MH 150 23.89% (mh150-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: MH 150 23.89% (mh150-il) Reynolds number: 500,000 Max Cl/Cd: 90.52 at α=5.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-mh150-il-500000.txt Download as CSV file: xf-mh150-il-500000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.000 -0.6343 0.08872 0.08454 -0.0784 0.9619 0.0302
-16.750 -0.6393 0.08559 0.08136 -0.0788 0.9430 0.0309
-16.500 -0.6423 0.08270 0.07838 -0.0791 0.9263 0.0318
-16.250 -0.6438 0.07962 0.07520 -0.0800 0.9120 0.0328
-16.000 -0.6494 0.07603 0.07155 -0.0813 0.8998 0.0338
-15.750 -0.6537 0.07248 0.06792 -0.0827 0.8880 0.0349
-15.500 -0.6538 0.06931 0.06466 -0.0842 0.8776 0.0364
-15.250 -0.6587 0.06563 0.06089 -0.0860 0.8673 0.0378
-15.000 -0.6617 0.06211 0.05731 -0.0879 0.8581 0.0396
-14.750 -0.6626 0.05885 0.05395 -0.0896 0.8486 0.0416
-14.500 -0.6683 0.05510 0.05013 -0.0916 0.8401 0.0436
-14.250 -0.6678 0.05196 0.04693 -0.0935 0.8316 0.0463
-14.000 -0.6725 0.04835 0.04325 -0.0956 0.8231 0.0489
-13.750 -0.6735 0.04516 0.03998 -0.0976 0.8153 0.0521
-13.500 -0.6740 0.04198 0.03677 -0.0997 0.8072 0.0558
-13.250 -0.6750 0.03888 0.03359 -0.1017 0.7994 0.0597
-13.000 -0.6732 0.03607 0.03072 -0.1036 0.7921 0.0642
-12.750 -0.6691 0.03351 0.02813 -0.1055 0.7843 0.0692
-12.500 -0.6650 0.03100 0.02555 -0.1073 0.7768 0.0746
-12.250 -0.6583 0.02867 0.02320 -0.1092 0.7699 0.0802
-12.000 -0.6487 0.02658 0.02109 -0.1110 0.7627 0.0864
-11.750 -0.6366 0.02475 0.01920 -0.1128 0.7556 0.0929
-11.500 -0.6220 0.02320 0.01761 -0.1144 0.7489 0.0999
-11.250 -0.6088 0.02168 0.01609 -0.1159 0.7420 0.1070
-11.000 -0.5894 0.02031 0.01468 -0.1181 0.7354 0.1148
-10.750 -0.5665 0.01914 0.01347 -0.1204 0.7290 0.1232
-10.500 -0.5406 0.01807 0.01241 -0.1229 0.7227 0.1320
-10.000 -0.4826 0.01630 0.01056 -0.1281 0.7097 0.1511
-9.750 -0.4506 0.01550 0.00977 -0.1310 0.7040 0.1611
-9.500 -0.4176 0.01482 0.00909 -0.1337 0.6977 0.1716
-9.250 -0.3842 0.01427 0.00851 -0.1361 0.6913 0.1833
-9.000 -0.3510 0.01384 0.00805 -0.1383 0.6852 0.1962
-8.750 -0.3176 0.01345 0.00768 -0.1402 0.6795 0.2092
-8.500 -0.2842 0.01311 0.00735 -0.1420 0.6735 0.2212
-8.250 -0.2514 0.01290 0.00709 -0.1435 0.6674 0.2318
-8.000 -0.2186 0.01277 0.00690 -0.1448 0.6617 0.2417
-7.750 -0.1856 0.01255 0.00670 -0.1462 0.6556 0.2501
-7.500 -0.1531 0.01247 0.00653 -0.1473 0.6497 0.2577
-7.250 -0.1209 0.01237 0.00635 -0.1484 0.6438 0.2644
-7.000 -0.0881 0.01223 0.00624 -0.1496 0.6385 0.2710
-6.750 -0.0557 0.01219 0.00610 -0.1506 0.6324 0.2769
-6.500 -0.0238 0.01207 0.00593 -0.1515 0.6265 0.2829
-6.250 0.0084 0.01202 0.00585 -0.1525 0.6210 0.2886
-6.000 0.0408 0.01196 0.00575 -0.1535 0.6156 0.2939
-5.750 0.0729 0.01191 0.00562 -0.1544 0.6097 0.2985
-5.500 0.1044 0.01183 0.00551 -0.1553 0.6038 0.3040
-5.250 0.1364 0.01179 0.00545 -0.1562 0.5986 0.3089
-5.000 0.1685 0.01176 0.00537 -0.1570 0.5931 0.3135
-4.750 0.2003 0.01174 0.00527 -0.1579 0.5876 0.3175
-4.500 0.2316 0.01170 0.00519 -0.1587 0.5817 0.3228
-4.250 0.2636 0.01164 0.00515 -0.1595 0.5769 0.3275
-4.000 0.2954 0.01162 0.00509 -0.1604 0.5714 0.3321
-3.750 0.3270 0.01166 0.00503 -0.1611 0.5662 0.3360
-3.500 0.3581 0.01164 0.00498 -0.1619 0.5608 0.3413
-3.250 0.3900 0.01158 0.00496 -0.1628 0.5562 0.3463
-3.000 0.4216 0.01158 0.00494 -0.1636 0.5509 0.3512
-2.750 0.4528 0.01164 0.00490 -0.1643 0.5457 0.3558
-2.500 0.4839 0.01167 0.00489 -0.1650 0.5405 0.3613
-2.250 0.5157 0.01163 0.00490 -0.1659 0.5363 0.3667
-2.000 0.5471 0.01165 0.00491 -0.1667 0.5315 0.3721
-1.750 0.5781 0.01171 0.00490 -0.1673 0.5268 0.3767
-1.500 0.6089 0.01178 0.00492 -0.1681 0.5216 0.3825
-1.250 0.6403 0.01177 0.00497 -0.1689 0.5174 0.3887
-1.000 0.6715 0.01181 0.00500 -0.1696 0.5128 0.3948
-0.750 0.7022 0.01188 0.00502 -0.1703 0.5083 0.4003
-0.500 0.7330 0.01195 0.00508 -0.1710 0.5038 0.4072
-0.250 0.7636 0.01205 0.00517 -0.1716 0.4996 0.4140
0.000 0.7944 0.01212 0.00523 -0.1723 0.4958 0.4205
0.250 0.8253 0.01214 0.00531 -0.1731 0.4915 0.4286
0.500 0.8555 0.01224 0.00539 -0.1736 0.4871 0.4363
0.750 0.8850 0.01244 0.00549 -0.1741 0.4824 0.4432
1.000 0.9156 0.01249 0.00562 -0.1748 0.4789 0.4515
1.250 0.9458 0.01257 0.00573 -0.1754 0.4752 0.4598
1.500 0.9757 0.01268 0.00583 -0.1760 0.4713 0.4679
1.750 1.0052 0.01280 0.00597 -0.1765 0.4675 0.4767
2.000 1.0341 0.01303 0.00614 -0.1769 0.4632 0.4852
2.250 1.0636 0.01315 0.00630 -0.1774 0.4598 0.4933
2.500 1.0928 0.01325 0.00645 -0.1778 0.4562 0.5019
2.750 1.1216 0.01340 0.00659 -0.1782 0.4525 0.5099
3.000 1.1501 0.01355 0.00677 -0.1785 0.4488 0.5186
3.250 1.1778 0.01379 0.00698 -0.1787 0.4451 0.5276
3.500 1.2061 0.01402 0.00720 -0.1790 0.4417 0.5358
3.750 1.2341 0.01414 0.00741 -0.1793 0.4388 0.5442
4.000 1.2616 0.01431 0.00760 -0.1794 0.4354 0.5526
4.250 1.2887 0.01450 0.00780 -0.1796 0.4319 0.5603
4.500 1.3149 0.01473 0.00804 -0.1795 0.4284 0.5684
4.750 1.3413 0.01508 0.00832 -0.1796 0.4244 0.5769
5.000 1.3676 0.01526 0.00858 -0.1795 0.4219 0.5848
5.250 1.3932 0.01546 0.00885 -0.1794 0.4191 0.5928
5.500 1.4185 0.01569 0.00910 -0.1793 0.4160 0.6006
5.750 1.4429 0.01594 0.00937 -0.1790 0.4128 0.6080
6.000 1.4658 0.01624 0.00968 -0.1784 0.4096 0.6158
6.250 1.4893 0.01664 0.01003 -0.1780 0.4058 0.6237
6.500 1.5105 0.01690 0.01037 -0.1772 0.4036 0.6309
6.750 1.5320 0.01719 0.01075 -0.1765 0.4010 0.6383
7.000 1.5536 0.01753 0.01113 -0.1759 0.3981 0.6460
7.250 1.5747 0.01790 0.01152 -0.1752 0.3951 0.6531
7.500 1.5948 0.01831 0.01196 -0.1744 0.3922 0.6601
7.750 1.6156 0.01879 0.01242 -0.1737 0.3891 0.6676
8.000 1.6372 0.01925 0.01289 -0.1732 0.3862 0.6747
8.250 1.6553 0.01971 0.01346 -0.1722 0.3839 0.6814
8.500 1.6737 0.02021 0.01403 -0.1713 0.3811 0.6884
8.750 1.6924 0.02075 0.01459 -0.1705 0.3784 0.6954
9.000 1.7101 0.02130 0.01520 -0.1696 0.3757 0.7018
9.250 1.7274 0.02192 0.01584 -0.1686 0.3728 0.7084
9.500 1.7483 0.02250 0.01636 -0.1680 0.3693 0.7153
9.750 1.7636 0.02319 0.01716 -0.1670 0.3673 0.7215
10.000 1.7786 0.02393 0.01800 -0.1659 0.3649 0.7276
10.250 1.7939 0.02470 0.01884 -0.1650 0.3621 0.7343
10.500 1.8090 0.02551 0.01969 -0.1641 0.3593 0.7406
10.750 1.8234 0.02633 0.02055 -0.1630 0.3565 0.7463
11.000 1.8387 0.02715 0.02136 -0.1620 0.3534 0.7525
11.250 1.8546 0.02800 0.02223 -0.1612 0.3505 0.7590
11.500 1.8652 0.02910 0.02346 -0.1600 0.3481 0.7644
11.750 1.8763 0.03021 0.02466 -0.1589 0.3452 0.7702
12.000 1.8875 0.03137 0.02587 -0.1579 0.3424 0.7765
12.250 1.8991 0.03250 0.02703 -0.1569 0.3395 0.7820
12.500 1.9113 0.03352 0.02806 -0.1558 0.3365 0.7873
12.750 1.9244 0.03454 0.02911 -0.1548 0.3335 0.7934
13.000 1.9316 0.03612 0.03080 -0.1538 0.3310 0.7992
13.250 1.9384 0.03769 0.03247 -0.1527 0.3282 0.8040
13.500 1.9467 0.03918 0.03404 -0.1517 0.3253 0.8096
13.750 1.9548 0.04076 0.03564 -0.1508 0.3222 0.8157
14.000 1.9653 0.04200 0.03688 -0.1498 0.3189 0.8205
14.250 1.9739 0.04348 0.03842 -0.1489 0.3161 0.8256
14.500 1.9765 0.04569 0.04076 -0.1480 0.3132 0.8314
14.750 1.9805 0.04778 0.04294 -0.1472 0.3100 0.8366
15.000 1.9847 0.04980 0.04503 -0.1464 0.3067 0.8415
15.250 1.9913 0.05156 0.04678 -0.1455 0.3034 0.8471
15.500 2.0000 0.05311 0.04834 -0.1448 0.3000 0.8525
15.750 1.9975 0.05597 0.05136 -0.1440 0.2969 0.8573
16.000 1.9961 0.05879 0.05428 -0.1433 0.2933 0.8628
16.250 1.9978 0.06127 0.05681 -0.1428 0.2896 0.8681
16.500 2.0023 0.06326 0.05879 -0.1420 0.2859 0.8732
16.750 2.0025 0.06590 0.06152 -0.1415 0.2825 0.8789
17.000 1.9951 0.06955 0.06530 -0.1410 0.2785 0.8841
17.250 1.9919 0.07265 0.06847 -0.1405 0.2744 0.8896
17.500 1.9933 0.07515 0.07095 -0.1400 0.2703 0.8958
17.750 1.9902 0.07821 0.07411 -0.1396 0.2664 0.9015
18.000 1.9790 0.08241 0.07843 -0.1394 0.2619 0.9075
18.250 1.9729 0.08591 0.08197 -0.1391 0.2573 0.9145
18.500 1.9746 0.08829 0.08433 -0.1387 0.2527 0.9245
18.750 1.9569 0.09326 0.08948 -0.1385 0.2480 0.9377
19.000 1.9477 0.09690 0.09317 -0.1383 0.2430 0.9999
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