AH 94-W-301 (ah94w301-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: AH 94-W-301 (ah94w301-il) Reynolds number: 200,000 Max Cl/Cd: 41.65 at α=12.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ah94w301-il-200000.txt Download as CSV file: xf-ah94w301-il-200000.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 = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.250 -0.3067 0.11166 0.10599 -0.0563 0.8377 0.2465
-12.000 -0.4131 0.09348 0.08768 -0.0603 0.8419 0.2685
-11.750 -0.3741 0.09557 0.08959 -0.0601 0.8114 0.2678
-11.500 -0.3329 0.09808 0.09196 -0.0595 0.7887 0.2666
-11.250 -0.3280 0.09553 0.08933 -0.0600 0.7752 0.2708
-11.000 -0.2992 0.09624 0.08995 -0.0598 0.7613 0.2716
-10.750 -0.2730 0.09655 0.09018 -0.0598 0.7486 0.2730
-10.500 -0.6805 0.04658 0.03990 -0.0651 0.7742 0.3344
-10.250 -0.6281 0.04916 0.04245 -0.0653 0.7602 0.3344
-10.000 -0.5806 0.05139 0.04464 -0.0653 0.7476 0.3345
-9.750 -0.7143 0.03772 0.03068 -0.0641 0.7446 0.3510
-9.500 -0.6462 0.04101 0.03406 -0.0649 0.7333 0.3507
-9.250 -0.5910 0.04357 0.03660 -0.0652 0.7230 0.3508
-9.000 -0.5418 0.04574 0.03876 -0.0654 0.7135 0.3509
-8.750 -0.4963 0.04764 0.04065 -0.0656 0.7040 0.3509
-8.500 -0.4532 0.04946 0.04241 -0.0657 0.6960 0.3509
-8.250 -0.4112 0.05118 0.04414 -0.0658 0.6883 0.3510
-8.000 -0.3709 0.05281 0.04577 -0.0659 0.6807 0.3509
-7.750 -0.3320 0.05438 0.04728 -0.0658 0.6738 0.3509
-7.500 -0.2938 0.05593 0.04880 -0.0659 0.6671 0.3507
-7.250 -0.6012 0.02838 0.02063 -0.0611 0.6720 0.3891
-7.000 -0.5644 0.02894 0.02130 -0.0615 0.6658 0.3909
-6.750 -0.5299 0.02940 0.02183 -0.0619 0.6593 0.3928
-6.500 -0.4995 0.02964 0.02207 -0.0622 0.6536 0.3953
-6.250 -0.4786 0.02924 0.02156 -0.0624 0.6488 0.3992
-6.000 -0.4781 0.02708 0.01906 -0.0631 0.6446 0.4062
-5.750 -0.4464 0.02720 0.01931 -0.0633 0.6393 0.4083
-5.500 -0.4141 0.02751 0.01970 -0.0635 0.6340 0.4102
-5.250 -0.3829 0.02780 0.01999 -0.0638 0.6291 0.4124
-5.000 -0.3537 0.02794 0.02009 -0.0642 0.6246 0.4153
-4.750 -0.3307 0.02746 0.01953 -0.0649 0.6203 0.4197
-4.500 -0.3123 0.02615 0.01801 -0.0663 0.6159 0.4253
-4.250 -0.2820 0.02625 0.01821 -0.0664 0.6114 0.4273
-4.000 -0.2510 0.02652 0.01853 -0.0666 0.6071 0.4293
-3.750 -0.2205 0.02676 0.01876 -0.0669 0.6032 0.4317
-3.500 -0.1913 0.02691 0.01887 -0.0674 0.5992 0.4347
-3.250 -0.1653 0.02650 0.01846 -0.0682 0.5950 0.4388
-3.000 -0.1397 0.02560 0.01736 -0.0701 0.5908 0.4443
-2.750 -0.1104 0.02565 0.01750 -0.0702 0.5869 0.4465
-2.500 -0.0803 0.02587 0.01776 -0.0703 0.5833 0.4486
-2.250 -0.0500 0.02607 0.01796 -0.0707 0.5800 0.4510
-2.000 -0.0203 0.02624 0.01809 -0.0713 0.5765 0.4539
-1.750 0.0074 0.02603 0.01791 -0.0720 0.5727 0.4578
-1.500 0.0365 0.02550 0.01725 -0.0738 0.5686 0.4631
-1.250 0.0653 0.02537 0.01716 -0.0742 0.5648 0.4659
-1.000 0.0947 0.02550 0.01735 -0.0744 0.5615 0.4680
-0.750 0.1249 0.02563 0.01748 -0.0748 0.5585 0.4703
-0.500 0.1554 0.02582 0.01763 -0.0754 0.5556 0.4732
-0.250 0.1840 0.02591 0.01774 -0.0760 0.5525 0.4769
0.000 0.2134 0.02568 0.01750 -0.0773 0.5487 0.4817
0.250 0.2430 0.02542 0.01721 -0.0784 0.5449 0.4854
0.500 0.2715 0.02547 0.01733 -0.0785 0.5414 0.4875
0.750 0.3012 0.02558 0.01747 -0.0788 0.5385 0.4898
1.000 0.3317 0.02572 0.01759 -0.0793 0.5358 0.4926
1.250 0.3629 0.02596 0.01778 -0.0801 0.5332 0.4962
1.500 0.3913 0.02602 0.01789 -0.0809 0.5302 0.5005
1.750 0.4219 0.02592 0.01773 -0.0824 0.5265 0.5050
2.000 0.4485 0.02590 0.01783 -0.0823 0.5230 0.5074
2.250 0.4765 0.02602 0.01802 -0.0823 0.5197 0.5097
2.500 0.5061 0.02616 0.01818 -0.0826 0.5170 0.5124
2.750 0.5369 0.02630 0.01831 -0.0833 0.5146 0.5158
3.000 0.5693 0.02648 0.01842 -0.0844 0.5122 0.5200
3.250 0.5985 0.02666 0.01860 -0.0854 0.5093 0.5244
3.500 0.6248 0.02672 0.01874 -0.0857 0.5057 0.5276
3.750 0.6499 0.02691 0.01905 -0.0853 0.5022 0.5301
4.000 0.6767 0.02714 0.01936 -0.0852 0.4992 0.5328
4.250 0.7053 0.02734 0.01959 -0.0854 0.4966 0.5361
4.500 0.7367 0.02743 0.01967 -0.0862 0.4943 0.5401
4.750 0.7710 0.02750 0.01965 -0.0877 0.4919 0.5445
5.000 0.8014 0.02781 0.01991 -0.0888 0.4891 0.5484
5.250 0.8210 0.02812 0.02042 -0.0878 0.4857 0.5510
5.500 0.8429 0.02854 0.02099 -0.0869 0.4824 0.5537
5.750 0.8675 0.02888 0.02142 -0.0865 0.4793 0.5570
6.000 0.8959 0.02904 0.02161 -0.0868 0.4766 0.5608
6.250 0.9280 0.02907 0.02159 -0.0877 0.4741 0.5652
6.500 0.9639 0.02912 0.02154 -0.0894 0.4719 0.5696
6.750 0.9950 0.02945 0.02187 -0.0903 0.4696 0.5728
7.000 1.0055 0.03015 0.02283 -0.0878 0.4660 0.5755
7.250 1.0217 0.03075 0.02358 -0.0863 0.4623 0.5786
7.500 1.0439 0.03112 0.02403 -0.0856 0.4590 0.5825
7.750 1.0718 0.03131 0.02424 -0.0858 0.4563 0.5869
8.000 1.1051 0.03132 0.02419 -0.0870 0.4539 0.5915
8.250 1.1422 0.03120 0.02401 -0.0885 0.4517 0.5953
8.500 1.1677 0.03166 0.02454 -0.0883 0.4490 0.5985
8.750 1.1642 0.03282 0.02597 -0.0841 0.4446 0.6014
9.000 1.1741 0.03354 0.02682 -0.0817 0.4407 0.6051
9.250 1.1984 0.03372 0.02703 -0.0814 0.4375 0.6098
9.500 1.2337 0.03354 0.02678 -0.0826 0.4349 0.6148
9.750 1.2778 0.03303 0.02621 -0.0848 0.4324 0.6190
10.000 1.3035 0.03334 0.02657 -0.0846 0.4293 0.6225
10.250 1.2716 0.03512 0.02865 -0.0766 0.4242 0.6249
10.500 1.2619 0.03606 0.02970 -0.0716 0.4200 0.6284
10.750 1.2940 0.03579 0.02941 -0.0720 0.4169 0.6339
11.000 1.3556 0.03471 0.02820 -0.0765 0.4142 0.6400
11.250 1.4051 0.03411 0.02756 -0.0793 0.4105 0.6445
11.500 1.3237 0.03794 0.03176 -0.0665 0.4049 0.6457
11.750 1.3239 0.03903 0.03296 -0.0640 0.4000 0.6493
12.000 1.3818 0.03708 0.03091 -0.0663 0.3967 0.6556
12.250 1.4570 0.03498 0.02856 -0.0711 0.3934 0.6632
12.500 1.3670 0.04094 0.03495 -0.0613 0.3868 0.6639
12.750 1.3510 0.04357 0.03773 -0.0589 0.3811 0.6670
13.000 1.4120 0.04090 0.03498 -0.0602 0.3782 0.6736
13.250 1.4854 0.03803 0.03191 -0.0631 0.3748 0.6814
13.500 1.3206 0.05207 0.04651 -0.0549 0.3633 0.6783
13.750 1.3950 0.04779 0.04210 -0.0562 0.3611 0.6865
14.000 1.4608 0.04430 0.03852 -0.0571 0.3580 0.6935
14.250 1.0604 0.08877 0.08363 -0.0545 0.3170 0.6759
14.500 1.1053 0.08616 0.08103 -0.0542 0.3164 0.6832
14.750 1.1484 0.08372 0.07862 -0.0539 0.3149 0.6895
15.000 1.3467 0.06373 0.05845 -0.0529 0.3269 0.7076
15.250 1.4072 0.05979 0.05446 -0.0526 0.3239 0.7155
15.500 1.3257 0.07119 0.06609 -0.0526 0.3111 0.7153
15.750 1.3792 0.06793 0.06276 -0.0523 0.3075 0.7243
16.000 1.3277 0.07660 0.07158 -0.0528 0.2960 0.7261
16.250 1.3700 0.07451 0.06943 -0.0525 0.2911 0.7343
16.500 1.3380 0.08111 0.07616 -0.0530 0.2805 0.7373
16.750 1.3707 0.08007 0.07505 -0.0527 0.2743 0.7464
17.000 1.3439 0.08635 0.08142 -0.0536 0.2635 0.7505
17.250 1.3788 0.08487 0.07984 -0.0530 0.2569 0.7591
17.500 1.3492 0.09155 0.08666 -0.0540 0.2457 0.7628
17.750 1.3598 0.09326 0.08830 -0.0541 0.2370 0.7709
18.000 1.3573 0.09654 0.09158 -0.0546 0.2272 0.7771
18.250 1.3477 0.10078 0.09587 -0.0552 0.2173 0.7831
18.500 1.3570 0.10259 0.09757 -0.0555 0.2085 0.7926
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