MH 95 15.86% (mh95-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: MH 95 15.86% (mh95-il) Reynolds number: 1,000,000 Max Cl/Cd: 74.28 at α=8.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-mh95-il-1000000-n5.txt Download as CSV file: xf-mh95-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: MH 95 15.86%
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
------ -------- --------- --------- -------- -------- --------
-19.750 -0.8558 0.12243 0.11958 -0.0476 1.0000 0.0089
-19.500 -0.8831 0.11354 0.11055 -0.0521 1.0000 0.0089
-19.250 -0.9062 0.10566 0.10255 -0.0560 1.0000 0.0089
-19.000 -0.9304 0.09785 0.09460 -0.0599 1.0000 0.0089
-18.750 -0.9483 0.09130 0.08794 -0.0631 1.0000 0.0089
-18.500 -0.9665 0.08486 0.08137 -0.0662 1.0000 0.0089
-18.250 -0.9832 0.07885 0.07525 -0.0689 1.0000 0.0089
-18.000 -0.9951 0.07373 0.07003 -0.0712 1.0000 0.0090
-17.750 -1.0097 0.06841 0.06459 -0.0733 1.0000 0.0089
-17.500 -1.0193 0.06396 0.06003 -0.0750 1.0000 0.0089
-17.250 -1.0278 0.05989 0.05585 -0.0763 1.0000 0.0089
-17.000 -1.0369 0.05591 0.05177 -0.0773 1.0000 0.0090
-16.750 -1.0419 0.05264 0.04842 -0.0778 1.0000 0.0090
-16.500 -1.0492 0.04934 0.04502 -0.0781 1.0000 0.0091
-16.250 -1.0547 0.04645 0.04205 -0.0779 1.0000 0.0091
-16.000 -1.0574 0.04404 0.03955 -0.0773 1.0000 0.0091
-15.750 -1.0614 0.04169 0.03712 -0.0764 1.0000 0.0092
-15.500 -1.0629 0.03975 0.03512 -0.0753 1.0000 0.0092
-15.250 -1.0666 0.03777 0.03306 -0.0737 1.0000 0.0092
-15.000 -1.0603 0.03583 0.03104 -0.0738 0.9996 0.0093
-14.750 -1.0502 0.03400 0.02913 -0.0743 0.9988 0.0093
-14.500 -1.0380 0.03236 0.02741 -0.0747 0.9979 0.0095
-14.250 -1.0253 0.03076 0.02573 -0.0752 0.9968 0.0095
-14.000 -1.0118 0.02926 0.02417 -0.0756 0.9955 0.0096
-13.750 -0.9960 0.02803 0.02287 -0.0759 0.9943 0.0097
-13.500 -0.9790 0.02687 0.02165 -0.0763 0.9933 0.0098
-13.250 -0.9668 0.02562 0.02033 -0.0758 0.9914 0.0098
-13.000 -0.9503 0.02464 0.01930 -0.0756 0.9896 0.0098
-12.750 -0.9329 0.02366 0.01826 -0.0756 0.9879 0.0099
-12.500 -0.9142 0.02270 0.01725 -0.0757 0.9863 0.0100
-12.250 -0.8929 0.02191 0.01640 -0.0760 0.9850 0.0101
-12.000 -0.8708 0.02113 0.01558 -0.0765 0.9839 0.0101
-11.750 -0.8514 0.02002 0.01442 -0.0768 0.9828 0.0103
-11.500 -0.8283 0.01922 0.01358 -0.0774 0.9819 0.0105
-11.250 -0.8141 0.01859 0.01292 -0.0758 0.9780 0.0107
-11.000 -0.7930 0.01795 0.01226 -0.0756 0.9757 0.0108
-10.750 -0.7701 0.01728 0.01156 -0.0758 0.9739 0.0110
-10.500 -0.7439 0.01675 0.01101 -0.0763 0.9725 0.0112
-10.250 -0.7166 0.01620 0.01043 -0.0771 0.9713 0.0114
-10.000 -0.6881 0.01563 0.00984 -0.0782 0.9702 0.0115
-9.750 -0.6582 0.01512 0.00930 -0.0793 0.9692 0.0118
-9.500 -0.6423 0.01472 0.00888 -0.0775 0.9638 0.0120
-9.250 -0.6181 0.01426 0.00839 -0.0774 0.9605 0.0122
-9.000 -0.5916 0.01382 0.00793 -0.0777 0.9579 0.0123
-8.750 -0.5630 0.01340 0.00748 -0.0784 0.9557 0.0126
-8.500 -0.5452 0.01310 0.00716 -0.0767 0.9506 0.0127
-8.250 -0.5277 0.01269 0.00672 -0.0750 0.9453 0.0130
-8.000 -0.5037 0.01231 0.00633 -0.0746 0.9417 0.0134
-7.750 -0.4838 0.01202 0.00603 -0.0732 0.9370 0.0137
-7.500 -0.4665 0.01178 0.00577 -0.0712 0.9310 0.0141
-7.250 -0.4422 0.01150 0.00547 -0.0707 0.9266 0.0145
-7.000 -0.4184 0.01125 0.00520 -0.0700 0.9221 0.0149
-6.750 -0.3982 0.01104 0.00498 -0.0686 0.9157 0.0153
-6.500 -0.3743 0.01079 0.00471 -0.0679 0.9101 0.0160
-6.250 -0.3513 0.01055 0.00447 -0.0670 0.9043 0.0169
-6.000 -0.3289 0.01035 0.00425 -0.0660 0.8971 0.0181
-5.750 -0.3039 0.01013 0.00402 -0.0655 0.8906 0.0197
-5.500 -0.2816 0.00994 0.00383 -0.0644 0.8825 0.0218
-5.250 -0.2575 0.00971 0.00360 -0.0637 0.8740 0.0269
-5.000 -0.2353 0.00950 0.00341 -0.0626 0.8642 0.0351
-4.750 -0.2124 0.00927 0.00321 -0.0616 0.8537 0.0477
-4.500 -0.1903 0.00903 0.00301 -0.0605 0.8416 0.0647
-4.250 -0.1690 0.00876 0.00282 -0.0593 0.8287 0.0894
-4.000 -0.1485 0.00847 0.00262 -0.0579 0.8151 0.1239
-3.750 -0.1288 0.00816 0.00243 -0.0564 0.7997 0.1667
-3.500 -0.1082 0.00793 0.00228 -0.0550 0.7838 0.2035
-3.250 -0.0882 0.00767 0.00213 -0.0535 0.7665 0.2467
-3.000 -0.0689 0.00740 0.00200 -0.0519 0.7482 0.2998
-2.750 -0.0496 0.00712 0.00187 -0.0503 0.7293 0.3568
-2.500 -0.0316 0.00678 0.00173 -0.0485 0.7098 0.4297
-2.250 -0.0129 0.00647 0.00162 -0.0468 0.6902 0.5005
-2.000 0.0080 0.00631 0.00155 -0.0454 0.6703 0.5492
-1.750 0.0311 0.00626 0.00152 -0.0444 0.6516 0.5779
-1.500 0.0548 0.00625 0.00150 -0.0435 0.6333 0.6023
-1.250 0.0790 0.00627 0.00150 -0.0427 0.6148 0.6214
-1.000 0.1035 0.00631 0.00150 -0.0419 0.5963 0.6369
-0.750 0.1282 0.00637 0.00152 -0.0412 0.5774 0.6496
-0.500 0.1531 0.00646 0.00153 -0.0405 0.5582 0.6616
-0.250 0.1777 0.00654 0.00156 -0.0398 0.5388 0.6722
0.000 0.2026 0.00663 0.00160 -0.0391 0.5196 0.6820
0.250 0.2272 0.00674 0.00164 -0.0384 0.4988 0.6922
0.500 0.2523 0.00685 0.00169 -0.0378 0.4795 0.7002
0.750 0.2769 0.00697 0.00174 -0.0372 0.4584 0.7076
1.000 0.3019 0.00711 0.00180 -0.0365 0.4378 0.7141
1.250 0.3264 0.00725 0.00187 -0.0359 0.4167 0.7196
1.500 0.3502 0.00743 0.00195 -0.0351 0.3923 0.7255
1.750 0.3732 0.00768 0.00204 -0.0341 0.3599 0.7314
2.000 0.3966 0.00788 0.00214 -0.0333 0.3328 0.7373
2.250 0.4209 0.00804 0.00224 -0.0326 0.3142 0.7435
2.500 0.4456 0.00820 0.00233 -0.0320 0.2988 0.7492
2.750 0.4700 0.00837 0.00243 -0.0313 0.2832 0.7540
3.000 0.4941 0.00853 0.00255 -0.0306 0.2685 0.7590
3.250 0.5185 0.00869 0.00266 -0.0299 0.2561 0.7638
3.500 0.5433 0.00884 0.00276 -0.0293 0.2452 0.7680
3.750 0.5673 0.00900 0.00288 -0.0286 0.2338 0.7717
4.000 0.5901 0.00918 0.00300 -0.0277 0.2211 0.7753
4.250 0.6135 0.00932 0.00312 -0.0268 0.2112 0.7792
4.500 0.6364 0.00948 0.00325 -0.0259 0.2022 0.7831
4.750 0.6592 0.00966 0.00337 -0.0249 0.1924 0.7866
5.000 0.6818 0.00983 0.00352 -0.0239 0.1829 0.7900
5.250 0.7035 0.01004 0.00369 -0.0228 0.1722 0.7937
5.500 0.7254 0.01025 0.00386 -0.0217 0.1620 0.7975
5.750 0.7475 0.01046 0.00404 -0.0207 0.1529 0.8013
6.000 0.7690 0.01071 0.00423 -0.0196 0.1436 0.8050
6.250 0.7908 0.01093 0.00444 -0.0185 0.1354 0.8086
6.500 0.8118 0.01116 0.00465 -0.0174 0.1282 0.8125
6.750 0.8327 0.01142 0.00488 -0.0162 0.1205 0.8164
7.000 0.8539 0.01166 0.00511 -0.0151 0.1144 0.8204
7.250 0.8751 0.01192 0.00534 -0.0140 0.1091 0.8244
7.500 0.8956 0.01217 0.00558 -0.0127 0.1045 0.8284
7.750 0.9166 0.01239 0.00583 -0.0116 0.1012 0.8326
8.000 0.9370 0.01265 0.00609 -0.0104 0.0978 0.8369
8.250 0.9571 0.01294 0.00636 -0.0092 0.0939 0.8411
8.500 0.9778 0.01317 0.00662 -0.0081 0.0918 0.8454
8.750 0.9976 0.01343 0.00690 -0.0068 0.0895 0.8502
9.000 1.0170 0.01371 0.00720 -0.0055 0.0871 0.8553
9.250 1.0362 0.01403 0.00752 -0.0042 0.0847 0.8601
9.500 1.0552 0.01432 0.00784 -0.0029 0.0829 0.8647
9.750 1.0743 0.01459 0.00816 -0.0016 0.0818 0.8703
10.000 1.0933 0.01489 0.00849 -0.0003 0.0803 0.8762
10.250 1.1114 0.01521 0.00885 0.0011 0.0789 0.8819
10.500 1.1284 0.01556 0.00923 0.0026 0.0774 0.8884
10.750 1.1454 0.01594 0.00963 0.0041 0.0757 0.8951
11.000 1.1608 0.01635 0.01009 0.0059 0.0738 0.9023
11.250 1.1778 0.01669 0.01049 0.0074 0.0732 0.9110
11.500 1.1940 0.01704 0.01090 0.0090 0.0724 0.9206
11.750 1.2095 0.01742 0.01135 0.0106 0.0716 0.9326
12.000 1.2261 0.01783 0.01183 0.0120 0.0705 0.9490
12.250 1.2523 0.01834 0.01239 0.0112 0.0694 0.9693
12.500 1.2745 0.01890 0.01298 0.0110 0.0677 1.0000
12.750 1.2895 0.01949 0.01359 0.0123 0.0667 1.0000
13.000 1.3029 0.02018 0.01429 0.0138 0.0654 1.0000
13.250 1.3186 0.02075 0.01491 0.0149 0.0649 1.0000
13.500 1.3339 0.02135 0.01556 0.0161 0.0642 1.0000
13.750 1.3485 0.02200 0.01625 0.0172 0.0632 1.0000
14.000 1.3623 0.02271 0.01699 0.0184 0.0622 1.0000
14.250 1.3751 0.02350 0.01781 0.0196 0.0612 1.0000
14.500 1.3871 0.02435 0.01869 0.0208 0.0602 1.0000
14.750 1.3983 0.02529 0.01966 0.0220 0.0591 1.0000
15.000 1.4081 0.02634 0.02074 0.0233 0.0580 1.0000
15.250 1.4184 0.02738 0.02183 0.0244 0.0574 1.0000
15.500 1.4302 0.02836 0.02287 0.0253 0.0568 1.0000
15.750 1.4406 0.02947 0.02404 0.0262 0.0562 1.0000
16.000 1.4502 0.03066 0.02529 0.0271 0.0555 1.0000
16.250 1.4593 0.03193 0.02661 0.0279 0.0545 1.0000
16.500 1.4674 0.03333 0.02806 0.0286 0.0538 1.0000
16.750 1.4743 0.03487 0.02964 0.0293 0.0530 1.0000
17.000 1.4801 0.03656 0.03138 0.0299 0.0522 1.0000
17.250 1.4840 0.03847 0.03334 0.0304 0.0512 1.0000
17.500 1.4892 0.04033 0.03527 0.0307 0.0506 1.0000
17.750 1.4949 0.04220 0.03721 0.0309 0.0501 1.0000
18.000 1.5003 0.04415 0.03924 0.0310 0.0491 1.0000
18.250 1.5040 0.04633 0.04148 0.0310 0.0483 1.0000
18.500 1.5060 0.04874 0.04396 0.0309 0.0475 1.0000
18.750 1.5065 0.05138 0.04666 0.0305 0.0465 1.0000
19.000 1.5045 0.05440 0.04974 0.0300 0.0456 1.0000
19.250 1.5021 0.05755 0.05296 0.0294 0.0451 1.0000
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