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


Details Polar file
Airfoil: DU 06-W-200 VAWT airfoil (du06-w-200-dt)
Reynolds number: 200,000
Max Cl/Cd: 51.11 at α=9°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-du06-w-200-dt-200000-n5.txt
Download as CSV file: xf-du06-w-200-dt-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -1.1111   0.11047   0.10503   0.0034   1.0000   0.0441
 -18.500  -1.1197   0.10538   0.09987   0.0011   1.0000   0.0455
 -18.250  -1.1268   0.10061   0.09499  -0.0010   1.0000   0.0471
 -18.000  -1.1317   0.09622   0.09048  -0.0028   1.0000   0.0488
 -17.750  -1.1378   0.09174   0.08591  -0.0046   1.0000   0.0504
 -17.500  -1.1453   0.08712   0.08124  -0.0064   1.0000   0.0519
 -17.250  -1.1505   0.08288   0.07693  -0.0080   1.0000   0.0538
 -17.000  -1.1529   0.07909   0.07303  -0.0093   1.0000   0.0560
 -16.750  -1.1547   0.07546   0.06930  -0.0105   1.0000   0.0581
 -16.500  -1.1593   0.07150   0.06531  -0.0118   1.0000   0.0601
 -16.250  -1.1608   0.06801   0.06175  -0.0129   1.0000   0.0625
 -16.000  -1.1592   0.06498   0.05862  -0.0137   1.0000   0.0652
 -15.750  -1.1588   0.06186   0.05544  -0.0145   1.0000   0.0677
 -15.500  -1.1589   0.05874   0.05228  -0.0152   1.0000   0.0704
 -15.250  -1.1557   0.05606   0.04953  -0.0158   1.0000   0.0735
 -15.000  -1.1497   0.05377   0.04714  -0.0161   1.0000   0.0766
 -14.750  -1.1484   0.05103   0.04439  -0.0165   1.0000   0.0794
 -14.500  -1.1438   0.04870   0.04201  -0.0167   1.0000   0.0829
 -14.250  -1.1358   0.04678   0.04000  -0.0168   1.0000   0.0866
 -14.000  -1.1310   0.04460   0.03780  -0.0168   1.0000   0.0899
 -13.750  -1.1251   0.04261   0.03579  -0.0168   1.0000   0.0938
 -13.500  -1.1159   0.04098   0.03408  -0.0166   1.0000   0.0980
 -13.250  -1.1088   0.03922   0.03230  -0.0164   1.0000   0.1019
 -13.000  -1.1010   0.03755   0.03062  -0.0161   1.0000   0.1064
 -12.750  -1.0897   0.03617   0.02918  -0.0158   1.0000   0.1113
 -12.500  -1.0809   0.03463   0.02764  -0.0155   1.0000   0.1159
 -12.250  -1.0705   0.03322   0.02622  -0.0151   1.0000   0.1213
 -12.000  -1.0570   0.03206   0.02501  -0.0148   1.0000   0.1267
 -11.750  -1.0471   0.03066   0.02363  -0.0144   1.0000   0.1320
 -11.500  -1.0332   0.02955   0.02249  -0.0141   1.0000   0.1380
 -11.250  -1.0204   0.02838   0.02133  -0.0137   1.0000   0.1437
 -11.000  -1.0069   0.02726   0.02023  -0.0133   1.0000   0.1502
 -10.750  -0.9915   0.02629   0.01924  -0.0130   1.0000   0.1567
 -10.500  -0.9780   0.02520   0.01818  -0.0126   1.0000   0.1636
 -10.250  -0.9610   0.02436   0.01732  -0.0124   1.0000   0.1708
 -10.000  -0.9471   0.02333   0.01635  -0.0120   1.0000   0.1780
  -9.750  -0.9292   0.02259   0.01559  -0.0118   0.9843   0.1858
  -9.500  -0.9066   0.02167   0.01466  -0.0128   0.9123   0.1946
  -9.250  -0.8896   0.02103   0.01390  -0.0119   0.8703   0.2030
  -9.000  -0.8759   0.02031   0.01312  -0.0108   0.8414   0.2114
  -8.750  -0.8573   0.01969   0.01242  -0.0103   0.8200   0.2206
  -8.500  -0.8381   0.01908   0.01176  -0.0099   0.8025   0.2308
  -8.250  -0.8179   0.01853   0.01115  -0.0095   0.7873   0.2412
  -8.000  -0.7962   0.01806   0.01062  -0.0091   0.7734   0.2527
  -7.750  -0.7740   0.01757   0.01010  -0.0089   0.7600   0.2649
  -7.500  -0.7512   0.01710   0.00961  -0.0087   0.7478   0.2772
  -7.250  -0.7276   0.01668   0.00916  -0.0086   0.7368   0.2903
  -7.000  -0.7032   0.01628   0.00875  -0.0085   0.7258   0.3043
  -6.750  -0.6783   0.01590   0.00836  -0.0085   0.7153   0.3190
  -6.250  -0.6274   0.01520   0.00765  -0.0086   0.6938   0.3508
  -6.000  -0.6014   0.01488   0.00733  -0.0086   0.6836   0.3676
  -5.750  -0.5749   0.01459   0.00704  -0.0087   0.6730   0.3843
  -5.500  -0.5480   0.01432   0.00678  -0.0088   0.6632   0.4011
  -5.250  -0.5209   0.01408   0.00653  -0.0089   0.6535   0.4178
  -5.000  -0.4933   0.01386   0.00633  -0.0091   0.6435   0.4340
  -4.500  -0.4379   0.01349   0.00597  -0.0093   0.6237   0.4662
  -4.250  -0.4101   0.01335   0.00583  -0.0093   0.6149   0.4825
  -4.000  -0.3818   0.01323   0.00576  -0.0094   0.6057   0.4982
  -3.750  -0.3537   0.01318   0.00571  -0.0094   0.5978   0.5140
  -3.500  -0.3251   0.01317   0.00575  -0.0094   0.5890   0.5293
  -3.250  -0.2967   0.01325   0.00582  -0.0094   0.5816   0.5442
  -3.000  -0.2677   0.01333   0.00593  -0.0094   0.5737   0.5576
  -2.750  -0.2386   0.01344   0.00599  -0.0095   0.5668   0.5705
  -2.500  -0.2094   0.01361   0.00615  -0.0095   0.5601   0.5811
  -2.250  -0.1801   0.01373   0.00624  -0.0097   0.5532   0.5912
  -2.000  -0.1505   0.01380   0.00618  -0.0100   0.5474   0.6021
  -1.500  -0.0912   0.01403   0.00631  -0.0106   0.5349   0.6188
  -1.250  -0.0623   0.01426   0.00650  -0.0105   0.5298   0.6235
  -1.000  -0.0327   0.01438   0.00660  -0.0108   0.5237   0.6301
  -0.750  -0.0030   0.01447   0.00662  -0.0111   0.5180   0.6369
  -0.500   0.0258   0.01468   0.00679  -0.0111   0.5130   0.6411
  -0.250   0.0553   0.01481   0.00689  -0.0113   0.5077   0.6466
   0.000   0.0852   0.01485   0.00687  -0.0118   0.5020   0.6528
   0.250   0.1138   0.01503   0.00703  -0.0117   0.4967   0.6558
   0.500   0.1428   0.01518   0.00717  -0.0118   0.4917   0.6595
   0.750   0.1722   0.01526   0.00724  -0.0121   0.4860   0.6642
   1.000   0.2021   0.01529   0.00719  -0.0127   0.4808   0.6694
   1.250   0.2305   0.01544   0.00732  -0.0126   0.4759   0.6717
   1.500   0.2593   0.01555   0.00748  -0.0127   0.4701   0.6745
   1.750   0.2882   0.01564   0.00756  -0.0128   0.4644   0.6778
   2.000   0.3174   0.01573   0.00758  -0.0131   0.4594   0.6818
   2.250   0.3476   0.01573   0.00758  -0.0138   0.4534   0.6861
   2.500   0.3758   0.01582   0.00771  -0.0138   0.4477   0.6880
   2.750   0.4040   0.01594   0.00779  -0.0138   0.4426   0.6902
   3.000   0.4327   0.01602   0.00794  -0.0139   0.4361   0.6928
   3.250   0.4614   0.01609   0.00802  -0.0141   0.4298   0.6957
   3.500   0.4904   0.01617   0.00805  -0.0144   0.4240   0.6988
   3.750   0.5202   0.01621   0.00811  -0.0150   0.4168   0.7022
   4.000   0.5484   0.01628   0.00818  -0.0151   0.4103   0.7042
   4.250   0.5763   0.01637   0.00832  -0.0152   0.4029   0.7061
   4.500   0.6042   0.01646   0.00844  -0.0152   0.3950   0.7081
   4.750   0.6321   0.01657   0.00856  -0.0153   0.3875   0.7104
   5.000   0.6602   0.01667   0.00868  -0.0155   0.3791   0.7128
   5.250   0.6884   0.01678   0.00879  -0.0157   0.3712   0.7154
   5.500   0.7168   0.01690   0.00890  -0.0161   0.3619   0.7182
   5.750   0.7448   0.01704   0.00903  -0.0163   0.3528   0.7205
   6.000   0.7712   0.01720   0.00920  -0.0162   0.3435   0.7221
   6.250   0.7979   0.01738   0.00942  -0.0162   0.3339   0.7236
   6.500   0.8239   0.01760   0.00961  -0.0161   0.3246   0.7253
   6.750   0.8504   0.01782   0.00986  -0.0161   0.3151   0.7270
   7.000   0.8763   0.01808   0.01012  -0.0161   0.3063   0.7288
   7.250   0.9021   0.01835   0.01039  -0.0161   0.2966   0.7304
   7.500   0.9277   0.01865   0.01068  -0.0161   0.2877   0.7321
   7.750   0.9527   0.01899   0.01100  -0.0160   0.2787   0.7340
   8.000   0.9779   0.01933   0.01135  -0.0161   0.2702   0.7358
   8.250   1.0018   0.01973   0.01172  -0.0159   0.2618   0.7371
   8.500   1.0255   0.02008   0.01212  -0.0157   0.2543   0.7381
   8.750   1.0479   0.02051   0.01257  -0.0153   0.2469   0.7393
   9.000   1.0702   0.02094   0.01303  -0.0149   0.2398   0.7405
   9.250   1.0915   0.02141   0.01354  -0.0144   0.2323   0.7419
   9.500   1.1117   0.02194   0.01409  -0.0138   0.2259   0.7436
   9.750   1.1322   0.02244   0.01465  -0.0133   0.2190   0.7453
  10.000   1.1495   0.02310   0.01529  -0.0125   0.2129   0.7468
  10.250   1.1681   0.02365   0.01592  -0.0118   0.2071   0.7484
  10.500   1.1823   0.02431   0.01663  -0.0107   0.2016   0.7499
  10.750   1.1949   0.02522   0.01752  -0.0097   0.1965   0.7515
  11.000   1.2119   0.02601   0.01841  -0.0093   0.1911   0.7530
  11.250   1.2253   0.02703   0.01948  -0.0088   0.1858   0.7544
  11.750   1.2492   0.02938   0.02197  -0.0079   0.1768   0.7572
  12.000   1.2602   0.03071   0.02338  -0.0077   0.1720   0.7589
  12.250   1.2682   0.03234   0.02503  -0.0075   0.1677   0.7608
  12.500   1.2779   0.03388   0.02666  -0.0074   0.1637   0.7629
  12.750   1.2877   0.03548   0.02835  -0.0074   0.1594   0.7648
  13.000   1.2945   0.03735   0.03028  -0.0075   0.1554   0.7666
  13.250   1.2987   0.03950   0.03244  -0.0076   0.1518   0.7684
  13.500   1.3067   0.04135   0.03439  -0.0077   0.1482   0.7702
  13.750   1.3125   0.04339   0.03654  -0.0079   0.1445   0.7718
  14.000   1.3157   0.04568   0.03891  -0.0081   0.1411   0.7734
  14.250   1.3167   0.04821   0.04147  -0.0083   0.1380   0.7752
  14.500   1.3205   0.05052   0.04388  -0.0086   0.1349   0.7771
  14.750   1.3239   0.05293   0.04642  -0.0089   0.1316   0.7791
  15.000   1.3252   0.05560   0.04917  -0.0094   0.1284   0.7812
  15.250   1.3250   0.05849   0.05211  -0.0100   0.1255   0.7833
  15.500   1.3250   0.06139   0.05503  -0.0106   0.1228   0.7855
  15.750   1.3273   0.06420   0.05798  -0.0114   0.1200   0.7877
  16.000   1.3277   0.06722   0.06113  -0.0122   0.1170   0.7898
  16.250   1.3266   0.07044   0.06443  -0.0130   0.1142   0.7923
  16.500   1.3246   0.07377   0.06780  -0.0140   0.1117   0.7950
  16.750   1.3233   0.07706   0.07115  -0.0149   0.1092   0.7979
  17.000   1.3222   0.08050   0.07474  -0.0160   0.1066   0.8010
  17.500   1.3161   0.08790   0.08235  -0.0185   0.1014   0.8069
  17.750   1.3121   0.09171   0.08619  -0.0198   0.0990   0.8101
  18.000   1.3085   0.09555   0.09011  -0.0212   0.0966   0.8136
  18.250   1.3025   0.09993   0.09465  -0.0229   0.0940   0.8174
  18.750   1.2892   0.10884   0.10375  -0.0267   0.0886   0.8258
  19.000   1.2843   0.11297   0.10789  -0.0284   0.0862   0.8312
  19.250   1.2756   0.11798   0.11307  -0.0307   0.0838   0.8370
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