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HAM-STD HS1-430 AIRFOIL (hs1430-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: HAM-STD HS1-430 AIRFOIL (hs1430-il)
Reynolds number: 200,000
Max Cl/Cd: 31.02 at α=10.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-hs1430-il-200000.txt
Download as CSV file: xf-hs1430-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HAM-STD HS1-430 AIRFOIL                         
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.3787   0.21132   0.20660  -0.0249   1.0000   0.1332
 -17.500  -0.3733   0.20981   0.20511  -0.0248   1.0000   0.1353
 -16.750  -1.1777   0.07474   0.06806  -0.0682   1.0000   0.1504
 -16.500  -1.1509   0.07511   0.06858  -0.0676   1.0000   0.1516
 -16.250  -1.1254   0.07586   0.06946  -0.0666   1.0000   0.1526
 -16.000  -1.1264   0.07432   0.06793  -0.0652   0.9998   0.1537
 -15.750  -1.1204   0.07151   0.06505  -0.0669   0.9970   0.1553
 -15.500  -1.1374   0.06727   0.06062  -0.0671   0.9939   0.1569
 -15.250  -1.1641   0.06279   0.05584  -0.0661   0.9910   0.1587
 -15.000  -1.1994   0.05853   0.05123  -0.0623   0.9859   0.1603
 -14.750  -1.2346   0.05509   0.04740  -0.0570   0.9804   0.1617
 -14.500  -1.1909   0.05452   0.04696  -0.0606   0.9780   0.1635
 -14.250  -1.1526   0.05440   0.04694  -0.0635   0.9762   0.1650
 -14.000  -1.1421   0.05349   0.04603  -0.0619   0.9697   0.1663
 -13.750  -1.1304   0.05245   0.04493  -0.0610   0.9654   0.1679
 -13.500  -1.1229   0.05113   0.04346  -0.0596   0.9626   0.1699
 -13.250  -1.1378   0.04961   0.04176  -0.0538   0.9545   0.1714
 -13.000  -1.1503   0.04793   0.03976  -0.0484   0.9500   0.1732
 -12.750  -1.1066   0.04734   0.03928  -0.0521   0.9485   0.1750
 -12.500  -1.0914   0.04691   0.03890  -0.0502   0.9402   0.1762
 -12.250  -1.0597   0.04646   0.03849  -0.0516   0.9376   0.1779
 -12.000  -1.0454   0.04587   0.03786  -0.0499   0.9315   0.1797
 -11.750  -1.0280   0.04495   0.03684  -0.0488   0.9271   0.1819
 -11.500  -1.0110   0.04364   0.03528  -0.0479   0.9247   0.1845
 -11.250  -0.9996   0.04276   0.03432  -0.0454   0.9169   0.1861
 -11.000  -0.9602   0.04227   0.03396  -0.0481   0.9150   0.1878
 -10.750  -0.9401   0.04189   0.03361  -0.0470   0.9086   0.1895
 -10.500  -0.9121   0.04129   0.03299  -0.0475   0.9051   0.1917
 -10.250  -0.8811   0.04048   0.03210  -0.0487   0.9033   0.1944
 -10.000  -0.8742   0.03978   0.03126  -0.0451   0.8943   0.1965
  -9.750  -0.8467   0.03872   0.03002  -0.0455   0.8923   0.1988
  -9.500  -0.8270   0.03809   0.02948  -0.0443   0.8840   0.2005
  -9.250  -0.7914   0.03751   0.02898  -0.0462   0.8816   0.2027
  -9.000  -0.7565   0.03686   0.02834  -0.0479   0.8799   0.2052
  -8.750  -0.7452   0.03650   0.02794  -0.0449   0.8707   0.2072
  -8.500  -0.7145   0.03572   0.02707  -0.0457   0.8678   0.2099
  -8.250  -0.6832   0.03495   0.02614  -0.0466   0.8660   0.2123
  -8.000  -0.6680   0.03425   0.02545  -0.0445   0.8574   0.2145
  -7.750  -0.6336   0.03353   0.02482  -0.0461   0.8542   0.2169
  -7.500  -0.5974   0.03282   0.02416  -0.0479   0.8521   0.2194
  -7.250  -0.5610   0.03205   0.02337  -0.0497   0.8506   0.2222
  -7.000  -0.5462   0.03177   0.02305  -0.0472   0.8423   0.2245
  -6.750  -0.5174   0.03116   0.02235  -0.0475   0.8383   0.2272
  -6.500  -0.4827   0.03040   0.02148  -0.0488   0.8359   0.2297
  -6.250  -0.4397   0.02913   0.02031  -0.0522   0.8344   0.2331
  -6.000  -0.3964   0.02831   0.01956  -0.0554   0.8330   0.2362
  -5.750  -0.3846   0.02822   0.01947  -0.0523   0.8231   0.2385
  -5.500  -0.3471   0.02753   0.01876  -0.0542   0.8195   0.2419
  -5.250  -0.3031   0.02674   0.01790  -0.0575   0.8167   0.2454
  -5.000  -0.2531   0.02600   0.01705  -0.0620   0.8143   0.2484
  -4.750  -0.2332   0.02529   0.01640  -0.0606   0.8041   0.2520
  -4.500  -0.1872   0.02448   0.01564  -0.0644   0.7983   0.2559
  -4.250  -0.1248   0.02364   0.01479  -0.0717   0.7943   0.2605
  -4.000  -0.1061   0.02345   0.01458  -0.0698   0.7848   0.2637
  -3.750  -0.0666   0.02306   0.01411  -0.0724   0.7773   0.2678
  -3.500  -0.0074   0.02232   0.01329  -0.0792   0.7716   0.2728
  -3.250   0.0077   0.02205   0.01311  -0.0766   0.7612   0.2766
  -3.000   0.0436   0.02167   0.01272  -0.0784   0.7525   0.2811
  -2.750   0.0836   0.02134   0.01235  -0.0811   0.7444   0.2863
  -2.500   0.0947   0.02132   0.01232  -0.0776   0.7336   0.2900
  -2.250   0.1322   0.02110   0.01196  -0.0796   0.7238   0.2943
  -2.000   0.1500   0.02085   0.01177  -0.0776   0.7137   0.2989
  -1.750   0.1696   0.02063   0.01162  -0.0759   0.7038   0.3038
  -1.500   0.2063   0.02037   0.01131  -0.0779   0.6950   0.3098
  -1.250   0.2094   0.02038   0.01138  -0.0727   0.6853   0.3138
  -1.000   0.2272   0.02031   0.01126  -0.0705   0.6746   0.3184
  -0.750   0.2486   0.02020   0.01111  -0.0692   0.6643   0.3231
  -0.500   0.2542   0.02011   0.01112  -0.0646   0.6527   0.3287
  -0.250   0.2758   0.01994   0.01094  -0.0633   0.6405   0.3359
   0.000   0.2813   0.02003   0.01109  -0.0587   0.6268   0.3424
   0.250   0.2960   0.02005   0.01106  -0.0560   0.6114   0.3508
   0.500   0.3037   0.02004   0.01114  -0.0519   0.5925   0.3634
   0.750   0.3112   0.02011   0.01125  -0.0479   0.5691   0.3805
   1.000   0.3136   0.02016   0.01136  -0.0429   0.5373   0.4131
   1.250   0.3078   0.02016   0.01161  -0.0364   0.4974   0.4925
   1.500   0.2969   0.02034   0.01221  -0.0288   0.4584   0.6303
   1.750   0.2922   0.02106   0.01295  -0.0225   0.4192   0.6968
   2.000   0.2941   0.02180   0.01367  -0.0177   0.3877   0.7418
   2.250   0.3020   0.02257   0.01448  -0.0139   0.3662   0.7814
   2.500   0.3164   0.02345   0.01541  -0.0114   0.3520   0.8192
   2.750   0.3379   0.02433   0.01630  -0.0102   0.3428   0.8527
   3.000   0.3603   0.02521   0.01714  -0.0093   0.3359   0.8782
   3.250   0.3839   0.02617   0.01800  -0.0088   0.3306   0.8977
   3.500   0.4118   0.02697   0.01877  -0.0090   0.3266   0.9143
   3.750   0.4376   0.02775   0.01949  -0.0088   0.3230   0.9306
   4.000   0.4777   0.02880   0.02048  -0.0116   0.3194   0.9401
   4.250   0.5166   0.02985   0.02144  -0.0142   0.3164   0.9515
   4.500   0.5680   0.03090   0.02237  -0.0195   0.3136   0.9555
   4.750   0.6130   0.03167   0.02302  -0.0236   0.3112   0.9604
   5.000   0.6488   0.03237   0.02367  -0.0256   0.3097   0.9696
   5.250   0.6947   0.03296   0.02423  -0.0300   0.3081   0.9721
   5.500   0.7390   0.03352   0.02475  -0.0340   0.3064   0.9754
   5.750   0.7831   0.03410   0.02529  -0.0380   0.3049   0.9798
   6.000   0.8246   0.03471   0.02586  -0.0415   0.3033   0.9855
   6.250   0.8646   0.03521   0.02632  -0.0447   0.3017   0.9893
   6.500   0.9067   0.03562   0.02668  -0.0485   0.3001   0.9921
   6.750   0.9502   0.03606   0.02708  -0.0524   0.2986   0.9956
   7.000   0.9935   0.03651   0.02746  -0.0563   0.2971   0.9990
   7.250   1.0204   0.03668   0.02756  -0.0570   0.2957   1.0000
   7.500   1.0408   0.03669   0.02747  -0.0563   0.2945   1.0000
   7.750   1.0608   0.03676   0.02749  -0.0555   0.2934   1.0000
   8.000   1.0718   0.03698   0.02773  -0.0531   0.2927   1.0000
   8.250   1.0840   0.03723   0.02800  -0.0509   0.2919   1.0000
   8.500   1.0967   0.03751   0.02829  -0.0489   0.2910   1.0000
   8.750   1.1094   0.03782   0.02863  -0.0468   0.2900   1.0000
   9.000   1.1224   0.03816   0.02898  -0.0448   0.2888   1.0000
   9.250   1.1356   0.03852   0.02935  -0.0428   0.2876   1.0000
   9.500   1.1486   0.03890   0.02973  -0.0408   0.2861   1.0000
   9.750   1.1614   0.03928   0.03011  -0.0388   0.2843   1.0000
  10.000   1.1778   0.03963   0.03042  -0.0374   0.2828   1.0000
  10.250   1.1973   0.03993   0.03068  -0.0366   0.2812   1.0000
  10.500   1.2238   0.04016   0.03082  -0.0368   0.2796   1.0000
  10.750   1.2554   0.04047   0.03105  -0.0380   0.2778   1.0000
  11.000   1.2571   0.04115   0.03183  -0.0343   0.2766   1.0000
  11.250   1.2600   0.04187   0.03264  -0.0309   0.2751   1.0000
  11.500   1.2654   0.04259   0.03342  -0.0280   0.2734   1.0000
  11.750   1.2737   0.04326   0.03413  -0.0256   0.2716   1.0000
  12.000   1.2854   0.04386   0.03475  -0.0237   0.2698   1.0000
  12.250   1.3018   0.04435   0.03521  -0.0226   0.2680   1.0000
  12.500   1.3262   0.04465   0.03543  -0.0226   0.2662   1.0000
  12.750   1.3676   0.04483   0.03546  -0.0252   0.2639   1.0000
  13.000   1.3564   0.04606   0.03686  -0.0202   0.2623   1.0000
  13.250   1.3512   0.04727   0.03820  -0.0162   0.2603   1.0000
  13.500   1.3519   0.04839   0.03940  -0.0132   0.2582   1.0000
  13.750   1.3610   0.04925   0.04028  -0.0114   0.2561   1.0000
  14.000   1.3811   0.04973   0.04071  -0.0110   0.2541   1.0000
  14.250   1.4204   0.04973   0.04055  -0.0131   0.2522   1.0000
  14.500   1.4220   0.05112   0.04204  -0.0105   0.2503   1.0000
  14.750   1.4078   0.05308   0.04419  -0.0062   0.2482   1.0000
  15.000   1.4046   0.05473   0.04595  -0.0035   0.2461   1.0000
  15.250   1.4122   0.05593   0.04718  -0.0020   0.2441   1.0000
  15.500   1.4328   0.05652   0.04772  -0.0019   0.2423   1.0000
  15.750   1.4785   0.05615   0.04717  -0.0046   0.2405   1.0000
  16.000   1.4558   0.05902   0.05028  -0.0003   0.2387   1.0000
  16.250   1.4317   0.06221   0.05369   0.0037   0.2367   1.0000
  16.500   1.4264   0.06444   0.05604   0.0057   0.2347   1.0000
  16.750   1.4370   0.06571   0.05733   0.0064   0.2329   1.0000
  17.000   1.4640   0.06593   0.05747   0.0057   0.2314   1.0000
  17.250   1.5011   0.06577   0.05719   0.0041   0.2299   1.0000
  17.500   1.4241   0.07313   0.06503   0.0108   0.2277   1.0000
  17.750   1.3896   0.07817   0.07031   0.0135   0.2255   1.0000
  18.000   1.3955   0.08000   0.07216   0.0138   0.2238   1.0000
  18.250   1.4266   0.07969   0.07178   0.0130   0.2224   1.0000
  18.500   1.4786   0.07787   0.06977   0.0110   0.2213   1.0000
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