AH 93-W-257 (ah93w257-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
|---|---|
|
Airfoil: AH 93-W-257 (ah93w257-il) Reynolds number: 200,000 Max Cl/Cd: 49.58 at α=10.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ah93w257-il-200000.txt Download as CSV file: xf-ah93w257-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: AH 93-W-257
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
------ -------- --------- --------- -------- -------- --------
-19.750 -1.1309 0.10207 0.09611 -0.0289 1.0000 0.1209
-19.500 -1.1437 0.09704 0.09088 -0.0309 1.0000 0.1233
-19.250 -1.1202 0.09735 0.09134 -0.0305 1.0000 0.1263
-19.000 -1.1112 0.09548 0.08950 -0.0312 1.0000 0.1293
-18.750 -1.1116 0.09228 0.08622 -0.0323 1.0000 0.1325
-18.500 -1.1090 0.08957 0.08345 -0.0332 1.0000 0.1358
-18.250 -1.0926 0.08881 0.08282 -0.0333 1.0000 0.1394
-18.000 -1.0916 0.08586 0.07984 -0.0343 1.0000 0.1435
-17.750 -1.0886 0.08324 0.07719 -0.0350 1.0000 0.1479
-17.500 -1.0775 0.08177 0.07584 -0.0354 1.0000 0.1527
-17.250 -1.0823 0.07811 0.07209 -0.0366 1.0000 0.1581
-17.000 -1.0694 0.07693 0.07106 -0.0367 1.0000 0.1636
-16.750 -1.0728 0.07353 0.06762 -0.0378 1.0000 0.1703
-16.500 -1.0648 0.07173 0.06595 -0.0382 1.0000 0.1771
-16.250 -1.0743 0.06767 0.06181 -0.0394 1.0000 0.1852
-16.000 -1.0639 0.06620 0.06052 -0.0396 1.0000 0.1931
-15.750 -1.0701 0.06268 0.05697 -0.0406 1.0000 0.2020
-15.500 -1.0683 0.06018 0.05455 -0.0412 1.0000 0.2109
-15.250 -1.0642 0.05800 0.05243 -0.0417 1.0000 0.2197
-15.000 -1.0785 0.05373 0.04808 -0.0429 1.0000 0.2293
-14.750 -1.0598 0.05321 0.04773 -0.0429 1.0000 0.2374
-14.500 -1.0725 0.04930 0.04374 -0.0439 1.0000 0.2467
-14.250 -1.0544 0.04870 0.04327 -0.0440 1.0000 0.2545
-14.000 -1.0646 0.04522 0.03972 -0.0448 1.0000 0.2632
-13.750 -1.0436 0.04487 0.03950 -0.0449 1.0000 0.2702
-13.500 -1.0614 0.04088 0.03541 -0.0458 1.0000 0.2788
-13.250 -1.0290 0.04152 0.03622 -0.0459 1.0000 0.2849
-13.000 -1.0481 0.03768 0.03232 -0.0468 1.0000 0.2934
-12.750 -0.9961 0.03836 0.03290 -0.0504 0.8770 0.3002
-12.500 -0.9959 0.03647 0.03078 -0.0504 0.8399 0.3076
-12.250 -0.9928 0.03488 0.02903 -0.0502 0.8172 0.3141
-12.000 -0.9644 0.03534 0.02947 -0.0500 0.7993 0.3193
-11.750 -0.9884 0.03153 0.02539 -0.0504 0.7863 0.3279
-11.500 -0.9540 0.03228 0.02618 -0.0501 0.7737 0.3326
-11.250 -0.9268 0.03258 0.02644 -0.0500 0.7636 0.3377
-11.000 -0.9606 0.02839 0.02202 -0.0502 0.7545 0.3466
-10.750 -0.9120 0.02987 0.02355 -0.0502 0.7461 0.3505
-10.500 -0.8813 0.03035 0.02404 -0.0502 0.7385 0.3553
-10.250 -0.9013 0.02669 0.02015 -0.0523 0.7313 0.3647
-10.000 -0.8630 0.02797 0.02150 -0.0509 0.7243 0.3682
-9.750 -0.8281 0.02895 0.02247 -0.0504 0.7179 0.3725
-9.500 -0.8262 0.02577 0.01908 -0.0554 0.7119 0.3831
-9.250 -0.7885 0.02744 0.02088 -0.0531 0.7059 0.3862
-9.000 -0.7491 0.02908 0.02257 -0.0515 0.7005 0.3891
-8.750 -0.7436 0.02542 0.01857 -0.0584 0.6959 0.4010
-8.500 -0.7115 0.02641 0.01966 -0.0566 0.6914 0.4031
-8.250 -0.6780 0.02753 0.02086 -0.0549 0.6864 0.4050
-8.000 -0.6448 0.02850 0.02186 -0.0538 0.6813 0.4072
-7.750 -0.6307 0.02493 0.01794 -0.0612 0.6768 0.4192
-7.500 -0.6002 0.02574 0.01880 -0.0597 0.6727 0.4211
-7.250 -0.5691 0.02677 0.01986 -0.0582 0.6689 0.4228
-7.000 -0.5379 0.02762 0.02079 -0.0570 0.6651 0.4245
-6.750 -0.5149 0.02451 0.01736 -0.0648 0.6611 0.4367
-6.500 -0.4858 0.02515 0.01809 -0.0634 0.6573 0.4385
-6.250 -0.4561 0.02593 0.01891 -0.0621 0.6535 0.4400
-6.000 -0.4262 0.02668 0.01967 -0.0609 0.6500 0.4415
-5.750 -0.3965 0.02749 0.02044 -0.0599 0.6465 0.4430
-5.500 -0.3683 0.02474 0.01743 -0.0674 0.6433 0.4555
-5.250 -0.3400 0.02537 0.01816 -0.0662 0.6400 0.4569
-5.000 -0.3114 0.02604 0.01890 -0.0651 0.6366 0.4582
-4.750 -0.2825 0.02669 0.01959 -0.0642 0.6333 0.4595
-4.500 -0.2533 0.02740 0.02032 -0.0631 0.6301 0.4608
-4.250 -0.2196 0.02487 0.01748 -0.0708 0.6269 0.4738
-4.000 -0.1922 0.02543 0.01807 -0.0696 0.6240 0.4751
-3.750 -0.1647 0.02616 0.01882 -0.0685 0.6210 0.4762
-3.500 -0.1370 0.02681 0.01957 -0.0675 0.6183 0.4773
-3.250 -0.1092 0.02753 0.02036 -0.0664 0.6153 0.4784
-3.000 -0.0812 0.02821 0.02109 -0.0655 0.6122 0.4797
-2.750 -0.0438 0.02574 0.01839 -0.0735 0.6090 0.4931
-2.500 -0.0170 0.02625 0.01895 -0.0723 0.6061 0.4942
-2.250 0.0101 0.02683 0.01955 -0.0712 0.6033 0.4953
-2.000 0.0375 0.02743 0.02015 -0.0701 0.6009 0.4963
-1.750 0.0646 0.02814 0.02086 -0.0693 0.5984 0.4975
-1.500 0.0914 0.02867 0.02147 -0.0687 0.5959 0.4989
-1.250 0.1322 0.02665 0.01930 -0.0765 0.5929 0.5124
-1.000 0.1578 0.02714 0.01988 -0.0755 0.5898 0.5135
-0.750 0.1838 0.02760 0.02040 -0.0745 0.5867 0.5145
-0.500 0.2102 0.02804 0.02088 -0.0737 0.5838 0.5156
-0.250 0.2369 0.02850 0.02136 -0.0728 0.5814 0.5169
0.000 0.2636 0.02900 0.02188 -0.0720 0.5792 0.5183
0.250 0.2906 0.02952 0.02239 -0.0713 0.5771 0.5200
0.500 0.3190 0.02984 0.02271 -0.0718 0.5748 0.5236
0.750 0.3582 0.02839 0.02123 -0.0780 0.5715 0.5340
1.000 0.3822 0.02892 0.02186 -0.0770 0.5681 0.5353
1.250 0.4069 0.02944 0.02246 -0.0760 0.5651 0.5367
1.500 0.4318 0.02994 0.02302 -0.0750 0.5625 0.5382
1.750 0.4582 0.03029 0.02340 -0.0745 0.5600 0.5403
2.000 0.5072 0.02871 0.02165 -0.0824 0.5577 0.5527
2.250 0.5331 0.02904 0.02199 -0.0815 0.5555 0.5539
2.500 0.5587 0.02962 0.02257 -0.0806 0.5533 0.5552
2.750 0.5787 0.03032 0.02345 -0.0792 0.5501 0.5567
3.000 0.5993 0.03101 0.02428 -0.0781 0.5466 0.5584
3.250 0.6234 0.03143 0.02479 -0.0776 0.5433 0.5609
3.500 0.6559 0.03128 0.02464 -0.0793 0.5403 0.5659
3.750 0.6993 0.03047 0.02373 -0.0844 0.5377 0.5740
4.000 0.7246 0.03075 0.02406 -0.0835 0.5356 0.5755
4.250 0.7504 0.03106 0.02439 -0.0825 0.5337 0.5771
4.500 0.7767 0.03153 0.02486 -0.0818 0.5316 0.5789
4.750 0.7905 0.03245 0.02602 -0.0805 0.5268 0.5815
5.000 0.8146 0.03291 0.02658 -0.0810 0.5227 0.5855
5.250 0.8603 0.03229 0.02589 -0.0866 0.5195 0.5943
5.500 0.8850 0.03241 0.02607 -0.0856 0.5169 0.5959
5.750 0.9114 0.03249 0.02618 -0.0848 0.5148 0.5976
6.000 0.9394 0.03254 0.02625 -0.0842 0.5129 0.5995
6.250 0.9697 0.03270 0.02639 -0.0842 0.5108 0.6020
6.500 0.9734 0.03416 0.02814 -0.0824 0.5041 0.6051
6.750 1.0058 0.03417 0.02819 -0.0845 0.5001 0.6108
7.000 1.0447 0.03372 0.02771 -0.0872 0.4971 0.6163
7.250 1.0745 0.03340 0.02741 -0.0868 0.4948 0.6181
7.500 1.1069 0.03299 0.02699 -0.0866 0.4927 0.6200
7.750 1.1350 0.03300 0.02703 -0.0863 0.4896 0.6222
8.000 1.1365 0.03425 0.02853 -0.0837 0.4825 0.6247
8.250 1.1678 0.03390 0.02822 -0.0844 0.4785 0.6286
8.500 1.2222 0.03276 0.02694 -0.0893 0.4754 0.6361
8.750 1.2622 0.03170 0.02584 -0.0902 0.4727 0.6384
9.000 1.2746 0.03216 0.02646 -0.0881 0.4670 0.6401
9.250 1.2890 0.03233 0.02675 -0.0861 0.4610 0.6420
9.500 1.3231 0.03148 0.02590 -0.0863 0.4567 0.6445
9.750 1.3695 0.03024 0.02453 -0.0881 0.4527 0.6482
10.000 1.3733 0.03095 0.02546 -0.0856 0.4453 0.6520
10.250 1.4116 0.03012 0.02457 -0.0878 0.4384 0.6572
10.500 1.4477 0.02920 0.02357 -0.0885 0.4326 0.6597
10.750 1.4430 0.02991 0.02451 -0.0842 0.4249 0.6614
11.000 1.4632 0.02952 0.02413 -0.0826 0.4182 0.6637
11.250 1.4646 0.02988 0.02458 -0.0789 0.4115 0.6662
11.500 1.4637 0.03080 0.02562 -0.0759 0.4033 0.6691
11.750 1.4834 0.03095 0.02574 -0.0754 0.3952 0.6727
12.000 1.4789 0.03282 0.02773 -0.0740 0.3851 0.6758
12.250 1.4876 0.03420 0.02910 -0.0740 0.3746 0.6791
12.500 1.4899 0.03566 0.03058 -0.0727 0.3636 0.6809
12.750 1.4770 0.03872 0.03377 -0.0713 0.3515 0.6827
13.000 1.4714 0.04127 0.03635 -0.0703 0.3390 0.6847
13.250 1.4667 0.04383 0.03889 -0.0693 0.3255 0.6869
13.500 1.4582 0.04689 0.04192 -0.0686 0.3109 0.6891
13.750 1.4457 0.05053 0.04555 -0.0681 0.2956 0.6912
14.000 1.4345 0.05415 0.04914 -0.0677 0.2798 0.6933
14.250 1.4243 0.05788 0.05280 -0.0677 0.2638 0.6955
14.500 1.4141 0.06180 0.05663 -0.0678 0.2478 0.6977
14.750 1.4041 0.06579 0.06055 -0.0680 0.2323 0.6996
15.000 1.3933 0.06969 0.06440 -0.0679 0.2176 0.7010
15.250 1.3824 0.07371 0.06838 -0.0678 0.2038 0.7025
15.500 1.3722 0.07772 0.07235 -0.0678 0.1905 0.7042
15.750 1.3627 0.08177 0.07635 -0.0680 0.1780 0.7061
16.000 1.3533 0.08590 0.08042 -0.0683 0.1662 0.7080
16.500 1.3381 0.09410 0.08854 -0.0695 0.1440 0.7121
16.750 1.3328 0.09808 0.09248 -0.0703 0.1338 0.7142
17.000 1.3275 0.10213 0.09648 -0.0713 0.1245 0.7163
|
Polar data table (+)
Polar graphs
<< Back to AH 93-W-257 (ah93w257-il)