AH 94-W-301 (ah94w301-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: AH 94-W-301 (ah94w301-il) Reynolds number: 200,000 Max Cl/Cd: 49.22 at α=10° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ah94w301-il-200000-n5.txt Download as CSV file: xf-ah94w301-il-200000-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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.000 -0.8688 0.10351 0.09731 -0.0365 1.0000 0.1967
-16.750 -0.8458 0.10339 0.09724 -0.0369 1.0000 0.1986
-16.500 -0.9138 0.09159 0.08520 -0.0394 1.0000 0.2084
-16.250 -0.8830 0.09245 0.08616 -0.0396 1.0000 0.2100
-16.000 -0.8564 0.09278 0.08656 -0.0399 1.0000 0.2118
-15.750 -0.8425 0.09148 0.08529 -0.0405 1.0000 0.2148
-15.500 -0.8986 0.08167 0.07527 -0.0422 1.0000 0.2236
-15.250 -0.8703 0.08217 0.07587 -0.0424 1.0000 0.2255
-15.000 -0.8485 0.08189 0.07564 -0.0427 1.0000 0.2279
-14.750 -0.8766 0.07572 0.06937 -0.0437 1.0000 0.2347
-14.500 -0.8841 0.07208 0.06569 -0.0443 1.0000 0.2393
-14.250 -0.8587 0.07224 0.06594 -0.0445 1.0000 0.2415
-14.000 -0.8478 0.07074 0.06448 -0.0448 1.0000 0.2450
-13.750 -0.9014 0.06225 0.05577 -0.0456 1.0000 0.2533
-13.500 -0.8649 0.06252 0.05615 -0.0471 0.9435 0.2555
-13.250 -0.8013 0.06177 0.05521 -0.0559 0.8656 0.2588
-13.000 -0.8163 0.05674 0.04991 -0.0578 0.8314 0.2654
-12.750 -0.8194 0.05355 0.04654 -0.0586 0.8069 0.2702
-12.500 -0.7919 0.05365 0.04660 -0.0591 0.7849 0.2726
-12.000 -0.8116 0.04670 0.03933 -0.0598 0.7562 0.2833
-11.750 -0.7980 0.04564 0.03819 -0.0599 0.7425 0.2865
-11.500 -0.7749 0.04543 0.03799 -0.0601 0.7294 0.2892
-11.000 -0.7900 0.03954 0.03183 -0.0603 0.7110 0.2995
-10.750 -0.7779 0.03840 0.03064 -0.0603 0.7013 0.3029
-10.500 -0.7567 0.03806 0.03029 -0.0603 0.6924 0.3057
-10.250 -0.7480 0.03664 0.02883 -0.0603 0.6838 0.3096
-10.000 -0.7561 0.03390 0.02593 -0.0602 0.6763 0.3148
-9.750 -0.7536 0.03209 0.02399 -0.0600 0.6693 0.3189
-9.500 -0.7313 0.03177 0.02372 -0.0600 0.6617 0.3216
-9.250 -0.7169 0.03088 0.02280 -0.0600 0.6547 0.3251
-9.000 -0.7129 0.02925 0.02106 -0.0597 0.6489 0.3294
-8.750 -0.7173 0.02710 0.01873 -0.0592 0.6436 0.3341
-8.500 -0.6969 0.02666 0.01832 -0.0591 0.6373 0.3369
-8.250 -0.6782 0.02619 0.01786 -0.0588 0.6310 0.3398
-8.000 -0.6697 0.02538 0.01698 -0.0578 0.6256 0.3433
-7.750 -0.6634 0.02436 0.01585 -0.0570 0.6207 0.3473
-7.500 -0.6513 0.02330 0.01466 -0.0574 0.6154 0.3514
-7.250 -0.6269 0.02303 0.01440 -0.0577 0.6102 0.3541
-7.000 -0.6020 0.02282 0.01419 -0.0580 0.6054 0.3570
-6.750 -0.5781 0.02254 0.01384 -0.0583 0.6010 0.3603
-6.500 -0.5541 0.02215 0.01340 -0.0588 0.5965 0.3640
-6.250 -0.5299 0.02170 0.01286 -0.0595 0.5915 0.3676
-6.000 -0.5038 0.02139 0.01249 -0.0601 0.5866 0.3707
-5.750 -0.4758 0.02130 0.01241 -0.0606 0.5822 0.3734
-5.500 -0.4480 0.02118 0.01226 -0.0611 0.5784 0.3764
-5.250 -0.4200 0.02099 0.01204 -0.0618 0.5747 0.3797
-5.000 -0.3919 0.02074 0.01175 -0.0627 0.5705 0.3831
-4.750 -0.3636 0.02045 0.01137 -0.0636 0.5662 0.3867
-4.500 -0.3347 0.02032 0.01123 -0.0643 0.5619 0.3895
-4.250 -0.3054 0.02027 0.01118 -0.0648 0.5581 0.3922
-4.000 -0.2760 0.02022 0.01108 -0.0655 0.5547 0.3951
-3.750 -0.2463 0.02009 0.01095 -0.0664 0.5513 0.3982
-3.500 -0.2163 0.01993 0.01077 -0.0673 0.5476 0.4018
-3.250 -0.1861 0.01975 0.01050 -0.0684 0.5438 0.4054
-3.000 -0.1563 0.01967 0.01044 -0.0691 0.5401 0.4080
-2.750 -0.1264 0.01965 0.01042 -0.0697 0.5366 0.4105
-2.500 -0.0961 0.01964 0.01037 -0.0704 0.5334 0.4134
-2.250 -0.0656 0.01960 0.01033 -0.0713 0.5303 0.4167
-2.000 -0.0350 0.01952 0.01024 -0.0722 0.5270 0.4202
-1.750 -0.0040 0.01941 0.01009 -0.0733 0.5237 0.4236
-1.500 0.0265 0.01935 0.01002 -0.0741 0.5204 0.4262
-1.250 0.0566 0.01935 0.01007 -0.0747 0.5173 0.4288
-1.000 0.0871 0.01938 0.01008 -0.0753 0.5142 0.4316
-0.750 0.1180 0.01941 0.01006 -0.0761 0.5113 0.4348
-0.500 0.1486 0.01938 0.01006 -0.0770 0.5082 0.4380
-0.250 0.1796 0.01934 0.01001 -0.0779 0.5051 0.4412
0.000 0.2108 0.01931 0.00993 -0.0789 0.5020 0.4443
0.250 0.2407 0.01933 0.01003 -0.0794 0.4991 0.4468
0.500 0.2709 0.01938 0.01011 -0.0799 0.4963 0.4496
0.750 0.3016 0.01943 0.01015 -0.0806 0.4936 0.4526
1.000 0.3326 0.01949 0.01016 -0.0814 0.4909 0.4557
1.250 0.3631 0.01952 0.01020 -0.0821 0.4880 0.4588
1.500 0.3937 0.01954 0.01023 -0.0829 0.4849 0.4621
1.750 0.4240 0.01958 0.01030 -0.0836 0.4820 0.4651
2.000 0.4535 0.01966 0.01046 -0.0840 0.4793 0.4677
2.250 0.4833 0.01974 0.01058 -0.0845 0.4766 0.4706
2.500 0.5136 0.01982 0.01066 -0.0851 0.4741 0.4735
2.750 0.5443 0.01990 0.01070 -0.0857 0.4716 0.4766
3.000 0.5749 0.02000 0.01077 -0.0865 0.4690 0.4801
3.250 0.6046 0.02010 0.01089 -0.0870 0.4661 0.4835
3.500 0.6332 0.02020 0.01110 -0.0873 0.4633 0.4863
3.750 0.6619 0.02033 0.01131 -0.0876 0.4605 0.4890
4.000 0.6908 0.02046 0.01148 -0.0879 0.4579 0.4917
4.250 0.7201 0.02057 0.01161 -0.0883 0.4552 0.4947
4.500 0.7499 0.02068 0.01170 -0.0887 0.4527 0.4981
4.750 0.7806 0.02082 0.01178 -0.0894 0.4504 0.5018
5.000 0.8090 0.02099 0.01200 -0.0897 0.4479 0.5052
5.250 0.8356 0.02117 0.01231 -0.0896 0.4452 0.5079
5.500 0.8624 0.02136 0.01260 -0.0895 0.4423 0.5106
5.750 0.8895 0.02153 0.01283 -0.0895 0.4394 0.5135
6.000 0.9170 0.02169 0.01303 -0.0896 0.4366 0.5167
6.250 0.9453 0.02186 0.01320 -0.0898 0.4343 0.5204
6.500 0.9747 0.02204 0.01334 -0.0902 0.4321 0.5242
6.750 1.0029 0.02225 0.01356 -0.0904 0.4298 0.5274
7.000 1.0256 0.02252 0.01399 -0.0897 0.4268 0.5302
7.250 1.0491 0.02279 0.01438 -0.0891 0.4238 0.5330
7.500 1.0733 0.02306 0.01473 -0.0886 0.4210 0.5362
7.750 1.0978 0.02331 0.01502 -0.0882 0.4183 0.5398
8.000 1.1232 0.02352 0.01525 -0.0879 0.4157 0.5437
8.250 1.1505 0.02373 0.01542 -0.0879 0.4132 0.5475
8.500 1.1762 0.02398 0.01572 -0.0877 0.4108 0.5506
8.750 1.1920 0.02441 0.01632 -0.0859 0.4078 0.5534
9.000 1.2083 0.02481 0.01685 -0.0842 0.4045 0.5565
9.250 1.2243 0.02518 0.01730 -0.0825 0.4013 0.5598
9.500 1.2389 0.02551 0.01767 -0.0804 0.3983 0.5636
9.750 1.2587 0.02577 0.01792 -0.0793 0.3954 0.5676
10.000 1.2822 0.02605 0.01817 -0.0787 0.3925 0.5714
10.250 1.2854 0.02691 0.01925 -0.0755 0.3885 0.5742
10.500 1.2937 0.02772 0.02019 -0.0732 0.3843 0.5773
10.750 1.3059 0.02842 0.02097 -0.0715 0.3804 0.5807
11.000 1.3248 0.02889 0.02144 -0.0706 0.3769 0.5845
11.250 1.3391 0.02964 0.02221 -0.0694 0.3731 0.5885
11.500 1.3366 0.03132 0.02405 -0.0671 0.3679 0.5920
11.750 1.3415 0.03267 0.02550 -0.0655 0.3625 0.5954
12.000 1.3579 0.03333 0.02616 -0.0647 0.3578 0.5992
12.250 1.3539 0.03555 0.02855 -0.0631 0.3522 0.6025
12.500 1.3515 0.03783 0.03095 -0.0618 0.3462 0.6060
12.750 1.3620 0.03912 0.03224 -0.0611 0.3412 0.6100
13.000 1.3598 0.04160 0.03480 -0.0602 0.3356 0.6135
13.250 1.3511 0.04476 0.03808 -0.0593 0.3288 0.6167
13.500 1.3593 0.04631 0.03966 -0.0587 0.3232 0.6202
13.750 1.3432 0.05036 0.04388 -0.0579 0.3161 0.6231
14.000 1.3383 0.05340 0.04699 -0.0574 0.3089 0.6267
14.250 1.3352 0.05637 0.05001 -0.0571 0.3020 0.6307
14.500 1.3210 0.06065 0.05438 -0.0569 0.2936 0.6342
14.750 1.3221 0.06332 0.05704 -0.0567 0.2862 0.6383
15.000 1.3078 0.06782 0.06163 -0.0567 0.2772 0.6412
15.250 1.3064 0.07081 0.06466 -0.0567 0.2692 0.6446
15.500 1.2978 0.07475 0.06866 -0.0568 0.2599 0.6479
15.750 1.2924 0.07838 0.07232 -0.0569 0.2512 0.6517
16.000 1.2910 0.08151 0.07544 -0.0571 0.2419 0.6562
16.250 1.2820 0.08570 0.07966 -0.0575 0.2324 0.6602
16.500 1.2816 0.08877 0.08270 -0.0577 0.2233 0.6645
16.750 1.2746 0.09273 0.08671 -0.0582 0.2135 0.6682
17.000 1.2714 0.09625 0.09024 -0.0586 0.2044 0.6726
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