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HAM-STD HS1-620 AIRFOIL (hs1620-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: HAM-STD HS1-620 AIRFOIL (hs1620-il)
Reynolds number: 200,000
Max Cl/Cd: 51.25 at α=2.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hs1620-il-200000-n5.txt
Download as CSV file: xf-hs1620-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.8294   0.09653   0.09126  -0.0720   1.0000   0.0520
 -16.000  -0.9118   0.08071   0.07511  -0.0796   1.0000   0.0523
 -15.750  -0.9567   0.07059   0.06473  -0.0850   0.9996   0.0526
 -15.500  -0.9837   0.06253   0.05642  -0.0904   0.9982   0.0531
 -15.250  -1.0023   0.05652   0.05017  -0.0940   0.9964   0.0536
 -15.000  -1.0141   0.05184   0.04525  -0.0965   0.9943   0.0541
 -14.750  -1.0215   0.04836   0.04157  -0.0976   0.9926   0.0547
 -14.500  -1.0261   0.04601   0.03916  -0.0966   0.9900   0.0552
 -14.250  -1.0287   0.04404   0.03710  -0.0951   0.9870   0.0558
 -14.000  -1.0296   0.04237   0.03534  -0.0933   0.9842   0.0564
 -13.750  -1.0265   0.04093   0.03379  -0.0915   0.9818   0.0572
 -13.500  -1.0190   0.03959   0.03233  -0.0897   0.9789   0.0581
 -13.250  -1.0099   0.03829   0.03088  -0.0880   0.9750   0.0591
 -13.000  -0.9936   0.03704   0.02948  -0.0874   0.9723   0.0602
 -12.750  -0.9720   0.03602   0.02844  -0.0876   0.9702   0.0612
 -12.500  -0.9469   0.03507   0.02743  -0.0884   0.9686   0.0624
 -12.250  -0.9347   0.03419   0.02647  -0.0863   0.9638   0.0636
 -12.000  -0.9137   0.03328   0.02542  -0.0859   0.9607   0.0652
 -11.750  -0.8892   0.03241   0.02450  -0.0862   0.9584   0.0665
 -11.500  -0.8615   0.03163   0.02370  -0.0870   0.9566   0.0679
 -11.250  -0.8319   0.03088   0.02286  -0.0881   0.9553   0.0697
 -11.000  -0.8191   0.03026   0.02214  -0.0856   0.9495   0.0713
 -10.750  -0.7939   0.02957   0.02143  -0.0857   0.9465   0.0729
 -10.500  -0.7651   0.02895   0.02078  -0.0865   0.9443   0.0748
 -10.250  -0.7341   0.02831   0.02006  -0.0876   0.9427   0.0771
 -10.000  -0.7020   0.02767   0.01936  -0.0890   0.9414   0.0793
  -9.750  -0.6889   0.02725   0.01895  -0.0863   0.9345   0.0810
  -9.500  -0.6607   0.02674   0.01838  -0.0867   0.9316   0.0835
  -9.250  -0.6294   0.02618   0.01776  -0.0878   0.9294   0.0862
  -9.000  -0.5963   0.02564   0.01722  -0.0892   0.9278   0.0888
  -8.500  -0.5496   0.02481   0.01632  -0.0878   0.9178   0.0943
  -8.250  -0.5187   0.02436   0.01587  -0.0886   0.9152   0.0975
  -7.750  -0.4502   0.02341   0.01489  -0.0916   0.9118   0.1050
  -7.500  -0.4352   0.02319   0.01464  -0.0890   0.9027   0.1082
  -7.250  -0.4036   0.02276   0.01420  -0.0899   0.8996   0.1122
  -7.000  -0.3696   0.02234   0.01378  -0.0913   0.8975   0.1168
  -6.750  -0.3344   0.02191   0.01333  -0.0929   0.8959   0.1215
  -6.500  -0.3193   0.02177   0.01322  -0.0903   0.8861   0.1252
  -6.250  -0.2864   0.02138   0.01278  -0.0913   0.8829   0.1305
  -6.000  -0.2518   0.02095   0.01239  -0.0927   0.8807   0.1355
  -5.750  -0.2313   0.02080   0.01221  -0.0912   0.8722   0.1404
  -5.500  -0.2015   0.02047   0.01192  -0.0916   0.8677   0.1454
  -5.250  -0.1678   0.02009   0.01151  -0.0927   0.8649   0.1515
  -5.000  -0.1403   0.01982   0.01126  -0.0926   0.8589   0.1566
  -4.750  -0.1140   0.01962   0.01107  -0.0922   0.8517   0.1620
  -4.500  -0.0794   0.01925   0.01067  -0.0935   0.8483   0.1683
  -4.250  -0.0419   0.01883   0.01028  -0.0954   0.8459   0.1744
  -4.000  -0.0195   0.01877   0.01019  -0.0942   0.8360   0.1799
  -3.750   0.0165   0.01839   0.00983  -0.0958   0.8320   0.1857
  -3.500   0.0566   0.01798   0.00942  -0.0983   0.8290   0.1925
  -3.250   0.0859   0.01782   0.00921  -0.0985   0.8207   0.1982
  -3.000   0.1257   0.01737   0.00881  -0.1009   0.8146   0.2046
  -2.750   0.1715   0.01693   0.00832  -0.1046   0.8080   0.2122
  -2.500   0.2098   0.01662   0.00798  -0.1067   0.7974   0.2186
  -2.250   0.2594   0.01624   0.00758  -0.1114   0.7889   0.2265
  -2.000   0.2963   0.01607   0.00734  -0.1132   0.7775   0.2335
  -1.750   0.3341   0.01583   0.00709  -0.1154   0.7662   0.2407
  -1.500   0.3708   0.01567   0.00688  -0.1172   0.7537   0.2488
  -1.250   0.4003   0.01564   0.00678  -0.1175   0.7408   0.2558
  -1.000   0.4333   0.01551   0.00665  -0.1186   0.7307   0.2643
  -0.750   0.4593   0.01549   0.00663  -0.1182   0.7198   0.2730
  -0.500   0.4901   0.01543   0.00655  -0.1189   0.7101   0.2833
  -0.250   0.5148   0.01540   0.00657  -0.1182   0.6998   0.2959
   0.000   0.5440   0.01534   0.00653  -0.1185   0.6899   0.3139
   0.250   0.5670   0.01527   0.00658  -0.1176   0.6789   0.3421
   0.500   0.5931   0.01508   0.00659  -0.1173   0.6685   0.4087
   0.750   0.6127   0.01470   0.00673  -0.1157   0.6575   0.5427
   1.000   0.6341   0.01444   0.00689  -0.1141   0.6471   0.6841
   1.250   0.6532   0.01439   0.00708  -0.1119   0.6349   0.7590
   1.500   0.6742   0.01445   0.00733  -0.1098   0.6225   0.8377
   1.750   0.7022   0.01468   0.00759  -0.1093   0.6080   0.9077
   2.000   0.7347   0.01498   0.00786  -0.1101   0.5919   0.9499
   2.250   0.7702   0.01536   0.00815  -0.1117   0.5733   0.9788
   2.500   0.8104   0.01582   0.00847  -0.1145   0.5498   0.9961
   2.750   0.8251   0.01610   0.00861  -0.1119   0.5279   1.0000
   3.000   0.8286   0.01632   0.00869  -0.1068   0.5068   1.0000
   3.250   0.8345   0.01662   0.00884  -0.1023   0.4847   1.0000
   3.500   0.8422   0.01700   0.00906  -0.0982   0.4620   1.0000
   3.750   0.8515   0.01743   0.00934  -0.0946   0.4397   1.0000
   4.000   0.8624   0.01790   0.00966  -0.0913   0.4190   1.0000
   4.250   0.8745   0.01839   0.01002  -0.0884   0.4007   1.0000
   4.500   0.8875   0.01892   0.01042  -0.0857   0.3849   1.0000
   4.750   0.9026   0.01941   0.01081  -0.0834   0.3706   1.0000
   5.000   0.9182   0.01991   0.01122  -0.0813   0.3590   1.0000
   5.250   0.9338   0.02045   0.01167  -0.0793   0.3486   1.0000
   5.500   0.9513   0.02094   0.01210  -0.0776   0.3402   1.0000
   5.750   0.9685   0.02145   0.01256  -0.0759   0.3322   1.0000
   6.000   0.9853   0.02201   0.01304  -0.0742   0.3253   1.0000
   6.250   1.0045   0.02248   0.01350  -0.0729   0.3186   1.0000
   6.500   1.0219   0.02304   0.01401  -0.0714   0.3124   1.0000
   6.750   1.0388   0.02365   0.01454  -0.0698   0.3071   1.0000
   7.000   1.0588   0.02411   0.01503  -0.0687   0.3019   1.0000
   7.250   1.0773   0.02465   0.01555  -0.0674   0.2966   1.0000
   7.500   1.0944   0.02528   0.01613  -0.0660   0.2918   1.0000
   7.750   1.1121   0.02589   0.01671  -0.0646   0.2875   1.0000
   8.000   1.1318   0.02640   0.01726  -0.0637   0.2830   1.0000
   8.250   1.1500   0.02700   0.01786  -0.0625   0.2785   1.0000
   8.500   1.1669   0.02767   0.01850  -0.0611   0.2743   1.0000
   8.750   1.1832   0.02840   0.01918  -0.0597   0.2706   1.0000
   9.000   1.2024   0.02896   0.01980  -0.0588   0.2668   1.0000
   9.250   1.2202   0.02960   0.02048  -0.0576   0.2627   1.0000
   9.500   1.2368   0.03031   0.02120  -0.0564   0.2588   1.0000
   9.750   1.2526   0.03109   0.02196  -0.0551   0.2553   1.0000
  10.000   1.2688   0.03187   0.02273  -0.0539   0.2519   1.0000
  10.250   1.2863   0.03258   0.02351  -0.0528   0.2482   1.0000
  10.500   1.3027   0.03336   0.02433  -0.0517   0.2445   1.0000
  10.750   1.3178   0.03422   0.02520  -0.0505   0.2410   1.0000
  11.000   1.3317   0.03516   0.02613  -0.0492   0.2377   1.0000
  11.250   1.3471   0.03605   0.02705  -0.0481   0.2344   1.0000
  11.500   1.3627   0.03693   0.02802  -0.0470   0.2309   1.0000
  11.750   1.3769   0.03791   0.02904  -0.0459   0.2273   1.0000
  12.000   1.3900   0.03898   0.03013  -0.0447   0.2239   1.0000
  12.250   1.4021   0.04014   0.03127  -0.0434   0.2209   1.0000
  12.500   1.4165   0.04117   0.03238  -0.0425   0.2177   1.0000
  12.750   1.4299   0.04229   0.03359  -0.0415   0.2143   1.0000
  13.000   1.4420   0.04351   0.03486  -0.0404   0.2110   1.0000
  13.250   1.4529   0.04483   0.03619  -0.0393   0.2080   1.0000
  13.500   1.4634   0.04620   0.03755  -0.0382   0.2052   1.0000
  13.750   1.4758   0.04748   0.03896  -0.0373   0.2019   1.0000
  14.000   1.4867   0.04890   0.04047  -0.0364   0.1986   1.0000
  14.250   1.4963   0.05043   0.04204  -0.0355   0.1955   1.0000
  14.500   1.5046   0.05209   0.04371  -0.0345   0.1926   1.0000
  14.750   1.5137   0.05371   0.04538  -0.0337   0.1898   1.0000
  15.000   1.5229   0.05537   0.04716  -0.0329   0.1865   1.0000
  15.250   1.5308   0.05716   0.04902  -0.0322   0.1833   1.0000
  15.500   1.5370   0.05912   0.05103  -0.0314   0.1804   1.0000
  15.750   1.5427   0.06113   0.05303  -0.0306   0.1777   1.0000
  16.000   1.5498   0.06311   0.05514  -0.0301   0.1748   1.0000
  16.250   1.5558   0.06521   0.05734  -0.0295   0.1716   1.0000
  16.500   1.5600   0.06751   0.05971  -0.0290   0.1687   1.0000
  16.750   1.5633   0.06989   0.06212  -0.0285   0.1661   1.0000
  17.000   1.5670   0.07228   0.06457  -0.0281   0.1635   1.0000
  17.250   1.5702   0.07479   0.06722  -0.0278   0.1605   1.0000
  17.500   1.5722   0.07747   0.06999  -0.0276   0.1576   1.0000
  17.750   1.5731   0.08028   0.07285  -0.0275   0.1550   1.0000
  18.000   1.5745   0.08299   0.07557  -0.0274   0.1527   1.0000
  18.250   1.5744   0.08607   0.07881  -0.0275   0.1500   1.0000
  18.500   1.5734   0.08924   0.08211  -0.0277   0.1471   1.0000
  18.750   1.5718   0.09250   0.08544  -0.0280   0.1445   1.0000
  19.000   1.5703   0.09573   0.08870  -0.0284   0.1422   1.0000
  19.250   1.5684   0.09910   0.09216  -0.0289   0.1398   1.0000
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