SD7032-099-88 (sd7032-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: SD7032-099-88 (sd7032-il) Reynolds number: 500,000 Max Cl/Cd: 97.81 at α=5.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-sd7032-il-500000-n5.txt Download as CSV file: xf-sd7032-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: SD7032-099-88
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
------ -------- --------- --------- -------- -------- --------
-9.250 -0.3392 0.09119 0.08894 -0.0372 1.0000 0.0063
-9.000 -0.3431 0.08743 0.08521 -0.0379 1.0000 0.0063
-8.750 -0.3443 0.08254 0.08036 -0.0405 0.9973 0.0065
-8.500 -0.3359 0.07742 0.07525 -0.0456 0.9881 0.0064
-8.250 -0.3277 0.07037 0.06821 -0.0537 0.9810 0.0065
-8.000 -0.3196 0.06138 0.05922 -0.0664 0.9694 0.0065
-7.750 -0.3635 0.02654 0.02315 -0.0970 0.9366 0.0064
-7.500 -0.3497 0.02181 0.01770 -0.0974 0.9287 0.0066
-7.250 -0.3304 0.01917 0.01464 -0.0974 0.9212 0.0070
-7.000 -0.3066 0.01802 0.01327 -0.0972 0.9152 0.0072
-6.750 -0.2822 0.01691 0.01196 -0.0970 0.9089 0.0075
-6.500 -0.2573 0.01592 0.01077 -0.0967 0.9024 0.0077
-6.250 -0.2319 0.01499 0.00964 -0.0964 0.8965 0.0081
-6.000 -0.2061 0.01409 0.00856 -0.0961 0.8896 0.0086
-5.750 -0.1801 0.01331 0.00759 -0.0958 0.8835 0.0091
-5.500 -0.1536 0.01266 0.00680 -0.0955 0.8760 0.0096
-5.250 -0.1274 0.01202 0.00605 -0.0953 0.8694 0.0102
-5.000 -0.1002 0.01168 0.00567 -0.0951 0.8614 0.0110
-4.750 -0.0731 0.01139 0.00529 -0.0949 0.8541 0.0122
-4.500 -0.0457 0.01108 0.00490 -0.0947 0.8455 0.0133
-4.250 -0.0187 0.01059 0.00435 -0.0946 0.8371 0.0146
-4.000 0.0087 0.01029 0.00398 -0.0944 0.8278 0.0162
-3.750 0.0363 0.01003 0.00364 -0.0943 0.8180 0.0177
-3.500 0.0636 0.00971 0.00325 -0.0941 0.8080 0.0200
-3.250 0.0912 0.00950 0.00297 -0.0940 0.7971 0.0223
-3.000 0.1189 0.00932 0.00271 -0.0938 0.7854 0.0243
-2.750 0.1465 0.00909 0.00243 -0.0937 0.7732 0.0278
-2.500 0.1743 0.00895 0.00221 -0.0936 0.7606 0.0311
-2.250 0.2019 0.00877 0.00201 -0.0934 0.7472 0.0416
-2.000 0.2294 0.00858 0.00185 -0.0933 0.7334 0.0702
-1.750 0.2568 0.00841 0.00173 -0.0933 0.7188 0.1071
-1.500 0.2843 0.00824 0.00163 -0.0932 0.7038 0.1522
-1.250 0.3115 0.00800 0.00156 -0.0932 0.6885 0.2263
-1.000 0.3387 0.00781 0.00151 -0.0932 0.6730 0.2995
-0.750 0.3659 0.00764 0.00148 -0.0932 0.6570 0.3755
-0.500 0.3929 0.00743 0.00148 -0.0931 0.6413 0.4739
-0.250 0.4194 0.00722 0.00153 -0.0929 0.6254 0.5831
0.000 0.4459 0.00714 0.00157 -0.0926 0.6098 0.6523
0.250 0.4724 0.00712 0.00161 -0.0922 0.5942 0.7025
0.500 0.4984 0.00711 0.00166 -0.0917 0.5787 0.7517
0.750 0.5238 0.00712 0.00172 -0.0910 0.5631 0.7977
1.000 0.5485 0.00714 0.00177 -0.0901 0.5478 0.8411
1.250 0.5719 0.00715 0.00181 -0.0890 0.5324 0.8855
1.500 0.5982 0.00714 0.00183 -0.0884 0.5164 0.9482
1.750 0.6305 0.00727 0.00186 -0.0894 0.4985 1.0000
2.000 0.6575 0.00745 0.00194 -0.0892 0.4807 1.0000
2.250 0.6844 0.00763 0.00202 -0.0891 0.4636 1.0000
2.500 0.7114 0.00782 0.00212 -0.0889 0.4477 1.0000
2.750 0.7382 0.00801 0.00222 -0.0888 0.4318 1.0000
3.250 0.7917 0.00841 0.00246 -0.0885 0.4014 1.0000
3.500 0.8183 0.00862 0.00261 -0.0883 0.3865 1.0000
4.000 0.8713 0.00904 0.00291 -0.0879 0.3587 1.0000
4.250 0.8976 0.00927 0.00309 -0.0877 0.3444 1.0000
4.500 0.9239 0.00949 0.00327 -0.0875 0.3316 1.0000
4.750 0.9500 0.00973 0.00346 -0.0873 0.3180 1.0000
5.000 0.9759 0.00998 0.00367 -0.0870 0.3044 1.0000
5.250 1.0016 0.01024 0.00389 -0.0867 0.2909 1.0000
5.500 1.0270 0.01053 0.00412 -0.0864 0.2760 1.0000
5.750 1.0523 0.01082 0.00437 -0.0861 0.2622 1.0000
6.000 1.0774 0.01112 0.00464 -0.0857 0.2486 1.0000
6.250 1.1022 0.01145 0.00492 -0.0853 0.2339 1.0000
6.500 1.1266 0.01180 0.00522 -0.0849 0.2185 1.0000
6.750 1.1505 0.01220 0.00554 -0.0843 0.2020 1.0000
7.000 1.1743 0.01259 0.00589 -0.0838 0.1873 1.0000
7.250 1.1983 0.01294 0.00623 -0.0833 0.1758 1.0000
7.500 1.2218 0.01333 0.00659 -0.0828 0.1641 1.0000
7.750 1.2448 0.01376 0.00698 -0.0821 0.1515 1.0000
8.000 1.2676 0.01419 0.00741 -0.0815 0.1402 1.0000
8.250 1.2896 0.01466 0.00785 -0.0807 0.1278 1.0000
8.500 1.3112 0.01516 0.00832 -0.0799 0.1155 1.0000
8.750 1.3320 0.01570 0.00882 -0.0790 0.1029 1.0000
9.000 1.3521 0.01628 0.00936 -0.0780 0.0903 1.0000
9.250 1.3714 0.01689 0.00995 -0.0769 0.0789 1.0000
9.500 1.3897 0.01755 0.01057 -0.0756 0.0686 1.0000
9.750 1.4078 0.01817 0.01120 -0.0743 0.0602 1.0000
10.000 1.4247 0.01885 0.01187 -0.0729 0.0520 1.0000
10.250 1.4395 0.01955 0.01256 -0.0711 0.0457 1.0000
10.500 1.4530 0.02023 0.01327 -0.0691 0.0405 1.0000
10.750 1.4655 0.02097 0.01403 -0.0670 0.0360 1.0000
11.000 1.4776 0.02174 0.01484 -0.0650 0.0319 1.0000
11.250 1.4885 0.02260 0.01572 -0.0629 0.0281 1.0000
11.500 1.5002 0.02343 0.01661 -0.0610 0.0252 1.0000
11.750 1.5091 0.02449 0.01769 -0.0590 0.0219 1.0000
12.000 1.5198 0.02543 0.01871 -0.0572 0.0200 1.0000
12.250 1.5276 0.02662 0.01993 -0.0553 0.0172 1.0000
12.500 1.5357 0.02784 0.02122 -0.0535 0.0154 1.0000
12.750 1.5425 0.02920 0.02266 -0.0518 0.0133 1.0000
13.000 1.5479 0.03074 0.02426 -0.0502 0.0118 1.0000
13.250 1.5536 0.03232 0.02593 -0.0488 0.0104 1.0000
13.500 1.5560 0.03426 0.02794 -0.0474 0.0088 1.0000
13.750 1.5593 0.03623 0.03001 -0.0462 0.0077 1.0000
14.000 1.5594 0.03860 0.03247 -0.0452 0.0065 1.0000
14.250 1.5599 0.04105 0.03503 -0.0444 0.0058 1.0000
14.500 1.5589 0.04380 0.03789 -0.0439 0.0051 1.0000
14.750 1.5567 0.04683 0.04103 -0.0437 0.0047 1.0000
15.000 1.5518 0.05033 0.04465 -0.0438 0.0042 1.0000
15.250 1.5483 0.05386 0.04832 -0.0441 0.0039 1.0000
15.500 1.5431 0.05780 0.05239 -0.0449 0.0036 1.0000
15.750 1.5368 0.06205 0.05677 -0.0459 0.0035 1.0000
16.000 1.5282 0.06686 0.06173 -0.0473 0.0033 1.0000
16.250 1.5190 0.07195 0.06696 -0.0490 0.0031 1.0000
16.500 1.5084 0.07743 0.07258 -0.0511 0.0030 1.0000
16.750 1.4956 0.08353 0.07882 -0.0536 0.0029 1.0000
17.000 1.4827 0.08984 0.08528 -0.0563 0.0028 1.0000
17.250 1.4698 0.09630 0.09189 -0.0593 0.0028 1.0000
17.500 1.4564 0.10302 0.09876 -0.0625 0.0027 1.0000
17.750 1.4426 0.10999 0.10588 -0.0659 0.0027 1.0000
18.000 1.4277 0.11727 0.11331 -0.0696 0.0027 1.0000
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Polar data table (+)
Polar graphs
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