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DU 06-W-200 VAWT airfoil (du06-w-200-dt) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: DU 06-W-200 VAWT airfoil (du06-w-200-dt)
Reynolds number: 500,000
Max Cl/Cd: 71.17 at α=9°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-du06-w-200-dt-500000-n5.txt
Download as CSV file: xf-du06-w-200-dt-500000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.250  -1.2295   0.10199   0.09716   0.0038   1.0000   0.0233
 -19.000  -1.2395   0.09694   0.09203   0.0018   1.0000   0.0239
 -18.750  -1.2480   0.09220   0.08721   0.0000   1.0000   0.0247
 -18.500  -1.2549   0.08776   0.08267  -0.0016   1.0000   0.0255
 -18.250  -1.2602   0.08357   0.07840  -0.0031   1.0000   0.0263
 -18.000  -1.2651   0.07950   0.07425  -0.0044   1.0000   0.0271
 -17.750  -1.2709   0.07538   0.07005  -0.0057   1.0000   0.0279
 -17.500  -1.2748   0.07157   0.06617  -0.0068   1.0000   0.0289
 -17.250  -1.2768   0.06805   0.06257  -0.0078   1.0000   0.0301
 -17.000  -1.2768   0.06482   0.05928  -0.0086   1.0000   0.0312
 -16.750  -1.2781   0.06151   0.05590  -0.0094   1.0000   0.0323
 -16.500  -1.2779   0.05841   0.05274  -0.0101   1.0000   0.0337
 -16.250  -1.2758   0.05560   0.04988  -0.0106   1.0000   0.0354
 -16.000  -1.2721   0.05302   0.04724  -0.0110   1.0000   0.0369
 -15.750  -1.2702   0.05030   0.04448  -0.0113   1.0000   0.0386
 -15.500  -1.2660   0.04789   0.04202  -0.0116   1.0000   0.0407
 -15.250  -1.2593   0.04579   0.03987  -0.0117   1.0000   0.0426
 -15.000  -1.2547   0.04354   0.03760  -0.0117   1.0000   0.0449
 -14.750  -1.2485   0.04149   0.03553  -0.0117   1.0000   0.0475
 -14.500  -1.2404   0.03969   0.03368  -0.0116   1.0000   0.0501
 -14.250  -1.2342   0.03777   0.03176  -0.0114   1.0000   0.0533
 -14.000  -1.2253   0.03616   0.03013  -0.0111   1.0000   0.0566
 -13.750  -1.2177   0.03449   0.02845  -0.0107   1.0000   0.0599
 -13.500  -1.2086   0.03298   0.02693  -0.0103   1.0000   0.0639
 -13.250  -1.1979   0.03159   0.02553  -0.0099   1.0000   0.0674
 -13.000  -1.1880   0.03016   0.02411  -0.0095   1.0000   0.0715
 -12.750  -1.1754   0.02895   0.02288  -0.0091   1.0000   0.0754
 -12.500  -1.1632   0.02771   0.02165  -0.0087   1.0000   0.0793
 -12.250  -1.1504   0.02653   0.02047  -0.0083   1.0000   0.0835
 -12.000  -1.1348   0.02555   0.01947  -0.0080   1.0000   0.0872
 -11.750  -1.1213   0.02442   0.01836  -0.0076   1.0000   0.0915
 -11.500  -1.1059   0.02342   0.01737  -0.0072   1.0000   0.0964
 -11.250  -1.0879   0.02255   0.01646  -0.0073   0.9513   0.1008
 -11.000  -1.0775   0.02176   0.01554  -0.0056   0.8695   0.1056
 -10.750  -1.0628   0.02106   0.01468  -0.0046   0.8300   0.1105
 -10.500  -1.0463   0.02026   0.01381  -0.0040   0.8052   0.1161
 -10.250  -1.0286   0.01948   0.01297  -0.0037   0.7869   0.1229
 -10.000  -1.0099   0.01874   0.01217  -0.0036   0.7718   0.1290
  -9.750  -0.9919   0.01802   0.01141  -0.0033   0.7581   0.1355
  -9.500  -0.9713   0.01739   0.01072  -0.0033   0.7457   0.1415
  -9.250  -0.9495   0.01668   0.01000  -0.0037   0.7346   0.1495
  -9.000  -0.9257   0.01614   0.00940  -0.0041   0.7242   0.1571
  -8.750  -0.9020   0.01560   0.00887  -0.0043   0.7150   0.1655
  -8.500  -0.8773   0.01518   0.00841  -0.0044   0.7056   0.1729
  -8.250  -0.8523   0.01474   0.00797  -0.0046   0.6967   0.1821
  -8.000  -0.8268   0.01436   0.00756  -0.0048   0.6873   0.1905
  -7.750  -0.8007   0.01399   0.00719  -0.0050   0.6776   0.2003
  -7.500  -0.7747   0.01362   0.00682  -0.0052   0.6677   0.2101
  -7.250  -0.7478   0.01330   0.00648  -0.0054   0.6576   0.2201
  -7.000  -0.7210   0.01297   0.00616  -0.0057   0.6483   0.2317
  -6.750  -0.6940   0.01263   0.00584  -0.0060   0.6381   0.2439
  -6.500  -0.6665   0.01234   0.00554  -0.0063   0.6283   0.2556
  -6.000  -0.6110   0.01180   0.00500  -0.0069   0.6068   0.2815
  -5.750  -0.5830   0.01154   0.00474  -0.0072   0.5958   0.2955
  -5.500  -0.5548   0.01129   0.00450  -0.0076   0.5847   0.3094
  -5.250  -0.5264   0.01105   0.00428  -0.0079   0.5752   0.3253
  -5.000  -0.4979   0.01083   0.00406  -0.0083   0.5660   0.3414
  -4.750  -0.4692   0.01061   0.00387  -0.0087   0.5575   0.3582
  -4.500  -0.4403   0.01043   0.00369  -0.0091   0.5488   0.3743
  -4.250  -0.4112   0.01025   0.00353  -0.0095   0.5412   0.3906
  -4.000  -0.3820   0.01009   0.00338  -0.0099   0.5339   0.4066
  -3.750  -0.3526   0.00996   0.00325  -0.0104   0.5275   0.4211
  -3.250  -0.2936   0.00970   0.00302  -0.0112   0.5149   0.4522
  -3.000  -0.2641   0.00958   0.00292  -0.0116   0.5096   0.4678
  -2.750  -0.2344   0.00945   0.00284  -0.0120   0.5041   0.4828
  -2.500  -0.2048   0.00935   0.00276  -0.0124   0.4987   0.4983
  -2.250  -0.1752   0.00927   0.00271  -0.0128   0.4939   0.5157
  -2.000  -0.1454   0.00918   0.00268  -0.0132   0.4890   0.5331
  -1.750  -0.1155   0.00914   0.00269  -0.0136   0.4840   0.5493
  -1.500  -0.0857   0.00916   0.00273  -0.0139   0.4794   0.5663
  -1.250  -0.0557   0.00921   0.00281  -0.0143   0.4753   0.5817
  -1.000  -0.0254   0.00925   0.00286  -0.0146   0.4705   0.5925
  -0.750   0.0049   0.00931   0.00289  -0.0151   0.4655   0.6020
  -0.500   0.0348   0.00941   0.00297  -0.0154   0.4611   0.6094
  -0.250   0.0652   0.00947   0.00301  -0.0158   0.4570   0.6167
   0.000   0.0955   0.00954   0.00307  -0.0162   0.4525   0.6218
   0.250   0.1256   0.00963   0.00315  -0.0165   0.4477   0.6270
   0.500   0.1557   0.00973   0.00319  -0.0169   0.4428   0.6324
   0.750   0.1860   0.00978   0.00323  -0.0173   0.4384   0.6364
   1.000   0.2160   0.00986   0.00332  -0.0176   0.4336   0.6396
   1.250   0.2460   0.00996   0.00340  -0.0179   0.4289   0.6430
   1.500   0.2759   0.01005   0.00347  -0.0183   0.4243   0.6464
   1.750   0.3062   0.01011   0.00351  -0.0187   0.4192   0.6497
   2.000   0.3363   0.01019   0.00356  -0.0191   0.4136   0.6525
   2.250   0.3658   0.01028   0.00364  -0.0194   0.4081   0.6545
   2.500   0.3957   0.01035   0.00373  -0.0197   0.4027   0.6566
   2.750   0.4254   0.01043   0.00381  -0.0200   0.3964   0.6588
   3.000   0.4550   0.01054   0.00390  -0.0203   0.3898   0.6612
   3.250   0.4848   0.01062   0.00397  -0.0207   0.3819   0.6634
   3.500   0.5142   0.01074   0.00405  -0.0210   0.3742   0.6656
   3.750   0.5440   0.01083   0.00413  -0.0214   0.3665   0.6675
   4.000   0.5732   0.01097   0.00421  -0.0217   0.3580   0.6693
   4.250   0.6023   0.01106   0.00432  -0.0220   0.3485   0.6709
   4.500   0.6311   0.01122   0.00445  -0.0222   0.3390   0.6725
   4.750   0.6598   0.01137   0.00459  -0.0224   0.3290   0.6741
   5.000   0.6883   0.01155   0.00475  -0.0226   0.3190   0.6757
   5.250   0.7165   0.01177   0.00492  -0.0228   0.3088   0.6775
   5.500   0.7451   0.01194   0.00509  -0.0230   0.3001   0.6793
   5.750   0.7731   0.01217   0.00529  -0.0232   0.2912   0.6815
   6.000   0.8013   0.01239   0.00548  -0.0234   0.2815   0.6836
   6.250   0.8291   0.01264   0.00570  -0.0236   0.2725   0.6854
   6.500   0.8567   0.01288   0.00590  -0.0237   0.2632   0.6865
   6.750   0.8841   0.01310   0.00612  -0.0238   0.2548   0.6875
   7.000   0.9111   0.01336   0.00637  -0.0238   0.2465   0.6887
   7.250   0.9383   0.01359   0.00662  -0.0239   0.2399   0.6898
   7.500   0.9652   0.01386   0.00688  -0.0240   0.2322   0.6907
   7.750   0.9916   0.01415   0.00717  -0.0240   0.2250   0.6917
   8.000   1.0180   0.01443   0.00745  -0.0240   0.2174   0.6926
   8.250   1.0437   0.01477   0.00777  -0.0239   0.2106   0.6936
   8.500   1.0698   0.01506   0.00807  -0.0239   0.2037   0.6946
   8.750   1.0946   0.01544   0.00844  -0.0237   0.1973   0.6957
   9.000   1.1202   0.01574   0.00876  -0.0236   0.1921   0.6970
   9.250   1.1448   0.01610   0.00913  -0.0234   0.1858   0.6982
   9.500   1.1685   0.01653   0.00954  -0.0232   0.1799   0.6993
   9.750   1.1928   0.01688   0.00992  -0.0229   0.1746   0.7003
  10.000   1.2155   0.01732   0.01036  -0.0226   0.1692   0.7012
  10.250   1.2375   0.01779   0.01084  -0.0221   0.1643   0.7021
  10.750   1.2794   0.01875   0.01184  -0.0210   0.1541   0.7040
  11.000   1.2980   0.01931   0.01242  -0.0202   0.1498   0.7050
  11.250   1.3141   0.01982   0.01300  -0.0190   0.1457   0.7060
  11.500   1.3295   0.02053   0.01374  -0.0180   0.1415   0.7071
  11.750   1.3430   0.02147   0.01470  -0.0171   0.1374   0.7082
  12.000   1.3591   0.02228   0.01557  -0.0166   0.1341   0.7094
  12.250   1.3734   0.02328   0.01663  -0.0161   0.1303   0.7107
  12.500   1.3850   0.02456   0.01795  -0.0157   0.1265   0.7121
  12.750   1.3949   0.02607   0.01949  -0.0155   0.1229   0.7136
  13.000   1.4076   0.02740   0.02088  -0.0154   0.1195   0.7150
  13.250   1.4174   0.02902   0.02255  -0.0154   0.1156   0.7162
  13.500   1.4234   0.03104   0.02459  -0.0154   0.1118   0.7174
  13.750   1.4304   0.03297   0.02658  -0.0154   0.1085   0.7186
  14.000   1.4375   0.03492   0.02858  -0.0155   0.1050   0.7197
  14.250   1.4406   0.03727   0.03098  -0.0156   0.1012   0.7209
  14.500   1.4400   0.04002   0.03378  -0.0158   0.0979   0.7221
  14.750   1.4440   0.04232   0.03616  -0.0159   0.0951   0.7233
  15.000   1.4452   0.04494   0.03884  -0.0162   0.0918   0.7246
  15.250   1.4424   0.04800   0.04195  -0.0165   0.0885   0.7259
  15.500   1.4378   0.05131   0.04531  -0.0170   0.0857   0.7272
  15.750   1.4384   0.05410   0.04818  -0.0174   0.0830   0.7286
  16.000   1.4361   0.05730   0.05144  -0.0179   0.0800   0.7300
  16.250   1.4314   0.06085   0.05504  -0.0187   0.0773   0.7313
  16.500   1.4258   0.06456   0.05881  -0.0195   0.0749   0.7327
  16.750   1.4245   0.06779   0.06212  -0.0202   0.0731   0.7341
  17.000   1.4218   0.07123   0.06563  -0.0210   0.0710   0.7355
  17.250   1.4172   0.07496   0.06942  -0.0220   0.0689   0.7367
  17.500   1.4100   0.07905   0.07357  -0.0231   0.0669   0.7381
  17.750   1.4031   0.08317   0.07776  -0.0243   0.0651   0.7396
  18.000   1.4007   0.08673   0.08141  -0.0253   0.0631   0.7413
  18.250   1.3946   0.09083   0.08559  -0.0266   0.0610   0.7431
  18.500   1.3860   0.09531   0.09015  -0.0280   0.0588   0.7449
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