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AH 94-145 (ah94145-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: AH 94-145 (ah94145-il)
Reynolds number: 1,000,000
Max Cl/Cd: 164.41 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ah94145-il-1000000-n5.txt
Download as CSV file: xf-ah94145-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 94-145                                       
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.8065   0.03342   0.02963  -0.1088   0.6863   0.0093
 -13.250  -0.7992   0.03060   0.02661  -0.1106   0.6841   0.0094
 -13.000  -0.7859   0.02850   0.02433  -0.1117   0.6819   0.0095
 -12.750  -0.7691   0.02679   0.02245  -0.1124   0.6797   0.0096
 -12.250  -0.7295   0.02399   0.01935  -0.1135   0.6759   0.0098
 -12.000  -0.7075   0.02281   0.01804  -0.1140   0.6740   0.0099
 -11.750  -0.6845   0.02175   0.01685  -0.1144   0.6720   0.0101
 -11.500  -0.6606   0.02079   0.01575  -0.1147   0.6700   0.0102
 -11.250  -0.6361   0.01991   0.01475  -0.1151   0.6682   0.0103
 -11.000  -0.6108   0.01912   0.01383  -0.1154   0.6664   0.0104
 -10.750  -0.5850   0.01841   0.01300  -0.1158   0.6646   0.0105
 -10.500  -0.5588   0.01776   0.01224  -0.1161   0.6628   0.0107
 -10.250  -0.5325   0.01706   0.01142  -0.1165   0.6610   0.0108
 -10.000  -0.5061   0.01629   0.01056  -0.1169   0.6598   0.0111
  -9.750  -0.4789   0.01570   0.00991  -0.1173   0.6583   0.0113
  -9.500  -0.4512   0.01521   0.00935  -0.1176   0.6566   0.0115
  -9.250  -0.4233   0.01476   0.00884  -0.1180   0.6548   0.0117
  -9.000  -0.3952   0.01434   0.00836  -0.1184   0.6531   0.0120
  -8.750  -0.3670   0.01396   0.00792  -0.1188   0.6515   0.0123
  -8.500  -0.3386   0.01360   0.00749  -0.1191   0.6500   0.0126
  -8.250  -0.3100   0.01325   0.00708  -0.1195   0.6484   0.0129
  -8.000  -0.2814   0.01292   0.00668  -0.1199   0.6468   0.0132
  -7.750  -0.2527   0.01262   0.00630  -0.1203   0.6450   0.0134
  -7.500  -0.2239   0.01218   0.00583  -0.1207   0.6437   0.0139
  -7.250  -0.1948   0.01186   0.00548  -0.1212   0.6424   0.0143
  -7.000  -0.1657   0.01158   0.00517  -0.1216   0.6410   0.0147
  -6.750  -0.1364   0.01132   0.00488  -0.1221   0.6395   0.0152
  -6.500  -0.1071   0.01108   0.00460  -0.1225   0.6379   0.0158
  -6.250  -0.0777   0.01086   0.00434  -0.1229   0.6362   0.0162
  -6.000  -0.0483   0.01061   0.00406  -0.1234   0.6345   0.0169
  -5.750  -0.0189   0.01039   0.00382  -0.1238   0.6330   0.0178
  -5.500   0.0106   0.01022   0.00362  -0.1243   0.6315   0.0188
  -5.250   0.0401   0.01007   0.00343  -0.1247   0.6299   0.0197
  -5.000   0.0698   0.00987   0.00322  -0.1252   0.6285   0.0211
  -4.750   0.0996   0.00970   0.00306  -0.1257   0.6272   0.0226
  -4.500   0.1294   0.00955   0.00289  -0.1262   0.6257   0.0241
  -4.250   0.1593   0.00939   0.00274  -0.1268   0.6243   0.0264
  -4.000   0.1891   0.00925   0.00261  -0.1273   0.6228   0.0289
  -3.750   0.2190   0.00913   0.00249  -0.1278   0.6213   0.0325
  -3.500   0.2489   0.00900   0.00238  -0.1283   0.6198   0.0369
  -3.250   0.2787   0.00890   0.00228  -0.1288   0.6182   0.0416
  -3.000   0.3085   0.00881   0.00219  -0.1293   0.6166   0.0468
  -2.750   0.3383   0.00873   0.00212  -0.1298   0.6148   0.0528
  -2.500   0.3682   0.00865   0.00206  -0.1304   0.6133   0.0588
  -2.250   0.3982   0.00858   0.00201  -0.1309   0.6120   0.0642
  -2.000   0.4282   0.00849   0.00196  -0.1314   0.6104   0.0710
  -1.750   0.4582   0.00842   0.00191  -0.1320   0.6087   0.0781
  -1.500   0.4882   0.00836   0.00187  -0.1325   0.6070   0.0865
  -1.250   0.5181   0.00829   0.00183  -0.1331   0.6054   0.0978
  -1.000   0.5481   0.00821   0.00180  -0.1337   0.6038   0.1144
  -0.750   0.5781   0.00811   0.00178  -0.1343   0.6022   0.1450
  -0.500   0.6083   0.00798   0.00177  -0.1350   0.6004   0.1919
  -0.250   0.6385   0.00783   0.00177  -0.1358   0.5985   0.2558
   0.000   0.6693   0.00762   0.00179  -0.1367   0.5971   0.3353
   0.250   0.7002   0.00738   0.00182  -0.1377   0.5956   0.4322
   0.500   0.7310   0.00720   0.00186  -0.1386   0.5939   0.5141
   0.750   0.7618   0.00704   0.00191  -0.1395   0.5921   0.5975
   1.000   0.7921   0.00696   0.00196  -0.1401   0.5901   0.6506
   1.250   0.8223   0.00684   0.00204  -0.1408   0.5881   0.7234
   1.500   0.8508   0.00673   0.00216  -0.1410   0.5861   0.8099
   1.750   0.8784   0.00675   0.00226  -0.1410   0.5841   0.8542
   2.000   0.9065   0.00678   0.00234  -0.1411   0.5822   0.8726
   2.250   0.9350   0.00682   0.00241  -0.1412   0.5803   0.8855
   2.500   0.9632   0.00685   0.00248  -0.1414   0.5781   0.8943
   2.750   0.9920   0.00691   0.00254  -0.1417   0.5757   0.9020
   3.000   1.0199   0.00696   0.00260  -0.1418   0.5733   0.9081
   3.250   1.0481   0.00702   0.00267  -0.1420   0.5708   0.9145
   3.500   1.0761   0.00710   0.00274  -0.1422   0.5680   0.9204
   3.750   1.1039   0.00713   0.00281  -0.1423   0.5649   0.9259
   4.000   1.1321   0.00719   0.00288  -0.1425   0.5602   0.9312
   4.250   1.1589   0.00728   0.00295  -0.1424   0.5539   0.9362
   4.500   1.1859   0.00733   0.00302  -0.1424   0.5465   0.9417
   5.000   1.2380   0.00754   0.00321  -0.1421   0.5275   0.9534
   5.500   1.2873   0.00783   0.00345  -0.1412   0.5046   0.9705
   5.750   1.3125   0.00801   0.00359  -0.1409   0.4902   0.9934
   6.000   1.3396   0.00827   0.00380  -0.1412   0.4757   0.9998
   6.250   1.3655   0.00860   0.00406  -0.1412   0.4572   0.9998
   6.500   1.3894   0.00905   0.00441  -0.1410   0.4340   0.9998
   6.750   1.4091   0.00978   0.00494  -0.1401   0.3944   0.9998
   7.000   1.4234   0.01082   0.00571  -0.1384   0.3453   0.9998
   7.250   1.4357   0.01189   0.00652  -0.1364   0.3007   0.9998
   7.500   1.4478   0.01284   0.00730  -0.1344   0.2672   0.9998
   7.750   1.4576   0.01372   0.00805  -0.1319   0.2407   0.9998
   8.000   1.4647   0.01474   0.00896  -0.1292   0.2176   0.9998
   8.250   1.4705   0.01597   0.01010  -0.1267   0.1943   0.9998
   8.500   1.4765   0.01736   0.01139  -0.1246   0.1737   0.9998
   8.750   1.4826   0.01889   0.01284  -0.1227   0.1546   0.9998
   9.000   1.4895   0.02047   0.01435  -0.1212   0.1389   0.9998
   9.250   1.4977   0.02200   0.01586  -0.1198   0.1263   0.9998
   9.500   1.5065   0.02353   0.01736  -0.1186   0.1160   0.9998
   9.750   1.5143   0.02513   0.01893  -0.1173   0.1065   0.9998
  10.000   1.5216   0.02679   0.02056  -0.1159   0.0976   0.9998
  10.250   1.5298   0.02837   0.02214  -0.1147   0.0897   0.9998
  10.500   1.5368   0.03002   0.02378  -0.1133   0.0828   0.9998
  10.750   1.5445   0.03162   0.02538  -0.1121   0.0769   0.9998
  11.000   1.5512   0.03332   0.02707  -0.1108   0.0712   0.9998
  11.250   1.5572   0.03504   0.02879  -0.1094   0.0653   0.9998
  11.500   1.5635   0.03675   0.03051  -0.1081   0.0604   0.9998
  11.750   1.5700   0.03849   0.03225  -0.1069   0.0559   0.9998
  12.000   1.5769   0.04023   0.03401  -0.1057   0.0521   0.9998
  12.250   1.5840   0.04195   0.03574  -0.1046   0.0483   0.9998
  12.500   1.5898   0.04385   0.03764  -0.1034   0.0447   0.9998
  12.750   1.5980   0.04553   0.03935  -0.1025   0.0419   0.9998
  13.000   1.6037   0.04748   0.04132  -0.1015   0.0392   0.9998
  13.250   1.6111   0.04926   0.04312  -0.1005   0.0370   0.9998
  13.500   1.6180   0.05111   0.04501  -0.0996   0.0348   0.9998
  13.750   1.6234   0.05316   0.04707  -0.0987   0.0325   0.9998
  14.000   1.6310   0.05498   0.04893  -0.0978   0.0309   0.9998
  14.250   1.6371   0.05699   0.05098  -0.0970   0.0292   0.9998
  14.500   1.6424   0.05906   0.05307  -0.0962   0.0275   0.9998
  14.750   1.6484   0.06109   0.05514  -0.0954   0.0261   0.9998
  15.000   1.6543   0.06317   0.05727  -0.0947   0.0249   0.9998
  15.250   1.6599   0.06527   0.05940  -0.0940   0.0235   0.9998
  15.500   1.6634   0.06765   0.06180  -0.0933   0.0221   0.9998
  15.750   1.6692   0.06977   0.06399  -0.0927   0.0213   0.9998
  16.000   1.6742   0.07197   0.06623  -0.0921   0.0204   0.9998
  16.250   1.6775   0.07441   0.06872  -0.0916   0.0194   0.9998
  16.500   1.6810   0.07682   0.07117  -0.0910   0.0184   0.9998
  16.750   1.6844   0.07931   0.07371  -0.0906   0.0177   0.9998
  17.000   1.6882   0.08173   0.07619  -0.0902   0.0169   0.9998
  17.250   1.6909   0.08430   0.07882  -0.0898   0.0162   0.9998
  17.500   1.6925   0.08701   0.08158  -0.0895   0.0155   0.9998
  17.750   1.6938   0.08978   0.08439  -0.0892   0.0149   0.9998
  18.000   1.6959   0.09249   0.08718  -0.0890   0.0145   0.9998
  18.250   1.6984   0.09516   0.08991  -0.0888   0.0139   0.9998
  18.500   1.6988   0.09812   0.09294  -0.0888   0.0134   0.9998
  18.750   1.6997   0.10102   0.09590  -0.0888   0.0128   0.9998
  19.000   1.6981   0.10427   0.09920  -0.0889   0.0123   0.9998
  19.250   1.6983   0.10728   0.10228  -0.0890   0.0118   0.9998
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