SPICA 11.73% smoothed (spicasm-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
|---|---|
|
Airfoil: SPICA 11.73% smoothed (spicasm-il) Reynolds number: 200,000 Max Cl/Cd: 77.88 at α=7° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-spicasm-il-200000.txt Download as CSV file: xf-spicasm-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: SPICA 11.73% smoothed
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.750 -0.2057 0.10059 0.09743 -0.0410 1.0000 0.0463
-9.500 -0.2196 0.09875 0.09568 -0.0416 1.0000 0.0465
-9.250 -0.2293 0.09631 0.09332 -0.0437 0.9975 0.0467
-9.000 -0.2030 0.09005 0.08706 -0.0441 0.9939 0.0474
-8.750 -0.1771 0.08570 0.08269 -0.0458 0.9878 0.0487
-8.500 -0.1592 0.08126 0.07825 -0.0497 0.9797 0.0502
-8.250 -0.1435 0.07658 0.07356 -0.0543 0.9709 0.0519
-8.000 -0.2632 0.08763 0.08452 -0.0428 0.9923 0.0485
-7.750 -0.2372 0.08344 0.08033 -0.0485 0.9834 0.0499
-7.500 -0.2150 0.07899 0.07587 -0.0554 0.9684 0.0516
-7.250 -0.1900 0.07317 0.07000 -0.0687 0.9482 0.0544
-7.000 -0.1611 0.06458 0.06105 -0.0890 0.9274 0.0561
-6.750 -0.1356 0.06069 0.05723 -0.0896 0.9144 0.0570
-6.500 -0.1085 0.05752 0.05399 -0.0922 0.8979 0.0582
-6.250 -0.0863 0.05441 0.05074 -0.0950 0.8787 0.0601
-6.000 -0.0699 0.05143 0.04757 -0.0971 0.8588 0.0628
-5.750 -0.0600 0.04778 0.04325 -0.1001 0.8401 0.0672
-5.500 -0.0434 0.04468 0.04019 -0.0997 0.8268 0.0683
-5.250 -0.0262 0.04261 0.03804 -0.0993 0.8146 0.0698
-5.000 -0.0092 0.04068 0.03598 -0.0988 0.8023 0.0720
-4.750 0.0128 0.04121 0.03575 -0.0981 0.7906 0.0791
-4.500 0.0270 0.03609 0.03065 -0.0983 0.7823 0.0811
-4.250 0.0460 0.03415 0.02872 -0.0977 0.7722 0.0831
-4.000 0.0671 0.03265 0.02707 -0.0972 0.7642 0.0871
-3.750 0.0875 0.03098 0.02498 -0.0964 0.7556 0.0958
-3.500 0.1093 0.02931 0.02328 -0.0960 0.7486 0.0991
-3.250 0.1309 0.02817 0.02185 -0.0952 0.7405 0.1116
-3.000 0.1543 0.02688 0.02051 -0.0948 0.7344 0.1184
-2.750 0.1757 0.02560 0.01912 -0.0942 0.7267 0.1312
-2.500 0.1988 0.02451 0.01788 -0.0936 0.7204 0.1471
-2.250 0.2370 0.02074 0.01280 -0.0908 0.7153 0.0651
-2.000 0.2626 0.01929 0.01119 -0.0901 0.7086 0.0626
-1.750 0.2900 0.01829 0.00994 -0.0896 0.7031 0.0613
-1.500 0.3160 0.01771 0.00926 -0.0890 0.6967 0.0630
-1.250 0.3428 0.01711 0.00854 -0.0884 0.6905 0.0640
-1.000 0.3703 0.01654 0.00783 -0.0880 0.6854 0.0646
-0.750 0.3956 0.01609 0.00738 -0.0873 0.6786 0.0658
-0.500 0.4214 0.01546 0.00672 -0.0866 0.6728 0.0680
-0.250 0.4465 0.01506 0.00637 -0.0860 0.6673 0.0726
0.000 0.4713 0.01484 0.00616 -0.0853 0.6606 0.0795
0.250 0.4967 0.01445 0.00575 -0.0846 0.6552 0.0926
0.500 0.5168 0.01357 0.00552 -0.0833 0.6490 0.2646
0.750 0.6137 0.01179 0.00539 -0.0971 0.6411 1.0000
1.000 0.6375 0.01193 0.00540 -0.0962 0.6351 1.0000
1.250 0.6602 0.01204 0.00544 -0.0951 0.6277 1.0000
1.500 0.6856 0.01218 0.00540 -0.0945 0.6218 1.0000
1.750 0.7073 0.01229 0.00551 -0.0932 0.6138 1.0000
2.000 0.7322 0.01241 0.00549 -0.0925 0.6074 1.0000
2.250 0.7549 0.01255 0.00562 -0.0914 0.6000 1.0000
2.500 0.7792 0.01267 0.00566 -0.0906 0.5932 1.0000
2.750 0.8033 0.01283 0.00576 -0.0898 0.5867 1.0000
3.000 0.8265 0.01296 0.00587 -0.0888 0.5792 1.0000
3.250 0.8522 0.01311 0.00591 -0.0883 0.5732 1.0000
3.500 0.8740 0.01324 0.00608 -0.0871 0.5649 1.0000
3.750 0.8995 0.01337 0.00612 -0.0865 0.5586 1.0000
4.000 0.9215 0.01352 0.00632 -0.0853 0.5502 1.0000
4.250 0.9465 0.01363 0.00635 -0.0846 0.5431 1.0000
4.500 0.9686 0.01377 0.00654 -0.0835 0.5345 1.0000
4.750 0.9934 0.01388 0.00658 -0.0828 0.5271 1.0000
5.000 1.0152 0.01402 0.00677 -0.0816 0.5176 1.0000
5.250 1.0396 0.01413 0.00682 -0.0809 0.5097 1.0000
5.500 1.0613 0.01426 0.00701 -0.0797 0.4995 1.0000
5.750 1.0839 0.01440 0.00715 -0.0786 0.4900 1.0000
6.000 1.1071 0.01452 0.00723 -0.0777 0.4802 1.0000
6.250 1.1280 0.01468 0.00744 -0.0764 0.4686 1.0000
6.500 1.1496 0.01486 0.00764 -0.0752 0.4573 1.0000
6.750 1.1710 0.01507 0.00782 -0.0740 0.4457 1.0000
7.000 1.1923 0.01531 0.00800 -0.0728 0.4338 1.0000
7.250 1.2120 0.01558 0.00830 -0.0714 0.4206 1.0000
7.500 1.2315 0.01589 0.00862 -0.0699 0.4073 1.0000
7.750 1.2506 0.01625 0.00897 -0.0685 0.3942 1.0000
8.000 1.2694 0.01664 0.00935 -0.0669 0.3813 1.0000
8.250 1.2878 0.01707 0.00976 -0.0654 0.3692 1.0000
8.500 1.3061 0.01754 0.01017 -0.0639 0.3576 1.0000
8.750 1.3228 0.01798 0.01066 -0.0621 0.3456 1.0000
9.000 1.3397 0.01848 0.01118 -0.0604 0.3346 1.0000
9.250 1.3561 0.01902 0.01170 -0.0587 0.3243 1.0000
9.500 1.3705 0.01956 0.01220 -0.0567 0.3132 1.0000
9.750 1.3823 0.02006 0.01277 -0.0542 0.3017 1.0000
10.000 1.3922 0.02061 0.01333 -0.0515 0.2912 1.0000
10.250 1.4010 0.02123 0.01391 -0.0486 0.2810 1.0000
10.500 1.4096 0.02183 0.01459 -0.0458 0.2714 1.0000
10.750 1.4184 0.02252 0.01533 -0.0433 0.2622 1.0000
11.000 1.4264 0.02330 0.01609 -0.0408 0.2535 1.0000
11.250 1.4337 0.02408 0.01698 -0.0383 0.2443 1.0000
11.500 1.4397 0.02503 0.01794 -0.0359 0.2356 1.0000
11.750 1.4454 0.02601 0.01901 -0.0337 0.2265 1.0000
12.000 1.4507 0.02713 0.02020 -0.0317 0.2176 1.0000
12.250 1.4532 0.02849 0.02155 -0.0297 0.2088 1.0000
12.500 1.4575 0.02983 0.02303 -0.0280 0.1987 1.0000
12.750 1.4609 0.03137 0.02463 -0.0265 0.1897 1.0000
13.000 1.4607 0.03325 0.02653 -0.0251 0.1800 1.0000
13.250 1.4627 0.03512 0.02852 -0.0240 0.1685 1.0000
13.500 1.4616 0.03736 0.03081 -0.0230 0.1554 1.0000
13.750 1.4553 0.04021 0.03364 -0.0222 0.1395 1.0000
14.000 1.4464 0.04347 0.03687 -0.0215 0.1185 1.0000
14.250 1.4291 0.04774 0.04101 -0.0209 0.0944 1.0000
14.500 1.4093 0.05252 0.04565 -0.0207 0.0735 1.0000
14.750 1.3898 0.05750 0.05055 -0.0207 0.0597 1.0000
15.000 1.3723 0.06253 0.05556 -0.0211 0.0506 1.0000
15.250 1.3602 0.06710 0.06019 -0.0216 0.0459 1.0000
15.500 1.3473 0.07196 0.06509 -0.0224 0.0430 1.0000
15.750 1.3359 0.07677 0.07000 -0.0234 0.0404 1.0000
16.000 1.3263 0.08147 0.07482 -0.0245 0.0387 1.0000
16.250 1.3154 0.08649 0.07993 -0.0258 0.0372 1.0000
16.500 1.3045 0.09161 0.08512 -0.0272 0.0362 1.0000
|
Polar data table (+)
Polar graphs
<< Back to SPICA 11.73% smoothed (spicasm-il)