MH 94 16.03% (mh94-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: MH 94 16.03% (mh94-il) Reynolds number: 1,000,000 Max Cl/Cd: 76.69 at α=8.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-mh94-il-1000000.txt Download as CSV file: xf-mh94-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: MH 94 16.03%
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.500 -0.8186 0.12754 0.12479 -0.0432 1.0000 0.0087
-19.250 -0.8599 0.11578 0.11276 -0.0492 1.0000 0.0084
-19.000 -0.8733 0.10964 0.10654 -0.0522 1.0000 0.0085
-18.750 -0.8891 0.10323 0.10001 -0.0553 1.0000 0.0086
-18.500 -0.9107 0.09613 0.09272 -0.0584 1.0000 0.0084
-18.250 -0.9180 0.09154 0.08807 -0.0605 1.0000 0.0085
-18.000 -0.9303 0.08630 0.08273 -0.0626 1.0000 0.0085
-17.750 -0.9426 0.08125 0.07754 -0.0645 1.0000 0.0084
-17.500 -0.9460 0.07749 0.07376 -0.0661 1.0000 0.0086
-17.250 -0.9551 0.07318 0.06935 -0.0675 1.0000 0.0086
-17.000 -0.9623 0.06927 0.06534 -0.0686 1.0000 0.0086
-16.750 -0.9696 0.06548 0.06145 -0.0695 1.0000 0.0086
-16.500 -0.9723 0.06231 0.05823 -0.0703 1.0000 0.0088
-16.250 -0.9775 0.05901 0.05485 -0.0709 1.0000 0.0089
-16.000 -0.9818 0.05599 0.05175 -0.0711 1.0000 0.0088
-15.750 -0.9879 0.05292 0.04858 -0.0710 1.0000 0.0088
-15.500 -0.9889 0.05046 0.04606 -0.0710 1.0000 0.0089
-15.250 -0.9951 0.04763 0.04314 -0.0704 1.0000 0.0088
-15.000 -0.9980 0.04525 0.04069 -0.0698 1.0000 0.0089
-14.750 -0.9989 0.04316 0.03854 -0.0691 1.0000 0.0090
-14.500 -1.0013 0.04105 0.03636 -0.0681 1.0000 0.0091
-14.250 -1.0017 0.03920 0.03445 -0.0669 1.0000 0.0092
-14.000 -1.0049 0.03723 0.03241 -0.0654 1.0000 0.0091
-13.750 -1.0043 0.03565 0.03077 -0.0640 1.0000 0.0093
-13.500 -1.0089 0.03376 0.02881 -0.0620 1.0000 0.0092
-13.250 -1.0078 0.03241 0.02740 -0.0601 1.0000 0.0094
-13.000 -1.0122 0.03075 0.02568 -0.0577 1.0000 0.0093
-12.750 -1.0124 0.02951 0.02439 -0.0554 1.0000 0.0094
-12.500 -1.0111 0.02826 0.02308 -0.0533 0.9999 0.0095
-12.250 -0.9942 0.02673 0.02149 -0.0543 0.9985 0.0095
-12.000 -0.9746 0.02548 0.02018 -0.0554 0.9968 0.0097
-11.750 -0.9541 0.02429 0.01892 -0.0565 0.9952 0.0098
-11.500 -0.9319 0.02321 0.01779 -0.0578 0.9938 0.0098
-11.250 -0.9125 0.02220 0.01673 -0.0582 0.9916 0.0100
-11.000 -0.8925 0.02134 0.01582 -0.0585 0.9889 0.0100
-10.750 -0.8685 0.02060 0.01504 -0.0593 0.9868 0.0101
-10.500 -0.8501 0.01921 0.01358 -0.0600 0.9844 0.0103
-10.250 -0.8250 0.01831 0.01262 -0.0612 0.9830 0.0105
-10.000 -0.8148 0.01762 0.01189 -0.0588 0.9774 0.0108
-9.750 -0.7897 0.01702 0.01127 -0.0591 0.9749 0.0109
-9.500 -0.7607 0.01641 0.01065 -0.0601 0.9733 0.0112
-9.250 -0.7301 0.01581 0.01002 -0.0613 0.9721 0.0116
-9.000 -0.6979 0.01528 0.00946 -0.0628 0.9712 0.0121
-8.750 -0.6777 0.01484 0.00900 -0.0617 0.9674 0.0124
-8.500 -0.6550 0.01434 0.00847 -0.0611 0.9636 0.0128
-8.250 -0.6256 0.01380 0.00793 -0.0619 0.9618 0.0138
-8.000 -0.5929 0.01337 0.00749 -0.0632 0.9607 0.0149
-7.750 -0.5598 0.01286 0.00699 -0.0647 0.9598 0.0167
-7.500 -0.5270 0.01239 0.00653 -0.0660 0.9588 0.0194
-7.250 -0.4947 0.01192 0.00610 -0.0672 0.9578 0.0246
-7.000 -0.4777 0.01155 0.00577 -0.0652 0.9522 0.0312
-6.750 -0.4519 0.01111 0.00539 -0.0650 0.9487 0.0419
-6.500 -0.4241 0.01060 0.00498 -0.0652 0.9462 0.0597
-6.250 -0.3955 0.01004 0.00456 -0.0657 0.9440 0.0858
-6.000 -0.3760 0.00951 0.00420 -0.0643 0.9390 0.1209
-5.750 -0.3555 0.00893 0.00384 -0.0630 0.9335 0.1664
-5.500 -0.3295 0.00837 0.00347 -0.0629 0.9299 0.2121
-5.250 -0.3052 0.00786 0.00317 -0.0624 0.9254 0.2591
-5.000 -0.2835 0.00747 0.00294 -0.0612 0.9186 0.3013
-4.750 -0.2564 0.00706 0.00269 -0.0612 0.9136 0.3439
-4.500 -0.2315 0.00675 0.00251 -0.0606 0.9070 0.3826
-4.250 -0.2054 0.00649 0.00235 -0.0602 0.8997 0.4154
-4.000 -0.1763 0.00631 0.00222 -0.0604 0.8931 0.4380
-3.750 -0.1499 0.00617 0.00212 -0.0600 0.8840 0.4608
-3.500 -0.1216 0.00602 0.00202 -0.0599 0.8755 0.4838
-3.250 -0.0940 0.00594 0.00194 -0.0597 0.8648 0.5004
-3.000 -0.0663 0.00587 0.00186 -0.0595 0.8538 0.5127
-2.750 -0.0382 0.00583 0.00179 -0.0594 0.8418 0.5225
-2.500 -0.0108 0.00581 0.00173 -0.0591 0.8278 0.5325
-2.250 0.0162 0.00579 0.00168 -0.0588 0.8131 0.5416
-2.000 0.0432 0.00579 0.00164 -0.0584 0.7978 0.5509
-1.750 0.0698 0.00580 0.00161 -0.0580 0.7816 0.5597
-1.500 0.0962 0.00583 0.00158 -0.0575 0.7647 0.5685
-1.250 0.1224 0.00586 0.00157 -0.0570 0.7473 0.5768
-1.000 0.1481 0.00591 0.00156 -0.0564 0.7285 0.5862
-0.750 0.1739 0.00597 0.00156 -0.0559 0.7096 0.5945
-0.500 0.1993 0.00603 0.00157 -0.0552 0.6898 0.6031
-0.250 0.2249 0.00612 0.00159 -0.0546 0.6696 0.6106
0.000 0.2498 0.00619 0.00161 -0.0539 0.6481 0.6186
0.250 0.2739 0.00632 0.00164 -0.0530 0.6223 0.6263
0.500 0.2976 0.00646 0.00168 -0.0520 0.5905 0.6336
0.750 0.3211 0.00662 0.00173 -0.0510 0.5589 0.6412
1.000 0.3453 0.00680 0.00178 -0.0502 0.5305 0.6483
1.250 0.3698 0.00692 0.00185 -0.0495 0.5053 0.6559
1.500 0.3946 0.00708 0.00192 -0.0488 0.4797 0.6634
1.750 0.4189 0.00726 0.00200 -0.0480 0.4537 0.6704
2.000 0.4435 0.00742 0.00209 -0.0473 0.4272 0.6777
2.250 0.4677 0.00764 0.00219 -0.0466 0.4001 0.6849
2.500 0.4921 0.00781 0.00229 -0.0459 0.3756 0.6920
2.750 0.5166 0.00800 0.00241 -0.0452 0.3518 0.6994
3.000 0.5410 0.00823 0.00252 -0.0445 0.3284 0.7062
3.250 0.5648 0.00842 0.00266 -0.0437 0.3061 0.7137
3.500 0.5892 0.00863 0.00279 -0.0430 0.2855 0.7210
3.750 0.6135 0.00884 0.00292 -0.0423 0.2666 0.7277
4.000 0.6375 0.00903 0.00307 -0.0416 0.2494 0.7349
4.250 0.6616 0.00925 0.00323 -0.0409 0.2329 0.7420
4.500 0.6854 0.00947 0.00338 -0.0401 0.2171 0.7487
4.750 0.7087 0.00969 0.00356 -0.0392 0.2013 0.7560
5.000 0.7321 0.00993 0.00373 -0.0384 0.1864 0.7629
5.500 0.7776 0.01040 0.00411 -0.0365 0.1590 0.7774
5.750 0.7999 0.01065 0.00431 -0.0355 0.1470 0.7843
6.000 0.8210 0.01087 0.00451 -0.0342 0.1364 0.7917
6.250 0.8418 0.01112 0.00473 -0.0329 0.1267 0.7998
6.500 0.8623 0.01139 0.00496 -0.0315 0.1184 0.8072
6.750 0.8835 0.01160 0.00520 -0.0303 0.1129 0.8152
7.250 0.9246 0.01212 0.00572 -0.0276 0.1035 0.8317
7.500 0.9459 0.01235 0.00596 -0.0264 0.1007 0.8405
7.750 0.9656 0.01260 0.00624 -0.0249 0.0976 0.8495
8.000 0.9844 0.01294 0.00658 -0.0234 0.0940 0.8595
8.250 1.0044 0.01314 0.00685 -0.0219 0.0926 0.8698
8.500 1.0246 0.01336 0.00711 -0.0206 0.0907 0.8806
8.750 1.0431 0.01361 0.00741 -0.0190 0.0888 0.8935
9.000 1.0602 0.01388 0.00772 -0.0171 0.0870 0.9086
9.500 1.0945 0.01449 0.00848 -0.0134 0.0833 0.9632
9.750 1.1244 0.01479 0.00883 -0.0144 0.0823 1.0000
10.000 1.1451 0.01512 0.00916 -0.0135 0.0811 1.0000
10.250 1.1646 0.01547 0.00954 -0.0123 0.0799 1.0000
10.500 1.1833 0.01587 0.00993 -0.0111 0.0785 1.0000
10.750 1.2008 0.01633 0.01038 -0.0097 0.0771 1.0000
11.000 1.2153 0.01691 0.01098 -0.0080 0.0757 1.0000
11.250 1.2297 0.01751 0.01162 -0.0062 0.0746 1.0000
11.500 1.2482 0.01791 0.01205 -0.0051 0.0740 1.0000
11.750 1.2656 0.01837 0.01254 -0.0038 0.0734 1.0000
12.000 1.2824 0.01885 0.01307 -0.0025 0.0726 1.0000
12.250 1.2987 0.01937 0.01362 -0.0012 0.0717 1.0000
12.500 1.3142 0.01995 0.01422 0.0001 0.0709 1.0000
12.750 1.3291 0.02056 0.01486 0.0015 0.0701 1.0000
13.000 1.3430 0.02124 0.01556 0.0029 0.0692 1.0000
13.250 1.3542 0.02208 0.01643 0.0046 0.0683 1.0000
13.500 1.3614 0.02318 0.01757 0.0066 0.0673 1.0000
13.750 1.3695 0.02427 0.01871 0.0083 0.0665 1.0000
14.000 1.3849 0.02494 0.01944 0.0093 0.0661 1.0000
14.250 1.3983 0.02576 0.02031 0.0104 0.0656 1.0000
14.500 1.4106 0.02667 0.02127 0.0115 0.0651 1.0000
14.750 1.4221 0.02765 0.02230 0.0126 0.0645 1.0000
15.000 1.4339 0.02864 0.02334 0.0136 0.0637 1.0000
15.250 1.4433 0.02984 0.02460 0.0146 0.0633 1.0000
15.500 1.4533 0.03103 0.02583 0.0155 0.0626 1.0000
15.750 1.4624 0.03232 0.02716 0.0163 0.0620 1.0000
16.000 1.4696 0.03382 0.02871 0.0171 0.0614 1.0000
16.250 1.4737 0.03562 0.03056 0.0180 0.0607 1.0000
16.500 1.4742 0.03781 0.03281 0.0187 0.0599 1.0000
16.750 1.4746 0.04009 0.03516 0.0194 0.0593 1.0000
17.000 1.4835 0.04168 0.03683 0.0195 0.0590 1.0000
17.250 1.4907 0.04350 0.03872 0.0197 0.0586 1.0000
17.500 1.4975 0.04540 0.04069 0.0197 0.0581 1.0000
17.750 1.5033 0.04744 0.04282 0.0196 0.0576 1.0000
18.000 1.5075 0.04971 0.04515 0.0194 0.0571 1.0000
18.250 1.5106 0.05216 0.04767 0.0190 0.0566 1.0000
18.500 1.5134 0.05471 0.05030 0.0186 0.0561 1.0000
18.750 1.5150 0.05747 0.05313 0.0179 0.0556 1.0000
19.000 1.5157 0.06039 0.05611 0.0171 0.0551 1.0000
19.250 1.5146 0.06361 0.05939 0.0161 0.0545 1.0000
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