MH 150 23.89% (mh150-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: MH 150 23.89% (mh150-il) Reynolds number: 1,000,000 Max Cl/Cd: 112.89 at α=5.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-mh150-il-1000000-n5.txt Download as CSV file: xf-mh150-il-1000000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -0.7255 0.11528 0.11142 -0.0537 0.8684 0.0136
-19.000 -0.7304 0.11092 0.10696 -0.0560 0.8589 0.0138
-18.750 -0.7343 0.10670 0.10266 -0.0584 0.8491 0.0140
-18.500 -0.7389 0.10244 0.09829 -0.0607 0.8399 0.0142
-18.250 -0.7412 0.09855 0.09433 -0.0628 0.8318 0.0144
-18.000 -0.7450 0.09445 0.09014 -0.0651 0.8233 0.0146
-17.750 -0.7462 0.09077 0.08637 -0.0671 0.8158 0.0149
-17.500 -0.7490 0.08688 0.08240 -0.0693 0.8082 0.0151
-17.250 -0.7496 0.08335 0.07878 -0.0712 0.7999 0.0154
-17.000 -0.7509 0.07972 0.07507 -0.0733 0.7931 0.0156
-16.750 -0.7512 0.07628 0.07156 -0.0752 0.7863 0.0159
-16.500 -0.7509 0.07293 0.06812 -0.0771 0.7787 0.0161
-16.250 -0.7520 0.06944 0.06455 -0.0791 0.7720 0.0165
-16.000 -0.7538 0.06589 0.06093 -0.0812 0.7655 0.0168
-15.750 -0.7532 0.06266 0.05762 -0.0831 0.7582 0.0173
-15.500 -0.7538 0.05930 0.05418 -0.0851 0.7515 0.0177
-15.250 -0.7514 0.05635 0.05118 -0.0868 0.7457 0.0182
-15.000 -0.7497 0.05330 0.04805 -0.0887 0.7388 0.0187
-14.750 -0.7467 0.05045 0.04511 -0.0905 0.7316 0.0191
-14.500 -0.7445 0.04751 0.04211 -0.0923 0.7261 0.0198
-14.250 -0.7420 0.04462 0.03917 -0.0942 0.7199 0.0204
-14.000 -0.7378 0.04194 0.03641 -0.0960 0.7130 0.0212
-13.750 -0.7312 0.03957 0.03397 -0.0976 0.7067 0.0220
-13.500 -0.7257 0.03705 0.03140 -0.0993 0.7010 0.0229
-13.250 -0.7195 0.03466 0.02895 -0.1010 0.6947 0.0239
-13.000 -0.7111 0.03252 0.02673 -0.1027 0.6882 0.0251
-12.750 -0.7019 0.03043 0.02461 -0.1043 0.6828 0.0263
-12.500 -0.6914 0.02848 0.02261 -0.1059 0.6766 0.0279
-12.250 -0.6790 0.02668 0.02076 -0.1075 0.6700 0.0297
-12.000 -0.6658 0.02492 0.01895 -0.1092 0.6643 0.0321
-11.750 -0.6508 0.02327 0.01728 -0.1109 0.6591 0.0348
-11.500 -0.6357 0.02183 0.01581 -0.1123 0.6526 0.0378
-11.000 -0.5965 0.01926 0.01318 -0.1162 0.6409 0.0458
-10.750 -0.5718 0.01810 0.01202 -0.1187 0.6357 0.0508
-10.500 -0.5450 0.01707 0.01098 -0.1212 0.6295 0.0564
-10.000 -0.4850 0.01530 0.00920 -0.1267 0.6177 0.0694
-9.750 -0.4525 0.01454 0.00844 -0.1295 0.6119 0.0770
-9.500 -0.4190 0.01387 0.00777 -0.1323 0.6061 0.0853
-9.250 -0.3847 0.01327 0.00717 -0.1351 0.6007 0.0948
-9.000 -0.3503 0.01274 0.00666 -0.1375 0.5952 0.1046
-8.750 -0.3167 0.01232 0.00625 -0.1395 0.5888 0.1139
-8.500 -0.2836 0.01198 0.00590 -0.1413 0.5827 0.1230
-8.250 -0.2497 0.01160 0.00555 -0.1431 0.5784 0.1343
-8.000 -0.2156 0.01122 0.00521 -0.1450 0.5732 0.1480
-7.750 -0.1816 0.01088 0.00490 -0.1469 0.5670 0.1633
-7.500 -0.1477 0.01059 0.00463 -0.1486 0.5608 0.1793
-7.250 -0.1138 0.01033 0.00442 -0.1501 0.5563 0.1921
-7.000 -0.0803 0.01014 0.00424 -0.1515 0.5512 0.2030
-6.750 -0.0475 0.01003 0.00410 -0.1527 0.5454 0.2118
-6.500 -0.0146 0.00991 0.00398 -0.1539 0.5398 0.2211
-6.250 0.0182 0.00982 0.00387 -0.1549 0.5350 0.2281
-6.000 0.0511 0.00972 0.00377 -0.1561 0.5299 0.2362
-5.750 0.0831 0.00969 0.00370 -0.1569 0.5244 0.2419
-5.500 0.1157 0.00963 0.00362 -0.1580 0.5193 0.2479
-5.250 0.1483 0.00957 0.00356 -0.1590 0.5146 0.2536
-5.000 0.1803 0.00956 0.00351 -0.1598 0.5093 0.2581
-4.750 0.2123 0.00955 0.00346 -0.1607 0.5043 0.2621
-4.500 0.2447 0.00952 0.00341 -0.1616 0.4999 0.2673
-4.250 0.2770 0.00949 0.00337 -0.1625 0.4958 0.2718
-4.000 0.3088 0.00950 0.00335 -0.1633 0.4907 0.2756
-3.750 0.3402 0.00953 0.00333 -0.1640 0.4854 0.2784
-3.500 0.3723 0.00953 0.00331 -0.1650 0.4809 0.2834
-3.250 0.4046 0.00951 0.00329 -0.1659 0.4776 0.2880
-3.000 0.4365 0.00952 0.00328 -0.1667 0.4737 0.2922
-2.750 0.4679 0.00955 0.00329 -0.1674 0.4692 0.2956
-2.500 0.4993 0.00960 0.00330 -0.1682 0.4643 0.2996
-2.250 0.5313 0.00961 0.00330 -0.1691 0.4603 0.3052
-2.000 0.5630 0.00962 0.00332 -0.1699 0.4565 0.3102
-1.750 0.5943 0.00966 0.00334 -0.1706 0.4527 0.3142
-1.500 0.6254 0.00972 0.00337 -0.1713 0.4487 0.3175
-1.250 0.6567 0.00978 0.00341 -0.1721 0.4445 0.3224
-1.000 0.6881 0.00981 0.00344 -0.1729 0.4414 0.3273
-0.750 0.7195 0.00985 0.00348 -0.1736 0.4381 0.3323
-0.500 0.7503 0.00992 0.00353 -0.1742 0.4341 0.3360
-0.250 0.7812 0.00999 0.00358 -0.1749 0.4299 0.3412
0.000 0.8118 0.01007 0.00366 -0.1756 0.4257 0.3466
0.250 0.8426 0.01014 0.00372 -0.1763 0.4228 0.3518
0.500 0.8733 0.01020 0.00379 -0.1769 0.4201 0.3565
0.750 0.9043 0.01026 0.00386 -0.1777 0.4170 0.3636
1.000 0.9348 0.01034 0.00394 -0.1783 0.4135 0.3702
1.250 0.9646 0.01046 0.00404 -0.1788 0.4096 0.3756
1.500 0.9942 0.01059 0.00416 -0.1793 0.4054 0.3813
1.750 1.0248 0.01065 0.00425 -0.1800 0.4030 0.3884
2.000 1.0548 0.01074 0.00434 -0.1805 0.4001 0.3953
2.250 1.0846 0.01084 0.00445 -0.1811 0.3971 0.4022
2.500 1.1143 0.01095 0.00458 -0.1816 0.3939 0.4106
2.750 1.1431 0.01110 0.00472 -0.1820 0.3906 0.4176
3.000 1.1717 0.01126 0.00487 -0.1823 0.3871 0.4239
3.250 1.2014 0.01135 0.00500 -0.1828 0.3849 0.4319
3.500 1.2303 0.01147 0.00514 -0.1832 0.3820 0.4391
3.750 1.2588 0.01161 0.00529 -0.1836 0.3788 0.4461
4.000 1.2871 0.01176 0.00546 -0.1839 0.3757 0.4554
4.250 1.3143 0.01196 0.00565 -0.1841 0.3725 0.4632
4.500 1.3413 0.01216 0.00586 -0.1842 0.3693 0.4707
4.750 1.3694 0.01229 0.00603 -0.1845 0.3673 0.4787
5.000 1.3967 0.01245 0.00621 -0.1846 0.3648 0.4856
5.250 1.4235 0.01263 0.00641 -0.1847 0.3618 0.4928
5.500 1.4495 0.01284 0.00664 -0.1847 0.3588 0.5018
5.750 1.4742 0.01308 0.00689 -0.1844 0.3560 0.5094
6.000 1.4964 0.01335 0.00717 -0.1837 0.3528 0.5172
6.250 1.5192 0.01359 0.00744 -0.1832 0.3505 0.5248
6.500 1.5434 0.01382 0.00771 -0.1829 0.3483 0.5318
6.750 1.5673 0.01409 0.00801 -0.1826 0.3458 0.5399
7.000 1.5902 0.01439 0.00835 -0.1822 0.3433 0.5483
7.250 1.6116 0.01477 0.00874 -0.1816 0.3404 0.5553
7.500 1.6320 0.01520 0.00919 -0.1808 0.3372 0.5632
7.750 1.6516 0.01569 0.00970 -0.1801 0.3342 0.5711
8.000 1.6738 0.01604 0.01009 -0.1796 0.3326 0.5782
8.250 1.6955 0.01644 0.01054 -0.1792 0.3305 0.5857
8.500 1.7160 0.01690 0.01105 -0.1786 0.3279 0.5936
8.750 1.7353 0.01744 0.01161 -0.1779 0.3253 0.6008
9.000 1.7533 0.01807 0.01226 -0.1771 0.3225 0.6074
9.250 1.7701 0.01879 0.01302 -0.1762 0.3195 0.6147
9.500 1.7870 0.01951 0.01377 -0.1754 0.3167 0.6218
9.750 1.8065 0.02009 0.01439 -0.1748 0.3148 0.6279
10.000 1.8246 0.02078 0.01514 -0.1742 0.3122 0.6347
10.250 1.8414 0.02155 0.01595 -0.1734 0.3092 0.6417
10.500 1.8554 0.02252 0.01694 -0.1724 0.3060 0.6480
10.750 1.8681 0.02360 0.01804 -0.1714 0.3027 0.6537
11.000 1.8816 0.02466 0.01915 -0.1704 0.3001 0.6601
11.250 1.8982 0.02548 0.02003 -0.1698 0.2980 0.6668
11.500 1.9121 0.02651 0.02110 -0.1689 0.2954 0.6726
11.750 1.9252 0.02761 0.02225 -0.1680 0.2926 0.6784
12.000 1.9352 0.02897 0.02365 -0.1670 0.2895 0.6846
12.250 1.9435 0.03046 0.02517 -0.1658 0.2863 0.6906
12.750 1.9651 0.03314 0.02795 -0.1639 0.2812 0.7014
13.000 1.9751 0.03458 0.02946 -0.1630 0.2784 0.7074
13.250 1.9834 0.03618 0.03110 -0.1620 0.2753 0.7132
13.750 1.9909 0.04025 0.03524 -0.1597 0.2682 0.7229
14.000 1.9994 0.04192 0.03698 -0.1589 0.2657 0.7284
14.250 2.0070 0.04368 0.03879 -0.1581 0.2626 0.7339
14.500 2.0098 0.04590 0.04105 -0.1570 0.2590 0.7385
14.750 2.0091 0.04847 0.04366 -0.1559 0.2550 0.7430
15.000 2.0097 0.05098 0.04623 -0.1549 0.2516 0.7476
15.250 2.0153 0.05298 0.04829 -0.1541 0.2483 0.7529
15.500 2.0147 0.05566 0.05102 -0.1532 0.2445 0.7575
15.750 2.0099 0.05874 0.05412 -0.1521 0.2400 0.7614
16.000 2.0062 0.06179 0.05724 -0.1512 0.2363 0.7656
16.250 2.0079 0.06428 0.05978 -0.1505 0.2324 0.7701
16.500 2.0009 0.06774 0.06329 -0.1496 0.2279 0.7743
16.750 1.9875 0.07190 0.06748 -0.1486 0.2230 0.7780
17.000 1.9871 0.07468 0.07031 -0.1481 0.2189 0.7819
17.250 1.9766 0.07863 0.07431 -0.1473 0.2136 0.7857
17.500 1.9623 0.08302 0.07873 -0.1466 0.2079 0.7891
17.750 1.9537 0.08681 0.08257 -0.1461 0.2026 0.7928
18.000 1.9348 0.09187 0.08766 -0.1456 0.1964 0.7959
18.250 1.9270 0.09565 0.09147 -0.1454 0.1911 0.7993
18.500 1.9113 0.10042 0.09628 -0.1452 0.1852 0.8024
18.750 1.8983 0.10487 0.10076 -0.1451 0.1798 0.8058
19.000 1.8866 0.10926 0.10519 -0.1452 0.1740 0.8092
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