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AH 82-150 F (ah82150f-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: AH 82-150 F (ah82150f-il)
Reynolds number: 100,000
Max Cl/Cd: 33.49 at α=9°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ah82150f-il-100000-n5.txt
Download as CSV file: xf-ah82150f-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 82-150 F                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.1648   0.12174   0.11620  -0.1109   0.9071   0.0313
 -12.750  -0.1569   0.11833   0.11277  -0.1119   0.9055   0.0301
 -12.500  -0.1521   0.11460   0.10904  -0.1134   0.9040   0.0291
 -12.250  -0.1485   0.11079   0.10523  -0.1152   0.9025   0.0284
 -12.000  -0.1462   0.10691   0.10135  -0.1172   0.9011   0.0289
 -11.750  -0.1454   0.10316   0.09762  -0.1189   0.8994   0.0290
 -11.500  -0.1465   0.09921   0.09371  -0.1208   0.8975   0.0299
 -11.250  -0.1454   0.09551   0.09003  -0.1225   0.8957   0.0295
 -11.000  -0.1473   0.09125   0.08580  -0.1247   0.8939   0.0297
 -10.750  -0.1495   0.08697   0.08155  -0.1268   0.8919   0.0296
 -10.500  -0.1526   0.08253   0.07713  -0.1292   0.8899   0.0292
 -10.250  -0.1595   0.07727   0.07190  -0.1323   0.8880   0.0289
 -10.000  -0.1707   0.07163   0.06629  -0.1363   0.8856   0.0284
  -9.750  -0.1898   0.06654   0.06119  -0.1388   0.8827   0.0279
  -9.500  -0.2107   0.06273   0.05731  -0.1388   0.8798   0.0276
  -9.250  -0.2325   0.05964   0.05412  -0.1370   0.8769   0.0274
  -9.000  -0.2532   0.05719   0.05154  -0.1336   0.8742   0.0271
  -8.750  -0.2745   0.05550   0.04973  -0.1288   0.8706   0.0271
  -8.500  -0.2933   0.05381   0.04789  -0.1239   0.8673   0.0269
  -8.250  -0.3083   0.05186   0.04574  -0.1192   0.8645   0.0269
  -8.000  -0.3179   0.04950   0.04311  -0.1150   0.8620   0.0269
  -7.750  -0.3210   0.04698   0.04025  -0.1115   0.8599   0.0271
  -7.500  -0.3381   0.04619   0.03929  -0.1048   0.8561   0.0273
  -7.250  -0.3500   0.04503   0.03791  -0.0988   0.8525   0.0275
  -7.000  -0.3501   0.04310   0.03563  -0.0948   0.8497   0.0280
  -6.750  -0.3437   0.04102   0.03314  -0.0917   0.8479   0.0287
  -6.500  -0.3313   0.03906   0.03072  -0.0894   0.8465   0.0302
  -6.250  -0.3370   0.03853   0.02988  -0.0837   0.8427   0.0316
  -6.000  -0.3431   0.03804   0.02915  -0.0779   0.8388   0.0326
  -5.750  -0.3302   0.03665   0.02763  -0.0760   0.8366   0.0346
  -5.500  -0.3095   0.03548   0.02625  -0.0751   0.8349   0.0367
  -5.250  -0.2854   0.03433   0.02485  -0.0746   0.8336   0.0395
  -5.000  -0.2592   0.03360   0.02379  -0.0743   0.8325   0.0437
  -4.750  -0.2547   0.03293   0.02313  -0.0706   0.8290   0.0463
  -4.500  -0.2484   0.03256   0.02273  -0.0671   0.8253   0.0485
  -4.250  -0.2293   0.03204   0.02210  -0.0658   0.8229   0.0533
  -4.000  -0.2065   0.03143   0.02137  -0.0652   0.8210   0.0589
  -3.750  -0.1822   0.03082   0.02074  -0.0648   0.8194   0.0641
  -3.500  -0.1556   0.03033   0.02015  -0.0649   0.8181   0.0721
  -3.250  -0.1587   0.03045   0.02028  -0.0599   0.8126   0.0763
  -3.000  -0.1411   0.03022   0.01998  -0.0583   0.8094   0.0853
  -2.500  -0.0925   0.02933   0.01927  -0.0577   0.8054   0.1382
  -2.250  -0.0699   0.02825   0.01911  -0.0573   0.8041   0.3285
  -2.000  -0.0783   0.02793   0.01943  -0.0515   0.7973   0.4698
  -1.750  -0.0721   0.02831   0.02111  -0.0439   0.7943   0.8011
  -1.500  -0.0588   0.02862   0.02123  -0.0405   0.7916   0.8546
  -1.250  -0.0411   0.02920   0.02166  -0.0372   0.7891   0.8910
  -1.000   0.1129   0.03125   0.02337  -0.0597   0.7927   0.9520
  -0.750   0.1804   0.03148   0.02337  -0.0680   0.7922   0.9629
  -0.500   0.2276   0.03155   0.02329  -0.0722   0.7911   0.9707
  -0.250   0.2551   0.03182   0.02345  -0.0735   0.7863   0.9754
   0.000   0.2792   0.03201   0.02356  -0.0737   0.7815   0.9801
   0.250   0.3100   0.03203   0.02350  -0.0749   0.7789   0.9832
   0.500   0.3480   0.03194   0.02332  -0.0773   0.7771   0.9847
   1.000   0.3885   0.03233   0.02364  -0.0764   0.7659   0.9909
   1.250   0.4220   0.03222   0.02348  -0.0778   0.7636   0.9923
   1.750   0.4591   0.03259   0.02381  -0.0760   0.7518   0.9969
   2.000   0.4923   0.03240   0.02361  -0.0772   0.7495   0.9978
   2.500   0.5215   0.03265   0.02387  -0.0736   0.7368   1.0000
   2.750   0.5515   0.03237   0.02359  -0.0741   0.7345   1.0000
   3.000   0.5419   0.03277   0.02401  -0.0681   0.7236   1.0000
   3.250   0.5699   0.03248   0.02373  -0.0681   0.7210   1.0000
   3.500   0.5634   0.03282   0.02410  -0.0627   0.7102   1.0000
   4.000   0.5857   0.03279   0.02414  -0.0574   0.6964   1.0000
   4.500   0.6093   0.03266   0.02408  -0.0523   0.6825   1.0000
   4.750   0.6087   0.03291   0.02437  -0.0480   0.6719   1.0000
   5.000   0.6339   0.03245   0.02399  -0.0473   0.6685   1.0000
   5.250   0.6341   0.03268   0.02426  -0.0431   0.6576   1.0000
   5.500   0.6528   0.03236   0.02401  -0.0415   0.6524   1.0000
   5.750   0.6611   0.03234   0.02405  -0.0384   0.6434   1.0000
   6.250   0.6905   0.03193   0.02381  -0.0341   0.6293   1.0000
   6.500   0.7020   0.03196   0.02391  -0.0317   0.6204   1.0000
   6.750   0.7259   0.03150   0.02355  -0.0309   0.6151   1.0000
   7.000   0.7416   0.03156   0.02371  -0.0292   0.6059   1.0000
   7.250   0.7696   0.03101   0.02328  -0.0290   0.6007   1.0000
   7.750   0.8201   0.03040   0.02297  -0.0280   0.5858   1.0000
   8.000   0.8396   0.03052   0.02324  -0.0271   0.5750   1.0000
   8.250   0.8679   0.03014   0.02302  -0.0270   0.5667   1.0000
   8.500   0.8948   0.02947   0.02246  -0.0263   0.5482   1.0000
   8.750   0.9241   0.02800   0.02083  -0.0248   0.4974   1.0000
   9.000   0.9390   0.02804   0.02058  -0.0225   0.4387   1.0000
   9.250   0.9428   0.02899   0.02112  -0.0195   0.3706   1.0000
   9.500   0.9353   0.03087   0.02242  -0.0157   0.2812   1.0000
   9.750   0.9193   0.03367   0.02435  -0.0117   0.1614   1.0000
  10.000   0.9034   0.03692   0.02665  -0.0082   0.0506   1.0000
  10.250   0.9060   0.03889   0.02849  -0.0063   0.0339   1.0000
  10.500   0.9124   0.04059   0.03025  -0.0048   0.0289   1.0000
  10.750   0.9184   0.04236   0.03214  -0.0034   0.0259   1.0000
  11.000   0.9252   0.04410   0.03406  -0.0021   0.0245   1.0000
  11.250   0.9303   0.04604   0.03620  -0.0009   0.0231   1.0000
  11.500   0.9344   0.04809   0.03841   0.0003   0.0221   1.0000
  11.750   0.9381   0.05022   0.04068   0.0015   0.0214   1.0000
  12.000   0.9409   0.05250   0.04307   0.0026   0.0206   1.0000
  12.250   0.9426   0.05492   0.04558   0.0038   0.0195   1.0000
  12.500   0.9505   0.05685   0.04758   0.0048   0.0187   1.0000
  12.750   0.9621   0.05848   0.04935   0.0054   0.0175   1.0000
  13.000   0.9754   0.06004   0.05103   0.0061   0.0167   1.0000
  13.250   0.9926   0.06148   0.05259   0.0068   0.0161   1.0000
  13.500   1.0119   0.06297   0.05421   0.0075   0.0157   1.0000
  13.750   1.0303   0.06470   0.05616   0.0080   0.0153   1.0000
  14.000   1.0473   0.06683   0.05849   0.0085   0.0150   1.0000
  14.250   1.0597   0.06934   0.06124   0.0089   0.0148   1.0000
  14.500   1.0672   0.07225   0.06440   0.0094   0.0147   1.0000
  14.750   1.0699   0.07557   0.06799   0.0099   0.0146   1.0000
  15.000   1.0682   0.07924   0.07194   0.0102   0.0145   1.0000
  15.250   1.0634   0.08310   0.07606   0.0103   0.0144   1.0000
  15.500   1.0559   0.08730   0.08052   0.0101   0.0143   1.0000
  15.750   1.0471   0.09167   0.08510   0.0095   0.0141   1.0000
  16.000   1.0363   0.09643   0.09010   0.0085   0.0140   1.0000
  16.250   1.0238   0.10160   0.09551   0.0070   0.0140   1.0000
  16.500   1.0110   0.10695   0.10105   0.0051   0.0138   1.0000
  16.750   0.9906   0.11406   0.10848   0.0022   0.0142   1.0000
  17.000   0.9744   0.12073   0.11536  -0.0012   0.0141   1.0000
  17.250   0.9492   0.12987   0.12477  -0.0062   0.0146   1.0000
  17.500   0.9247   0.13981   0.13493  -0.0122   0.0150   1.0000
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