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DU 06-W-200 VAWT airfoil (du06-w-200-dt) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: DU 06-W-200 VAWT airfoil (du06-w-200-dt)
Reynolds number: 100,000
Max Cl/Cd: 36.15 at α=9.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-du06-w-200-dt-100000-n5.txt
Download as CSV file: xf-du06-w-200-dt-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -0.9673   0.13320   0.12733   0.0094   1.0000   0.0650
 -18.500  -0.9997   0.12281   0.11670   0.0035   1.0000   0.0667
 -18.250  -0.9926   0.12048   0.11444   0.0025   1.0000   0.0689
 -18.000  -1.0015   0.11504   0.10892  -0.0004   1.0000   0.0710
 -17.750  -1.0177   0.10830   0.10202  -0.0038   1.0000   0.0732
 -17.500  -1.0356   0.10144   0.09493  -0.0072   1.0000   0.0755
 -17.250  -1.0406   0.09709   0.09053  -0.0090   1.0000   0.0777
 -17.000  -1.0439   0.09307   0.08649  -0.0107   1.0000   0.0801
 -16.750  -1.0503   0.08854   0.08185  -0.0126   1.0000   0.0827
 -16.500  -1.0586   0.08374   0.07686  -0.0146   1.0000   0.0856
 -16.250  -1.0632   0.07967   0.07268  -0.0160   1.0000   0.0884
 -16.000  -1.0641   0.07631   0.06931  -0.0171   1.0000   0.0912
 -15.750  -1.0668   0.07266   0.06558  -0.0184   1.0000   0.0944
 -15.500  -1.0700   0.06896   0.06170  -0.0195   1.0000   0.0980
 -15.250  -1.0697   0.06593   0.05863  -0.0202   1.0000   0.1013
 -15.000  -1.0691   0.06301   0.05568  -0.0209   1.0000   0.1048
 -14.750  -1.0688   0.06006   0.05262  -0.0216   1.0000   0.1089
 -14.500  -1.0674   0.05730   0.04972  -0.0220   1.0000   0.1130
 -14.250  -1.0641   0.05497   0.04743  -0.0222   1.0000   0.1169
 -14.000  -1.0614   0.05260   0.04495  -0.0224   1.0000   0.1214
 -13.750  -1.0578   0.05031   0.04251  -0.0225   1.0000   0.1262
 -13.500  -1.0524   0.04840   0.04066  -0.0223   1.0000   0.1305
 -13.250  -1.0472   0.04643   0.03861  -0.0222   1.0000   0.1356
 -13.000  -1.0404   0.04457   0.03664  -0.0220   1.0000   0.1411
 -12.750  -1.0334   0.04289   0.03501  -0.0217   1.0000   0.1460
 -12.500  -1.0255   0.04122   0.03325  -0.0214   1.0000   0.1521
 -12.250  -1.0164   0.03970   0.03170  -0.0210   1.0000   0.1579
 -12.000  -1.0073   0.03822   0.03022  -0.0206   1.0000   0.1639
 -11.750  -0.9965   0.03681   0.02871  -0.0203   1.0000   0.1708
 -11.500  -0.9859   0.03551   0.02748  -0.0198   1.0000   0.1769
 -11.250  -0.9741   0.03424   0.02612  -0.0194   1.0000   0.1844
 -11.000  -0.9619   0.03306   0.02501  -0.0189   1.0000   0.1910
 -10.750  -0.9493   0.03191   0.02380  -0.0184   1.0000   0.1990
 -10.500  -0.9360   0.03083   0.02276  -0.0179   1.0000   0.2065
 -10.250  -0.9224   0.02979   0.02170  -0.0174   1.0000   0.2151
 -10.000  -0.9086   0.02880   0.02077  -0.0168   1.0000   0.2233
  -9.750  -0.8946   0.02785   0.01980  -0.0163   1.0000   0.2327
  -9.500  -0.8812   0.02696   0.01899  -0.0155   1.0000   0.2415
  -9.250  -0.8679   0.02613   0.01814  -0.0148   1.0000   0.2517
  -9.000  -0.8547   0.02534   0.01745  -0.0140   1.0000   0.2615
  -8.750  -0.8371   0.02462   0.01679  -0.0138   0.9855   0.2724
  -8.500  -0.8058   0.02390   0.01605  -0.0160   0.9441   0.2866
  -8.250  -0.7779   0.02326   0.01537  -0.0171   0.9115   0.3009
  -8.000  -0.7548   0.02271   0.01482  -0.0170   0.8841   0.3146
  -7.750  -0.7339   0.02224   0.01432  -0.0163   0.8612   0.3285
  -7.500  -0.7135   0.02181   0.01386  -0.0154   0.8412   0.3427
  -7.250  -0.6928   0.02141   0.01344  -0.0146   0.8238   0.3578
  -7.000  -0.6714   0.02106   0.01305  -0.0138   0.8083   0.3733
  -6.750  -0.6492   0.02073   0.01269  -0.0130   0.7937   0.3891
  -6.500  -0.6263   0.02044   0.01238  -0.0124   0.7795   0.4054
  -6.250  -0.6027   0.02019   0.01210  -0.0118   0.7663   0.4214
  -6.000  -0.5787   0.01997   0.01185  -0.0113   0.7545   0.4377
  -5.750  -0.5539   0.01980   0.01166  -0.0108   0.7425   0.4539
  -5.500  -0.5287   0.01968   0.01154  -0.0103   0.7308   0.4697
  -5.250  -0.5031   0.01967   0.01151  -0.0096   0.7204   0.4847
  -5.000  -0.4766   0.01974   0.01161  -0.0090   0.7087   0.4988
  -4.750  -0.4498   0.01988   0.01174  -0.0084   0.6983   0.5122
  -4.500  -0.4229   0.02004   0.01187  -0.0078   0.6886   0.5253
  -4.250  -0.3957   0.02017   0.01197  -0.0074   0.6786   0.5385
  -4.000  -0.3679   0.02055   0.01232  -0.0066   0.6699   0.5480
  -3.750  -0.3402   0.02078   0.01252  -0.0063   0.6597   0.5584
  -3.500  -0.3135   0.02083   0.01245  -0.0061   0.6519   0.5707
  -3.250  -0.2850   0.02126   0.01287  -0.0055   0.6424   0.5777
  -3.000  -0.2581   0.02131   0.01279  -0.0054   0.6352   0.5886
  -2.750  -0.2301   0.02161   0.01305  -0.0051   0.6265   0.5963
  -2.500  -0.2029   0.02169   0.01303  -0.0050   0.6191   0.6057
  -2.250  -0.1752   0.02193   0.01322  -0.0048   0.6117   0.6132
  -2.000  -0.1478   0.02200   0.01321  -0.0048   0.6043   0.6218
  -1.750  -0.1203   0.02226   0.01338  -0.0043   0.5983   0.6279
  -1.500  -0.0929   0.02224   0.01331  -0.0046   0.5906   0.6372
  -1.250  -0.0655   0.02252   0.01355  -0.0040   0.5844   0.6419
  -1.000  -0.0380   0.02239   0.01331  -0.0046   0.5782   0.6523
  -0.750  -0.0108   0.02268   0.01360  -0.0039   0.5712   0.6558
  -0.500   0.0164   0.02284   0.01369  -0.0035   0.5657   0.6611
  -0.250   0.0440   0.02274   0.01353  -0.0041   0.5592   0.6698
   0.000   0.0708   0.02295   0.01374  -0.0035   0.5527   0.6732
   0.250   0.0980   0.02305   0.01377  -0.0031   0.5476   0.6782
   0.500   0.1259   0.02295   0.01363  -0.0039   0.5408   0.6864
   0.750   0.1524   0.02311   0.01380  -0.0033   0.5347   0.6895
   1.000   0.1794   0.02320   0.01382  -0.0028   0.5296   0.6936
   1.250   0.2067   0.02321   0.01385  -0.0032   0.5225   0.6997
   1.500   0.2342   0.02320   0.01381  -0.0033   0.5164   0.7048
   1.750   0.2608   0.02329   0.01385  -0.0028   0.5112   0.7081
   2.000   0.2872   0.02338   0.01402  -0.0027   0.5041   0.7124
   2.250   0.3156   0.02333   0.01390  -0.0032   0.4980   0.7182
   2.500   0.3427   0.02337   0.01391  -0.0032   0.4922   0.7219
   2.750   0.3683   0.02347   0.01410  -0.0027   0.4850   0.7251
   3.000   0.3954   0.02350   0.01409  -0.0026   0.4791   0.7289
   3.250   0.4229   0.02355   0.01416  -0.0029   0.4723   0.7336
   3.500   0.4508   0.02356   0.01418  -0.0034   0.4652   0.7378
   3.750   0.4772   0.02359   0.01417  -0.0029   0.4598   0.7405
   4.000   0.5024   0.02372   0.01443  -0.0027   0.4517   0.7437
   4.250   0.5295   0.02374   0.01443  -0.0027   0.4450   0.7472
   4.500   0.5572   0.02381   0.01454  -0.0032   0.4377   0.7512
   4.750   0.5847   0.02386   0.01461  -0.0035   0.4300   0.7546
   5.000   0.6102   0.02391   0.01467  -0.0031   0.4233   0.7571
   5.250   0.6352   0.02404   0.01491  -0.0029   0.4147   0.7599
   5.500   0.6621   0.02405   0.01488  -0.0028   0.4079   0.7629
   5.750   0.6877   0.02421   0.01516  -0.0030   0.3983   0.7662
   6.000   0.7161   0.02424   0.01514  -0.0035   0.3912   0.7694
   6.250   0.7407   0.02443   0.01546  -0.0034   0.3814   0.7719
   6.500   0.7658   0.02450   0.01552  -0.0031   0.3740   0.7741
   6.750   0.7897   0.02472   0.01586  -0.0028   0.3643   0.7763
   7.000   0.8149   0.02486   0.01599  -0.0027   0.3562   0.7788
   7.250   0.8393   0.02511   0.01631  -0.0027   0.3465   0.7814
   7.500   0.8644   0.02534   0.01655  -0.0028   0.3380   0.7837
   7.750   0.8893   0.02562   0.01685  -0.0030   0.3288   0.7859
   8.000   0.9127   0.02595   0.01722  -0.0029   0.3201   0.7882
   8.250   0.9342   0.02627   0.01758  -0.0024   0.3117   0.7901
   8.500   0.9554   0.02669   0.01805  -0.0019   0.3033   0.7920
   8.750   0.9767   0.02711   0.01847  -0.0015   0.2951   0.7939
   9.000   0.9971   0.02763   0.01906  -0.0012   0.2868   0.7958
   9.250   1.0172   0.02814   0.01959  -0.0009   0.2790   0.7979
   9.500   1.0365   0.02877   0.02027  -0.0005   0.2713   0.8004
   9.750   1.0551   0.02943   0.02096  -0.0002   0.2638   0.8030
  10.000   1.0723   0.03011   0.02167   0.0003   0.2572   0.8050
  10.250   1.0850   0.03088   0.02255   0.0014   0.2503   0.8068
  10.500   1.0993   0.03158   0.02321   0.0023   0.2445   0.8088
  10.750   1.1112   0.03267   0.02445   0.0029   0.2378   0.8109
  11.000   1.1242   0.03375   0.02557   0.0033   0.2316   0.8132
  11.250   1.1379   0.03485   0.02669   0.0035   0.2261   0.8156
  11.500   1.1476   0.03634   0.02831   0.0035   0.2199   0.8183
  11.750   1.1593   0.03764   0.02964   0.0036   0.2146   0.8210
  12.000   1.1686   0.03908   0.03114   0.0039   0.2096   0.8235
  12.250   1.1745   0.04091   0.03312   0.0039   0.2043   0.8262
  12.500   1.1832   0.04251   0.03477   0.0040   0.1995   0.8289
  12.750   1.1931   0.04407   0.03635   0.0040   0.1951   0.8316
  13.000   1.1951   0.04652   0.03897   0.0035   0.1901   0.8344
  13.500   1.2111   0.05001   0.04251   0.0033   0.1816   0.8399
  13.750   1.2087   0.05296   0.04566   0.0027   0.1774   0.8429
  14.000   1.2073   0.05587   0.04872   0.0021   0.1732   0.8461
  14.250   1.2110   0.05818   0.05110   0.0017   0.1692   0.8497
  14.750   1.2091   0.06402   0.05717   0.0004   0.1619   0.8573
  15.000   1.2023   0.06773   0.06105  -0.0007   0.1581   0.8616
  15.250   1.2036   0.07047   0.06386  -0.0014   0.1546   0.8668
  15.500   1.2178   0.07139   0.06474  -0.0010   0.1515   0.8730
  15.750   1.1944   0.07765   0.07129  -0.0034   0.1481   0.8782
  16.000   1.1751   0.08358   0.07744  -0.0058   0.1446   0.8843
  16.250   1.1681   0.08765   0.08164  -0.0071   0.1413   0.8929
  16.500   1.1777   0.08896   0.08298  -0.0070   0.1385   0.9098
  16.750   1.1625   0.09344   0.08762  -0.0083   0.1357   0.9997
  17.250   1.0215   0.12500   0.11974  -0.0243   0.1258   1.0000
  17.500   1.0708   0.12011   0.11477  -0.0220   0.1246   1.0000
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