SPICA 11.73% smoothed (spicasm-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: SPICA 11.73% smoothed (spicasm-il) Reynolds number: 500,000 Max Cl/Cd: 104.23 at α=5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-spicasm-il-500000-n5.txt Download as CSV file: xf-spicasm-il-500000-n5.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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-11.000 -0.2953 0.11432 0.11192 -0.0356 1.0000 0.0194
-10.750 -0.2943 0.11080 0.10843 -0.0369 1.0000 0.0195
-10.250 -0.2898 0.10250 0.10016 -0.0414 0.9905 0.0196
-10.000 -0.2787 0.09807 0.09572 -0.0452 0.9742 0.0196
-9.750 -0.2547 0.09299 0.09060 -0.0521 0.9505 0.0195
-9.500 -0.2131 0.08759 0.08512 -0.0623 0.9301 0.0194
-9.250 -0.1647 0.08115 0.07851 -0.0761 0.8952 0.0192
-9.000 -0.1578 0.07416 0.07125 -0.0846 0.8419 0.0196
-8.750 -0.1334 0.07583 0.07277 -0.0824 0.8095 0.0209
-8.250 -0.1448 0.06832 0.06510 -0.0850 0.7669 0.0203
-8.000 -0.1384 0.06702 0.06375 -0.0848 0.7497 0.0211
-7.750 -0.1461 0.06419 0.06087 -0.0855 0.7343 0.0213
-7.500 -0.1484 0.06057 0.05718 -0.0879 0.7213 0.0214
-7.250 -0.1529 0.05514 0.05166 -0.0913 0.7103 0.0207
-7.000 -0.1544 0.04929 0.04564 -0.0940 0.7012 0.0204
-6.750 -0.1510 0.04386 0.04000 -0.0954 0.6923 0.0203
-6.500 -0.1409 0.04015 0.03610 -0.0956 0.6839 0.0204
-6.250 -0.1276 0.03709 0.03285 -0.0955 0.6752 0.0206
-6.000 -0.1124 0.03432 0.02987 -0.0951 0.6676 0.0210
-5.750 -0.0989 0.03051 0.02576 -0.0943 0.6602 0.0212
-5.500 -0.0854 0.02642 0.02125 -0.0930 0.6537 0.0213
-5.250 -0.0697 0.02272 0.01713 -0.0915 0.6472 0.0216
-5.000 -0.0525 0.01945 0.01335 -0.0900 0.6412 0.0218
-4.750 -0.0310 0.01757 0.01111 -0.0889 0.6355 0.0221
-4.500 -0.0071 0.01642 0.00970 -0.0882 0.6295 0.0226
-4.250 0.0173 0.01549 0.00853 -0.0875 0.6239 0.0229
-4.000 0.0427 0.01471 0.00757 -0.0870 0.6189 0.0231
-3.750 0.0684 0.01408 0.00679 -0.0865 0.6136 0.0233
-3.500 0.0941 0.01359 0.00616 -0.0860 0.6086 0.0235
-3.250 0.1201 0.01311 0.00559 -0.0856 0.6041 0.0236
-3.000 0.1457 0.01252 0.00494 -0.0851 0.5995 0.0240
-2.750 0.1716 0.01215 0.00452 -0.0846 0.5949 0.0244
-2.250 0.2239 0.01159 0.00390 -0.0838 0.5861 0.0251
-2.000 0.2501 0.01135 0.00363 -0.0834 0.5816 0.0255
-1.750 0.2763 0.01114 0.00338 -0.0830 0.5771 0.0260
-1.500 0.3025 0.01097 0.00318 -0.0826 0.5729 0.0266
-1.250 0.3292 0.01081 0.00300 -0.0823 0.5684 0.0274
-1.000 0.3557 0.01067 0.00283 -0.0819 0.5635 0.0280
-0.750 0.3818 0.01053 0.00265 -0.0814 0.5589 0.0286
-0.500 0.4083 0.01037 0.00250 -0.0811 0.5545 0.0296
-0.250 0.4350 0.01027 0.00240 -0.0808 0.5494 0.0308
0.000 0.4616 0.01021 0.00231 -0.0804 0.5444 0.0321
0.250 0.4883 0.01015 0.00223 -0.0801 0.5394 0.0340
0.500 0.5150 0.01008 0.00219 -0.0798 0.5332 0.0383
0.750 0.5410 0.01005 0.00218 -0.0794 0.5265 0.0506
1.000 0.5678 0.01000 0.00216 -0.0791 0.5196 0.0649
1.250 0.5940 0.00995 0.00214 -0.0787 0.5130 0.0828
1.500 0.6100 0.00874 0.00224 -0.0770 0.5077 0.5683
2.000 0.7333 0.00804 0.00247 -0.0914 0.4914 1.0000
2.250 0.7571 0.00812 0.00250 -0.0906 0.4837 1.0000
2.500 0.7807 0.00822 0.00255 -0.0897 0.4768 1.0000
2.750 0.8046 0.00831 0.00260 -0.0888 0.4688 1.0000
3.000 0.8281 0.00843 0.00266 -0.0879 0.4606 1.0000
3.250 0.8516 0.00855 0.00274 -0.0870 0.4513 1.0000
3.500 0.8752 0.00868 0.00282 -0.0862 0.4427 1.0000
3.750 0.8983 0.00883 0.00292 -0.0852 0.4336 1.0000
4.000 0.9218 0.00898 0.00303 -0.0844 0.4238 1.0000
4.250 0.9447 0.00915 0.00315 -0.0834 0.4138 1.0000
4.500 0.9675 0.00934 0.00329 -0.0824 0.4034 1.0000
4.750 0.9907 0.00951 0.00343 -0.0815 0.3936 1.0000
5.000 1.0131 0.00972 0.00360 -0.0805 0.3824 1.0000
5.250 1.0351 0.00995 0.00377 -0.0794 0.3709 1.0000
5.500 1.0577 0.01017 0.00395 -0.0785 0.3592 1.0000
5.750 1.0796 0.01041 0.00415 -0.0774 0.3469 1.0000
6.000 1.1012 0.01067 0.00437 -0.0763 0.3348 1.0000
6.250 1.1225 0.01095 0.00460 -0.0752 0.3231 1.0000
6.500 1.1436 0.01124 0.00486 -0.0740 0.3112 1.0000
6.750 1.1647 0.01153 0.00511 -0.0729 0.2997 1.0000
7.000 1.1856 0.01182 0.00538 -0.0717 0.2900 1.0000
7.500 1.2263 0.01245 0.00597 -0.0692 0.2703 1.0000
7.750 1.2459 0.01278 0.00628 -0.0679 0.2616 1.0000
8.000 1.2649 0.01314 0.00662 -0.0665 0.2516 1.0000
8.250 1.2834 0.01350 0.00697 -0.0650 0.2412 1.0000
8.500 1.3001 0.01393 0.00735 -0.0632 0.2296 1.0000
8.750 1.3150 0.01438 0.00776 -0.0611 0.2184 1.0000
9.000 1.3302 0.01476 0.00813 -0.0590 0.2097 1.0000
9.250 1.3441 0.01518 0.00855 -0.0568 0.2021 1.0000
9.500 1.3571 0.01566 0.00902 -0.0545 0.1920 1.0000
9.750 1.3714 0.01612 0.00948 -0.0524 0.1840 1.0000
10.000 1.3836 0.01668 0.01003 -0.0502 0.1755 1.0000
10.250 1.3970 0.01721 0.01057 -0.0482 0.1667 1.0000
10.500 1.4073 0.01791 0.01125 -0.0459 0.1552 1.0000
10.750 1.4166 0.01871 0.01201 -0.0436 0.1440 1.0000
11.000 1.4230 0.01971 0.01296 -0.0412 0.1295 1.0000
11.250 1.4277 0.02088 0.01408 -0.0388 0.1148 1.0000
11.500 1.4298 0.02231 0.01544 -0.0364 0.0992 1.0000
11.750 1.4300 0.02400 0.01706 -0.0341 0.0833 1.0000
12.000 1.4300 0.02585 0.01885 -0.0322 0.0691 1.0000
12.250 1.4262 0.02812 0.02106 -0.0303 0.0536 1.0000
12.500 1.4196 0.03079 0.02364 -0.0286 0.0365 1.0000
12.750 1.4132 0.03359 0.02640 -0.0272 0.0249 1.0000
13.000 1.4128 0.03597 0.02882 -0.0263 0.0203 1.0000
13.250 1.4136 0.03829 0.03119 -0.0255 0.0177 1.0000
13.500 1.4159 0.04053 0.03350 -0.0249 0.0163 1.0000
13.750 1.4167 0.04297 0.03601 -0.0244 0.0152 1.0000
14.000 1.4178 0.04542 0.03854 -0.0240 0.0145 1.0000
14.250 1.4197 0.04786 0.04106 -0.0237 0.0139 1.0000
14.500 1.4204 0.05048 0.04378 -0.0235 0.0134 1.0000
14.750 1.4204 0.05324 0.04662 -0.0234 0.0130 1.0000
15.000 1.4187 0.05626 0.04972 -0.0234 0.0126 1.0000
15.250 1.4156 0.05953 0.05309 -0.0235 0.0121 1.0000
15.500 1.4109 0.06310 0.05675 -0.0238 0.0118 1.0000
15.750 1.4079 0.06649 0.06024 -0.0241 0.0116 1.0000
16.000 1.4052 0.06995 0.06381 -0.0246 0.0112 1.0000
16.250 1.4013 0.07365 0.06760 -0.0252 0.0111 1.0000
16.500 1.3965 0.07753 0.07159 -0.0259 0.0108 1.0000
16.750 1.3919 0.08146 0.07561 -0.0268 0.0106 1.0000
17.000 1.3854 0.08574 0.08000 -0.0278 0.0104 1.0000
17.250 1.3786 0.09017 0.08454 -0.0290 0.0102 1.0000
17.500 1.3717 0.09466 0.08913 -0.0303 0.0100 1.0000
17.750 1.3635 0.09942 0.09399 -0.0317 0.0099 1.0000
18.000 1.3540 0.10449 0.09917 -0.0334 0.0097 1.0000
18.250 1.3442 0.10971 0.10449 -0.0353 0.0095 1.0000
18.500 1.3342 0.11504 0.10992 -0.0373 0.0094 1.0000
18.750 1.3235 0.12054 0.11552 -0.0395 0.0093 1.0000
|
Polar data table (+)
Polar graphs
<< Back to SPICA 11.73% smoothed (spicasm-il)