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DU 06-W-200 VAWT airfoil (du06-w-200-dt) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: DU 06-W-200 VAWT airfoil (du06-w-200-dt)
Reynolds number: 100,000
Max Cl/Cd: 32.73 at α=10.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-du06-w-200-dt-100000.txt
Download as CSV file: xf-du06-w-200-dt-100000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.9910   0.10177   0.09620  -0.0140   1.0000   0.1114
 -16.500  -1.0713   0.08625   0.08031  -0.0219   1.0000   0.1102
 -16.250  -1.1211   0.07710   0.07082  -0.0256   1.0000   0.1105
 -16.000  -1.1598   0.07034   0.06372  -0.0275   1.0000   0.1114
 -15.750  -1.1344   0.06982   0.06338  -0.0267   1.0000   0.1165
 -15.500  -1.1428   0.06641   0.05987  -0.0272   1.0000   0.1198
 -15.250  -1.1642   0.06192   0.05512  -0.0277   1.0000   0.1225
 -15.000  -1.1884   0.05757   0.05044  -0.0277   1.0000   0.1248
 -14.750  -1.1697   0.05626   0.04927  -0.0273   1.0000   0.1302
 -14.500  -1.1694   0.05408   0.04702  -0.0269   1.0000   0.1348
 -14.250  -1.1848   0.05082   0.04348  -0.0264   1.0000   0.1384
 -14.000  -1.1735   0.04906   0.04176  -0.0259   1.0000   0.1439
 -13.750  -1.1659   0.04755   0.04024  -0.0253   1.0000   0.1495
 -13.500  -1.1781   0.04491   0.03730  -0.0243   1.0000   0.1539
 -13.250  -1.1560   0.04387   0.03642  -0.0239   1.0000   0.1608
 -13.000  -1.1549   0.04210   0.03453  -0.0230   1.0000   0.1668
 -12.750  -1.1501   0.04029   0.03261  -0.0220   1.0000   0.1728
 -12.500  -1.1341   0.03929   0.03170  -0.0214   1.0000   0.1801
 -12.250  -1.1419   0.03750   0.02959  -0.0195   1.0000   0.1857
 -12.000  -1.1136   0.03665   0.02901  -0.0196   1.0000   0.1944
 -11.750  -1.1145   0.03518   0.02727  -0.0179   1.0000   0.2014
 -11.500  -1.0890   0.03433   0.02664  -0.0177   1.0000   0.2103
 -11.250  -1.0831   0.03299   0.02507  -0.0164   1.0000   0.2186
 -11.000  -1.0590   0.03219   0.02447  -0.0161   1.0000   0.2280
 -10.750  -1.0444   0.03106   0.02328  -0.0153   1.0000   0.2374
 -10.500  -1.0271   0.03017   0.02241  -0.0146   1.0000   0.2476
 -10.250  -1.0065   0.02928   0.02161  -0.0140   1.0000   0.2577
 -10.000  -0.9917   0.02829   0.02054  -0.0132   1.0000   0.2688
  -9.750  -0.9709   0.02755   0.01991  -0.0126   1.0000   0.2802
  -9.500  -0.9507   0.02678   0.01925  -0.0120   1.0000   0.2918
  -9.250  -0.9338   0.02598   0.01847  -0.0111   1.0000   0.3041
  -9.000  -0.9201   0.02528   0.01776  -0.0098   1.0000   0.3171
  -8.750  -0.9058   0.02482   0.01752  -0.0082   1.0000   0.3288
  -8.500  -0.9048   0.02443   0.01720  -0.0049   1.0000   0.3390
  -8.250  -0.9073   0.02409   0.01686  -0.0016   1.0000   0.3500
  -8.000  -0.8596   0.02352   0.01639  -0.0062   0.9885   0.3705
  -7.750  -0.8079   0.02307   0.01607  -0.0112   0.9770   0.3923
  -7.500  -0.7570   0.02258   0.01561  -0.0161   0.9652   0.4161
  -7.250  -0.7116   0.02221   0.01531  -0.0196   0.9509   0.4380
  -7.000  -0.6693   0.02211   0.01533  -0.0219   0.9355   0.4583
  -6.750  -0.6321   0.02212   0.01541  -0.0230   0.9188   0.4773
  -6.500  -0.5999   0.02231   0.01565  -0.0228   0.9015   0.4947
  -6.250  -0.5707   0.02267   0.01605  -0.0218   0.8844   0.5101
  -6.000  -0.5434   0.02316   0.01652  -0.0205   0.8677   0.5245
  -5.750  -0.5180   0.02363   0.01695  -0.0190   0.8514   0.5385
  -5.500  -0.4854   0.02509   0.01843  -0.0169   0.8363   0.5449
  -5.250  -0.4603   0.02573   0.01899  -0.0152   0.8218   0.5565
  -5.000  -0.4290   0.02718   0.02039  -0.0130   0.8094   0.5618
  -4.750  -0.4041   0.02775   0.02088  -0.0118   0.7955   0.5728
  -4.500  -0.3723   0.02919   0.02228  -0.0099   0.7825   0.5773
  -4.250  -0.3490   0.02957   0.02254  -0.0087   0.7715   0.5888
  -4.000  -0.3174   0.03087   0.02379  -0.0069   0.7602   0.5929
  -3.750  -0.2946   0.03104   0.02388  -0.0063   0.7496   0.6049
  -3.500  -0.2638   0.03211   0.02487  -0.0044   0.7406   0.6092
  -3.250  -0.2412   0.03218   0.02489  -0.0040   0.7300   0.6212
  -3.000  -0.2111   0.03304   0.02566  -0.0022   0.7224   0.6262
  -2.750  -0.1888   0.03302   0.02562  -0.0021   0.7125   0.6379
  -2.500  -0.1593   0.03364   0.02616  -0.0005   0.7053   0.6434
  -2.250  -0.1375   0.03359   0.02609  -0.0003   0.6962   0.6549
  -2.000  -0.1085   0.03404   0.02647   0.0011   0.6891   0.6612
  -1.750  -0.0869   0.03396   0.02637   0.0015   0.6812   0.6721
  -1.500  -0.0684   0.03367   0.02601   0.0017   0.6738   0.6859
  -1.250  -0.0375   0.03407   0.02638   0.0033   0.6675   0.6895
  -1.000  -0.0186   0.03392   0.02622   0.0034   0.6592   0.7025
  -0.750   0.0114   0.03406   0.02631   0.0048   0.6531   0.7071
  -0.500   0.0286   0.03391   0.02616   0.0050   0.6455   0.7202
  -0.250   0.0590   0.03402   0.02626   0.0062   0.6384   0.7247
   0.000   0.0766   0.03369   0.02584   0.0069   0.6332   0.7372
   0.250   0.1055   0.03388   0.02611   0.0076   0.6244   0.7422
   0.500   0.1228   0.03349   0.02564   0.0084   0.6187   0.7542
   0.750   0.1512   0.03358   0.02578   0.0091   0.6110   0.7594
   1.000   0.1672   0.03332   0.02549   0.0099   0.6042   0.7710
   1.250   0.1986   0.03301   0.02508   0.0108   0.5991   0.7761
   1.500   0.2107   0.03311   0.02528   0.0114   0.5901   0.7874
   1.750   0.2414   0.03272   0.02485   0.0122   0.5840   0.7924
   2.000   0.2602   0.03275   0.02491   0.0130   0.5763   0.8009
   2.250   0.2830   0.03246   0.02462   0.0138   0.5690   0.8079
   2.500   0.3098   0.03210   0.02416   0.0144   0.5636   0.8148
   2.750   0.3236   0.03220   0.02437   0.0154   0.5543   0.8227
   3.000   0.3533   0.03175   0.02384   0.0159   0.5484   0.8284
   3.250   0.3655   0.03195   0.02413   0.0170   0.5397   0.8363
   3.500   0.3932   0.03154   0.02369   0.0175   0.5328   0.8414
   3.750   0.4150   0.03153   0.02369   0.0181   0.5251   0.8473
   4.000   0.4316   0.03144   0.02361   0.0191   0.5171   0.8539
   4.250   0.4635   0.03092   0.02299   0.0192   0.5114   0.8582
   4.500   0.4790   0.03119   0.02341   0.0203   0.5010   0.8637
   4.750   0.5054   0.03075   0.02284   0.0205   0.4954   0.8690
   5.000   0.5211   0.03103   0.02328   0.0216   0.4851   0.8733
   5.250   0.5517   0.03053   0.02268   0.0216   0.4787   0.8776
   5.500   0.5665   0.03087   0.02314   0.0226   0.4686   0.8822
   5.750   0.5941   0.03047   0.02266   0.0226   0.4619   0.8864
   6.000   0.6122   0.03069   0.02300   0.0235   0.4521   0.8900
   6.250   0.6419   0.03027   0.02251   0.0235   0.4449   0.8937
   6.500   0.6591   0.03059   0.02295   0.0242   0.4354   0.8977
   6.750   0.6877   0.03026   0.02254   0.0240   0.4280   0.9011
   7.000   0.7061   0.03052   0.02292   0.0247   0.4186   0.9045
   7.250   0.7363   0.03010   0.02244   0.0246   0.4109   0.9076
   7.500   0.7545   0.03046   0.02292   0.0251   0.4015   0.9110
   7.750   0.7853   0.03006   0.02245   0.0248   0.3938   0.9142
   8.000   0.8032   0.03053   0.02304   0.0251   0.3843   0.9172
   8.250   0.8352   0.03012   0.02255   0.0246   0.3768   0.9197
   8.500   0.8517   0.03063   0.02321   0.0253   0.3673   0.9231
   8.750   0.8853   0.03019   0.02265   0.0246   0.3598   0.9258
   9.000   0.9009   0.03088   0.02352   0.0251   0.3502   0.9287
   9.250   0.9365   0.03047   0.02294   0.0242   0.3428   0.9316
   9.500   0.9491   0.03136   0.02405   0.0248   0.3333   0.9351
   9.750   0.9867   0.03097   0.02346   0.0238   0.3260   0.9378
  10.000   0.9962   0.03211   0.02488   0.0245   0.3169   0.9413
  10.250   1.0352   0.03186   0.02440   0.0232   0.3095   0.9441
  10.500   1.0415   0.03321   0.02606   0.0241   0.3008   0.9485
  10.750   1.0807   0.03302   0.02566   0.0228   0.2933   0.9521
  11.000   1.0852   0.03458   0.02754   0.0236   0.2854   0.9580
  11.250   1.1220   0.03463   0.02745   0.0223   0.2778   0.9623
  11.500   1.1297   0.03630   0.02940   0.0224   0.2706   0.9689
  11.750   1.1589   0.03688   0.02996   0.0212   0.2632   0.9759
  12.000   1.1769   0.03826   0.03145   0.0204   0.2565   0.9914
  12.250   1.1797   0.03992   0.03330   0.0209   0.2503   1.0000
  12.500   1.2278   0.04005   0.03321   0.0185   0.2432   1.0000
  12.750   1.2061   0.04312   0.03667   0.0198   0.2385   1.0000
  13.000   1.2151   0.04493   0.03858   0.0191   0.2327   1.0000
  13.250   1.2544   0.04531   0.03882   0.0178   0.2265   1.0000
  13.500   1.2171   0.05036   0.04427   0.0174   0.2228   1.0000
  13.750   1.1863   0.05591   0.05009   0.0156   0.2187   1.0000
  14.000   1.2752   0.05180   0.04561   0.0157   0.2113   1.0000
  14.250   1.1910   0.06203   0.05634   0.0130   0.2097   1.0000
  14.500   0.6875   0.15183   0.14662  -0.0268   0.2117   1.0000
  15.000   1.1867   0.07272   0.06724   0.0085   0.1965   1.0000
  15.250   0.6512   0.17386   0.16879  -0.0423   0.2305   1.0000
  15.500   0.7043   0.17958   0.17457  -0.0415   0.2280   1.0000
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