PSU-90-125WL (psu-90-125wl-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: PSU-90-125WL (psu-90-125wl-il) Reynolds number: 500,000 Max Cl/Cd: 87.8 at α=5.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-psu-90-125wl-il-500000-n5.txt Download as CSV file: xf-psu-90-125wl-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: PSU-90-125WL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.750 -0.5601 0.08865 0.08620 -0.0481 1.0000 0.0102
-12.500 -0.6604 0.06126 0.05850 -0.0659 1.0000 0.0098
-12.250 -0.6863 0.05301 0.05007 -0.0722 1.0000 0.0097
-12.000 -0.7084 0.04709 0.04397 -0.0759 1.0000 0.0097
-11.750 -0.7290 0.04257 0.03928 -0.0775 1.0000 0.0096
-11.500 -0.7461 0.03946 0.03602 -0.0770 1.0000 0.0097
-11.250 -0.7666 0.03714 0.03357 -0.0742 1.0000 0.0098
-11.000 -0.7680 0.03443 0.03063 -0.0744 0.9948 0.0098
-10.750 -0.7550 0.03157 0.02748 -0.0761 0.9873 0.0100
-10.500 -0.7369 0.02920 0.02484 -0.0775 0.9815 0.0101
-10.250 -0.7181 0.02730 0.02269 -0.0782 0.9735 0.0103
-10.000 -0.6961 0.02561 0.02076 -0.0789 0.9658 0.0105
-9.750 -0.6712 0.02405 0.01899 -0.0800 0.9580 0.0107
-9.500 -0.6461 0.02276 0.01751 -0.0807 0.9486 0.0108
-9.250 -0.6183 0.02152 0.01609 -0.0818 0.9403 0.0109
-9.000 -0.5903 0.02048 0.01488 -0.0827 0.9305 0.0111
-8.750 -0.5673 0.01881 0.01304 -0.0829 0.9186 0.0115
-8.500 -0.5431 0.01787 0.01198 -0.0830 0.9068 0.0119
-8.250 -0.5194 0.01712 0.01112 -0.0827 0.8956 0.0121
-8.000 -0.4963 0.01643 0.01032 -0.0822 0.8851 0.0124
-7.750 -0.4736 0.01579 0.00958 -0.0816 0.8754 0.0127
-7.500 -0.4505 0.01519 0.00888 -0.0810 0.8667 0.0129
-7.250 -0.4273 0.01464 0.00822 -0.0804 0.8580 0.0133
-7.000 -0.4036 0.01413 0.00762 -0.0799 0.8507 0.0136
-6.750 -0.3796 0.01365 0.00706 -0.0793 0.8435 0.0139
-6.500 -0.3552 0.01322 0.00654 -0.0789 0.8371 0.0142
-6.250 -0.3304 0.01283 0.00606 -0.0785 0.8304 0.0146
-5.750 -0.2798 0.01211 0.00519 -0.0777 0.8187 0.0152
-5.500 -0.2548 0.01168 0.00469 -0.0774 0.8128 0.0162
-5.250 -0.2290 0.01138 0.00433 -0.0771 0.8074 0.0173
-5.000 -0.2028 0.01111 0.00401 -0.0769 0.8017 0.0183
-4.750 -0.1763 0.01089 0.00371 -0.0766 0.7965 0.0192
-4.500 -0.1496 0.01067 0.00345 -0.0764 0.7914 0.0209
-4.250 -0.1232 0.01041 0.00319 -0.0762 0.7860 0.0261
-4.000 -0.0974 0.01006 0.00293 -0.0760 0.7811 0.0514
-3.750 -0.0714 0.00972 0.00271 -0.0758 0.7760 0.0842
-3.500 -0.0455 0.00937 0.00252 -0.0757 0.7706 0.1266
-3.250 -0.0196 0.00904 0.00235 -0.0755 0.7658 0.1763
-3.000 0.0069 0.00877 0.00221 -0.0754 0.7606 0.2182
-2.750 0.0334 0.00851 0.00208 -0.0753 0.7552 0.2637
-2.250 0.0855 0.00788 0.00187 -0.0751 0.7451 0.3951
-2.000 0.1115 0.00757 0.00180 -0.0749 0.7397 0.4671
-1.750 0.1382 0.00742 0.00176 -0.0747 0.7347 0.5146
-1.500 0.1655 0.00731 0.00174 -0.0746 0.7289 0.5511
-1.250 0.1928 0.00725 0.00172 -0.0744 0.7229 0.5810
-1.000 0.2203 0.00721 0.00172 -0.0743 0.7169 0.6040
-0.750 0.2479 0.00719 0.00171 -0.0742 0.7103 0.6237
-0.500 0.2755 0.00718 0.00170 -0.0741 0.7040 0.6404
-0.250 0.3032 0.00717 0.00171 -0.0740 0.6969 0.6555
0.000 0.3307 0.00717 0.00171 -0.0739 0.6900 0.6685
0.250 0.3583 0.00717 0.00172 -0.0738 0.6819 0.6802
0.500 0.3857 0.00718 0.00173 -0.0736 0.6734 0.6917
0.750 0.4130 0.00721 0.00175 -0.0735 0.6634 0.7033
1.000 0.4401 0.00722 0.00177 -0.0733 0.6525 0.7147
1.250 0.4670 0.00725 0.00180 -0.0730 0.6405 0.7254
1.500 0.4938 0.00729 0.00184 -0.0728 0.6270 0.7360
1.750 0.5202 0.00735 0.00188 -0.0724 0.6112 0.7470
2.000 0.5460 0.00743 0.00193 -0.0720 0.5930 0.7579
2.250 0.5713 0.00754 0.00200 -0.0715 0.5736 0.7689
2.500 0.5965 0.00767 0.00208 -0.0709 0.5523 0.7802
2.750 0.6210 0.00784 0.00219 -0.0703 0.5309 0.7920
3.000 0.6456 0.00799 0.00232 -0.0696 0.5097 0.8043
3.250 0.6697 0.00816 0.00245 -0.0689 0.4886 0.8173
3.500 0.6936 0.00833 0.00260 -0.0681 0.4676 0.8311
3.750 0.7172 0.00852 0.00275 -0.0673 0.4466 0.8456
4.000 0.7401 0.00872 0.00293 -0.0663 0.4256 0.8616
4.250 0.7626 0.00891 0.00310 -0.0653 0.4041 0.8796
4.500 0.7842 0.00912 0.00329 -0.0640 0.3837 0.9007
5.000 0.8353 0.00959 0.00370 -0.0633 0.3408 0.9582
5.250 0.8692 0.00990 0.00393 -0.0650 0.3181 1.0000
5.500 0.8918 0.01021 0.00417 -0.0642 0.2982 1.0000
5.750 0.9144 0.01054 0.00442 -0.0634 0.2799 1.0000
6.000 0.9368 0.01087 0.00469 -0.0626 0.2599 1.0000
6.250 0.9588 0.01123 0.00497 -0.0617 0.2409 1.0000
6.500 0.9800 0.01163 0.00528 -0.0607 0.2204 1.0000
6.750 1.0002 0.01209 0.00562 -0.0596 0.1965 1.0000
7.000 1.0200 0.01256 0.00600 -0.0584 0.1734 1.0000
7.250 1.0398 0.01302 0.00637 -0.0572 0.1548 1.0000
7.500 1.0592 0.01349 0.00676 -0.0560 0.1381 1.0000
7.750 1.0777 0.01400 0.00718 -0.0546 0.1192 1.0000
8.000 1.0953 0.01453 0.00763 -0.0531 0.1020 1.0000
8.250 1.1116 0.01504 0.00808 -0.0513 0.0885 1.0000
8.500 1.1271 0.01557 0.00856 -0.0494 0.0759 1.0000
8.750 1.1416 0.01616 0.00909 -0.0474 0.0633 1.0000
9.000 1.1556 0.01679 0.00966 -0.0454 0.0515 1.0000
9.250 1.1693 0.01745 0.01027 -0.0434 0.0413 1.0000
9.500 1.1844 0.01804 0.01088 -0.0417 0.0351 1.0000
9.750 1.1969 0.01880 0.01160 -0.0396 0.0267 1.0000
10.000 1.2079 0.01965 0.01242 -0.0375 0.0186 1.0000
10.250 1.2172 0.02064 0.01337 -0.0353 0.0115 1.0000
10.500 1.2293 0.02147 0.01424 -0.0335 0.0097 1.0000
10.750 1.2403 0.02240 0.01520 -0.0316 0.0083 1.0000
11.000 1.2513 0.02335 0.01621 -0.0299 0.0075 1.0000
11.250 1.2632 0.02427 0.01721 -0.0283 0.0071 1.0000
11.500 1.2740 0.02529 0.01832 -0.0268 0.0068 1.0000
11.750 1.2846 0.02636 0.01946 -0.0253 0.0065 1.0000
12.000 1.2935 0.02758 0.02077 -0.0238 0.0062 1.0000
12.250 1.3019 0.02887 0.02214 -0.0223 0.0059 1.0000
12.500 1.3093 0.03029 0.02365 -0.0210 0.0058 1.0000
12.750 1.3150 0.03189 0.02533 -0.0196 0.0056 1.0000
13.000 1.3196 0.03364 0.02718 -0.0183 0.0055 1.0000
13.250 1.3204 0.03579 0.02944 -0.0170 0.0053 1.0000
13.500 1.3229 0.03785 0.03161 -0.0160 0.0052 1.0000
13.750 1.3262 0.03991 0.03379 -0.0152 0.0052 1.0000
14.000 1.3282 0.04217 0.03616 -0.0145 0.0051 1.0000
14.250 1.3284 0.04471 0.03881 -0.0139 0.0050 1.0000
14.500 1.3278 0.04745 0.04167 -0.0136 0.0050 1.0000
14.750 1.3279 0.05024 0.04456 -0.0135 0.0048 1.0000
15.000 1.3256 0.05344 0.04788 -0.0137 0.0048 1.0000
15.250 1.3214 0.05703 0.05160 -0.0141 0.0048 1.0000
15.500 1.3188 0.06058 0.05527 -0.0148 0.0047 1.0000
15.750 1.3128 0.06477 0.05958 -0.0158 0.0046 1.0000
16.000 1.3075 0.06904 0.06399 -0.0171 0.0045 1.0000
16.250 1.3031 0.07333 0.06839 -0.0186 0.0044 1.0000
16.500 1.2943 0.07845 0.07364 -0.0205 0.0044 1.0000
16.750 1.2876 0.08342 0.07874 -0.0226 0.0043 1.0000
17.000 1.2786 0.08891 0.08435 -0.0250 0.0043 1.0000
17.250 1.2676 0.09486 0.09044 -0.0277 0.0043 1.0000
17.500 1.2563 0.10104 0.09675 -0.0306 0.0043 1.0000
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