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HAM-STD HS1-430 AIRFOIL (hs1430-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: HAM-STD HS1-430 AIRFOIL (hs1430-il)
Reynolds number: 100,000
Max Cl/Cd: 21.18 at α=10°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hs1430-il-100000-n5.txt
Download as CSV file: xf-hs1430-il-100000-n5.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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.8514   0.07748   0.06883  -0.0859   0.9778   0.1613
 -14.250  -0.8528   0.07411   0.06536  -0.0873   0.9756   0.1628
 -14.000  -0.8363   0.07316   0.06447  -0.0873   0.9708   0.1639
 -13.750  -0.8308   0.07109   0.06236  -0.0875   0.9669   0.1653
 -13.500  -0.8352   0.06813   0.05928  -0.0875   0.9638   0.1669
 -13.250  -0.8503   0.06473   0.05569  -0.0862   0.9600   0.1687
 -13.000  -0.8754   0.06137   0.05210  -0.0824   0.9533   0.1705
 -12.750  -0.8980   0.05785   0.04823  -0.0792   0.9493   0.1727
 -12.500  -0.9038   0.05624   0.04651  -0.0756   0.9424   0.1740
 -12.250  -0.8839   0.05555   0.04586  -0.0756   0.9386   0.1753
 -12.000  -0.8647   0.05469   0.04498  -0.0756   0.9361   0.1768
 -11.750  -0.8686   0.05373   0.04397  -0.0714   0.9279   0.1782
 -11.500  -0.8592   0.05251   0.04264  -0.0698   0.9246   0.1801
 -11.250  -0.8683   0.05131   0.04130  -0.0645   0.9164   0.1818
 -11.000  -0.8753   0.04993   0.03971  -0.0595   0.9090   0.1838
 -10.750  -0.8660   0.04863   0.03824  -0.0573   0.9040   0.1859
 -10.500  -0.8555   0.04815   0.03779  -0.0546   0.8956   0.1871
 -10.250  -0.8316   0.04741   0.03705  -0.0547   0.8921   0.1890
 -10.000  -0.8258   0.04680   0.03639  -0.0512   0.8833   0.1907
  -9.750  -0.8046   0.04581   0.03529  -0.0507   0.8799   0.1932
  -9.500  -0.8023   0.04508   0.03442  -0.0466   0.8706   0.1953
  -9.250  -0.7867   0.04389   0.03294  -0.0451   0.8663   0.1981
  -9.000  -0.7704   0.04343   0.03253  -0.0434   0.8584   0.1996
  -8.750  -0.7449   0.04283   0.03199  -0.0433   0.8531   0.2014
  -8.500  -0.7151   0.04210   0.03126  -0.0441   0.8501   0.2037
  -8.250  -0.7056   0.04178   0.03090  -0.0411   0.8412   0.2057
  -8.000  -0.6832   0.04109   0.03013  -0.0405   0.8367   0.2083
  -7.750  -0.6572   0.04024   0.02912  -0.0405   0.8337   0.2112
  -7.500  -0.6426   0.03981   0.02858  -0.0384   0.8269   0.2134
  -7.250  -0.6195   0.03938   0.02825  -0.0378   0.8209   0.2153
  -7.000  -0.5898   0.03877   0.02767  -0.0385   0.8175   0.2177
  -6.750  -0.5576   0.03804   0.02694  -0.0395   0.8149   0.2204
  -6.500  -0.5414   0.03779   0.02666  -0.0376   0.8075   0.2228
  -6.250  -0.5203   0.03740   0.02620  -0.0366   0.8015   0.2256
  -6.000  -0.4920   0.03677   0.02545  -0.0369   0.7980   0.2286
  -5.750  -0.4572   0.03599   0.02470  -0.0384   0.7954   0.2313
  -5.500  -0.4198   0.03521   0.02397  -0.0403   0.7933   0.2341
  -5.250  -0.4120   0.03538   0.02417  -0.0369   0.7828   0.2361
  -5.000  -0.3826   0.03487   0.02366  -0.0373   0.7782   0.2393
  -4.750  -0.3472   0.03416   0.02291  -0.0388   0.7748   0.2430
  -4.500  -0.3075   0.03334   0.02199  -0.0410   0.7719   0.2468
  -4.250  -0.2948   0.03335   0.02199  -0.0383   0.7619   0.2492
  -4.000  -0.2636   0.03274   0.02146  -0.0391   0.7554   0.2524
  -3.750  -0.2251   0.03199   0.02074  -0.0411   0.7510   0.2562
  -3.500  -0.1805   0.03114   0.01988  -0.0443   0.7475   0.2608
  -3.250  -0.1717   0.03136   0.02011  -0.0409   0.7375   0.2638
  -3.000  -0.1443   0.03105   0.01976  -0.0409   0.7304   0.2675
  -2.750  -0.1035   0.03034   0.01902  -0.0433   0.7251   0.2718
  -2.500  -0.0575   0.02948   0.01823  -0.0469   0.7202   0.2768
  -2.250  -0.0577   0.02989   0.01871  -0.0417   0.7088   0.2797
  -2.000  -0.0256   0.02945   0.01827  -0.0425   0.7010   0.2846
  -1.750   0.0254   0.02860   0.01735  -0.0469   0.6947   0.2904
  -1.500   0.0214   0.02913   0.01791  -0.0409   0.6820   0.2931
  -1.250   0.0541   0.02864   0.01744  -0.0418   0.6723   0.2984
  -1.000   0.0766   0.02842   0.01730  -0.0409   0.6627   0.3039
  -0.750   0.0886   0.02855   0.01748  -0.0380   0.6521   0.3091
  -0.500   0.1215   0.02815   0.01705  -0.0389   0.6434   0.3165
   0.000   0.1496   0.02827   0.01730  -0.0339   0.6210   0.3301
   0.250   0.1686   0.02820   0.01728  -0.0324   0.6095   0.3401
   0.750   0.1971   0.02827   0.01754  -0.0276   0.5816   0.3698
   1.000   0.2138   0.02812   0.01753  -0.0256   0.5650   0.4000
   1.250   0.2246   0.02808   0.01776  -0.0227   0.5460   0.4506
   1.500   0.2381   0.02780   0.01798  -0.0199   0.5251   0.5507
   1.750   0.2551   0.02782   0.01823  -0.0177   0.5008   0.6427
   2.000   0.2723   0.02809   0.01851  -0.0155   0.4753   0.6950
   2.250   0.2885   0.02859   0.01898  -0.0133   0.4503   0.7356
   2.500   0.3064   0.02933   0.01970  -0.0116   0.4256   0.7705
   2.750   0.3280   0.03031   0.02064  -0.0107   0.4019   0.8019
   3.000   0.3515   0.03141   0.02167  -0.0103   0.3811   0.8285
   3.250   0.3752   0.03250   0.02266  -0.0100   0.3646   0.8512
   3.500   0.3978   0.03359   0.02363  -0.0096   0.3519   0.8735
   3.750   0.4219   0.03459   0.02455  -0.0094   0.3424   0.8951
   4.000   0.4454   0.03555   0.02541  -0.0092   0.3347   0.9131
   4.250   0.4647   0.03639   0.02612  -0.0082   0.3292   0.9289
   4.500   0.5009   0.03725   0.02692  -0.0106   0.3238   0.9365
   4.750   0.5268   0.03805   0.02763  -0.0110   0.3194   0.9496
   5.000   0.5653   0.03888   0.02836  -0.0140   0.3153   0.9546
   5.250   0.5991   0.03962   0.02898  -0.0161   0.3121   0.9613
   5.500   0.6310   0.04033   0.02960  -0.0177   0.3093   0.9700
   5.750   0.6705   0.04099   0.03022  -0.0210   0.3064   0.9746
   6.000   0.7076   0.04167   0.03085  -0.0238   0.3035   0.9804
   6.250   0.7435   0.04247   0.03158  -0.0264   0.3007   0.9872
   6.500   0.7844   0.04314   0.03218  -0.0300   0.2980   0.9917
   6.750   0.8266   0.04381   0.03274  -0.0339   0.2957   0.9967
   7.000   0.8626   0.04432   0.03314  -0.0364   0.2939   1.0000
   7.250   0.8737   0.04455   0.03333  -0.0343   0.2925   1.0000
   7.500   0.8850   0.04482   0.03359  -0.0321   0.2911   1.0000
   7.750   0.8964   0.04514   0.03390  -0.0300   0.2895   1.0000
   8.000   0.9082   0.04549   0.03424  -0.0280   0.2880   1.0000
   8.250   0.9211   0.04585   0.03457  -0.0262   0.2865   1.0000
   8.500   0.9350   0.04620   0.03490  -0.0245   0.2852   1.0000
   8.750   0.9490   0.04659   0.03526  -0.0229   0.2838   1.0000
   9.000   0.9637   0.04698   0.03562  -0.0214   0.2825   1.0000
   9.250   0.9794   0.04736   0.03595  -0.0200   0.2812   1.0000
   9.500   0.9965   0.04773   0.03625  -0.0189   0.2798   1.0000
   9.750   1.0167   0.04802   0.03646  -0.0182   0.2784   1.0000
  10.000   1.0295   0.04861   0.03706  -0.0165   0.2771   1.0000
  10.250   1.0387   0.04936   0.03786  -0.0145   0.2757   1.0000
  10.500   1.0478   0.05014   0.03870  -0.0124   0.2742   1.0000
  10.750   1.0563   0.05097   0.03957  -0.0104   0.2723   1.0000
  11.000   1.0663   0.05177   0.04040  -0.0086   0.2706   1.0000
  11.250   1.0781   0.05253   0.04115  -0.0071   0.2690   1.0000
  11.500   1.0921   0.05319   0.04179  -0.0058   0.2673   1.0000
  11.750   1.1096   0.05372   0.04226  -0.0050   0.2657   1.0000
  12.000   1.1334   0.05402   0.04246  -0.0050   0.2641   1.0000
  12.250   1.1303   0.05559   0.04417  -0.0020   0.2624   1.0000
  12.500   1.1287   0.05718   0.04589   0.0007   0.2605   1.0000
  12.750   1.1297   0.05871   0.04751   0.0029   0.2586   1.0000
  13.000   1.1342   0.06009   0.04895   0.0047   0.2566   1.0000
  13.250   1.1443   0.06118   0.05004   0.0059   0.2548   1.0000
  13.500   1.1617   0.06185   0.05067   0.0064   0.2531   1.0000
  13.750   1.1893   0.06197   0.05067   0.0060   0.2515   1.0000
  14.000   1.1653   0.06536   0.05433   0.0098   0.2493   1.0000
  14.250   1.1508   0.06841   0.05756   0.0124   0.2470   1.0000
  14.500   1.1463   0.07085   0.06011   0.0141   0.2448   1.0000
  14.750   1.1522   0.07254   0.06184   0.0150   0.2429   1.0000
  15.000   1.1708   0.07324   0.06249   0.0151   0.2413   1.0000
  15.250   1.1756   0.07512   0.06440   0.0159   0.2394   1.0000
  15.500   1.1040   0.08397   0.07374   0.0198   0.2357   1.0000
  15.750   1.0868   0.08826   0.07816   0.0208   0.2330   1.0000
  16.000   1.1022   0.08925   0.07913   0.0208   0.2314   1.0000
  16.250   1.1312   0.08890   0.07868   0.0204   0.2302   1.0000
  17.750   0.6637   0.17795   0.16932   0.0004   0.1759   1.0000
  18.000   0.6773   0.17933   0.17069  -0.0006   0.1746   1.0000
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