DU 06-W-200 VAWT airfoil (du06-w-200-dt) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: DU 06-W-200 VAWT airfoil (du06-w-200-dt) Reynolds number: 500,000 Max Cl/Cd: 71.48 at α=9.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-du06-w-200-dt-500000.txt Download as CSV file: xf-du06-w-200-dt-500000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.500 -1.2255 0.10610 0.10160 0.0051 1.0000 0.0326
-19.250 -1.2361 0.10094 0.09637 0.0029 1.0000 0.0335
-19.000 -1.2443 0.09621 0.09156 0.0011 1.0000 0.0345
-18.750 -1.2497 0.09193 0.08719 -0.0005 1.0000 0.0356
-18.500 -1.2529 0.08804 0.08320 -0.0019 1.0000 0.0366
-18.250 -1.2643 0.08303 0.07814 -0.0036 1.0000 0.0378
-18.000 -1.2725 0.07854 0.07359 -0.0051 1.0000 0.0390
-17.750 -1.2774 0.07458 0.06956 -0.0063 1.0000 0.0403
-17.500 -1.2787 0.07112 0.06602 -0.0073 1.0000 0.0418
-17.250 -1.2804 0.06766 0.06248 -0.0082 1.0000 0.0432
-17.000 -1.2862 0.06375 0.05853 -0.0092 1.0000 0.0449
-16.750 -1.2876 0.06045 0.05518 -0.0099 1.0000 0.0467
-16.500 -1.2850 0.05766 0.05232 -0.0105 1.0000 0.0487
-16.250 -1.2840 0.05474 0.04933 -0.0110 1.0000 0.0507
-16.000 -1.2844 0.05174 0.04632 -0.0114 1.0000 0.0530
-15.750 -1.2804 0.04929 0.04382 -0.0117 1.0000 0.0556
-15.500 -1.2739 0.04714 0.04160 -0.0118 1.0000 0.0580
-15.250 -1.2729 0.04449 0.03894 -0.0119 1.0000 0.0609
-15.000 -1.2667 0.04244 0.03687 -0.0119 1.0000 0.0640
-14.750 -1.2577 0.04068 0.03505 -0.0118 1.0000 0.0670
-14.500 -1.2542 0.03848 0.03286 -0.0117 1.0000 0.0706
-14.250 -1.2451 0.03686 0.03122 -0.0114 1.0000 0.0744
-14.000 -1.2366 0.03525 0.02957 -0.0111 1.0000 0.0781
-13.750 -1.2296 0.03355 0.02789 -0.0107 1.0000 0.0824
-13.500 -1.2174 0.03229 0.02659 -0.0103 1.0000 0.0866
-13.250 -1.2091 0.03072 0.02504 -0.0098 1.0000 0.0912
-13.000 -1.1983 0.02937 0.02370 -0.0094 1.0000 0.0959
-12.750 -1.1838 0.02832 0.02260 -0.0091 1.0000 0.1002
-12.500 -1.1744 0.02687 0.02119 -0.0086 1.0000 0.1054
-12.250 -1.1598 0.02584 0.02014 -0.0082 1.0000 0.1104
-12.000 -1.1460 0.02473 0.01903 -0.0078 1.0000 0.1153
-11.750 -1.1325 0.02360 0.01793 -0.0074 1.0000 0.1208
-11.500 -1.1143 0.02282 0.01711 -0.0072 1.0000 0.1258
-11.250 -1.1014 0.02164 0.01598 -0.0067 1.0000 0.1321
-11.000 -1.0840 0.02078 0.01513 -0.0065 1.0000 0.1382
-10.750 -1.0676 0.01986 0.01423 -0.0062 1.0000 0.1443
-10.500 -1.0506 0.01898 0.01338 -0.0060 1.0000 0.1514
-10.250 -1.0328 0.01818 0.01260 -0.0058 1.0000 0.1584
-10.000 -1.0164 0.01733 0.01180 -0.0055 1.0000 0.1663
-9.750 -0.9867 0.01661 0.01105 -0.0074 0.9308 0.1752
-9.500 -0.9696 0.01603 0.01036 -0.0065 0.8813 0.1834
-9.250 -0.9497 0.01545 0.00969 -0.0061 0.8497 0.1923
-9.000 -0.9269 0.01507 0.00920 -0.0058 0.8279 0.2017
-8.750 -0.9045 0.01453 0.00865 -0.0058 0.8103 0.2124
-8.500 -0.8802 0.01412 0.00820 -0.0058 0.7953 0.2228
-8.250 -0.8549 0.01376 0.00779 -0.0059 0.7820 0.2340
-8.000 -0.8301 0.01332 0.00736 -0.0059 0.7698 0.2464
-7.750 -0.8046 0.01295 0.00697 -0.0060 0.7580 0.2591
-7.500 -0.7782 0.01258 0.00662 -0.0062 0.7465 0.2725
-7.250 -0.7516 0.01226 0.00628 -0.0064 0.7361 0.2867
-7.000 -0.7247 0.01192 0.00596 -0.0066 0.7254 0.3021
-6.750 -0.6975 0.01159 0.00565 -0.0069 0.7152 0.3187
-6.500 -0.6703 0.01129 0.00536 -0.0072 0.7050 0.3356
-6.250 -0.6424 0.01099 0.00509 -0.0075 0.6941 0.3526
-6.000 -0.6145 0.01072 0.00483 -0.0078 0.6836 0.3705
-5.750 -0.5862 0.01046 0.00459 -0.0081 0.6720 0.3882
-5.500 -0.5577 0.01023 0.00438 -0.0084 0.6607 0.4053
-5.250 -0.5291 0.01003 0.00418 -0.0087 0.6500 0.4228
-5.000 -0.5002 0.00984 0.00399 -0.0091 0.6385 0.4399
-4.750 -0.4711 0.00966 0.00382 -0.0094 0.6274 0.4566
-4.250 -0.4128 0.00937 0.00352 -0.0101 0.6058 0.4892
-4.000 -0.3836 0.00924 0.00340 -0.0104 0.5964 0.5057
-3.750 -0.3543 0.00912 0.00330 -0.0108 0.5869 0.5220
-3.500 -0.3250 0.00904 0.00325 -0.0111 0.5785 0.5393
-3.250 -0.2954 0.00901 0.00325 -0.0114 0.5703 0.5567
-3.000 -0.2657 0.00906 0.00329 -0.0116 0.5630 0.5729
-2.750 -0.2355 0.00911 0.00334 -0.0120 0.5558 0.5871
-2.500 -0.2055 0.00924 0.00343 -0.0123 0.5492 0.5984
-2.250 -0.1753 0.00936 0.00354 -0.0126 0.5430 0.6080
-2.000 -0.1448 0.00947 0.00359 -0.0130 0.5367 0.6174
-1.750 -0.1150 0.00964 0.00371 -0.0132 0.5310 0.6232
-1.500 -0.0847 0.00979 0.00384 -0.0135 0.5259 0.6297
-1.250 -0.0542 0.00991 0.00391 -0.0139 0.5204 0.6364
-1.000 -0.0245 0.01008 0.00407 -0.0141 0.5149 0.6405
-0.750 0.0054 0.01026 0.00422 -0.0143 0.5099 0.6452
-0.500 0.0360 0.01038 0.00429 -0.0148 0.5050 0.6510
-0.250 0.0657 0.01049 0.00441 -0.0149 0.5001 0.6546
0.000 0.0952 0.01070 0.00457 -0.0151 0.4951 0.6580
0.250 0.1253 0.01082 0.00472 -0.0153 0.4906 0.6620
0.500 0.1555 0.01093 0.00480 -0.0157 0.4854 0.6668
0.750 0.1853 0.01102 0.00485 -0.0160 0.4805 0.6703
1.000 0.2146 0.01118 0.00501 -0.0161 0.4759 0.6729
1.250 0.2444 0.01127 0.00514 -0.0163 0.4714 0.6759
1.500 0.2741 0.01136 0.00523 -0.0166 0.4664 0.6791
1.750 0.3039 0.01149 0.00530 -0.0169 0.4614 0.6826
2.000 0.3343 0.01159 0.00538 -0.0174 0.4566 0.6859
2.250 0.3635 0.01156 0.00540 -0.0175 0.4513 0.6882
2.500 0.3928 0.01164 0.00547 -0.0177 0.4462 0.6903
2.750 0.4220 0.01176 0.00558 -0.0179 0.4410 0.6926
3.000 0.4517 0.01179 0.00566 -0.0182 0.4351 0.6951
3.250 0.4812 0.01186 0.00571 -0.0185 0.4291 0.6979
3.500 0.5109 0.01195 0.00577 -0.0188 0.4232 0.7005
3.750 0.5412 0.01200 0.00582 -0.0193 0.4168 0.7027
4.000 0.5700 0.01200 0.00581 -0.0195 0.4104 0.7047
4.250 0.5990 0.01203 0.00588 -0.0197 0.4036 0.7064
4.500 0.6280 0.01209 0.00596 -0.0199 0.3960 0.7083
4.750 0.6568 0.01219 0.00605 -0.0201 0.3887 0.7102
5.000 0.6859 0.01226 0.00613 -0.0204 0.3799 0.7123
5.250 0.7148 0.01236 0.00622 -0.0206 0.3715 0.7144
5.500 0.7438 0.01247 0.00631 -0.0209 0.3624 0.7164
5.750 0.7727 0.01260 0.00642 -0.0213 0.3531 0.7183
6.000 0.8012 0.01279 0.00655 -0.0215 0.3426 0.7199
6.250 0.8292 0.01285 0.00662 -0.0217 0.3322 0.7216
6.500 0.8564 0.01303 0.00679 -0.0217 0.3221 0.7233
6.750 0.8835 0.01325 0.00699 -0.0217 0.3113 0.7250
7.000 0.9109 0.01345 0.00720 -0.0218 0.3017 0.7268
7.250 0.9374 0.01373 0.00743 -0.0218 0.2922 0.7283
7.500 0.9649 0.01394 0.00765 -0.0220 0.2829 0.7299
7.750 0.9913 0.01423 0.00791 -0.0220 0.2737 0.7314
8.000 1.0180 0.01449 0.00815 -0.0221 0.2646 0.7327
8.250 1.0443 0.01478 0.00842 -0.0221 0.2562 0.7339
8.500 1.0701 0.01510 0.00872 -0.0221 0.2476 0.7352
8.750 1.0959 0.01542 0.00904 -0.0221 0.2402 0.7364
9.000 1.1212 0.01573 0.00934 -0.0221 0.2326 0.7374
9.250 1.1456 0.01606 0.00967 -0.0219 0.2254 0.7385
9.500 1.1701 0.01637 0.01000 -0.0217 0.2182 0.7395
9.750 1.1926 0.01682 0.01043 -0.0213 0.2114 0.7406
10.000 1.2170 0.01713 0.01079 -0.0211 0.2053 0.7417
10.250 1.2382 0.01763 0.01128 -0.0205 0.1987 0.7428
10.500 1.2605 0.01804 0.01173 -0.0201 0.1930 0.7442
10.750 1.2817 0.01850 0.01221 -0.0196 0.1872 0.7457
11.000 1.2983 0.01919 0.01287 -0.0186 0.1811 0.7471
11.250 1.3186 0.01957 0.01333 -0.0179 0.1766 0.7484
11.500 1.3331 0.02018 0.01396 -0.0166 0.1717 0.7497
11.750 1.3452 0.02116 0.01491 -0.0155 0.1665 0.7510
12.000 1.3635 0.02182 0.01564 -0.0151 0.1625 0.7522
12.250 1.3783 0.02275 0.01661 -0.0146 0.1579 0.7534
12.500 1.3885 0.02405 0.01793 -0.0141 0.1535 0.7547
12.750 1.4008 0.02527 0.01921 -0.0138 0.1495 0.7561
13.000 1.4145 0.02645 0.02047 -0.0137 0.1453 0.7575
13.250 1.4233 0.02809 0.02213 -0.0136 0.1411 0.7589
13.500 1.4273 0.03020 0.02426 -0.0135 0.1369 0.7604
13.750 1.4407 0.03151 0.02567 -0.0135 0.1334 0.7621
14.000 1.4485 0.03336 0.02758 -0.0136 0.1295 0.7640
14.250 1.4507 0.03575 0.02998 -0.0137 0.1257 0.7658
14.500 1.4535 0.03811 0.03239 -0.0138 0.1223 0.7675
14.750 1.4613 0.04002 0.03438 -0.0140 0.1191 0.7691
15.000 1.4637 0.04250 0.03690 -0.0142 0.1156 0.7705
15.250 1.4609 0.04549 0.03993 -0.0145 0.1122 0.7721
15.500 1.4598 0.04831 0.04282 -0.0148 0.1092 0.7739
15.750 1.4638 0.05067 0.04528 -0.0151 0.1063 0.7757
16.000 1.4634 0.05358 0.04826 -0.0156 0.1033 0.7775
16.250 1.4594 0.05694 0.05166 -0.0163 0.1006 0.7794
16.500 1.4521 0.06073 0.05548 -0.0170 0.0978 0.7813
16.750 1.4555 0.06336 0.05821 -0.0176 0.0959 0.7835
17.000 1.4560 0.06635 0.06128 -0.0183 0.0935 0.7856
17.250 1.4527 0.06985 0.06484 -0.0191 0.0910 0.7876
17.500 1.4463 0.07374 0.06879 -0.0202 0.0887 0.7898
17.750 1.4373 0.07794 0.07302 -0.0213 0.0860 0.7921
18.000 1.4384 0.08101 0.07621 -0.0221 0.0841 0.7948
18.250 1.4364 0.08450 0.07980 -0.0232 0.0818 0.7977
18.500 1.4312 0.08844 0.08380 -0.0244 0.0794 0.8006
18.750 1.4217 0.09298 0.08839 -0.0259 0.0772 0.8035
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