MH 95 15.86% (mh95-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: MH 95 15.86% (mh95-il) Reynolds number: 1,000,000 Max Cl/Cd: 78.01 at α=6.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-mh95-il-1000000.txt Download as CSV file: xf-mh95-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: MH 95 15.86%
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
------ -------- --------- --------- -------- -------- --------
-18.000 -0.7407 0.11647 0.11401 -0.0508 1.0000 0.0128
-17.500 -0.7887 0.09917 0.09646 -0.0602 1.0000 0.0126
-17.250 -0.8204 0.08979 0.08692 -0.0652 1.0000 0.0126
-17.000 -0.8511 0.08117 0.07813 -0.0697 1.0000 0.0125
-16.750 -0.8711 0.07467 0.07148 -0.0730 1.0000 0.0125
-16.500 -0.8946 0.06824 0.06488 -0.0757 1.0000 0.0125
-16.250 -0.9116 0.06314 0.05965 -0.0774 1.0000 0.0124
-16.000 -0.9241 0.05902 0.05541 -0.0784 1.0000 0.0125
-15.750 -0.9365 0.05530 0.05155 -0.0789 1.0000 0.0125
-15.500 -0.9452 0.05235 0.04850 -0.0788 1.0000 0.0126
-15.250 -0.9574 0.04916 0.04518 -0.0780 1.0000 0.0126
-15.000 -0.9670 0.04655 0.04247 -0.0768 1.0000 0.0126
-14.750 -0.9755 0.04424 0.04005 -0.0753 1.0000 0.0126
-14.500 -0.9839 0.04216 0.03785 -0.0734 1.0000 0.0126
-14.250 -0.9906 0.04040 0.03601 -0.0711 1.0000 0.0127
-14.000 -0.9972 0.03860 0.03410 -0.0686 1.0000 0.0127
-13.750 -1.0033 0.03725 0.03266 -0.0658 1.0000 0.0127
-13.500 -1.0120 0.03520 0.03047 -0.0627 1.0000 0.0128
-13.250 -1.0008 0.03342 0.02858 -0.0626 0.9992 0.0128
-13.000 -0.9900 0.03118 0.02622 -0.0625 0.9981 0.0129
-12.750 -0.9751 0.02943 0.02437 -0.0627 0.9968 0.0130
-12.500 -0.9572 0.02805 0.02293 -0.0631 0.9955 0.0131
-12.250 -0.9385 0.02673 0.02156 -0.0635 0.9943 0.0133
-12.000 -0.9171 0.02564 0.02042 -0.0643 0.9934 0.0134
-11.750 -0.9006 0.02456 0.01930 -0.0638 0.9912 0.0135
-11.500 -0.8815 0.02363 0.01832 -0.0637 0.9890 0.0136
-11.250 -0.8597 0.02275 0.01739 -0.0640 0.9871 0.0138
-11.000 -0.8364 0.02187 0.01647 -0.0646 0.9856 0.0139
-10.750 -0.8120 0.02098 0.01553 -0.0653 0.9842 0.0141
-10.500 -0.7854 0.02021 0.01473 -0.0663 0.9832 0.0143
-10.250 -0.7573 0.01949 0.01397 -0.0674 0.9823 0.0145
-10.000 -0.7423 0.01878 0.01322 -0.0659 0.9782 0.0147
-9.750 -0.7191 0.01815 0.01255 -0.0658 0.9754 0.0150
-9.500 -0.6914 0.01761 0.01197 -0.0666 0.9736 0.0153
-9.250 -0.6628 0.01702 0.01134 -0.0675 0.9723 0.0155
-9.000 -0.6368 0.01607 0.01036 -0.0682 0.9709 0.0158
-8.750 -0.6084 0.01528 0.00954 -0.0693 0.9700 0.0163
-8.500 -0.5929 0.01485 0.00910 -0.0672 0.9653 0.0166
-8.250 -0.5699 0.01434 0.00858 -0.0667 0.9620 0.0169
-8.000 -0.5397 0.01385 0.00808 -0.0677 0.9604 0.0174
-7.750 -0.5090 0.01336 0.00757 -0.0686 0.9589 0.0178
-7.500 -0.4775 0.01291 0.00710 -0.0697 0.9575 0.0183
-7.250 -0.4458 0.01246 0.00663 -0.0708 0.9561 0.0187
-7.000 -0.4303 0.01205 0.00620 -0.0686 0.9508 0.0195
-6.750 -0.4070 0.01170 0.00585 -0.0678 0.9466 0.0203
-6.500 -0.3784 0.01135 0.00549 -0.0681 0.9437 0.0213
-6.250 -0.3495 0.01098 0.00510 -0.0684 0.9411 0.0225
-6.000 -0.3299 0.01070 0.00483 -0.0668 0.9358 0.0244
-5.750 -0.3073 0.01040 0.00454 -0.0657 0.9305 0.0274
-5.500 -0.2821 0.01000 0.00420 -0.0653 0.9263 0.0366
-5.250 -0.2633 0.00949 0.00386 -0.0637 0.9205 0.0691
-5.000 -0.2456 0.00900 0.00355 -0.0618 0.9136 0.1094
-4.750 -0.2234 0.00842 0.00321 -0.0610 0.9081 0.1659
-4.500 -0.2064 0.00802 0.00300 -0.0589 0.9002 0.2121
-4.250 -0.1840 0.00761 0.00276 -0.0580 0.8934 0.2602
-4.000 -0.1630 0.00725 0.00257 -0.0567 0.8856 0.3077
-3.750 -0.1407 0.00689 0.00238 -0.0556 0.8771 0.3584
-3.500 -0.1189 0.00656 0.00221 -0.0545 0.8681 0.4062
-3.250 -0.0960 0.00622 0.00203 -0.0535 0.8584 0.4613
-3.000 -0.0754 0.00587 0.00189 -0.0521 0.8471 0.5234
-2.750 -0.0530 0.00559 0.00178 -0.0510 0.8357 0.5828
-2.500 -0.0293 0.00543 0.00173 -0.0500 0.8229 0.6320
-2.250 -0.0043 0.00539 0.00171 -0.0493 0.8089 0.6612
-2.000 0.0216 0.00538 0.00169 -0.0487 0.7943 0.6766
-1.750 0.0477 0.00540 0.00167 -0.0482 0.7796 0.6866
-1.500 0.0739 0.00545 0.00165 -0.0477 0.7644 0.6960
-1.250 0.0994 0.00550 0.00164 -0.0470 0.7481 0.7039
-1.000 0.1249 0.00556 0.00164 -0.0464 0.7315 0.7116
-0.750 0.1502 0.00563 0.00164 -0.0458 0.7144 0.7182
-0.500 0.1752 0.00571 0.00166 -0.0450 0.6969 0.7250
-0.250 0.2004 0.00580 0.00168 -0.0443 0.6793 0.7314
0.000 0.2251 0.00588 0.00170 -0.0436 0.6610 0.7377
0.250 0.2497 0.00598 0.00175 -0.0428 0.6419 0.7439
0.500 0.2744 0.00610 0.00178 -0.0420 0.6230 0.7497
0.750 0.2988 0.00620 0.00182 -0.0412 0.6024 0.7548
1.000 0.3228 0.00632 0.00187 -0.0404 0.5813 0.7597
1.250 0.3466 0.00647 0.00193 -0.0395 0.5589 0.7646
1.500 0.3697 0.00665 0.00199 -0.0384 0.5321 0.7691
1.750 0.3914 0.00684 0.00206 -0.0372 0.5004 0.7739
2.000 0.4144 0.00703 0.00216 -0.0361 0.4727 0.7789
2.250 0.4379 0.00722 0.00225 -0.0352 0.4496 0.7839
2.500 0.4616 0.00741 0.00234 -0.0344 0.4270 0.7882
2.750 0.4849 0.00757 0.00243 -0.0335 0.4042 0.7929
3.000 0.5082 0.00776 0.00255 -0.0326 0.3823 0.7973
3.250 0.5317 0.00795 0.00266 -0.0317 0.3626 0.8016
3.500 0.5552 0.00816 0.00277 -0.0309 0.3436 0.8054
3.750 0.5782 0.00834 0.00288 -0.0300 0.3246 0.8094
4.250 0.6233 0.00871 0.00314 -0.0279 0.2912 0.8169
4.500 0.6459 0.00888 0.00326 -0.0269 0.2773 0.8208
4.750 0.6685 0.00907 0.00339 -0.0259 0.2641 0.8243
5.000 0.6903 0.00925 0.00352 -0.0248 0.2510 0.8281
5.250 0.7115 0.00945 0.00368 -0.0236 0.2378 0.8321
5.500 0.7337 0.00964 0.00384 -0.0225 0.2266 0.8360
5.750 0.7558 0.00984 0.00400 -0.0215 0.2158 0.8399
6.000 0.7774 0.01009 0.00419 -0.0204 0.2043 0.8433
6.250 0.7989 0.01028 0.00437 -0.0192 0.1939 0.8477
6.500 0.8199 0.01051 0.00457 -0.0180 0.1836 0.8520
6.750 0.8402 0.01078 0.00479 -0.0167 0.1716 0.8563
7.250 0.8807 0.01132 0.00525 -0.0141 0.1495 0.8648
7.500 0.9000 0.01160 0.00551 -0.0126 0.1399 0.8695
7.750 0.9186 0.01193 0.00579 -0.0111 0.1303 0.8745
8.000 0.9387 0.01222 0.00605 -0.0099 0.1237 0.8790
8.250 0.9568 0.01252 0.00635 -0.0083 0.1168 0.8841
8.500 0.9759 0.01279 0.00663 -0.0068 0.1121 0.8895
8.750 0.9937 0.01314 0.00696 -0.0052 0.1072 0.8952
9.000 1.0121 0.01341 0.00726 -0.0037 0.1040 0.9011
9.250 1.0306 0.01368 0.00757 -0.0022 0.1014 0.9075
9.500 1.0480 0.01401 0.00790 -0.0006 0.0985 0.9140
9.750 1.0628 0.01437 0.00829 0.0015 0.0955 0.9218
10.000 1.0790 0.01470 0.00867 0.0033 0.0933 0.9305
10.250 1.0953 0.01495 0.00899 0.0052 0.0920 0.9413
10.500 1.1120 0.01524 0.00934 0.0068 0.0903 0.9555
10.750 1.1378 0.01564 0.00977 0.0064 0.0882 0.9714
11.000 1.1672 0.01619 0.01033 0.0050 0.0855 1.0000
11.250 1.1817 0.01683 0.01097 0.0065 0.0834 1.0000
11.500 1.2012 0.01721 0.01139 0.0074 0.0827 1.0000
11.750 1.2193 0.01764 0.01186 0.0084 0.0818 1.0000
12.000 1.2367 0.01811 0.01236 0.0095 0.0805 1.0000
12.250 1.2529 0.01863 0.01291 0.0108 0.0795 1.0000
12.500 1.2684 0.01920 0.01349 0.0120 0.0780 1.0000
12.750 1.2824 0.01985 0.01416 0.0134 0.0769 1.0000
13.000 1.2929 0.02070 0.01503 0.0152 0.0753 1.0000
13.250 1.3009 0.02170 0.01607 0.0172 0.0738 1.0000
13.500 1.3172 0.02227 0.01669 0.0181 0.0733 1.0000
13.750 1.3328 0.02289 0.01735 0.0191 0.0725 1.0000
14.000 1.3472 0.02359 0.01809 0.0202 0.0715 1.0000
14.250 1.3598 0.02441 0.01896 0.0213 0.0706 1.0000
14.500 1.3728 0.02524 0.01982 0.0224 0.0696 1.0000
14.750 1.3836 0.02622 0.02083 0.0236 0.0686 1.0000
15.000 1.3928 0.02734 0.02198 0.0248 0.0676 1.0000
15.250 1.3984 0.02875 0.02343 0.0261 0.0665 1.0000
15.500 1.4006 0.03045 0.02520 0.0275 0.0652 1.0000
15.750 1.4122 0.03155 0.02636 0.0282 0.0649 1.0000
16.000 1.4233 0.03269 0.02757 0.0289 0.0643 1.0000
16.250 1.4338 0.03393 0.02887 0.0294 0.0635 1.0000
16.500 1.4425 0.03535 0.03035 0.0300 0.0628 1.0000
16.750 1.4509 0.03684 0.03189 0.0305 0.0620 1.0000
17.000 1.4579 0.03849 0.03360 0.0309 0.0612 1.0000
17.250 1.4635 0.04032 0.03547 0.0312 0.0604 1.0000
17.500 1.4668 0.04243 0.03764 0.0314 0.0596 1.0000
17.750 1.4654 0.04506 0.04032 0.0316 0.0586 1.0000
18.000 1.4621 0.04796 0.04329 0.0316 0.0575 1.0000
18.250 1.4694 0.04989 0.04530 0.0313 0.0571 1.0000
18.500 1.4747 0.05205 0.04754 0.0310 0.0565 1.0000
18.750 1.4800 0.05427 0.04984 0.0306 0.0556 1.0000
19.000 1.4824 0.05687 0.05250 0.0300 0.0548 1.0000
19.250 1.4817 0.05988 0.05560 0.0293 0.0543 1.0000
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