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HAM-STD HS1-708 AIRFOIL (hs1708-il) Xfoil prediction polar at RE=50,000 Ncrit=9


Details Polar file
Airfoil: HAM-STD HS1-708 AIRFOIL (hs1708-il)
Reynolds number: 50,000
Max Cl/Cd: 42.8 at α=7.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-hs1708-il-50000.txt
Download as CSV file: xf-hs1708-il-50000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HAM-STD HS1-708 AIRFOIL                         
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.050 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.250  -0.3524   0.11525   0.10876  -0.0266   1.0000   0.1495
  -8.000  -0.3739   0.11582   0.10947  -0.0239   1.0000   0.1506
  -7.750  -0.3959   0.11644   0.11023  -0.0220   1.0000   0.1512
  -7.500  -0.3768   0.10984   0.10362  -0.0194   1.0000   0.1559
  -7.250  -0.3831   0.10803   0.10188  -0.0170   1.0000   0.1596
  -7.000  -0.3936   0.10690   0.10084  -0.0160   1.0000   0.1633
  -6.750  -0.4080   0.10691   0.10096  -0.0182   1.0000   0.1658
  -6.500  -0.4062   0.10296   0.09706  -0.0164   1.0000   0.1681
  -6.250  -0.4015   0.09955   0.09368  -0.0135   1.0000   0.1738
  -6.000  -0.4045   0.09836   0.09253  -0.0174   1.0000   0.1802
  -5.500  -0.3964   0.09182   0.08606  -0.0158   1.0000   0.1930
  -5.250  -0.3903   0.08856   0.08280  -0.0179   1.0000   0.1988
  -5.000  -0.3732   0.08647   0.08064  -0.0260   1.0000   0.2108
  -4.750  -0.3717   0.08202   0.07627  -0.0200   1.0000   0.2151
  -4.500  -0.3553   0.07871   0.07291  -0.0243   1.0000   0.2274
  -4.250  -0.3415   0.07531   0.06950  -0.0256   1.0000   0.2423
  -4.000  -0.3279   0.07192   0.06610  -0.0259   1.0000   0.2588
  -3.750  -0.3021   0.06870   0.06276  -0.0314   1.0000   0.2844
  -3.500  -0.2935   0.06532   0.05943  -0.0284   1.0000   0.3060
  -3.250  -0.2738   0.06218   0.05624  -0.0301   1.0000   0.3446
  -2.500  -0.2579   0.05413   0.04837  -0.0161   1.0000   0.4983
  -2.250  -0.2506   0.05154   0.04582  -0.0117   1.0000   0.5546
  -2.000  -0.0027   0.04163   0.03307  -0.0782   1.0000   0.2293
  -1.750   0.0339   0.03972   0.03072  -0.0812   1.0000   0.2327
  -1.500   0.0713   0.03808   0.02857  -0.0841   1.0000   0.2359
  -1.250   0.1021   0.03707   0.02729  -0.0857   1.0000   0.2501
  -1.000   0.1346   0.03607   0.02594  -0.0874   1.0000   0.2586
  -0.750   0.1640   0.03547   0.02510  -0.0885   1.0000   0.2751
  -0.500   0.1931   0.03501   0.02445  -0.0895   1.0000   0.2931
  -0.250   0.2224   0.03474   0.02393  -0.0906   1.0000   0.3125
   0.000   0.2495   0.03458   0.02367  -0.0912   1.0000   0.3378
   0.250   0.2773   0.03454   0.02352  -0.0918   1.0000   0.3638
   0.500   0.3050   0.03461   0.02359  -0.0925   1.0000   0.3979
   0.750   0.3339   0.03470   0.02386  -0.0935   1.0000   0.4409
   1.000   0.3676   0.03461   0.02438  -0.0955   1.0000   0.5289
   1.250   0.3728   0.03410   0.02469  -0.0922   1.0000   1.0000
   1.500   0.3945   0.03520   0.02538  -0.0923   1.0000   1.0000
   1.750   0.4141   0.03637   0.02629  -0.0923   1.0000   1.0000
   2.000   0.4464   0.03777   0.02748  -0.0949   0.9943   1.0000
   2.250   0.5026   0.03930   0.02883  -0.1016   0.9742   1.0000
   2.500   0.5482   0.04056   0.02999  -0.1062   0.9540   1.0000
   2.750   0.5939   0.04169   0.03107  -0.1104   0.9339   1.0000
   3.000   0.6420   0.04272   0.03208  -0.1148   0.9146   1.0000
   3.250   0.6768   0.04354   0.03294  -0.1166   0.8925   1.0000
   3.500   0.7261   0.04419   0.03365  -0.1205   0.8729   1.0000
   3.750   0.7572   0.04483   0.03436  -0.1212   0.8495   1.0000
   4.000   0.8058   0.04500   0.03466  -0.1242   0.8296   1.0000
   4.250   0.8361   0.04538   0.03514  -0.1243   0.8055   1.0000
   4.500   0.8856   0.04494   0.03487  -0.1264   0.7861   1.0000
   4.750   0.9128   0.04512   0.03520  -0.1257   0.7615   1.0000
   5.000   0.9611   0.04411   0.03439  -0.1269   0.7428   1.0000
   5.250   0.9884   0.04398   0.03442  -0.1256   0.7191   1.0000
   5.500   1.0356   0.04232   0.03302  -0.1258   0.7008   1.0000
   5.750   1.0902   0.03988   0.03084  -0.1264   0.6841   1.0000
   6.000   1.1174   0.03928   0.03046  -0.1245   0.6605   1.0000
   6.250   1.1749   0.03626   0.02772  -0.1248   0.6418   1.0000
   6.500   1.2167   0.03428   0.02595  -0.1236   0.6152   1.0000
   6.750   1.2603   0.03145   0.02312  -0.1214   0.5760   1.0000
   7.000   1.2901   0.03041   0.02191  -0.1187   0.5311   1.0000
   7.250   1.3117   0.03065   0.02205  -0.1160   0.4892   1.0000
   7.500   1.3270   0.03130   0.02257  -0.1127   0.4460   1.0000
   7.750   1.3365   0.03226   0.02336  -0.1088   0.3986   1.0000
   8.000   1.3395   0.03373   0.02446  -0.1040   0.3413   1.0000
   8.250   1.3369   0.03578   0.02605  -0.0987   0.2800   1.0000
   8.500   1.3426   0.03800   0.02780  -0.0949   0.2321   1.0000
   8.750   1.3584   0.04020   0.02971  -0.0927   0.2002   1.0000
   9.000   1.3761   0.04231   0.03181  -0.0911   0.1779   1.0000
   9.250   1.4099   0.04504   0.03439  -0.0916   0.1615   1.0000
   9.500   1.4340   0.04791   0.03754  -0.0908   0.1507   1.0000
   9.750   1.4528   0.05079   0.04064  -0.0895   0.1414   1.0000
  10.000   1.4829   0.05422   0.04397  -0.0900   0.1332   1.0000
  10.250   1.4879   0.05779   0.04822  -0.0869   0.1306   1.0000
  10.500   1.4900   0.06159   0.05257  -0.0837   0.1279   1.0000
  10.750   1.4918   0.06517   0.05656  -0.0808   0.1246   1.0000
  11.000   1.5084   0.06909   0.06046  -0.0801   0.1194   1.0000
  11.250   1.4924   0.07298   0.06485  -0.0756   0.1186   1.0000
  11.500   1.4743   0.07709   0.06937  -0.0714   0.1183   1.0000
  11.750   1.4527   0.08120   0.07379  -0.0672   0.1184   1.0000
  12.000   1.4296   0.08570   0.07856  -0.0638   0.1187   1.0000
  12.250   1.4055   0.09066   0.08376  -0.0614   0.1191   1.0000
  12.500   1.3819   0.09614   0.08944  -0.0599   0.1196   1.0000
  12.750   1.2627   0.11056   0.10426  -0.0649   0.1311   1.0000
  13.000   1.2371   0.11942   0.11318  -0.0682   0.1326   1.0000
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