0972   0.5107   0.5313
   2.750   0.6477   0.01919   0.01085  -0.0973   0.5084   0.5334
   3.000   0.6761   0.01939   0.01117  -0.0975   0.5058   0.5355
   3.250   0.7049   0.01957   0.01142  -0.0977   0.5029   0.5377
   3.500   0.7343   0.01970   0.01161  -0.0981   0.5002   0.5402
   3.750   0.7644   0.01982   0.01177  -0.0986   0.4978   0.5432
   4.000   0.7954   0.01991   0.01186  -0.0994   0.4956   0.5469
   4.250   0.8281   0.01993   0.01182  -0.1006   0.4935   0.5510
   4.500   0.8581   0.02004   0.01195  -0.1010   0.4914   0.5531
   4.750   0.8857   0.02027   0.01228  -0.1010   0.4888   0.5549
   5.000   0.9128   0.02053   0.01268  -0.1010   0.4860   0.5570
   5.250   0.9403   0.02076   0.01301  -0.1011   0.4829   0.5594
   5.500   0.9686   0.02093   0.01325  -0.1013   0.4799   0.5622
   5.750   0.9980   0.02105   0.01341  -0.1017   0.4773   0.5653
   6.000   1.0285   0.02112   0.01348  -0.1024   0.4748   0.5685
   6.250   1.0607   0.02116   0.01345  -0.1034   0.4724   0.5720
   6.500   1.0875   0.02139   0.01378  -0.1033   0.4696   0.5739
   6.750   1.1119   0.02170   0.01426  -0.1028   0.4658   0.5758
   7.000   1.1374   0.02194   0.01462  -0.1025   0.4621   0.5778
   7.250   1.1642   0.02209   0.01485  -0.1024   0.4585   0.5800
   7.500   1.1923   0.02215   0.01493  -0.1025   0.4551   0.5824
   7.750   1.2214   0.02220   0.01497  -0.1027   0.4516   0.5853
   8.000   1.2438   0.02252   0.01544  -0.1022   0.4460   0.5884
   8.250   1.2696   0.02267   0.01565  -0.1022   0.4408   0.5918
   8.500   1.2965   0.02269   0.01567  -0.1021   0.4360   0.5941
   8.750   1.3191   0.02289   0.01595  -0.1013   0.4305   0.5958
   9.000   1.3381   0.02322   0.01642  -0.1001   0.4235   0.5976
   9.250   1.3606   0.02334   0.01656  -0.0992   0.4173   0.5997
   9.500   1.3781   0.02372   0.01706  -0.0978   0.4101   0.6021
   9.750   1.3944   0.02407   0.01747  -0.0962   0.4020   0.6047
  10.000   1.4087   0.02446   0.01789  -0.0944   0.3939   0.6073
  10.250   1.4130   0.02505   0.01855  -0.0913   0.3848   0.6098
  10.500   1.4222   0.02583   0.01933  -0.0893   0.3751   0.6124
  10.750   1.4292   0.02690   0.02040  -0.0876   0.3640   0.6149
  11.000   1.4319   0.02838   0.02197  -0.0858   0.3525   0.6166
  11.250   1.4328   0.03018   0.02380  -0.0842   0.3405   0.6184
  11.500   1.4304   0.03242   0.02604  -0.0829   0.3274   0.6202
  11.750   1.4258   0.03506   0.02873  -0.0818   0.3131   0.6220
  12.000   1.4192   0.03800   0.03166  -0.0808   0.2985   0.6238
  12.250   1.4099   0.04124   0.03489  -0.0799   0.2835   0.6256
  12.500   1.3986   0.04475   0.03837  -0.0790   0.2686   0.6274
  12.750   1.3863   0.04840   0.04198  -0.0782   0.2538   0.6292
  13.000   1.3736   0.05215   0.04568  -0.0775   0.2394   0.6309
  13.250   1.3618   0.05599   0.04946  -0.0770   0.2252   0.6328
  13.500   1.3510   0.05991   0.05333  -0.0767   0.2115   0.6348
  13.750   1.3419   0.06376   0.05713  -0.0766   0.1982   0.6366
  14.000   1.3343   0.06744   0.06080  -0.0764   0.1856   0.6380
  14.250   1.3269   0.07119   0.06455  -0.0763   0.1739   0.6394
  14.500   1.3204   0.07489   0.06823  -0.0762   0.1629   0.6408
  14.750   1.3141   0.07865   0.07199  -0.0763   0.1527   0.6423
  15.000   1.3088   0.08237   0.07569  -0.0765   0.1426   0.6438
  15.250   1.3058   0.08588   0.07920  -0.0767   0.1332   0.6454
  15.500   1.3027   0.08941   0.08273  -0.0770   0.1246   0.6471
  15.750   1.2992   0.09308   0.08639  -0.0774   0.1167   0.6488
  16.000   1.2969   0.09662   0.08992  -0.0779   0.1092   0.6506
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