UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT (ua79sfm-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT (ua79sfm-il) Reynolds number: 200,000 Max Cl/Cd: 80.03 at α=8.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ua79sfm-il-200000-n5.txt Download as CSV file: xf-ua79sfm-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN
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
------ -------- --------- --------- -------- -------- --------
-12.250 -0.2105 0.09407 0.09079 -0.0715 -0.0011 4.4574
-12.000 -0.2018 0.09140 0.08813 -0.0717 -0.0012 4.4573
-11.750 -0.2058 0.08614 0.08289 -0.0747 -0.0014 4.4571
-11.500 -0.1968 0.08281 0.07955 -0.0757 -0.0015 4.4569
-11.250 -0.1933 0.07843 0.07518 -0.0781 -0.0015 4.4569
-11.000 -0.2195 0.06348 0.06024 -0.0856 -0.0016 4.4481
-10.750 -0.2421 0.06133 0.05813 -0.0845 -0.0016 4.4480
-10.500 -0.2604 0.05694 0.05369 -0.0875 -0.0014 4.4478
-10.250 -0.2806 0.05308 0.04974 -0.0904 -0.0012 4.4476
-10.000 -0.2992 0.04989 0.04644 -0.0926 -0.0010 4.4473
-9.750 -0.3243 0.04803 0.04450 -0.0921 -0.0007 4.4472
-9.500 -0.3482 0.04657 0.04296 -0.0900 -0.0002 4.4471
-9.250 -0.3577 0.04361 0.03982 -0.0898 -0.0001 4.4466
-9.000 -0.3722 0.03756 0.03321 -0.0893 0.0000 4.4435
-8.750 -0.3827 0.03630 0.03183 -0.0858 -0.0001 4.4430
-8.500 -0.3798 0.03443 0.02981 -0.0843 -0.0003 4.4426
-8.250 -0.3707 0.03217 0.02732 -0.0835 -0.0004 4.4421
-8.000 -0.3581 0.02989 0.02475 -0.0828 -0.0004 4.4413
-7.750 -0.3430 0.02774 0.02229 -0.0821 -0.0004 4.4405
-7.500 -0.3504 0.02697 0.02139 -0.0779 -0.0002 4.4400
-7.250 -0.3361 0.02532 0.01946 -0.0766 0.0001 4.4393
-7.000 -0.3171 0.02378 0.01763 -0.0756 0.0004 4.4385
-6.750 -0.2949 0.02252 0.01610 -0.0751 0.0007 4.4379
-6.500 -0.2893 0.02190 0.01539 -0.0724 0.0026 4.4376
-6.250 -0.2745 0.02118 0.01457 -0.0709 0.0039 4.4375
-6.000 -0.2555 0.02045 0.01375 -0.0701 0.0048 4.4374
-5.750 -0.2349 0.01975 0.01298 -0.0694 0.0056 4.4374
-5.500 -0.2136 0.01912 0.01228 -0.0690 0.0063 4.4376
-5.250 -0.2147 0.01889 0.01205 -0.0656 0.0108 4.4377
-5.000 -0.1985 0.01840 0.01152 -0.0645 0.0128 4.4379
-4.750 -0.1791 0.01793 0.01099 -0.0638 0.0142 4.4383
-4.500 -0.1580 0.01752 0.01050 -0.0633 0.0152 4.4389
-4.250 -0.1543 0.01735 0.01032 -0.0605 0.0202 4.4393
-4.000 -0.1393 0.01708 0.00998 -0.0592 0.0232 4.4400
-3.750 -0.1191 0.01680 0.00962 -0.0585 0.0249 4.4410
-3.500 -0.0973 0.01654 0.00929 -0.0580 0.0262 4.4425
-3.250 -0.0809 0.01637 0.00907 -0.0568 0.0287 4.4441
-3.000 -0.0755 0.01622 0.00891 -0.0542 0.0352 4.4460
-2.500 -0.0427 0.01433 0.00843 -0.0529 0.0388 3.6549
-2.250 -0.0020 0.01451 0.00964 -0.0530 0.0390 2.5538
-2.000 0.0259 0.01557 0.01074 -0.0514 0.0456 2.3430
-1.750 0.0567 0.01627 0.01135 -0.0509 0.0484 2.2384
-1.500 0.0963 0.01687 0.01186 -0.0514 0.0496 2.1967
-1.250 0.1198 0.01690 0.01179 -0.0511 0.0517 2.1656
-1.000 0.1342 0.01694 0.01180 -0.0495 0.0601 2.1503
-0.750 0.1584 0.01693 0.01171 -0.0490 0.0650 2.1355
-0.500 0.1867 0.01690 0.01162 -0.0490 0.0677 2.1153
-0.250 0.2146 0.01689 0.01154 -0.0491 0.0698 2.0917
0.000 0.2235 0.01708 0.01173 -0.0469 0.0836 2.0702
0.250 0.2490 0.01696 0.01156 -0.0467 0.0877 2.0594
0.500 0.2754 0.01681 0.01136 -0.0467 0.0907 2.0469
0.750 0.3026 0.01665 0.01117 -0.0467 0.0929 2.0328
1.000 0.3104 0.01685 0.01139 -0.0444 0.1109 2.0183
1.250 0.3356 0.01676 0.01128 -0.0443 0.1149 2.0054
1.500 0.3577 0.01650 0.01100 -0.0439 0.1183 2.0009
1.750 0.3578 0.01653 0.01104 -0.0412 0.1389 2.0009
2.000 0.3747 0.01621 0.01070 -0.0403 0.1448 2.0009
2.250 0.3943 0.01583 0.01029 -0.0398 0.1487 2.0009
2.500 0.3943 0.01580 0.01028 -0.0369 0.1725 2.0009
2.750 0.4135 0.01537 0.00983 -0.0362 0.1782 2.0009
3.000 0.4343 0.01491 0.00936 -0.0357 0.1819 2.0009
3.250 0.4325 0.01497 0.00946 -0.0327 0.2086 2.0009
3.500 0.4521 0.01455 0.00904 -0.0319 0.2132 2.0009
3.750 0.4522 0.01461 0.00911 -0.0291 0.2403 2.0009
4.000 0.4714 0.01417 0.00868 -0.0283 0.2461 2.0009
4.250 0.4744 0.01414 0.00867 -0.0258 0.2740 2.0009
4.500 0.4936 0.01364 0.00820 -0.0249 0.2817 2.0009
4.750 0.4989 0.01356 0.00815 -0.0226 0.3096 2.0009
5.000 0.5171 0.01311 0.00772 -0.0216 0.3197 2.0009
5.250 0.5382 0.01262 0.00726 -0.0209 0.3260 2.0009
5.500 0.5420 0.01265 0.00732 -0.0185 0.3583 2.0009
5.750 0.5628 0.01219 0.00690 -0.0178 0.3670 2.0009
6.000 0.5712 0.01212 0.00687 -0.0159 0.3943 2.0009
6.250 0.5888 0.01177 0.00656 -0.0148 0.4102 2.0009
6.500 0.6121 0.01128 0.00611 -0.0143 0.4194 2.0009
6.750 0.6169 0.01132 0.00621 -0.0120 0.4555 2.0009
7.250 0.6464 0.01085 0.00585 -0.0094 0.5060 2.0009
7.500 0.6711 0.01034 0.00539 -0.0089 0.5240 2.0009
7.750 0.6783 0.01030 0.00541 -0.0069 0.5677 2.0009
8.000 0.6992 0.00968 0.00476 -0.0058 0.6436 2.0009
8.250 0.7155 0.00894 0.00357 -0.0039 0.9692 2.0009
8.500 0.7086 0.00917 0.00347 -0.0003 1.2648 2.0009
8.750 0.6943 0.00968 0.00369 0.0037 1.5464 2.0009
9.000 0.6786 0.01032 0.00406 0.0075 1.8491 2.0009
9.250 0.6644 0.01100 0.00450 0.0109 2.1797 2.0009
9.500 0.6493 0.01181 0.00502 0.0142 2.5846 2.0009
9.750 0.6283 0.01294 0.00572 0.0176 3.2479 2.0009
10.000 0.6090 0.01411 0.00655 0.0206 4.1282 2.0009
10.250 0.6080 0.01455 0.00704 0.0226 4.2096 2.0009
10.500 0.6104 0.01485 0.00743 0.0243 4.2211 2.0009
10.750 0.6114 0.01522 0.00789 0.0260 4.2331 2.0009
11.000 0.6134 0.01554 0.00832 0.0276 4.2376 2.0009
11.250 0.6149 0.01589 0.00878 0.0292 4.2418 2.0009
11.500 0.6158 0.01628 0.00928 0.0308 4.2456 2.0009
11.750 0.6164 0.01669 0.00980 0.0323 4.2483 2.0009
12.000 0.6159 0.01718 0.01040 0.0338 4.2517 2.0009
12.250 0.6151 0.01768 0.01102 0.0352 4.2542 2.0009
12.500 0.6137 0.01824 0.01169 0.0365 4.2559 2.0009
12.750 0.6110 0.01888 0.01245 0.0378 4.2576 2.0009
13.000 0.6090 0.01950 0.01318 0.0390 4.2584 2.0009
13.250 0.6068 0.02015 0.01394 0.0401 4.2590 2.0009
13.500 0.6039 0.02087 0.01478 0.0411 4.2598 2.0009
13.750 0.6003 0.02165 0.01567 0.0420 4.2600 2.0009
14.000 0.5960 0.02249 0.01663 0.0428 4.2609 2.0009
14.250 0.5918 0.02334 0.01759 0.0436 4.2609 2.0009
14.500 0.5869 0.02428 0.01864 0.0442 4.2615 2.0009
14.750 0.5821 0.02525 0.01970 0.0448 4.2619 2.0009
15.000 0.5777 0.02622 0.02078 0.0452 4.2618 2.0009
15.250 0.5734 0.02719 0.02184 0.0456 4.2621 2.0009
15.500 0.5697 0.02813 0.02286 0.0460 4.2621 2.0009
15.750 0.5669 0.02903 0.02383 0.0464 4.2625 2.0009
16.000 0.5650 0.02987 0.02474 0.0468 4.2626 2.0009
16.250 0.5645 0.03060 0.02553 0.0472 4.2628 2.0009
16.500 0.5652 0.03123 0.02622 0.0477 4.2626 2.0009
16.750 0.5671 0.03176 0.02680 0.0483 4.2626 2.0009
17.000 0.5701 0.03224 0.02734 0.0489 4.2626 2.0009
17.250 0.5741 0.03265 0.02780 0.0496 4.2625 2.0009
17.500 0.5779 0.03311 0.02833 0.0502 4.2621 2.0009
17.750 0.5820 0.03358 0.02888 0.0508 4.2617 2.0009
18.000 0.5848 0.03420 0.02958 0.0513 4.2613 2.0009
18.250 0.5870 0.03491 0.03038 0.0517 4.2610 2.0009
18.500 0.5888 0.03572 0.03129 0.0520 4.2605 2.0009
18.750 0.5886 0.03664 0.03231 0.0522 4.2600 2.0009
19.000 0.5872 0.03772 0.03349 0.0522 4.2596 2.0009
19.250 0.5855 0.03886 0.03474 0.0522 4.2590 2.0009
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