MH 150 23.89% (mh150-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: MH 150 23.89% (mh150-il) Reynolds number: 1,000,000 Max Cl/Cd: 117.32 at α=6.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-mh150-il-1000000.txt Download as CSV file: xf-mh150-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: MH 150 23.89%
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.250 -0.7097 0.10027 0.09668 -0.0654 0.9467 0.0190
-18.000 -0.7164 0.09649 0.09282 -0.0666 0.9298 0.0193
-17.750 -0.7263 0.09204 0.08826 -0.0684 0.9146 0.0197
-17.500 -0.7312 0.08823 0.08436 -0.0700 0.9006 0.0200
-17.250 -0.7373 0.08418 0.08019 -0.0720 0.8874 0.0204
-17.000 -0.7393 0.08058 0.07651 -0.0738 0.8764 0.0208
-16.750 -0.7430 0.07682 0.07264 -0.0757 0.8653 0.0212
-16.500 -0.7430 0.07349 0.06922 -0.0775 0.8559 0.0216
-16.250 -0.7442 0.07002 0.06564 -0.0794 0.8459 0.0221
-16.000 -0.7490 0.06616 0.06169 -0.0815 0.8372 0.0227
-15.750 -0.7533 0.06235 0.05781 -0.0837 0.8285 0.0233
-15.500 -0.7566 0.05874 0.05409 -0.0858 0.8194 0.0240
-15.250 -0.7564 0.05552 0.05081 -0.0877 0.8122 0.0247
-14.750 -0.7588 0.04888 0.04399 -0.0917 0.7956 0.0265
-14.500 -0.7593 0.04563 0.04068 -0.0938 0.7888 0.0277
-14.250 -0.7556 0.04291 0.03789 -0.0955 0.7811 0.0289
-14.000 -0.7557 0.03981 0.03470 -0.0975 0.7732 0.0305
-13.750 -0.7525 0.03704 0.03189 -0.0995 0.7667 0.0322
-13.500 -0.7492 0.03435 0.02913 -0.1013 0.7592 0.0342
-13.250 -0.7437 0.03193 0.02664 -0.1031 0.7516 0.0366
-13.000 -0.7379 0.02947 0.02415 -0.1050 0.7458 0.0394
-12.750 -0.7291 0.02731 0.02195 -0.1068 0.7387 0.0426
-12.500 -0.7184 0.02533 0.01991 -0.1086 0.7310 0.0465
-12.250 -0.7058 0.02343 0.01800 -0.1105 0.7253 0.0510
-12.000 -0.6916 0.02169 0.01626 -0.1124 0.7189 0.0563
-11.750 -0.6766 0.02020 0.01473 -0.1141 0.7120 0.0619
-11.500 -0.6554 0.01881 0.01334 -0.1166 0.7058 0.0685
-11.000 -0.6038 0.01644 0.01097 -0.1220 0.6932 0.0835
-10.750 -0.5744 0.01549 0.01000 -0.1249 0.6864 0.0917
-10.500 -0.5426 0.01462 0.00916 -0.1278 0.6815 0.1003
-10.250 -0.5098 0.01388 0.00843 -0.1306 0.6752 0.1092
-10.000 -0.4763 0.01326 0.00778 -0.1332 0.6684 0.1183
-9.750 -0.4418 0.01267 0.00721 -0.1359 0.6629 0.1278
-9.500 -0.4073 0.01216 0.00672 -0.1383 0.6576 0.1376
-9.250 -0.3737 0.01174 0.00630 -0.1402 0.6514 0.1475
-9.000 -0.3406 0.01140 0.00594 -0.1420 0.6444 0.1576
-8.750 -0.3068 0.01106 0.00562 -0.1437 0.6396 0.1680
-8.500 -0.2730 0.01074 0.00532 -0.1454 0.6340 0.1795
-8.250 -0.2394 0.01044 0.00504 -0.1470 0.6280 0.1931
-8.000 -0.2058 0.01020 0.00481 -0.1486 0.6220 0.2072
-7.750 -0.1720 0.00996 0.00462 -0.1501 0.6169 0.2206
-7.500 -0.1389 0.00981 0.00447 -0.1513 0.6109 0.2314
-7.250 -0.1066 0.00973 0.00435 -0.1523 0.6046 0.2397
-7.000 -0.0738 0.00963 0.00423 -0.1533 0.5997 0.2462
-6.750 -0.0408 0.00952 0.00412 -0.1545 0.5944 0.2532
-6.500 -0.0089 0.00949 0.00404 -0.1553 0.5884 0.2583
-6.250 0.0232 0.00946 0.00395 -0.1562 0.5816 0.2636
-6.000 0.0564 0.00936 0.00386 -0.1573 0.5776 0.2696
-5.750 0.0886 0.00932 0.00380 -0.1582 0.5723 0.2745
-5.500 0.1201 0.00935 0.00375 -0.1589 0.5663 0.2777
-5.250 0.1527 0.00929 0.00367 -0.1599 0.5603 0.2833
-5.000 0.1855 0.00922 0.00361 -0.1609 0.5560 0.2882
-4.750 0.2176 0.00920 0.00356 -0.1618 0.5509 0.2924
-4.500 0.2490 0.00924 0.00353 -0.1624 0.5453 0.2957
-4.250 0.2809 0.00924 0.00349 -0.1633 0.5398 0.2995
-4.000 0.3139 0.00917 0.00343 -0.1644 0.5354 0.3049
-3.750 0.3459 0.00916 0.00341 -0.1652 0.5302 0.3092
-3.500 0.3773 0.00920 0.00340 -0.1659 0.5247 0.3130
-3.250 0.4085 0.00926 0.00340 -0.1666 0.5198 0.3159
-3.000 0.4413 0.00920 0.00336 -0.1676 0.5160 0.3214
-2.750 0.4735 0.00919 0.00335 -0.1685 0.5113 0.3266
-2.500 0.5049 0.00924 0.00336 -0.1693 0.5060 0.3312
-2.250 0.5357 0.00932 0.00339 -0.1699 0.5005 0.3351
-2.000 0.5680 0.00930 0.00338 -0.1708 0.4970 0.3404
-1.750 0.6001 0.00930 0.00339 -0.1717 0.4928 0.3465
-1.500 0.6314 0.00935 0.00342 -0.1725 0.4882 0.3517
-1.250 0.6619 0.00946 0.00347 -0.1730 0.4830 0.3557
-1.000 0.6937 0.00947 0.00349 -0.1739 0.4795 0.3615
-0.750 0.7257 0.00948 0.00352 -0.1748 0.4758 0.3683
-0.500 0.7567 0.00953 0.00357 -0.1755 0.4715 0.3742
-0.250 0.7871 0.00964 0.00363 -0.1760 0.4668 0.3790
0.000 0.8180 0.00973 0.00371 -0.1768 0.4619 0.3869
0.250 0.8495 0.00975 0.00376 -0.1776 0.4593 0.3937
0.500 0.8802 0.00981 0.00382 -0.1782 0.4559 0.3991
0.750 0.9115 0.00986 0.00389 -0.1790 0.4521 0.4084
1.000 0.9415 0.00998 0.00399 -0.1796 0.4479 0.4161
1.250 0.9707 0.01015 0.00411 -0.1800 0.4429 0.4223
1.500 1.0022 0.01016 0.00418 -0.1808 0.4404 0.4313
1.750 1.0327 0.01024 0.00427 -0.1814 0.4372 0.4390
2.000 1.0627 0.01034 0.00437 -0.1820 0.4336 0.4465
2.250 1.0924 0.01046 0.00450 -0.1825 0.4299 0.4558
2.500 1.1208 0.01065 0.00466 -0.1828 0.4255 0.4634
2.750 1.1507 0.01074 0.00478 -0.1834 0.4227 0.4720
3.000 1.1809 0.01082 0.00490 -0.1839 0.4202 0.4805
3.250 1.2099 0.01094 0.00502 -0.1843 0.4169 0.4872
3.500 1.2390 0.01107 0.00517 -0.1848 0.4133 0.4962
3.750 1.2667 0.01127 0.00535 -0.1850 0.4094 0.5046
4.000 1.2936 0.01150 0.00556 -0.1850 0.4053 0.5118
4.250 1.3231 0.01158 0.00571 -0.1856 0.4034 0.5212
4.500 1.3517 0.01171 0.00586 -0.1859 0.4008 0.5292
4.750 1.3794 0.01186 0.00603 -0.1861 0.3977 0.5361
5.000 1.4065 0.01205 0.00623 -0.1862 0.3944 0.5445
5.250 1.4319 0.01231 0.00647 -0.1861 0.3906 0.5521
5.500 1.4566 0.01259 0.00674 -0.1858 0.3869 0.5591
5.750 1.4843 0.01271 0.00693 -0.1860 0.3851 0.5679
6.000 1.5108 0.01288 0.00713 -0.1860 0.3827 0.5756
6.250 1.5357 0.01309 0.00736 -0.1858 0.3798 0.5820
6.500 1.5577 0.01333 0.00763 -0.1851 0.3767 0.5900
6.750 1.5787 0.01367 0.00797 -0.1843 0.3736 0.5977
7.000 1.5980 0.01412 0.00840 -0.1833 0.3697 0.6037
7.250 1.6225 0.01435 0.00870 -0.1831 0.3678 0.6119
7.500 1.6464 0.01460 0.00900 -0.1828 0.3656 0.6197
7.750 1.6687 0.01493 0.00935 -0.1822 0.3632 0.6260
8.000 1.6902 0.01530 0.00976 -0.1817 0.3605 0.6335
8.250 1.7095 0.01577 0.01026 -0.1808 0.3576 0.6408
8.500 1.7267 0.01638 0.01085 -0.1798 0.3541 0.6474
8.750 1.7445 0.01697 0.01146 -0.1788 0.3511 0.6539
9.000 1.7667 0.01734 0.01191 -0.1784 0.3494 0.6611
9.250 1.7875 0.01779 0.01241 -0.1779 0.3472 0.6679
9.500 1.8070 0.01833 0.01297 -0.1773 0.3446 0.6736
9.750 1.8247 0.01898 0.01366 -0.1765 0.3418 0.6808
10.000 1.8397 0.01979 0.01450 -0.1754 0.3386 0.6872
10.250 1.8516 0.02083 0.01552 -0.1740 0.3347 0.6931
10.500 1.8709 0.02143 0.01618 -0.1735 0.3329 0.6993
10.750 1.8898 0.02205 0.01688 -0.1730 0.3308 0.7057
11.000 1.9067 0.02281 0.01769 -0.1723 0.3284 0.7119
11.250 1.9221 0.02369 0.01859 -0.1714 0.3257 0.7173
11.500 1.9341 0.02481 0.01975 -0.1703 0.3227 0.7236
11.750 1.9434 0.02611 0.02107 -0.1690 0.3194 0.7293
12.000 1.9548 0.02729 0.02228 -0.1679 0.3166 0.7351
12.250 1.9714 0.02812 0.02318 -0.1673 0.3148 0.7406
12.500 1.9856 0.02914 0.02428 -0.1665 0.3125 0.7464
12.750 1.9975 0.03032 0.02551 -0.1656 0.3097 0.7520
13.000 2.0065 0.03175 0.02697 -0.1645 0.3069 0.7575
13.250 2.0120 0.03349 0.02873 -0.1632 0.3036 0.7626
13.500 2.0177 0.03523 0.03051 -0.1619 0.3002 0.7679
13.750 2.0311 0.03640 0.03176 -0.1613 0.2983 0.7733
14.000 2.0431 0.03768 0.03309 -0.1606 0.2957 0.7785
14.250 2.0503 0.03939 0.03487 -0.1596 0.2928 0.7835
14.500 2.0552 0.04130 0.03682 -0.1586 0.2895 0.7885
14.750 2.0530 0.04391 0.03944 -0.1572 0.2854 0.7932
15.000 2.0622 0.04549 0.04108 -0.1564 0.2829 0.7980
15.250 2.0700 0.04725 0.04292 -0.1557 0.2803 0.8028
15.500 2.0758 0.04916 0.04489 -0.1549 0.2770 0.8076
15.750 2.0739 0.05188 0.04765 -0.1538 0.2732 0.8122
16.000 2.0681 0.05495 0.05072 -0.1526 0.2686 0.8162
16.250 2.0746 0.05691 0.05277 -0.1520 0.2661 0.8206
16.500 2.0788 0.05905 0.05498 -0.1512 0.2625 0.8251
16.750 2.0719 0.06238 0.05835 -0.1502 0.2577 0.8294
17.000 2.0621 0.06605 0.06202 -0.1492 0.2526 0.8333
17.250 2.0642 0.06852 0.06458 -0.1486 0.2487 0.8373
17.500 2.0576 0.07187 0.06796 -0.1478 0.2434 0.8410
17.750 2.0410 0.07639 0.07250 -0.1469 0.2377 0.8446
18.000 2.0394 0.07933 0.07551 -0.1464 0.2334 0.8490
18.250 2.0293 0.08318 0.07939 -0.1458 0.2278 0.8525
18.500 2.0112 0.08801 0.08425 -0.1452 0.2220 0.8556
18.750 2.0065 0.09133 0.08762 -0.1448 0.2165 0.8595
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