AS5046 (16%) (as5046-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: AS5046 (16%) (as5046-il) Reynolds number: 1,000,000 Max Cl/Cd: 83.55 at α=7.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-as5046-il-1000000-n5.txt Download as CSV file: xf-as5046-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: AS5046 (16%)
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.250 -0.8853 0.10705 0.10457 -0.0233 1.0000 0.0045
-17.000 -0.9164 0.09642 0.09375 -0.0291 1.0000 0.0045
-16.750 -0.9411 0.08753 0.08469 -0.0338 1.0000 0.0045
-16.500 -0.9605 0.08011 0.07712 -0.0377 1.0000 0.0045
-16.250 -0.9751 0.07385 0.07071 -0.0407 1.0000 0.0045
-16.000 -0.9765 0.06733 0.06365 -0.0471 0.8436 0.0045
-15.750 -0.9860 0.06292 0.05890 -0.0486 0.7890 0.0045
-15.500 -0.9928 0.05879 0.05457 -0.0500 0.7734 0.0045
-15.250 -0.9999 0.05483 0.05043 -0.0511 0.7635 0.0045
-15.000 -1.0079 0.05096 0.04637 -0.0518 0.7565 0.0046
-14.500 -1.0172 0.04461 0.03970 -0.0521 0.7456 0.0046
-14.250 -1.0182 0.04196 0.03691 -0.0519 0.7411 0.0046
-14.000 -1.0169 0.03962 0.03443 -0.0516 0.7369 0.0047
-13.500 -1.0083 0.03557 0.03015 -0.0508 0.7300 0.0047
-13.250 -1.0015 0.03380 0.02828 -0.0504 0.7271 0.0048
-13.000 -0.9932 0.03219 0.02658 -0.0499 0.7242 0.0048
-12.750 -0.9835 0.03071 0.02501 -0.0494 0.7214 0.0049
-12.500 -0.9727 0.02934 0.02354 -0.0489 0.7185 0.0049
-12.000 -0.9476 0.02688 0.02093 -0.0480 0.7137 0.0050
-11.750 -0.9339 0.02573 0.01972 -0.0475 0.7117 0.0050
-11.500 -0.9192 0.02466 0.01859 -0.0471 0.7097 0.0051
-11.250 -0.9039 0.02364 0.01750 -0.0467 0.7077 0.0051
-11.000 -0.8878 0.02267 0.01647 -0.0464 0.7058 0.0052
-10.750 -0.8710 0.02176 0.01550 -0.0460 0.7040 0.0053
-10.500 -0.8536 0.02090 0.01458 -0.0457 0.7021 0.0054
-10.250 -0.8359 0.02008 0.01370 -0.0454 0.7001 0.0055
-10.000 -0.8184 0.01931 0.01288 -0.0450 0.6983 0.0056
-9.750 -0.8023 0.01861 0.01213 -0.0442 0.6969 0.0057
-9.500 -0.7821 0.01796 0.01143 -0.0439 0.6956 0.0058
-9.250 -0.7614 0.01733 0.01076 -0.0435 0.6942 0.0059
-9.000 -0.7399 0.01674 0.01011 -0.0432 0.6928 0.0061
-8.750 -0.7175 0.01619 0.00951 -0.0429 0.6914 0.0062
-8.500 -0.6945 0.01568 0.00896 -0.0427 0.6898 0.0063
-8.250 -0.6707 0.01521 0.00845 -0.0426 0.6882 0.0064
-8.000 -0.6463 0.01479 0.00798 -0.0425 0.6867 0.0065
-7.750 -0.6227 0.01423 0.00738 -0.0423 0.6852 0.0067
-7.500 -0.5978 0.01381 0.00693 -0.0423 0.6838 0.0070
-7.250 -0.5720 0.01346 0.00655 -0.0423 0.6823 0.0072
-7.000 -0.5458 0.01312 0.00620 -0.0424 0.6814 0.0075
-6.750 -0.5192 0.01280 0.00586 -0.0425 0.6804 0.0078
-6.500 -0.4923 0.01249 0.00554 -0.0427 0.6792 0.0082
-6.250 -0.4651 0.01221 0.00524 -0.0429 0.6779 0.0085
-6.000 -0.4378 0.01192 0.00493 -0.0431 0.6765 0.0089
-5.750 -0.4103 0.01164 0.00466 -0.0433 0.6751 0.0096
-5.500 -0.3824 0.01140 0.00441 -0.0436 0.6739 0.0105
-5.250 -0.3544 0.01118 0.00418 -0.0439 0.6726 0.0116
-5.000 -0.3263 0.01096 0.00396 -0.0442 0.6713 0.0135
-4.750 -0.2980 0.01074 0.00375 -0.0445 0.6699 0.0160
-4.500 -0.2697 0.01054 0.00355 -0.0448 0.6684 0.0199
-4.250 -0.2413 0.01031 0.00335 -0.0452 0.6669 0.0284
-4.000 -0.2131 0.00999 0.00313 -0.0456 0.6653 0.0539
-3.750 -0.1865 0.00900 0.00265 -0.0464 0.6642 0.1817
-3.500 -0.1586 0.00800 0.00221 -0.0475 0.6626 0.3200
-3.250 -0.1294 0.00695 0.00178 -0.0489 0.6608 0.4791
-3.000 -0.0992 0.00660 0.00174 -0.0497 0.6588 0.5656
-2.750 -0.0691 0.00658 0.00173 -0.0502 0.6568 0.5828
-2.500 -0.0390 0.00658 0.00171 -0.0507 0.6546 0.5918
-2.250 -0.0091 0.00659 0.00170 -0.0511 0.6520 0.5992
-2.000 0.0209 0.00662 0.00166 -0.0516 0.6491 0.6040
-1.750 0.0510 0.00660 0.00166 -0.0520 0.6462 0.6078
-1.500 0.0810 0.00658 0.00165 -0.0525 0.6424 0.6116
-1.250 0.1110 0.00659 0.00163 -0.0529 0.6387 0.6149
-1.000 0.1410 0.00660 0.00160 -0.0534 0.6356 0.6177
-0.750 0.1709 0.00663 0.00158 -0.0538 0.6325 0.6198
-0.500 0.2010 0.00661 0.00158 -0.0543 0.6292 0.6222
-0.250 0.2309 0.00660 0.00159 -0.0547 0.6252 0.6249
0.000 0.2607 0.00662 0.00159 -0.0552 0.6203 0.6273
0.250 0.2904 0.00663 0.00158 -0.0556 0.6136 0.6293
0.500 0.3200 0.00664 0.00156 -0.0559 0.6026 0.6309
0.750 0.3495 0.00666 0.00155 -0.0563 0.5911 0.6323
1.000 0.3789 0.00671 0.00155 -0.0566 0.5791 0.6338
1.250 0.4080 0.00677 0.00156 -0.0569 0.5643 0.6351
1.500 0.4369 0.00687 0.00159 -0.0572 0.5469 0.6361
1.750 0.4653 0.00697 0.00163 -0.0574 0.5260 0.6374
2.000 0.4930 0.00716 0.00171 -0.0575 0.4973 0.6388
2.250 0.5203 0.00739 0.00183 -0.0575 0.4663 0.6402
2.500 0.5477 0.00761 0.00195 -0.0576 0.4402 0.6415
2.750 0.5752 0.00783 0.00208 -0.0577 0.4148 0.6428
3.000 0.6023 0.00809 0.00223 -0.0577 0.3874 0.6440
3.250 0.6293 0.00834 0.00238 -0.0577 0.3614 0.6452
3.500 0.6565 0.00858 0.00253 -0.0577 0.3394 0.6466
3.750 0.6833 0.00884 0.00270 -0.0577 0.3152 0.6480
4.000 0.7098 0.00913 0.00288 -0.0577 0.2900 0.6493
4.250 0.7360 0.00943 0.00306 -0.0576 0.2648 0.6504
4.750 0.7893 0.00994 0.00343 -0.0575 0.2301 0.6523
5.000 0.8156 0.01019 0.00362 -0.0574 0.2131 0.6537
5.250 0.8420 0.01044 0.00383 -0.0573 0.1994 0.6552
5.500 0.8679 0.01072 0.00405 -0.0572 0.1840 0.6565
5.750 0.8936 0.01101 0.00429 -0.0570 0.1694 0.6577
6.000 0.9201 0.01123 0.00450 -0.0569 0.1602 0.6589
6.250 0.9461 0.01149 0.00473 -0.0568 0.1512 0.6602
6.500 0.9719 0.01175 0.00497 -0.0566 0.1424 0.6614
6.750 0.9979 0.01199 0.00521 -0.0565 0.1353 0.6628
7.000 1.0229 0.01230 0.00548 -0.0562 0.1260 0.6643
7.250 1.0485 0.01255 0.00573 -0.0560 0.1193 0.6657
7.500 1.0730 0.01288 0.00602 -0.0557 0.1106 0.6669
7.750 1.0972 0.01323 0.00633 -0.0553 0.1015 0.6680
8.000 1.1212 0.01356 0.00665 -0.0549 0.0933 0.6690
8.250 1.1445 0.01394 0.00699 -0.0544 0.0852 0.6702
8.500 1.1672 0.01434 0.00737 -0.0538 0.0776 0.6716
8.750 1.1903 0.01469 0.00773 -0.0532 0.0717 0.6730
9.000 1.2121 0.01512 0.00815 -0.0525 0.0659 0.6744
9.250 1.2345 0.01549 0.00853 -0.0518 0.0613 0.6758
9.500 1.2550 0.01597 0.00899 -0.0509 0.0558 0.6773
9.750 1.2763 0.01637 0.00941 -0.0501 0.0523 0.6790
10.000 1.2955 0.01687 0.00991 -0.0490 0.0481 0.6806
10.250 1.3151 0.01732 0.01038 -0.0480 0.0451 0.6822
10.500 1.3312 0.01782 0.01089 -0.0464 0.0422 0.6836
10.750 1.3454 0.01834 0.01143 -0.0444 0.0398 0.6849
11.000 1.3621 0.01887 0.01200 -0.0430 0.0379 0.6860
11.250 1.3775 0.01950 0.01266 -0.0415 0.0357 0.6878
11.500 1.3919 0.02021 0.01340 -0.0401 0.0338 0.6894
11.750 1.4075 0.02087 0.01412 -0.0389 0.0326 0.6911
12.000 1.4219 0.02165 0.01495 -0.0377 0.0311 0.6929
12.250 1.4348 0.02259 0.01593 -0.0365 0.0294 0.6947
12.500 1.4477 0.02361 0.01699 -0.0356 0.0280 0.6965
12.750 1.4616 0.02463 0.01807 -0.0349 0.0270 0.6983
13.000 1.4744 0.02577 0.01926 -0.0342 0.0258 0.7001
13.250 1.4860 0.02705 0.02058 -0.0336 0.0246 0.7017
13.500 1.4972 0.02840 0.02198 -0.0330 0.0235 0.7036
13.750 1.5091 0.02968 0.02333 -0.0324 0.0227 0.7059
14.000 1.5198 0.03107 0.02479 -0.0319 0.0218 0.7084
14.250 1.5290 0.03258 0.02636 -0.0312 0.0208 0.7109
14.500 1.5367 0.03423 0.02806 -0.0306 0.0200 0.7133
14.750 1.5445 0.03587 0.02976 -0.0299 0.0193 0.7157
15.000 1.5522 0.03752 0.03149 -0.0293 0.0187 0.7179
15.250 1.5585 0.03932 0.03336 -0.0287 0.0181 0.7203
15.500 1.5637 0.04121 0.03533 -0.0282 0.0175 0.7232
15.750 1.5676 0.04326 0.03745 -0.0276 0.0170 0.7262
16.000 1.5695 0.04553 0.03979 -0.0271 0.0163 0.7294
16.250 1.5718 0.04780 0.04215 -0.0266 0.0159 0.7326
16.750 1.5768 0.05258 0.04712 -0.0262 0.0151 0.7400
17.000 1.5777 0.05529 0.04992 -0.0262 0.0147 0.7445
17.250 1.5773 0.05820 0.05293 -0.0264 0.0143 0.7493
17.500 1.5760 0.06134 0.05617 -0.0267 0.0139 0.7548
17.750 1.5731 0.06478 0.05971 -0.0272 0.0135 0.7620
18.000 1.5683 0.06855 0.06360 -0.0279 0.0132 0.7706
18.250 1.5640 0.07235 0.06753 -0.0287 0.0130 0.7829
18.500 1.5598 0.07625 0.07160 -0.0297 0.0127 0.8016
18.750 1.5545 0.08043 0.07604 -0.0311 0.0125 0.8565
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