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HAM-STD HS1-620 AIRFOIL (hs1620-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: HAM-STD HS1-620 AIRFOIL (hs1620-il)
Reynolds number: 500,000
Max Cl/Cd: 57.26 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hs1620-il-500000-n5.txt
Download as CSV file: xf-hs1620-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -0.8814   0.08850   0.08406  -0.1014   0.9911   0.0385
 -18.000  -0.9192   0.08006   0.07549  -0.1054   0.9899   0.0388
 -17.750  -0.9645   0.07037   0.06563  -0.1103   0.9886   0.0389
 -17.500  -1.0097   0.05991   0.05494  -0.1163   0.9872   0.0391
 -17.250  -1.0405   0.05119   0.04599  -0.1222   0.9857   0.0393
 -17.000  -1.0555   0.04545   0.04007  -0.1260   0.9843   0.0396
 -16.750  -1.0603   0.04144   0.03590  -0.1285   0.9831   0.0399
 -16.500  -1.0589   0.03842   0.03274  -0.1301   0.9820   0.0403
 -16.250  -1.0573   0.03583   0.03004  -0.1309   0.9812   0.0407
 -16.000  -1.0671   0.03391   0.02804  -0.1282   0.9781   0.0410
 -15.750  -1.0709   0.03235   0.02640  -0.1256   0.9753   0.0414
 -15.500  -1.0684   0.03102   0.02500  -0.1236   0.9733   0.0419
 -15.250  -1.0609   0.02985   0.02376  -0.1220   0.9716   0.0425
 -15.000  -1.0517   0.02886   0.02269  -0.1202   0.9704   0.0431
 -14.750  -1.0409   0.02800   0.02175  -0.1184   0.9694   0.0438
 -14.500  -1.0233   0.02721   0.02088  -0.1176   0.9687   0.0446
 -14.250  -1.0279   0.02674   0.02035  -0.1119   0.9639   0.0450
 -14.000  -1.0148   0.02599   0.01957  -0.1100   0.9616   0.0457
 -13.750  -0.9968   0.02533   0.01887  -0.1089   0.9601   0.0464
 -13.500  -0.9756   0.02471   0.01821  -0.1084   0.9590   0.0473
 -13.250  -0.9505   0.02410   0.01754  -0.1085   0.9580   0.0482
 -13.000  -0.9208   0.02347   0.01685  -0.1095   0.9571   0.0493
 -12.750  -0.8893   0.02275   0.01610  -0.1109   0.9564   0.0504
 -12.500  -0.8561   0.02206   0.01539  -0.1127   0.9557   0.0517
 -12.250  -0.8478   0.02171   0.01500  -0.1088   0.9493   0.0526
 -12.000  -0.8224   0.02125   0.01450  -0.1087   0.9475   0.0538
 -11.750  -0.7947   0.02077   0.01398  -0.1091   0.9462   0.0550
 -11.500  -0.7660   0.02025   0.01345  -0.1097   0.9452   0.0563
 -11.250  -0.7357   0.01978   0.01296  -0.1105   0.9443   0.0578
 -11.000  -0.7045   0.01935   0.01249  -0.1115   0.9437   0.0595
 -10.750  -0.6736   0.01889   0.01202  -0.1125   0.9431   0.0611
 -10.500  -0.6416   0.01845   0.01157  -0.1137   0.9426   0.0629
 -10.250  -0.6089   0.01804   0.01113  -0.1150   0.9420   0.0647
 -10.000  -0.5999   0.01792   0.01099  -0.1110   0.9358   0.0660
  -9.750  -0.5734   0.01755   0.01062  -0.1109   0.9334   0.0680
  -9.500  -0.5428   0.01719   0.01026  -0.1116   0.9320   0.0703
  -9.250  -0.5106   0.01684   0.00988  -0.1127   0.9309   0.0724
  -9.000  -0.4779   0.01644   0.00950  -0.1139   0.9299   0.0749
  -8.750  -0.4443   0.01609   0.00913  -0.1152   0.9288   0.0776
  -8.500  -0.4101   0.01570   0.00875  -0.1168   0.9278   0.0805
  -8.250  -0.3755   0.01535   0.00840  -0.1183   0.9268   0.0837
  -8.000  -0.3646   0.01529   0.00833  -0.1146   0.9195   0.0857
  -7.750  -0.3355   0.01497   0.00803  -0.1149   0.9168   0.0889
  -7.500  -0.3025   0.01467   0.00773  -0.1161   0.9148   0.0926
  -7.250  -0.2681   0.01432   0.00740  -0.1175   0.9130   0.0964
  -7.000  -0.2325   0.01401   0.00708  -0.1193   0.9114   0.1006
  -6.750  -0.2207   0.01391   0.00701  -0.1157   0.9023   0.1036
  -6.500  -0.1891   0.01364   0.00675  -0.1165   0.8988   0.1082
  -6.250  -0.1532   0.01334   0.00647  -0.1183   0.8963   0.1130
  -6.000  -0.1358   0.01322   0.00637  -0.1159   0.8872   0.1172
  -5.750  -0.1022   0.01295   0.00611  -0.1171   0.8821   0.1221
  -5.500  -0.0704   0.01272   0.00589  -0.1179   0.8762   0.1276
  -5.250  -0.0416   0.01252   0.00569  -0.1181   0.8673   0.1325
  -5.000  -0.0053   0.01228   0.00546  -0.1199   0.8602   0.1385
  -4.750   0.0286   0.01208   0.00523  -0.1212   0.8492   0.1438
  -4.500   0.0652   0.01187   0.00499  -0.1231   0.8344   0.1500
  -4.250   0.1010   0.01173   0.00475  -0.1247   0.8147   0.1554
  -4.000   0.1325   0.01167   0.00459  -0.1254   0.7937   0.1613
  -3.750   0.1611   0.01168   0.00450  -0.1255   0.7750   0.1663
  -3.500   0.1886   0.01168   0.00444  -0.1254   0.7595   0.1714
  -3.250   0.2157   0.01170   0.00441  -0.1251   0.7456   0.1767
  -2.750   0.2689   0.01174   0.00435  -0.1245   0.7204   0.1861
  -2.500   0.2949   0.01178   0.00434  -0.1240   0.7077   0.1913
  -2.250   0.3202   0.01184   0.00433  -0.1234   0.6937   0.1960
  -2.000   0.3464   0.01186   0.00432  -0.1230   0.6833   0.2007
  -1.750   0.3724   0.01187   0.00432  -0.1226   0.6739   0.2060
  -1.500   0.3985   0.01190   0.00433  -0.1222   0.6650   0.2111
  -1.250   0.4242   0.01194   0.00433  -0.1217   0.6548   0.2154
  -1.000   0.4493   0.01196   0.00434  -0.1211   0.6454   0.2211
  -0.750   0.4748   0.01198   0.00437  -0.1206   0.6360   0.2271
  -0.500   0.4991   0.01205   0.00439  -0.1197   0.6264   0.2325
  -0.250   0.5237   0.01209   0.00442  -0.1190   0.6154   0.2377
   0.000   0.5464   0.01215   0.00447  -0.1179   0.6037   0.2444
   0.250   0.5680   0.01223   0.00452  -0.1165   0.5903   0.2510
   0.750   0.6067   0.01242   0.00467  -0.1127   0.5626   0.2661
   1.000   0.6244   0.01259   0.00479  -0.1105   0.5442   0.2759
   1.250   0.6422   0.01279   0.00495  -0.1084   0.5224   0.2899
   1.500   0.6605   0.01302   0.00515  -0.1065   0.4984   0.3125
   1.750   0.6789   0.01321   0.00540  -0.1047   0.4736   0.3670
   2.000   0.6967   0.01335   0.00570  -0.1029   0.4483   0.4577
   2.250   0.7142   0.01334   0.00608  -0.1011   0.4228   0.6175
   2.500   0.7323   0.01355   0.00643  -0.0992   0.3978   0.7025
   2.750   0.7508   0.01375   0.00677  -0.0974   0.3776   0.7707
   3.000   0.7651   0.01390   0.00720  -0.0942   0.3614   0.8772
   3.250   0.7836   0.01426   0.00759  -0.0920   0.3467   0.9501
   3.500   0.8146   0.01465   0.00791  -0.0929   0.3335   0.9875
   3.750   0.8420   0.01499   0.00817  -0.0932   0.3237   1.0000
   4.000   0.8621   0.01526   0.00839  -0.0918   0.3162   1.0000
   4.250   0.8810   0.01560   0.00866  -0.0902   0.3090   1.0000
   4.500   0.9019   0.01588   0.00892  -0.0890   0.3032   1.0000
   4.750   0.9227   0.01620   0.00919  -0.0878   0.2970   1.0000
   5.000   0.9427   0.01656   0.00950  -0.0865   0.2913   1.0000
   5.250   0.9638   0.01689   0.00981  -0.0854   0.2868   1.0000
   5.500   0.9854   0.01721   0.01011  -0.0844   0.2822   1.0000
   5.750   1.0060   0.01758   0.01044  -0.0832   0.2772   1.0000
   6.000   1.0258   0.01799   0.01082  -0.0820   0.2726   1.0000
   6.250   1.0468   0.01836   0.01117  -0.0810   0.2688   1.0000
   6.500   1.0683   0.01871   0.01152  -0.0800   0.2650   1.0000
   6.750   1.0887   0.01912   0.01192  -0.0790   0.2608   1.0000
   7.000   1.1085   0.01957   0.01235  -0.0778   0.2569   1.0000
   7.250   1.1274   0.02007   0.01281  -0.0765   0.2530   1.0000
   7.500   1.1488   0.02045   0.01321  -0.0757   0.2499   1.0000
   7.750   1.1691   0.02089   0.01365  -0.0747   0.2464   1.0000
   8.000   1.1887   0.02137   0.01413  -0.0736   0.2429   1.0000
   8.250   1.2073   0.02191   0.01465  -0.0723   0.2391   1.0000
   8.500   1.2255   0.02248   0.01521  -0.0711   0.2357   1.0000
   8.750   1.2457   0.02296   0.01571  -0.0702   0.2328   1.0000
   9.000   1.2651   0.02349   0.01625  -0.0692   0.2296   1.0000
   9.250   1.2836   0.02407   0.01684  -0.0680   0.2261   1.0000
   9.500   1.3004   0.02476   0.01751  -0.0667   0.2225   1.0000
   9.750   1.3178   0.02543   0.01818  -0.0655   0.2194   1.0000
  10.000   1.3371   0.02601   0.01879  -0.0646   0.2164   1.0000
  10.250   1.3549   0.02667   0.01947  -0.0636   0.2129   1.0000
  10.500   1.3711   0.02744   0.02024  -0.0623   0.2094   1.0000
  10.750   1.3864   0.02828   0.02106  -0.0610   0.2061   1.0000
  11.000   1.4037   0.02901   0.02183  -0.0600   0.2034   1.0000
  11.250   1.4209   0.02977   0.02262  -0.0590   0.2005   1.0000
  11.500   1.4371   0.03060   0.02347  -0.0579   0.1972   1.0000
  11.750   1.4515   0.03157   0.02445  -0.0567   0.1940   1.0000
  12.000   1.4650   0.03262   0.02549  -0.0554   0.1909   1.0000
  12.250   1.4817   0.03346   0.02639  -0.0545   0.1883   1.0000
  12.500   1.4968   0.03443   0.02739  -0.0535   0.1852   1.0000
  12.750   1.5107   0.03550   0.02848  -0.0524   0.1819   1.0000
  13.000   1.5222   0.03677   0.02975  -0.0512   0.1787   1.0000
  13.250   1.5361   0.03788   0.03089  -0.0502   0.1759   1.0000
  13.500   1.5500   0.03901   0.03207  -0.0493   0.1730   1.0000
  13.750   1.5625   0.04027   0.03336  -0.0483   0.1698   1.0000
  14.000   1.5730   0.04172   0.03482  -0.0472   0.1667   1.0000
  14.250   1.5837   0.04316   0.03629  -0.0462   0.1639   1.0000
  14.500   1.5964   0.04445   0.03763  -0.0454   0.1611   1.0000
  14.750   1.6073   0.04592   0.03914  -0.0445   0.1582   1.0000
  15.000   1.6163   0.04757   0.04081  -0.0436   0.1552   1.0000
  15.250   1.6235   0.04940   0.04266  -0.0426   0.1525   1.0000
  15.500   1.6349   0.05086   0.04419  -0.0419   0.1500   1.0000
  15.750   1.6438   0.05258   0.04596  -0.0412   0.1472   1.0000
  16.000   1.6512   0.05446   0.04788  -0.0404   0.1443   1.0000
  16.250   1.6556   0.05667   0.05011  -0.0395   0.1417   1.0000
  16.500   1.6642   0.05847   0.05197  -0.0389   0.1394   1.0000
  16.750   1.6710   0.06048   0.05404  -0.0383   0.1367   1.0000
  17.000   1.6761   0.06265   0.05626  -0.0377   0.1339   1.0000
  17.250   1.6778   0.06524   0.05888  -0.0371   0.1314   1.0000
  17.500   1.6825   0.06752   0.06122  -0.0366   0.1291   1.0000
  17.750   1.6871   0.06984   0.06361  -0.0362   0.1267   1.0000
  18.000   1.6895   0.07242   0.06625  -0.0358   0.1242   1.0000
  18.250   1.6889   0.07538   0.06925  -0.0355   0.1217   1.0000
  18.500   1.6886   0.07833   0.07226  -0.0352   0.1196   1.0000
  18.750   1.6916   0.08090   0.07492  -0.0351   0.1175   1.0000
  19.000   1.6905   0.08401   0.07808  -0.0350   0.1150   1.0000
  19.250   1.6873   0.08739   0.08152  -0.0351   0.1128   1.0000
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