MH 94 16.03% (mh94-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: MH 94 16.03% (mh94-il) Reynolds number: 1,000,000 Max Cl/Cd: 75.82 at α=8.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-mh94-il-1000000-n5.txt Download as CSV file: xf-mh94-il-1000000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.000 -0.9488 0.09857 0.09490 -0.0558 1.0000 0.0059
-18.750 -0.9628 0.09293 0.08917 -0.0583 1.0000 0.0059
-18.500 -0.9791 0.08706 0.08319 -0.0608 1.0000 0.0058
-18.250 -0.9861 0.08272 0.07877 -0.0624 1.0000 0.0058
-18.000 -0.9985 0.07773 0.07369 -0.0643 1.0000 0.0059
-17.750 -1.0105 0.07295 0.06881 -0.0660 1.0000 0.0058
-17.500 -1.0204 0.06858 0.06435 -0.0675 1.0000 0.0059
-17.250 -1.0306 0.06433 0.06000 -0.0687 1.0000 0.0059
-17.000 -1.0361 0.06083 0.05642 -0.0695 1.0000 0.0059
-16.750 -1.0437 0.05720 0.05271 -0.0702 1.0000 0.0059
-16.500 -1.0516 0.05371 0.04913 -0.0707 1.0000 0.0060
-16.250 -1.0611 0.05019 0.04552 -0.0709 1.0000 0.0061
-16.000 -1.0633 0.04762 0.04289 -0.0708 1.0000 0.0060
-15.750 -1.0689 0.04483 0.04003 -0.0704 1.0000 0.0060
-15.500 -1.0705 0.04260 0.03773 -0.0698 1.0000 0.0061
-15.250 -1.0771 0.04002 0.03507 -0.0690 1.0000 0.0061
-15.000 -1.0798 0.03793 0.03291 -0.0679 1.0000 0.0061
-14.750 -1.0833 0.03585 0.03077 -0.0667 1.0000 0.0062
-14.500 -1.0731 0.03387 0.02872 -0.0676 0.9994 0.0062
-14.250 -1.0612 0.03205 0.02685 -0.0685 0.9985 0.0063
-14.000 -1.0497 0.03030 0.02503 -0.0692 0.9975 0.0063
-13.750 -1.0353 0.02883 0.02351 -0.0699 0.9964 0.0064
-13.500 -1.0209 0.02729 0.02191 -0.0706 0.9952 0.0064
-13.250 -1.0036 0.02607 0.02065 -0.0713 0.9941 0.0065
-13.000 -0.9873 0.02477 0.01929 -0.0720 0.9930 0.0066
-12.750 -0.9730 0.02366 0.01814 -0.0718 0.9911 0.0067
-12.500 -0.9558 0.02266 0.01710 -0.0719 0.9893 0.0067
-12.250 -0.9375 0.02165 0.01605 -0.0722 0.9876 0.0068
-12.000 -0.9170 0.02076 0.01512 -0.0727 0.9862 0.0069
-11.750 -0.8948 0.01991 0.01423 -0.0734 0.9849 0.0070
-11.500 -0.8712 0.01914 0.01343 -0.0742 0.9838 0.0071
-11.250 -0.8464 0.01838 0.01263 -0.0752 0.9829 0.0073
-11.000 -0.8287 0.01776 0.01198 -0.0745 0.9802 0.0073
-10.750 -0.8097 0.01716 0.01136 -0.0739 0.9772 0.0075
-10.500 -0.7867 0.01654 0.01070 -0.0741 0.9752 0.0076
-10.250 -0.7610 0.01597 0.01010 -0.0746 0.9736 0.0077
-10.000 -0.7334 0.01539 0.00949 -0.0755 0.9725 0.0080
-9.750 -0.7047 0.01486 0.00894 -0.0765 0.9713 0.0081
-9.500 -0.6890 0.01444 0.00850 -0.0746 0.9669 0.0084
-9.250 -0.6699 0.01402 0.00807 -0.0734 0.9629 0.0089
-9.000 -0.6440 0.01361 0.00766 -0.0735 0.9604 0.0093
-8.750 -0.6173 0.01322 0.00724 -0.0736 0.9584 0.0097
-8.500 -0.5945 0.01290 0.00691 -0.0729 0.9552 0.0102
-8.250 -0.5774 0.01258 0.00659 -0.0710 0.9498 0.0109
-8.000 -0.5535 0.01224 0.00625 -0.0705 0.9462 0.0118
-7.750 -0.5270 0.01191 0.00591 -0.0705 0.9434 0.0128
-7.500 -0.5066 0.01163 0.00563 -0.0691 0.9384 0.0142
-7.250 -0.4847 0.01135 0.00535 -0.0681 0.9330 0.0160
-7.000 -0.4584 0.01104 0.00505 -0.0679 0.9290 0.0188
-6.750 -0.4348 0.01077 0.00479 -0.0671 0.9237 0.0220
-6.500 -0.4113 0.01049 0.00453 -0.0664 0.9172 0.0271
-6.250 -0.3842 0.01020 0.00426 -0.0663 0.9120 0.0326
-6.000 -0.3610 0.00993 0.00402 -0.0655 0.9044 0.0406
-5.750 -0.3354 0.00963 0.00375 -0.0651 0.8970 0.0526
-5.500 -0.3111 0.00933 0.00351 -0.0645 0.8886 0.0681
-5.250 -0.2872 0.00894 0.00322 -0.0639 0.8792 0.0960
-5.000 -0.2650 0.00851 0.00295 -0.0630 0.8685 0.1343
-4.750 -0.2424 0.00808 0.00267 -0.0622 0.8575 0.1813
-4.500 -0.2205 0.00763 0.00242 -0.0612 0.8449 0.2350
-4.250 -0.1977 0.00725 0.00221 -0.0604 0.8318 0.2850
-4.000 -0.1730 0.00704 0.00207 -0.0598 0.8182 0.3168
-3.750 -0.1490 0.00681 0.00193 -0.0590 0.8031 0.3554
-3.500 -0.1252 0.00661 0.00182 -0.0583 0.7868 0.3945
-3.250 -0.1004 0.00651 0.00174 -0.0576 0.7691 0.4218
-3.000 -0.0752 0.00648 0.00168 -0.0569 0.7504 0.4381
-2.750 -0.0499 0.00647 0.00163 -0.0563 0.7306 0.4501
-2.500 -0.0245 0.00650 0.00159 -0.0557 0.7096 0.4616
-2.250 0.0006 0.00652 0.00156 -0.0550 0.6887 0.4727
-2.000 0.0259 0.00656 0.00154 -0.0544 0.6679 0.4829
-1.750 0.0513 0.00660 0.00152 -0.0538 0.6473 0.4935
-1.500 0.0768 0.00665 0.00151 -0.0532 0.6272 0.5024
-1.250 0.1023 0.00671 0.00151 -0.0526 0.6073 0.5125
-1.000 0.1277 0.00677 0.00152 -0.0520 0.5861 0.5224
-0.750 0.1531 0.00685 0.00153 -0.0515 0.5649 0.5327
-0.500 0.1786 0.00692 0.00155 -0.0509 0.5428 0.5418
-0.250 0.2042 0.00702 0.00157 -0.0504 0.5203 0.5505
0.000 0.2294 0.00713 0.00161 -0.0498 0.4962 0.5581
0.250 0.2542 0.00728 0.00166 -0.0491 0.4687 0.5664
0.500 0.2779 0.00750 0.00172 -0.0483 0.4301 0.5735
0.750 0.3014 0.00772 0.00180 -0.0474 0.3907 0.5814
1.000 0.3258 0.00792 0.00188 -0.0467 0.3605 0.5893
1.250 0.3512 0.00806 0.00195 -0.0462 0.3391 0.5964
1.500 0.3767 0.00821 0.00203 -0.0457 0.3186 0.6043
1.750 0.4022 0.00836 0.00212 -0.0452 0.3003 0.6114
2.000 0.4274 0.00851 0.00221 -0.0447 0.2814 0.6189
2.250 0.4527 0.00868 0.00231 -0.0441 0.2631 0.6266
2.500 0.4778 0.00884 0.00242 -0.0436 0.2465 0.6335
2.750 0.5031 0.00899 0.00253 -0.0431 0.2324 0.6414
3.250 0.5529 0.00934 0.00277 -0.0419 0.2035 0.6563
3.500 0.5779 0.00951 0.00290 -0.0414 0.1903 0.6637
3.750 0.6027 0.00968 0.00303 -0.0408 0.1777 0.6705
4.000 0.6273 0.00986 0.00318 -0.0401 0.1666 0.6779
4.250 0.6516 0.01006 0.00333 -0.0395 0.1551 0.6847
4.500 0.6756 0.01026 0.00349 -0.0387 0.1441 0.6913
4.750 0.6996 0.01045 0.00366 -0.0380 0.1339 0.6987
5.000 0.7235 0.01066 0.00383 -0.0373 0.1252 0.7052
5.250 0.7469 0.01087 0.00402 -0.0365 0.1173 0.7120
5.500 0.7706 0.01104 0.00419 -0.0357 0.1119 0.7195
6.000 0.8157 0.01142 0.00455 -0.0337 0.1024 0.7326
6.250 0.8379 0.01160 0.00474 -0.0326 0.0983 0.7403
6.500 0.8593 0.01183 0.00495 -0.0314 0.0941 0.7468
6.750 0.8816 0.01200 0.00516 -0.0304 0.0917 0.7541
7.000 0.9037 0.01221 0.00538 -0.0294 0.0890 0.7615
7.250 0.9253 0.01244 0.00562 -0.0282 0.0867 0.7687
7.500 0.9462 0.01268 0.00587 -0.0270 0.0841 0.7766
7.750 0.9681 0.01289 0.00611 -0.0260 0.0827 0.7840
8.000 0.9895 0.01310 0.00636 -0.0249 0.0813 0.7921
8.250 1.0107 0.01333 0.00662 -0.0237 0.0798 0.8003
8.500 1.0309 0.01360 0.00691 -0.0225 0.0778 0.8081
8.750 1.0508 0.01387 0.00721 -0.0211 0.0761 0.8174
9.000 1.0707 0.01415 0.00752 -0.0198 0.0746 0.8261
9.250 1.0909 0.01439 0.00781 -0.0186 0.0738 0.8362
9.500 1.1105 0.01465 0.00813 -0.0173 0.0729 0.8460
9.750 1.1297 0.01492 0.00845 -0.0159 0.0720 0.8572
10.000 1.1482 0.01520 0.00879 -0.0144 0.0708 0.8694
10.250 1.1657 0.01551 0.00915 -0.0128 0.0698 0.8826
10.500 1.1820 0.01583 0.00953 -0.0109 0.0687 0.9001
10.750 1.1968 0.01615 0.00993 -0.0089 0.0674 0.9244
11.000 1.2218 0.01650 0.01038 -0.0089 0.0664 0.9686
11.250 1.2431 0.01686 0.01078 -0.0083 0.0658 1.0000
11.500 1.2616 0.01726 0.01120 -0.0072 0.0651 1.0000
11.750 1.2792 0.01769 0.01167 -0.0059 0.0645 1.0000
12.000 1.2964 0.01816 0.01216 -0.0046 0.0637 1.0000
12.250 1.3131 0.01865 0.01267 -0.0033 0.0629 1.0000
12.500 1.3288 0.01919 0.01324 -0.0019 0.0623 1.0000
12.750 1.3445 0.01975 0.01382 -0.0006 0.0615 1.0000
13.000 1.3587 0.02039 0.01448 0.0008 0.0605 1.0000
13.250 1.3720 0.02110 0.01522 0.0023 0.0596 1.0000
13.500 1.3862 0.02177 0.01593 0.0037 0.0591 1.0000
13.750 1.4009 0.02243 0.01663 0.0049 0.0587 1.0000
14.000 1.4147 0.02314 0.01740 0.0062 0.0582 1.0000
14.250 1.4282 0.02390 0.01820 0.0074 0.0577 1.0000
14.500 1.4408 0.02473 0.01908 0.0086 0.0571 1.0000
14.750 1.4528 0.02562 0.02002 0.0098 0.0564 1.0000
15.000 1.4642 0.02658 0.02102 0.0110 0.0558 1.0000
15.250 1.4748 0.02761 0.02210 0.0121 0.0553 1.0000
15.500 1.4844 0.02876 0.02328 0.0132 0.0547 1.0000
15.750 1.4932 0.03001 0.02457 0.0142 0.0540 1.0000
16.000 1.5005 0.03140 0.02601 0.0152 0.0533 1.0000
16.250 1.5065 0.03295 0.02762 0.0162 0.0528 1.0000
16.500 1.5161 0.03428 0.02901 0.0168 0.0524 1.0000
16.750 1.5236 0.03582 0.03063 0.0174 0.0521 1.0000
17.000 1.5313 0.03740 0.03228 0.0179 0.0516 1.0000
17.250 1.5378 0.03913 0.03408 0.0183 0.0511 1.0000
17.500 1.5437 0.04097 0.03599 0.0186 0.0506 1.0000
17.750 1.5486 0.04298 0.03806 0.0188 0.0500 1.0000
18.000 1.5523 0.04517 0.04032 0.0188 0.0494 1.0000
18.250 1.5543 0.04760 0.04282 0.0187 0.0490 1.0000
18.500 1.5554 0.05021 0.04549 0.0184 0.0485 1.0000
18.750 1.5554 0.05304 0.04839 0.0180 0.0481 1.0000
19.000 1.5524 0.05630 0.05173 0.0173 0.0475 1.0000
19.250 1.5479 0.05984 0.05535 0.0163 0.0469 1.0000
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