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HAM-STD HS1-620 AIRFOIL (hs1620-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: HAM-STD HS1-620 AIRFOIL (hs1620-il)
Reynolds number: 100,000
Max Cl/Cd: 38.18 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hs1620-il-100000-n5.txt
Download as CSV file: xf-hs1620-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HAM-STD HS1-620 AIRFOIL                         
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.8650   0.06537   0.05853  -0.0751   1.0000   0.0748
 -12.500  -0.9302   0.06038   0.05328  -0.0689   0.9999   0.0746
 -12.250  -0.9428   0.05671   0.04933  -0.0679   0.9958   0.0756
 -12.000  -0.9469   0.05300   0.04522  -0.0675   0.9919   0.0772
 -11.750  -0.9432   0.04995   0.04180  -0.0669   0.9874   0.0788
 -11.500  -0.9196   0.04909   0.04097  -0.0675   0.9841   0.0801
 -11.250  -0.8971   0.04775   0.03953  -0.0684   0.9812   0.0818
 -11.000  -0.8827   0.04586   0.03739  -0.0679   0.9765   0.0838
 -10.750  -0.8644   0.04397   0.03520  -0.0680   0.9724   0.0860
 -10.500  -0.8357   0.04328   0.03455  -0.0692   0.9695   0.0877
 -10.250  -0.8139   0.04222   0.03338  -0.0692   0.9651   0.0899
 -10.000  -0.7930   0.04069   0.03153  -0.0692   0.9605   0.0927
  -9.750  -0.7638   0.03994   0.03079  -0.0703   0.9572   0.0948
  -9.500  -0.7354   0.03921   0.03000  -0.0712   0.9539   0.0974
  -9.250  -0.7148   0.03814   0.02872  -0.0706   0.9480   0.1004
  -9.000  -0.6858   0.03742   0.02796  -0.0716   0.9444   0.1030
  -8.750  -0.6531   0.03681   0.02730  -0.0732   0.9418   0.1062
  -8.500  -0.6329   0.03595   0.02622  -0.0722   0.9351   0.1098
  -8.250  -0.6034   0.03542   0.02574  -0.0731   0.9308   0.1127
  -8.000  -0.5704   0.03484   0.02508  -0.0746   0.9278   0.1167
  -7.750  -0.5471   0.03421   0.02431  -0.0741   0.9220   0.1206
  -7.500  -0.5200   0.03382   0.02397  -0.0743   0.9165   0.1239
  -7.250  -0.4866   0.03322   0.02322  -0.0758   0.9133   0.1290
  -7.000  -0.4590   0.03280   0.02281  -0.0761   0.9082   0.1329
  -6.750  -0.4344   0.03245   0.02244  -0.0757   0.9014   0.1372
  -6.500  -0.4016   0.03194   0.02181  -0.0769   0.8980   0.1427
  -6.250  -0.3660   0.03155   0.02145  -0.0787   0.8955   0.1477
  -6.000  -0.3490   0.03131   0.02110  -0.0768   0.8858   0.1527
  -5.750  -0.3156   0.03092   0.02074  -0.0780   0.8820   0.1578
  -5.500  -0.2794   0.03048   0.02024  -0.0798   0.8796   0.1644
  -5.250  -0.2626   0.03039   0.02011  -0.0779   0.8698   0.1691
  -5.000  -0.2294   0.03005   0.01980  -0.0791   0.8659   0.1750
  -4.750  -0.1929   0.02958   0.01921  -0.0808   0.8633   0.1825
  -4.500  -0.1749   0.02957   0.01927  -0.0791   0.8537   0.1870
  -4.250  -0.1420   0.02923   0.01889  -0.0801   0.8497   0.1941
  -4.000  -0.1061   0.02875   0.01838  -0.0817   0.8470   0.2009
  -3.750  -0.0849   0.02873   0.01839  -0.0806   0.8385   0.2065
  -3.500  -0.0538   0.02845   0.01803  -0.0812   0.8337   0.2141
  -3.250  -0.0189   0.02795   0.01759  -0.0826   0.8307   0.2209
  -3.000   0.0181   0.02743   0.01706  -0.0843   0.8285   0.2290
  -2.750   0.0363   0.02758   0.01716  -0.0825   0.8183   0.2352
  -2.500   0.0696   0.02708   0.01675  -0.0836   0.8145   0.2425
  -2.250   0.1067   0.02654   0.01620  -0.0852   0.8118   0.2515
  -2.000   0.1333   0.02637   0.01607  -0.0850   0.8052   0.2588
  -1.750   0.1619   0.02607   0.01583  -0.0851   0.7984   0.2672
  -1.500   0.2011   0.02538   0.01513  -0.0869   0.7943   0.2775
  -1.250   0.2358   0.02473   0.01458  -0.0880   0.7877   0.2878
  -1.000   0.2659   0.02433   0.01416  -0.0881   0.7778   0.2989
  -0.750   0.3129   0.02326   0.01319  -0.0913   0.7725   0.3150
  -0.500   0.3354   0.02315   0.01315  -0.0901   0.7602   0.3299
  -0.250   0.3785   0.02238   0.01251  -0.0929   0.7540   0.3593
   0.000   0.4063   0.02210   0.01245  -0.0929   0.7451   0.4050
   0.500   0.4797   0.02044   0.01207  -0.0953   0.7313   0.7457
   0.750   0.5036   0.02066   0.01259  -0.0934   0.7197   0.8539
   1.000   0.5739   0.02046   0.01232  -0.1014   0.7116   0.9378
   1.250   0.6143   0.02082   0.01264  -0.1040   0.6988   0.9764
   1.500   0.6861   0.02086   0.01253  -0.1131   0.6874   0.9992
   1.750   0.7038   0.02091   0.01249  -0.1111   0.6745   1.0000
   2.000   0.7227   0.02093   0.01241  -0.1093   0.6620   1.0000
   2.250   0.7488   0.02088   0.01221  -0.1089   0.6492   1.0000
   2.500   0.7570   0.02106   0.01233  -0.1049   0.6350   1.0000
   2.750   0.7738   0.02116   0.01233  -0.1026   0.6207   1.0000
   3.000   0.7929   0.02125   0.01230  -0.1007   0.6054   1.0000
   3.250   0.8049   0.02146   0.01243  -0.0975   0.5886   1.0000
   3.500   0.8177   0.02171   0.01259  -0.0944   0.5705   1.0000
   3.750   0.8323   0.02197   0.01275  -0.0918   0.5513   1.0000
   4.000   0.8474   0.02226   0.01291  -0.0892   0.5307   1.0000
   4.250   0.8628   0.02260   0.01309  -0.0868   0.5093   1.0000
   4.500   0.8777   0.02300   0.01332  -0.0844   0.4879   1.0000
   4.750   0.8924   0.02346   0.01362  -0.0819   0.4673   1.0000
   5.000   0.9070   0.02398   0.01398  -0.0796   0.4481   1.0000
   5.250   0.9218   0.02453   0.01439  -0.0774   0.4306   1.0000
   5.500   0.9372   0.02510   0.01484  -0.0753   0.4151   1.0000
   5.750   0.9532   0.02569   0.01529  -0.0734   0.4017   1.0000
   6.000   0.9696   0.02629   0.01578  -0.0716   0.3895   1.0000
   6.250   0.9870   0.02688   0.01629  -0.0700   0.3791   1.0000
   6.500   1.0043   0.02750   0.01681  -0.0685   0.3693   1.0000
   6.750   1.0228   0.02810   0.01734  -0.0672   0.3609   1.0000
   7.000   1.0410   0.02871   0.01790  -0.0658   0.3529   1.0000
   7.250   1.0602   0.02934   0.01840  -0.0647   0.3461   1.0000
   7.500   1.0787   0.02996   0.01905  -0.0635   0.3390   1.0000
   7.750   1.0972   0.03061   0.01966  -0.0623   0.3325   1.0000
   8.000   1.1180   0.03124   0.02016  -0.0615   0.3269   1.0000
   8.250   1.1362   0.03191   0.02088  -0.0604   0.3210   1.0000
   8.500   1.1544   0.03260   0.02157  -0.0592   0.3152   1.0000
   8.750   1.1739   0.03327   0.02218  -0.0583   0.3101   1.0000
   9.000   1.1939   0.03396   0.02284  -0.0575   0.3053   1.0000
   9.250   1.2106   0.03472   0.02367  -0.0562   0.3001   1.0000
   9.500   1.2280   0.03548   0.02444  -0.0551   0.2952   1.0000
   9.750   1.2474   0.03619   0.02510  -0.0543   0.2908   1.0000
  10.000   1.2662   0.03696   0.02586  -0.0534   0.2866   1.0000
  10.250   1.2805   0.03786   0.02687  -0.0520   0.2820   1.0000
  10.500   1.2960   0.03873   0.02778  -0.0507   0.2775   1.0000
  10.750   1.3127   0.03956   0.02860  -0.0496   0.2735   1.0000
  11.000   1.3329   0.04031   0.02929  -0.0490   0.2698   1.0000
  11.250   1.3433   0.04144   0.03058  -0.0473   0.2657   1.0000
  11.500   1.3552   0.04251   0.03174  -0.0457   0.2615   1.0000
  11.750   1.3687   0.04351   0.03277  -0.0444   0.2576   1.0000
  12.000   1.3857   0.04437   0.03359  -0.0436   0.2542   1.0000
  12.250   1.3972   0.04555   0.03487  -0.0421   0.2507   1.0000
  12.500   1.4041   0.04697   0.03644  -0.0403   0.2466   1.0000
  12.750   1.4133   0.04827   0.03782  -0.0388   0.2428   1.0000
  13.000   1.4250   0.04942   0.03899  -0.0375   0.2395   1.0000
  13.250   1.4421   0.05030   0.03981  -0.0369   0.2364   1.0000
  13.500   1.4422   0.05228   0.04202  -0.0348   0.2327   1.0000
  13.750   1.4460   0.05410   0.04398  -0.0331   0.2290   1.0000
  14.000   1.4527   0.05571   0.04567  -0.0318   0.2256   1.0000
  14.250   1.4629   0.05705   0.04703  -0.0308   0.2225   1.0000
  14.500   1.4733   0.05845   0.04845  -0.0299   0.2196   1.0000
  14.750   1.4681   0.06120   0.05144  -0.0281   0.2161   1.0000
  15.000   1.4675   0.06364   0.05402  -0.0268   0.2127   1.0000
  15.250   1.4713   0.06567   0.05614  -0.0259   0.2095   1.0000
  15.500   1.4809   0.06716   0.05763  -0.0252   0.2067   1.0000
  15.750   1.4815   0.06962   0.06019  -0.0243   0.2038   1.0000
  16.000   1.4686   0.07358   0.06441  -0.0232   0.2004   1.0000
  16.250   1.4625   0.07691   0.06789  -0.0225   0.1971   1.0000
  16.500   1.4648   0.07933   0.07036  -0.0221   0.1941   1.0000
  16.750   1.4772   0.08059   0.07159  -0.0219   0.1916   1.0000
  17.000   1.4549   0.08609   0.07737  -0.0217   0.1884   1.0000
  17.250   1.4292   0.09232   0.08385  -0.0220   0.1849   1.0000
  17.500   1.4195   0.09661   0.08826  -0.0225   0.1817   1.0000
  17.750   1.4293   0.09825   0.08990  -0.0226   0.1791   1.0000
  18.000   1.4198   0.10264   0.09440  -0.0234   0.1763   1.0000
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