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HAM-STD HS1-620 AIRFOIL (hs1620-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: HAM-STD HS1-620 AIRFOIL (hs1620-il)
Reynolds number: 500,000
Max Cl/Cd: 72.24 at α=2.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-hs1620-il-500000.txt
Download as CSV file: xf-hs1620-il-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -0.8851   0.12299   0.11934  -0.0659   1.0000   0.0433
 -19.250  -0.9376   0.11114   0.10725  -0.0720   1.0000   0.0438
 -19.000  -0.9778   0.10182   0.09774  -0.0765   1.0000   0.0441
 -18.750  -1.0128   0.09369   0.08943  -0.0802   1.0000   0.0444
 -18.500  -1.0449   0.08618   0.08176  -0.0835   1.0000   0.0447
 -18.250  -1.0745   0.07923   0.07464  -0.0865   1.0000   0.0449
 -18.000  -1.0918   0.07463   0.06999  -0.0875   1.0000   0.0452
 -17.750  -1.1088   0.06998   0.06529  -0.0886   1.0000   0.0456
 -17.500  -1.1282   0.06492   0.06015  -0.0901   1.0000   0.0458
 -17.250  -1.1475   0.06000   0.05513  -0.0914   1.0000   0.0461
 -17.000  -1.1657   0.05550   0.05053  -0.0923   1.0000   0.0464
 -16.750  -1.1832   0.05153   0.04646  -0.0923   1.0000   0.0467
 -16.500  -1.1996   0.04811   0.04293  -0.0916   1.0000   0.0470
 -16.250  -1.2154   0.04516   0.03988  -0.0900   1.0000   0.0473
 -16.000  -1.2146   0.04244   0.03704  -0.0908   0.9985   0.0479
 -15.750  -1.2124   0.04017   0.03464  -0.0909   0.9965   0.0484
 -15.500  -1.2098   0.03832   0.03265  -0.0901   0.9947   0.0490
 -15.250  -1.2030   0.03686   0.03101  -0.0894   0.9930   0.0495
 -15.000  -1.2074   0.03529   0.02937  -0.0860   0.9893   0.0500
 -14.750  -1.2029   0.03402   0.02808  -0.0836   0.9861   0.0506
 -14.500  -1.1848   0.03303   0.02705  -0.0833   0.9841   0.0513
 -14.250  -1.1612   0.03216   0.02613  -0.0838   0.9825   0.0522
 -14.000  -1.1336   0.03139   0.02528  -0.0849   0.9814   0.0532
 -13.750  -1.1196   0.03057   0.02435  -0.0830   0.9770   0.0541
 -13.500  -1.0989   0.02968   0.02338  -0.0826   0.9741   0.0550
 -13.250  -1.0748   0.02878   0.02250  -0.0829   0.9721   0.0561
 -13.000  -1.0456   0.02813   0.02182  -0.0839   0.9707   0.0572
 -12.750  -1.0148   0.02752   0.02116  -0.0851   0.9697   0.0585
 -12.500  -0.9821   0.02699   0.02051  -0.0867   0.9689   0.0597
 -12.250  -0.9727   0.02623   0.01974  -0.0835   0.9632   0.0607
 -12.000  -0.9462   0.02559   0.01911  -0.0838   0.9607   0.0620
 -11.750  -0.9153   0.02508   0.01857  -0.0849   0.9591   0.0635
 -11.500  -0.8827   0.02463   0.01803  -0.0862   0.9579   0.0652
 -11.250  -0.8515   0.02396   0.01736  -0.0874   0.9569   0.0668
 -11.000  -0.8177   0.02345   0.01686  -0.0890   0.9561   0.0686
 -10.750  -0.7995   0.02309   0.01646  -0.0873   0.9511   0.0701
 -10.500  -0.7714   0.02272   0.01601  -0.0875   0.9479   0.0718
 -10.250  -0.7408   0.02207   0.01540  -0.0884   0.9460   0.0739
 -10.000  -0.7069   0.02166   0.01498  -0.0899   0.9447   0.0762
  -9.750  -0.6714   0.02131   0.01455  -0.0916   0.9438   0.0784
  -9.500  -0.6371   0.02071   0.01401  -0.0933   0.9429   0.0810
  -9.250  -0.6004   0.02032   0.01361  -0.0953   0.9422   0.0838
  -9.000  -0.5832   0.02005   0.01330  -0.0931   0.9356   0.0860
  -8.750  -0.5519   0.01956   0.01286  -0.0940   0.9330   0.0890
  -8.500  -0.5167   0.01920   0.01246  -0.0956   0.9315   0.0922
  -8.250  -0.4816   0.01871   0.01201  -0.0973   0.9303   0.0957
  -8.000  -0.4448   0.01834   0.01163  -0.0992   0.9293   0.0996
  -7.750  -0.4076   0.01788   0.01119  -0.1013   0.9285   0.1036
  -7.500  -0.3689   0.01748   0.01081  -0.1036   0.9279   0.1081
  -7.250  -0.3298   0.01703   0.01037  -0.1061   0.9274   0.1128
  -7.000  -0.3154   0.01684   0.01021  -0.1031   0.9188   0.1164
  -6.750  -0.2795   0.01646   0.00982  -0.1048   0.9170   0.1214
  -6.500  -0.2419   0.01605   0.00946  -0.1069   0.9159   0.1269
  -6.250  -0.2029   0.01562   0.00904  -0.1092   0.9150   0.1327
  -6.000  -0.1624   0.01522   0.00867  -0.1119   0.9143   0.1389
  -5.750  -0.1209   0.01479   0.00828  -0.1149   0.9137   0.1452
  -5.500  -0.0796   0.01444   0.00794  -0.1177   0.9129   0.1517
  -5.250  -0.0387   0.01402   0.00755  -0.1205   0.9119   0.1582
  -5.000  -0.0233   0.01386   0.00742  -0.1176   0.9021   0.1628
  -4.750   0.0150   0.01351   0.00705  -0.1197   0.8995   0.1688
  -4.500   0.0566   0.01307   0.00667  -0.1226   0.8969   0.1755
  -4.250   0.0781   0.01287   0.00645  -0.1210   0.8863   0.1803
  -4.000   0.1174   0.01245   0.00605  -0.1233   0.8808   0.1867
  -3.750   0.1428   0.01226   0.00587  -0.1226   0.8689   0.1920
  -3.500   0.1833   0.01204   0.00558  -0.1252   0.8613   0.1976
  -3.250   0.2143   0.01176   0.00532  -0.1258   0.8484   0.2039
  -3.000   0.2479   0.01161   0.00514  -0.1270   0.8350   0.2097
  -2.750   0.2825   0.01153   0.00497  -0.1283   0.8212   0.2148
  -2.500   0.3145   0.01138   0.00477  -0.1292   0.8056   0.2213
  -2.250   0.3452   0.01135   0.00467  -0.1297   0.7901   0.2273
  -2.000   0.3734   0.01139   0.00463  -0.1297   0.7765   0.2327
  -1.750   0.4015   0.01136   0.00457  -0.1297   0.7651   0.2387
  -1.500   0.4296   0.01135   0.00452  -0.1298   0.7536   0.2456
  -1.250   0.4563   0.01136   0.00452  -0.1295   0.7427   0.2518
  -1.000   0.4843   0.01140   0.00448  -0.1295   0.7325   0.2585
  -0.750   0.5102   0.01134   0.00448  -0.1291   0.7230   0.2674
  -0.500   0.5373   0.01139   0.00447  -0.1289   0.7130   0.2756
  -0.250   0.5629   0.01134   0.00447  -0.1284   0.7034   0.2870
   0.000   0.5887   0.01135   0.00447  -0.1279   0.6932   0.3008
   0.250   0.6138   0.01128   0.00450  -0.1274   0.6839   0.3266
   0.500   0.6375   0.01105   0.00454  -0.1266   0.6741   0.4097
   0.750   0.6575   0.01043   0.00467  -0.1253   0.6647   0.6350
   1.000   0.6783   0.01026   0.00480  -0.1236   0.6538   0.7375
   1.250   0.6981   0.01018   0.00497  -0.1215   0.6434   0.8169
   1.500   0.7157   0.01024   0.00520  -0.1187   0.6319   0.8935
   1.750   0.7375   0.01044   0.00543  -0.1169   0.6200   0.9386
   2.000   0.7625   0.01073   0.00564  -0.1161   0.6058   0.9646
   2.250   0.7941   0.01108   0.00592  -0.1168   0.5886   0.9822
   2.500   0.8316   0.01154   0.00627  -0.1191   0.5683   0.9927
   2.750   0.8712   0.01206   0.00666  -0.1218   0.5421   0.9989
   3.000   0.8766   0.01231   0.00678  -0.1171   0.5172   1.0000
   3.250   0.8782   0.01258   0.00690  -0.1115   0.4911   1.0000
   3.500   0.8811   0.01295   0.00710  -0.1063   0.4641   1.0000
   3.750   0.8901   0.01336   0.00736  -0.1025   0.4366   1.0000
   4.000   0.9005   0.01385   0.00768  -0.0991   0.4102   1.0000
   4.250   0.9130   0.01435   0.00803  -0.0961   0.3876   1.0000
   4.500   0.9285   0.01482   0.00838  -0.0939   0.3694   1.0000
   4.750   0.9456   0.01525   0.00872  -0.0919   0.3555   1.0000
   5.000   0.9624   0.01573   0.00910  -0.0900   0.3443   1.0000
   5.250   0.9820   0.01612   0.00945  -0.0885   0.3351   1.0000
   5.500   0.9992   0.01662   0.00986  -0.0867   0.3264   1.0000
   5.750   1.0204   0.01696   0.01019  -0.0857   0.3200   1.0000
   6.000   1.0393   0.01741   0.01059  -0.0842   0.3135   1.0000
   6.250   1.0569   0.01793   0.01106  -0.0826   0.3071   1.0000
   6.500   1.0791   0.01826   0.01139  -0.0817   0.3024   1.0000
   6.750   1.0989   0.01869   0.01181  -0.0805   0.2973   1.0000
   7.000   1.1169   0.01922   0.01229  -0.0790   0.2923   1.0000
   7.250   1.1356   0.01974   0.01278  -0.0777   0.2875   1.0000
   7.500   1.1574   0.02010   0.01317  -0.0769   0.2836   1.0000
   7.750   1.1772   0.02056   0.01363  -0.0758   0.2793   1.0000
   8.000   1.1951   0.02113   0.01416  -0.0744   0.2752   1.0000
   8.250   1.2113   0.02180   0.01478  -0.0728   0.2704   1.0000
   8.500   1.2330   0.02218   0.01522  -0.0720   0.2673   1.0000
   8.750   1.2530   0.02266   0.01571  -0.0711   0.2638   1.0000
   9.000   1.2713   0.02323   0.01628  -0.0699   0.2600   1.0000
   9.250   1.2879   0.02391   0.01693  -0.0684   0.2560   1.0000
   9.500   1.3050   0.02459   0.01760  -0.0671   0.2521   1.0000
   9.750   1.3248   0.02511   0.01816  -0.0662   0.2491   1.0000
  10.000   1.3435   0.02570   0.01878  -0.0652   0.2455   1.0000
  10.250   1.3607   0.02638   0.01946  -0.0640   0.2419   1.0000
  10.500   1.3753   0.02723   0.02027  -0.0625   0.2381   1.0000
  10.750   1.3921   0.02796   0.02103  -0.0614   0.2349   1.0000
  11.000   1.4107   0.02859   0.02172  -0.0605   0.2319   1.0000
  11.250   1.4281   0.02932   0.02247  -0.0595   0.2287   1.0000
  11.500   1.4432   0.03019   0.02334  -0.0582   0.2253   1.0000
  11.750   1.4564   0.03121   0.02433  -0.0568   0.2216   1.0000
  12.000   1.4725   0.03206   0.02523  -0.0557   0.2187   1.0000
  12.250   1.4894   0.03287   0.02610  -0.0549   0.2158   1.0000
  12.500   1.5050   0.03377   0.02703  -0.0539   0.2125   1.0000
  12.750   1.5180   0.03488   0.02813  -0.0527   0.2092   1.0000
  13.000   1.5286   0.03614   0.02936  -0.0512   0.2055   1.0000
  13.250   1.5447   0.03708   0.03038  -0.0504   0.2029   1.0000
  13.500   1.5597   0.03810   0.03147  -0.0496   0.1998   1.0000
  13.750   1.5727   0.03929   0.03268  -0.0486   0.1965   1.0000
  14.000   1.5829   0.04071   0.03409  -0.0474   0.1933   1.0000
  14.250   1.5938   0.04208   0.03548  -0.0463   0.1901   1.0000
  14.500   1.6077   0.04327   0.03675  -0.0456   0.1873   1.0000
  14.750   1.6200   0.04458   0.03811  -0.0448   0.1842   1.0000
  15.000   1.6292   0.04617   0.03971  -0.0438   0.1812   1.0000
  15.250   1.6360   0.04794   0.04146  -0.0426   0.1779   1.0000
  15.500   1.6477   0.04937   0.04298  -0.0419   0.1754   1.0000
  15.750   1.6589   0.05086   0.04454  -0.0412   0.1724   1.0000
  16.000   1.6671   0.05264   0.04635  -0.0405   0.1694   1.0000
  16.250   1.6727   0.05464   0.04836  -0.0395   0.1665   1.0000
  16.500   1.6792   0.05659   0.05035  -0.0387   0.1638   1.0000
  16.750   1.6888   0.05830   0.05215  -0.0382   0.1610   1.0000
  17.000   1.6955   0.06029   0.05420  -0.0376   0.1581   1.0000
  17.250   1.6994   0.06257   0.05649  -0.0370   0.1553   1.0000
  17.500   1.7008   0.06507   0.05900  -0.0362   0.1524   1.0000
  17.750   1.7086   0.06705   0.06109  -0.0359   0.1500   1.0000
  18.000   1.7136   0.06934   0.06345  -0.0355   0.1472   1.0000
  18.250   1.7158   0.07191   0.06606  -0.0351   0.1446   1.0000
  18.500   1.7139   0.07491   0.06906  -0.0346   0.1419   1.0000
  18.750   1.7180   0.07732   0.07156  -0.0344   0.1395   1.0000
  19.000   1.7202   0.07998   0.07432  -0.0343   0.1370   1.0000
  19.250   1.7207   0.08285   0.07724  -0.0342   0.1344   1.0000
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