AH 93-W-300 (ah93w300-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: AH 93-W-300 (ah93w300-il) Reynolds number: 500,000 Max Cl/Cd: 61.36 at α=6.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ah93w300-il-500000.txt Download as CSV file: xf-ah93w300-il-500000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.000 -1.0162 0.09216 0.08705 -0.0468 1.0000 0.1345
-18.750 -1.0170 0.08904 0.08388 -0.0477 1.0000 0.1390
-18.500 -1.0214 0.08565 0.08055 -0.0485 1.0000 0.1437
-18.250 -1.0236 0.08245 0.07731 -0.0493 1.0000 0.1486
-18.000 -1.0274 0.07922 0.07412 -0.0500 1.0000 0.1534
-17.750 -1.0297 0.07608 0.07095 -0.0506 1.0000 0.1586
-17.500 -1.0332 0.07295 0.06786 -0.0512 1.0000 0.1636
-17.250 -1.0350 0.06999 0.06488 -0.0517 1.0000 0.1690
-17.000 -1.0383 0.06696 0.06187 -0.0521 1.0000 0.1741
-16.750 -1.0397 0.06413 0.05903 -0.0524 1.0000 0.1797
-16.500 -1.0425 0.06125 0.05617 -0.0527 1.0000 0.1848
-16.250 -1.0439 0.05856 0.05348 -0.0529 1.0000 0.1904
-16.000 -1.0454 0.05590 0.05081 -0.0530 1.0000 0.1956
-15.750 -1.0470 0.05334 0.04828 -0.0529 1.0000 0.2011
-15.500 -1.0471 0.05092 0.04581 -0.0528 1.0000 0.2062
-15.250 -1.0490 0.04856 0.04351 -0.0525 1.0000 0.2113
-15.000 -1.0501 0.04628 0.04122 -0.0520 1.0000 0.2166
-14.750 -1.0504 0.04422 0.03916 -0.0514 1.0000 0.2213
-14.500 -1.0531 0.04212 0.03710 -0.0505 1.0000 0.2263
-14.250 -1.0547 0.04015 0.03510 -0.0495 1.0000 0.2312
-14.000 -1.0584 0.03837 0.03336 -0.0480 1.0000 0.2357
-13.250 -1.0224 0.03215 0.02716 -0.0526 0.9805 0.2519
-13.000 -0.9963 0.03028 0.02525 -0.0561 0.9689 0.2579
-12.750 -0.9679 0.02844 0.02339 -0.0600 0.9554 0.2634
-12.500 -0.9423 0.02670 0.02161 -0.0633 0.9350 0.2693
-12.250 -0.9245 0.02537 0.02014 -0.0643 0.9096 0.2742
-12.000 -0.9143 0.02410 0.01881 -0.0639 0.8859 0.2789
-11.750 -0.9038 0.02293 0.01758 -0.0634 0.8657 0.2837
-11.500 -0.8910 0.02188 0.01641 -0.0631 0.8493 0.2884
-11.250 -0.8783 0.02088 0.01533 -0.0626 0.8337 0.2927
-11.000 -0.8654 0.01991 0.01434 -0.0622 0.8204 0.2973
-10.750 -0.8509 0.01904 0.01340 -0.0618 0.8071 0.3020
-10.500 -0.8352 0.01829 0.01249 -0.0614 0.7945 0.3061
-10.250 -0.8224 0.01747 0.01172 -0.0606 0.7845 0.3109
-10.000 -0.8130 0.01683 0.01103 -0.0590 0.7732 0.3158
-9.750 -0.7944 0.01634 0.01040 -0.0589 0.7621 0.3207
-9.500 -0.7730 0.01586 0.00994 -0.0589 0.7534 0.3256
-9.250 -0.7496 0.01553 0.00959 -0.0589 0.7437 0.3302
-9.000 -0.7245 0.01531 0.00927 -0.0590 0.7338 0.3345
-8.750 -0.6979 0.01509 0.00896 -0.0593 0.7260 0.3383
-8.500 -0.6715 0.01480 0.00871 -0.0595 0.7171 0.3428
-8.250 -0.6444 0.01462 0.00850 -0.0597 0.7077 0.3471
-8.000 -0.6162 0.01449 0.00830 -0.0601 0.6987 0.3513
-7.750 -0.5871 0.01433 0.00808 -0.0607 0.6914 0.3551
-7.500 -0.5587 0.01412 0.00787 -0.0610 0.6827 0.3594
-7.250 -0.5299 0.01401 0.00773 -0.0614 0.6735 0.3633
-7.000 -0.5001 0.01390 0.00760 -0.0619 0.6656 0.3673
-6.750 -0.4698 0.01379 0.00744 -0.0626 0.6576 0.3711
-6.500 -0.4399 0.01369 0.00725 -0.0631 0.6490 0.3745
-6.250 -0.4105 0.01358 0.00713 -0.0635 0.6400 0.3785
-6.000 -0.3798 0.01347 0.00705 -0.0641 0.6327 0.3823
-5.750 -0.3491 0.01340 0.00694 -0.0648 0.6244 0.3860
-5.500 -0.3186 0.01339 0.00682 -0.0653 0.6157 0.3896
-5.250 -0.2876 0.01331 0.00670 -0.0660 0.6082 0.3929
-5.000 -0.2571 0.01317 0.00661 -0.0666 0.6001 0.3970
-4.750 -0.2265 0.01314 0.00655 -0.0671 0.5919 0.4005
-4.500 -0.1957 0.01316 0.00650 -0.0677 0.5837 0.4041
-4.250 -0.1640 0.01311 0.00644 -0.0684 0.5767 0.4078
-4.000 -0.1326 0.01311 0.00636 -0.0691 0.5686 0.4107
-3.750 -0.1026 0.01305 0.00627 -0.0696 0.5603 0.4147
-3.500 -0.0714 0.01300 0.00626 -0.0702 0.5537 0.4183
-3.250 -0.0400 0.01299 0.00625 -0.0708 0.5463 0.4219
-3.000 -0.0090 0.01302 0.00622 -0.0714 0.5386 0.4254
-2.750 0.0220 0.01309 0.00620 -0.0720 0.5311 0.4287
-2.500 0.0539 0.01306 0.00616 -0.0727 0.5249 0.4317
-2.250 0.0845 0.01299 0.00612 -0.0732 0.5180 0.4358
-2.000 0.1150 0.01304 0.00614 -0.0737 0.5112 0.4392
-1.750 0.1461 0.01310 0.00619 -0.0743 0.5048 0.4426
-1.500 0.1777 0.01312 0.00621 -0.0749 0.4988 0.4461
-1.250 0.2088 0.01317 0.00621 -0.0755 0.4925 0.4493
-1.000 0.2396 0.01329 0.00623 -0.0760 0.4861 0.4517
-0.750 0.2700 0.01324 0.00623 -0.0765 0.4805 0.4561
-0.500 0.3010 0.01325 0.00629 -0.0770 0.4750 0.4596
-0.250 0.3317 0.01332 0.00635 -0.0775 0.4691 0.4628
0.000 0.3617 0.01343 0.00641 -0.0778 0.4631 0.4661
0.250 0.3922 0.01355 0.00649 -0.0783 0.4574 0.4694
0.500 0.4234 0.01360 0.00654 -0.0788 0.4524 0.4723
0.750 0.4537 0.01363 0.00655 -0.0793 0.4468 0.4755
1.000 0.4829 0.01368 0.00660 -0.0795 0.4410 0.4793
1.250 0.5124 0.01382 0.00673 -0.0797 0.4352 0.4825
1.500 0.5428 0.01387 0.00683 -0.0801 0.4306 0.4858
1.750 0.5726 0.01396 0.00692 -0.0804 0.4252 0.4892
2.000 0.6016 0.01410 0.00701 -0.0806 0.4197 0.4925
2.250 0.6302 0.01431 0.00715 -0.0807 0.4137 0.4952
2.500 0.6602 0.01436 0.00723 -0.0811 0.4094 0.4976
2.750 0.6890 0.01435 0.00727 -0.0812 0.4041 0.5023
3.000 0.7168 0.01447 0.00739 -0.0812 0.3987 0.5058
3.250 0.7435 0.01471 0.00759 -0.0810 0.3927 0.5090
3.500 0.7723 0.01478 0.00771 -0.0811 0.3884 0.5123
3.750 0.8003 0.01490 0.00784 -0.0810 0.3832 0.5156
4.000 0.8267 0.01509 0.00799 -0.0808 0.3778 0.5187
4.250 0.8518 0.01537 0.00820 -0.0803 0.3721 0.5212
4.500 0.8793 0.01540 0.00829 -0.0802 0.3677 0.5249
4.750 0.9051 0.01550 0.00843 -0.0798 0.3625 0.5290
5.000 0.9287 0.01570 0.00863 -0.0791 0.3573 0.5324
5.250 0.9507 0.01598 0.00889 -0.0781 0.3520 0.5357
5.500 0.9742 0.01612 0.00909 -0.0772 0.3476 0.5392
5.750 0.9931 0.01632 0.00930 -0.0756 0.3426 0.5425
6.000 1.0103 0.01662 0.00957 -0.0738 0.3375 0.5454
6.250 1.0300 0.01698 0.00990 -0.0725 0.3326 0.5478
6.500 1.0537 0.01722 0.01018 -0.0719 0.3278 0.5508
6.750 1.0750 0.01752 0.01051 -0.0710 0.3226 0.5558
7.000 1.0933 0.01800 0.01097 -0.0696 0.3173 0.5596
7.250 1.1149 0.01837 0.01140 -0.0688 0.3127 0.5632
7.500 1.1359 0.01877 0.01183 -0.0680 0.3075 0.5667
7.750 1.1536 0.01933 0.01237 -0.0668 0.3023 0.5700
8.000 1.1709 0.01994 0.01297 -0.0656 0.2973 0.5732
8.250 1.1915 0.02043 0.01350 -0.0649 0.2924 0.5761
8.500 1.2090 0.02108 0.01413 -0.0638 0.2871 0.5786
8.750 1.2226 0.02190 0.01494 -0.0625 0.2818 0.5841
9.000 1.2433 0.02243 0.01556 -0.0620 0.2771 0.5885
9.250 1.2594 0.02323 0.01639 -0.0611 0.2719 0.5923
9.500 1.2717 0.02427 0.01741 -0.0598 0.2667 0.5959
9.750 1.2886 0.02510 0.01829 -0.0591 0.2621 0.5997
10.000 1.3039 0.02606 0.01927 -0.0583 0.2570 0.6035
10.250 1.3142 0.02735 0.02053 -0.0573 0.2520 0.6065
10.500 1.3286 0.02844 0.02164 -0.0565 0.2475 0.6093
10.750 1.3431 0.02952 0.02279 -0.0560 0.2426 0.6154
11.000 1.3520 0.03102 0.02430 -0.0551 0.2377 0.6200
11.250 1.3633 0.03239 0.02572 -0.0544 0.2334 0.6244
11.500 1.3751 0.03378 0.02717 -0.0538 0.2287 0.6288
11.750 1.3826 0.03550 0.02888 -0.0531 0.2241 0.6330
12.000 1.3894 0.03733 0.03072 -0.0524 0.2199 0.6370
12.250 1.4007 0.03886 0.03229 -0.0520 0.2156 0.6403
12.500 1.4063 0.04091 0.03438 -0.0515 0.2113 0.6465
12.750 1.4105 0.04307 0.03657 -0.0509 0.2072 0.6519
13.000 1.4197 0.04491 0.03850 -0.0507 0.2034 0.6572
13.250 1.4256 0.04702 0.04065 -0.0504 0.1994 0.6624
13.500 1.4250 0.04978 0.04340 -0.0499 0.1956 0.6670
13.750 1.4333 0.05177 0.04544 -0.0498 0.1922 0.6714
14.000 1.4377 0.05419 0.04793 -0.0497 0.1885 0.6780
14.250 1.4392 0.05684 0.05063 -0.0496 0.1849 0.6843
14.500 1.4396 0.05968 0.05351 -0.0495 0.1816 0.6904
14.750 1.4459 0.06197 0.05588 -0.0495 0.1784 0.6967
15.000 1.4472 0.06483 0.05877 -0.0496 0.1750 0.7018
15.250 1.4454 0.06795 0.06191 -0.0497 0.1718 0.7082
15.500 1.4487 0.07060 0.06466 -0.0498 0.1689 0.7159
15.750 1.4511 0.07340 0.06755 -0.0501 0.1659 0.7235
16.000 1.4514 0.07642 0.07059 -0.0503 0.1628 0.7306
16.250 1.4475 0.07990 0.07408 -0.0507 0.1598 0.7377
16.500 1.4519 0.08252 0.07684 -0.0510 0.1571 0.7466
16.750 1.4516 0.08570 0.08009 -0.0515 0.1542 0.7551
17.000 1.4503 0.08898 0.08339 -0.0520 0.1514 0.7631
17.250 1.4493 0.09216 0.08662 -0.0525 0.1487 0.7729
17.500 1.4504 0.09527 0.08985 -0.0531 0.1461 0.7835
17.750 1.4515 0.09828 0.09295 -0.0537 0.1434 0.7947
18.000 1.4485 0.10177 0.09648 -0.0544 0.1409 0.8072
18.250 1.4485 0.10483 0.09959 -0.0550 0.1384 0.8204
18.500 1.4502 0.10781 0.10269 -0.0557 0.1359 0.8359
18.750 1.4474 0.11124 0.10622 -0.0565 0.1333 0.8522
19.000 1.4463 0.11431 0.10933 -0.0571 0.1309 0.8711
19.250 1.4457 0.11715 0.11226 -0.0574 0.1286 0.8948
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