MH 93 15.98% (mh93-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: MH 93 15.98% (mh93-il) Reynolds number: 1,000,000 Max Cl/Cd: 88.94 at α=10° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-mh93-il-1000000-n5.txt Download as CSV file: xf-mh93-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: MH 93 15.98%
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
------ -------- --------- --------- -------- -------- --------
-19.500 -0.9976 0.14591 0.14338 0.0330 1.0000 0.0047
-19.250 -1.0252 0.13491 0.13223 0.0262 1.0000 0.0047
-19.000 -1.0538 0.12406 0.12122 0.0195 1.0000 0.0047
-18.750 -1.0806 0.11392 0.11091 0.0133 1.0000 0.0046
-18.500 -1.1029 0.10493 0.10179 0.0079 1.0000 0.0047
-18.250 -1.1272 0.09595 0.09264 0.0026 1.0000 0.0046
-18.000 -1.1488 0.08776 0.08429 -0.0022 1.0000 0.0045
-17.750 -1.1659 0.08067 0.07706 -0.0062 1.0000 0.0046
-17.500 -1.1778 0.07463 0.07090 -0.0095 1.0000 0.0046
-17.250 -1.1919 0.06855 0.06469 -0.0127 1.0000 0.0046
-17.000 -1.2016 0.06339 0.05941 -0.0152 1.0000 0.0046
-16.750 -1.2098 0.05870 0.05460 -0.0172 1.0000 0.0046
-16.500 -1.2160 0.05451 0.05030 -0.0188 1.0000 0.0047
-16.250 -1.2212 0.05069 0.04637 -0.0200 1.0000 0.0047
-16.000 -1.2246 0.04728 0.04286 -0.0208 1.0000 0.0047
-15.750 -1.2251 0.04439 0.03988 -0.0211 1.0000 0.0048
-15.500 -1.2255 0.04169 0.03708 -0.0212 1.0000 0.0048
-15.250 -1.2238 0.03933 0.03464 -0.0210 1.0000 0.0048
-15.000 -1.2223 0.03708 0.03230 -0.0205 1.0000 0.0048
-14.750 -1.2189 0.03510 0.03024 -0.0198 1.0000 0.0049
-14.500 -1.2151 0.03324 0.02831 -0.0189 1.0000 0.0049
-14.250 -1.2102 0.03157 0.02655 -0.0178 1.0000 0.0050
-14.000 -1.2032 0.03011 0.02504 -0.0166 1.0000 0.0050
-13.750 -1.1969 0.02866 0.02351 -0.0153 1.0000 0.0050
-13.500 -1.1886 0.02742 0.02220 -0.0139 1.0000 0.0050
-13.250 -1.1799 0.02623 0.02095 -0.0123 1.0000 0.0050
-13.000 -1.1702 0.02516 0.01982 -0.0108 1.0000 0.0051
-12.750 -1.1587 0.02422 0.01883 -0.0092 1.0000 0.0053
-12.500 -1.1467 0.02333 0.01789 -0.0077 1.0000 0.0054
-12.250 -1.1345 0.02249 0.01700 -0.0060 1.0000 0.0054
-11.750 -1.1028 0.02098 0.01531 -0.0037 0.9157 0.0055
-11.500 -1.0934 0.02047 0.01462 -0.0009 0.8722 0.0055
-11.250 -1.0813 0.01991 0.01393 0.0014 0.8461 0.0056
-11.000 -1.0674 0.01939 0.01329 0.0034 0.8257 0.0057
-10.500 -1.0379 0.01836 0.01208 0.0074 0.7920 0.0058
-10.250 -1.0222 0.01789 0.01154 0.0094 0.7774 0.0058
-10.000 -1.0083 0.01733 0.01089 0.0117 0.7644 0.0059
-9.750 -0.9925 0.01688 0.01036 0.0137 0.7510 0.0060
-9.500 -0.9738 0.01646 0.00987 0.0153 0.7383 0.0061
-9.250 -0.9537 0.01604 0.00940 0.0165 0.7270 0.0063
-9.000 -0.9326 0.01567 0.00898 0.0177 0.7150 0.0065
-8.750 -0.9110 0.01529 0.00854 0.0188 0.7038 0.0066
-8.500 -0.8888 0.01495 0.00815 0.0198 0.6926 0.0068
-8.250 -0.8660 0.01462 0.00776 0.0207 0.6814 0.0069
-8.000 -0.8427 0.01431 0.00740 0.0215 0.6708 0.0071
-7.750 -0.8191 0.01401 0.00704 0.0223 0.6599 0.0074
-7.500 -0.7951 0.01372 0.00671 0.0230 0.6492 0.0076
-7.250 -0.7707 0.01345 0.00639 0.0237 0.6390 0.0078
-7.000 -0.7466 0.01314 0.00604 0.0244 0.6281 0.0083
-6.750 -0.7219 0.01288 0.00574 0.0250 0.6179 0.0087
-6.500 -0.6968 0.01264 0.00546 0.0256 0.6070 0.0093
-6.250 -0.6713 0.01241 0.00519 0.0261 0.5970 0.0100
-5.750 -0.6201 0.01196 0.00468 0.0270 0.5761 0.0120
-5.500 -0.5943 0.01175 0.00444 0.0275 0.5661 0.0139
-5.250 -0.5683 0.01154 0.00422 0.0279 0.5553 0.0164
-5.000 -0.5424 0.01133 0.00400 0.0283 0.5456 0.0207
-4.750 -0.5163 0.01112 0.00379 0.0287 0.5350 0.0261
-4.500 -0.4903 0.01089 0.00358 0.0291 0.5261 0.0346
-4.250 -0.4643 0.01067 0.00338 0.0294 0.5156 0.0459
-4.000 -0.4385 0.01042 0.00318 0.0299 0.5063 0.0626
-3.750 -0.4135 0.01010 0.00296 0.0304 0.4966 0.0906
-3.500 -0.3893 0.00969 0.00273 0.0310 0.4881 0.1354
-3.000 -0.3418 0.00883 0.00230 0.0323 0.4691 0.2500
-2.750 -0.3178 0.00844 0.00213 0.0329 0.4602 0.3116
-2.500 -0.2927 0.00813 0.00199 0.0334 0.4516 0.3611
-2.250 -0.2676 0.00786 0.00187 0.0339 0.4418 0.4119
-2.000 -0.2421 0.00759 0.00177 0.0343 0.4330 0.4630
-1.750 -0.2155 0.00744 0.00170 0.0346 0.4245 0.4969
-1.500 -0.1882 0.00733 0.00164 0.0348 0.4154 0.5221
-1.250 -0.1608 0.00725 0.00159 0.0349 0.4061 0.5464
-1.000 -0.1331 0.00717 0.00155 0.0351 0.3976 0.5698
-0.750 -0.1058 0.00710 0.00152 0.0352 0.3893 0.5939
-0.500 -0.0784 0.00702 0.00149 0.0354 0.3804 0.6204
-0.250 -0.0509 0.00698 0.00148 0.0355 0.3717 0.6445
0.000 -0.0231 0.00693 0.00148 0.0356 0.3643 0.6660
0.250 0.0048 0.00693 0.00149 0.0357 0.3557 0.6853
0.500 0.0331 0.00693 0.00151 0.0357 0.3477 0.7024
0.750 0.0613 0.00696 0.00154 0.0357 0.3398 0.7175
1.000 0.0899 0.00699 0.00156 0.0357 0.3329 0.7308
1.250 0.1183 0.00704 0.00161 0.0356 0.3248 0.7431
1.500 0.1469 0.00708 0.00165 0.0356 0.3183 0.7533
1.750 0.1756 0.00714 0.00170 0.0355 0.3114 0.7631
2.000 0.2040 0.00722 0.00176 0.0354 0.3043 0.7717
2.250 0.2328 0.00728 0.00181 0.0353 0.2980 0.7803
2.500 0.2612 0.00736 0.00188 0.0352 0.2918 0.7882
2.750 0.2898 0.00744 0.00195 0.0351 0.2867 0.7974
3.000 0.3182 0.00751 0.00203 0.0351 0.2810 0.8055
3.250 0.3465 0.00762 0.00212 0.0350 0.2743 0.8133
3.500 0.3752 0.00771 0.00220 0.0348 0.2693 0.8189
3.750 0.4036 0.00779 0.00229 0.0347 0.2645 0.8241
4.000 0.4319 0.00790 0.00238 0.0346 0.2592 0.8294
4.250 0.4604 0.00801 0.00248 0.0345 0.2544 0.8343
4.500 0.4888 0.00812 0.00258 0.0344 0.2490 0.8386
4.750 0.5168 0.00824 0.00269 0.0343 0.2436 0.8431
5.000 0.5449 0.00836 0.00282 0.0342 0.2393 0.8478
5.250 0.5732 0.00847 0.00292 0.0341 0.2350 0.8522
5.500 0.6011 0.00861 0.00305 0.0340 0.2296 0.8563
5.750 0.6285 0.00875 0.00320 0.0340 0.2245 0.8607
6.000 0.6563 0.00887 0.00333 0.0340 0.2209 0.8657
6.250 0.6839 0.00902 0.00347 0.0339 0.2161 0.8709
6.500 0.7109 0.00920 0.00364 0.0339 0.2105 0.8756
6.750 0.7381 0.00932 0.00379 0.0340 0.2069 0.8801
7.000 0.7653 0.00948 0.00396 0.0340 0.2023 0.8843
7.250 0.7920 0.00968 0.00414 0.0340 0.1971 0.8883
7.500 0.8190 0.00985 0.00431 0.0340 0.1927 0.8918
7.750 0.8452 0.01003 0.00450 0.0341 0.1873 0.8954
8.000 0.8708 0.01026 0.00472 0.0343 0.1814 0.8993
8.250 0.8972 0.01043 0.00491 0.0344 0.1780 0.9034
8.500 0.9234 0.01063 0.00512 0.0345 0.1740 0.9073
8.750 0.9483 0.01088 0.00536 0.0347 0.1689 0.9108
9.000 0.9733 0.01108 0.00559 0.0350 0.1653 0.9149
9.250 0.9983 0.01129 0.00582 0.0353 0.1615 0.9194
9.500 1.0227 0.01154 0.00607 0.0356 0.1573 0.9238
9.750 1.0462 0.01181 0.00635 0.0361 0.1529 0.9279
10.000 1.0700 0.01203 0.00661 0.0366 0.1499 0.9326
10.250 1.0928 0.01229 0.00689 0.0371 0.1457 0.9381
10.500 1.1142 0.01263 0.00722 0.0379 0.1409 0.9435
10.750 1.1366 0.01287 0.00751 0.0385 0.1379 0.9492
11.000 1.1580 0.01317 0.00783 0.0392 0.1338 0.9559
11.250 1.1795 0.01357 0.00823 0.0397 0.1289 0.9630
11.500 1.2032 0.01391 0.00861 0.0399 0.1251 0.9706
11.750 1.2304 0.01435 0.00906 0.0391 0.1201 0.9765
12.000 1.2571 0.01488 0.00958 0.0382 0.1151 0.9830
12.250 1.2856 0.01539 0.01011 0.0369 0.1101 0.9886
12.500 1.3098 0.01607 0.01078 0.0361 0.1048 1.0000
12.750 1.3154 0.01660 0.01134 0.0389 0.1016 1.0000
13.000 1.3223 0.01735 0.01209 0.0410 0.0975 1.0000
13.250 1.3294 0.01825 0.01301 0.0427 0.0936 1.0000
13.500 1.3377 0.01921 0.01398 0.0439 0.0893 1.0000
13.750 1.3432 0.02045 0.01522 0.0452 0.0850 1.0000
14.000 1.3515 0.02161 0.01642 0.0460 0.0817 1.0000
14.250 1.3576 0.02301 0.01784 0.0468 0.0783 1.0000
14.500 1.3620 0.02463 0.01948 0.0474 0.0753 1.0000
14.750 1.3688 0.02613 0.02103 0.0478 0.0730 1.0000
15.000 1.3742 0.02783 0.02278 0.0480 0.0709 1.0000
15.250 1.3755 0.02993 0.02491 0.0482 0.0683 1.0000
15.500 1.3770 0.03209 0.02712 0.0482 0.0661 1.0000
15.750 1.3793 0.03425 0.02934 0.0480 0.0641 1.0000
16.000 1.3788 0.03674 0.03189 0.0478 0.0622 1.0000
16.250 1.3753 0.03958 0.03478 0.0473 0.0603 1.0000
16.500 1.3709 0.04258 0.03783 0.0468 0.0587 1.0000
16.750 1.3695 0.04539 0.04072 0.0461 0.0574 1.0000
17.000 1.3643 0.04870 0.04410 0.0453 0.0555 1.0000
17.250 1.3584 0.05217 0.04764 0.0442 0.0545 1.0000
17.500 1.3458 0.05651 0.05203 0.0429 0.0523 1.0000
17.750 1.3385 0.06033 0.05594 0.0416 0.0517 1.0000
18.000 1.3315 0.06419 0.05987 0.0402 0.0504 1.0000
18.250 1.3224 0.06836 0.06412 0.0387 0.0492 1.0000
18.500 1.3117 0.07282 0.06867 0.0370 0.0481 1.0000
18.750 1.2976 0.07783 0.07374 0.0350 0.0466 1.0000
19.000 1.2843 0.08282 0.07881 0.0329 0.0457 1.0000
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