SM701 (sm701-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: SM701 (sm701-il) Reynolds number: 100,000 Max Cl/Cd: 46.8 at α=5.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-sm701-il-100000-n5.txt Download as CSV file: xf-sm701-il-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: SM701
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
------ -------- --------- --------- -------- -------- --------
-10.750 -0.4224 0.09787 0.09300 -0.0523 1.0000 0.0335
-10.500 -0.4678 0.07831 0.07332 -0.0682 0.9946 0.0319
-10.250 -0.5340 0.06322 0.05766 -0.0825 0.9834 0.0308
-10.000 -0.5592 0.05778 0.05183 -0.0863 0.9720 0.0306
-9.750 -0.5669 0.05406 0.04780 -0.0874 0.9611 0.0305
-9.500 -0.5638 0.05079 0.04426 -0.0882 0.9523 0.0307
-9.250 -0.5540 0.04773 0.04091 -0.0893 0.9453 0.0310
-9.000 -0.5436 0.04577 0.03880 -0.0889 0.9376 0.0315
-8.750 -0.5271 0.04379 0.03663 -0.0895 0.9317 0.0324
-8.500 -0.5133 0.04152 0.03406 -0.0894 0.9252 0.0332
-8.250 -0.4977 0.03934 0.03153 -0.0891 0.9185 0.0340
-8.000 -0.4730 0.03693 0.02873 -0.0902 0.9151 0.0346
-7.750 -0.4588 0.03528 0.02680 -0.0886 0.9077 0.0350
-7.500 -0.4342 0.03354 0.02477 -0.0888 0.9035 0.0356
-7.250 -0.4047 0.03195 0.02298 -0.0896 0.9008 0.0363
-7.000 -0.3848 0.03087 0.02187 -0.0888 0.8949 0.0371
-6.750 -0.3612 0.02991 0.02087 -0.0886 0.8899 0.0384
-6.500 -0.3319 0.02894 0.01979 -0.0893 0.8868 0.0405
-6.250 -0.3005 0.02791 0.01862 -0.0902 0.8847 0.0424
-6.000 -0.2861 0.02723 0.01794 -0.0882 0.8775 0.0434
-5.750 -0.2605 0.02638 0.01711 -0.0883 0.8734 0.0451
-5.500 -0.2307 0.02552 0.01622 -0.0890 0.8707 0.0474
-5.250 -0.1986 0.02473 0.01531 -0.0901 0.8688 0.0508
-5.000 -0.1872 0.02435 0.01499 -0.0878 0.8607 0.0544
-4.750 -0.1590 0.02369 0.01429 -0.0883 0.8572 0.0611
-4.500 -0.1274 0.02286 0.01350 -0.0895 0.8547 0.0732
-4.250 -0.0939 0.02193 0.01274 -0.0913 0.8528 0.1057
-4.000 -0.0817 0.02148 0.01253 -0.0894 0.8448 0.1524
-3.750 -0.0526 0.02009 0.01184 -0.0913 0.8414 0.2921
-3.500 -0.0236 0.01957 0.01238 -0.0916 0.8388 0.5308
-3.250 0.0123 0.01983 0.01257 -0.0925 0.8368 0.5858
-3.000 0.0257 0.02025 0.01295 -0.0896 0.8286 0.6044
-2.750 0.0551 0.02047 0.01307 -0.0893 0.8248 0.6228
-2.500 0.0869 0.02073 0.01328 -0.0891 0.8221 0.6426
-2.000 0.1281 0.02145 0.01395 -0.0850 0.8105 0.6754
-1.750 0.1618 0.02135 0.01374 -0.0858 0.8071 0.6821
-1.500 0.2031 0.02103 0.01323 -0.0885 0.8045 0.6885
-1.250 0.2195 0.02117 0.01335 -0.0865 0.7963 0.6919
-1.000 0.2517 0.02100 0.01310 -0.0871 0.7916 0.6957
-0.750 0.2921 0.02068 0.01266 -0.0893 0.7883 0.7000
-0.500 0.3145 0.02069 0.01259 -0.0888 0.7800 0.7049
-0.250 0.3479 0.02047 0.01231 -0.0896 0.7745 0.7083
0.000 0.3891 0.02011 0.01187 -0.0917 0.7707 0.7115
0.250 0.4055 0.02023 0.01198 -0.0898 0.7606 0.7155
0.500 0.4452 0.01991 0.01157 -0.0919 0.7557 0.7200
0.750 0.4674 0.01994 0.01158 -0.0910 0.7467 0.7242
1.000 0.5006 0.01972 0.01133 -0.0917 0.7402 0.7275
1.250 0.5255 0.01969 0.01129 -0.0912 0.7316 0.7314
1.500 0.5581 0.01950 0.01106 -0.0919 0.7238 0.7360
1.750 0.5830 0.01947 0.01102 -0.0915 0.7143 0.7407
2.000 0.6144 0.01928 0.01081 -0.0918 0.7061 0.7445
2.250 0.6345 0.01931 0.01087 -0.0904 0.6949 0.7491
2.500 0.6656 0.01916 0.01068 -0.0909 0.6853 0.7539
2.750 0.6909 0.01908 0.01061 -0.0903 0.6737 0.7585
3.000 0.7106 0.01910 0.01068 -0.0887 0.6607 0.7632
3.250 0.7341 0.01908 0.01066 -0.0879 0.6471 0.7690
3.500 0.7578 0.01905 0.01064 -0.0871 0.6324 0.7746
3.750 0.7787 0.01904 0.01065 -0.0856 0.6165 0.7796
4.000 0.8004 0.01905 0.01065 -0.0844 0.5988 0.7857
4.250 0.8229 0.01904 0.01061 -0.0834 0.5795 0.7917
4.500 0.8455 0.01904 0.01056 -0.0822 0.5592 0.7979
4.750 0.8674 0.01915 0.01059 -0.0811 0.5361 0.8055
5.000 0.8877 0.01928 0.01063 -0.0796 0.5139 0.8120
5.250 0.9084 0.01951 0.01075 -0.0783 0.4916 0.8200
5.500 0.9263 0.01981 0.01098 -0.0766 0.4700 0.8275
5.750 0.9445 0.02018 0.01125 -0.0751 0.4497 0.8366
6.000 0.9607 0.02055 0.01156 -0.0731 0.4314 0.8459
6.250 0.9770 0.02097 0.01193 -0.0713 0.4139 0.8570
6.500 0.9922 0.02138 0.01231 -0.0693 0.3979 0.8694
6.750 1.0061 0.02178 0.01270 -0.0670 0.3832 0.8835
7.000 1.0197 0.02217 0.01309 -0.0648 0.3695 0.9013
7.250 1.0331 0.02253 0.01348 -0.0625 0.3570 0.9281
7.500 1.0517 0.02291 0.01384 -0.0616 0.3443 1.0000
7.750 1.0736 0.02359 0.01444 -0.0615 0.3319 1.0000
8.000 1.0948 0.02425 0.01510 -0.0613 0.3200 1.0000
8.250 1.1151 0.02496 0.01577 -0.0609 0.3093 1.0000
8.500 1.1343 0.02569 0.01645 -0.0603 0.2994 1.0000
8.750 1.1537 0.02641 0.01720 -0.0598 0.2896 1.0000
9.250 1.1899 0.02796 0.01876 -0.0584 0.2722 1.0000
9.500 1.2075 0.02879 0.01954 -0.0576 0.2648 1.0000
9.750 1.2246 0.02961 0.02044 -0.0568 0.2567 1.0000
10.000 1.2411 0.03049 0.02128 -0.0559 0.2500 1.0000
10.250 1.2574 0.03138 0.02228 -0.0551 0.2425 1.0000
10.500 1.2730 0.03231 0.02320 -0.0542 0.2363 1.0000
10.750 1.2886 0.03328 0.02425 -0.0534 0.2299 1.0000
11.000 1.3030 0.03429 0.02533 -0.0524 0.2236 1.0000
11.250 1.3180 0.03532 0.02635 -0.0516 0.2182 1.0000
11.500 1.3316 0.03642 0.02760 -0.0506 0.2122 1.0000
11.750 1.3445 0.03756 0.02878 -0.0497 0.2068 1.0000
12.000 1.3579 0.03872 0.03000 -0.0488 0.2018 1.0000
12.250 1.3694 0.04001 0.03144 -0.0479 0.1964 1.0000
12.500 1.3807 0.04129 0.03277 -0.0469 0.1916 1.0000
12.750 1.3929 0.04259 0.03412 -0.0461 0.1872 1.0000
13.000 1.4017 0.04413 0.03584 -0.0452 0.1821 1.0000
13.250 1.4107 0.04563 0.03743 -0.0443 0.1776 1.0000
13.500 1.4218 0.04704 0.03884 -0.0436 0.1736 1.0000
13.750 1.4272 0.04894 0.04098 -0.0427 0.1691 1.0000
14.000 1.4333 0.05078 0.04295 -0.0419 0.1647 1.0000
14.250 1.4408 0.05249 0.04469 -0.0412 0.1609 1.0000
14.500 1.4455 0.05457 0.04692 -0.0406 0.1570 1.0000
14.750 1.4475 0.05694 0.04950 -0.0400 0.1529 1.0000
15.000 1.4505 0.05919 0.05187 -0.0396 0.1490 1.0000
15.250 1.4572 0.06111 0.05379 -0.0392 0.1456 1.0000
15.500 1.4538 0.06427 0.05721 -0.0390 0.1419 1.0000
15.750 1.4514 0.06737 0.06051 -0.0389 0.1381 1.0000
16.000 1.4516 0.07021 0.06345 -0.0390 0.1347 1.0000
16.250 1.4561 0.07253 0.06577 -0.0391 0.1315 1.0000
16.500 1.4454 0.07703 0.07058 -0.0398 0.1282 1.0000
16.750 1.4372 0.08132 0.07508 -0.0407 0.1248 1.0000
17.000 1.4328 0.08513 0.07901 -0.0416 0.1216 1.0000
17.250 1.4360 0.08785 0.08174 -0.0422 0.1186 1.0000
17.500 1.4189 0.09393 0.08810 -0.0443 0.1158 1.0000
17.750 1.4010 0.10038 0.09480 -0.0469 0.1130 1.0000
18.000 1.3881 0.10616 0.10074 -0.0495 0.1100 1.0000
18.250 1.3872 0.10986 0.10449 -0.0511 0.1071 1.0000
18.500 1.3758 0.11558 0.11033 -0.0539 0.1045 1.0000
18.750 1.3316 0.12784 0.12292 -0.0607 0.1022 1.0000
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