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