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HAM-STD HS1-712 AIRFOIL (hs1712-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: HAM-STD HS1-712 AIRFOIL (hs1712-il)
Reynolds number: 1,000,000
Max Cl/Cd: 103.69 at α=4°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-hs1712-il-1000000.txt
Download as CSV file: xf-hs1712-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HAM-STD HS1-712 AIRFOIL                         
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.3046   0.14055   0.13870  -0.0557   0.9923   0.0141
 -12.500  -0.2970   0.13719   0.13535  -0.0573   0.9912   0.0146
 -12.250  -0.7083   0.03325   0.03039  -0.1259   0.9780   0.0125
 -12.000  -0.6890   0.02993   0.02679  -0.1289   0.9764   0.0127
 -11.750  -0.6639   0.02765   0.02428  -0.1313   0.9754   0.0130
 -11.500  -0.6356   0.02594   0.02237  -0.1335   0.9746   0.0131
 -11.250  -0.6089   0.02312   0.01924  -0.1363   0.9739   0.0135
 -11.000  -0.5780   0.02164   0.01762  -0.1385   0.9734   0.0138
 -10.750  -0.5456   0.02071   0.01661  -0.1404   0.9729   0.0142
 -10.500  -0.5123   0.01984   0.01566  -0.1424   0.9726   0.0145
 -10.250  -0.4790   0.01898   0.01468  -0.1443   0.9722   0.0149
 -10.000  -0.4461   0.01819   0.01377  -0.1460   0.9720   0.0154
  -9.750  -0.4130   0.01749   0.01296  -0.1477   0.9717   0.0157
  -9.500  -0.3797   0.01673   0.01206  -0.1495   0.9715   0.0161
  -9.250  -0.3646   0.01591   0.01117  -0.1472   0.9664   0.0166
  -9.000  -0.3335   0.01534   0.01056  -0.1483   0.9654   0.0171
  -8.750  -0.3005   0.01483   0.00999  -0.1498   0.9646   0.0177
  -8.500  -0.2665   0.01430   0.00939  -0.1514   0.9640   0.0183
  -8.250  -0.2323   0.01387   0.00889  -0.1530   0.9634   0.0189
  -8.000  -0.1991   0.01314   0.00809  -0.1546   0.9628   0.0198
  -7.750  -0.1658   0.01270   0.00763  -0.1560   0.9621   0.0207
  -7.500  -0.1326   0.01230   0.00718  -0.1573   0.9614   0.0216
  -7.250  -0.0992   0.01185   0.00666  -0.1587   0.9607   0.0225
  -7.000  -0.0657   0.01142   0.00623  -0.1601   0.9599   0.0238
  -6.750  -0.0322   0.01112   0.00590  -0.1614   0.9590   0.0252
  -6.500  -0.0037   0.01086   0.00564  -0.1616   0.9563   0.0267
  -6.250   0.0239   0.01070   0.00549  -0.1614   0.9526   0.0281
  -6.000   0.0555   0.01047   0.00524  -0.1622   0.9499   0.0298
  -5.750   0.0880   0.01033   0.00510  -0.1631   0.9474   0.0316
  -5.500   0.1205   0.01013   0.00487  -0.1641   0.9451   0.0336
  -5.250   0.1498   0.01000   0.00472  -0.1643   0.9418   0.0359
  -5.000   0.1781   0.00974   0.00445  -0.1645   0.9378   0.0383
  -4.750   0.2083   0.00950   0.00418  -0.1649   0.9336   0.0409
  -4.500   0.2409   0.00902   0.00368  -0.1661   0.9296   0.0440
  -4.250   0.2689   0.00878   0.00343  -0.1661   0.9234   0.0464
  -4.000   0.2987   0.00854   0.00320  -0.1665   0.9169   0.0490
  -3.750   0.3287   0.00836   0.00301  -0.1670   0.9086   0.0512
  -3.500   0.3585   0.00821   0.00284  -0.1673   0.8960   0.0539
  -3.250   0.3881   0.00809   0.00267  -0.1675   0.8793   0.0568
  -3.000   0.4172   0.00803   0.00252  -0.1677   0.8577   0.0600
  -2.750   0.4456   0.00801   0.00240  -0.1677   0.8348   0.0648
  -2.500   0.4734   0.00801   0.00234  -0.1677   0.8133   0.0742
  -2.250   0.5005   0.00804   0.00230  -0.1675   0.7929   0.0930
  -2.000   0.5282   0.00805   0.00230  -0.1675   0.7773   0.1139
  -1.750   0.5538   0.00812   0.00228  -0.1669   0.7327   0.1320
  -1.500   0.5796   0.00825   0.00233  -0.1665   0.7121   0.1487
  -1.250   0.6068   0.00833   0.00238  -0.1664   0.6970   0.1657
  -1.000   0.6342   0.00841   0.00244  -0.1663   0.6802   0.1807
  -0.750   0.6614   0.00850   0.00248  -0.1662   0.6629   0.1938
  -0.500   0.6884   0.00860   0.00253  -0.1660   0.6455   0.2051
  -0.250   0.7154   0.00869   0.00258  -0.1658   0.6276   0.2193
   0.000   0.7425   0.00879   0.00264  -0.1657   0.6110   0.2325
   0.250   0.7694   0.00889   0.00270  -0.1655   0.5911   0.2471
   0.500   0.7957   0.00901   0.00277  -0.1653   0.5703   0.2698
   0.750   0.8226   0.00904   0.00288  -0.1652   0.5531   0.3310
   1.000   0.8498   0.00879   0.00309  -0.1656   0.5173   0.5710
   1.250   0.8746   0.00871   0.00336  -0.1653   0.4777   0.7794
   1.500   0.8871   0.00873   0.00358  -0.1616   0.4394   0.9383
   1.750   0.9046   0.00897   0.00363  -0.1592   0.3950   1.0000
   2.000   0.9287   0.00939   0.00383  -0.1586   0.3593   1.0000
   2.250   0.9547   0.00964   0.00399  -0.1583   0.3482   1.0000
   2.500   0.9814   0.00984   0.00413  -0.1581   0.3401   1.0000
   2.750   1.0083   0.01002   0.00427  -0.1580   0.3330   1.0000
   3.000   1.0345   0.01024   0.00444  -0.1577   0.3252   1.0000
   3.250   1.0617   0.01037   0.00455  -0.1577   0.3178   1.0000
   3.500   1.0878   0.01058   0.00471  -0.1574   0.3082   1.0000
   3.750   1.1141   0.01076   0.00484  -0.1571   0.2967   1.0000
   4.000   1.1396   0.01099   0.00500  -0.1568   0.2839   1.0000
   4.250   1.1644   0.01126   0.00518  -0.1562   0.2696   1.0000
   4.500   1.1888   0.01155   0.00539  -0.1556   0.2555   1.0000
   4.750   1.2129   0.01183   0.00561  -0.1550   0.2421   1.0000
   5.000   1.2370   0.01211   0.00582  -0.1544   0.2299   1.0000
   5.250   1.2605   0.01241   0.00607  -0.1536   0.2175   1.0000
   5.500   1.2831   0.01275   0.00634  -0.1526   0.2040   1.0000
   5.750   1.3051   0.01312   0.00662  -0.1516   0.1900   1.0000
   6.000   1.3267   0.01349   0.00693  -0.1504   0.1765   1.0000
   6.250   1.3470   0.01391   0.00726  -0.1490   0.1618   1.0000
   6.500   1.3651   0.01436   0.00764  -0.1472   0.1470   1.0000
   6.750   1.3831   0.01484   0.00804  -0.1453   0.1330   1.0000
   7.000   1.4004   0.01538   0.00850  -0.1434   0.1184   1.0000
   7.250   1.4169   0.01596   0.00899  -0.1413   0.1021   1.0000
   7.500   1.4334   0.01657   0.00952  -0.1392   0.0879   1.0000
   7.750   1.4511   0.01710   0.01000  -0.1374   0.0793   1.0000
   8.000   1.4695   0.01759   0.01047  -0.1358   0.0773   1.0000
   8.250   1.4879   0.01808   0.01095  -0.1341   0.0754   1.0000
   8.500   1.5064   0.01857   0.01145  -0.1326   0.0737   1.0000
   8.750   1.5252   0.01902   0.01193  -0.1311   0.0726   1.0000
   9.000   1.5440   0.01947   0.01243  -0.1296   0.0718   1.0000
   9.250   1.5623   0.01995   0.01295  -0.1280   0.0708   1.0000
   9.500   1.5800   0.02048   0.01352  -0.1264   0.0698   1.0000
   9.750   1.5967   0.02107   0.01414  -0.1246   0.0689   1.0000
  10.000   1.6123   0.02173   0.01483  -0.1227   0.0676   1.0000
  10.250   1.6290   0.02232   0.01546  -0.1210   0.0665   1.0000
  10.500   1.6480   0.02275   0.01593  -0.1198   0.0653   1.0000
  10.750   1.6661   0.02324   0.01646  -0.1184   0.0637   1.0000
  11.000   1.6832   0.02381   0.01706  -0.1169   0.0618   1.0000
  11.250   1.6992   0.02444   0.01772  -0.1152   0.0602   1.0000
  11.500   1.7152   0.02509   0.01839  -0.1136   0.0588   1.0000
  11.750   1.7301   0.02581   0.01912  -0.1119   0.0569   1.0000
  12.000   1.7433   0.02665   0.01998  -0.1099   0.0551   1.0000
  12.250   1.7569   0.02746   0.02085  -0.1081   0.0536   1.0000
  12.500   1.7682   0.02846   0.02187  -0.1060   0.0518   1.0000
  12.750   1.7782   0.02955   0.02300  -0.1038   0.0499   1.0000
  13.000   1.7946   0.03021   0.02373  -0.1025   0.0481   1.0000
  13.250   1.8067   0.03118   0.02475  -0.1007   0.0453   1.0000
  13.750   1.8267   0.03351   0.02703  -0.0968   0.0343   1.0000
  14.000   1.8319   0.03511   0.02865  -0.0944   0.0324   1.0000
  14.250   1.8388   0.03663   0.03025  -0.0924   0.0313   1.0000
  14.500   1.8436   0.03837   0.03207  -0.0902   0.0303   1.0000
  14.750   1.8461   0.04038   0.03415  -0.0880   0.0294   1.0000
  15.000   1.8459   0.04271   0.03655  -0.0858   0.0283   1.0000
  15.250   1.8525   0.04447   0.03840  -0.0843   0.0277   1.0000
  15.500   1.8581   0.04637   0.04039  -0.0829   0.0269   1.0000
  15.750   1.8607   0.04862   0.04273  -0.0814   0.0261   1.0000
  16.000   1.8607   0.05125   0.04544  -0.0800   0.0252   1.0000
  16.250   1.8580   0.05429   0.04856  -0.0786   0.0245   1.0000
  16.500   1.8631   0.05651   0.05088  -0.0778   0.0238   1.0000
  16.750   1.8657   0.05905   0.05351  -0.0770   0.0230   1.0000
  17.000   1.8654   0.06200   0.05653  -0.0763   0.0222   1.0000
  17.250   1.8622   0.06537   0.05999  -0.0757   0.0214   1.0000
  17.500   1.8593   0.06877   0.06348  -0.0752   0.0207   1.0000
  17.750   1.8577   0.07208   0.06688  -0.0750   0.0201   1.0000
  18.000   1.8538   0.07569   0.07059  -0.0748   0.0194   1.0000
  18.250   1.8475   0.07972   0.07471  -0.0748   0.0187   1.0000
  18.500   1.8381   0.08426   0.07933  -0.0751   0.0181   1.0000
  18.750   1.8290   0.08884   0.08403  -0.0755   0.0177   1.0000
  19.000   1.8197   0.09356   0.08886  -0.0762   0.0172   1.0000
  19.250   1.8089   0.09855   0.09396  -0.0772   0.0167   1.0000
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