MH 150 23.89% (mh150-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: MH 150 23.89% (mh150-il) Reynolds number: 500,000 Max Cl/Cd: 88.06 at α=4.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-mh150-il-500000-n5.txt Download as CSV file: xf-mh150-il-500000-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 = 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 0.06451 -0.0813 0.8005 0.0262
-15.250 -0.6629 0.06636 0.06102 -0.0833 0.7935 0.0271
-15.000 -0.6621 0.06314 0.05772 -0.0852 0.7861 0.0282
-14.750 -0.6613 0.05996 0.05445 -0.0870 0.7786 0.0293
-14.500 -0.6610 0.05676 0.05118 -0.0889 0.7720 0.0305
-14.250 -0.6597 0.05365 0.04801 -0.0908 0.7652 0.0319
-14.000 -0.6578 0.05069 0.04497 -0.0927 0.7580 0.0334
-13.750 -0.6560 0.04775 0.04194 -0.0945 0.7513 0.0350
-13.500 -0.6524 0.04499 0.03913 -0.0963 0.7449 0.0369
-13.250 -0.6501 0.04211 0.03619 -0.0982 0.7380 0.0388
-13.000 -0.6452 0.03959 0.03359 -0.0999 0.7314 0.0412
-12.750 -0.6409 0.03700 0.03095 -0.1018 0.7253 0.0437
-12.500 -0.6346 0.03466 0.02856 -0.1035 0.7185 0.0466
-12.250 -0.6279 0.03237 0.02620 -0.1052 0.7119 0.0499
-12.000 -0.6197 0.03021 0.02399 -0.1069 0.7062 0.0534
-11.750 -0.6092 0.02824 0.02199 -0.1086 0.6999 0.0575
-11.500 -0.5974 0.02639 0.02010 -0.1103 0.6932 0.0621
-11.000 -0.5715 0.02309 0.01674 -0.1134 0.6813 0.0727
-10.750 -0.5555 0.02168 0.01532 -0.1151 0.6751 0.0790
-10.500 -0.5352 0.02039 0.01399 -0.1172 0.6687 0.0861
-10.250 -0.5118 0.01923 0.01281 -0.1196 0.6629 0.0937
-10.000 -0.4856 0.01820 0.01178 -0.1220 0.6569 0.1018
-9.750 -0.4573 0.01731 0.01087 -0.1245 0.6509 0.1100
-9.500 -0.4274 0.01655 0.01006 -0.1270 0.6450 0.1187
-9.250 -0.3957 0.01578 0.00930 -0.1297 0.6395 0.1288
-9.000 -0.3628 0.01508 0.00861 -0.1325 0.6331 0.1408
-8.750 -0.3293 0.01445 0.00798 -0.1351 0.6270 0.1538
-8.000 -0.2290 0.01310 0.00667 -0.1414 0.6103 0.1945
-7.750 -0.1961 0.01282 0.00637 -0.1430 0.6042 0.2063
-7.500 -0.1631 0.01258 0.00613 -0.1445 0.5990 0.2160
-7.250 -0.1306 0.01242 0.00593 -0.1457 0.5938 0.2250
-7.000 -0.0977 0.01224 0.00574 -0.1470 0.5881 0.2330
-6.750 -0.0659 0.01215 0.00558 -0.1480 0.5823 0.2406
-6.500 -0.0331 0.01201 0.00543 -0.1492 0.5772 0.2472
-6.250 -0.0007 0.01191 0.00530 -0.1503 0.5715 0.2539
-6.000 0.0310 0.01187 0.00519 -0.1511 0.5661 0.2593
-5.750 0.0631 0.01179 0.00507 -0.1522 0.5609 0.2647
-5.500 0.0957 0.01170 0.00497 -0.1532 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
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