MH 102 16.99% (mh102-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: MH 102 16.99% (mh102-il) Reynolds number: 500,000 Max Cl/Cd: 94.17 at α=8° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-mh102-il-500000.txt Download as CSV file: xf-mh102-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: MH 102 16.99%
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 -0.7232 0.14966 0.14643 -0.0191 1.0000 0.0116
-19.500 -0.7426 0.14126 0.13787 -0.0238 1.0000 0.0117
-19.250 -0.7549 0.13471 0.13120 -0.0274 1.0000 0.0116
-19.000 -0.7642 0.12883 0.12522 -0.0306 1.0000 0.0117
-18.750 -0.7727 0.12333 0.11961 -0.0335 1.0000 0.0117
-18.500 -0.7780 0.11863 0.11483 -0.0358 1.0000 0.0117
-18.250 -0.7846 0.11362 0.10972 -0.0384 1.0000 0.0118
-18.000 -0.7914 0.10862 0.10460 -0.0410 1.0000 0.0119
-17.750 -0.7940 0.10453 0.10044 -0.0430 1.0000 0.0119
-17.500 -0.7986 0.10008 0.09589 -0.0452 1.0000 0.0120
-17.250 -0.8007 0.09618 0.09192 -0.0470 1.0000 0.0121
-17.000 -0.8009 0.09267 0.08836 -0.0486 1.0000 0.0121
-16.750 -0.7999 0.08989 0.08556 -0.0493 1.0000 0.0123
-16.500 -0.7996 0.08671 0.08236 -0.0506 1.0000 0.0124
-16.250 -0.8002 0.08345 0.07908 -0.0518 1.0000 0.0125
-16.000 -0.8016 0.08001 0.07561 -0.0533 1.0000 0.0127
-15.750 -0.8034 0.07651 0.07207 -0.0548 1.0000 0.0127
-15.500 -0.8067 0.07286 0.06839 -0.0563 1.0000 0.0128
-15.250 -0.8102 0.06929 0.06476 -0.0578 1.0000 0.0128
-15.000 -0.8177 0.06532 0.06075 -0.0596 1.0000 0.0131
-14.750 -0.8256 0.06133 0.05670 -0.0613 1.0000 0.0133
-14.500 -0.8323 0.05756 0.05287 -0.0629 1.0000 0.0132
-14.250 -0.8418 0.05339 0.04863 -0.0647 1.0000 0.0135
-14.000 -0.8506 0.04933 0.04450 -0.0665 1.0000 0.0136
-13.750 -0.8622 0.04496 0.04005 -0.0684 1.0000 0.0137
-13.500 -0.8705 0.04089 0.03589 -0.0703 1.0000 0.0138
-13.250 -0.8781 0.03691 0.03181 -0.0722 1.0000 0.0140
-13.000 -0.8843 0.03331 0.02811 -0.0739 1.0000 0.0140
-12.750 -0.8902 0.03026 0.02495 -0.0748 1.0000 0.0143
-12.500 -0.8956 0.02799 0.02257 -0.0743 1.0000 0.0144
-12.250 -0.9057 0.02618 0.02067 -0.0720 1.0000 0.0147
-12.000 -0.9255 0.02482 0.01926 -0.0668 1.0000 0.0148
-11.750 -0.9380 0.02390 0.01830 -0.0614 1.0000 0.0150
-11.500 -0.9445 0.02305 0.01743 -0.0568 1.0000 0.0154
-11.250 -0.9136 0.02191 0.01623 -0.0590 0.9959 0.0162
-11.000 -0.8787 0.02095 0.01519 -0.0616 0.9910 0.0172
-10.750 -0.8481 0.01964 0.01384 -0.0637 0.9839 0.0190
-10.500 -0.8157 0.01863 0.01276 -0.0656 0.9769 0.0208
-10.250 -0.7835 0.01765 0.01174 -0.0674 0.9684 0.0237
-10.000 -0.7533 0.01669 0.01075 -0.0686 0.9566 0.0274
-9.750 -0.7212 0.01570 0.00976 -0.0702 0.9440 0.0339
-9.500 -0.6884 0.01477 0.00884 -0.0718 0.9294 0.0441
-9.250 -0.6601 0.01392 0.00802 -0.0724 0.9107 0.0593
-9.000 -0.6369 0.01318 0.00733 -0.0719 0.8903 0.0802
-8.750 -0.6154 0.01259 0.00679 -0.0710 0.8711 0.1037
-8.500 -0.5925 0.01220 0.00643 -0.0702 0.8537 0.1238
-8.250 -0.5685 0.01193 0.00615 -0.0694 0.8379 0.1402
-8.000 -0.5435 0.01174 0.00593 -0.0688 0.8234 0.1532
-7.750 -0.5180 0.01161 0.00573 -0.0682 0.8093 0.1635
-7.500 -0.4919 0.01151 0.00556 -0.0677 0.7952 0.1729
-7.250 -0.4662 0.01137 0.00539 -0.0672 0.7819 0.1811
-7.000 -0.4393 0.01135 0.00525 -0.0668 0.7697 0.1888
-6.750 -0.4135 0.01120 0.00510 -0.0663 0.7572 0.1967
-6.500 -0.3864 0.01117 0.00497 -0.0659 0.7451 0.2035
-6.250 -0.3603 0.01106 0.00479 -0.0654 0.7332 0.2096
-6.000 -0.3335 0.01099 0.00469 -0.0651 0.7212 0.2167
-5.750 -0.3062 0.01097 0.00456 -0.0648 0.7102 0.2230
-5.500 -0.2801 0.01082 0.00440 -0.0643 0.6992 0.2292
-5.250 -0.2528 0.01075 0.00427 -0.0640 0.6882 0.2346
-5.000 -0.2256 0.01074 0.00413 -0.0637 0.6774 0.2388
-4.750 -0.1992 0.01054 0.00395 -0.0633 0.6663 0.2448
-4.500 -0.1721 0.01047 0.00383 -0.0629 0.6562 0.2501
-4.250 -0.1446 0.01044 0.00371 -0.0627 0.6458 0.2550
-4.000 -0.1179 0.01030 0.00356 -0.0623 0.6362 0.2611
-3.750 -0.0909 0.01024 0.00345 -0.0620 0.6260 0.2670
-3.500 -0.0632 0.01022 0.00336 -0.0618 0.6161 0.2727
-3.250 -0.0366 0.01011 0.00324 -0.0614 0.6063 0.2797
-3.000 -0.0091 0.01005 0.00316 -0.0612 0.5971 0.2865
-2.750 0.0181 0.01003 0.00307 -0.0609 0.5881 0.2933
-2.500 0.0453 0.00995 0.00301 -0.0606 0.5793 0.3016
-2.250 0.0728 0.00996 0.00295 -0.0604 0.5703 0.3095
-2.000 0.0998 0.00987 0.00290 -0.0601 0.5617 0.3186
-1.500 0.1543 0.00982 0.00282 -0.0596 0.5457 0.3387
-1.250 0.1817 0.00979 0.00279 -0.0593 0.5375 0.3498
-1.000 0.2087 0.00980 0.00278 -0.0591 0.5300 0.3619
-0.750 0.2361 0.00974 0.00277 -0.0588 0.5225 0.3745
-0.500 0.2631 0.00976 0.00276 -0.0586 0.5153 0.3884
-0.250 0.2905 0.00974 0.00277 -0.0583 0.5085 0.4042
0.000 0.3177 0.00972 0.00278 -0.0581 0.5015 0.4211
0.250 0.3443 0.00975 0.00281 -0.0578 0.4951 0.4390
0.500 0.3716 0.00969 0.00283 -0.0576 0.4889 0.4588
0.750 0.3984 0.00967 0.00287 -0.0573 0.4826 0.4816
1.000 0.4246 0.00968 0.00292 -0.0569 0.4767 0.5078
1.500 0.4778 0.00959 0.00304 -0.0562 0.4654 0.5700
1.750 0.5034 0.00961 0.00312 -0.0557 0.4598 0.6072
2.000 0.5295 0.00953 0.00321 -0.0552 0.4548 0.6491
2.250 0.5550 0.00948 0.00330 -0.0546 0.4494 0.6924
2.500 0.5797 0.00948 0.00340 -0.0538 0.4444 0.7362
2.750 0.6042 0.00946 0.00353 -0.0529 0.4394 0.7828
3.000 0.6286 0.00941 0.00365 -0.0519 0.4345 0.8302
3.250 0.6528 0.00942 0.00377 -0.0508 0.4296 0.8771
3.500 0.6808 0.00955 0.00392 -0.0506 0.4242 0.9202
3.750 0.7208 0.00961 0.00405 -0.0529 0.4190 0.9528
4.000 0.7647 0.00975 0.00418 -0.0562 0.4130 0.9725
4.250 0.8072 0.00999 0.00432 -0.0593 0.4069 0.9853
4.500 0.8493 0.01007 0.00445 -0.0622 0.4014 0.9962
4.750 0.8817 0.01020 0.00455 -0.0633 0.3957 1.0000
5.000 0.9019 0.01039 0.00467 -0.0619 0.3906 1.0000
5.250 0.9241 0.01049 0.00480 -0.0607 0.3858 1.0000
5.500 0.9464 0.01061 0.00492 -0.0597 0.3803 1.0000
5.750 0.9680 0.01078 0.00505 -0.0585 0.3750 1.0000
6.000 0.9904 0.01094 0.00521 -0.0574 0.3696 1.0000
6.250 1.0135 0.01106 0.00535 -0.0565 0.3638 1.0000
6.500 1.0355 0.01126 0.00550 -0.0554 0.3578 1.0000
6.750 1.0585 0.01143 0.00568 -0.0545 0.3521 1.0000
7.000 1.0816 0.01158 0.00584 -0.0536 0.3456 1.0000
7.250 1.1028 0.01183 0.00604 -0.0525 0.3391 1.0000
7.500 1.1264 0.01197 0.00623 -0.0517 0.3325 1.0000
7.750 1.1479 0.01220 0.00643 -0.0506 0.3253 1.0000
8.000 1.1696 0.01242 0.00666 -0.0496 0.3185 1.0000
8.250 1.1909 0.01265 0.00689 -0.0485 0.3109 1.0000
8.500 1.2109 0.01293 0.00715 -0.0472 0.3037 1.0000
8.750 1.2314 0.01318 0.00741 -0.0459 0.2958 1.0000
9.000 1.2493 0.01352 0.00772 -0.0444 0.2884 1.0000
9.250 1.2677 0.01379 0.00801 -0.0428 0.2806 1.0000
9.500 1.2810 0.01418 0.00836 -0.0404 0.2734 1.0000
9.750 1.2978 0.01449 0.00870 -0.0386 0.2661 1.0000
10.000 1.3096 0.01497 0.00913 -0.0361 0.2589 1.0000
10.250 1.3261 0.01533 0.00953 -0.0344 0.2519 1.0000
10.500 1.3381 0.01586 0.01004 -0.0322 0.2448 1.0000
10.750 1.3524 0.01634 0.01054 -0.0303 0.2384 1.0000
11.000 1.3648 0.01690 0.01111 -0.0284 0.2317 1.0000
11.250 1.3755 0.01758 0.01179 -0.0263 0.2256 1.0000
11.500 1.3886 0.01819 0.01243 -0.0246 0.2189 1.0000
11.750 1.3961 0.01909 0.01331 -0.0225 0.2127 1.0000
12.000 1.4093 0.01978 0.01406 -0.0210 0.2070 1.0000
12.250 1.4179 0.02074 0.01503 -0.0193 0.2009 1.0000
12.500 1.4256 0.02182 0.01612 -0.0177 0.1954 1.0000
12.750 1.4362 0.02280 0.01714 -0.0164 0.1897 1.0000
13.000 1.4410 0.02419 0.01853 -0.0149 0.1842 1.0000
13.250 1.4497 0.02539 0.01978 -0.0137 0.1791 1.0000
13.500 1.4566 0.02678 0.02121 -0.0127 0.1738 1.0000
13.750 1.4578 0.02865 0.02307 -0.0114 0.1688 1.0000
14.000 1.4665 0.03003 0.02453 -0.0107 0.1640 1.0000
14.250 1.4703 0.03184 0.02638 -0.0099 0.1592 1.0000
14.500 1.4683 0.03419 0.02872 -0.0090 0.1546 1.0000
14.750 1.4756 0.03583 0.03045 -0.0086 0.1503 1.0000
15.000 1.4765 0.03808 0.03274 -0.0081 0.1458 1.0000
15.250 1.4719 0.04090 0.03557 -0.0076 0.1415 1.0000
15.500 1.4771 0.04289 0.03765 -0.0074 0.1375 1.0000
15.750 1.4766 0.04550 0.04030 -0.0073 0.1334 1.0000
16.000 1.4707 0.04870 0.04351 -0.0073 0.1295 1.0000
16.250 1.4726 0.05120 0.04609 -0.0074 0.1257 1.0000
16.500 1.4712 0.05408 0.04904 -0.0076 0.1220 1.0000
16.750 1.4649 0.05759 0.05256 -0.0080 0.1183 1.0000
17.000 1.4630 0.06065 0.05568 -0.0084 0.1151 1.0000
17.250 1.4623 0.06363 0.05874 -0.0088 0.1114 1.0000
17.500 1.4565 0.06727 0.06241 -0.0095 0.1082 1.0000
17.750 1.4491 0.07115 0.06632 -0.0103 0.1050 1.0000
18.000 1.4496 0.07414 0.06940 -0.0110 0.1020 1.0000
18.250 1.4454 0.07776 0.07307 -0.0119 0.0989 1.0000
18.500 1.4362 0.08208 0.07740 -0.0130 0.0958 1.0000
18.750 1.4342 0.08551 0.08092 -0.0140 0.0929 1.0000
19.000 1.4310 0.08916 0.08464 -0.0151 0.0900 1.0000
19.250 1.4236 0.09343 0.08894 -0.0165 0.0872 1.0000
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