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HAM-STD HS1-620 AIRFOIL (hs1620-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: HAM-STD HS1-620 AIRFOIL (hs1620-il)
Reynolds number: 1,000,000
Max Cl/Cd: 76.25 at α=2.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-hs1620-il-1000000.txt
Download as CSV file: xf-hs1620-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.250  -1.0184   0.08674   0.08307  -0.0971   0.9946   0.0368
 -19.000  -1.0706   0.07602   0.07219  -0.1030   0.9942   0.0369
 -18.750  -1.1363   0.06264   0.05857  -0.1107   0.9936   0.0369
 -18.500  -1.1827   0.05117   0.04683  -0.1187   0.9931   0.0370
 -18.250  -1.2029   0.04431   0.03979  -0.1239   0.9925   0.0373
 -18.000  -1.2225   0.04011   0.03548  -0.1239   0.9896   0.0375
 -17.750  -1.2294   0.03696   0.03222  -0.1243   0.9877   0.0378
 -17.500  -1.2302   0.03452   0.02970  -0.1243   0.9862   0.0382
 -17.250  -1.2263   0.03263   0.02772  -0.1240   0.9849   0.0386
 -17.000  -1.2191   0.03108   0.02610  -0.1235   0.9839   0.0390
 -16.750  -1.2096   0.02978   0.02472  -0.1228   0.9831   0.0395
 -16.500  -1.1971   0.02869   0.02355  -0.1221   0.9823   0.0399
 -16.250  -1.1816   0.02778   0.02256  -0.1216   0.9817   0.0403
 -16.000  -1.1731   0.02670   0.02142  -0.1200   0.9810   0.0409
 -15.750  -1.2036   0.02611   0.02076  -0.1097   0.9747   0.0410
 -15.500  -1.1900   0.02523   0.01985  -0.1081   0.9732   0.0417
 -15.250  -1.1695   0.02450   0.01910  -0.1076   0.9722   0.0425
 -15.000  -1.1473   0.02390   0.01846  -0.1073   0.9714   0.0432
 -14.750  -1.1234   0.02337   0.01789  -0.1072   0.9708   0.0439
 -14.500  -1.0985   0.02290   0.01736  -0.1072   0.9702   0.0446
 -14.250  -1.0730   0.02228   0.01669  -0.1075   0.9697   0.0453
 -14.000  -1.0441   0.02154   0.01595  -0.1085   0.9692   0.0464
 -13.750  -1.0312   0.02107   0.01545  -0.1058   0.9646   0.0471
 -13.500  -1.0038   0.02053   0.01489  -0.1061   0.9624   0.0480
 -13.250  -0.9731   0.02007   0.01438  -0.1070   0.9612   0.0490
 -13.000  -0.9432   0.01958   0.01386  -0.1078   0.9603   0.0500
 -12.750  -0.9149   0.01900   0.01328  -0.1084   0.9595   0.0513
 -12.500  -0.8846   0.01855   0.01283  -0.1093   0.9588   0.0525
 -12.250  -0.8533   0.01817   0.01242  -0.1103   0.9583   0.0537
 -12.000  -0.8217   0.01784   0.01204  -0.1113   0.9579   0.0547
 -11.750  -0.7909   0.01730   0.01152  -0.1123   0.9575   0.0564
 -11.500  -0.7577   0.01690   0.01112  -0.1138   0.9572   0.0580
 -11.250  -0.7229   0.01656   0.01076  -0.1154   0.9570   0.0595
 -11.000  -0.6893   0.01612   0.01031  -0.1169   0.9567   0.0613
 -10.750  -0.6564   0.01572   0.00993  -0.1182   0.9564   0.0631
 -10.500  -0.6232   0.01541   0.00960  -0.1195   0.9560   0.0649
 -10.250  -0.5904   0.01505   0.00923  -0.1208   0.9556   0.0669
 -10.000  -0.5836   0.01498   0.00917  -0.1162   0.9491   0.0684
  -9.750  -0.5512   0.01466   0.00885  -0.1173   0.9480   0.0706
  -9.500  -0.5182   0.01432   0.00850  -0.1185   0.9471   0.0728
  -9.250  -0.4853   0.01395   0.00816  -0.1197   0.9462   0.0754
  -9.000  -0.4518   0.01366   0.00786  -0.1210   0.9454   0.0780
  -8.750  -0.4188   0.01330   0.00752  -0.1222   0.9446   0.0811
  -8.500  -0.3848   0.01299   0.00722  -0.1236   0.9438   0.0842
  -8.250  -0.3505   0.01266   0.00690  -0.1250   0.9429   0.0874
  -8.000  -0.3163   0.01235   0.00660  -0.1264   0.9419   0.0910
  -7.750  -0.2912   0.01218   0.00644  -0.1258   0.9385   0.0942
  -7.500  -0.2653   0.01194   0.00623  -0.1253   0.9350   0.0980
  -7.250  -0.2337   0.01170   0.00599  -0.1261   0.9327   0.1016
  -7.000  -0.2009   0.01138   0.00571  -0.1272   0.9307   0.1065
  -6.750  -0.1671   0.01112   0.00546  -0.1285   0.9287   0.1110
  -6.500  -0.1335   0.01085   0.00522  -0.1297   0.9266   0.1165
  -6.250  -0.1091   0.01072   0.00509  -0.1289   0.9215   0.1207
  -6.000  -0.0795   0.01048   0.00489  -0.1292   0.9173   0.1264
  -5.750  -0.0471   0.01026   0.00466  -0.1301   0.9135   0.1314
  -5.500  -0.0174   0.01004   0.00449  -0.1304   0.9080   0.1374
  -5.250   0.0103   0.00988   0.00432  -0.1302   0.8998   0.1419
  -5.000   0.0404   0.00967   0.00413  -0.1307   0.8917   0.1480
  -4.750   0.0703   0.00953   0.00397  -0.1310   0.8806   0.1530
  -4.500   0.0989   0.00939   0.00381  -0.1310   0.8663   0.1585
  -4.250   0.1287   0.00929   0.00368  -0.1313   0.8491   0.1639
  -3.750   0.1845   0.00928   0.00349  -0.1311   0.8058   0.1739
  -3.500   0.2109   0.00934   0.00346  -0.1307   0.7859   0.1788
  -3.250   0.2371   0.00943   0.00345  -0.1302   0.7681   0.1824
  -2.750   0.2899   0.00948   0.00343  -0.1295   0.7394   0.1935
  -2.500   0.3166   0.00954   0.00344  -0.1291   0.7280   0.1972
  -2.250   0.3435   0.00955   0.00342  -0.1289   0.7172   0.2025
  -2.000   0.3703   0.00956   0.00342  -0.1286   0.7078   0.2079
  -1.750   0.3977   0.00958   0.00343  -0.1285   0.6988   0.2126
  -1.500   0.4239   0.00967   0.00345  -0.1280   0.6894   0.2157
  -1.250   0.4511   0.00962   0.00343  -0.1279   0.6806   0.2231
  -1.000   0.4764   0.00968   0.00346  -0.1273   0.6708   0.2284
  -0.750   0.5036   0.00970   0.00347  -0.1271   0.6626   0.2331
  -0.500   0.5294   0.00974   0.00349  -0.1266   0.6534   0.2386
  -0.250   0.5549   0.00976   0.00351  -0.1261   0.6446   0.2465
   0.000   0.5802   0.00980   0.00355  -0.1255   0.6342   0.2529
   0.250   0.6042   0.00986   0.00359  -0.1246   0.6240   0.2603
   0.500   0.6283   0.00989   0.00363  -0.1238   0.6129   0.2708
   0.750   0.6490   0.00995   0.00369  -0.1221   0.6016   0.2832
   1.000   0.6677   0.01003   0.00377  -0.1201   0.5876   0.3027
   1.250   0.6885   0.00999   0.00388  -0.1187   0.5723   0.3617
   1.500   0.7085   0.00979   0.00406  -0.1172   0.5555   0.5043
   1.750   0.7283   0.00966   0.00432  -0.1157   0.5348   0.6628
   2.000   0.7472   0.00985   0.00457  -0.1139   0.5092   0.7262
   2.250   0.7656   0.01006   0.00486  -0.1119   0.4810   0.7876
   2.500   0.7816   0.01025   0.00521  -0.1092   0.4530   0.8762
   2.750   0.7944   0.01062   0.00557  -0.1057   0.4259   0.9354
   3.000   0.8128   0.01104   0.00588  -0.1036   0.3989   0.9703
   3.250   0.8394   0.01151   0.00621  -0.1035   0.3727   0.9908
   3.500   0.8746   0.01201   0.00656  -0.1055   0.3504   0.9987
   3.750   0.8955   0.01229   0.00676  -0.1042   0.3370   1.0000
   4.000   0.9125   0.01257   0.00696  -0.1021   0.3259   1.0000
   4.250   0.9327   0.01280   0.00715  -0.1007   0.3181   1.0000
   4.500   0.9520   0.01312   0.00740  -0.0991   0.3093   1.0000
   4.750   0.9743   0.01335   0.00760  -0.0981   0.3036   1.0000
   5.000   0.9963   0.01362   0.00783  -0.0970   0.2978   1.0000
   5.250   1.0165   0.01396   0.00813  -0.0957   0.2911   1.0000
   5.500   1.0388   0.01423   0.00838  -0.0948   0.2865   1.0000
   5.750   1.0616   0.01450   0.00863  -0.0940   0.2825   1.0000
   6.000   1.0833   0.01481   0.00892  -0.0930   0.2778   1.0000
   6.250   1.1037   0.01520   0.00926  -0.0917   0.2721   1.0000
   6.500   1.1261   0.01550   0.00955  -0.0909   0.2687   1.0000
   6.750   1.1487   0.01579   0.00984  -0.0901   0.2655   1.0000
   7.000   1.1703   0.01613   0.01017  -0.0892   0.2616   1.0000
   7.250   1.1908   0.01653   0.01053  -0.0881   0.2571   1.0000
   7.500   1.2104   0.01696   0.01095  -0.0868   0.2527   1.0000
   7.750   1.2332   0.01726   0.01127  -0.0861   0.2504   1.0000
   8.000   1.2548   0.01762   0.01162  -0.0853   0.2471   1.0000
   8.250   1.2754   0.01803   0.01202  -0.0843   0.2435   1.0000
   8.500   1.2947   0.01851   0.01247  -0.0830   0.2391   1.0000
   8.750   1.3139   0.01900   0.01296  -0.0819   0.2356   1.0000
   9.000   1.3357   0.01937   0.01335  -0.0811   0.2329   1.0000
   9.250   1.3563   0.01980   0.01379  -0.0802   0.2297   1.0000
   9.500   1.3757   0.02031   0.01427  -0.0791   0.2261   1.0000
   9.750   1.3929   0.02092   0.01487  -0.0777   0.2221   1.0000
  10.000   1.4117   0.02146   0.01542  -0.0766   0.2193   1.0000
  10.250   1.4324   0.02191   0.01589  -0.0758   0.2167   1.0000
  10.500   1.4518   0.02244   0.01643  -0.0748   0.2135   1.0000
  10.750   1.4692   0.02308   0.01707  -0.0736   0.2101   1.0000
  11.000   1.4842   0.02387   0.01784  -0.0720   0.2062   1.0000
  11.250   1.5035   0.02443   0.01843  -0.0711   0.2038   1.0000
  11.500   1.5226   0.02501   0.01903  -0.0702   0.2009   1.0000
  11.750   1.5393   0.02574   0.01976  -0.0690   0.1976   1.0000
  12.000   1.5546   0.02657   0.02058  -0.0677   0.1940   1.0000
  12.250   1.5692   0.02745   0.02146  -0.0663   0.1906   1.0000
  12.500   1.5872   0.02813   0.02218  -0.0654   0.1881   1.0000
  12.750   1.6039   0.02891   0.02298  -0.0644   0.1851   1.0000
  13.000   1.6181   0.02987   0.02394  -0.0631   0.1818   1.0000
  13.250   1.6297   0.03102   0.02508  -0.0616   0.1780   1.0000
  13.500   1.6466   0.03183   0.02593  -0.0607   0.1757   1.0000
  13.750   1.6617   0.03279   0.02692  -0.0597   0.1731   1.0000
  14.000   1.6753   0.03386   0.02800  -0.0586   0.1699   1.0000
  14.250   1.6859   0.03518   0.02932  -0.0572   0.1665   1.0000
  14.500   1.6988   0.03633   0.03050  -0.0562   0.1638   1.0000
  14.750   1.7131   0.03740   0.03161  -0.0553   0.1614   1.0000
  15.000   1.7252   0.03866   0.03289  -0.0542   0.1584   1.0000
  15.250   1.7349   0.04012   0.03436  -0.0530   0.1552   1.0000
  15.500   1.7437   0.04169   0.03595  -0.0518   0.1522   1.0000
  15.750   1.7572   0.04289   0.03720  -0.0511   0.1499   1.0000
  16.000   1.7674   0.04438   0.03872  -0.0501   0.1471   1.0000
  16.250   1.7755   0.04606   0.04041  -0.0491   0.1440   1.0000
  16.500   1.7809   0.04801   0.04239  -0.0479   0.1410   1.0000
  16.750   1.7927   0.04940   0.04382  -0.0473   0.1388   1.0000
  17.000   1.8004   0.05118   0.04564  -0.0464   0.1362   1.0000
  17.250   1.8062   0.05313   0.04762  -0.0455   0.1334   1.0000
  17.500   1.8081   0.05553   0.05003  -0.0444   0.1304   1.0000
  17.750   1.8179   0.05715   0.05172  -0.0439   0.1285   1.0000
  18.000   1.8233   0.05925   0.05387  -0.0432   0.1260   1.0000
  18.250   1.8268   0.06153   0.05617  -0.0425   0.1235   1.0000
  18.500   1.8250   0.06438   0.05905  -0.0416   0.1207   1.0000
  18.750   1.8312   0.06643   0.06117  -0.0411   0.1189   1.0000
  19.000   1.8347   0.06879   0.06359  -0.0407   0.1167   1.0000
  19.250   1.8351   0.07151   0.06634  -0.0402   0.1144   1.0000
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