AH 93-W-215 (ah93w215-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: AH 93-W-215 (ah93w215-il) Reynolds number: 500,000 Max Cl/Cd: 93.79 at α=8.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ah93w215-il-500000.txt Download as CSV file: xf-ah93w215-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: AH 93-W-215
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.9831 0.09198 0.08771 -0.0663 1.0000 0.0416
-19.500 -0.9906 0.08750 0.08313 -0.0686 1.0000 0.0420
-19.250 -0.9980 0.08310 0.07861 -0.0707 1.0000 0.0424
-19.000 -1.0067 0.07852 0.07390 -0.0730 1.0000 0.0429
-18.750 -1.0122 0.07456 0.06981 -0.0748 1.0000 0.0434
-18.500 -1.0090 0.07219 0.06747 -0.0753 1.0000 0.0440
-18.250 -1.0091 0.06919 0.06444 -0.0764 1.0000 0.0445
-18.000 -1.0091 0.06619 0.06141 -0.0776 1.0000 0.0452
-17.750 -1.0089 0.06327 0.05844 -0.0786 1.0000 0.0457
-17.500 -1.0085 0.06039 0.05549 -0.0796 1.0000 0.0463
-17.250 -1.0085 0.05752 0.05254 -0.0806 1.0000 0.0471
-17.000 -1.0079 0.05480 0.04972 -0.0814 1.0000 0.0477
-16.750 -1.0068 0.05218 0.04699 -0.0821 1.0000 0.0483
-16.500 -1.0043 0.04997 0.04477 -0.0821 1.0000 0.0490
-16.250 -1.0017 0.04780 0.04260 -0.0822 1.0000 0.0498
-16.000 -0.9982 0.04572 0.04050 -0.0824 1.0000 0.0505
-15.750 -0.9940 0.04374 0.03849 -0.0824 1.0000 0.0513
-15.500 -0.9895 0.04185 0.03655 -0.0824 1.0000 0.0521
-15.250 -0.9846 0.04009 0.03473 -0.0821 1.0000 0.0529
-15.000 -0.9788 0.03844 0.03301 -0.0818 1.0000 0.0537
-14.750 -0.9706 0.03667 0.03120 -0.0821 0.9997 0.0547
-14.500 -0.9535 0.03446 0.02903 -0.0834 0.9677 0.0559
-14.250 -0.8485 0.03174 0.02613 -0.1028 0.9035 0.0589
-14.000 -0.7637 0.02977 0.02372 -0.1181 0.8190 0.0620
-13.750 -0.7382 0.02869 0.02241 -0.1207 0.7843 0.0635
-13.500 -0.7134 0.02770 0.02126 -0.1228 0.7652 0.0652
-13.000 -0.6757 0.02567 0.01900 -0.1247 0.7406 0.0685
-12.750 -0.6575 0.02471 0.01797 -0.1254 0.7315 0.0703
-12.500 -0.6393 0.02391 0.01711 -0.1256 0.7242 0.0720
-12.250 -0.6196 0.02324 0.01634 -0.1259 0.7172 0.0741
-12.000 -0.6036 0.02234 0.01536 -0.1259 0.7109 0.0760
-11.750 -0.5879 0.02155 0.01458 -0.1256 0.7057 0.0783
-11.500 -0.5706 0.02093 0.01391 -0.1251 0.7005 0.0805
-11.250 -0.5512 0.02042 0.01330 -0.1248 0.6953 0.0827
-11.000 -0.5377 0.01962 0.01248 -0.1240 0.6901 0.0854
-10.750 -0.5216 0.01906 0.01191 -0.1232 0.6859 0.0880
-10.500 -0.5043 0.01860 0.01140 -0.1222 0.6818 0.0907
-10.250 -0.4904 0.01801 0.01079 -0.1208 0.6779 0.0934
-10.000 -0.4760 0.01748 0.01025 -0.1195 0.6740 0.0965
-9.750 -0.4577 0.01712 0.00983 -0.1185 0.6701 0.0998
-9.500 -0.4423 0.01669 0.00936 -0.1171 0.6666 0.1031
-9.250 -0.4302 0.01620 0.00891 -0.1150 0.6634 0.1069
-9.000 -0.4147 0.01586 0.00855 -0.1132 0.6598 0.1106
-8.750 -0.4015 0.01547 0.00813 -0.1111 0.6565 0.1148
-8.500 -0.3885 0.01510 0.00777 -0.1088 0.6533 0.1192
-8.250 -0.3705 0.01490 0.00750 -0.1073 0.6501 0.1238
-8.000 -0.3582 0.01457 0.00719 -0.1048 0.6470 0.1288
-7.750 -0.3451 0.01434 0.00698 -0.1022 0.6445 0.1343
-7.500 -0.3327 0.01413 0.00677 -0.0994 0.6415 0.1397
-7.250 -0.3185 0.01389 0.00656 -0.0969 0.6384 0.1462
-7.000 -0.3004 0.01370 0.00635 -0.0952 0.6355 0.1530
-6.750 -0.2832 0.01346 0.00614 -0.0934 0.6328 0.1613
-6.500 -0.2633 0.01329 0.00595 -0.0920 0.6300 0.1699
-6.250 -0.2422 0.01314 0.00581 -0.0909 0.6271 0.1800
-6.000 -0.2243 0.01289 0.00562 -0.0891 0.6248 0.1909
-5.750 -0.2047 0.01267 0.00545 -0.0876 0.6221 0.2031
-5.500 -0.1846 0.01246 0.00528 -0.0862 0.6193 0.2172
-5.250 -0.1643 0.01223 0.00511 -0.0848 0.6166 0.2333
-5.000 -0.1441 0.01199 0.00493 -0.0834 0.6141 0.2529
-4.750 -0.1242 0.01173 0.00476 -0.0820 0.6116 0.2772
-4.500 -0.1028 0.01154 0.00464 -0.0810 0.6087 0.3075
-4.250 -0.0835 0.01127 0.00453 -0.0794 0.6062 0.3414
-4.000 -0.0641 0.01102 0.00442 -0.0779 0.6039 0.3759
-3.750 -0.0432 0.01082 0.00435 -0.0765 0.6014 0.4084
-3.500 -0.0210 0.01068 0.00429 -0.0754 0.5988 0.4364
-3.250 0.0026 0.01058 0.00423 -0.0745 0.5961 0.4602
-3.000 0.0269 0.01051 0.00419 -0.0737 0.5935 0.4803
-2.750 0.0520 0.01049 0.00417 -0.0731 0.5910 0.4979
-2.500 0.0791 0.01056 0.00424 -0.0730 0.5880 0.5134
-2.250 0.1030 0.01050 0.00422 -0.0721 0.5860 0.5267
-2.000 0.1274 0.01047 0.00421 -0.0713 0.5834 0.5398
-1.750 0.1521 0.01043 0.00421 -0.0706 0.5807 0.5510
-1.500 0.1779 0.01044 0.00419 -0.0701 0.5780 0.5621
-1.250 0.2033 0.01040 0.00419 -0.0695 0.5754 0.5727
-1.000 0.2297 0.01043 0.00416 -0.0691 0.5727 0.5831
-0.750 0.2572 0.01048 0.00422 -0.0690 0.5698 0.5925
-0.500 0.2827 0.01052 0.00426 -0.0685 0.5674 0.6020
-0.250 0.3067 0.01047 0.00428 -0.0676 0.5648 0.6107
0.000 0.3315 0.01047 0.00429 -0.0669 0.5619 0.6204
0.250 0.3567 0.01045 0.00429 -0.0662 0.5590 0.6295
0.500 0.3822 0.01045 0.00430 -0.0657 0.5562 0.6394
0.750 0.4080 0.01046 0.00430 -0.0652 0.5535 0.6496
1.000 0.4359 0.01058 0.00440 -0.0652 0.5503 0.6611
1.250 0.4589 0.01056 0.00445 -0.0641 0.5479 0.6709
1.500 0.4822 0.01054 0.00449 -0.0631 0.5448 0.6800
1.750 0.5065 0.01054 0.00450 -0.0623 0.5417 0.6886
2.000 0.5312 0.01052 0.00452 -0.0616 0.5386 0.6972
2.250 0.5562 0.01054 0.00452 -0.0609 0.5357 0.7061
2.500 0.5837 0.01062 0.00459 -0.0609 0.5325 0.7143
2.750 0.6065 0.01064 0.00467 -0.0598 0.5295 0.7237
3.000 0.6284 0.01064 0.00472 -0.0585 0.5261 0.7327
3.250 0.6511 0.01063 0.00476 -0.0574 0.5226 0.7420
3.500 0.6743 0.01065 0.00478 -0.0564 0.5193 0.7518
3.750 0.6989 0.01068 0.00483 -0.0557 0.5160 0.7612
4.000 0.7231 0.01078 0.00492 -0.0549 0.5124 0.7712
4.250 0.7427 0.01078 0.00503 -0.0532 0.5090 0.7809
4.500 0.7627 0.01081 0.00508 -0.0516 0.5052 0.7918
4.750 0.7839 0.01082 0.00515 -0.0502 0.5016 0.8013
5.250 0.8274 0.01097 0.00532 -0.0477 0.4940 0.8218
5.500 0.8420 0.01098 0.00539 -0.0449 0.4899 0.8331
5.750 0.8577 0.01098 0.00547 -0.0424 0.4857 0.8436
6.000 0.8747 0.01102 0.00551 -0.0402 0.4817 0.8546
6.250 0.8948 0.01114 0.00562 -0.0386 0.4774 0.8657
6.500 0.9086 0.01119 0.00578 -0.0358 0.4733 0.8774
6.750 0.9229 0.01125 0.00589 -0.0331 0.4686 0.8902
7.000 0.9413 0.01134 0.00600 -0.0313 0.4641 0.9029
7.250 0.9642 0.01146 0.00614 -0.0305 0.4593 0.9157
7.500 0.9890 0.01156 0.00634 -0.0302 0.4538 0.9295
7.750 1.0241 0.01172 0.00653 -0.0321 0.4479 0.9419
8.000 1.0660 0.01197 0.00678 -0.0356 0.4416 0.9526
8.250 1.1133 0.01222 0.00710 -0.0402 0.4348 0.9602
8.500 1.1584 0.01252 0.00738 -0.0444 0.4279 0.9675
8.750 1.2014 0.01281 0.00771 -0.0481 0.4210 0.9758
9.000 1.2311 0.01319 0.00809 -0.0492 0.4136 1.0000
9.250 1.2437 0.01351 0.00837 -0.0470 0.4075 1.0000
9.500 1.2586 0.01381 0.00870 -0.0451 0.4007 1.0000
9.750 1.2713 0.01422 0.00908 -0.0430 0.3941 1.0000
10.000 1.2857 0.01464 0.00953 -0.0413 0.3877 1.0000
10.250 1.2990 0.01512 0.01002 -0.0395 0.3807 1.0000
10.500 1.3095 0.01577 0.01062 -0.0374 0.3742 1.0000
10.750 1.3235 0.01633 0.01124 -0.0360 0.3672 1.0000
11.000 1.3320 0.01717 0.01204 -0.0340 0.3594 1.0000
11.250 1.3432 0.01798 0.01289 -0.0325 0.3521 1.0000
11.500 1.3520 0.01899 0.01390 -0.0309 0.3445 1.0000
11.750 1.3607 0.02008 0.01499 -0.0296 0.3376 1.0000
12.000 1.3685 0.02131 0.01625 -0.0283 0.3292 1.0000
12.250 1.3737 0.02276 0.01768 -0.0270 0.3213 1.0000
12.500 1.3803 0.02420 0.01915 -0.0259 0.3129 1.0000
12.750 1.3834 0.02589 0.02083 -0.0246 0.3050 1.0000
13.000 1.3894 0.02745 0.02242 -0.0237 0.2970 1.0000
13.250 1.3904 0.02936 0.02431 -0.0225 0.2893 1.0000
13.500 1.3961 0.03098 0.02597 -0.0216 0.2815 1.0000
13.750 1.3944 0.03315 0.02810 -0.0204 0.2738 1.0000
14.000 1.3996 0.03489 0.02989 -0.0197 0.2662 1.0000
14.250 1.3980 0.03714 0.03210 -0.0186 0.2585 1.0000
14.500 1.4026 0.03901 0.03402 -0.0180 0.2512 1.0000
14.750 1.4011 0.04137 0.03637 -0.0171 0.2435 1.0000
15.000 1.4042 0.04341 0.03844 -0.0166 0.2360 1.0000
15.250 1.4012 0.04604 0.04104 -0.0158 0.2278 1.0000
15.500 1.4045 0.04814 0.04317 -0.0154 0.2204 1.0000
15.750 1.4014 0.05085 0.04586 -0.0148 0.2128 1.0000
16.000 1.4035 0.05312 0.04816 -0.0145 0.2054 1.0000
16.250 1.4002 0.05597 0.05099 -0.0141 0.1980 1.0000
16.500 1.4025 0.05830 0.05335 -0.0139 0.1913 1.0000
16.750 1.3985 0.06129 0.05633 -0.0136 0.1837 1.0000
17.000 1.3990 0.06386 0.05892 -0.0134 0.1769 1.0000
17.250 1.3960 0.06684 0.06191 -0.0133 0.1701 1.0000
17.500 1.3950 0.06964 0.06472 -0.0133 0.1636 1.0000
17.750 1.3915 0.07274 0.06783 -0.0134 0.1569 1.0000
18.000 1.3887 0.07579 0.07088 -0.0134 0.1502 1.0000
18.250 1.3856 0.07897 0.07407 -0.0136 0.1441 1.0000
18.500 1.3825 0.08214 0.07725 -0.0139 0.1383 1.0000
18.750 1.3793 0.08537 0.08050 -0.0142 0.1320 1.0000
19.000 1.3742 0.08884 0.08398 -0.0146 0.1263 1.0000
19.250 1.3719 0.09204 0.08721 -0.0151 0.1208 1.0000
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