DU 06-W-200 VAWT airfoil (du06-w-200-dt) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: DU 06-W-200 VAWT airfoil (du06-w-200-dt) Reynolds number: 1,000,000 Max Cl/Cd: 87.36 at α=9.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-du06-w-200-dt-1000000-n5.txt Download as CSV file: xf-du06-w-200-dt-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.3262 0.09569 0.09119 0.0027 1.0000 0.0127
-19.500 -1.3348 0.09107 0.08648 0.0010 1.0000 0.0130
-19.250 -1.3421 0.08665 0.08198 -0.0006 1.0000 0.0134
-19.000 -1.3503 0.08217 0.07742 -0.0021 1.0000 0.0138
-18.750 -1.3570 0.07797 0.07315 -0.0034 1.0000 0.0143
-18.500 -1.3619 0.07407 0.06918 -0.0045 1.0000 0.0148
-18.250 -1.3652 0.07041 0.06544 -0.0055 1.0000 0.0153
-18.000 -1.3669 0.06699 0.06194 -0.0064 1.0000 0.0158
-17.750 -1.3680 0.06370 0.05859 -0.0072 1.0000 0.0163
-17.500 -1.3695 0.06042 0.05525 -0.0079 1.0000 0.0169
-17.250 -1.3689 0.05742 0.05219 -0.0084 1.0000 0.0176
-17.000 -1.3667 0.05467 0.04939 -0.0089 1.0000 0.0183
-16.750 -1.3630 0.05214 0.04681 -0.0092 1.0000 0.0190
-16.500 -1.3597 0.04960 0.04422 -0.0095 1.0000 0.0198
-16.250 -1.3563 0.04712 0.04170 -0.0097 1.0000 0.0207
-16.000 -1.3508 0.04494 0.03948 -0.0098 1.0000 0.0218
-15.500 -1.3385 0.04081 0.03528 -0.0097 1.0000 0.0240
-15.250 -1.3308 0.03898 0.03342 -0.0096 1.0000 0.0254
-15.000 -1.3223 0.03726 0.03166 -0.0094 1.0000 0.0266
-14.750 -1.3139 0.03560 0.02998 -0.0091 1.0000 0.0279
-14.500 -1.3059 0.03396 0.02832 -0.0087 1.0000 0.0295
-14.250 -1.2956 0.03256 0.02690 -0.0083 1.0000 0.0310
-14.000 -1.2865 0.03106 0.02538 -0.0078 1.0000 0.0328
-13.750 -1.2759 0.02970 0.02402 -0.0074 1.0000 0.0351
-13.500 -1.2653 0.02835 0.02265 -0.0069 1.0000 0.0376
-13.250 -1.2538 0.02707 0.02139 -0.0064 1.0000 0.0406
-13.000 -1.2415 0.02586 0.02017 -0.0060 1.0000 0.0436
-12.750 -1.2291 0.02466 0.01899 -0.0055 1.0000 0.0472
-12.500 -1.2173 0.02361 0.01789 -0.0048 0.9238 0.0511
-12.250 -1.2091 0.02275 0.01680 -0.0030 0.8432 0.0554
-12.000 -1.1948 0.02183 0.01577 -0.0024 0.8073 0.0595
-11.750 -1.1800 0.02086 0.01475 -0.0020 0.7844 0.0648
-11.500 -1.1643 0.01991 0.01378 -0.0017 0.7683 0.0702
-11.250 -1.1467 0.01907 0.01290 -0.0014 0.7551 0.0754
-11.000 -1.1286 0.01825 0.01206 -0.0013 0.7428 0.0802
-10.750 -1.1092 0.01748 0.01127 -0.0013 0.7320 0.0848
-10.500 -1.0894 0.01684 0.01057 -0.0012 0.7214 0.0883
-10.250 -1.0692 0.01607 0.00981 -0.0014 0.7120 0.0939
-10.000 -1.0451 0.01548 0.00918 -0.0020 0.7035 0.0988
-9.750 -1.0210 0.01490 0.00860 -0.0024 0.6954 0.1047
-9.500 -0.9962 0.01445 0.00813 -0.0027 0.6872 0.1107
-9.250 -0.9716 0.01396 0.00767 -0.0029 0.6793 0.1186
-9.000 -0.9457 0.01360 0.00728 -0.0031 0.6701 0.1253
-8.750 -0.9197 0.01321 0.00690 -0.0033 0.6610 0.1321
-8.500 -0.8932 0.01288 0.00656 -0.0036 0.6512 0.1394
-8.250 -0.8667 0.01251 0.00621 -0.0038 0.6417 0.1482
-8.000 -0.8393 0.01225 0.00592 -0.0041 0.6323 0.1550
-7.750 -0.8121 0.01193 0.00561 -0.0044 0.6219 0.1630
-7.250 -0.7566 0.01140 0.00507 -0.0050 0.6002 0.1802
-7.000 -0.7284 0.01118 0.00483 -0.0053 0.5888 0.1886
-6.750 -0.7003 0.01094 0.00460 -0.0057 0.5771 0.1985
-6.250 -0.6433 0.01052 0.00417 -0.0064 0.5551 0.2186
-6.000 -0.6148 0.01029 0.00395 -0.0068 0.5461 0.2308
-5.750 -0.5859 0.01008 0.00376 -0.0072 0.5380 0.2417
-5.250 -0.5278 0.00972 0.00342 -0.0080 0.5226 0.2653
-5.000 -0.4987 0.00954 0.00325 -0.0084 0.5152 0.2782
-4.750 -0.4693 0.00937 0.00310 -0.0088 0.5095 0.2907
-4.500 -0.4399 0.00918 0.00295 -0.0093 0.5038 0.3056
-4.250 -0.4104 0.00902 0.00282 -0.0097 0.4978 0.3210
-4.000 -0.3809 0.00885 0.00269 -0.0102 0.4927 0.3372
-3.750 -0.3511 0.00870 0.00257 -0.0106 0.4881 0.3523
-3.250 -0.2915 0.00844 0.00236 -0.0116 0.4780 0.3840
-3.000 -0.2615 0.00831 0.00228 -0.0121 0.4741 0.3977
-2.750 -0.2314 0.00819 0.00219 -0.0126 0.4694 0.4128
-2.500 -0.2014 0.00808 0.00211 -0.0130 0.4648 0.4276
-2.250 -0.1713 0.00800 0.00205 -0.0135 0.4606 0.4425
-2.000 -0.1411 0.00791 0.00199 -0.0140 0.4571 0.4562
-1.500 -0.0806 0.00773 0.00188 -0.0149 0.4480 0.4869
-1.250 -0.0505 0.00766 0.00184 -0.0154 0.4438 0.5021
-1.000 -0.0202 0.00759 0.00180 -0.0159 0.4403 0.5160
-0.750 0.0101 0.00750 0.00177 -0.0164 0.4363 0.5340
-0.500 0.0403 0.00744 0.00177 -0.0168 0.4318 0.5556
-0.250 0.0705 0.00744 0.00180 -0.0173 0.4266 0.5733
0.000 0.1009 0.00745 0.00183 -0.0177 0.4228 0.5866
0.250 0.1314 0.00748 0.00189 -0.0181 0.4189 0.5980
0.500 0.1618 0.00752 0.00192 -0.0186 0.4142 0.6054
0.750 0.1921 0.00760 0.00198 -0.0190 0.4090 0.6117
1.000 0.2226 0.00765 0.00201 -0.0194 0.4048 0.6174
1.250 0.2530 0.00770 0.00207 -0.0198 0.3994 0.6218
1.500 0.2831 0.00779 0.00213 -0.0202 0.3933 0.6257
1.750 0.3135 0.00785 0.00219 -0.0206 0.3885 0.6295
2.000 0.3438 0.00793 0.00223 -0.0210 0.3822 0.6327
2.250 0.3738 0.00804 0.00228 -0.0214 0.3742 0.6351
2.500 0.4039 0.00810 0.00235 -0.0218 0.3658 0.6375
2.750 0.4337 0.00822 0.00244 -0.0221 0.3573 0.6400
3.000 0.4637 0.00831 0.00252 -0.0225 0.3495 0.6421
3.250 0.4933 0.00844 0.00261 -0.0228 0.3400 0.6441
3.500 0.5230 0.00858 0.00270 -0.0232 0.3295 0.6461
3.750 0.5525 0.00872 0.00280 -0.0235 0.3201 0.6481
4.250 0.6113 0.00904 0.00303 -0.0242 0.2994 0.6511
4.500 0.6404 0.00921 0.00316 -0.0245 0.2906 0.6524
4.750 0.6697 0.00934 0.00328 -0.0248 0.2825 0.6540
5.000 0.6986 0.00951 0.00343 -0.0250 0.2742 0.6556
5.250 0.7274 0.00969 0.00358 -0.0253 0.2645 0.6571
5.500 0.7562 0.00988 0.00375 -0.0255 0.2558 0.6586
5.750 0.7847 0.01009 0.00392 -0.0258 0.2467 0.6600
6.000 0.8134 0.01029 0.00409 -0.0260 0.2391 0.6617
6.250 0.8419 0.01050 0.00428 -0.0262 0.2317 0.6639
6.500 0.8703 0.01070 0.00447 -0.0264 0.2255 0.6659
6.750 0.8987 0.01091 0.00465 -0.0266 0.2185 0.6673
7.000 0.9265 0.01116 0.00487 -0.0268 0.2109 0.6682
7.250 0.9546 0.01137 0.00506 -0.0269 0.2042 0.6687
7.500 0.9819 0.01163 0.00529 -0.0270 0.1965 0.6697
7.750 1.0098 0.01182 0.00549 -0.0272 0.1911 0.6706
8.000 1.0371 0.01206 0.00572 -0.0273 0.1852 0.6715
8.250 1.0642 0.01232 0.00597 -0.0273 0.1796 0.6724
8.500 1.0913 0.01256 0.00621 -0.0274 0.1737 0.6733
8.750 1.1175 0.01288 0.00651 -0.0274 0.1672 0.6743
9.000 1.1443 0.01312 0.00677 -0.0274 0.1631 0.6753
9.250 1.1706 0.01340 0.00705 -0.0274 0.1580 0.6762
9.500 1.1958 0.01377 0.00740 -0.0272 0.1517 0.6770
9.750 1.2218 0.01405 0.00769 -0.0272 0.1478 0.6779
10.000 1.2469 0.01438 0.00802 -0.0270 0.1429 0.6787
10.250 1.2707 0.01480 0.00842 -0.0267 0.1369 0.6796
10.500 1.2954 0.01512 0.00876 -0.0265 0.1330 0.6804
10.750 1.3186 0.01554 0.00917 -0.0261 0.1277 0.6813
11.000 1.3408 0.01601 0.00963 -0.0257 0.1224 0.6821
11.250 1.3633 0.01642 0.01005 -0.0252 0.1181 0.6830
11.500 1.3836 0.01695 0.01056 -0.0246 0.1130 0.6838
11.750 1.4035 0.01747 0.01109 -0.0239 0.1089 0.6845
12.000 1.4211 0.01797 0.01161 -0.0228 0.1052 0.6852
12.250 1.4348 0.01866 0.01229 -0.0214 0.1008 0.6858
12.500 1.4494 0.01945 0.01310 -0.0204 0.0967 0.6870
12.750 1.4644 0.02026 0.01395 -0.0196 0.0935 0.6883
13.000 1.4768 0.02132 0.01503 -0.0189 0.0898 0.6896
13.250 1.4873 0.02262 0.01636 -0.0183 0.0858 0.6909
13.500 1.4999 0.02387 0.01765 -0.0181 0.0828 0.6920
13.750 1.5083 0.02553 0.01933 -0.0179 0.0785 0.6931
14.000 1.5154 0.02739 0.02122 -0.0178 0.0748 0.6942
14.250 1.5236 0.02918 0.02304 -0.0177 0.0717 0.6953
14.500 1.5286 0.03130 0.02520 -0.0177 0.0686 0.6964
14.750 1.5317 0.03361 0.02754 -0.0177 0.0660 0.6974
15.000 1.5365 0.03578 0.02977 -0.0177 0.0642 0.6985
15.250 1.5395 0.03815 0.03221 -0.0178 0.0621 0.6995
15.500 1.5386 0.04094 0.03503 -0.0180 0.0596 0.7005
15.750 1.5348 0.04405 0.03818 -0.0182 0.0571 0.7013
16.000 1.5327 0.04702 0.04121 -0.0185 0.0548 0.7022
16.250 1.5279 0.05031 0.04455 -0.0188 0.0523 0.7029
16.500 1.5200 0.05409 0.04838 -0.0194 0.0496 0.7041
16.750 1.5148 0.05762 0.05197 -0.0200 0.0475 0.7053
17.000 1.5102 0.06114 0.05556 -0.0207 0.0456 0.7064
17.250 1.5020 0.06514 0.05961 -0.0215 0.0434 0.7076
17.500 1.4930 0.06928 0.06380 -0.0225 0.0414 0.7087
17.750 1.4868 0.07316 0.06776 -0.0234 0.0399 0.7099
18.000 1.4776 0.07746 0.07212 -0.0245 0.0379 0.7110
18.250 1.4684 0.08180 0.07653 -0.0257 0.0366 0.7122
18.500 1.4590 0.08623 0.08103 -0.0269 0.0347 0.7133
18.750 1.4496 0.09075 0.08561 -0.0283 0.0331 0.7145
19.000 1.4382 0.09558 0.09051 -0.0298 0.0316 0.7156
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