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HAM-STD HS1-712 AIRFOIL (hs1712-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: HAM-STD HS1-712 AIRFOIL (hs1712-il)
Reynolds number: 1,000,000
Max Cl/Cd: 89.69 at α=3°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hs1712-il-1000000-n5.txt
Download as CSV file: xf-hs1712-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.3410   0.16130   0.15932  -0.0565   0.9917   0.0064
 -15.000  -0.3329   0.15800   0.15602  -0.0583   0.9909   0.0066
 -14.000  -0.8265   0.03275   0.02965  -0.1378   0.9773   0.0092
 -13.750  -0.8120   0.02927   0.02595  -0.1405   0.9759   0.0093
 -13.500  -0.7917   0.02706   0.02356  -0.1422   0.9749   0.0094
 -13.250  -0.7686   0.02534   0.02169  -0.1437   0.9740   0.0096
 -13.000  -0.7438   0.02389   0.02010  -0.1450   0.9733   0.0098
 -12.750  -0.7178   0.02261   0.01868  -0.1462   0.9725   0.0099
 -12.500  -0.6908   0.02149   0.01743  -0.1474   0.9718   0.0101
 -12.250  -0.6632   0.02050   0.01632  -0.1485   0.9711   0.0103
 -12.000  -0.6407   0.01971   0.01542  -0.1482   0.9686   0.0104
 -11.750  -0.6149   0.01895   0.01456  -0.1486   0.9669   0.0106
 -11.500  -0.5880   0.01807   0.01358  -0.1492   0.9653   0.0108
 -11.250  -0.5601   0.01728   0.01270  -0.1500   0.9638   0.0111
 -11.000  -0.5312   0.01663   0.01198  -0.1508   0.9624   0.0114
 -10.750  -0.5018   0.01604   0.01133  -0.1516   0.9610   0.0116
 -10.500  -0.4715   0.01549   0.01071  -0.1526   0.9597   0.0119
 -10.250  -0.4408   0.01497   0.01011  -0.1536   0.9584   0.0122
 -10.000  -0.4140   0.01453   0.00961  -0.1537   0.9559   0.0126
  -9.750  -0.3862   0.01411   0.00912  -0.1540   0.9537   0.0129
  -9.500  -0.3576   0.01371   0.00866  -0.1544   0.9519   0.0131
  -9.250  -0.3285   0.01324   0.00814  -0.1550   0.9501   0.0135
  -9.000  -0.2988   0.01283   0.00768  -0.1556   0.9482   0.0140
  -8.750  -0.2683   0.01247   0.00729  -0.1564   0.9463   0.0145
  -8.500  -0.2375   0.01215   0.00692  -0.1572   0.9447   0.0151
  -8.250  -0.2085   0.01186   0.00658  -0.1576   0.9424   0.0156
  -8.000  -0.1800   0.01158   0.00626  -0.1579   0.9396   0.0161
  -7.750  -0.1509   0.01123   0.00589  -0.1583   0.9368   0.0168
  -7.500  -0.1211   0.01094   0.00557  -0.1589   0.9343   0.0174
  -7.250  -0.0907   0.01068   0.00528  -0.1595   0.9318   0.0182
  -7.000  -0.0599   0.01044   0.00499  -0.1602   0.9294   0.0190
  -6.750  -0.0308   0.01017   0.00471  -0.1606   0.9260   0.0200
  -6.500  -0.0016   0.00994   0.00446  -0.1609   0.9211   0.0211
  -6.250   0.0287   0.00972   0.00420  -0.1615   0.9153   0.0221
  -6.000   0.0584   0.00951   0.00399  -0.1619   0.9086   0.0237
  -5.750   0.0881   0.00934   0.00379  -0.1623   0.8985   0.0256
  -5.500   0.1178   0.00924   0.00368  -0.1627   0.8860   0.0281
  -5.250   0.1473   0.00918   0.00357  -0.1630   0.8708   0.0309
  -5.000   0.1764   0.00916   0.00346  -0.1632   0.8553   0.0333
  -4.750   0.2045   0.00917   0.00335  -0.1631   0.8334   0.0350
  -4.500   0.2317   0.00924   0.00327  -0.1629   0.8069   0.0365
  -4.250   0.2588   0.00925   0.00315  -0.1627   0.7903   0.0377
  -4.000   0.2870   0.00921   0.00304  -0.1628   0.7770   0.0390
  -3.750   0.3122   0.00930   0.00294  -0.1622   0.7250   0.0400
  -3.500   0.3378   0.00945   0.00292  -0.1617   0.6982   0.0409
  -3.250   0.3649   0.00948   0.00284  -0.1616   0.6721   0.0420
  -3.000   0.3920   0.00951   0.00277  -0.1615   0.6493   0.0430
  -2.750   0.4197   0.00954   0.00271  -0.1615   0.6304   0.0440
  -2.500   0.4476   0.00956   0.00265  -0.1615   0.6140   0.0451
  -2.250   0.4750   0.00962   0.00263  -0.1615   0.5929   0.0462
  -2.000   0.5020   0.00972   0.00263  -0.1613   0.5708   0.0477
  -1.750   0.5295   0.00979   0.00264  -0.1613   0.5571   0.0492
  -1.500   0.5576   0.00981   0.00264  -0.1614   0.5365   0.0579
  -1.250   0.5831   0.01004   0.00269  -0.1609   0.4982   0.0612
  -1.000   0.6081   0.01033   0.00279  -0.1604   0.4533   0.0653
  -0.750   0.6319   0.01072   0.00294  -0.1597   0.3929   0.0748
  -0.500   0.6571   0.01100   0.00306  -0.1593   0.3536   0.0883
   0.000   0.7125   0.01111   0.00320  -0.1594   0.3383   0.1218
   0.250   0.7404   0.01116   0.00327  -0.1595   0.3324   0.1389
   0.500   0.7678   0.01124   0.00337  -0.1595   0.3258   0.1592
   0.750   0.7958   0.01127   0.00344  -0.1596   0.3204   0.1743
   1.000   0.8232   0.01136   0.00353  -0.1596   0.3112   0.1898
   1.250   0.8505   0.01145   0.00363  -0.1595   0.3014   0.2083
   1.500   0.8772   0.01158   0.00373  -0.1594   0.2879   0.2251
   1.750   0.9037   0.01172   0.00385  -0.1592   0.2747   0.2423
   2.000   0.9303   0.01184   0.00397  -0.1591   0.2621   0.2711
   2.250   0.9575   0.01177   0.00419  -0.1594   0.2459   0.4328
   2.750   1.0030   0.01128   0.00477  -0.1576   0.2146   0.9185
   3.000   1.0198   0.01137   0.00482  -0.1550   0.1971   1.0000
   3.250   1.0439   0.01172   0.00504  -0.1544   0.1777   1.0000
   3.500   1.0681   0.01206   0.00528  -0.1537   0.1609   1.0000
   3.750   1.0918   0.01241   0.00552  -0.1530   0.1442   1.0000
   4.000   1.1155   0.01276   0.00578  -0.1523   0.1292   1.0000
   4.250   1.1372   0.01324   0.00611  -0.1512   0.1059   1.0000
   4.500   1.1583   0.01374   0.00648  -0.1499   0.0794   1.0000
   4.750   1.1816   0.01406   0.00674  -0.1491   0.0761   1.0000
   5.000   1.2052   0.01434   0.00699  -0.1484   0.0732   1.0000
   5.250   1.2291   0.01458   0.00723  -0.1477   0.0722   1.0000
   5.500   1.2525   0.01484   0.00749  -0.1469   0.0711   1.0000
   5.750   1.2754   0.01511   0.00775  -0.1460   0.0700   1.0000
   6.000   1.2966   0.01540   0.00804  -0.1447   0.0690   1.0000
   6.250   1.3174   0.01571   0.00836  -0.1434   0.0681   1.0000
   6.500   1.3381   0.01604   0.00870  -0.1420   0.0672   1.0000
   6.750   1.3589   0.01636   0.00903  -0.1408   0.0666   1.0000
   7.000   1.3800   0.01666   0.00935  -0.1395   0.0661   1.0000
   7.250   1.4011   0.01697   0.00968  -0.1384   0.0652   1.0000
   7.500   1.4220   0.01730   0.01002  -0.1372   0.0638   1.0000
   7.750   1.4425   0.01765   0.01040  -0.1359   0.0623   1.0000
   8.000   1.4624   0.01804   0.01079  -0.1345   0.0608   1.0000
   8.250   1.4822   0.01844   0.01121  -0.1332   0.0600   1.0000
   8.500   1.5019   0.01885   0.01163  -0.1318   0.0592   1.0000
   8.750   1.5208   0.01929   0.01208  -0.1304   0.0582   1.0000
   9.000   1.5394   0.01975   0.01256  -0.1289   0.0572   1.0000
   9.250   1.5580   0.02023   0.01304  -0.1274   0.0562   1.0000
   9.500   1.5762   0.02072   0.01356  -0.1259   0.0553   1.0000
   9.750   1.5941   0.02122   0.01409  -0.1243   0.0548   1.0000
  10.000   1.6117   0.02176   0.01466  -0.1228   0.0540   1.0000
  10.250   1.6284   0.02235   0.01527  -0.1211   0.0528   1.0000
  10.500   1.6435   0.02304   0.01598  -0.1192   0.0514   1.0000
  10.750   1.6585   0.02374   0.01671  -0.1173   0.0501   1.0000
  11.000   1.6765   0.02424   0.01727  -0.1160   0.0491   1.0000
  11.250   1.6931   0.02484   0.01791  -0.1144   0.0476   1.0000
  11.500   1.7084   0.02553   0.01864  -0.1127   0.0454   1.0000
  11.750   1.7251   0.02614   0.01928  -0.1113   0.0386   1.0000
  12.000   1.7341   0.02726   0.02031  -0.1087   0.0331   1.0000
  12.250   1.7454   0.02825   0.02133  -0.1066   0.0311   1.0000
  12.500   1.7557   0.02934   0.02246  -0.1044   0.0298   1.0000
  12.750   1.7648   0.03053   0.02370  -0.1021   0.0284   1.0000
  13.000   1.7763   0.03156   0.02478  -0.1002   0.0276   1.0000
  13.250   1.7871   0.03265   0.02594  -0.0983   0.0267   1.0000
  13.500   1.7964   0.03389   0.02724  -0.0963   0.0259   1.0000
  13.750   1.8045   0.03527   0.02867  -0.0943   0.0250   1.0000
  14.000   1.8127   0.03668   0.03014  -0.0924   0.0243   1.0000
  14.250   1.8221   0.03802   0.03155  -0.0907   0.0236   1.0000
  14.500   1.8303   0.03951   0.03311  -0.0890   0.0227   1.0000
  14.750   1.8368   0.04118   0.03484  -0.0873   0.0218   1.0000
  15.000   1.8421   0.04302   0.03673  -0.0856   0.0209   1.0000
  15.250   1.8482   0.04484   0.03862  -0.0841   0.0201   1.0000
  15.500   1.8530   0.04682   0.04067  -0.0827   0.0190   1.0000
  15.750   1.8562   0.04903   0.04294  -0.0812   0.0181   1.0000
  16.000   1.8591   0.05135   0.04533  -0.0800   0.0172   1.0000
  16.250   1.8613   0.05384   0.04790  -0.0789   0.0163   1.0000
  16.500   1.8618   0.05657   0.05070  -0.0779   0.0156   1.0000
  16.750   1.8612   0.05949   0.05369  -0.0770   0.0148   1.0000
  17.000   1.8607   0.06247   0.05676  -0.0763   0.0143   1.0000
  17.250   1.8585   0.06573   0.06010  -0.0757   0.0136   1.0000
  17.500   1.8550   0.06921   0.06368  -0.0753   0.0131   1.0000
  17.750   1.8496   0.07301   0.06756  -0.0750   0.0126   1.0000
  18.000   1.8442   0.07685   0.07151  -0.0749   0.0122   1.0000
  18.250   1.8379   0.08092   0.07568  -0.0750   0.0118   1.0000
  18.500   1.8300   0.08528   0.08015  -0.0753   0.0115   1.0000
  18.750   1.8205   0.08995   0.08492  -0.0758   0.0112   1.0000
  19.000   1.8096   0.09492   0.09001  -0.0766   0.0109   1.0000
  19.250   1.7974   0.10014   0.09534  -0.0776   0.0106   1.0000
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