WB-135/35 13.5% smoothed (wb13535sm-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
|---|---|
|
Airfoil: WB-135/35 13.5% smoothed (wb13535sm-il) Reynolds number: 500,000 Max Cl/Cd: 101.34 at α=3.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-wb13535sm-il-500000.txt Download as CSV file: xf-wb13535sm-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: WB-135/35 13.5% smoothed
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
------ -------- --------- --------- -------- -------- --------
-12.250 -0.6652 0.05261 0.04947 -0.0799 1.0000 0.0136
-12.000 -0.6887 0.04675 0.04339 -0.0843 1.0000 0.0134
-11.750 -0.7052 0.04299 0.03950 -0.0865 1.0000 0.0133
-11.500 -0.7278 0.04097 0.03740 -0.0847 1.0000 0.0132
-11.250 -0.7500 0.03934 0.03567 -0.0807 0.9984 0.0133
-11.000 -0.7350 0.03490 0.03093 -0.0851 0.9921 0.0134
-10.750 -0.7160 0.03172 0.02752 -0.0878 0.9864 0.0136
-10.500 -0.6920 0.02900 0.02456 -0.0903 0.9824 0.0137
-10.250 -0.6683 0.02740 0.02285 -0.0916 0.9759 0.0142
-10.000 -0.6402 0.02546 0.02075 -0.0935 0.9721 0.0144
-9.750 -0.6123 0.02396 0.01912 -0.0949 0.9674 0.0149
-9.500 -0.5842 0.02252 0.01753 -0.0962 0.9616 0.0154
-9.250 -0.5522 0.02115 0.01600 -0.0980 0.9575 0.0159
-9.000 -0.5232 0.02020 0.01490 -0.0989 0.9499 0.0166
-8.750 -0.4944 0.01861 0.01317 -0.1001 0.9430 0.0174
-8.500 -0.4710 0.01730 0.01179 -0.1000 0.9327 0.0180
-8.250 -0.4444 0.01644 0.01085 -0.1003 0.9235 0.0188
-8.000 -0.4197 0.01574 0.01004 -0.1000 0.9131 0.0198
-7.750 -0.3973 0.01511 0.00931 -0.0992 0.9016 0.0206
-7.500 -0.3737 0.01460 0.00868 -0.0984 0.8909 0.0215
-7.250 -0.3537 0.01373 0.00767 -0.0972 0.8801 0.0231
-7.000 -0.3318 0.01319 0.00707 -0.0961 0.8689 0.0247
-6.750 -0.3083 0.01278 0.00655 -0.0953 0.8586 0.0267
-6.500 -0.2848 0.01228 0.00592 -0.0945 0.8495 0.0290
-6.250 -0.2621 0.01175 0.00531 -0.0935 0.8394 0.0333
-6.000 -0.2388 0.01123 0.00473 -0.0926 0.8301 0.0427
-5.750 -0.2203 0.01011 0.00404 -0.0913 0.8213 0.1351
-5.500 -0.1948 0.00990 0.00387 -0.0908 0.8125 0.1633
-5.250 -0.1680 0.00980 0.00371 -0.0905 0.8054 0.1786
-5.000 -0.1417 0.00970 0.00359 -0.0901 0.7973 0.1910
-4.500 -0.0885 0.00952 0.00334 -0.0895 0.7831 0.2133
-4.250 -0.0617 0.00944 0.00322 -0.0892 0.7767 0.2248
-4.000 -0.0352 0.00936 0.00312 -0.0889 0.7692 0.2369
-3.750 -0.0084 0.00932 0.00301 -0.0885 0.7617 0.2487
-3.500 0.0176 0.00919 0.00290 -0.0881 0.7536 0.2588
-3.250 0.0442 0.00912 0.00278 -0.0877 0.7467 0.2684
-3.000 0.0708 0.00905 0.00269 -0.0874 0.7395 0.2797
-2.750 0.0976 0.00899 0.00261 -0.0870 0.7328 0.2923
-2.500 0.1243 0.00893 0.00255 -0.0867 0.7267 0.3051
-2.250 0.1509 0.00886 0.00249 -0.0864 0.7205 0.3178
-1.750 0.2046 0.00877 0.00239 -0.0858 0.7085 0.3436
-1.500 0.2314 0.00874 0.00234 -0.0855 0.7021 0.3572
-1.250 0.2581 0.00870 0.00231 -0.0852 0.6956 0.3704
-1.000 0.2846 0.00865 0.00228 -0.0848 0.6893 0.3835
-0.750 0.3117 0.00863 0.00226 -0.0846 0.6843 0.3971
-0.500 0.3381 0.00858 0.00226 -0.0842 0.6785 0.4116
-0.250 0.3647 0.00854 0.00226 -0.0839 0.6727 0.4282
0.000 0.3914 0.00853 0.00226 -0.0836 0.6670 0.4455
0.250 0.4177 0.00848 0.00228 -0.0832 0.6605 0.4638
0.500 0.4441 0.00847 0.00229 -0.0828 0.6550 0.4833
0.750 0.4702 0.00842 0.00233 -0.0824 0.6486 0.5051
1.000 0.4962 0.00840 0.00235 -0.0819 0.6422 0.5276
1.250 0.5220 0.00836 0.00238 -0.0814 0.6356 0.5516
1.500 0.5472 0.00831 0.00241 -0.0808 0.6279 0.5776
1.750 0.5721 0.00825 0.00244 -0.0801 0.6200 0.6078
2.000 0.5960 0.00815 0.00247 -0.0792 0.6114 0.6478
2.250 0.6164 0.00787 0.00252 -0.0775 0.6028 0.7359
2.500 0.7314 0.00760 0.00274 -0.0965 0.5854 0.9962
2.750 0.7645 0.00770 0.00278 -0.0977 0.5705 1.0000
3.000 0.7870 0.00782 0.00284 -0.0966 0.5532 1.0000
3.250 0.8087 0.00798 0.00291 -0.0953 0.5315 1.0000
3.500 0.8286 0.00821 0.00301 -0.0936 0.4999 1.0000
3.750 0.8449 0.00861 0.00318 -0.0913 0.4548 1.0000
4.000 0.8604 0.00909 0.00343 -0.0890 0.4137 1.0000
4.500 0.8970 0.00986 0.00394 -0.0854 0.3692 1.0000
4.750 0.9165 0.01019 0.00419 -0.0838 0.3553 1.0000
5.250 0.9572 0.01077 0.00467 -0.0809 0.3315 1.0000
5.500 0.9776 0.01104 0.00490 -0.0795 0.3216 1.0000
5.750 0.9975 0.01133 0.00515 -0.0781 0.3127 1.0000
6.000 1.0188 0.01155 0.00538 -0.0769 0.3047 1.0000
6.500 1.0594 0.01206 0.00587 -0.0741 0.2883 1.0000
6.750 1.0781 0.01236 0.00614 -0.0724 0.2802 1.0000
7.000 1.0981 0.01260 0.00638 -0.0710 0.2696 1.0000
7.250 1.1169 0.01288 0.00664 -0.0694 0.2565 1.0000
7.500 1.1337 0.01322 0.00692 -0.0675 0.2398 1.0000
7.750 1.1461 0.01365 0.00723 -0.0647 0.2129 1.0000
8.000 1.1506 0.01442 0.00772 -0.0607 0.1704 1.0000
8.250 1.1415 0.01594 0.00878 -0.0548 0.1020 1.0000
8.500 1.1262 0.01805 0.01041 -0.0486 0.0277 1.0000
8.750 1.1371 0.01886 0.01122 -0.0462 0.0216 1.0000
9.000 1.1489 0.01964 0.01206 -0.0441 0.0195 1.0000
9.250 1.1599 0.02052 0.01303 -0.0419 0.0179 1.0000
9.500 1.1722 0.02135 0.01393 -0.0401 0.0172 1.0000
9.750 1.1835 0.02226 0.01492 -0.0382 0.0167 1.0000
10.000 1.1923 0.02338 0.01612 -0.0362 0.0159 1.0000
10.250 1.2010 0.02454 0.01736 -0.0344 0.0155 1.0000
10.500 1.2080 0.02587 0.01878 -0.0325 0.0152 1.0000
10.750 1.2105 0.02759 0.02058 -0.0305 0.0146 1.0000
11.000 1.2088 0.02973 0.02282 -0.0284 0.0140 1.0000
11.250 1.2063 0.03205 0.02524 -0.0265 0.0138 1.0000
11.500 1.2089 0.03403 0.02731 -0.0252 0.0134 1.0000
11.750 1.2122 0.03603 0.02940 -0.0241 0.0132 1.0000
12.000 1.2156 0.03806 0.03152 -0.0231 0.0130 1.0000
12.250 1.2157 0.04048 0.03402 -0.0220 0.0128 1.0000
12.500 1.2172 0.04281 0.03644 -0.0212 0.0125 1.0000
12.750 1.2176 0.04533 0.03904 -0.0205 0.0125 1.0000
13.000 1.2175 0.04796 0.04176 -0.0198 0.0124 1.0000
13.250 1.2175 0.05063 0.04451 -0.0193 0.0121 1.0000
13.500 1.2170 0.05340 0.04736 -0.0187 0.0120 1.0000
13.750 1.2174 0.05612 0.05014 -0.0183 0.0117 1.0000
14.000 1.2185 0.05881 0.05289 -0.0179 0.0115 1.0000
14.250 1.2204 0.06140 0.05554 -0.0176 0.0114 1.0000
14.500 1.2226 0.06396 0.05816 -0.0172 0.0113 1.0000
14.750 1.2251 0.06651 0.06076 -0.0168 0.0111 1.0000
15.000 1.2287 0.06878 0.06303 -0.0162 0.0107 1.0000
15.250 1.2376 0.07017 0.06441 -0.0146 0.0105 1.0000
15.500 1.2585 0.07017 0.06441 -0.0110 0.0102 1.0000
15.750 1.2489 0.07449 0.06892 -0.0126 0.0100 1.0000
16.000 1.2490 0.07762 0.07218 -0.0129 0.0100 1.0000
16.250 1.2537 0.08005 0.07471 -0.0125 0.0100 1.0000
16.500 1.2509 0.08370 0.07849 -0.0133 0.0099 1.0000
16.750 1.2499 0.08710 0.08202 -0.0138 0.0098 1.0000
17.000 1.2480 0.09071 0.08577 -0.0143 0.0098 1.0000
17.250 1.2456 0.09441 0.08961 -0.0148 0.0098 1.0000
17.500 1.2472 0.09747 0.09278 -0.0144 0.0100 1.0000
17.750 1.2412 0.10186 0.09731 -0.0156 0.0100 1.0000
|
Polar data table (+)
Polar graphs
<< Back to WB-135/35 13.5% smoothed (wb13535sm-il)