MH 94 16.03% (mh94-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: MH 94 16.03% (mh94-il) Reynolds number: 500,000 Max Cl/Cd: 61.35 at α=7.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-mh94-il-500000-n5.txt Download as CSV file: xf-mh94-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.7766 0.14044 0.13685 -0.0362 1.0000 0.0081
-19.500 -0.7943 0.13272 0.12900 -0.0402 1.0000 0.0081
-19.250 -0.8115 0.12538 0.12151 -0.0438 1.0000 0.0080
-19.000 -0.8257 0.11887 0.11489 -0.0470 1.0000 0.0080
-18.750 -0.8392 0.11266 0.10857 -0.0500 1.0000 0.0080
-18.500 -0.8507 0.10694 0.10273 -0.0526 1.0000 0.0080
-18.250 -0.8607 0.10162 0.09732 -0.0550 1.0000 0.0080
-18.000 -0.8725 0.09615 0.09174 -0.0574 1.0000 0.0080
-17.750 -0.8810 0.09135 0.08684 -0.0594 1.0000 0.0080
-17.500 -0.8910 0.08645 0.08185 -0.0614 1.0000 0.0081
-17.250 -0.8995 0.08189 0.07720 -0.0632 1.0000 0.0081
-17.000 -0.9061 0.07776 0.07297 -0.0646 1.0000 0.0081
-16.750 -0.9130 0.07371 0.06882 -0.0659 1.0000 0.0081
-16.500 -0.9189 0.06990 0.06493 -0.0671 1.0000 0.0082
-16.250 -0.9258 0.06609 0.06104 -0.0681 1.0000 0.0083
-16.000 -0.9295 0.06282 0.05769 -0.0688 1.0000 0.0082
-15.750 -0.9350 0.05947 0.05426 -0.0693 1.0000 0.0083
-15.500 -0.9379 0.05653 0.05124 -0.0696 1.0000 0.0083
-15.250 -0.9429 0.05350 0.04813 -0.0697 1.0000 0.0083
-15.000 -0.9460 0.05081 0.04537 -0.0696 1.0000 0.0083
-14.750 -0.9483 0.04831 0.04281 -0.0693 1.0000 0.0084
-14.500 -0.9511 0.04592 0.04035 -0.0687 1.0000 0.0085
-14.250 -0.9527 0.04376 0.03812 -0.0680 1.0000 0.0085
-14.000 -0.9552 0.04163 0.03591 -0.0670 1.0000 0.0086
-13.750 -0.9560 0.03974 0.03397 -0.0658 1.0000 0.0086
-13.500 -0.9590 0.03777 0.03193 -0.0644 1.0000 0.0086
-13.250 -0.9592 0.03614 0.03024 -0.0628 1.0000 0.0087
-13.000 -0.9620 0.03441 0.02844 -0.0610 1.0000 0.0088
-12.750 -0.9626 0.03295 0.02693 -0.0590 1.0000 0.0089
-12.500 -0.9605 0.03152 0.02544 -0.0574 0.9998 0.0089
-12.250 -0.9459 0.02991 0.02375 -0.0582 0.9983 0.0091
-12.000 -0.9293 0.02847 0.02225 -0.0591 0.9964 0.0092
-11.750 -0.9121 0.02714 0.02086 -0.0599 0.9946 0.0094
-11.500 -0.8938 0.02593 0.01958 -0.0607 0.9928 0.0095
-11.250 -0.8780 0.02480 0.01838 -0.0608 0.9901 0.0097
-11.000 -0.8590 0.02383 0.01736 -0.0611 0.9876 0.0099
-10.750 -0.8373 0.02296 0.01643 -0.0618 0.9855 0.0101
-10.500 -0.8175 0.02181 0.01524 -0.0626 0.9835 0.0105
-10.250 -0.7997 0.02096 0.01435 -0.0623 0.9804 0.0107
-10.000 -0.7830 0.02025 0.01361 -0.0615 0.9763 0.0111
-9.750 -0.7606 0.01958 0.01289 -0.0617 0.9735 0.0113
-9.500 -0.7353 0.01892 0.01220 -0.0623 0.9716 0.0117
-9.250 -0.7187 0.01837 0.01160 -0.0609 0.9673 0.0122
-9.000 -0.6989 0.01781 0.01099 -0.0600 0.9629 0.0126
-8.750 -0.6729 0.01716 0.01033 -0.0604 0.9604 0.0133
-8.500 -0.6438 0.01660 0.00976 -0.0613 0.9587 0.0140
-8.250 -0.6129 0.01609 0.00921 -0.0625 0.9575 0.0151
-8.000 -0.6006 0.01569 0.00881 -0.0597 0.9508 0.0160
-7.750 -0.5741 0.01524 0.00835 -0.0598 0.9478 0.0176
-7.500 -0.5447 0.01476 0.00788 -0.0606 0.9457 0.0200
-7.250 -0.5144 0.01431 0.00743 -0.0614 0.9440 0.0235
-7.000 -0.4913 0.01392 0.00705 -0.0607 0.9400 0.0278
-6.750 -0.4718 0.01357 0.00671 -0.0592 0.9340 0.0324
-6.500 -0.4449 0.01309 0.00630 -0.0593 0.9308 0.0427
-6.250 -0.4158 0.01258 0.00587 -0.0599 0.9283 0.0576
-6.000 -0.3987 0.01216 0.00554 -0.0580 0.9212 0.0765
-5.750 -0.3757 0.01155 0.00511 -0.0574 0.9160 0.1112
-5.500 -0.3488 0.01086 0.00465 -0.0577 0.9124 0.1603
-5.250 -0.3301 0.01035 0.00434 -0.0561 0.9047 0.2037
-5.000 -0.3051 0.00975 0.00398 -0.0559 0.8989 0.2581
-4.750 -0.2772 0.00922 0.00366 -0.0562 0.8939 0.3110
-4.500 -0.2538 0.00890 0.00346 -0.0554 0.8855 0.3459
-4.250 -0.2234 0.00856 0.00322 -0.0560 0.8794 0.3820
-4.000 -0.1984 0.00827 0.00308 -0.0554 0.8704 0.4211
-3.750 -0.1683 0.00805 0.00292 -0.0559 0.8622 0.4500
-3.500 -0.1408 0.00792 0.00280 -0.0557 0.8518 0.4670
-3.250 -0.1103 0.00783 0.00267 -0.0561 0.8417 0.4802
-3.000 -0.0823 0.00774 0.00257 -0.0559 0.8290 0.4920
-2.750 -0.0541 0.00768 0.00248 -0.0559 0.8156 0.5029
-2.500 -0.0259 0.00765 0.00240 -0.0557 0.8009 0.5137
-2.250 0.0014 0.00762 0.00232 -0.0555 0.7845 0.5235
-2.000 0.0284 0.00763 0.00226 -0.0551 0.7668 0.5338
-1.750 0.0546 0.00763 0.00222 -0.0546 0.7480 0.5437
-1.250 0.1059 0.00771 0.00216 -0.0534 0.7079 0.5632
-1.000 0.1314 0.00778 0.00214 -0.0527 0.6875 0.5720
-0.750 0.1564 0.00783 0.00214 -0.0520 0.6679 0.5801
-0.500 0.1814 0.00791 0.00215 -0.0513 0.6469 0.5885
-0.250 0.2061 0.00799 0.00216 -0.0505 0.6263 0.5961
0.000 0.2304 0.00810 0.00219 -0.0497 0.6043 0.6042
0.250 0.2549 0.00821 0.00222 -0.0489 0.5826 0.6118
0.500 0.2791 0.00832 0.00226 -0.0480 0.5591 0.6193
0.750 0.3030 0.00846 0.00231 -0.0472 0.5340 0.6272
1.000 0.3258 0.00864 0.00238 -0.0461 0.5045 0.6342
1.250 0.3476 0.00887 0.00246 -0.0448 0.4680 0.6421
1.500 0.3696 0.00912 0.00256 -0.0437 0.4318 0.6493
1.750 0.3927 0.00932 0.00266 -0.0427 0.4028 0.6567
2.000 0.4163 0.00953 0.00277 -0.0418 0.3774 0.6645
2.250 0.4399 0.00973 0.00289 -0.0410 0.3526 0.6715
2.500 0.4638 0.00993 0.00301 -0.0402 0.3313 0.6793
2.750 0.4878 0.01014 0.00313 -0.0395 0.3110 0.6865
3.000 0.5112 0.01035 0.00328 -0.0386 0.2907 0.6936
3.500 0.5586 0.01079 0.00358 -0.0370 0.2541 0.7078
3.750 0.5822 0.01099 0.00375 -0.0362 0.2389 0.7149
4.000 0.6059 0.01120 0.00391 -0.0355 0.2242 0.7223
4.250 0.6292 0.01142 0.00409 -0.0346 0.2093 0.7290
4.500 0.6521 0.01165 0.00428 -0.0337 0.1954 0.7363
4.750 0.6749 0.01190 0.00447 -0.0328 0.1823 0.7437
5.000 0.6968 0.01213 0.00467 -0.0317 0.1702 0.7504
5.250 0.7185 0.01236 0.00488 -0.0305 0.1589 0.7580
5.750 0.7608 0.01285 0.00532 -0.0281 0.1389 0.7724
6.000 0.7814 0.01313 0.00557 -0.0268 0.1299 0.7805
6.250 0.8027 0.01338 0.00582 -0.0256 0.1234 0.7877
6.500 0.8230 0.01366 0.00610 -0.0243 0.1171 0.7958
7.000 0.8643 0.01419 0.00667 -0.0218 0.1079 0.8121
7.250 0.8842 0.01451 0.00698 -0.0204 0.1040 0.8209
7.500 0.9044 0.01476 0.00729 -0.0191 0.1009 0.8293
7.750 0.9239 0.01506 0.00761 -0.0177 0.0976 0.8391
8.000 0.9423 0.01539 0.00796 -0.0162 0.0948 0.8486
8.250 0.9613 0.01569 0.00831 -0.0147 0.0927 0.8594
8.500 0.9796 0.01597 0.00865 -0.0131 0.0909 0.8708
8.750 0.9972 0.01627 0.00901 -0.0114 0.0890 0.8834
9.000 1.0139 0.01660 0.00940 -0.0096 0.0872 0.8983
9.250 1.0291 0.01694 0.00980 -0.0075 0.0854 0.9175
9.500 1.0473 0.01734 0.01026 -0.0061 0.0836 0.9458
10.000 1.0961 0.01814 0.01115 -0.0062 0.0808 1.0000
10.250 1.1141 0.01861 0.01164 -0.0050 0.0795 1.0000
10.500 1.1315 0.01911 0.01216 -0.0037 0.0783 1.0000
10.750 1.1480 0.01965 0.01271 -0.0024 0.0771 1.0000
11.000 1.1635 0.02026 0.01333 -0.0010 0.0760 1.0000
11.250 1.1770 0.02097 0.01406 0.0006 0.0748 1.0000
11.500 1.1934 0.02154 0.01468 0.0018 0.0740 1.0000
11.750 1.2092 0.02215 0.01534 0.0030 0.0732 1.0000
12.000 1.2247 0.02278 0.01602 0.0042 0.0722 1.0000
12.250 1.2391 0.02349 0.01678 0.0055 0.0713 1.0000
12.500 1.2527 0.02426 0.01760 0.0068 0.0705 1.0000
12.750 1.2657 0.02508 0.01846 0.0081 0.0697 1.0000
13.000 1.2779 0.02598 0.01939 0.0093 0.0689 1.0000
13.250 1.2890 0.02697 0.02042 0.0106 0.0681 1.0000
13.500 1.2984 0.02810 0.02158 0.0119 0.0674 1.0000
13.750 1.3064 0.02935 0.02287 0.0132 0.0666 1.0000
14.000 1.3187 0.03036 0.02396 0.0141 0.0660 1.0000
14.250 1.3294 0.03150 0.02518 0.0150 0.0654 1.0000
14.500 1.3394 0.03273 0.02649 0.0159 0.0648 1.0000
14.750 1.3486 0.03407 0.02790 0.0167 0.0641 1.0000
15.000 1.3575 0.03547 0.02937 0.0174 0.0635 1.0000
15.250 1.3656 0.03697 0.03095 0.0180 0.0629 1.0000
15.500 1.3730 0.03860 0.03264 0.0186 0.0623 1.0000
15.750 1.3792 0.04037 0.03447 0.0190 0.0617 1.0000
16.000 1.3847 0.04227 0.03643 0.0193 0.0610 1.0000
16.250 1.3885 0.04440 0.03862 0.0194 0.0604 1.0000
16.500 1.3913 0.04671 0.04099 0.0195 0.0599 1.0000
16.750 1.3925 0.04923 0.04357 0.0194 0.0593 1.0000
17.000 1.3973 0.05148 0.04593 0.0192 0.0589 1.0000
17.250 1.4010 0.05391 0.04846 0.0189 0.0585 1.0000
17.500 1.4042 0.05646 0.05112 0.0184 0.0579 1.0000
17.750 1.4063 0.05920 0.05396 0.0177 0.0573 1.0000
18.000 1.4074 0.06212 0.05697 0.0169 0.0568 1.0000
18.250 1.4077 0.06522 0.06017 0.0160 0.0563 1.0000
18.500 1.4075 0.06847 0.06352 0.0148 0.0557 1.0000
18.750 1.4061 0.07195 0.06709 0.0135 0.0552 1.0000
19.000 1.4035 0.07564 0.07087 0.0120 0.0547 1.0000
19.250 1.4001 0.07953 0.07484 0.0104 0.0542 1.0000
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