AH 93-W-300 (ah93w300-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: AH 93-W-300 (ah93w300-il) Reynolds number: 500,000 Max Cl/Cd: 58.69 at α=6.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ah93w300-il-500000-n5.txt Download as CSV file: xf-ah93w300-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: AH 93-W-300
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
------ -------- --------- --------- -------- -------- --------
-18.250 -0.9437 0.09172 0.08632 -0.0473 1.0000 0.1159
-18.000 -0.9415 0.08897 0.08356 -0.0480 1.0000 0.1194
-17.750 -0.9438 0.08573 0.08031 -0.0488 1.0000 0.1228
-17.500 -0.9433 0.08287 0.07745 -0.0494 1.0000 0.1267
-17.250 -0.9429 0.08000 0.07457 -0.0501 1.0000 0.1304
-17.000 -0.9453 0.07689 0.07146 -0.0506 1.0000 0.1346
-16.750 -0.9431 0.07430 0.06887 -0.0511 1.0000 0.1390
-16.500 -0.9482 0.07101 0.06559 -0.0516 1.0000 0.1435
-16.250 -0.9463 0.06848 0.06306 -0.0519 1.0000 0.1483
-16.000 -0.9507 0.06535 0.05994 -0.0522 1.0000 0.1529
-15.750 -0.9496 0.06287 0.05746 -0.0523 1.0000 0.1579
-15.500 -0.9527 0.06001 0.05461 -0.0524 1.0000 0.1626
-15.250 -0.9525 0.05758 0.05219 -0.0524 1.0000 0.1677
-15.000 -0.9536 0.05508 0.04969 -0.0522 1.0000 0.1725
-14.750 -0.9561 0.05258 0.04721 -0.0519 1.0000 0.1778
-14.500 -0.9532 0.05041 0.04503 -0.0519 0.9991 0.1827
-14.250 -0.9430 0.04732 0.04196 -0.0544 0.9795 0.1890
-14.000 -0.9183 0.04477 0.03937 -0.0590 0.9519 0.1952
-13.750 -0.9015 0.04192 0.03646 -0.0626 0.9202 0.2018
-13.500 -0.8906 0.04016 0.03456 -0.0631 0.8875 0.2069
-13.250 -0.8893 0.03795 0.03226 -0.0629 0.8608 0.2121
-13.000 -0.8821 0.03627 0.03049 -0.0627 0.8407 0.2173
-12.750 -0.8776 0.03443 0.02856 -0.0625 0.8233 0.2222
-12.500 -0.8730 0.03258 0.02666 -0.0623 0.8076 0.2275
-12.000 -0.8603 0.02931 0.02327 -0.0617 0.7813 0.2374
-11.750 -0.8510 0.02794 0.02182 -0.0614 0.7684 0.2426
-11.500 -0.8411 0.02657 0.02039 -0.0612 0.7583 0.2471
-11.250 -0.8333 0.02506 0.01887 -0.0609 0.7478 0.2522
-11.000 -0.8222 0.02381 0.01755 -0.0606 0.7366 0.2573
-10.750 -0.8091 0.02273 0.01641 -0.0604 0.7272 0.2618
-10.500 -0.7996 0.02137 0.01504 -0.0601 0.7181 0.2672
-10.250 -0.7855 0.02037 0.01398 -0.0598 0.7086 0.2730
-10.000 -0.7738 0.01928 0.01285 -0.0594 0.6995 0.2786
-9.750 -0.7613 0.01824 0.01180 -0.0589 0.6916 0.2847
-9.500 -0.7460 0.01754 0.01104 -0.0583 0.6822 0.2895
-9.250 -0.7375 0.01677 0.01022 -0.0568 0.6733 0.2937
-9.000 -0.7186 0.01614 0.00957 -0.0568 0.6663 0.2983
-8.750 -0.6951 0.01570 0.00909 -0.0571 0.6586 0.3029
-8.500 -0.6703 0.01538 0.00871 -0.0573 0.6496 0.3070
-8.250 -0.6462 0.01504 0.00834 -0.0574 0.6407 0.3117
-8.000 -0.6193 0.01476 0.00804 -0.0579 0.6337 0.3164
-7.750 -0.5913 0.01456 0.00780 -0.0583 0.6259 0.3207
-7.500 -0.5639 0.01435 0.00754 -0.0586 0.6176 0.3247
-7.250 -0.5358 0.01414 0.00732 -0.0591 0.6099 0.3288
-7.000 -0.5066 0.01396 0.00712 -0.0596 0.6021 0.3331
-6.750 -0.4772 0.01384 0.00694 -0.0601 0.5937 0.3369
-6.500 -0.4481 0.01373 0.00677 -0.0606 0.5858 0.3403
-6.250 -0.4182 0.01355 0.00661 -0.0612 0.5790 0.3443
-6.000 -0.3881 0.01343 0.00647 -0.0619 0.5708 0.3484
-5.750 -0.3580 0.01336 0.00633 -0.0624 0.5627 0.3521
-5.500 -0.3275 0.01330 0.00621 -0.0630 0.5559 0.3554
-5.250 -0.2968 0.01317 0.00610 -0.0637 0.5488 0.3592
-5.000 -0.2663 0.01308 0.00600 -0.0643 0.5406 0.3631
-4.500 -0.2046 0.01298 0.00582 -0.0656 0.5271 0.3705
-4.250 -0.1734 0.01295 0.00574 -0.0663 0.5199 0.3737
-4.000 -0.1428 0.01289 0.00567 -0.0669 0.5122 0.3773
-3.750 -0.1120 0.01286 0.00562 -0.0675 0.5055 0.3810
-3.500 -0.0805 0.01281 0.00557 -0.0682 0.4992 0.3849
-3.250 -0.0494 0.01281 0.00552 -0.0689 0.4921 0.3884
-3.000 -0.0187 0.01284 0.00548 -0.0694 0.4850 0.3914
-2.750 0.0125 0.01280 0.00545 -0.0701 0.4793 0.3949
-2.500 0.0439 0.01277 0.00544 -0.0707 0.4731 0.3986
-2.250 0.0749 0.01278 0.00542 -0.0713 0.4667 0.4022
-2.000 0.1055 0.01282 0.00542 -0.0719 0.4608 0.4058
-1.750 0.1369 0.01284 0.00541 -0.0725 0.4559 0.4091
-1.500 0.1681 0.01285 0.00541 -0.0731 0.4502 0.4121
-1.250 0.1990 0.01287 0.00543 -0.0737 0.4444 0.4155
-1.000 0.2294 0.01291 0.00546 -0.0742 0.4390 0.4190
-0.750 0.2603 0.01295 0.00549 -0.0747 0.4343 0.4227
-0.500 0.2915 0.01298 0.00552 -0.0753 0.4294 0.4261
-0.250 0.3222 0.01304 0.00555 -0.0758 0.4238 0.4291
0.000 0.3523 0.01312 0.00559 -0.0762 0.4184 0.4318
0.250 0.3823 0.01318 0.00565 -0.0766 0.4133 0.4354
0.500 0.4132 0.01321 0.00572 -0.0771 0.4087 0.4390
0.750 0.4436 0.01328 0.00578 -0.0776 0.4033 0.4424
1.000 0.4731 0.01338 0.00586 -0.0778 0.3978 0.4456
1.250 0.5021 0.01351 0.00594 -0.0780 0.3924 0.4487
1.500 0.5324 0.01358 0.00601 -0.0784 0.3880 0.4515
1.750 0.5621 0.01365 0.00610 -0.0787 0.3826 0.4551
2.000 0.5908 0.01376 0.00621 -0.0789 0.3771 0.4584
2.250 0.6189 0.01391 0.00634 -0.0789 0.3718 0.4617
2.500 0.6485 0.01399 0.00645 -0.0792 0.3673 0.4652
2.750 0.6769 0.01412 0.00657 -0.0793 0.3618 0.4686
3.000 0.7041 0.01429 0.00670 -0.0792 0.3562 0.4716
3.250 0.7312 0.01446 0.00683 -0.0790 0.3512 0.4740
3.500 0.7593 0.01456 0.00698 -0.0790 0.3462 0.4775
3.750 0.7859 0.01472 0.00715 -0.0788 0.3407 0.4810
4.000 0.8106 0.01494 0.00735 -0.0783 0.3351 0.4845
4.250 0.8368 0.01510 0.00752 -0.0780 0.3306 0.4879
4.500 0.8620 0.01528 0.00771 -0.0775 0.3253 0.4909
4.750 0.8845 0.01551 0.00792 -0.0766 0.3199 0.4937
5.000 0.9030 0.01577 0.00814 -0.0749 0.3151 0.4961
5.250 0.9247 0.01595 0.00836 -0.0738 0.3106 0.4993
5.500 0.9453 0.01620 0.00863 -0.0726 0.3055 0.5028
5.750 0.9656 0.01656 0.00899 -0.0714 0.3003 0.5060
6.000 0.9881 0.01689 0.00933 -0.0706 0.2957 0.5092
6.250 1.0106 0.01722 0.00969 -0.0699 0.2907 0.5124
6.500 1.0310 0.01765 0.01011 -0.0689 0.2855 0.5156
6.750 1.0504 0.01814 0.01058 -0.0678 0.2808 0.5187
7.000 1.0721 0.01855 0.01100 -0.0671 0.2760 0.5212
7.250 1.0914 0.01906 0.01151 -0.0661 0.2708 0.5240
7.750 1.1293 0.02020 0.01270 -0.0643 0.2612 0.5308
8.000 1.1478 0.02082 0.01334 -0.0635 0.2561 0.5343
8.250 1.1630 0.02163 0.01416 -0.0623 0.2511 0.5379
8.500 1.1817 0.02230 0.01485 -0.0616 0.2466 0.5414
8.750 1.1984 0.02310 0.01566 -0.0607 0.2415 0.5444
9.000 1.2124 0.02410 0.01664 -0.0597 0.2365 0.5469
9.250 1.2284 0.02500 0.01755 -0.0589 0.2320 0.5491
9.500 1.2442 0.02595 0.01854 -0.0582 0.2269 0.5528
9.750 1.2555 0.02723 0.01984 -0.0573 0.2220 0.5568
10.000 1.2709 0.02827 0.02092 -0.0567 0.2177 0.5609
10.250 1.2835 0.02953 0.02222 -0.0560 0.2129 0.5647
10.500 1.2929 0.03104 0.02373 -0.0551 0.2084 0.5682
10.750 1.3054 0.03237 0.02510 -0.0545 0.2045 0.5715
11.000 1.3164 0.03384 0.02659 -0.0539 0.2001 0.5745
11.250 1.3230 0.03569 0.02844 -0.0532 0.1959 0.5769
11.500 1.3333 0.03727 0.03006 -0.0527 0.1924 0.5804
11.750 1.3424 0.03901 0.03185 -0.0522 0.1883 0.5850
12.000 1.3483 0.04107 0.03395 -0.0518 0.1844 0.5894
12.250 1.3546 0.04313 0.03607 -0.0514 0.1811 0.5938
12.500 1.3629 0.04504 0.03803 -0.0511 0.1776 0.5980
12.750 1.3673 0.04735 0.04036 -0.0507 0.1739 0.6017
13.000 1.3692 0.04993 0.04296 -0.0504 0.1707 0.6049
13.250 1.3761 0.05207 0.04515 -0.0503 0.1676 0.6079
13.500 1.3808 0.05448 0.04762 -0.0502 0.1643 0.6122
13.750 1.3812 0.05735 0.05053 -0.0501 0.1610 0.6170
14.000 1.3842 0.05997 0.05322 -0.0501 0.1583 0.6222
14.250 1.3883 0.06253 0.05585 -0.0501 0.1553 0.6272
14.500 1.3892 0.06543 0.05879 -0.0502 0.1523 0.6318
14.750 1.3866 0.06876 0.06216 -0.0504 0.1495 0.6357
15.000 1.3898 0.07145 0.06490 -0.0505 0.1470 0.6394
15.250 1.3919 0.07430 0.06781 -0.0508 0.1441 0.6439
15.500 1.3904 0.07762 0.07120 -0.0511 0.1414 0.6494
15.750 1.3875 0.08110 0.07473 -0.0515 0.1389 0.6549
16.000 1.3899 0.08400 0.07771 -0.0520 0.1366 0.6608
16.250 1.3913 0.08698 0.08074 -0.0524 0.1340 0.6663
16.500 1.3876 0.09063 0.08444 -0.0530 0.1315 0.6707
16.750 1.3859 0.09404 0.08789 -0.0536 0.1292 0.6757
17.000 1.3873 0.09714 0.09108 -0.0543 0.1268 0.6818
17.250 1.3869 0.10044 0.09445 -0.0550 0.1243 0.6880
17.500 1.3846 0.10397 0.09802 -0.0558 0.1219 0.6941
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