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DU 06-W-200 VAWT airfoil (du06-w-200-dt) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: DU 06-W-200 VAWT airfoil (du06-w-200-dt)
Reynolds number: 500,000
Max Cl/Cd: 71.48 at α=9.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-du06-w-200-dt-500000.txt
Download as CSV file: xf-du06-w-200-dt-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: DU 06-W-200  VAWT 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -1.2255   0.10610   0.10160   0.0051   1.0000   0.0326
 -19.250  -1.2361   0.10094   0.09637   0.0029   1.0000   0.0335
 -19.000  -1.2443   0.09621   0.09156   0.0011   1.0000   0.0345
 -18.750  -1.2497   0.09193   0.08719  -0.0005   1.0000   0.0356
 -18.500  -1.2529   0.08804   0.08320  -0.0019   1.0000   0.0366
 -18.250  -1.2643   0.08303   0.07814  -0.0036   1.0000   0.0378
 -18.000  -1.2725   0.07854   0.07359  -0.0051   1.0000   0.0390
 -17.750  -1.2774   0.07458   0.06956  -0.0063   1.0000   0.0403
 -17.500  -1.2787   0.07112   0.06602  -0.0073   1.0000   0.0418
 -17.250  -1.2804   0.06766   0.06248  -0.0082   1.0000   0.0432
 -17.000  -1.2862   0.06375   0.05853  -0.0092   1.0000   0.0449
 -16.750  -1.2876   0.06045   0.05518  -0.0099   1.0000   0.0467
 -16.500  -1.2850   0.05766   0.05232  -0.0105   1.0000   0.0487
 -16.250  -1.2840   0.05474   0.04933  -0.0110   1.0000   0.0507
 -16.000  -1.2844   0.05174   0.04632  -0.0114   1.0000   0.0530
 -15.750  -1.2804   0.04929   0.04382  -0.0117   1.0000   0.0556
 -15.500  -1.2739   0.04714   0.04160  -0.0118   1.0000   0.0580
 -15.250  -1.2729   0.04449   0.03894  -0.0119   1.0000   0.0609
 -15.000  -1.2667   0.04244   0.03687  -0.0119   1.0000   0.0640
 -14.750  -1.2577   0.04068   0.03505  -0.0118   1.0000   0.0670
 -14.500  -1.2542   0.03848   0.03286  -0.0117   1.0000   0.0706
 -14.250  -1.2451   0.03686   0.03122  -0.0114   1.0000   0.0744
 -14.000  -1.2366   0.03525   0.02957  -0.0111   1.0000   0.0781
 -13.750  -1.2296   0.03355   0.02789  -0.0107   1.0000   0.0824
 -13.500  -1.2174   0.03229   0.02659  -0.0103   1.0000   0.0866
 -13.250  -1.2091   0.03072   0.02504  -0.0098   1.0000   0.0912
 -13.000  -1.1983   0.02937   0.02370  -0.0094   1.0000   0.0959
 -12.750  -1.1838   0.02832   0.02260  -0.0091   1.0000   0.1002
 -12.500  -1.1744   0.02687   0.02119  -0.0086   1.0000   0.1054
 -12.250  -1.1598   0.02584   0.02014  -0.0082   1.0000   0.1104
 -12.000  -1.1460   0.02473   0.01903  -0.0078   1.0000   0.1153
 -11.750  -1.1325   0.02360   0.01793  -0.0074   1.0000   0.1208
 -11.500  -1.1143   0.02282   0.01711  -0.0072   1.0000   0.1258
 -11.250  -1.1014   0.02164   0.01598  -0.0067   1.0000   0.1321
 -11.000  -1.0840   0.02078   0.01513  -0.0065   1.0000   0.1382
 -10.750  -1.0676   0.01986   0.01423  -0.0062   1.0000   0.1443
 -10.500  -1.0506   0.01898   0.01338  -0.0060   1.0000   0.1514
 -10.250  -1.0328   0.01818   0.01260  -0.0058   1.0000   0.1584
 -10.000  -1.0164   0.01733   0.01180  -0.0055   1.0000   0.1663
  -9.750  -0.9867   0.01661   0.01105  -0.0074   0.9308   0.1752
  -9.500  -0.9696   0.01603   0.01036  -0.0065   0.8813   0.1834
  -9.250  -0.9497   0.01545   0.00969  -0.0061   0.8497   0.1923
  -9.000  -0.9269   0.01507   0.00920  -0.0058   0.8279   0.2017
  -8.750  -0.9045   0.01453   0.00865  -0.0058   0.8103   0.2124
  -8.500  -0.8802   0.01412   0.00820  -0.0058   0.7953   0.2228
  -8.250  -0.8549   0.01376   0.00779  -0.0059   0.7820   0.2340
  -8.000  -0.8301   0.01332   0.00736  -0.0059   0.7698   0.2464
  -7.750  -0.8046   0.01295   0.00697  -0.0060   0.7580   0.2591
  -7.500  -0.7782   0.01258   0.00662  -0.0062   0.7465   0.2725
  -7.250  -0.7516   0.01226   0.00628  -0.0064   0.7361   0.2867
  -7.000  -0.7247   0.01192   0.00596  -0.0066   0.7254   0.3021
  -6.750  -0.6975   0.01159   0.00565  -0.0069   0.7152   0.3187
  -6.500  -0.6703   0.01129   0.00536  -0.0072   0.7050   0.3356
  -6.250  -0.6424   0.01099   0.00509  -0.0075   0.6941   0.3526
  -6.000  -0.6145   0.01072   0.00483  -0.0078   0.6836   0.3705
  -5.750  -0.5862   0.01046   0.00459  -0.0081   0.6720   0.3882
  -5.500  -0.5577   0.01023   0.00438  -0.0084   0.6607   0.4053
  -5.250  -0.5291   0.01003   0.00418  -0.0087   0.6500   0.4228
  -5.000  -0.5002   0.00984   0.00399  -0.0091   0.6385   0.4399
  -4.750  -0.4711   0.00966   0.00382  -0.0094   0.6274   0.4566
  -4.250  -0.4128   0.00937   0.00352  -0.0101   0.6058   0.4892
  -4.000  -0.3836   0.00924   0.00340  -0.0104   0.5964   0.5057
  -3.750  -0.3543   0.00912   0.00330  -0.0108   0.5869   0.5220
  -3.500  -0.3250   0.00904   0.00325  -0.0111   0.5785   0.5393
  -3.250  -0.2954   0.00901   0.00325  -0.0114   0.5703   0.5567
  -3.000  -0.2657   0.00906   0.00329  -0.0116   0.5630   0.5729
  -2.750  -0.2355   0.00911   0.00334  -0.0120   0.5558   0.5871
  -2.500  -0.2055   0.00924   0.00343  -0.0123   0.5492   0.5984
  -2.250  -0.1753   0.00936   0.00354  -0.0126   0.5430   0.6080
  -2.000  -0.1448   0.00947   0.00359  -0.0130   0.5367   0.6174
  -1.750  -0.1150   0.00964   0.00371  -0.0132   0.5310   0.6232
  -1.500  -0.0847   0.00979   0.00384  -0.0135   0.5259   0.6297
  -1.250  -0.0542   0.00991   0.00391  -0.0139   0.5204   0.6364
  -1.000  -0.0245   0.01008   0.00407  -0.0141   0.5149   0.6405
  -0.750   0.0054   0.01026   0.00422  -0.0143   0.5099   0.6452
  -0.500   0.0360   0.01038   0.00429  -0.0148   0.5050   0.6510
  -0.250   0.0657   0.01049   0.00441  -0.0149   0.5001   0.6546
   0.000   0.0952   0.01070   0.00457  -0.0151   0.4951   0.6580
   0.250   0.1253   0.01082   0.00472  -0.0153   0.4906   0.6620
   0.500   0.1555   0.01093   0.00480  -0.0157   0.4854   0.6668
   0.750   0.1853   0.01102   0.00485  -0.0160   0.4805   0.6703
   1.000   0.2146   0.01118   0.00501  -0.0161   0.4759   0.6729
   1.250   0.2444   0.01127   0.00514  -0.0163   0.4714   0.6759
   1.500   0.2741   0.01136   0.00523  -0.0166   0.4664   0.6791
   1.750   0.3039   0.01149   0.00530  -0.0169   0.4614   0.6826
   2.000   0.3343   0.01159   0.00538  -0.0174   0.4566   0.6859
   2.250   0.3635   0.01156   0.00540  -0.0175   0.4513   0.6882
   2.500   0.3928   0.01164   0.00547  -0.0177   0.4462   0.6903
   2.750   0.4220   0.01176   0.00558  -0.0179   0.4410   0.6926
   3.000   0.4517   0.01179   0.00566  -0.0182   0.4351   0.6951
   3.250   0.4812   0.01186   0.00571  -0.0185   0.4291   0.6979
   3.500   0.5109   0.01195   0.00577  -0.0188   0.4232   0.7005
   3.750   0.5412   0.01200   0.00582  -0.0193   0.4168   0.7027
   4.000   0.5700   0.01200   0.00581  -0.0195   0.4104   0.7047
   4.250   0.5990   0.01203   0.00588  -0.0197   0.4036   0.7064
   4.500   0.6280   0.01209   0.00596  -0.0199   0.3960   0.7083
   4.750   0.6568   0.01219   0.00605  -0.0201   0.3887   0.7102
   5.000   0.6859   0.01226   0.00613  -0.0204   0.3799   0.7123
   5.250   0.7148   0.01236   0.00622  -0.0206   0.3715   0.7144
   5.500   0.7438   0.01247   0.00631  -0.0209   0.3624   0.7164
   5.750   0.7727   0.01260   0.00642  -0.0213   0.3531   0.7183
   6.000   0.8012   0.01279   0.00655  -0.0215   0.3426   0.7199
   6.250   0.8292   0.01285   0.00662  -0.0217   0.3322   0.7216
   6.500   0.8564   0.01303   0.00679  -0.0217   0.3221   0.7233
   6.750   0.8835   0.01325   0.00699  -0.0217   0.3113   0.7250
   7.000   0.9109   0.01345   0.00720  -0.0218   0.3017   0.7268
   7.250   0.9374   0.01373   0.00743  -0.0218   0.2922   0.7283
   7.500   0.9649   0.01394   0.00765  -0.0220   0.2829   0.7299
   7.750   0.9913   0.01423   0.00791  -0.0220   0.2737   0.7314
   8.000   1.0180   0.01449   0.00815  -0.0221   0.2646   0.7327
   8.250   1.0443   0.01478   0.00842  -0.0221   0.2562   0.7339
   8.500   1.0701   0.01510   0.00872  -0.0221   0.2476   0.7352
   8.750   1.0959   0.01542   0.00904  -0.0221   0.2402   0.7364
   9.000   1.1212   0.01573   0.00934  -0.0221   0.2326   0.7374
   9.250   1.1456   0.01606   0.00967  -0.0219   0.2254   0.7385
   9.500   1.1701   0.01637   0.01000  -0.0217   0.2182   0.7395
   9.750   1.1926   0.01682   0.01043  -0.0213   0.2114   0.7406
  10.000   1.2170   0.01713   0.01079  -0.0211   0.2053   0.7417
  10.250   1.2382   0.01763   0.01128  -0.0205   0.1987   0.7428
  10.500   1.2605   0.01804   0.01173  -0.0201   0.1930   0.7442
  10.750   1.2817   0.01850   0.01221  -0.0196   0.1872   0.7457
  11.000   1.2983   0.01919   0.01287  -0.0186   0.1811   0.7471
  11.250   1.3186   0.01957   0.01333  -0.0179   0.1766   0.7484
  11.500   1.3331   0.02018   0.01396  -0.0166   0.1717   0.7497
  11.750   1.3452   0.02116   0.01491  -0.0155   0.1665   0.7510
  12.000   1.3635   0.02182   0.01564  -0.0151   0.1625   0.7522
  12.250   1.3783   0.02275   0.01661  -0.0146   0.1579   0.7534
  12.500   1.3885   0.02405   0.01793  -0.0141   0.1535   0.7547
  12.750   1.4008   0.02527   0.01921  -0.0138   0.1495   0.7561
  13.000   1.4145   0.02645   0.02047  -0.0137   0.1453   0.7575
  13.250   1.4233   0.02809   0.02213  -0.0136   0.1411   0.7589
  13.500   1.4273   0.03020   0.02426  -0.0135   0.1369   0.7604
  13.750   1.4407   0.03151   0.02567  -0.0135   0.1334   0.7621
  14.000   1.4485   0.03336   0.02758  -0.0136   0.1295   0.7640
  14.250   1.4507   0.03575   0.02998  -0.0137   0.1257   0.7658
  14.500   1.4535   0.03811   0.03239  -0.0138   0.1223   0.7675
  14.750   1.4613   0.04002   0.03438  -0.0140   0.1191   0.7691
  15.000   1.4637   0.04250   0.03690  -0.0142   0.1156   0.7705
  15.250   1.4609   0.04549   0.03993  -0.0145   0.1122   0.7721
  15.500   1.4598   0.04831   0.04282  -0.0148   0.1092   0.7739
  15.750   1.4638   0.05067   0.04528  -0.0151   0.1063   0.7757
  16.000   1.4634   0.05358   0.04826  -0.0156   0.1033   0.7775
  16.250   1.4594   0.05694   0.05166  -0.0163   0.1006   0.7794
  16.500   1.4521   0.06073   0.05548  -0.0170   0.0978   0.7813
  16.750   1.4555   0.06336   0.05821  -0.0176   0.0959   0.7835
  17.000   1.4560   0.06635   0.06128  -0.0183   0.0935   0.7856
  17.250   1.4527   0.06985   0.06484  -0.0191   0.0910   0.7876
  17.500   1.4463   0.07374   0.06879  -0.0202   0.0887   0.7898
  17.750   1.4373   0.07794   0.07302  -0.0213   0.0860   0.7921
  18.000   1.4384   0.08101   0.07621  -0.0221   0.0841   0.7948
  18.250   1.4364   0.08450   0.07980  -0.0232   0.0818   0.7977
  18.500   1.4312   0.08844   0.08380  -0.0244   0.0794   0.8006
  18.750   1.4217   0.09298   0.08839  -0.0259   0.0772   0.8035
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