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HAM-STD HS1-712 AIRFOIL (hs1712-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: HAM-STD HS1-712 AIRFOIL (hs1712-il)
Reynolds number: 500,000
Max Cl/Cd: 83.54 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hs1712-il-500000-n5.txt
Download as CSV file: xf-hs1712-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.6476   0.03443   0.03078  -0.1267   0.9722   0.0126
 -11.500  -0.6272   0.03032   0.02628  -0.1308   0.9715   0.0128
 -11.250  -0.6135   0.02813   0.02381  -0.1306   0.9680   0.0130
 -11.000  -0.5919   0.02628   0.02172  -0.1315   0.9659   0.0133
 -10.750  -0.5663   0.02487   0.02018  -0.1327   0.9645   0.0135
 -10.500  -0.5383   0.02374   0.01894  -0.1340   0.9633   0.0138
 -10.250  -0.5090   0.02272   0.01778  -0.1353   0.9624   0.0142
 -10.000  -0.4784   0.02173   0.01666  -0.1368   0.9615   0.0146
  -9.750  -0.4458   0.02076   0.01554  -0.1387   0.9607   0.0151
  -9.500  -0.4115   0.01982   0.01442  -0.1408   0.9599   0.0157
  -9.250  -0.3765   0.01888   0.01334  -0.1430   0.9593   0.0162
  -9.000  -0.3418   0.01810   0.01249  -0.1451   0.9587   0.0167
  -8.750  -0.3224   0.01764   0.01196  -0.1435   0.9540   0.0172
  -8.500  -0.2939   0.01706   0.01129  -0.1441   0.9519   0.0178
  -8.250  -0.2633   0.01647   0.01059  -0.1450   0.9505   0.0184
  -8.000  -0.2316   0.01592   0.00992  -0.1461   0.9494   0.0190
  -7.750  -0.1994   0.01534   0.00932  -0.1474   0.9484   0.0198
  -7.500  -0.1663   0.01488   0.00880  -0.1488   0.9473   0.0208
  -7.250  -0.1325   0.01440   0.00824  -0.1503   0.9462   0.0219
  -7.000  -0.0984   0.01393   0.00773  -0.1519   0.9452   0.0230
  -6.750  -0.0646   0.01356   0.00734  -0.1533   0.9442   0.0241
  -6.500  -0.0432   0.01335   0.00709  -0.1519   0.9390   0.0252
  -6.250  -0.0142   0.01311   0.00685  -0.1522   0.9362   0.0265
  -6.000   0.0172   0.01290   0.00663  -0.1531   0.9341   0.0281
  -5.750   0.0496   0.01269   0.00639  -0.1541   0.9323   0.0301
  -5.500   0.0827   0.01247   0.00611  -0.1552   0.9306   0.0326
  -5.250   0.1171   0.01218   0.00580  -0.1567   0.9290   0.0347
  -5.000   0.1396   0.01209   0.00565  -0.1554   0.9221   0.0368
  -4.750   0.1706   0.01171   0.00527  -0.1562   0.9175   0.0390
  -4.500   0.2047   0.01142   0.00492  -0.1576   0.9144   0.0412
  -4.250   0.2326   0.01110   0.00462  -0.1578   0.9087   0.0432
  -4.000   0.2614   0.01088   0.00438  -0.1580   0.9024   0.0452
  -3.750   0.2948   0.01060   0.00411  -0.1592   0.8979   0.0475
  -3.500   0.3240   0.01042   0.00394  -0.1595   0.8899   0.0496
  -3.250   0.3591   0.01017   0.00368  -0.1611   0.8806   0.0537
  -3.000   0.3921   0.00997   0.00342  -0.1621   0.8630   0.0600
  -2.750   0.4259   0.00981   0.00315  -0.1633   0.8355   0.0665
  -2.500   0.4557   0.00978   0.00299  -0.1636   0.8028   0.0764
  -2.250   0.4840   0.00983   0.00292  -0.1636   0.7819   0.0909
  -2.000   0.5103   0.00986   0.00288  -0.1632   0.7401   0.1052
  -1.750   0.5352   0.01000   0.00287  -0.1626   0.7170   0.1190
  -1.500   0.5618   0.01011   0.00290  -0.1623   0.7007   0.1337
  -1.250   0.5888   0.01019   0.00295  -0.1621   0.6828   0.1480
  -1.000   0.6156   0.01028   0.00300  -0.1619   0.6650   0.1634
  -0.750   0.6420   0.01038   0.00305  -0.1616   0.6462   0.1785
  -0.500   0.6684   0.01049   0.00311  -0.1613   0.6286   0.1913
  -0.250   0.6949   0.01060   0.00316  -0.1610   0.6112   0.2033
   0.000   0.7210   0.01071   0.00323  -0.1607   0.5907   0.2169
   0.250   0.7463   0.01087   0.00331  -0.1602   0.5694   0.2298
   0.500   0.7722   0.01099   0.00340  -0.1599   0.5514   0.2485
   0.750   0.7964   0.01118   0.00352  -0.1592   0.5145   0.2776
   1.000   0.8199   0.01136   0.00370  -0.1585   0.4758   0.3509
   1.250   0.8448   0.01104   0.00406  -0.1586   0.4361   0.6825
   1.500   0.8634   0.01110   0.00437  -0.1565   0.3958   0.8377
   1.750   0.8721   0.01108   0.00440  -0.1518   0.3679   0.9843
   2.000   0.8966   0.01133   0.00452  -0.1512   0.3533   1.0000
   2.250   0.9220   0.01160   0.00470  -0.1508   0.3444   1.0000
   2.500   0.9482   0.01181   0.00486  -0.1505   0.3377   1.0000
   2.750   0.9740   0.01203   0.00504  -0.1502   0.3302   1.0000
   3.000   0.9997   0.01226   0.00522  -0.1498   0.3230   1.0000
   3.250   1.0255   0.01246   0.00539  -0.1495   0.3133   1.0000
   3.500   1.0509   0.01269   0.00557  -0.1491   0.3039   1.0000
   3.750   1.0756   0.01295   0.00577  -0.1485   0.2916   1.0000
   4.000   1.1003   0.01320   0.00597  -0.1480   0.2804   1.0000
   4.250   1.1245   0.01347   0.00618  -0.1474   0.2704   1.0000
   4.500   1.1484   0.01375   0.00641  -0.1467   0.2604   1.0000
   4.750   1.1720   0.01403   0.00665  -0.1459   0.2507   1.0000
   5.000   1.1946   0.01436   0.00692  -0.1450   0.2389   1.0000
   5.250   1.2163   0.01472   0.00721  -0.1439   0.2251   1.0000
   5.500   1.2366   0.01509   0.00753  -0.1425   0.2113   1.0000
   5.750   1.2564   0.01550   0.00787  -0.1410   0.1979   1.0000
   6.000   1.2760   0.01594   0.00824  -0.1395   0.1847   1.0000
   6.250   1.2955   0.01639   0.00864  -0.1380   0.1729   1.0000
   6.500   1.3148   0.01685   0.00905  -0.1364   0.1607   1.0000
   6.750   1.3344   0.01730   0.00947  -0.1350   0.1504   1.0000
   7.000   1.3528   0.01783   0.00994  -0.1334   0.1379   1.0000
   7.250   1.3709   0.01838   0.01044  -0.1317   0.1265   1.0000
   7.500   1.3890   0.01893   0.01094  -0.1301   0.1161   1.0000
   7.750   1.4066   0.01951   0.01149  -0.1284   0.1053   1.0000
   8.000   1.4238   0.02012   0.01206  -0.1266   0.0965   1.0000
   8.250   1.4405   0.02075   0.01266  -0.1248   0.0860   1.0000
   8.500   1.4572   0.02139   0.01328  -0.1231   0.0791   1.0000
   8.750   1.4738   0.02203   0.01391  -0.1213   0.0769   1.0000
   9.000   1.4905   0.02266   0.01456  -0.1196   0.0752   1.0000
   9.250   1.5072   0.02330   0.01522  -0.1179   0.0737   1.0000
   9.500   1.5241   0.02392   0.01588  -0.1163   0.0725   1.0000
   9.750   1.5408   0.02454   0.01657  -0.1147   0.0715   1.0000
  10.000   1.5570   0.02521   0.01730  -0.1130   0.0704   1.0000
  10.250   1.5721   0.02595   0.01809  -0.1112   0.0692   1.0000
  10.500   1.5860   0.02679   0.01898  -0.1093   0.0680   1.0000
  10.750   1.5992   0.02768   0.01992  -0.1073   0.0670   1.0000
  11.000   1.6146   0.02840   0.02072  -0.1057   0.0658   1.0000
  11.250   1.6304   0.02910   0.02150  -0.1042   0.0640   1.0000
  11.500   1.6448   0.02993   0.02240  -0.1025   0.0618   1.0000
  11.750   1.6578   0.03086   0.02338  -0.1007   0.0599   1.0000
  12.000   1.6705   0.03183   0.02440  -0.0990   0.0582   1.0000
  12.250   1.6820   0.03290   0.02551  -0.0971   0.0566   1.0000
  12.500   1.6925   0.03406   0.02671  -0.0953   0.0550   1.0000
  12.750   1.7026   0.03527   0.02799  -0.0934   0.0534   1.0000
  13.000   1.7110   0.03667   0.02944  -0.0915   0.0515   1.0000
  13.250   1.7181   0.03820   0.03103  -0.0895   0.0499   1.0000
  13.500   1.7303   0.03935   0.03230  -0.0881   0.0477   1.0000
  13.750   1.7403   0.04070   0.03374  -0.0866   0.0445   1.0000
  14.000   1.7481   0.04229   0.03532  -0.0851   0.0357   1.0000
  14.250   1.7517   0.04431   0.03735  -0.0833   0.0337   1.0000
  14.500   1.7537   0.04656   0.03964  -0.0816   0.0319   1.0000
  14.750   1.7564   0.04883   0.04201  -0.0800   0.0308   1.0000
  15.000   1.7566   0.05143   0.04470  -0.0785   0.0296   1.0000
  15.250   1.7551   0.05433   0.04770  -0.0772   0.0287   1.0000
  15.500   1.7552   0.05714   0.05062  -0.0761   0.0278   1.0000
  15.750   1.7564   0.05990   0.05349  -0.0753   0.0270   1.0000
  16.000   1.7554   0.06299   0.05670  -0.0746   0.0261   1.0000
  16.250   1.7522   0.06643   0.06025  -0.0740   0.0253   1.0000
  16.500   1.7467   0.07025   0.06418  -0.0736   0.0246   1.0000
  16.750   1.7445   0.07370   0.06776  -0.0734   0.0240   1.0000
  17.000   1.7414   0.07733   0.07151  -0.0734   0.0233   1.0000
  17.250   1.7363   0.08133   0.07563  -0.0735   0.0225   1.0000
  17.500   1.7292   0.08568   0.08010  -0.0739   0.0219   1.0000
  17.750   1.7199   0.09044   0.08498  -0.0745   0.0213   1.0000
  18.000   1.7104   0.09534   0.09000  -0.0754   0.0209   1.0000
  18.250   1.7023   0.10008   0.09488  -0.0764   0.0203   1.0000
  18.500   1.6926   0.10517   0.10010  -0.0777   0.0198   1.0000
  18.750   1.6820   0.11050   0.10556  -0.0793   0.0193   1.0000
  19.000   1.6705   0.11607   0.11125  -0.0812   0.0189   1.0000
  19.250   1.6589   0.12173   0.11703  -0.0833   0.0184   1.0000
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