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NACA CYH (nacacyh-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA CYH (nacacyh-il)
Reynolds number: 1,000,000
Max Cl/Cd: 101.04 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-nacacyh-il-1000000-n5.txt
Download as CSV file: xf-nacacyh-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA CYH                                        
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -1.3140   0.03727   0.03419  -0.0711   1.0000   0.0104
 -17.000  -1.3212   0.03455   0.03133  -0.0702   1.0000   0.0106
 -16.750  -1.3238   0.03250   0.02913  -0.0683   1.0000   0.0108
 -16.500  -1.3229   0.03083   0.02734  -0.0661   1.0000   0.0110
 -16.250  -1.3178   0.02946   0.02589  -0.0637   1.0000   0.0114
 -16.000  -1.3065   0.02830   0.02464  -0.0620   1.0000   0.0119
 -15.750  -1.2924   0.02727   0.02355  -0.0605   1.0000   0.0123
 -15.500  -1.2769   0.02631   0.02250  -0.0591   1.0000   0.0128
 -15.250  -1.2605   0.02538   0.02148  -0.0577   1.0000   0.0132
 -15.000  -1.2435   0.02447   0.02047  -0.0564   1.0000   0.0136
 -14.750  -1.2253   0.02362   0.01952  -0.0551   1.0000   0.0140
 -14.500  -1.2042   0.02303   0.01891  -0.0540   1.0000   0.0144
 -14.250  -1.1821   0.02255   0.01840  -0.0531   1.0000   0.0149
 -14.000  -1.1597   0.02208   0.01790  -0.0521   1.0000   0.0153
 -13.750  -1.1373   0.02159   0.01736  -0.0512   1.0000   0.0158
 -13.500  -1.1150   0.02108   0.01679  -0.0502   1.0000   0.0163
 -13.250  -1.0927   0.02055   0.01619  -0.0493   1.0000   0.0167
 -13.000  -1.0702   0.02003   0.01559  -0.0483   1.0000   0.0171
 -12.750  -1.0474   0.01954   0.01502  -0.0473   1.0000   0.0174
 -12.500  -1.0254   0.01895   0.01437  -0.0463   1.0000   0.0177
 -12.250  -1.0023   0.01852   0.01392  -0.0453   1.0000   0.0181
 -12.000  -0.9732   0.01815   0.01353  -0.0456   0.9923   0.0185
 -11.750  -0.9419   0.01786   0.01320  -0.0462   0.9799   0.0188
 -11.500  -0.9114   0.01757   0.01287  -0.0466   0.9640   0.0193
 -11.250  -0.8851   0.01726   0.01249  -0.0461   0.9424   0.0197
 -11.000  -0.8623   0.01694   0.01206  -0.0449   0.9137   0.0201
 -10.750  -0.8397   0.01664   0.01161  -0.0436   0.8821   0.0205
 -10.500  -0.8159   0.01638   0.01119  -0.0426   0.8532   0.0208
 -10.250  -0.7912   0.01610   0.01076  -0.0417   0.8308   0.0212
 -10.000  -0.7659   0.01583   0.01036  -0.0410   0.8125   0.0214
  -9.750  -0.7401   0.01560   0.01002  -0.0404   0.7980   0.0216
  -9.500  -0.7150   0.01518   0.00948  -0.0398   0.7855   0.0219
  -9.250  -0.6912   0.01447   0.00868  -0.0390   0.7746   0.0224
  -9.000  -0.6655   0.01408   0.00822  -0.0384   0.7654   0.0228
  -8.750  -0.6394   0.01376   0.00783  -0.0379   0.7566   0.0232
  -8.500  -0.6131   0.01342   0.00743  -0.0374   0.7492   0.0235
  -8.250  -0.5866   0.01311   0.00706  -0.0370   0.7417   0.0238
  -8.000  -0.5599   0.01283   0.00672  -0.0366   0.7355   0.0242
  -7.750  -0.5332   0.01252   0.00636  -0.0362   0.7293   0.0245
  -7.250  -0.4796   0.01191   0.00563  -0.0354   0.7178   0.0252
  -7.000  -0.4526   0.01162   0.00528  -0.0350   0.7123   0.0255
  -6.750  -0.4256   0.01136   0.00496  -0.0346   0.7066   0.0258
  -6.500  -0.3983   0.01111   0.00466  -0.0343   0.6997   0.0261
  -6.250  -0.3711   0.01089   0.00439  -0.0340   0.6923   0.0264
  -6.000  -0.3434   0.01070   0.00415  -0.0337   0.6863   0.0267
  -5.750  -0.3158   0.01052   0.00393  -0.0335   0.6794   0.0269
  -5.500  -0.2883   0.01033   0.00370  -0.0332   0.6729   0.0270
  -5.250  -0.2611   0.01003   0.00335  -0.0329   0.6665   0.0275
  -5.000  -0.2337   0.00980   0.00307  -0.0327   0.6599   0.0280
  -4.750  -0.2060   0.00960   0.00284  -0.0324   0.6525   0.0286
  -4.500  -0.1783   0.00944   0.00264  -0.0322   0.6449   0.0291
  -4.250  -0.1504   0.00928   0.00246  -0.0321   0.6379   0.0297
  -4.000  -0.1226   0.00916   0.00230  -0.0319   0.6288   0.0303
  -3.750  -0.0946   0.00904   0.00215  -0.0318   0.6193   0.0310
  -3.500  -0.0666   0.00894   0.00202  -0.0317   0.6107   0.0317
  -3.250  -0.0385   0.00885   0.00189  -0.0316   0.6024   0.0325
  -3.000  -0.0103   0.00877   0.00178  -0.0315   0.5948   0.0333
  -2.750   0.0178   0.00868   0.00168  -0.0314   0.5862   0.0354
  -2.500   0.0458   0.00859   0.00159  -0.0313   0.5780   0.0388
  -2.250   0.0736   0.00850   0.00150  -0.0313   0.5682   0.0477
  -2.000   0.1012   0.00836   0.00144  -0.0312   0.5579   0.0715
  -1.750   0.1290   0.00830   0.00138  -0.0311   0.5470   0.0846
  -1.500   0.1568   0.00822   0.00134  -0.0311   0.5361   0.1028
  -1.250   0.1843   0.00810   0.00130  -0.0310   0.5257   0.1336
  -1.000   0.2116   0.00799   0.00127  -0.0309   0.5149   0.1736
  -0.750   0.2390   0.00790   0.00126  -0.0309   0.5032   0.2111
  -0.500   0.2661   0.00778   0.00126  -0.0308   0.4905   0.2641
  -0.250   0.2931   0.00769   0.00127  -0.0307   0.4765   0.3126
   0.000   0.3197   0.00758   0.00129  -0.0306   0.4598   0.3748
   0.250   0.3445   0.00731   0.00131  -0.0302   0.4415   0.4981
   0.500   0.3587   0.00630   0.00136  -0.0275   0.4249   0.8430
   0.750   0.3838   0.00634   0.00146  -0.0268   0.4057   0.8894
   1.000   0.4096   0.00646   0.00156  -0.0262   0.3874   0.9179
   1.250   0.4365   0.00659   0.00167  -0.0260   0.3720   0.9359
   1.500   0.4644   0.00674   0.00178  -0.0259   0.3596   0.9504
   1.750   0.4923   0.00690   0.00188  -0.0260   0.3484   0.9606
   2.000   0.5225   0.00706   0.00198  -0.0266   0.3367   0.9662
   2.250   0.5504   0.00720   0.00208  -0.0266   0.3270   0.9726
   2.500   0.5825   0.00738   0.00220  -0.0278   0.3162   0.9758
   2.750   0.6140   0.00754   0.00231  -0.0287   0.3062   0.9796
   3.000   0.6440   0.00768   0.00242  -0.0293   0.2998   0.9841
   3.250   0.6784   0.00783   0.00253  -0.0310   0.2916   0.9855
   3.500   0.7107   0.00797   0.00265  -0.0323   0.2843   0.9867
   3.750   0.7421   0.00809   0.00275  -0.0333   0.2783   0.9878
   4.000   0.7728   0.00825   0.00287  -0.0342   0.2715   0.9892
   4.250   0.8034   0.00837   0.00299  -0.0351   0.2648   0.9907
   4.500   0.8334   0.00854   0.00312  -0.0359   0.2573   0.9923
   4.750   0.8632   0.00867   0.00325  -0.0366   0.2509   0.9940
   5.000   0.8943   0.00887   0.00341  -0.0378   0.2401   0.9949
   5.250   0.9245   0.00915   0.00359  -0.0388   0.2191   0.9959
   5.500   0.9525   0.00967   0.00390  -0.0395   0.1824   0.9973
   5.750   0.9804   0.01018   0.00426  -0.0403   0.1541   0.9987
   6.000   1.0089   0.01060   0.00459  -0.0410   0.1346   0.9999
   6.250   1.0289   0.01102   0.00491  -0.0400   0.1166   1.0000
   6.500   1.0484   0.01142   0.00523  -0.0388   0.1020   1.0000
   6.750   1.0683   0.01178   0.00553  -0.0377   0.0910   1.0000
   7.000   1.0887   0.01212   0.00583  -0.0366   0.0824   1.0000
   7.250   1.1090   0.01248   0.00615  -0.0357   0.0749   1.0000
   7.500   1.1298   0.01280   0.00646  -0.0348   0.0688   1.0000
   7.750   1.1501   0.01318   0.00681  -0.0338   0.0614   1.0000
   8.000   1.1697   0.01364   0.00720  -0.0328   0.0522   1.0000
   8.250   1.1867   0.01431   0.00776  -0.0315   0.0355   1.0000
   8.500   1.2000   0.01529   0.00861  -0.0297   0.0155   1.0000
   8.750   1.2197   0.01577   0.00911  -0.0288   0.0135   1.0000
   9.000   1.2398   0.01622   0.00959  -0.0281   0.0124   1.0000
   9.250   1.2597   0.01666   0.01006  -0.0273   0.0117   1.0000
   9.500   1.2787   0.01716   0.01059  -0.0265   0.0109   1.0000
   9.750   1.2963   0.01773   0.01119  -0.0255   0.0102   1.0000
  10.000   1.3120   0.01831   0.01182  -0.0241   0.0096   1.0000
  10.250   1.3274   0.01884   0.01238  -0.0228   0.0092   1.0000
  10.500   1.3420   0.01944   0.01303  -0.0214   0.0089   1.0000
  10.750   1.3559   0.02013   0.01376  -0.0201   0.0085   1.0000
  11.000   1.3692   0.02090   0.01457  -0.0189   0.0082   1.0000
  11.250   1.3817   0.02177   0.01550  -0.0178   0.0079   1.0000
  11.500   1.3929   0.02280   0.01657  -0.0168   0.0075   1.0000
  11.750   1.4022   0.02404   0.01788  -0.0157   0.0072   1.0000
  12.000   1.4138   0.02515   0.01905  -0.0151   0.0071   1.0000
  12.250   1.4246   0.02640   0.02036  -0.0145   0.0069   1.0000
  12.500   1.4346   0.02778   0.02180  -0.0141   0.0068   1.0000
  12.750   1.4437   0.02927   0.02337  -0.0137   0.0066   1.0000
  13.000   1.4520   0.03089   0.02506  -0.0134   0.0064   1.0000
  13.250   1.4594   0.03263   0.02686  -0.0132   0.0062   1.0000
  13.500   1.4656   0.03452   0.02882  -0.0130   0.0060   1.0000
  13.750   1.4705   0.03659   0.03096  -0.0129   0.0059   1.0000
  14.000   1.4738   0.03884   0.03328  -0.0128   0.0057   1.0000
  14.250   1.4752   0.04136   0.03588  -0.0129   0.0056   1.0000
  14.500   1.4747   0.04414   0.03873  -0.0130   0.0055   1.0000
  14.750   1.4716   0.04726   0.04195  -0.0132   0.0054   1.0000
  15.000   1.4660   0.05081   0.04560  -0.0136   0.0053   1.0000
  15.250   1.4625   0.05423   0.04912  -0.0142   0.0052   1.0000
  15.500   1.4587   0.05781   0.05280  -0.0150   0.0052   1.0000
  15.750   1.4537   0.06166   0.05675  -0.0159   0.0051   1.0000
  16.000   1.4469   0.06587   0.06107  -0.0170   0.0051   1.0000
  16.250   1.4390   0.07030   0.06560  -0.0183   0.0051   1.0000
  16.500   1.4298   0.07506   0.07047  -0.0197   0.0050   1.0000
  16.750   1.4192   0.08010   0.07561  -0.0213   0.0050   1.0000
  17.000   1.4070   0.08545   0.08108  -0.0231   0.0049   1.0000
  17.250   1.3944   0.09097   0.08671  -0.0250   0.0049   1.0000
  17.500   1.3809   0.09674   0.09259  -0.0270   0.0049   1.0000
  17.750   1.3663   0.10268   0.09864  -0.0292   0.0048   1.0000
  18.000   1.3519   0.10869   0.10476  -0.0314   0.0048   1.0000
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