MH 102 16.99% (mh102-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: MH 102 16.99% (mh102-il) Reynolds number: 1,000,000 Max Cl/Cd: 110.16 at α=6.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-mh102-il-1000000-n5.txt Download as CSV file: xf-mh102-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: MH 102 16.99%
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
------ -------- --------- --------- -------- -------- --------
-17.250 -0.8826 0.08818 0.08455 -0.0474 1.0000 0.0054
-17.000 -0.8958 0.08278 0.07908 -0.0501 1.0000 0.0054
-16.750 -0.9153 0.07655 0.07274 -0.0533 1.0000 0.0054
-16.500 -0.9353 0.07052 0.06662 -0.0564 1.0000 0.0054
-16.250 -0.9637 0.06355 0.05953 -0.0600 1.0000 0.0054
-16.000 -0.9869 0.05740 0.05327 -0.0631 1.0000 0.0054
-15.750 -1.0091 0.05140 0.04715 -0.0662 1.0000 0.0053
-15.500 -1.0295 0.04556 0.04119 -0.0693 1.0000 0.0054
-15.250 -1.0451 0.04024 0.03575 -0.0722 1.0000 0.0053
-15.000 -1.0561 0.03551 0.03089 -0.0751 1.0000 0.0054
-14.750 -1.0629 0.03158 0.02684 -0.0773 1.0000 0.0055
-14.500 -1.0660 0.02861 0.02378 -0.0785 1.0000 0.0055
-14.250 -1.0677 0.02634 0.02142 -0.0786 1.0000 0.0056
-14.000 -1.0692 0.02462 0.01962 -0.0775 1.0000 0.0056
-13.750 -1.0725 0.02326 0.01818 -0.0751 1.0000 0.0057
-13.500 -1.0764 0.02234 0.01721 -0.0715 1.0000 0.0057
-13.250 -1.0641 0.02148 0.01629 -0.0703 0.9978 0.0058
-13.000 -1.0426 0.02063 0.01539 -0.0705 0.9902 0.0059
-12.500 -0.9908 0.01886 0.01352 -0.0723 0.9709 0.0064
-12.250 -0.9516 0.01801 0.01262 -0.0756 0.9539 0.0067
-12.000 -0.9077 0.01722 0.01175 -0.0797 0.9242 0.0071
-11.500 -0.8674 0.01641 0.01063 -0.0776 0.8571 0.0077
-11.250 -0.8490 0.01604 0.01013 -0.0761 0.8343 0.0080
-11.000 -0.8297 0.01565 0.00965 -0.0748 0.8146 0.0083
-10.750 -0.8096 0.01527 0.00918 -0.0736 0.7969 0.0091
-10.500 -0.7881 0.01493 0.00876 -0.0726 0.7808 0.0096
-10.250 -0.7665 0.01457 0.00832 -0.0716 0.7659 0.0105
-10.000 -0.7441 0.01424 0.00793 -0.0707 0.7516 0.0114
-9.750 -0.7212 0.01391 0.00753 -0.0699 0.7376 0.0126
-9.500 -0.6978 0.01359 0.00716 -0.0692 0.7253 0.0143
-9.250 -0.6743 0.01326 0.00679 -0.0684 0.7137 0.0165
-9.000 -0.6502 0.01295 0.00643 -0.0678 0.7023 0.0191
-8.750 -0.6260 0.01263 0.00608 -0.0672 0.6911 0.0227
-8.500 -0.6016 0.01234 0.00576 -0.0665 0.6793 0.0265
-8.250 -0.5767 0.01203 0.00543 -0.0660 0.6688 0.0313
-8.000 -0.5521 0.01173 0.00511 -0.0654 0.6590 0.0376
-7.750 -0.5271 0.01140 0.00479 -0.0649 0.6493 0.0460
-7.500 -0.5025 0.01106 0.00446 -0.0644 0.6390 0.0572
-7.250 -0.4776 0.01072 0.00414 -0.0638 0.6284 0.0711
-7.000 -0.4534 0.01030 0.00381 -0.0633 0.6190 0.0916
-6.750 -0.4285 0.00994 0.00352 -0.0628 0.6097 0.1137
-6.500 -0.4025 0.00969 0.00332 -0.0624 0.6013 0.1310
-6.250 -0.3759 0.00950 0.00316 -0.0621 0.5921 0.1448
-6.000 -0.3491 0.00935 0.00301 -0.0618 0.5829 0.1568
-5.750 -0.3217 0.00924 0.00289 -0.0616 0.5730 0.1647
-5.500 -0.2943 0.00915 0.00278 -0.0614 0.5646 0.1728
-5.250 -0.2668 0.00903 0.00268 -0.0612 0.5563 0.1823
-5.000 -0.2390 0.00898 0.00259 -0.0610 0.5484 0.1881
-4.750 -0.2110 0.00891 0.00249 -0.0608 0.5406 0.1928
-4.250 -0.1553 0.00881 0.00233 -0.0605 0.5238 0.2021
-4.000 -0.1273 0.00879 0.00226 -0.0604 0.5155 0.2052
-3.750 -0.0993 0.00873 0.00218 -0.0602 0.5090 0.2103
-3.500 -0.0713 0.00868 0.00212 -0.0601 0.5019 0.2153
-3.250 -0.0433 0.00867 0.00207 -0.0600 0.4948 0.2193
-3.000 -0.0150 0.00864 0.00202 -0.0599 0.4879 0.2233
-2.750 0.0128 0.00861 0.00197 -0.0597 0.4803 0.2293
-2.500 0.0409 0.00859 0.00193 -0.0596 0.4744 0.2342
-2.250 0.0692 0.00858 0.00190 -0.0595 0.4684 0.2382
-2.000 0.0970 0.00856 0.00186 -0.0594 0.4616 0.2445
-1.750 0.1252 0.00854 0.00184 -0.0593 0.4559 0.2509
-1.500 0.1534 0.00854 0.00182 -0.0592 0.4500 0.2558
-1.250 0.1812 0.00853 0.00181 -0.0591 0.4437 0.2625
-1.000 0.2094 0.00852 0.00180 -0.0590 0.4384 0.2694
-0.750 0.2375 0.00852 0.00179 -0.0589 0.4327 0.2768
-0.500 0.2652 0.00852 0.00180 -0.0587 0.4269 0.2850
-0.250 0.2934 0.00854 0.00180 -0.0586 0.4220 0.2917
0.000 0.3214 0.00852 0.00181 -0.0586 0.4172 0.3003
0.250 0.3493 0.00855 0.00183 -0.0584 0.4116 0.3087
0.500 0.3768 0.00856 0.00186 -0.0583 0.4065 0.3198
0.750 0.4050 0.00856 0.00188 -0.0582 0.4023 0.3292
1.000 0.4329 0.00856 0.00191 -0.0581 0.3976 0.3398
1.250 0.4605 0.00860 0.00195 -0.0580 0.3926 0.3497
1.500 0.4881 0.00862 0.00199 -0.0578 0.3883 0.3624
1.750 0.5160 0.00862 0.00203 -0.0577 0.3843 0.3766
2.000 0.5436 0.00864 0.00208 -0.0576 0.3794 0.3897
2.500 0.5983 0.00871 0.00220 -0.0572 0.3705 0.4190
2.750 0.6259 0.00871 0.00226 -0.0571 0.3663 0.4369
3.000 0.6530 0.00874 0.00233 -0.0569 0.3613 0.4563
3.250 0.6797 0.00879 0.00242 -0.0566 0.3559 0.4755
3.500 0.7070 0.00880 0.00250 -0.0565 0.3518 0.4979
3.750 0.7338 0.00881 0.00258 -0.0562 0.3466 0.5265
4.000 0.7600 0.00885 0.00269 -0.0559 0.3408 0.5570
4.250 0.7863 0.00886 0.00279 -0.0556 0.3361 0.5898
4.500 0.8125 0.00887 0.00290 -0.0552 0.3302 0.6268
4.750 0.8377 0.00892 0.00303 -0.0547 0.3237 0.6634
5.000 0.8633 0.00894 0.00315 -0.0542 0.3186 0.7027
5.250 0.8880 0.00897 0.00329 -0.0536 0.3115 0.7448
5.500 0.9119 0.00903 0.00344 -0.0528 0.3048 0.7875
5.750 0.9351 0.00904 0.00359 -0.0518 0.2978 0.8356
6.000 0.9566 0.00912 0.00378 -0.0504 0.2900 0.8874
6.250 0.9847 0.00919 0.00395 -0.0503 0.2831 0.9399
6.500 1.0300 0.00946 0.00420 -0.0542 0.2730 0.9765
6.750 1.0685 0.00970 0.00440 -0.0567 0.2638 0.9981
7.000 1.0927 0.00995 0.00461 -0.0561 0.2560 1.0000
7.250 1.1150 0.01016 0.00480 -0.0551 0.2487 1.0000
7.500 1.1364 0.01042 0.00501 -0.0540 0.2415 1.0000
7.750 1.1587 0.01063 0.00522 -0.0530 0.2346 1.0000
8.250 1.2016 0.01114 0.00568 -0.0508 0.2215 1.0000
8.500 1.2217 0.01145 0.00595 -0.0495 0.2139 1.0000
8.750 1.2426 0.01171 0.00620 -0.0483 0.2080 1.0000
9.000 1.2626 0.01199 0.00646 -0.0471 0.2019 1.0000
9.250 1.2808 0.01231 0.00676 -0.0455 0.1953 1.0000
9.500 1.2979 0.01259 0.00704 -0.0436 0.1895 1.0000
9.750 1.3121 0.01296 0.00738 -0.0413 0.1833 1.0000
10.000 1.3286 0.01326 0.00769 -0.0395 0.1786 1.0000
10.250 1.3436 0.01363 0.00805 -0.0375 0.1729 1.0000
10.500 1.3576 0.01406 0.00846 -0.0354 0.1672 1.0000
10.750 1.3732 0.01445 0.00886 -0.0336 0.1622 1.0000
11.000 1.3856 0.01498 0.00937 -0.0315 0.1561 1.0000
11.250 1.3998 0.01546 0.00986 -0.0297 0.1516 1.0000
11.500 1.4130 0.01600 0.01041 -0.0278 0.1467 1.0000
11.750 1.4238 0.01669 0.01109 -0.0258 0.1416 1.0000
12.000 1.4372 0.01729 0.01172 -0.0242 0.1378 1.0000
12.250 1.4482 0.01806 0.01249 -0.0225 0.1329 1.0000
12.500 1.4575 0.01896 0.01340 -0.0208 0.1282 1.0000
12.750 1.4692 0.01979 0.01425 -0.0194 0.1245 1.0000
13.000 1.4781 0.02084 0.01531 -0.0180 0.1200 1.0000
13.250 1.4866 0.02198 0.01647 -0.0166 0.1162 1.0000
13.500 1.4957 0.02315 0.01767 -0.0155 0.1119 1.0000
13.750 1.5027 0.02453 0.01906 -0.0144 0.1080 1.0000
14.000 1.5090 0.02603 0.02058 -0.0134 0.1041 1.0000
14.250 1.5160 0.02754 0.02213 -0.0126 0.1004 1.0000
14.500 1.5188 0.02946 0.02406 -0.0117 0.0962 1.0000
14.750 1.5235 0.03129 0.02593 -0.0111 0.0927 1.0000
15.000 1.5262 0.03334 0.02801 -0.0105 0.0890 1.0000
15.250 1.5256 0.03576 0.03045 -0.0100 0.0853 1.0000
15.500 1.5291 0.03786 0.03260 -0.0097 0.0829 1.0000
15.750 1.5282 0.04044 0.03522 -0.0095 0.0793 1.0000
16.000 1.5258 0.04323 0.03805 -0.0093 0.0765 1.0000
16.250 1.5260 0.04583 0.04071 -0.0093 0.0741 1.0000
16.500 1.5248 0.04862 0.04355 -0.0093 0.0718 1.0000
16.750 1.5189 0.05196 0.04693 -0.0095 0.0687 1.0000
17.000 1.5157 0.05507 0.05009 -0.0097 0.0665 1.0000
17.250 1.5112 0.05837 0.05345 -0.0100 0.0637 1.0000
17.500 1.5049 0.06192 0.05704 -0.0104 0.0614 1.0000
17.750 1.4990 0.06548 0.06065 -0.0109 0.0591 1.0000
18.000 1.4931 0.06912 0.06435 -0.0115 0.0569 1.0000
18.250 1.4831 0.07330 0.06857 -0.0123 0.0543 1.0000
18.500 1.4778 0.07694 0.07227 -0.0131 0.0530 1.0000
18.750 1.4726 0.08063 0.07603 -0.0139 0.0508 1.0000
19.000 1.4650 0.08471 0.08016 -0.0149 0.0492 1.0000
19.250 1.4549 0.08918 0.08468 -0.0162 0.0472 1.0000
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