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 = 0.500 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -18.750 -0.6351 0.11749 0.11340 -0.0582 0.9346 0.0192 -18.500 -0.6401 0.11367 0.10951 -0.0595 0.9183 0.0195 -18.250 -0.6455 0.10973 0.10547 -0.0610 0.9038 0.0198 -18.000 -0.6483 0.10594 0.10159 -0.0626 0.8908 0.0202 -17.750 -0.6516 0.10206 0.09761 -0.0644 0.8796 0.0206 -17.500 -0.6531 0.09842 0.09387 -0.0661 0.8684 0.0211 -17.250 -0.6544 0.09477 0.09012 -0.0679 0.8588 0.0215 -17.000 -0.6548 0.09123 0.08648 -0.0697 0.8491 0.0220 -16.750 -0.6572 0.08749 0.08264 -0.0716 0.8405 0.0225 -16.500 -0.6597 0.08365 0.07872 -0.0737 0.8323 0.0231 -16.250 -0.6609 0.08008 0.07507 -0.0756 0.8236 0.0238 -16.000 -0.6617 0.07659 0.07148 -0.0775 0.8160 0.0246 -15.750 -0.6605 0.07334 0.06816 -0.0793 0.8082 0.0254 -15.500 -0.6621 0.06978 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0.5559 0.2702 -5.250 0.1275 0.01166 0.00488 -0.1541 0.5502 0.2752 -5.000 0.1590 0.01165 0.00479 -0.1549 0.5448 0.2792 -4.750 0.1911 0.01160 0.00472 -0.1559 0.5401 0.2841 -4.500 0.2234 0.01154 0.00465 -0.1568 0.5353 0.2889 -4.250 0.2551 0.01153 0.00460 -0.1577 0.5299 0.2933 -4.000 0.2862 0.01156 0.00455 -0.1583 0.5245 0.2970 -3.750 0.3181 0.01153 0.00450 -0.1593 0.5199 0.3017 -3.500 0.3503 0.01150 0.00447 -0.1602 0.5157 0.3065 -3.250 0.3819 0.01150 0.00445 -0.1611 0.5109 0.3112 -3.000 0.4129 0.01155 0.00443 -0.1617 0.5058 0.3153 -2.750 0.4441 0.01158 0.00442 -0.1625 0.5009 0.3201 -2.500 0.4762 0.01156 0.00441 -0.1635 0.4967 0.3253 -2.250 0.5076 0.01158 0.00442 -0.1643 0.4923 0.3303 -2.000 0.5385 0.01163 0.00443 -0.1649 0.4879 0.3345 -1.750 0.5693 0.01169 0.00445 -0.1656 0.4836 0.3385 -1.500 0.6007 0.01172 0.00448 -0.1665 0.4797 0.3437 -1.250 0.6321 0.01175 0.00452 -0.1673 0.4755 0.3493 -1.000 0.6628 0.01182 0.00455 -0.1679 0.4710 0.3542 -0.750 0.6932 0.01190 0.00460 -0.1685 0.4666 0.3586 -0.250 0.7547 0.01204 0.00474 -0.1700 0.4594 0.3703 0.000 0.7852 0.01211 0.00481 -0.1706 0.4558 0.3763 0.250 0.8158 0.01218 0.00489 -0.1713 0.4519 0.3825 0.500 0.8458 0.01229 0.00498 -0.1719 0.4478 0.3890 0.750 0.8750 0.01243 0.00509 -0.1723 0.4436 0.3953 1.000 0.9051 0.01252 0.00519 -0.1729 0.4404 0.4012 1.250 0.9355 0.01260 0.00531 -0.1736 0.4370 0.4087 1.500 0.9651 0.01272 0.00543 -0.1741 0.4334 0.4165 1.750 0.9942 0.01285 0.00556 -0.1745 0.4299 0.4236 2.000 1.0230 0.01301 0.00571 -0.1749 0.4264 0.4313 2.250 1.0515 0.01317 0.00587 -0.1753 0.4232 0.4387 2.500 1.0807 0.01329 0.00602 -0.1757 0.4201 0.4456 2.750 1.1096 0.01342 0.00618 -0.1762 0.4165 0.4535 3.000 1.1375 0.01359 0.00636 -0.1764 0.4129 0.4618 3.250 1.1650 0.01378 0.00655 -0.1766 0.4096 0.4697 3.500 1.1917 0.01400 0.00678 -0.1767 0.4065 0.4784 3.750 1.2191 0.01419 0.00698 -0.1769 0.4039 0.4860 4.000 1.2467 0.01435 0.00719 -0.1771 0.4012 0.4934 4.250 1.2735 0.01454 0.00741 -0.1772 0.3980 0.5014 4.500 1.2990 0.01477 0.00765 -0.1771 0.3946 0.5092 4.750 1.3236 0.01503 0.00793 -0.1769 0.3913 0.5173 5.000 1.3453 0.01533 0.00823 -0.1762 0.3882 0.5258 5.250 1.3684 0.01559 0.00851 -0.1757 0.3858 0.5331 5.500 1.3931 0.01582 0.00881 -0.1755 0.3834 0.5405 5.750 1.4171 0.01611 0.00915 -0.1752 0.3806 0.5489 6.000 1.4398 0.01646 0.00951 -0.1748 0.3775 0.5565 6.250 1.4615 0.01685 0.00993 -0.1743 0.3743 0.5643 6.500 1.4818 0.01730 0.01040 -0.1736 0.3713 0.5724 6.750 1.5020 0.01778 0.01088 -0.1729 0.3687 0.5797 7.000 1.5247 0.01814 0.01132 -0.1725 0.3666 0.5874 7.250 1.5462 0.01856 0.01181 -0.1721 0.3639 0.5954 7.500 1.5664 0.01906 0.01233 -0.1715 0.3610 0.6027 7.750 1.5856 0.01962 0.01293 -0.1708 0.3580 0.6098 8.000 1.6036 0.02025 0.01360 -0.1700 0.3553 0.6175 8.250 1.6202 0.02098 0.01433 -0.1691 0.3525 0.6248 8.500 1.6390 0.02161 0.01502 -0.1684 0.3502 0.6313 8.750 1.6584 0.02220 0.01569 -0.1679 0.3477 0.6386 9.000 1.6764 0.02290 0.01644 -0.1672 0.3451 0.6459 9.250 1.6934 0.02366 0.01723 -0.1665 0.3424 0.6521 9.500 1.7086 0.02454 0.01817 -0.1656 0.3395 0.6586 9.750 1.7224 0.02553 0.01918 -0.1646 0.3367 0.6655 10.000 1.7354 0.02659 0.02026 -0.1636 0.3340 0.6719 10.250 1.7524 0.02740 0.02116 -0.1630 0.3318 0.6778 10.500 1.7679 0.02832 0.02216 -0.1623 0.3292 0.6843 10.750 1.7814 0.02939 0.02329 -0.1615 0.3263 0.6910 11.000 1.7939 0.03055 0.02448 -0.1606 0.3234 0.6967 11.250 1.8033 0.03193 0.02591 -0.1595 0.3203 0.7023 11.500 1.8116 0.03341 0.02740 -0.1583 0.3173 0.7084 11.750 1.8250 0.03457 0.02866 -0.1576 0.3149 0.7147 12.000 1.8372 0.03583 0.02999 -0.1569 0.3120 0.7200 12.250 1.8468 0.03730 0.03153 -0.1560 0.3089 0.7255 12.500 1.8551 0.03890 0.03318 -0.1551 0.3059 0.7314 12.750 1.8613 0.04073 0.03503 -0.1541 0.3029 0.7371 13.000 1.8682 0.04251 0.03686 -0.1531 0.3000 0.7419 13.250 1.8784 0.04404 0.03850 -0.1525 0.2974 0.7472 13.500 1.8861 0.04581 0.04034 -0.1517 0.2944 0.7529 13.750 1.8929 0.04770 0.04228 -0.1510 0.2912 0.7584 14.000 1.8956 0.04998 0.04461 -0.1501 0.2878 0.7628 14.250 1.8973 0.05236 0.04702 -0.1491 0.2844 0.7674 14.500 1.9040 0.05433 0.04909 -0.1485 0.2818 0.7727 14.750 1.9099 0.05638 0.05122 -0.1479 0.2786 0.7781 15.000 1.9112 0.05893 0.05384 -0.1472 0.2749 0.7823 15.250 1.9110 0.06162 0.05656 -0.1464 0.2711 0.7866 15.500 1.9095 0.06450 0.05950 -0.1457 0.2678 0.7911 15.750 1.9135 0.06683 0.06191 -0.1452 0.2645 0.7961 16.000 1.9124 0.06973 0.06489 -0.1446 0.2606 0.8004 16.250 1.9095 0.07280 0.06801 -0.1440 0.2565 0.8044 16.500 1.9032 0.07631 0.07155 -0.1434 0.2526 0.8084 16.750 1.9046 0.07901 0.07434 -0.1431 0.2489 0.8129 17.250 1.8932 0.08601 0.08145 -0.1423 0.2401 0.8207 17.500 1.8867 0.08966 0.08516 -0.1420 0.2361 0.8246 17.750 1.8839 0.09290 0.08848 -0.1418 0.2317 0.8288 18.000 1.8745 0.09698 0.09261 -0.1417 0.2269 0.8325 18.250 1.8671 0.10075 0.09640 -0.1416 0.2224 0.8360 18.500 1.8608 0.10449 0.10022 -0.1417 0.2179 0.8397 18.750 1.8537 0.10833 0.10411 -0.1419 0.2128 0.8437 19.000 1.8424 0.11273 0.10853 -0.1422 0.2079 0.8476 19.250 1.8390 0.11617 0.11204 -0.1425 0.2031 0.8516