SPICA 11.73% smoothed (spicasm-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: SPICA 11.73% smoothed (spicasm-il) Reynolds number: 200,000 Max Cl/Cd: 77.63 at α=6° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-spicasm-il-200000-n5.txt Download as CSV file: xf-spicasm-il-200000-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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.750 -0.2859 0.11660 0.11289 -0.0377 1.0000 0.0333
-10.500 -0.2881 0.11355 0.10988 -0.0396 1.0000 0.0335
-10.250 -0.2899 0.11035 0.10672 -0.0414 1.0000 0.0336
-10.000 -0.2842 0.10703 0.10344 -0.0410 1.0000 0.0337
-9.750 -0.2753 0.10419 0.10063 -0.0400 1.0000 0.0340
-9.500 -0.2691 0.10164 0.09811 -0.0394 1.0000 0.0344
-9.250 -0.2658 0.09915 0.09567 -0.0392 1.0000 0.0348
-9.000 -0.2577 0.09618 0.09274 -0.0404 0.9934 0.0356
-8.750 -0.2422 0.09242 0.08898 -0.0447 0.9795 0.0374
-8.500 -0.2322 0.08721 0.08376 -0.0547 0.9537 0.0393
-8.250 -0.2147 0.08078 0.07729 -0.0678 0.9233 0.0396
-8.000 -0.1912 0.07483 0.07124 -0.0768 0.8976 0.0398
-7.750 -0.1622 0.07163 0.06797 -0.0781 0.8777 0.0404
-7.250 -0.1305 0.06489 0.06097 -0.0854 0.8283 0.0415
-7.000 -0.1223 0.06170 0.05766 -0.0878 0.8085 0.0421
-6.750 -0.1145 0.05853 0.05436 -0.0897 0.7917 0.0427
-6.500 -0.1058 0.05522 0.05088 -0.0918 0.7768 0.0446
-6.000 -0.0951 0.04231 0.03718 -0.0955 0.7538 0.0333
-5.750 -0.0800 0.04008 0.03482 -0.0952 0.7428 0.0329
-5.500 -0.0642 0.03753 0.03205 -0.0948 0.7334 0.0325
-5.250 -0.0477 0.03475 0.02900 -0.0943 0.7241 0.0321
-5.000 -0.0300 0.03206 0.02599 -0.0936 0.7156 0.0318
-4.750 -0.0112 0.02948 0.02305 -0.0927 0.7075 0.0319
-4.500 0.0087 0.02698 0.02012 -0.0917 0.7001 0.0326
-4.250 0.0300 0.02497 0.01777 -0.0907 0.6924 0.0325
-4.000 0.0524 0.02324 0.01570 -0.0899 0.6858 0.0324
-3.750 0.0757 0.02168 0.01382 -0.0890 0.6788 0.0324
-3.500 0.1000 0.02033 0.01214 -0.0883 0.6726 0.0325
-3.250 0.1250 0.01918 0.01072 -0.0876 0.6663 0.0328
-3.000 0.1505 0.01822 0.00951 -0.0870 0.6601 0.0331
-2.750 0.1765 0.01745 0.00849 -0.0864 0.6549 0.0335
-2.500 0.2022 0.01681 0.00782 -0.0860 0.6489 0.0343
-2.250 0.2282 0.01642 0.00737 -0.0856 0.6432 0.0354
-2.000 0.2544 0.01601 0.00687 -0.0852 0.6383 0.0365
-1.750 0.2804 0.01551 0.00633 -0.0847 0.6327 0.0372
-1.500 0.3062 0.01508 0.00584 -0.0842 0.6274 0.0379
-1.000 0.3574 0.01440 0.00507 -0.0831 0.6172 0.0399
-0.750 0.3828 0.01414 0.00482 -0.0825 0.6119 0.0412
-0.500 0.4087 0.01397 0.00461 -0.0821 0.6072 0.0434
-0.250 0.4346 0.01383 0.00446 -0.0816 0.6017 0.0471
0.000 0.4604 0.01369 0.00433 -0.0811 0.5960 0.0515
0.250 0.4863 0.01355 0.00414 -0.0807 0.5912 0.0586
0.500 0.5119 0.01340 0.00402 -0.0802 0.5855 0.0721
1.000 0.6235 0.01105 0.00408 -0.0920 0.5728 1.0000
1.250 0.6469 0.01113 0.00409 -0.0911 0.5661 1.0000
1.500 0.6705 0.01124 0.00408 -0.0902 0.5599 1.0000
1.750 0.6940 0.01134 0.00411 -0.0893 0.5529 1.0000
2.000 0.7175 0.01144 0.00414 -0.0883 0.5458 1.0000
2.250 0.7412 0.01156 0.00417 -0.0875 0.5393 1.0000
2.500 0.7649 0.01167 0.00425 -0.0866 0.5322 1.0000
3.000 0.8123 0.01191 0.00441 -0.0849 0.5186 1.0000
3.250 0.8358 0.01205 0.00448 -0.0840 0.5117 1.0000
3.500 0.8594 0.01217 0.00460 -0.0831 0.5042 1.0000
3.750 0.8828 0.01231 0.00469 -0.0822 0.4967 1.0000
4.000 0.9063 0.01245 0.00483 -0.0813 0.4888 1.0000
4.250 0.9295 0.01261 0.00495 -0.0804 0.4806 1.0000
4.500 0.9528 0.01276 0.00510 -0.0795 0.4716 1.0000
4.750 0.9756 0.01294 0.00523 -0.0786 0.4629 1.0000
5.000 0.9985 0.01311 0.00542 -0.0776 0.4531 1.0000
5.250 1.0211 0.01331 0.00560 -0.0767 0.4433 1.0000
5.750 1.0651 0.01375 0.00600 -0.0746 0.4220 1.0000
6.000 1.0868 0.01400 0.00624 -0.0735 0.4113 1.0000
6.250 1.1077 0.01428 0.00648 -0.0723 0.4002 1.0000
6.500 1.1285 0.01457 0.00677 -0.0711 0.3884 1.0000
6.750 1.1491 0.01488 0.00707 -0.0698 0.3765 1.0000
7.000 1.1690 0.01521 0.00739 -0.0685 0.3648 1.0000
7.250 1.1881 0.01557 0.00773 -0.0671 0.3529 1.0000
7.500 1.2066 0.01596 0.00810 -0.0656 0.3412 1.0000
7.750 1.2251 0.01635 0.00849 -0.0641 0.3296 1.0000
8.000 1.2427 0.01677 0.00891 -0.0625 0.3188 1.0000
8.250 1.2589 0.01723 0.00936 -0.0607 0.3089 1.0000
8.500 1.2756 0.01768 0.00984 -0.0590 0.2988 1.0000
8.750 1.2909 0.01816 0.01033 -0.0571 0.2900 1.0000
9.000 1.3038 0.01867 0.01084 -0.0547 0.2814 1.0000
9.250 1.3173 0.01916 0.01138 -0.0525 0.2736 1.0000
9.500 1.3283 0.01976 0.01199 -0.0500 0.2654 1.0000
9.750 1.3406 0.02034 0.01261 -0.0479 0.2563 1.0000
10.000 1.3498 0.02106 0.01332 -0.0454 0.2467 1.0000
10.250 1.3588 0.02182 0.01409 -0.0430 0.2366 1.0000
10.500 1.3683 0.02261 0.01492 -0.0409 0.2266 1.0000
10.750 1.3757 0.02355 0.01587 -0.0386 0.2185 1.0000
11.000 1.3845 0.02449 0.01686 -0.0367 0.2087 1.0000
11.250 1.3923 0.02554 0.01795 -0.0349 0.2002 1.0000
11.500 1.3982 0.02676 0.01919 -0.0331 0.1914 1.0000
11.750 1.4063 0.02794 0.02044 -0.0316 0.1822 1.0000
12.000 1.4112 0.02938 0.02192 -0.0301 0.1733 1.0000
12.250 1.4148 0.03101 0.02357 -0.0286 0.1627 1.0000
12.500 1.4180 0.03276 0.02534 -0.0274 0.1508 1.0000
12.750 1.4189 0.03479 0.02737 -0.0262 0.1379 1.0000
13.000 1.4189 0.03699 0.02957 -0.0252 0.1258 1.0000
13.250 1.4174 0.03940 0.03199 -0.0243 0.1135 1.0000
13.500 1.4136 0.04213 0.03470 -0.0235 0.1004 1.0000
13.750 1.4080 0.04513 0.03768 -0.0229 0.0872 1.0000
14.000 1.3991 0.04858 0.04108 -0.0224 0.0727 1.0000
14.250 1.3897 0.05222 0.04470 -0.0221 0.0595 1.0000
14.500 1.3786 0.05620 0.04865 -0.0221 0.0466 1.0000
14.750 1.3671 0.06041 0.05284 -0.0223 0.0368 1.0000
15.000 1.3571 0.06460 0.05706 -0.0226 0.0313 1.0000
15.250 1.3482 0.06881 0.06133 -0.0232 0.0280 1.0000
15.500 1.3406 0.07299 0.06561 -0.0239 0.0259 1.0000
15.750 1.3338 0.07719 0.06992 -0.0248 0.0244 1.0000
16.000 1.3242 0.08190 0.07474 -0.0259 0.0231 1.0000
16.500 1.3077 0.09136 0.08446 -0.0286 0.0216 1.0000
16.750 1.3002 0.09611 0.08935 -0.0301 0.0210 1.0000
17.000 1.2913 0.10120 0.09457 -0.0318 0.0204 1.0000
17.250 1.2821 0.10644 0.09993 -0.0337 0.0198 1.0000
17.500 1.2729 0.11176 0.10538 -0.0358 0.0194 1.0000
17.750 1.2627 0.11732 0.11106 -0.0380 0.0190 1.0000
18.000 1.2520 0.12307 0.11690 -0.0405 0.0185 1.0000
|
Polar data table (+)
Polar graphs
<< Back to SPICA 11.73% smoothed (spicasm-il)