NACA0012H for VAWT from Sandia report SAND80-2114 (naca0012h-sa) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: NACA0012H for VAWT from Sandia report SAND80-2114 (naca0012h-sa) Reynolds number: 100,000 Max Cl/Cd: 33.53 at α=7.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca0012h-sa-100000-n5.txt Download as CSV file: xf-naca0012h-sa-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA0012H for VAWT from Sandia report SAND80-211
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.750 -1.0473 0.06564 0.05889 -0.0331 1.0000 0.0703
-13.500 -1.0644 0.06051 0.05361 -0.0356 1.0000 0.0709
-13.250 -1.0768 0.05651 0.04944 -0.0368 1.0000 0.0717
-13.000 -1.0876 0.05308 0.04585 -0.0370 1.0000 0.0726
-12.750 -1.0971 0.05007 0.04265 -0.0364 1.0000 0.0736
-12.500 -1.1057 0.04736 0.03972 -0.0349 1.0000 0.0748
-12.250 -1.1132 0.04488 0.03697 -0.0326 1.0000 0.0762
-12.000 -1.1178 0.04247 0.03421 -0.0301 1.0000 0.0777
-11.750 -1.1102 0.04074 0.03232 -0.0285 1.0000 0.0792
-11.500 -1.0962 0.03968 0.03128 -0.0273 1.0000 0.0807
-11.250 -1.0834 0.03851 0.03004 -0.0259 1.0000 0.0826
-11.000 -1.0715 0.03712 0.02847 -0.0244 1.0000 0.0848
-10.750 -1.0595 0.03554 0.02659 -0.0229 1.0000 0.0873
-10.500 -1.0445 0.03416 0.02506 -0.0216 1.0000 0.0895
-10.250 -1.0264 0.03329 0.02421 -0.0205 1.0000 0.0916
-10.000 -1.0087 0.03235 0.02320 -0.0193 1.0000 0.0943
-9.750 -0.9911 0.03125 0.02190 -0.0181 1.0000 0.0974
-9.500 -0.9728 0.03010 0.02054 -0.0170 1.0000 0.1004
-9.250 -0.9530 0.02932 0.01981 -0.0160 1.0000 0.1030
-9.000 -0.9331 0.02855 0.01899 -0.0149 1.0000 0.1063
-8.750 -0.9130 0.02767 0.01793 -0.0138 1.0000 0.1102
-8.500 -0.8925 0.02681 0.01700 -0.0128 1.0000 0.1136
-8.250 -0.8718 0.02616 0.01638 -0.0117 1.0000 0.1171
-8.000 -0.8507 0.02547 0.01560 -0.0107 1.0000 0.1215
-7.750 -0.8293 0.02473 0.01471 -0.0096 1.0000 0.1259
-7.500 -0.8084 0.02412 0.01417 -0.0085 1.0000 0.1298
-7.250 -0.7870 0.02354 0.01355 -0.0074 1.0000 0.1347
-7.000 -0.7652 0.02292 0.01282 -0.0064 1.0000 0.1399
-6.750 -0.7442 0.02238 0.01235 -0.0052 1.0000 0.1444
-6.500 -0.7226 0.02188 0.01181 -0.0041 1.0000 0.1502
-6.250 -0.7011 0.02135 0.01124 -0.0029 1.0000 0.1558
-6.000 -0.6799 0.02089 0.01083 -0.0017 1.0000 0.1615
-5.750 -0.6579 0.02046 0.01033 -0.0006 1.0000 0.1685
-5.500 -0.6368 0.02000 0.00995 0.0006 1.0000 0.1744
-5.250 -0.6151 0.01961 0.00956 0.0018 1.0000 0.1818
-5.000 -0.5937 0.01921 0.00920 0.0030 1.0000 0.1889
-4.750 -0.5722 0.01886 0.00887 0.0041 1.0000 0.1969
-4.500 -0.5508 0.01850 0.00855 0.0053 1.0000 0.2048
-4.250 -0.5294 0.01819 0.00828 0.0065 1.0000 0.2136
-4.000 -0.5080 0.01788 0.00802 0.0077 1.0000 0.2224
-3.750 -0.4865 0.01761 0.00777 0.0088 1.0000 0.2323
-3.500 -0.4653 0.01733 0.00758 0.0100 1.0000 0.2421
-3.250 -0.4436 0.01711 0.00739 0.0110 1.0000 0.2533
-3.000 -0.4223 0.01686 0.00723 0.0121 1.0000 0.2646
-2.750 -0.4009 0.01663 0.00708 0.0131 1.0000 0.2770
-2.500 -0.3598 0.01635 0.00691 0.0103 0.9924 0.2950
-2.250 -0.3179 0.01600 0.00670 0.0073 0.9827 0.3162
-2.000 -0.2771 0.01558 0.00651 0.0046 0.9716 0.3425
-1.750 -0.2378 0.01510 0.00636 0.0023 0.9598 0.3876
-1.500 -0.2006 0.01454 0.00627 0.0005 0.9478 0.4657
-1.250 -0.1658 0.01405 0.00624 -0.0004 0.9339 0.5601
-1.000 -0.1321 0.01369 0.00623 -0.0007 0.9168 0.6383
-0.750 -0.0993 0.01346 0.00625 -0.0007 0.8973 0.7005
-0.500 -0.0659 0.01331 0.00625 -0.0005 0.8745 0.7500
-0.250 -0.0321 0.01323 0.00625 -0.0004 0.8506 0.7902
0.000 0.0000 0.01321 0.00627 0.0000 0.8227 0.8227
0.250 0.0321 0.01323 0.00625 0.0004 0.7902 0.8506
0.500 0.0659 0.01331 0.00625 0.0005 0.7500 0.8745
0.750 0.0993 0.01346 0.00625 0.0006 0.7005 0.8973
1.000 0.1321 0.01369 0.00623 0.0007 0.6383 0.9168
1.250 0.1657 0.01405 0.00624 0.0004 0.5601 0.9339
1.500 0.2006 0.01454 0.00627 -0.0005 0.4657 0.9478
1.750 0.2378 0.01510 0.00636 -0.0023 0.3876 0.9598
2.000 0.2771 0.01558 0.00651 -0.0046 0.3425 0.9716
2.250 0.3179 0.01600 0.00670 -0.0073 0.3162 0.9827
2.500 0.3598 0.01635 0.00690 -0.0103 0.2950 0.9924
2.750 0.4008 0.01663 0.00708 -0.0131 0.2771 1.0000
3.000 0.4222 0.01686 0.00722 -0.0121 0.2646 1.0000
3.250 0.4435 0.01711 0.00738 -0.0110 0.2533 1.0000
3.500 0.4652 0.01733 0.00758 -0.0099 0.2421 1.0000
3.750 0.4864 0.01761 0.00777 -0.0088 0.2324 1.0000
4.000 0.5079 0.01788 0.00802 -0.0077 0.2224 1.0000
4.250 0.5293 0.01819 0.00827 -0.0065 0.2137 1.0000
4.500 0.5507 0.01850 0.00854 -0.0053 0.2048 1.0000
4.750 0.5722 0.01886 0.00887 -0.0041 0.1969 1.0000
5.000 0.5936 0.01921 0.00919 -0.0029 0.1889 1.0000
5.250 0.6150 0.01961 0.00955 -0.0018 0.1818 1.0000
5.500 0.6367 0.02000 0.00995 -0.0006 0.1745 1.0000
5.750 0.6579 0.02046 0.01033 0.0006 0.1685 1.0000
6.000 0.6798 0.02089 0.01083 0.0017 0.1615 1.0000
6.250 0.7010 0.02134 0.01124 0.0029 0.1558 1.0000
6.500 0.7226 0.02188 0.01181 0.0041 0.1502 1.0000
6.750 0.7441 0.02238 0.01234 0.0052 0.1444 1.0000
7.000 0.7652 0.02292 0.01282 0.0064 0.1399 1.0000
7.250 0.7869 0.02354 0.01355 0.0074 0.1347 1.0000
7.500 0.8084 0.02412 0.01417 0.0085 0.1298 1.0000
7.750 0.8293 0.02473 0.01471 0.0096 0.1259 1.0000
8.000 0.8507 0.02547 0.01560 0.0107 0.1215 1.0000
8.250 0.8718 0.02616 0.01637 0.0117 0.1171 1.0000
8.500 0.8926 0.02681 0.01700 0.0127 0.1136 1.0000
8.750 0.9131 0.02767 0.01793 0.0138 0.1102 1.0000
9.000 0.9332 0.02855 0.01899 0.0149 0.1063 1.0000
9.250 0.9531 0.02932 0.01981 0.0159 0.1030 1.0000
9.500 0.9730 0.03010 0.02054 0.0169 0.1004 1.0000
9.750 0.9912 0.03125 0.02190 0.0181 0.0974 1.0000
10.000 1.0089 0.03236 0.02320 0.0193 0.0943 1.0000
10.250 1.0266 0.03329 0.02421 0.0205 0.0916 1.0000
10.500 1.0447 0.03417 0.02506 0.0215 0.0895 1.0000
10.750 1.0597 0.03554 0.02660 0.0228 0.0873 1.0000
11.000 1.0718 0.03712 0.02848 0.0243 0.0848 1.0000
11.250 1.0838 0.03851 0.03004 0.0258 0.0826 1.0000
11.500 1.0966 0.03968 0.03128 0.0272 0.0807 1.0000
11.750 1.1107 0.04074 0.03232 0.0284 0.0791 1.0000
12.000 1.1182 0.04249 0.03423 0.0300 0.0777 1.0000
12.250 1.1137 0.04490 0.03699 0.0325 0.0762 1.0000
12.500 1.1064 0.04738 0.03973 0.0347 0.0748 1.0000
12.750 1.0980 0.05007 0.04265 0.0362 0.0736 1.0000
13.000 1.0886 0.05307 0.04584 0.0369 0.0726 1.0000
13.250 1.0782 0.05647 0.04941 0.0367 0.0716 1.0000
13.500 1.0664 0.06041 0.05349 0.0355 0.0709 1.0000
13.750 1.0519 0.06517 0.05839 0.0333 0.0702 1.0000
|
Polar data table (+)
Polar graphs
<< Back to NACA0012H for VAWT from Sandia report SAND80-2114 (naca0012h-sa)