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WORTMANN FX 72-MS-150B AIRFOIL (fx72150b-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 72-MS-150B AIRFOIL (fx72150b-il)
Reynolds number: 200,000
Max Cl/Cd: 76.95 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx72150b-il-200000-n5.txt
Download as CSV file: xf-fx72150b-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 72-MS-150B AIRFOIL                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.000   0.2506   0.10645   0.10118  -0.1488   0.7292   0.0227
 -10.750   0.2562   0.10434   0.09903  -0.1502   0.7253   0.0228
 -10.500   0.2622   0.10230   0.09700  -0.1515   0.7206   0.0229
 -10.250   0.2706   0.09982   0.09451  -0.1523   0.7160   0.0230
 -10.000   0.2832   0.09706   0.09170  -0.1526   0.7118   0.0232
  -9.750   0.2933   0.09481   0.08941  -0.1532   0.7079   0.0236
  -9.500   0.3021   0.09269   0.08729  -0.1539   0.7033   0.0239
  -9.250   0.3108   0.09055   0.08515  -0.1547   0.6990   0.0246
  -9.000   0.3192   0.08845   0.08302  -0.1555   0.6950   0.0249
  -8.750   0.3272   0.08636   0.08090  -0.1563   0.6914   0.0256
  -8.500   0.3340   0.08427   0.07882  -0.1573   0.6872   0.0264
  -8.250   0.3377   0.08232   0.07688  -0.1586   0.6833   0.0268
  -8.000   0.3428   0.08039   0.07493  -0.1597   0.6796   0.0269
  -7.750   0.3443   0.07836   0.07289  -0.1613   0.6764   0.0270
  -7.500   0.3606   0.07582   0.07036  -0.1604   0.6724   0.0275
  -7.250   0.3714   0.07400   0.06853  -0.1604   0.6685   0.0284
  -7.000   0.3792   0.07220   0.06671  -0.1609   0.6649   0.0298
  -6.750   0.3812   0.07033   0.06483  -0.1620   0.6616   0.0314
  -6.500   0.3794   0.06855   0.06309  -0.1628   0.6582   0.0316
  -6.250   0.3798   0.06665   0.06125  -0.1641   0.6545   0.0318
  -6.000   0.3895   0.06446   0.05907  -0.1638   0.6511   0.0320
  -5.750   0.4007   0.06265   0.05723  -0.1633   0.6480   0.0324
  -5.500   0.4116   0.06082   0.05537  -0.1639   0.6453   0.0330
  -5.250   0.4222   0.05886   0.05341  -0.1653   0.6424   0.0337
  -5.000   0.4335   0.05677   0.05135  -0.1673   0.6392   0.0343
  -4.750   0.4475   0.05433   0.04892  -0.1705   0.6360   0.0353
  -4.500   0.4842   0.04803   0.04253  -0.1873   0.6330   0.0371
  -4.000   0.5536   0.03607   0.03015  -0.2057   0.6285   0.0226
  -3.750   0.5972   0.03181   0.02560  -0.2147   0.6259   0.0221
  -3.500   0.6537   0.02648   0.01959  -0.2257   0.6232   0.0232
  -3.250   0.6918   0.02448   0.01725  -0.2297   0.6205   0.0236
  -3.000   0.7348   0.02193   0.01407  -0.2343   0.6181   0.0233
  -2.750   0.7693   0.02075   0.01257  -0.2364   0.6158   0.0235
  -2.500   0.8024   0.01987   0.01142  -0.2380   0.6138   0.0240
  -2.000   0.8651   0.01859   0.00976  -0.2402   0.6096   0.0256
  -1.750   0.8946   0.01818   0.00925  -0.2409   0.6072   0.0276
  -1.500   0.9237   0.01793   0.00898  -0.2416   0.6047   0.0298
  -1.250   0.9537   0.01763   0.00860  -0.2424   0.6023   0.0315
  -1.000   0.9842   0.01738   0.00833  -0.2434   0.6001   0.0337
  -0.750   1.0147   0.01725   0.00812  -0.2443   0.5983   0.0377
  -0.500   1.0455   0.01718   0.00799  -0.2452   0.5966   0.0440
  -0.250   1.0757   0.01713   0.00790  -0.2461   0.5949   0.0548
   0.000   1.1048   0.01706   0.00794  -0.2469   0.5929   0.0880
   0.250   1.1372   0.01666   0.00815  -0.2488   0.5909   0.3245
   0.500   1.1642   0.01677   0.00855  -0.2490   0.5889   0.4885
   0.750   1.1901   0.01702   0.00882  -0.2489   0.5870   0.5357
   1.000   1.2158   0.01727   0.00907  -0.2486   0.5850   0.5725
   1.250   1.2417   0.01747   0.00926  -0.2484   0.5831   0.5960
   1.500   1.2695   0.01765   0.00933  -0.2486   0.5813   0.6069
   1.750   1.2977   0.01780   0.00942  -0.2490   0.5798   0.6133
   2.000   1.3222   0.01805   0.00967  -0.2488   0.5778   0.6201
   2.250   1.3466   0.01831   0.00994  -0.2486   0.5760   0.6261
   2.500   1.3713   0.01856   0.01021  -0.2484   0.5742   0.6308
   2.750   1.3964   0.01881   0.01047  -0.2483   0.5725   0.6362
   3.000   1.4218   0.01906   0.01071  -0.2483   0.5708   0.6418
   3.250   1.4473   0.01929   0.01094  -0.2483   0.5691   0.6473
   3.500   1.4734   0.01951   0.01117  -0.2484   0.5676   0.6544
   3.750   1.5000   0.01973   0.01137  -0.2485   0.5661   0.6610
   4.000   1.5275   0.01994   0.01157  -0.2489   0.5648   0.6681
   4.250   1.5543   0.02020   0.01182  -0.2491   0.5636   0.6757
   4.500   1.5742   0.02060   0.01234  -0.2482   0.5620   0.6837
   4.750   1.5944   0.02101   0.01282  -0.2474   0.5603   0.6933
   5.000   1.6149   0.02140   0.01330  -0.2466   0.5586   0.7048
   5.250   1.6356   0.02178   0.01376  -0.2458   0.5570   0.7183
   5.500   1.6567   0.02214   0.01422  -0.2451   0.5555   0.7351
   5.750   1.6779   0.02245   0.01464  -0.2444   0.5540   0.7600
   6.000   1.6952   0.02255   0.01496  -0.2428   0.5526   0.9145
   6.250   1.7199   0.02291   0.01533  -0.2428   0.5514   1.0000
   6.500   1.7457   0.02323   0.01567  -0.2430   0.5501   1.0000
   6.750   1.7734   0.02352   0.01595  -0.2435   0.5488   1.0000
   7.000   1.7912   0.02407   0.01658  -0.2424   0.5470   1.0000
   7.250   1.7902   0.02502   0.01767  -0.2381   0.5444   1.0000
   7.500   1.7943   0.02592   0.01870  -0.2348   0.5419   1.0000
   7.750   1.8041   0.02676   0.01962  -0.2326   0.5398   1.0000
   8.000   1.8178   0.02748   0.02042  -0.2310   0.5379   1.0000
   8.250   1.8366   0.02802   0.02102  -0.2301   0.5362   1.0000
   8.500   1.8600   0.02838   0.02143  -0.2299   0.5346   1.0000
   8.750   1.8882   0.02857   0.02166  -0.2304   0.5331   1.0000
   9.000   1.9062   0.02916   0.02233  -0.2295   0.5312   1.0000
   9.250   1.8414   0.03369   0.02714  -0.2181   0.5244   1.0000
   9.500   1.8442   0.03525   0.02879  -0.2156   0.5213   1.0000
   9.750   1.8632   0.03584   0.02947  -0.2150   0.5194   1.0000
  10.000   1.8941   0.03561   0.02929  -0.2156   0.5177   1.0000
  10.250   1.7872   0.04570   0.03964  -0.2033   0.5059   1.0000
  10.500   1.8109   0.04581   0.03983  -0.2031   0.5039   1.0000
  10.750   1.8518   0.04431   0.03837  -0.2042   0.5025   1.0000
  11.000   1.9065   0.04163   0.03570  -0.2065   0.5008   1.0000
  11.250   1.6189   0.07560   0.07001  -0.1882   0.4608   1.0000
  11.500   1.6411   0.07561   0.07010  -0.1878   0.4588   1.0000
  11.750   1.6700   0.07469   0.06925  -0.1877   0.4575   1.0000
  12.000   1.7072   0.07255   0.06719  -0.1878   0.4565   1.0000
  12.250   1.7473   0.07015   0.06485  -0.1880   0.4554   1.0000
  13.250   1.6959   0.08919   0.08430  -0.1829   0.4141   1.0000
  13.750   1.7297   0.09037   0.08559  -0.1819   0.3945   1.0000
  14.000   1.7211   0.09479   0.09008  -0.1811   0.3776   1.0000
  14.250   1.7807   0.08873   0.08377  -0.1810   0.3510   1.0000
  14.500   1.7953   0.08935   0.08417  -0.1802   0.3235   1.0000
  15.000   1.7780   0.09757   0.09198  -0.1781   0.2641   1.0000
  15.250   1.7618   0.10297   0.09720  -0.1773   0.2345   1.0000
  15.500   1.7451   0.10858   0.10264  -0.1767   0.2071   1.0000
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