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NACA 1-H-15 AIRFOIL (n1h15-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 1-H-15 AIRFOIL (n1h15-il)
Reynolds number: 500,000
Max Cl/Cd: 102.18 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n1h15-il-500000-n5.txt
Download as CSV file: xf-n1h15-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 1-H-15 AIRFOIL                             
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.250  -0.2559   0.09511   0.09171  -0.0484   0.6977   0.0183
 -10.000  -0.2707   0.08839   0.08502  -0.0521   0.6968   0.0192
  -9.750  -0.2709   0.08473   0.08136  -0.0540   0.6959   0.0192
  -9.500  -0.2584   0.08361   0.08024  -0.0545   0.6949   0.0195
  -9.250  -0.2585   0.08026   0.07690  -0.0563   0.6939   0.0197
  -9.000  -0.2549   0.07775   0.07440  -0.0577   0.6930   0.0200
  -8.750  -0.2623   0.07385   0.07051  -0.0601   0.6920   0.0201
  -8.500  -0.2741   0.07010   0.06676  -0.0621   0.6909   0.0203
  -8.250  -0.2888   0.06625   0.06287  -0.0627   0.6898   0.0203
  -8.000  -0.2933   0.06211   0.05870  -0.0642   0.6886   0.0204
  -7.750  -0.2950   0.05780   0.05433  -0.0654   0.6873   0.0207
  -7.500  -0.2948   0.05320   0.04961  -0.0660   0.6860   0.0209
  -7.250  -0.2934   0.04820   0.04443  -0.0660   0.6847   0.0214
  -7.000  -0.3331   0.03132   0.02644  -0.0609   0.6835   0.0229
  -6.750  -0.3200   0.02890   0.02378  -0.0596   0.6824   0.0231
  -6.500  -0.3006   0.02760   0.02233  -0.0588   0.6813   0.0234
  -6.250  -0.2785   0.02682   0.02146  -0.0584   0.6803   0.0236
  -6.000  -0.2563   0.02597   0.02050  -0.0579   0.6794   0.0239
  -5.750  -0.2351   0.02472   0.01908  -0.0572   0.6785   0.0243
  -5.500  -0.2151   0.02297   0.01704  -0.0561   0.6775   0.0246
  -5.250  -0.1934   0.02153   0.01534  -0.0552   0.6766   0.0249
  -5.000  -0.1706   0.02025   0.01382  -0.0544   0.6756   0.0252
  -4.750  -0.1461   0.01918   0.01254  -0.0540   0.6746   0.0254
  -4.500  -0.1204   0.01826   0.01146  -0.0539   0.6735   0.0258
  -4.250  -0.0939   0.01750   0.01056  -0.0538   0.6723   0.0261
  -4.000  -0.0670   0.01690   0.00984  -0.0538   0.6712   0.0265
  -3.750  -0.0398   0.01638   0.00920  -0.0539   0.6700   0.0269
  -3.500  -0.0124   0.01586   0.00859  -0.0539   0.6689   0.0271
  -3.250   0.0151   0.01542   0.00807  -0.0540   0.6677   0.0273
  -3.000   0.0425   0.01492   0.00751  -0.0541   0.6666   0.0275
  -2.750   0.0695   0.01429   0.00684  -0.0541   0.6655   0.0279
  -2.500   0.0965   0.01386   0.00639  -0.0542   0.6644   0.0282
  -2.250   0.1235   0.01351   0.00603  -0.0542   0.6635   0.0286
  -2.000   0.1503   0.01321   0.00572  -0.0541   0.6626   0.0290
  -1.750   0.1771   0.01295   0.00543  -0.0540   0.6618   0.0294
  -1.500   0.2037   0.01272   0.00518  -0.0539   0.6610   0.0298
  -1.250   0.2310   0.01256   0.00504  -0.0541   0.6599   0.0303
  -1.000   0.2587   0.01245   0.00497  -0.0544   0.6585   0.0311
  -0.750   0.2861   0.01234   0.00487  -0.0546   0.6570   0.0318
  -0.500   0.3134   0.01223   0.00477  -0.0547   0.6556   0.0324
  -0.250   0.3407   0.01213   0.00468  -0.0549   0.6542   0.0327
   0.000   0.3677   0.01200   0.00456  -0.0549   0.6530   0.0334
   0.250   0.3947   0.01189   0.00446  -0.0550   0.6519   0.0344
   0.500   0.4219   0.01180   0.00439  -0.0551   0.6508   0.0355
   0.750   0.4493   0.01174   0.00432  -0.0552   0.6498   0.0368
   1.000   0.4767   0.01167   0.00426  -0.0553   0.6488   0.0385
   1.250   0.5039   0.01160   0.00419  -0.0554   0.6478   0.0424
   1.500   0.5306   0.01147   0.00414  -0.0553   0.6469   0.0635
   1.750   0.5516   0.01095   0.00430  -0.0546   0.6455   0.3019
   2.250   0.7182   0.01001   0.00524  -0.0787   0.6445   0.9823
   2.500   0.7780   0.01016   0.00540  -0.0859   0.6435   0.9900
   2.750   0.8193   0.01030   0.00555  -0.0892   0.6420   0.9941
   3.000   0.8543   0.01036   0.00563  -0.0913   0.6404   0.9956
   3.250   0.8861   0.01037   0.00564  -0.0925   0.6382   0.9967
   3.500   0.9172   0.01034   0.00561  -0.0936   0.6361   0.9977
   3.750   0.9478   0.01018   0.00542  -0.0943   0.6334   0.9987
   4.000   0.9797   0.01024   0.00550  -0.0957   0.6306   0.9997
   4.250   1.0102   0.01046   0.00580  -0.0971   0.6261   1.0000
   4.500   1.0372   0.01058   0.00595  -0.0974   0.6231   1.0000
   4.750   1.0635   0.01059   0.00596  -0.0975   0.6201   1.0000
   5.000   1.0903   0.01067   0.00608  -0.0978   0.6161   1.0000
   5.250   1.1193   0.01110   0.00660  -0.0992   0.6103   1.0000
   5.500   1.1469   0.01124   0.00672  -0.0999   0.6009   1.0000
   5.750   1.1740   0.01168   0.00718  -0.1010   0.5868   1.0000
   6.000   1.1971   0.01239   0.00785  -0.1017   0.5639   1.0000
   6.250   1.2106   0.01339   0.00872  -0.1009   0.5338   1.0000
   6.500   1.1998   0.01501   0.01016  -0.0961   0.5005   1.0000
   6.750   1.1670   0.01635   0.01140  -0.0864   0.4820   1.0000
   7.000   1.1382   0.01802   0.01292  -0.0781   0.4553   1.0000
   7.250   1.1129   0.02004   0.01476  -0.0710   0.4227   1.0000
   7.500   1.0795   0.02286   0.01729  -0.0635   0.3744   1.0000
   7.750   1.0459   0.02610   0.02016  -0.0567   0.3118   1.0000
   8.000   1.0149   0.02948   0.02310  -0.0506   0.2345   1.0000
   8.250   0.9992   0.03208   0.02535  -0.0465   0.1716   1.0000
   8.500   0.9973   0.03387   0.02692  -0.0437   0.1306   1.0000
   8.750   0.9980   0.03557   0.02843  -0.0414   0.0970   1.0000
   9.000   1.0027   0.03702   0.02974  -0.0395   0.0718   1.0000
   9.250   1.0109   0.03825   0.03089  -0.0379   0.0572   1.0000
   9.500   1.0206   0.03941   0.03201  -0.0365   0.0496   1.0000
   9.750   1.0317   0.04049   0.03309  -0.0352   0.0454   1.0000
  10.000   1.0430   0.04157   0.03416  -0.0340   0.0426   1.0000
  10.250   1.0553   0.04258   0.03519  -0.0330   0.0410   1.0000
  10.500   1.0678   0.04359   0.03623  -0.0319   0.0397   1.0000
  10.750   1.0794   0.04470   0.03736  -0.0308   0.0386   1.0000
  11.000   1.0910   0.04581   0.03851  -0.0298   0.0374   1.0000
  11.250   1.1019   0.04699   0.03970  -0.0288   0.0362   1.0000
  11.500   1.1119   0.04826   0.04098  -0.0276   0.0349   1.0000
  11.750   1.1222   0.04952   0.04227  -0.0266   0.0339   1.0000
  12.000   1.1333   0.05074   0.04354  -0.0257   0.0335   1.0000
  12.250   1.1443   0.05196   0.04481  -0.0248   0.0328   1.0000
  12.500   1.1560   0.05313   0.04602  -0.0239   0.0318   1.0000
  12.750   1.1665   0.05442   0.04735  -0.0231   0.0310   1.0000
  13.000   1.1764   0.05579   0.04875  -0.0222   0.0302   1.0000
  13.250   1.1858   0.05721   0.05020  -0.0213   0.0295   1.0000
  13.500   1.1938   0.05874   0.05176  -0.0204   0.0287   1.0000
  13.750   1.2014   0.06035   0.05341  -0.0195   0.0280   1.0000
  14.000   1.2119   0.06172   0.05484  -0.0188   0.0276   1.0000
  14.250   1.2223   0.06311   0.05629  -0.0181   0.0269   1.0000
  14.500   1.2326   0.06449   0.05773  -0.0175   0.0261   1.0000
  14.750   1.2423   0.06597   0.05925  -0.0168   0.0255   1.0000
  15.000   1.2514   0.06750   0.06084  -0.0162   0.0247   1.0000
  15.250   1.2599   0.06911   0.06248  -0.0156   0.0242   1.0000
  15.500   1.2669   0.07087   0.06425  -0.0150   0.0233   1.0000
  15.750   1.2746   0.07259   0.06604  -0.0144   0.0229   1.0000
  16.000   1.2844   0.07413   0.06766  -0.0140   0.0221   1.0000
  16.250   1.2926   0.07582   0.06943  -0.0135   0.0216   1.0000
  16.500   1.3015   0.07746   0.07113  -0.0131   0.0209   1.0000
  16.750   1.3097   0.07920   0.07292  -0.0128   0.0202   1.0000
  17.000   1.3164   0.08110   0.07488  -0.0124   0.0197   1.0000
  17.250   1.3234   0.08299   0.07679  -0.0122   0.0190   1.0000
  17.500   1.3289   0.08507   0.07895  -0.0118   0.0186   1.0000
  17.750   1.3356   0.08703   0.08100  -0.0116   0.0181   1.0000
  18.000   1.3418   0.08905   0.08310  -0.0114   0.0176   1.0000
  18.250   1.3478   0.09114   0.08526  -0.0113   0.0169   1.0000
  18.500   1.3537   0.09324   0.08744  -0.0112   0.0164   1.0000
  18.750   1.3591   0.09540   0.08966  -0.0112   0.0159   1.0000
  19.000   1.3621   0.09792   0.09223  -0.0112   0.0156   1.0000
  19.250   1.3648   0.10047   0.09484  -0.0113   0.0151   1.0000
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