AH 93-W-215 (ah93w215-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: AH 93-W-215 (ah93w215-il) Reynolds number: 200,000 Max Cl/Cd: 58.83 at α=8.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ah93w215-il-200000-n5.txt Download as CSV file: xf-ah93w215-il-200000-n5.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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.750 -0.7834 0.10879 0.10367 -0.0600 1.0000 0.0472
-18.500 -0.8188 0.09908 0.09370 -0.0653 1.0000 0.0478
-18.250 -0.8450 0.09126 0.08563 -0.0696 1.0000 0.0484
-18.000 -0.8497 0.08723 0.08156 -0.0715 1.0000 0.0489
-17.750 -0.8530 0.08347 0.07777 -0.0733 1.0000 0.0495
-17.500 -0.8577 0.07955 0.07378 -0.0751 1.0000 0.0500
-17.250 -0.8628 0.07563 0.06979 -0.0769 1.0000 0.0507
-17.000 -0.8679 0.07182 0.06589 -0.0785 1.0000 0.0514
-16.750 -0.8729 0.06811 0.06207 -0.0800 1.0000 0.0522
-16.500 -0.8772 0.06460 0.05844 -0.0813 1.0000 0.0530
-16.250 -0.8805 0.06131 0.05500 -0.0824 1.0000 0.0538
-16.000 -0.8809 0.05854 0.05218 -0.0832 1.0000 0.0546
-15.750 -0.8795 0.05608 0.04971 -0.0837 1.0000 0.0553
-15.500 -0.8779 0.05370 0.04730 -0.0841 1.0000 0.0560
-15.250 -0.8765 0.05136 0.04491 -0.0844 1.0000 0.0570
-15.000 -0.8742 0.04920 0.04269 -0.0845 1.0000 0.0579
-14.750 -0.8718 0.04712 0.04052 -0.0845 1.0000 0.0590
-14.500 -0.8551 0.04478 0.03804 -0.0870 0.9973 0.0603
-14.250 -0.8306 0.04213 0.03540 -0.0905 0.9129 0.0616
-14.000 -0.7576 0.03913 0.03211 -0.1049 0.8639 0.0647
-13.750 -0.6962 0.03692 0.02950 -0.1159 0.8214 0.0675
-13.250 -0.6351 0.03389 0.02610 -0.1245 0.7747 0.0717
-13.000 -0.6118 0.03268 0.02471 -0.1266 0.7610 0.0739
-12.750 -0.5940 0.03151 0.02344 -0.1277 0.7502 0.0758
-12.500 -0.5794 0.03046 0.02233 -0.1280 0.7409 0.0776
-12.250 -0.5635 0.02952 0.02126 -0.1282 0.7328 0.0798
-12.000 -0.5473 0.02866 0.02028 -0.1281 0.7257 0.0822
-11.750 -0.5335 0.02774 0.01932 -0.1278 0.7188 0.0842
-11.500 -0.5193 0.02689 0.01841 -0.1274 0.7124 0.0864
-11.250 -0.5038 0.02615 0.01758 -0.1270 0.7070 0.0892
-10.750 -0.4759 0.02469 0.01603 -0.1253 0.6965 0.0942
-10.500 -0.4619 0.02404 0.01532 -0.1243 0.6920 0.0972
-10.250 -0.4460 0.02350 0.01466 -0.1234 0.6881 0.1005
-10.000 -0.4332 0.02285 0.01402 -0.1220 0.6838 0.1034
-9.750 -0.4204 0.02226 0.01343 -0.1205 0.6794 0.1067
-9.500 -0.4057 0.02178 0.01288 -0.1192 0.6753 0.1106
-9.250 -0.3921 0.02128 0.01233 -0.1175 0.6713 0.1143
-9.000 -0.3789 0.02080 0.01180 -0.1159 0.6679 0.1183
-8.750 -0.3645 0.02037 0.01135 -0.1141 0.6644 0.1229
-8.500 -0.3524 0.01991 0.01089 -0.1121 0.6609 0.1271
-8.250 -0.3398 0.01949 0.01048 -0.1099 0.6575 0.1319
-7.750 -0.3144 0.01880 0.00972 -0.1054 0.6509 0.1425
-7.500 -0.3002 0.01856 0.00942 -0.1032 0.6480 0.1489
-7.250 -0.2893 0.01828 0.00918 -0.1004 0.6448 0.1549
-7.000 -0.2762 0.01804 0.00895 -0.0980 0.6416 0.1619
-6.750 -0.2609 0.01778 0.00869 -0.0959 0.6386 0.1692
-6.500 -0.2449 0.01753 0.00845 -0.0939 0.6356 0.1782
-6.250 -0.2282 0.01727 0.00820 -0.0921 0.6328 0.1871
-6.000 -0.2098 0.01706 0.00796 -0.0905 0.6300 0.1981
-5.750 -0.1920 0.01681 0.00773 -0.0889 0.6274 0.2101
-5.500 -0.1752 0.01656 0.00755 -0.0870 0.6244 0.2228
-5.250 -0.1572 0.01633 0.00737 -0.0853 0.6215 0.2376
-5.000 -0.1392 0.01608 0.00719 -0.0837 0.6187 0.2550
-4.750 -0.1212 0.01582 0.00701 -0.0820 0.6158 0.2757
-4.500 -0.1028 0.01557 0.00683 -0.0804 0.6130 0.2991
-4.000 -0.0641 0.01511 0.00654 -0.0774 0.6081 0.3587
-3.750 -0.0450 0.01493 0.00649 -0.0758 0.6056 0.3894
-3.500 -0.0253 0.01480 0.00647 -0.0743 0.6027 0.4181
-3.250 -0.0041 0.01470 0.00645 -0.0730 0.5996 0.4438
-3.000 0.0178 0.01463 0.00644 -0.0718 0.5966 0.4663
-2.750 0.0410 0.01458 0.00641 -0.0709 0.5938 0.4855
-2.500 0.0651 0.01456 0.00638 -0.0701 0.5915 0.5034
-2.250 0.0901 0.01455 0.00635 -0.0694 0.5892 0.5198
-2.000 0.1140 0.01456 0.00638 -0.0686 0.5866 0.5338
-1.750 0.1365 0.01457 0.00643 -0.0675 0.5834 0.5467
-1.500 0.1599 0.01458 0.00646 -0.0666 0.5803 0.5595
-1.250 0.1839 0.01459 0.00650 -0.0657 0.5775 0.5707
-1.000 0.2084 0.01460 0.00648 -0.0650 0.5747 0.5831
-0.750 0.2336 0.01460 0.00649 -0.0644 0.5721 0.5939
-0.500 0.2598 0.01463 0.00647 -0.0640 0.5698 0.6055
-0.250 0.2834 0.01467 0.00657 -0.0631 0.5671 0.6172
0.000 0.3052 0.01472 0.00669 -0.0618 0.5637 0.6296
0.250 0.3279 0.01476 0.00676 -0.0608 0.5604 0.6422
0.500 0.3520 0.01478 0.00682 -0.0599 0.5573 0.6517
0.750 0.3768 0.01481 0.00684 -0.0593 0.5545 0.6612
1.000 0.4027 0.01482 0.00683 -0.0588 0.5520 0.6697
1.250 0.4286 0.01487 0.00688 -0.0584 0.5494 0.6780
1.750 0.4713 0.01500 0.00713 -0.0558 0.5423 0.6944
2.000 0.4943 0.01504 0.00719 -0.0548 0.5389 0.7033
2.250 0.5184 0.01507 0.00722 -0.0540 0.5359 0.7116
2.500 0.5441 0.01510 0.00724 -0.0535 0.5332 0.7204
2.750 0.5674 0.01517 0.00732 -0.0526 0.5302 0.7297
3.000 0.5863 0.01527 0.00753 -0.0509 0.5262 0.7381
3.250 0.6066 0.01534 0.00764 -0.0494 0.5224 0.7483
3.500 0.6289 0.01539 0.00773 -0.0483 0.5189 0.7568
3.750 0.6526 0.01543 0.00776 -0.0474 0.5159 0.7667
4.000 0.6771 0.01549 0.00782 -0.0467 0.5129 0.7760
4.250 0.6923 0.01562 0.00806 -0.0443 0.5086 0.7866
4.500 0.7100 0.01572 0.00822 -0.0424 0.5044 0.7964
4.750 0.7296 0.01578 0.00831 -0.0408 0.5006 0.8070
5.000 0.7526 0.01582 0.00834 -0.0398 0.4973 0.8171
5.250 0.7707 0.01592 0.00849 -0.0379 0.4936 0.8285
5.500 0.7823 0.01605 0.00871 -0.0348 0.4890 0.8396
5.750 0.7958 0.01613 0.00884 -0.0321 0.4846 0.8523
6.000 0.8166 0.01619 0.00892 -0.0307 0.4808 0.8636
6.250 0.8387 0.01628 0.00901 -0.0297 0.4771 0.8753
6.500 0.8514 0.01652 0.00936 -0.0271 0.4719 0.8896
6.750 0.8746 0.01671 0.00961 -0.0266 0.4670 0.9028
7.000 0.9058 0.01683 0.00974 -0.0276 0.4625 0.9151
7.250 0.9359 0.01708 0.01005 -0.0286 0.4572 0.9287
7.500 0.9690 0.01740 0.01046 -0.0304 0.4510 0.9424
7.750 1.0087 0.01762 0.01068 -0.0333 0.4456 0.9547
8.250 1.0842 0.01843 0.01160 -0.0390 0.4327 1.0000
8.500 1.0956 0.01867 0.01178 -0.0365 0.4276 1.0000
8.750 1.1038 0.01908 0.01222 -0.0337 0.4221 1.0000
9.000 1.1114 0.01956 0.01273 -0.0310 0.4157 1.0000
9.250 1.1245 0.01996 0.01308 -0.0291 0.4102 1.0000
9.500 1.1321 0.02061 0.01376 -0.0267 0.4038 1.0000
9.750 1.1407 0.02129 0.01446 -0.0246 0.3971 1.0000
10.000 1.1543 0.02184 0.01496 -0.0231 0.3915 1.0000
10.250 1.1597 0.02284 0.01605 -0.0211 0.3846 1.0000
10.500 1.1694 0.02371 0.01691 -0.0196 0.3781 1.0000
10.750 1.1780 0.02469 0.01790 -0.0182 0.3712 1.0000
11.000 1.1847 0.02589 0.01914 -0.0168 0.3640 1.0000
11.250 1.1954 0.02684 0.02004 -0.0156 0.3572 1.0000
11.500 1.1996 0.02836 0.02164 -0.0144 0.3498 1.0000
11.750 1.2079 0.02956 0.02281 -0.0134 0.3425 1.0000
12.000 1.2137 0.03104 0.02434 -0.0124 0.3354 1.0000
12.250 1.2198 0.03253 0.02585 -0.0115 0.3283 1.0000
12.500 1.2267 0.03395 0.02726 -0.0106 0.3212 1.0000
12.750 1.2301 0.03572 0.02908 -0.0097 0.3134 1.0000
13.000 1.2364 0.03721 0.03053 -0.0089 0.3060 1.0000
13.250 1.2387 0.03917 0.03257 -0.0081 0.2982 1.0000
13.500 1.2443 0.04078 0.03414 -0.0074 0.2909 1.0000
13.750 1.2465 0.04285 0.03627 -0.0068 0.2834 1.0000
14.000 1.2505 0.04471 0.03811 -0.0062 0.2757 1.0000
14.250 1.2532 0.04681 0.04027 -0.0057 0.2683 1.0000
14.500 1.2559 0.04889 0.04235 -0.0052 0.2606 1.0000
14.750 1.2581 0.05110 0.04458 -0.0049 0.2530 1.0000
15.000 1.2592 0.05344 0.04692 -0.0045 0.2448 1.0000
15.250 1.2611 0.05577 0.04927 -0.0043 0.2374 1.0000
15.500 1.2624 0.05816 0.05168 -0.0041 0.2298 1.0000
15.750 1.2630 0.06068 0.05422 -0.0039 0.2223 1.0000
16.000 1.2646 0.06316 0.05673 -0.0039 0.2153 1.0000
16.250 1.2653 0.06573 0.05930 -0.0038 0.2085 1.0000
16.500 1.2651 0.06847 0.06209 -0.0039 0.2010 1.0000
16.750 1.2652 0.07116 0.06476 -0.0039 0.1946 1.0000
17.000 1.2652 0.07398 0.06764 -0.0041 0.1875 1.0000
17.500 1.2640 0.07977 0.07349 -0.0046 0.1746 1.0000
17.750 1.2617 0.08287 0.07659 -0.0050 0.1684 1.0000
18.000 1.2609 0.08589 0.07966 -0.0054 0.1621 1.0000
18.250 1.2578 0.08921 0.08299 -0.0059 0.1558 1.0000
18.500 1.2563 0.09237 0.08619 -0.0065 0.1499 1.0000
18.750 1.2536 0.09569 0.08955 -0.0071 0.1441 1.0000
19.000 1.2506 0.09908 0.09294 -0.0078 0.1384 1.0000
19.250 1.2475 0.10253 0.09646 -0.0086 0.1325 1.0000
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