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AH 95-160 (ah95160-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: AH 95-160 (ah95160-il)
Reynolds number: 1,000,000
Max Cl/Cd: 163.17 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ah95160-il-1000000-n5.txt
Download as CSV file: xf-ah95160-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 95-160                                       
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.8635   0.04514   0.04125  -0.0962   0.6884   0.0108
 -14.750  -0.8914   0.03562   0.03144  -0.1070   0.6863   0.0108
 -14.500  -0.8953   0.03199   0.02763  -0.1101   0.6838   0.0109
 -14.250  -0.8948   0.02976   0.02525  -0.1108   0.6819   0.0109
 -14.000  -0.8837   0.02811   0.02346  -0.1112   0.6803   0.0110
 -13.750  -0.8690   0.02672   0.02194  -0.1114   0.6784   0.0110
 -13.500  -0.8517   0.02551   0.02061  -0.1115   0.6765   0.0111
 -13.250  -0.8341   0.02426   0.01924  -0.1116   0.6745   0.0112
 -13.000  -0.8156   0.02302   0.01788  -0.1117   0.6724   0.0114
 -12.750  -0.7949   0.02201   0.01676  -0.1118   0.6703   0.0115
 -12.500  -0.7725   0.02116   0.01581  -0.1119   0.6681   0.0117
 -12.000  -0.7249   0.01970   0.01420  -0.1122   0.6648   0.0120
 -11.750  -0.7001   0.01906   0.01348  -0.1123   0.6634   0.0122
 -11.500  -0.6748   0.01845   0.01280  -0.1125   0.6619   0.0124
 -11.250  -0.6492   0.01788   0.01216  -0.1126   0.6603   0.0126
 -11.000  -0.6232   0.01733   0.01153  -0.1128   0.6587   0.0128
 -10.750  -0.5969   0.01681   0.01093  -0.1130   0.6570   0.0130
 -10.500  -0.5703   0.01633   0.01037  -0.1132   0.6552   0.0132
 -10.250  -0.5434   0.01589   0.00986  -0.1134   0.6534   0.0134
 -10.000  -0.5163   0.01549   0.00938  -0.1136   0.6516   0.0136
  -9.750  -0.4891   0.01505   0.00887  -0.1139   0.6498   0.0139
  -9.500  -0.4620   0.01455   0.00832  -0.1141   0.6486   0.0142
  -9.250  -0.4343   0.01414   0.00787  -0.1144   0.6475   0.0145
  -9.000  -0.4064   0.01377   0.00747  -0.1147   0.6462   0.0149
  -8.750  -0.3783   0.01343   0.00709  -0.1150   0.6448   0.0152
  -8.500  -0.3500   0.01311   0.00673  -0.1153   0.6433   0.0156
  -8.250  -0.3216   0.01281   0.00638  -0.1156   0.6416   0.0160
  -8.000  -0.2931   0.01253   0.00605  -0.1159   0.6399   0.0164
  -7.750  -0.2645   0.01226   0.00573  -0.1162   0.6384   0.0167
  -7.500  -0.2360   0.01194   0.00538  -0.1166   0.6370   0.0173
  -7.250  -0.2073   0.01169   0.00510  -0.1169   0.6355   0.0180
  -7.000  -0.1784   0.01147   0.00485  -0.1173   0.6339   0.0186
  -6.750  -0.1494   0.01126   0.00461  -0.1176   0.6324   0.0194
  -6.500  -0.1203   0.01103   0.00436  -0.1180   0.6313   0.0202
  -6.250  -0.0911   0.01081   0.00414  -0.1184   0.6299   0.0213
  -6.000  -0.0618   0.01061   0.00393  -0.1188   0.6286   0.0225
  -5.750  -0.0325   0.01044   0.00374  -0.1192   0.6273   0.0235
  -5.500  -0.0031   0.01024   0.00354  -0.1196   0.6258   0.0252
  -5.250   0.0263   0.01009   0.00337  -0.1201   0.6242   0.0268
  -5.000   0.0557   0.00993   0.00321  -0.1205   0.6226   0.0289
  -4.750   0.0851   0.00979   0.00306  -0.1209   0.6210   0.0313
  -4.500   0.1146   0.00965   0.00293  -0.1213   0.6195   0.0344
  -4.250   0.1440   0.00954   0.00280  -0.1218   0.6180   0.0377
  -4.000   0.1736   0.00943   0.00270  -0.1222   0.6167   0.0413
  -3.750   0.2033   0.00931   0.00260  -0.1227   0.6156   0.0452
  -3.500   0.2331   0.00921   0.00251  -0.1232   0.6142   0.0494
  -3.250   0.2628   0.00910   0.00243  -0.1237   0.6127   0.0541
  -3.000   0.2926   0.00901   0.00236  -0.1242   0.6112   0.0586
  -2.750   0.3224   0.00893   0.00229  -0.1246   0.6097   0.0634
  -2.500   0.3521   0.00885   0.00222  -0.1251   0.6082   0.0686
  -2.250   0.3818   0.00878   0.00217  -0.1256   0.6067   0.0739
  -2.000   0.4115   0.00871   0.00211  -0.1261   0.6051   0.0808
  -1.750   0.4411   0.00866   0.00206  -0.1266   0.6033   0.0869
  -1.500   0.4707   0.00861   0.00203  -0.1271   0.6015   0.0963
  -1.250   0.5005   0.00853   0.00200  -0.1276   0.6003   0.1089
  -0.750   0.5603   0.00830   0.00195  -0.1288   0.5975   0.1636
  -0.500   0.5901   0.00814   0.00194  -0.1294   0.5957   0.2117
  -0.250   0.6200   0.00795   0.00193  -0.1301   0.5939   0.2786
   0.000   0.6498   0.00776   0.00193  -0.1308   0.5922   0.3518
   0.250   0.6797   0.00753   0.00195  -0.1316   0.5905   0.4434
   0.500   0.7094   0.00737   0.00198  -0.1322   0.5888   0.5184
   0.750   0.7390   0.00726   0.00203  -0.1328   0.5870   0.5852
   1.000   0.7686   0.00722   0.00208  -0.1333   0.5852   0.6252
   1.250   0.7983   0.00715   0.00215  -0.1339   0.5836   0.6720
   1.500   0.8276   0.00705   0.00223  -0.1343   0.5820   0.7326
   1.750   0.8564   0.00699   0.00232  -0.1346   0.5802   0.7815
   2.250   0.9140   0.00702   0.00246  -0.1352   0.5759   0.8280
   2.500   0.9427   0.00705   0.00252  -0.1355   0.5737   0.8437
   2.750   0.9710   0.00710   0.00259  -0.1357   0.5716   0.8571
   3.000   0.9993   0.00715   0.00266  -0.1359   0.5696   0.8689
   3.250   1.0279   0.00718   0.00274  -0.1362   0.5676   0.8805
   3.500   1.0561   0.00722   0.00282  -0.1364   0.5652   0.8926
   3.750   1.0836   0.00726   0.00289  -0.1364   0.5623   0.9040
   4.000   1.1108   0.00731   0.00296  -0.1364   0.5591   0.9156
   4.750   1.1880   0.00744   0.00317  -0.1354   0.5447   0.9626
   5.000   1.2167   0.00751   0.00323  -0.1359   0.5379   0.9998
   5.250   1.2450   0.00763   0.00334  -0.1362   0.5289   0.9998
   5.500   1.2726   0.00780   0.00347  -0.1365   0.5190   0.9998
   5.750   1.2993   0.00800   0.00363  -0.1367   0.5077   0.9998
   6.000   1.3259   0.00821   0.00381  -0.1368   0.4963   0.9998
   6.250   1.3521   0.00844   0.00400  -0.1368   0.4841   0.9998
   6.500   1.3772   0.00873   0.00424  -0.1367   0.4699   0.9998
   6.750   1.4011   0.00908   0.00453  -0.1364   0.4534   0.9998
   7.000   1.4226   0.00955   0.00490  -0.1357   0.4329   0.9998
   7.250   1.4416   0.01013   0.00537  -0.1346   0.4061   0.9998
   7.500   1.4555   0.01094   0.00601  -0.1328   0.3738   0.9998
   7.750   1.4649   0.01190   0.00679  -0.1302   0.3410   0.9998
   8.000   1.4676   0.01295   0.00770  -0.1266   0.3110   0.9998
   8.250   1.4693   0.01426   0.00888  -0.1233   0.2821   0.9998
   8.500   1.4715   0.01576   0.01026  -0.1205   0.2568   0.9998
   8.750   1.4738   0.01746   0.01186  -0.1182   0.2338   0.9998
   9.000   1.4774   0.01922   0.01354  -0.1163   0.2140   0.9998
   9.250   1.4815   0.02103   0.01528  -0.1145   0.1962   0.9998
   9.500   1.4850   0.02291   0.01710  -0.1128   0.1796   0.9998
   9.750   1.4888   0.02480   0.01894  -0.1111   0.1649   0.9998
  10.000   1.4923   0.02669   0.02078  -0.1095   0.1515   0.9998
  10.250   1.4962   0.02856   0.02261  -0.1079   0.1398   0.9998
  10.500   1.4997   0.03046   0.02447  -0.1062   0.1292   0.9998
  10.750   1.5037   0.03230   0.02629  -0.1047   0.1193   0.9998
  11.000   1.5094   0.03402   0.02799  -0.1033   0.1111   0.9998
  11.250   1.5136   0.03589   0.02984  -0.1018   0.1033   0.9998
  11.500   1.5204   0.03758   0.03152  -0.1006   0.0969   0.9998
  11.750   1.5266   0.03937   0.03331  -0.0994   0.0912   0.9998
  12.000   1.5335   0.04111   0.03506  -0.0983   0.0854   0.9998
  12.250   1.5398   0.04292   0.03686  -0.0971   0.0800   0.9998
  12.500   1.5467   0.04470   0.03865  -0.0961   0.0753   0.9998
  12.750   1.5535   0.04649   0.04044  -0.0951   0.0707   0.9998
  13.000   1.5606   0.04832   0.04228  -0.0942   0.0668   0.9998
  13.250   1.5660   0.05029   0.04424  -0.0931   0.0622   0.9998
  13.500   1.5740   0.05202   0.04600  -0.0923   0.0588   0.9998
  13.750   1.5790   0.05408   0.04806  -0.0913   0.0551   0.9998
  14.000   1.5862   0.05592   0.04993  -0.0905   0.0520   0.9998
  14.250   1.5926   0.05788   0.05190  -0.0897   0.0489   0.9998
  14.500   1.5974   0.06002   0.05405  -0.0889   0.0459   0.9998
  14.750   1.6046   0.06188   0.05594  -0.0882   0.0434   0.9998
  15.000   1.6091   0.06407   0.05815  -0.0874   0.0409   0.9998
  15.250   1.6147   0.06617   0.06027  -0.0867   0.0388   0.9998
  15.500   1.6211   0.06817   0.06231  -0.0861   0.0368   0.9998
  15.750   1.6246   0.07054   0.06471  -0.0855   0.0347   0.9998
  16.000   1.6299   0.07269   0.06689  -0.0849   0.0332   0.9998
  16.250   1.6354   0.07483   0.06907  -0.0844   0.0318   0.9998
  16.500   1.6389   0.07723   0.07150  -0.0839   0.0303   0.9998
  16.750   1.6425   0.07961   0.07392  -0.0833   0.0289   0.9998
  17.000   1.6469   0.08195   0.07631  -0.0830   0.0278   0.9998
  17.250   1.6506   0.08437   0.07878  -0.0826   0.0266   0.9998
  17.500   1.6539   0.08684   0.08128  -0.0822   0.0254   0.9998
  17.750   1.6552   0.08956   0.08405  -0.0819   0.0244   0.9998
  18.000   1.6592   0.09196   0.08650  -0.0817   0.0235   0.9998
  18.250   1.6613   0.09464   0.08924  -0.0815   0.0226   0.9998
  18.500   1.6629   0.09737   0.09202  -0.0814   0.0216   0.9998
  18.750   1.6636   0.10024   0.09493  -0.0813   0.0207   0.9998
  19.000   1.6655   0.10299   0.09774  -0.0813   0.0201   0.9998
  19.250   1.6677   0.10568   0.10049  -0.0814   0.0193   0.9998
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