AH 94-W-301 (ah94w301-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: AH 94-W-301 (ah94w301-il) Reynolds number: 500,000 Max Cl/Cd: 76.86 at α=9.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ah94w301-il-500000-n5.txt Download as CSV file: xf-ah94w301-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: AH 94-W-301
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
------ -------- --------- --------- -------- -------- --------
-18.500 -1.0719 0.09765 0.09269 -0.0320 1.0000 0.1584
-18.250 -1.0745 0.09438 0.08941 -0.0329 1.0000 0.1619
-18.000 -1.0717 0.09175 0.08676 -0.0337 1.0000 0.1653
-17.750 -1.0680 0.08925 0.08422 -0.0344 1.0000 0.1681
-17.500 -1.0711 0.08603 0.08101 -0.0352 1.0000 0.1716
-17.250 -1.0696 0.08335 0.07833 -0.0359 1.0000 0.1751
-17.000 -1.0666 0.08083 0.07579 -0.0365 1.0000 0.1784
-16.750 -1.0648 0.07818 0.07311 -0.0371 1.0000 0.1815
-16.500 -1.0652 0.07540 0.07035 -0.0376 1.0000 0.1852
-16.250 -1.0649 0.07269 0.06763 -0.0381 1.0000 0.1891
-16.000 -1.0629 0.07017 0.06507 -0.0386 1.0000 0.1926
-15.750 -1.0589 0.06790 0.06280 -0.0389 1.0000 0.1958
-15.500 -1.0601 0.06515 0.06006 -0.0393 1.0000 0.1995
-15.250 -1.0561 0.06251 0.05741 -0.0402 0.9986 0.2035
-15.000 -1.0051 0.05900 0.05368 -0.0511 0.8898 0.2084
-14.750 -1.0040 0.05651 0.05092 -0.0516 0.8214 0.2124
-14.500 -1.0010 0.05438 0.04865 -0.0517 0.7935 0.2165
-14.250 -0.9958 0.05240 0.04655 -0.0519 0.7734 0.2203
-14.000 -0.9901 0.05041 0.04445 -0.0522 0.7567 0.2236
-13.750 -0.9874 0.04824 0.04223 -0.0524 0.7415 0.2276
-13.500 -0.9843 0.04603 0.03996 -0.0527 0.7278 0.2318
-13.250 -0.9768 0.04427 0.03811 -0.0529 0.7153 0.2356
-13.000 -0.9694 0.04249 0.03626 -0.0531 0.7036 0.2390
-12.750 -0.9669 0.04035 0.03407 -0.0533 0.6938 0.2432
-12.500 -0.9604 0.03852 0.03221 -0.0535 0.6849 0.2473
-12.250 -0.9524 0.03684 0.03045 -0.0536 0.6756 0.2511
-12.000 -0.9436 0.03529 0.02884 -0.0538 0.6674 0.2546
-11.750 -0.9397 0.03338 0.02691 -0.0538 0.6593 0.2586
-11.500 -0.9323 0.03184 0.02531 -0.0537 0.6508 0.2626
-11.250 -0.9232 0.03039 0.02380 -0.0537 0.6436 0.2664
-11.000 -0.9122 0.02911 0.02246 -0.0537 0.6366 0.2697
-10.750 -0.9064 0.02749 0.02083 -0.0536 0.6301 0.2736
-10.250 -0.8852 0.02494 0.01818 -0.0534 0.6186 0.2812
-10.000 -0.8706 0.02392 0.01710 -0.0535 0.6126 0.2844
-9.750 -0.8611 0.02264 0.01580 -0.0532 0.6066 0.2880
-9.250 -0.8375 0.02043 0.01352 -0.0528 0.5959 0.2956
-9.000 -0.8245 0.01955 0.01260 -0.0523 0.5908 0.2990
-8.750 -0.8139 0.01876 0.01175 -0.0514 0.5860 0.3019
-8.500 -0.7975 0.01788 0.01085 -0.0517 0.5812 0.3056
-8.250 -0.7757 0.01720 0.01012 -0.0527 0.5766 0.3095
-8.000 -0.7500 0.01668 0.00957 -0.0539 0.5727 0.3131
-7.750 -0.7228 0.01632 0.00916 -0.0549 0.5681 0.3163
-7.500 -0.6957 0.01599 0.00879 -0.0558 0.5632 0.3195
-7.250 -0.6684 0.01566 0.00844 -0.0567 0.5584 0.3231
-7.000 -0.6400 0.01541 0.00815 -0.0576 0.5542 0.3266
-6.750 -0.6104 0.01518 0.00790 -0.0587 0.5509 0.3300
-6.500 -0.5804 0.01500 0.00768 -0.0597 0.5472 0.3332
-6.250 -0.5505 0.01480 0.00746 -0.0607 0.5432 0.3362
-6.000 -0.5206 0.01460 0.00725 -0.0617 0.5390 0.3395
-5.750 -0.4904 0.01445 0.00707 -0.0627 0.5348 0.3430
-5.500 -0.4597 0.01431 0.00691 -0.0637 0.5313 0.3465
-5.250 -0.4284 0.01418 0.00676 -0.0648 0.5282 0.3495
-5.000 -0.3971 0.01408 0.00661 -0.0658 0.5249 0.3520
-4.750 -0.3660 0.01393 0.00647 -0.0669 0.5214 0.3554
-4.500 -0.3348 0.01381 0.00635 -0.0679 0.5178 0.3588
-4.250 -0.3036 0.01373 0.00624 -0.0689 0.5140 0.3621
-4.000 -0.2722 0.01366 0.00614 -0.0699 0.5106 0.3650
-3.750 -0.2403 0.01358 0.00604 -0.0709 0.5079 0.3678
-3.500 -0.2084 0.01351 0.00595 -0.0720 0.5050 0.3706
-3.250 -0.1766 0.01341 0.00587 -0.0731 0.5019 0.3739
-3.000 -0.1449 0.01334 0.00581 -0.0741 0.4988 0.3771
-2.750 -0.1132 0.01330 0.00574 -0.0751 0.4957 0.3800
-2.500 -0.0816 0.01327 0.00568 -0.0760 0.4925 0.3831
-2.250 -0.0499 0.01326 0.00563 -0.0770 0.4895 0.3861
-2.000 -0.0177 0.01321 0.00558 -0.0780 0.4868 0.3888
-1.750 0.0143 0.01314 0.00555 -0.0790 0.4840 0.3918
-1.500 0.0463 0.01310 0.00553 -0.0800 0.4811 0.3949
-1.250 0.0782 0.01309 0.00551 -0.0809 0.4783 0.3982
-1.000 0.1099 0.01308 0.00549 -0.0818 0.4755 0.4013
-0.750 0.1415 0.01310 0.00546 -0.0827 0.4727 0.4040
-0.500 0.1729 0.01314 0.00546 -0.0835 0.4698 0.4062
-0.250 0.2050 0.01309 0.00546 -0.0845 0.4676 0.4093
0.000 0.2370 0.01307 0.00548 -0.0854 0.4648 0.4126
0.250 0.2689 0.01307 0.00550 -0.0863 0.4619 0.4157
0.500 0.3005 0.01308 0.00551 -0.0871 0.4592 0.4186
0.750 0.3320 0.01311 0.00553 -0.0879 0.4565 0.4213
1.000 0.3633 0.01316 0.00554 -0.0886 0.4539 0.4237
1.250 0.3944 0.01321 0.00557 -0.0894 0.4513 0.4264
1.500 0.4257 0.01323 0.00563 -0.0901 0.4489 0.4296
1.750 0.4575 0.01324 0.00569 -0.0909 0.4466 0.4327
2.000 0.4889 0.01327 0.00575 -0.0917 0.4439 0.4357
2.250 0.5201 0.01331 0.00580 -0.0924 0.4411 0.4385
2.500 0.5511 0.01337 0.00585 -0.0930 0.4386 0.4412
2.750 0.5819 0.01345 0.00591 -0.0936 0.4361 0.4437
3.000 0.6124 0.01351 0.00598 -0.0942 0.4336 0.4467
3.250 0.6426 0.01360 0.00608 -0.0947 0.4308 0.4498
3.500 0.6736 0.01365 0.00618 -0.0953 0.4286 0.4528
3.750 0.7044 0.01371 0.00628 -0.0959 0.4262 0.4557
4.000 0.7350 0.01378 0.00637 -0.0965 0.4238 0.4587
4.250 0.7652 0.01387 0.00647 -0.0969 0.4213 0.4617
4.500 0.7951 0.01397 0.00657 -0.0973 0.4186 0.4642
4.750 0.8246 0.01406 0.00668 -0.0977 0.4158 0.4672
5.000 0.8537 0.01418 0.00682 -0.0980 0.4131 0.4701
5.250 0.8829 0.01430 0.00696 -0.0982 0.4109 0.4730
5.500 0.9128 0.01439 0.00711 -0.0986 0.4089 0.4761
5.750 0.9422 0.01450 0.00725 -0.0989 0.4064 0.4793
6.000 0.9712 0.01462 0.00739 -0.0991 0.4037 0.4823
6.250 0.9997 0.01474 0.00754 -0.0993 0.4010 0.4848
6.500 1.0278 0.01487 0.00770 -0.0993 0.3985 0.4878
6.750 1.0552 0.01503 0.00788 -0.0993 0.3960 0.4907
7.000 1.0817 0.01522 0.00808 -0.0991 0.3933 0.4937
7.250 1.1096 0.01536 0.00828 -0.0991 0.3910 0.4970
7.500 1.1371 0.01550 0.00848 -0.0990 0.3886 0.5004
7.750 1.1638 0.01567 0.00868 -0.0988 0.3859 0.5033
8.000 1.1895 0.01584 0.00888 -0.0984 0.3828 0.5059
8.250 1.2140 0.01603 0.00911 -0.0979 0.3799 0.5090
8.500 1.2369 0.01626 0.00936 -0.0970 0.3767 0.5120
8.750 1.2593 0.01650 0.00963 -0.0961 0.3736 0.5152
9.000 1.2824 0.01669 0.00989 -0.0952 0.3700 0.5188
9.250 1.3004 0.01692 0.01017 -0.0935 0.3661 0.5221
9.500 1.3170 0.01722 0.01048 -0.0915 0.3624 0.5249
9.750 1.3339 0.01762 0.01089 -0.0897 0.3584 0.5275
10.000 1.3535 0.01799 0.01132 -0.0885 0.3539 0.5307
10.250 1.3725 0.01840 0.01179 -0.0872 0.3480 0.5339
10.500 1.3876 0.01896 0.01237 -0.0855 0.3423 0.5373
10.750 1.4032 0.01957 0.01300 -0.0839 0.3378 0.5408
11.000 1.4213 0.02012 0.01361 -0.0828 0.3328 0.5443
11.250 1.4350 0.02089 0.01439 -0.0812 0.3269 0.5473
11.500 1.4456 0.02188 0.01541 -0.0795 0.3212 0.5502
11.750 1.4605 0.02275 0.01635 -0.0785 0.3146 0.5536
12.000 1.4682 0.02410 0.01772 -0.0770 0.3072 0.5568
12.250 1.4779 0.02544 0.01911 -0.0758 0.3001 0.5602
12.500 1.4830 0.02719 0.02088 -0.0745 0.2916 0.5635
12.750 1.4875 0.02908 0.02279 -0.0733 0.2835 0.5668
13.000 1.4864 0.03147 0.02518 -0.0720 0.2742 0.5696
13.250 1.4858 0.03390 0.02765 -0.0709 0.2650 0.5728
13.500 1.4772 0.03708 0.03085 -0.0697 0.2558 0.5759
13.750 1.4718 0.04003 0.03383 -0.0686 0.2457 0.5791
14.000 1.4601 0.04360 0.03743 -0.0675 0.2363 0.5820
14.250 1.4459 0.04754 0.04138 -0.0665 0.2261 0.5847
14.500 1.4334 0.05143 0.04528 -0.0657 0.2156 0.5874
14.750 1.4180 0.05572 0.04958 -0.0650 0.2061 0.5898
15.000 1.4022 0.06014 0.05400 -0.0644 0.1963 0.5920
15.250 1.3911 0.06416 0.05804 -0.0641 0.1872 0.5945
15.500 1.3775 0.06854 0.06243 -0.0638 0.1783 0.5974
15.750 1.3652 0.07284 0.06675 -0.0637 0.1695 0.6005
16.000 1.3551 0.07697 0.07091 -0.0636 0.1617 0.6038
16.250 1.3439 0.08125 0.07518 -0.0637 0.1538 0.6071
16.500 1.3363 0.08522 0.07919 -0.0638 0.1462 0.6104
16.750 1.3292 0.08911 0.08307 -0.0640 0.1393 0.6135
17.000 1.3211 0.09321 0.08718 -0.0644 0.1322 0.6161
17.250 1.3172 0.09683 0.09083 -0.0647 0.1258 0.6194
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