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HAM-STD HS1-620 AIRFOIL (hs1620-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: HAM-STD HS1-620 AIRFOIL (hs1620-il)
Reynolds number: 200,000
Max Cl/Cd: 59.4 at α=3.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-hs1620-il-200000.txt
Download as CSV file: xf-hs1620-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.9131   0.07006   0.06491  -0.0855   1.0000   0.0714
 -14.250  -0.9724   0.06324   0.05784  -0.0846   1.0000   0.0712
 -14.000  -1.0223   0.05899   0.05337  -0.0801   1.0000   0.0712
 -13.750  -1.0684   0.05630   0.05049  -0.0726   1.0000   0.0712
 -13.500  -1.1045   0.05324   0.04713  -0.0661   1.0000   0.0715
 -13.250  -1.1271   0.05027   0.04381  -0.0610   1.0000   0.0720
 -13.000  -1.1150   0.04916   0.04281  -0.0593   1.0000   0.0728
 -12.750  -1.1059   0.04827   0.04195  -0.0571   1.0000   0.0736
 -12.500  -1.0993   0.04719   0.04082  -0.0547   1.0000   0.0746
 -12.250  -1.0941   0.04589   0.03941  -0.0522   1.0000   0.0757
 -12.000  -1.0919   0.04416   0.03743  -0.0494   1.0000   0.0769
 -11.750  -1.0836   0.04198   0.03474  -0.0480   0.9985   0.0785
 -11.500  -1.0464   0.04118   0.03411  -0.0507   0.9950   0.0800
 -11.250  -1.0115   0.04045   0.03334  -0.0531   0.9916   0.0818
 -11.000  -0.9844   0.03920   0.03188  -0.0541   0.9866   0.0838
 -10.750  -0.9553   0.03783   0.03020  -0.0556   0.9830   0.0861
 -10.500  -0.9171   0.03748   0.02999  -0.0583   0.9808   0.0881
 -10.250  -0.8914   0.03656   0.02897  -0.0586   0.9739   0.0902
 -10.000  -0.8588   0.03554   0.02760  -0.0603   0.9704   0.0930
  -9.750  -0.8208   0.03494   0.02713  -0.0630   0.9684   0.0953
  -9.500  -0.7973   0.03431   0.02650  -0.0626   0.9610   0.0977
  -9.250  -0.7636   0.03358   0.02549  -0.0643   0.9577   0.1009
  -9.000  -0.7256   0.03296   0.02497  -0.0668   0.9558   0.1037
  -8.750  -0.7014   0.03247   0.02448  -0.0664   0.9481   0.1065
  -8.500  -0.6663   0.03184   0.02358  -0.0682   0.9445   0.1104
  -8.250  -0.6275   0.03134   0.02324  -0.0708   0.9424   0.1137
  -8.000  -0.6027   0.03094   0.02280  -0.0705   0.9354   0.1172
  -7.750  -0.5697   0.03035   0.02211  -0.0718   0.9313   0.1213
  -7.500  -0.5314   0.03000   0.02184  -0.0741   0.9288   0.1255
  -7.250  -0.4912   0.02949   0.02116  -0.0767   0.9270   0.1308
  -7.000  -0.4708   0.02917   0.02096  -0.0755   0.9178   0.1342
  -6.750  -0.4336   0.02880   0.02053  -0.0775   0.9147   0.1398
  -6.500  -0.3947   0.02831   0.02007  -0.0799   0.9127   0.1450
  -6.250  -0.3705   0.02815   0.01992  -0.0793   0.9052   0.1498
  -6.000  -0.3369   0.02769   0.01939  -0.0805   0.9007   0.1556
  -5.750  -0.2980   0.02733   0.01911  -0.0828   0.8982   0.1615
  -5.500  -0.2575   0.02684   0.01853  -0.0853   0.8966   0.1686
  -5.250  -0.2388   0.02677   0.01855  -0.0837   0.8870   0.1731
  -5.000  -0.2016   0.02643   0.01814  -0.0855   0.8837   0.1804
  -4.750  -0.1622   0.02586   0.01764  -0.0878   0.8817   0.1870
  -4.500  -0.1215   0.02546   0.01722  -0.0903   0.8801   0.1948
  -4.250  -0.1042   0.02540   0.01713  -0.0883   0.8700   0.2002
  -4.000  -0.0666   0.02492   0.01674  -0.0903   0.8671   0.2073
  -3.750  -0.0261   0.02447   0.01619  -0.0926   0.8652   0.2153
  -3.500   0.0151   0.02368   0.01551  -0.0952   0.8639   0.2231
  -3.250   0.0333   0.02373   0.01556  -0.0933   0.8540   0.2292
  -3.000   0.0726   0.02302   0.01481  -0.0954   0.8511   0.2372
  -2.750   0.1156   0.02207   0.01395  -0.0981   0.8493   0.2459
  -2.500   0.1622   0.02119   0.01300  -0.1014   0.8477   0.2550
  -2.250   0.2103   0.02006   0.01199  -0.1052   0.8464   0.2651
  -2.000   0.2286   0.01991   0.01185  -0.1031   0.8354   0.2723
  -1.750   0.2753   0.01896   0.01094  -0.1066   0.8323   0.2828
  -1.500   0.3296   0.01804   0.01005  -0.1118   0.8297   0.2957
  -1.250   0.3568   0.01766   0.00975  -0.1115   0.8203   0.3062
  -1.000   0.4020   0.01709   0.00921  -0.1150   0.8149   0.3210
  -0.750   0.4528   0.01635   0.00859  -0.1198   0.8106   0.3417
  -0.500   0.4768   0.01614   0.00851  -0.1190   0.7999   0.3642
  -0.250   0.5190   0.01540   0.00811  -0.1221   0.7933   0.4343
   0.000   0.5381   0.01450   0.00827  -0.1200   0.7836   0.6992
   0.250   0.5687   0.01419   0.00841  -0.1191   0.7749   0.8573
   0.500   0.6079   0.01440   0.00865  -0.1205   0.7646   0.9296
   0.750   0.6590   0.01459   0.00872  -0.1249   0.7546   0.9629
   1.000   0.7126   0.01493   0.00898  -0.1301   0.7427   0.9795
   1.250   0.7751   0.01511   0.00899  -0.1373   0.7312   0.9894
   1.500   0.8262   0.01542   0.00925  -0.1423   0.7170   0.9981
   1.750   0.8530   0.01546   0.00919  -0.1423   0.7045   1.0000
   2.000   0.8729   0.01543   0.00903  -0.1407   0.6917   1.0000
   2.250   0.8842   0.01548   0.00903  -0.1373   0.6777   1.0000
   2.500   0.9010   0.01552   0.00897  -0.1350   0.6640   1.0000
   2.750   0.9178   0.01558   0.00890  -0.1326   0.6493   1.0000
   3.000   0.9275   0.01568   0.00896  -0.1287   0.6329   1.0000
   3.250   0.9382   0.01580   0.00899  -0.1250   0.6156   1.0000
   3.500   0.9474   0.01595   0.00904  -0.1210   0.5966   1.0000
   3.750   0.9540   0.01614   0.00912  -0.1164   0.5755   1.0000
   4.000   0.9559   0.01639   0.00924  -0.1108   0.5522   1.0000
   4.250   0.9581   0.01674   0.00942  -0.1054   0.5264   1.0000
   4.500   0.9621   0.01721   0.00971  -0.1004   0.4982   1.0000
   4.750   0.9678   0.01777   0.01007  -0.0960   0.4713   1.0000
   5.000   0.9767   0.01839   0.01048  -0.0924   0.4483   1.0000
   5.250   0.9885   0.01900   0.01093  -0.0894   0.4291   1.0000
   5.500   1.0028   0.01958   0.01139  -0.0870   0.4129   1.0000
   5.750   1.0186   0.02016   0.01184  -0.0849   0.3995   1.0000
   6.000   1.0350   0.02076   0.01231  -0.0830   0.3879   1.0000
   6.250   1.0536   0.02128   0.01278  -0.0815   0.3778   1.0000
   6.500   1.0723   0.02186   0.01324  -0.0801   0.3688   1.0000
   6.750   1.0924   0.02239   0.01372  -0.0789   0.3607   1.0000
   7.000   1.1115   0.02292   0.01421  -0.0776   0.3530   1.0000
   7.250   1.1354   0.02351   0.01464  -0.0773   0.3459   1.0000
   7.500   1.1534   0.02402   0.01521  -0.0758   0.3396   1.0000
   7.750   1.1729   0.02456   0.01573  -0.0746   0.3334   1.0000
   8.000   1.1995   0.02514   0.01615  -0.0748   0.3272   1.0000
   8.250   1.2173   0.02569   0.01677  -0.0734   0.3221   1.0000
   8.500   1.2359   0.02626   0.01736  -0.0721   0.3166   1.0000
   8.750   1.2571   0.02683   0.01788  -0.0714   0.3114   1.0000
   9.000   1.2842   0.02742   0.01838  -0.0717   0.3063   1.0000
   9.250   1.2992   0.02804   0.01910  -0.0698   0.3017   1.0000
   9.500   1.3169   0.02866   0.01974  -0.0685   0.2970   1.0000
   9.750   1.3374   0.02926   0.02030  -0.0677   0.2925   1.0000
  10.000   1.3657   0.02988   0.02084  -0.0683   0.2877   1.0000
  10.250   1.3776   0.03061   0.02169  -0.0661   0.2838   1.0000
  10.500   1.3928   0.03131   0.02244  -0.0645   0.2794   1.0000
  10.750   1.4104   0.03197   0.02309  -0.0633   0.2753   1.0000
  11.000   1.4433   0.03254   0.02351  -0.0647   0.2705   1.0000
  11.250   1.4494   0.03343   0.02457  -0.0617   0.2672   1.0000
  11.500   1.4607   0.03427   0.02551  -0.0597   0.2632   1.0000
  11.750   1.4752   0.03504   0.02631  -0.0582   0.2593   1.0000
  12.000   1.4939   0.03574   0.02697  -0.0574   0.2557   1.0000
  12.250   1.5164   0.03651   0.02771  -0.0572   0.2518   1.0000
  12.500   1.5223   0.03759   0.02895  -0.0545   0.2484   1.0000
  12.750   1.5319   0.03858   0.03003  -0.0526   0.2446   1.0000
  13.000   1.5454   0.03944   0.03090  -0.0511   0.2411   1.0000
  13.250   1.5667   0.04012   0.03151  -0.0508   0.2376   1.0000
  13.500   1.5772   0.04128   0.03277  -0.0492   0.2342   1.0000
  13.750   1.5807   0.04263   0.03427  -0.0467   0.2308   1.0000
  14.000   1.5884   0.04382   0.03554  -0.0449   0.2273   1.0000
  14.250   1.6007   0.04481   0.03653  -0.0436   0.2240   1.0000
  14.500   1.6274   0.04534   0.03692  -0.0440   0.2203   1.0000
  14.750   1.6220   0.04728   0.03910  -0.0410   0.2175   1.0000
  15.000   1.6234   0.04901   0.04097  -0.0389   0.2142   1.0000
  15.250   1.6305   0.05043   0.04245  -0.0374   0.2109   1.0000
  15.500   1.6425   0.05153   0.04353  -0.0365   0.2079   1.0000
  15.750   1.6595   0.05250   0.04447  -0.0360   0.2046   1.0000
  16.000   1.6524   0.05503   0.04722  -0.0337   0.2017   1.0000
  16.250   1.6528   0.05712   0.04945  -0.0321   0.1985   1.0000
  16.500   1.6593   0.05875   0.05112  -0.0311   0.1954   1.0000
  16.750   1.6734   0.05980   0.05210  -0.0306   0.1925   1.0000
  17.000   1.6775   0.06180   0.05420  -0.0295   0.1895   1.0000
  17.250   1.6687   0.06493   0.05754  -0.0280   0.1866   1.0000
  17.500   1.6679   0.06741   0.06013  -0.0271   0.1836   1.0000
  17.750   1.6751   0.06912   0.06185  -0.0265   0.1807   1.0000
  18.000   1.6980   0.06937   0.06195  -0.0264   0.1777   1.0000
  18.250   1.6802   0.07368   0.06654  -0.0253   0.1752   1.0000
  18.500   1.6691   0.07750   0.07055  -0.0246   0.1723   1.0000
  18.750   1.6684   0.08021   0.07335  -0.0243   0.1695   1.0000
  19.000   1.6788   0.08165   0.07475  -0.0242   0.1668   1.0000
  19.250   1.6897   0.08307   0.07615  -0.0240   0.1641   1.0000
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