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TH 25816 HALE AIRFOIL (th25816-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: TH 25816 HALE AIRFOIL (th25816-il)
Reynolds number: 1,000,000
Max Cl/Cd: 59.62 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-th25816-il-1000000-n5.txt
Download as CSV file: xf-th25816-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: TH 25816 HALE 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.3036   0.05818   0.05362  -0.2518   0.9407   0.0107
 -19.500  -0.3047   0.05563   0.05101  -0.2524   0.9401   0.0108
 -19.250  -0.3021   0.05336   0.04867  -0.2533   0.9393   0.0109
 -19.000  -0.2962   0.05138   0.04664  -0.2541   0.9386   0.0110
 -18.750  -0.2928   0.04933   0.04453  -0.2547   0.9380   0.0111
 -18.500  -0.2866   0.04758   0.04273  -0.2552   0.9375   0.0111
 -18.250  -0.2806   0.04583   0.04093  -0.2557   0.9368   0.0113
 -18.000  -0.2719   0.04424   0.03928  -0.2563   0.9360   0.0113
 -17.750  -0.2707   0.04285   0.03784  -0.2551   0.9350   0.0113
 -17.500  -0.2719   0.04154   0.03650  -0.2532   0.9339   0.0114
 -17.250  -0.2691   0.04042   0.03535  -0.2517   0.9323   0.0115
 -17.000  -0.2653   0.03921   0.03410  -0.2505   0.9309   0.0116
 -16.750  -0.2601   0.03798   0.03283  -0.2496   0.9297   0.0116
 -16.500  -0.2510   0.03687   0.03168  -0.2491   0.9284   0.0118
 -16.250  -0.2400   0.03574   0.03051  -0.2491   0.9272   0.0120
 -16.000  -0.2293   0.03457   0.02929  -0.2490   0.9260   0.0120
 -15.750  -0.2164   0.03351   0.02819  -0.2491   0.9250   0.0122
 -15.500  -0.2043   0.03241   0.02704  -0.2491   0.9240   0.0123
 -15.250  -0.1876   0.03145   0.02603  -0.2497   0.9229   0.0125
 -15.000  -0.1877   0.03048   0.02502  -0.2471   0.9211   0.0124
 -14.750  -0.1864   0.02981   0.02434  -0.2441   0.9187   0.0125
 -14.500  -0.1787   0.02912   0.02362  -0.2423   0.9164   0.0127
 -14.250  -0.1689   0.02831   0.02278  -0.2412   0.9142   0.0128
 -14.000  -0.1566   0.02747   0.02190  -0.2405   0.9122   0.0129
 -13.750  -0.1397   0.02666   0.02104  -0.2406   0.9105   0.0130
 -13.500  -0.1325   0.02593   0.02028  -0.2387   0.9077   0.0131
 -13.250  -0.1361   0.02549   0.01982  -0.2341   0.9024   0.0131
 -13.000  -0.1235   0.02489   0.01918  -0.2330   0.8987   0.0133
 -12.750  -0.1107   0.02420   0.01845  -0.2320   0.8951   0.0134
 -12.500  -0.1114   0.02370   0.01792  -0.2279   0.8869   0.0134
 -12.250  -0.1020   0.02289   0.01706  -0.2264   0.8787   0.0137
 -12.000  -0.0887   0.02213   0.01622  -0.2255   0.8677   0.0141
 -11.750  -0.0746   0.02158   0.01556  -0.2245   0.8535   0.0141
 -11.500  -0.0666   0.02115   0.01501  -0.2220   0.8394   0.0144
 -11.250  -0.0619   0.02082   0.01458  -0.2188   0.8274   0.0146
 -11.000  -0.0594   0.02049   0.01418  -0.2151   0.8173   0.0148
 -10.750  -0.0627   0.02027   0.01389  -0.2099   0.8084   0.0149
 -10.500  -0.0659   0.01998   0.01354  -0.2049   0.8006   0.0151
 -10.000  -0.0631   0.01941   0.01289  -0.1968   0.7893   0.0155
  -9.750  -0.0609   0.01912   0.01255  -0.1929   0.7842   0.0157
  -9.500  -0.0609   0.01889   0.01228  -0.1884   0.7789   0.0159
  -9.250  -0.0577   0.01865   0.01201  -0.1846   0.7748   0.0161
  -9.000  -0.0538   0.01840   0.01173  -0.1809   0.7705   0.0163
  -8.750  -0.0511   0.01815   0.01145  -0.1770   0.7663   0.0165
  -8.500  -0.0471   0.01792   0.01118  -0.1733   0.7624   0.0168
  -8.250  -0.0420   0.01762   0.01086  -0.1699   0.7593   0.0173
  -8.000  -0.0370   0.01735   0.01058  -0.1665   0.7563   0.0175
  -7.750  -0.0314   0.01712   0.01033  -0.1631   0.7529   0.0180
  -7.500  -0.0261   0.01689   0.01008  -0.1596   0.7493   0.0186
  -7.250  -0.0202   0.01667   0.00983  -0.1562   0.7459   0.0189
  -7.000  -0.0121   0.01646   0.00958  -0.1532   0.7432   0.0192
  -6.750  -0.0051   0.01624   0.00936  -0.1500   0.7408   0.0200
  -6.500   0.0007   0.01600   0.00913  -0.1466   0.7381   0.0208
  -6.250   0.0069   0.01577   0.00888  -0.1432   0.7353   0.0223
  -6.000   0.0145   0.01557   0.00867  -0.1400   0.7324   0.0233
  -5.750   0.0191   0.01534   0.00842  -0.1363   0.7293   0.0268
  -5.500   0.0233   0.01507   0.00817  -0.1325   0.7265   0.0344
  -5.250   0.0219   0.01472   0.00790  -0.1276   0.7241   0.0528
  -5.000   0.0205   0.01442   0.00765  -0.1227   0.7214   0.0665
  -4.750   0.0173   0.01406   0.00738  -0.1174   0.7186   0.0878
  -4.500   0.0130   0.01371   0.00709  -0.1119   0.7158   0.1095
  -4.250   0.0004   0.01326   0.00674  -0.1047   0.7128   0.1420
  -4.000  -0.0065   0.01298   0.00649  -0.0985   0.7099   0.1582
  -3.500  -0.0377   0.01221   0.00591  -0.0825   0.7041   0.2147
  -3.250  -0.0371   0.01165   0.00556  -0.0779   0.7015   0.2746
  -3.000  -0.0323   0.01103   0.00521  -0.0743   0.6990   0.3463
  -2.750  -0.0319   0.00996   0.00468  -0.0700   0.6965   0.4781
  -2.500  -0.0195   0.00925   0.00440  -0.0679   0.6942   0.5902
  -2.250   0.0011   0.00909   0.00441  -0.0670   0.6925   0.6364
  -2.000   0.0238   0.00907   0.00446  -0.0665   0.6906   0.6580
  -1.750   0.0483   0.00912   0.00449  -0.0664   0.6884   0.6643
  -1.500   0.0729   0.00917   0.00451  -0.0663   0.6860   0.6687
  -1.250   0.0971   0.00921   0.00455  -0.0661   0.6836   0.6739
  -1.000   0.1222   0.00926   0.00458  -0.0661   0.6815   0.6785
  -0.750   0.1477   0.00932   0.00460  -0.0662   0.6794   0.6825
  -0.500   0.1737   0.00936   0.00461  -0.0664   0.6773   0.6864
  -0.250   0.1985   0.00941   0.00468  -0.0663   0.6757   0.6893
   0.000   0.2232   0.00948   0.00474  -0.0663   0.6737   0.6919
   0.250   0.2478   0.00955   0.00481  -0.0662   0.6714   0.6946
   0.500   0.2722   0.00963   0.00487  -0.0661   0.6690   0.6972
   0.750   0.2961   0.00972   0.00495  -0.0659   0.6667   0.6998
   1.250   0.3441   0.00990   0.00509  -0.0656   0.6624   0.7052
   1.500   0.3689   0.00998   0.00517  -0.0656   0.6604   0.7081
   1.750   0.3924   0.01008   0.00529  -0.0654   0.6583   0.7110
   2.000   0.4163   0.01018   0.00540  -0.0652   0.6562   0.7139
   2.250   0.4403   0.01029   0.00551  -0.0651   0.6538   0.7167
   2.500   0.4646   0.01040   0.00560  -0.0650   0.6516   0.7192
   2.750   0.4879   0.01050   0.00572  -0.0648   0.6492   0.7223
   3.000   0.5114   0.01061   0.00583  -0.0646   0.6469   0.7257
   3.250   0.5354   0.01073   0.00594  -0.0645   0.6443   0.7292
   3.500   0.5567   0.01090   0.00613  -0.0638   0.6422   0.7327
   3.750   0.5790   0.01106   0.00631  -0.0634   0.6397   0.7357
   4.000   0.6009   0.01121   0.00649  -0.0630   0.6368   0.7388
   4.250   0.6227   0.01137   0.00666  -0.0624   0.6338   0.7423
   4.500   0.6445   0.01154   0.00683  -0.0619   0.6309   0.7458
   4.750   0.6666   0.01171   0.00699  -0.0615   0.6277   0.7498
   5.000   0.6870   0.01193   0.00724  -0.0608   0.6248   0.7534
   5.250   0.7065   0.01216   0.00751  -0.0599   0.6214   0.7570
   5.500   0.7255   0.01240   0.00778  -0.0589   0.6173   0.7610
   5.750   0.7448   0.01265   0.00802  -0.0580   0.6133   0.7649
   6.000   0.7650   0.01289   0.00827  -0.0573   0.6098   0.7686
   6.250   0.7846   0.01316   0.00857  -0.0565   0.6060   0.7719
   6.500   0.8013   0.01350   0.00894  -0.0551   0.6014   0.7754
   6.750   0.8181   0.01384   0.00928  -0.0538   0.5965   0.7793
   7.000   0.8365   0.01416   0.00962  -0.0528   0.5920   0.7833
   7.250   0.8523   0.01457   0.01005  -0.0514   0.5859   0.7870
   7.500   0.8656   0.01504   0.01052  -0.0495   0.5798   0.7903
   7.750   0.8827   0.01542   0.01093  -0.0484   0.5745   0.7935
   8.000   0.8977   0.01588   0.01142  -0.0469   0.5676   0.7969
   8.250   0.9077   0.01651   0.01204  -0.0445   0.5597   0.8003
   8.500   0.9207   0.01708   0.01260  -0.0428   0.5503   0.8034
   8.750   0.9271   0.01789   0.01339  -0.0400   0.5384   0.8064
   9.000   0.9338   0.01871   0.01419  -0.0372   0.5274   0.8094
   9.250   0.9347   0.01979   0.01525  -0.0336   0.5117   0.8125
   9.500   0.9382   0.02079   0.01622  -0.0305   0.4959   0.8157
   9.750   0.9336   0.02220   0.01755  -0.0262   0.4751   0.8186
  10.000   0.9261   0.02381   0.01906  -0.0217   0.4513   0.8212
  10.250   0.9214   0.02534   0.02049  -0.0177   0.4298   0.8234
  10.500   0.9206   0.02672   0.02184  -0.0144   0.4125   0.8259
  10.750   0.9196   0.02816   0.02322  -0.0112   0.3941   0.8284
  11.000   0.9185   0.02965   0.02465  -0.0081   0.3740   0.8308
  11.250   0.9213   0.03100   0.02595  -0.0056   0.3581   0.8331
  11.500   0.9229   0.03244   0.02732  -0.0031   0.3398   0.8351
  11.750   0.9269   0.03380   0.02862  -0.0009   0.3234   0.8370
  12.000   0.9309   0.03518   0.02995   0.0011   0.3084   0.8387
  12.250   0.9376   0.03644   0.03114   0.0027   0.2930   0.8402
  12.500   0.9409   0.03791   0.03257   0.0048   0.2767   0.8420
  12.750   0.9471   0.03921   0.03383   0.0064   0.2621   0.8438
  13.000   0.9553   0.04042   0.03502   0.0077   0.2493   0.8455
  13.250   0.9607   0.04185   0.03641   0.0093   0.2365   0.8471
  13.500   0.9679   0.04316   0.03768   0.0106   0.2241   0.8486
  13.750   0.9732   0.04463   0.03909   0.0120   0.2084   0.8501
  14.000   0.9807   0.04601   0.04044   0.0132   0.1970   0.8517
  14.250   0.9897   0.04728   0.04169   0.0141   0.1866   0.8532
  14.500   0.9966   0.04873   0.04308   0.0152   0.1737   0.8547
  14.750   1.0027   0.05028   0.04460   0.0163   0.1631   0.8559
  15.000   1.0114   0.05165   0.04592   0.0171   0.1524   0.8570
  15.250   1.0171   0.05325   0.04746   0.0181   0.1387   0.8580
  15.500   1.0242   0.05476   0.04896   0.0189   0.1310   0.8594
  15.750   1.0325   0.05619   0.05038   0.0196   0.1225   0.8608
  16.000   1.0407   0.05763   0.05181   0.0203   0.1139   0.8621
  16.250   1.0465   0.05932   0.05348   0.0211   0.1062   0.8635
  16.500   1.0565   0.06069   0.05487   0.0215   0.1011   0.8648
  16.750   1.0648   0.06219   0.05636   0.0220   0.0954   0.8661
  17.000   1.0720   0.06383   0.05801   0.0225   0.0886   0.8674
  17.250   1.0798   0.06543   0.05961   0.0229   0.0842   0.8688
  17.500   1.0892   0.06691   0.06109   0.0231   0.0803   0.8701
  17.750   1.0978   0.06848   0.06268   0.0234   0.0762   0.8713
  18.000   1.1047   0.07025   0.06446   0.0237   0.0728   0.8724
  18.250   1.1139   0.07180   0.06603   0.0238   0.0696   0.8734
  18.500   1.1227   0.07342   0.06767   0.0238   0.0664   0.8742
  18.750   1.1280   0.07539   0.06964   0.0240   0.0628   0.8748
  19.000   1.1361   0.07708   0.07136   0.0241   0.0597   0.8759
  19.250   1.1449   0.07867   0.07300   0.0240   0.0579   0.8770
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