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HAM-STD HS1-620 AIRFOIL (hs1620-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: HAM-STD HS1-620 AIRFOIL (hs1620-il)
Reynolds number: 1,000,000
Max Cl/Cd: 70.65 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hs1620-il-1000000-n5.txt
Download as CSV file: xf-hs1620-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -0.8873   0.09298   0.08932  -0.1104   0.9913   0.0316
 -19.250  -0.9593   0.08010   0.07624  -0.1168   0.9901   0.0316
 -19.000  -1.1191   0.05379   0.04941  -0.1312   0.9880   0.0311
 -18.750  -1.1547   0.04460   0.03997  -0.1377   0.9865   0.0313
 -18.500  -1.1649   0.03982   0.03505  -0.1408   0.9853   0.0315
 -18.250  -1.1660   0.03645   0.03156  -0.1427   0.9843   0.0318
 -18.000  -1.1615   0.03383   0.02884  -0.1442   0.9835   0.0321
 -17.750  -1.1535   0.03173   0.02665  -0.1451   0.9827   0.0323
 -17.500  -1.1463   0.02978   0.02462  -0.1455   0.9820   0.0327
 -17.250  -1.1376   0.02812   0.02289  -0.1455   0.9812   0.0331
 -17.000  -1.1334   0.02683   0.02154  -0.1438   0.9792   0.0335
 -16.750  -1.1296   0.02576   0.02041  -0.1415   0.9764   0.0339
 -16.500  -1.1204   0.02479   0.01939  -0.1399   0.9746   0.0344
 -16.250  -1.1089   0.02393   0.01847  -0.1383   0.9731   0.0349
 -16.000  -1.0961   0.02315   0.01764  -0.1368   0.9719   0.0354
 -15.750  -1.0823   0.02244   0.01688  -0.1352   0.9708   0.0359
 -15.500  -1.0676   0.02181   0.01619  -0.1336   0.9697   0.0363
 -15.250  -1.0513   0.02114   0.01548  -0.1323   0.9688   0.0369
 -15.000  -1.0360   0.02060   0.01491  -0.1306   0.9673   0.0375
 -14.750  -1.0221   0.02016   0.01444  -0.1285   0.9652   0.0380
 -14.500  -1.0040   0.01972   0.01397  -0.1271   0.9635   0.0387
 -14.250  -0.9833   0.01929   0.01351  -0.1262   0.9622   0.0393
 -14.000  -0.9609   0.01888   0.01307  -0.1256   0.9611   0.0400
 -13.750  -0.9371   0.01846   0.01262  -0.1252   0.9601   0.0407
 -13.500  -0.9124   0.01797   0.01211  -0.1251   0.9589   0.0416
 -13.250  -0.8859   0.01749   0.01162  -0.1252   0.9575   0.0426
 -13.000  -0.8585   0.01705   0.01115  -0.1254   0.9561   0.0436
 -12.750  -0.8332   0.01669   0.01076  -0.1252   0.9541   0.0444
 -12.500  -0.8108   0.01639   0.01043  -0.1243   0.9515   0.0451
 -12.250  -0.7866   0.01603   0.01006  -0.1238   0.9495   0.0461
 -12.000  -0.7607   0.01568   0.00970  -0.1237   0.9477   0.0472
 -11.750  -0.7337   0.01536   0.00936  -0.1237   0.9461   0.0485
 -11.500  -0.7057   0.01505   0.00903  -0.1239   0.9444   0.0496
 -11.250  -0.6775   0.01469   0.00866  -0.1242   0.9429   0.0509
 -11.000  -0.6484   0.01436   0.00833  -0.1247   0.9414   0.0523
 -10.750  -0.6225   0.01413   0.00808  -0.1244   0.9395   0.0536
 -10.500  -0.5964   0.01391   0.00785  -0.1241   0.9375   0.0547
 -10.250  -0.5699   0.01363   0.00759  -0.1240   0.9355   0.0565
 -10.000  -0.5423   0.01338   0.00734  -0.1240   0.9335   0.0583
  -9.750  -0.5138   0.01315   0.00709  -0.1242   0.9314   0.0598
  -9.500  -0.4847   0.01287   0.00682  -0.1246   0.9295   0.0617
  -9.250  -0.4546   0.01262   0.00656  -0.1252   0.9277   0.0637
  -9.000  -0.4248   0.01241   0.00634  -0.1257   0.9259   0.0657
  -8.750  -0.3986   0.01220   0.00616  -0.1254   0.9232   0.0680
  -8.500  -0.3712   0.01201   0.00597  -0.1253   0.9202   0.0704
  -8.250  -0.3427   0.01181   0.00578  -0.1255   0.9171   0.0724
  -8.000  -0.3130   0.01158   0.00556  -0.1259   0.9141   0.0753
  -7.750  -0.2818   0.01137   0.00534  -0.1267   0.9113   0.0782
  -7.500  -0.2549   0.01119   0.00519  -0.1265   0.9072   0.0810
  -7.250  -0.2269   0.01103   0.00503  -0.1265   0.9025   0.0840
  -7.000  -0.1970   0.01083   0.00484  -0.1270   0.8978   0.0871
  -6.750  -0.1676   0.01065   0.00467  -0.1273   0.8926   0.0910
  -6.500  -0.1391   0.01049   0.00451  -0.1274   0.8848   0.0943
  -6.250  -0.1091   0.01031   0.00433  -0.1278   0.8769   0.0986
  -6.000  -0.0799   0.01017   0.00417  -0.1281   0.8649   0.1027
  -5.750  -0.0508   0.01004   0.00400  -0.1283   0.8474   0.1074
  -5.500  -0.0232   0.00999   0.00385  -0.1281   0.8215   0.1118
  -5.000   0.0266   0.01009   0.00370  -0.1266   0.7678   0.1209
  -4.750   0.0518   0.01011   0.00366  -0.1260   0.7483   0.1263
  -4.250   0.1046   0.01011   0.00357  -0.1253   0.7189   0.1360
  -4.000   0.1313   0.01012   0.00354  -0.1250   0.7078   0.1409
  -3.750   0.1581   0.01011   0.00351  -0.1247   0.6957   0.1460
  -3.500   0.1848   0.01011   0.00348  -0.1245   0.6847   0.1513
  -3.250   0.2110   0.01013   0.00347  -0.1241   0.6726   0.1558
  -3.000   0.2377   0.01013   0.00345  -0.1238   0.6613   0.1613
  -2.750   0.2636   0.01017   0.00345  -0.1233   0.6500   0.1659
  -2.500   0.2908   0.01017   0.00343  -0.1231   0.6408   0.1704
  -2.250   0.3169   0.01019   0.00344  -0.1227   0.6307   0.1753
  -2.000   0.3436   0.01020   0.00344  -0.1224   0.6223   0.1799
  -1.750   0.3703   0.01023   0.00344  -0.1221   0.6132   0.1838
  -1.500   0.3958   0.01026   0.00346  -0.1216   0.6042   0.1893
  -1.250   0.4216   0.01030   0.00348  -0.1211   0.5926   0.1944
  -1.000   0.4462   0.01038   0.00351  -0.1203   0.5803   0.1977
  -0.750   0.4689   0.01047   0.00356  -0.1192   0.5652   0.2025
  -0.500   0.4907   0.01054   0.00361  -0.1178   0.5502   0.2076
  -0.250   0.5108   0.01067   0.00368  -0.1161   0.5329   0.2122
   0.000   0.5302   0.01087   0.00378  -0.1142   0.5109   0.2157
   0.250   0.5493   0.01110   0.00391  -0.1123   0.4861   0.2214
   0.500   0.5697   0.01134   0.00406  -0.1107   0.4610   0.2265
   0.750   0.5912   0.01159   0.00422  -0.1094   0.4368   0.2315
   1.000   0.6125   0.01189   0.00440  -0.1081   0.4100   0.2355
   1.250   0.6335   0.01221   0.00461  -0.1067   0.3830   0.2422
   1.500   0.6556   0.01249   0.00481  -0.1056   0.3615   0.2491
   2.000   0.7014   0.01295   0.00519  -0.1038   0.3322   0.2670
   2.500   0.7486   0.01332   0.00558  -0.1023   0.3120   0.3048
   2.750   0.7731   0.01338   0.00579  -0.1018   0.3048   0.3699
   3.000   0.7981   0.01337   0.00599  -0.1015   0.2989   0.4513
   3.250   0.8225   0.01315   0.00630  -0.1012   0.2927   0.6424
   3.500   0.8463   0.01322   0.00656  -0.1005   0.2870   0.7131
   3.750   0.8701   0.01325   0.00680  -0.0998   0.2822   0.7795
   4.000   0.8898   0.01326   0.00713  -0.0980   0.2774   0.8859
   4.250   0.9063   0.01344   0.00743  -0.0954   0.2726   0.9560
   4.500   0.9333   0.01367   0.00765  -0.0953   0.2684   0.9854
   4.750   0.9625   0.01386   0.00782  -0.0959   0.2644   1.0000
   5.000   0.9848   0.01411   0.00805  -0.0950   0.2603   1.0000
   5.250   1.0062   0.01441   0.00831  -0.0939   0.2557   1.0000
   5.500   1.0286   0.01469   0.00856  -0.0930   0.2518   1.0000
   5.750   1.0518   0.01494   0.00880  -0.0922   0.2490   1.0000
   6.000   1.0746   0.01521   0.00906  -0.0915   0.2455   1.0000
   6.250   1.0964   0.01554   0.00936  -0.0905   0.2415   1.0000
   6.500   1.1173   0.01590   0.00969  -0.0894   0.2373   1.0000
   6.750   1.1397   0.01620   0.00999  -0.0886   0.2347   1.0000
   7.000   1.1622   0.01651   0.01029  -0.0878   0.2318   1.0000
   7.250   1.1841   0.01684   0.01061  -0.0870   0.2283   1.0000
   7.500   1.2048   0.01724   0.01098  -0.0859   0.2246   1.0000
   7.750   1.2249   0.01766   0.01139  -0.0848   0.2210   1.0000
   8.000   1.2465   0.01802   0.01175  -0.0840   0.2186   1.0000
   8.250   1.2681   0.01839   0.01213  -0.0831   0.2156   1.0000
   8.500   1.2887   0.01881   0.01254  -0.0822   0.2119   1.0000
   8.750   1.3078   0.01931   0.01302  -0.0810   0.2082   1.0000
   9.000   1.3271   0.01981   0.01350  -0.0798   0.2047   1.0000
   9.250   1.3479   0.02024   0.01394  -0.0789   0.2020   1.0000
   9.500   1.3679   0.02071   0.01441  -0.0780   0.1987   1.0000
   9.750   1.3863   0.02126   0.01496  -0.0768   0.1955   1.0000
  10.000   1.4041   0.02187   0.01555  -0.0755   0.1921   1.0000
  10.250   1.4234   0.02240   0.01609  -0.0745   0.1895   1.0000
  10.500   1.4425   0.02295   0.01666  -0.0735   0.1865   1.0000
  10.750   1.4601   0.02359   0.01730  -0.0723   0.1834   1.0000
  11.000   1.4771   0.02428   0.01798  -0.0711   0.1802   1.0000
  11.250   1.4941   0.02498   0.01868  -0.0699   0.1770   1.0000
  11.500   1.5117   0.02566   0.01938  -0.0688   0.1743   1.0000
  11.750   1.5284   0.02639   0.02013  -0.0677   0.1711   1.0000
  12.000   1.5441   0.02720   0.02093  -0.0664   0.1677   1.0000
  12.250   1.5585   0.02811   0.02184  -0.0650   0.1645   1.0000
  12.500   1.5752   0.02888   0.02264  -0.0640   0.1619   1.0000
  12.750   1.5909   0.02975   0.02351  -0.0629   0.1589   1.0000
  13.000   1.6045   0.03077   0.02454  -0.0616   0.1556   1.0000
  13.250   1.6180   0.03180   0.02558  -0.0603   0.1525   1.0000
  13.500   1.6329   0.03278   0.02658  -0.0593   0.1501   1.0000
  13.750   1.6471   0.03380   0.02763  -0.0582   0.1474   1.0000
  14.000   1.6595   0.03499   0.02883  -0.0570   0.1442   1.0000
  14.250   1.6707   0.03628   0.03012  -0.0557   0.1412   1.0000
  14.500   1.6843   0.03739   0.03127  -0.0548   0.1389   1.0000
  14.750   1.6963   0.03866   0.03257  -0.0537   0.1363   1.0000
  15.000   1.7073   0.04003   0.03395  -0.0526   0.1334   1.0000
  15.250   1.7160   0.04161   0.03555  -0.0514   0.1305   1.0000
  15.500   1.7281   0.04293   0.03690  -0.0506   0.1282   1.0000
  15.750   1.7378   0.04448   0.03848  -0.0496   0.1257   1.0000
  16.000   1.7467   0.04610   0.04012  -0.0486   0.1229   1.0000
  16.250   1.7532   0.04796   0.04201  -0.0475   0.1202   1.0000
  16.500   1.7632   0.04951   0.04360  -0.0467   0.1181   1.0000
  16.750   1.7703   0.05137   0.04550  -0.0458   0.1156   1.0000
  17.000   1.7767   0.05329   0.04744  -0.0449   0.1131   1.0000
  17.250   1.7807   0.05549   0.04968  -0.0440   0.1107   1.0000
  17.500   1.7884   0.05734   0.05157  -0.0434   0.1087   1.0000
  17.750   1.7931   0.05953   0.05381  -0.0427   0.1065   1.0000
  18.000   1.7962   0.06187   0.05618  -0.0419   0.1040   1.0000
  18.250   1.7976   0.06441   0.05876  -0.0412   0.1019   1.0000
  18.500   1.8022   0.06666   0.06107  -0.0407   0.1002   1.0000
  18.750   1.8046   0.06916   0.06362  -0.0402   0.0982   1.0000
  19.000   1.8045   0.07196   0.06647  -0.0397   0.0961   1.0000
  19.250   1.8029   0.07496   0.06951  -0.0393   0.0940   1.0000
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