AH 93-W-300 (ah93w300-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: AH 93-W-300 (ah93w300-il) Reynolds number: 200,000 Max Cl/Cd: 41.01 at α=6.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ah93w300-il-200000-n5.txt Download as CSV file: xf-ah93w300-il-200000-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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.250 -0.8614 0.10137 0.09473 -0.0472 1.0000 0.1481
-18.000 -0.8569 0.09887 0.09228 -0.0480 1.0000 0.1522
-17.750 -0.8589 0.09553 0.08893 -0.0490 1.0000 0.1572
-17.500 -0.8583 0.09257 0.08598 -0.0498 1.0000 0.1618
-17.250 -0.8579 0.08961 0.08303 -0.0506 1.0000 0.1668
-17.000 -0.8607 0.08626 0.07966 -0.0515 1.0000 0.1719
-16.750 -0.8582 0.08366 0.07709 -0.0521 1.0000 0.1769
-16.500 -0.8640 0.08004 0.07342 -0.0529 1.0000 0.1824
-16.250 -0.8591 0.07782 0.07126 -0.0533 1.0000 0.1872
-16.000 -0.8661 0.07417 0.06754 -0.0540 1.0000 0.1930
-15.750 -0.8608 0.07208 0.06551 -0.0543 1.0000 0.1978
-15.500 -0.8642 0.06903 0.06244 -0.0547 1.0000 0.2035
-15.250 -0.8640 0.06644 0.05986 -0.0550 1.0000 0.2084
-15.000 -0.8622 0.06413 0.05759 -0.0551 1.0000 0.2136
-14.750 -0.8705 0.06077 0.05416 -0.0552 1.0000 0.2193
-14.500 -0.8635 0.05924 0.05271 -0.0550 1.0000 0.2239
-14.250 -0.8687 0.05649 0.04993 -0.0548 1.0000 0.2295
-14.000 -0.8706 0.05427 0.04772 -0.0542 1.0000 0.2343
-13.750 -0.8697 0.05252 0.04603 -0.0535 1.0000 0.2391
-13.500 -0.8802 0.04989 0.04336 -0.0525 1.0000 0.2445
-13.250 -0.8600 0.04789 0.04140 -0.0549 0.9898 0.2496
-13.000 -0.8449 0.04537 0.03886 -0.0577 0.9734 0.2556
-12.750 -0.8291 0.04282 0.03623 -0.0608 0.9567 0.2616
-12.500 -0.8044 0.04117 0.03459 -0.0637 0.9395 0.2672
-12.250 -0.7949 0.03834 0.03162 -0.0664 0.9197 0.2740
-12.000 -0.7741 0.03708 0.03037 -0.0678 0.8997 0.2792
-11.750 -0.7634 0.03532 0.02852 -0.0686 0.8799 0.2852
-11.500 -0.7607 0.03317 0.02621 -0.0688 0.8610 0.2910
-11.250 -0.7440 0.03242 0.02548 -0.0686 0.8449 0.2953
-11.000 -0.7356 0.03102 0.02398 -0.0683 0.8295 0.3004
-10.750 -0.7354 0.02908 0.02186 -0.0678 0.8155 0.3057
-10.500 -0.7166 0.02857 0.02137 -0.0674 0.8024 0.3095
-10.250 -0.7037 0.02764 0.02039 -0.0670 0.7909 0.3139
-10.000 -0.6973 0.02628 0.01892 -0.0664 0.7789 0.3190
-9.750 -0.6869 0.02524 0.01777 -0.0657 0.7678 0.3234
-9.500 -0.6690 0.02472 0.01726 -0.0652 0.7579 0.3273
-9.250 -0.6571 0.02389 0.01639 -0.0644 0.7472 0.3317
-9.000 -0.6534 0.02296 0.01531 -0.0626 0.7371 0.3363
-8.750 -0.6401 0.02237 0.01465 -0.0617 0.7284 0.3402
-8.500 -0.6194 0.02204 0.01434 -0.0613 0.7191 0.3438
-8.250 -0.5998 0.02164 0.01388 -0.0609 0.7095 0.3479
-8.000 -0.5800 0.02121 0.01331 -0.0606 0.7009 0.3523
-7.750 -0.5587 0.02079 0.01282 -0.0604 0.6927 0.3564
-7.500 -0.5329 0.02062 0.01269 -0.0603 0.6840 0.3596
-7.250 -0.5077 0.02043 0.01246 -0.0602 0.6754 0.3633
-7.000 -0.4827 0.02019 0.01213 -0.0603 0.6674 0.3674
-6.750 -0.4578 0.01988 0.01174 -0.0604 0.6588 0.3716
-6.500 -0.4312 0.01968 0.01150 -0.0605 0.6504 0.3752
-6.250 -0.4036 0.01959 0.01138 -0.0606 0.6427 0.3785
-6.000 -0.3760 0.01944 0.01124 -0.0608 0.6349 0.3821
-5.750 -0.3486 0.01926 0.01101 -0.0611 0.6263 0.3861
-5.500 -0.3211 0.01907 0.01068 -0.0615 0.6182 0.3903
-5.250 -0.2928 0.01895 0.01051 -0.0617 0.6110 0.3937
-5.000 -0.2640 0.01887 0.01048 -0.0620 0.6031 0.3968
-4.750 -0.2353 0.01880 0.01039 -0.0623 0.5948 0.4004
-4.500 -0.2066 0.01871 0.01022 -0.0626 0.5874 0.4044
-4.250 -0.1774 0.01859 0.01002 -0.0631 0.5804 0.4084
-4.000 -0.1482 0.01846 0.00985 -0.0636 0.5726 0.4119
-3.750 -0.1192 0.01844 0.00984 -0.0638 0.5649 0.4150
-3.500 -0.0900 0.01845 0.00980 -0.0641 0.5581 0.4183
-3.250 -0.0603 0.01840 0.00976 -0.0645 0.5513 0.4220
-3.000 -0.0307 0.01834 0.00966 -0.0650 0.5439 0.4259
-2.750 -0.0010 0.01828 0.00948 -0.0656 0.5369 0.4299
-2.500 0.0284 0.01827 0.00945 -0.0659 0.5305 0.4330
-2.250 0.0579 0.01827 0.00951 -0.0662 0.5237 0.4359
-2.000 0.0873 0.01829 0.00952 -0.0665 0.5167 0.4393
-1.750 0.1168 0.01832 0.00949 -0.0668 0.5103 0.4430
-1.500 0.1467 0.01833 0.00945 -0.0673 0.5043 0.4468
-1.250 0.1768 0.01830 0.00938 -0.0679 0.4978 0.4504
-1.000 0.2061 0.01831 0.00938 -0.0682 0.4913 0.4535
-0.750 0.2349 0.01839 0.00945 -0.0683 0.4856 0.4566
-0.500 0.2642 0.01846 0.00953 -0.0686 0.4802 0.4598
-0.250 0.2937 0.01851 0.00960 -0.0689 0.4742 0.4633
0.000 0.3230 0.01856 0.00961 -0.0692 0.4681 0.4668
0.250 0.3524 0.01863 0.00960 -0.0696 0.4626 0.4706
0.500 0.3820 0.01870 0.00960 -0.0700 0.4576 0.4741
0.750 0.4104 0.01876 0.00975 -0.0701 0.4520 0.4770
1.000 0.4387 0.01885 0.00988 -0.0702 0.4462 0.4800
1.250 0.4668 0.01897 0.00997 -0.0702 0.4408 0.4832
1.500 0.4951 0.01912 0.01006 -0.0704 0.4358 0.4868
1.750 0.5238 0.01921 0.01019 -0.0706 0.4304 0.4906
2.000 0.5521 0.01931 0.01027 -0.0708 0.4246 0.4943
2.250 0.5799 0.01943 0.01032 -0.0709 0.4192 0.4974
2.750 0.6333 0.01970 0.01068 -0.0705 0.4090 0.5036
3.000 0.6597 0.01985 0.01088 -0.0702 0.4033 0.5070
3.250 0.6855 0.02003 0.01103 -0.0699 0.3979 0.5105
3.500 0.7113 0.02023 0.01117 -0.0697 0.3931 0.5139
3.750 0.7373 0.02039 0.01136 -0.0695 0.3878 0.5175
4.000 0.7627 0.02057 0.01154 -0.0692 0.3823 0.5210
4.250 0.7862 0.02076 0.01173 -0.0685 0.3770 0.5242
4.500 0.8088 0.02100 0.01195 -0.0677 0.3722 0.5274
4.750 0.8318 0.02120 0.01226 -0.0669 0.3670 0.5306
5.000 0.8532 0.02144 0.01253 -0.0659 0.3615 0.5338
5.250 0.8713 0.02170 0.01279 -0.0644 0.3566 0.5372
5.500 0.8889 0.02200 0.01305 -0.0628 0.3520 0.5410
5.750 0.9076 0.02229 0.01340 -0.0614 0.3468 0.5447
6.000 0.9269 0.02266 0.01376 -0.0603 0.3415 0.5480
6.250 0.9455 0.02308 0.01417 -0.0591 0.3365 0.5511
6.500 0.9645 0.02352 0.01465 -0.0581 0.3318 0.5543
6.750 0.9834 0.02398 0.01521 -0.0570 0.3266 0.5577
7.000 1.0009 0.02452 0.01578 -0.0559 0.3214 0.5614
7.250 1.0177 0.02513 0.01636 -0.0548 0.3167 0.5652
7.500 1.0358 0.02573 0.01701 -0.0539 0.3118 0.5691
7.750 1.0528 0.02639 0.01771 -0.0530 0.3066 0.5728
8.000 1.0682 0.02715 0.01844 -0.0519 0.3016 0.5760
8.250 1.0838 0.02793 0.01921 -0.0510 0.2970 0.5792
8.500 1.0992 0.02872 0.02012 -0.0501 0.2919 0.5830
8.750 1.1129 0.02963 0.02108 -0.0491 0.2868 0.5868
9.000 1.1250 0.03067 0.02212 -0.0480 0.2822 0.5907
9.250 1.1395 0.03166 0.02319 -0.0473 0.2774 0.5948
9.500 1.1519 0.03280 0.02437 -0.0465 0.2723 0.5987
9.750 1.1629 0.03404 0.02560 -0.0457 0.2676 0.6025
10.000 1.1745 0.03533 0.02691 -0.0451 0.2630 0.6061
10.250 1.1858 0.03668 0.02831 -0.0445 0.2579 0.6097
10.500 1.1943 0.03818 0.02986 -0.0438 0.2532 0.6138
10.750 1.2032 0.03969 0.03142 -0.0431 0.2489 0.6180
11.000 1.2122 0.04131 0.03314 -0.0426 0.2441 0.6224
11.250 1.2194 0.04308 0.03495 -0.0421 0.2393 0.6268
11.500 1.2257 0.04495 0.03680 -0.0416 0.2352 0.6311
11.750 1.2338 0.04682 0.03876 -0.0413 0.2306 0.6353
12.000 1.2396 0.04891 0.04088 -0.0411 0.2260 0.6394
12.250 1.2443 0.05107 0.04305 -0.0408 0.2219 0.6436
12.500 1.2503 0.05320 0.04530 -0.0407 0.2177 0.6483
12.750 1.2546 0.05555 0.04773 -0.0406 0.2133 0.6532
13.000 1.2580 0.05799 0.05019 -0.0405 0.2094 0.6583
13.250 1.2621 0.06045 0.05271 -0.0405 0.2056 0.6634
13.500 1.2658 0.06304 0.05537 -0.0407 0.2015 0.6682
14.000 1.2711 0.06835 0.06074 -0.0410 0.1942 0.6778
14.250 1.2726 0.07127 0.06380 -0.0413 0.1904 0.6833
14.500 1.2744 0.07413 0.06672 -0.0417 0.1866 0.6892
14.750 1.2758 0.07705 0.06965 -0.0420 0.1834 0.6954
15.000 1.2777 0.08002 0.07269 -0.0425 0.1800 0.7012
15.250 1.2774 0.08326 0.07604 -0.0431 0.1763 0.7065
15.500 1.2785 0.08626 0.07909 -0.0436 0.1730 0.7124
15.750 1.2806 0.08918 0.08203 -0.0442 0.1701 0.7190
16.000 1.2792 0.09269 0.08568 -0.0450 0.1667 0.7258
16.250 1.2794 0.09598 0.08901 -0.0458 0.1634 0.7327
16.500 1.2810 0.09892 0.09200 -0.0465 0.1606 0.7402
16.750 1.2810 0.10221 0.09539 -0.0473 0.1576 0.7483
17.000 1.2784 0.10593 0.09922 -0.0484 0.1543 0.7564
17.250 1.2795 0.10908 0.10242 -0.0494 0.1514 0.7648
17.500 1.2843 0.11161 0.10494 -0.0500 0.1490 0.7745
17.750 1.2790 0.11575 0.10925 -0.0514 0.1458 0.7835
18.000 1.2776 0.11924 0.11284 -0.0526 0.1429 0.7931
18.250 1.2798 0.12215 0.11577 -0.0535 0.1403 0.8049
18.500 1.2810 0.12521 0.11889 -0.0546 0.1378 0.8174
18.750 1.2757 0.12925 0.12307 -0.0560 0.1349 0.8309
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