MH 94 16.03% (mh94-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: MH 94 16.03% (mh94-il) Reynolds number: 500,000 Max Cl/Cd: 62.71 at α=6° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-mh94-il-500000.txt Download as CSV file: xf-mh94-il-500000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.250 -0.6598 0.12638 0.12337 -0.0433 1.0000 0.0150
-17.000 -0.6965 0.11421 0.11106 -0.0497 1.0000 0.0146
-16.750 -0.7325 0.10303 0.09971 -0.0559 1.0000 0.0143
-16.500 -0.7676 0.09277 0.08924 -0.0616 1.0000 0.0143
-16.250 -0.8001 0.08386 0.08011 -0.0662 1.0000 0.0142
-16.000 -0.8215 0.07742 0.07350 -0.0691 1.0000 0.0140
-15.750 -0.8478 0.07067 0.06651 -0.0717 1.0000 0.0138
-15.500 -0.8611 0.06624 0.06196 -0.0731 1.0000 0.0139
-15.250 -0.8832 0.06083 0.05630 -0.0742 1.0000 0.0136
-15.000 -0.8958 0.05700 0.05230 -0.0745 1.0000 0.0136
-14.750 -0.9030 0.05407 0.04926 -0.0744 1.0000 0.0137
-14.500 -0.9111 0.05113 0.04617 -0.0739 1.0000 0.0137
-14.250 -0.9166 0.04861 0.04355 -0.0731 1.0000 0.0138
-14.000 -0.9224 0.04605 0.04084 -0.0720 1.0000 0.0137
-13.750 -0.9250 0.04407 0.03877 -0.0708 1.0000 0.0139
-13.500 -0.9278 0.04190 0.03646 -0.0691 1.0000 0.0138
-13.250 -0.9290 0.04021 0.03469 -0.0675 1.0000 0.0140
-13.000 -0.9293 0.03845 0.03282 -0.0655 1.0000 0.0139
-12.750 -0.9292 0.03696 0.03125 -0.0635 1.0000 0.0141
-12.500 -0.9287 0.03554 0.02974 -0.0613 1.0000 0.0142
-12.250 -0.9276 0.03416 0.02828 -0.0589 1.0000 0.0142
-12.000 -0.9269 0.03292 0.02696 -0.0564 1.0000 0.0143
-11.750 -0.9263 0.03173 0.02571 -0.0537 1.0000 0.0144
-11.500 -0.9260 0.03064 0.02455 -0.0508 1.0000 0.0145
-11.250 -0.9268 0.02957 0.02342 -0.0476 1.0000 0.0146
-11.000 -0.9283 0.02864 0.02242 -0.0443 1.0000 0.0147
-10.750 -0.9313 0.02777 0.02149 -0.0405 1.0000 0.0148
-10.500 -0.9267 0.02681 0.02045 -0.0381 0.9993 0.0149
-10.250 -0.9037 0.02578 0.01936 -0.0390 0.9966 0.0151
-10.000 -0.8818 0.02463 0.01814 -0.0398 0.9939 0.0154
-9.750 -0.8651 0.02360 0.01709 -0.0395 0.9898 0.0156
-9.500 -0.8441 0.02273 0.01621 -0.0396 0.9860 0.0160
-9.250 -0.8164 0.02192 0.01538 -0.0409 0.9837 0.0165
-9.000 -0.7920 0.02126 0.01468 -0.0412 0.9803 0.0172
-8.750 -0.7697 0.02050 0.01387 -0.0410 0.9758 0.0177
-8.500 -0.7417 0.01972 0.01305 -0.0419 0.9730 0.0183
-8.250 -0.7113 0.01887 0.01221 -0.0434 0.9711 0.0193
-8.000 -0.6928 0.01828 0.01159 -0.0421 0.9655 0.0202
-7.750 -0.6655 0.01764 0.01091 -0.0425 0.9619 0.0215
-7.500 -0.6346 0.01694 0.01021 -0.0438 0.9596 0.0235
-7.250 -0.6013 0.01629 0.00957 -0.0454 0.9580 0.0267
-7.000 -0.5825 0.01575 0.00903 -0.0439 0.9521 0.0307
-6.750 -0.5556 0.01509 0.00842 -0.0441 0.9482 0.0398
-6.500 -0.5248 0.01434 0.00782 -0.0452 0.9458 0.0619
-6.250 -0.4932 0.01344 0.00720 -0.0467 0.9440 0.1069
-6.000 -0.4724 0.01257 0.00667 -0.0459 0.9392 0.1689
-5.750 -0.4502 0.01181 0.00620 -0.0453 0.9338 0.2310
-5.500 -0.4187 0.01108 0.00577 -0.0465 0.9314 0.2949
-5.250 -0.3835 0.01051 0.00542 -0.0483 0.9298 0.3486
-5.000 -0.3462 0.01004 0.00513 -0.0504 0.9287 0.3930
-4.750 -0.3089 0.00966 0.00487 -0.0524 0.9276 0.4311
-4.500 -0.2921 0.00944 0.00472 -0.0499 0.9188 0.4549
-4.250 -0.2568 0.00917 0.00448 -0.0513 0.9162 0.4772
-4.000 -0.2206 0.00890 0.00427 -0.0528 0.9140 0.5013
-3.750 -0.1833 0.00865 0.00407 -0.0546 0.9119 0.5231
-3.500 -0.1617 0.00853 0.00394 -0.0530 0.9032 0.5366
-3.250 -0.1272 0.00831 0.00374 -0.0541 0.8990 0.5486
-3.000 -0.0901 0.00810 0.00352 -0.0557 0.8954 0.5593
-2.750 -0.0660 0.00800 0.00341 -0.0547 0.8855 0.5695
-2.500 -0.0309 0.00782 0.00323 -0.0559 0.8795 0.5790
-2.250 -0.0042 0.00774 0.00313 -0.0554 0.8688 0.5887
-2.000 0.0299 0.00761 0.00298 -0.0564 0.8604 0.5978
-1.750 0.0567 0.00756 0.00291 -0.0559 0.8477 0.6074
-1.500 0.0855 0.00749 0.00284 -0.0559 0.8351 0.6162
-1.250 0.1152 0.00747 0.00276 -0.0560 0.8222 0.6254
-1.000 0.1439 0.00744 0.00269 -0.0559 0.8078 0.6334
-0.750 0.1708 0.00744 0.00267 -0.0554 0.7922 0.6416
-0.500 0.1979 0.00747 0.00263 -0.0551 0.7756 0.6496
-0.250 0.2244 0.00749 0.00263 -0.0546 0.7582 0.6571
0.000 0.2508 0.00755 0.00261 -0.0540 0.7397 0.6652
0.250 0.2764 0.00760 0.00262 -0.0534 0.7205 0.6724
0.500 0.3017 0.00769 0.00264 -0.0526 0.7002 0.6799
1.000 0.3500 0.00790 0.00270 -0.0507 0.6525 0.6946
1.250 0.3725 0.00807 0.00274 -0.0495 0.6232 0.7024
1.500 0.3954 0.00820 0.00279 -0.0483 0.5948 0.7095
1.750 0.4178 0.00837 0.00287 -0.0471 0.5683 0.7168
2.000 0.4408 0.00855 0.00294 -0.0460 0.5415 0.7246
2.250 0.4629 0.00872 0.00303 -0.0447 0.5138 0.7315
2.500 0.4853 0.00892 0.00315 -0.0436 0.4880 0.7391
2.750 0.5079 0.00913 0.00325 -0.0425 0.4603 0.7465
3.000 0.5293 0.00935 0.00339 -0.0411 0.4327 0.7535
3.250 0.5516 0.00959 0.00352 -0.0400 0.4053 0.7612
3.500 0.5732 0.00984 0.00367 -0.0388 0.3795 0.7683
3.750 0.5953 0.01006 0.00384 -0.0376 0.3554 0.7755
4.000 0.6176 0.01033 0.00399 -0.0366 0.3315 0.7834
4.250 0.6387 0.01059 0.00418 -0.0353 0.3086 0.7903
4.500 0.6604 0.01085 0.00438 -0.0341 0.2877 0.7980
4.750 0.6823 0.01111 0.00456 -0.0330 0.2682 0.8057
5.000 0.7031 0.01136 0.00477 -0.0316 0.2501 0.8131
5.250 0.7240 0.01164 0.00497 -0.0303 0.2329 0.8215
5.500 0.7435 0.01189 0.00519 -0.0287 0.2160 0.8291
5.750 0.7631 0.01217 0.00542 -0.0272 0.1998 0.8377
6.000 0.7820 0.01247 0.00567 -0.0256 0.1840 0.8460
6.250 0.8006 0.01279 0.00594 -0.0239 0.1694 0.8551
6.500 0.8185 0.01313 0.00623 -0.0221 0.1563 0.8644
6.750 0.8367 0.01345 0.00654 -0.0203 0.1457 0.8745
7.000 0.8540 0.01376 0.00685 -0.0184 0.1373 0.8848
7.250 0.8702 0.01414 0.00720 -0.0163 0.1300 0.8968
7.500 0.8868 0.01439 0.00751 -0.0142 0.1249 0.9098
7.750 0.9012 0.01468 0.00782 -0.0117 0.1201 0.9257
8.000 0.9148 0.01506 0.00822 -0.0092 0.1158 0.9477
8.250 0.9456 0.01538 0.00861 -0.0102 0.1124 0.9719
8.500 0.9742 0.01582 0.00903 -0.0110 0.1088 1.0000
8.750 0.9920 0.01639 0.00956 -0.0099 0.1056 1.0000
9.000 1.0113 0.01687 0.01005 -0.0088 0.1034 1.0000
9.250 1.0316 0.01726 0.01047 -0.0079 0.1013 1.0000
9.500 1.0509 0.01769 0.01092 -0.0069 0.0992 1.0000
9.750 1.0684 0.01821 0.01144 -0.0056 0.0974 1.0000
10.000 1.0834 0.01886 0.01208 -0.0040 0.0954 1.0000
10.250 1.0961 0.01970 0.01290 -0.0022 0.0935 1.0000
10.500 1.1145 0.02016 0.01343 -0.0011 0.0925 1.0000
10.750 1.1318 0.02070 0.01402 0.0001 0.0912 1.0000
11.000 1.1483 0.02129 0.01465 0.0014 0.0899 1.0000
11.250 1.1642 0.02191 0.01530 0.0026 0.0885 1.0000
11.500 1.1793 0.02258 0.01599 0.0039 0.0872 1.0000
11.750 1.1930 0.02337 0.01679 0.0053 0.0861 1.0000
12.000 1.2045 0.02437 0.01779 0.0069 0.0847 1.0000
12.250 1.2167 0.02543 0.01888 0.0083 0.0835 1.0000
12.500 1.2316 0.02617 0.01969 0.0094 0.0829 1.0000
12.750 1.2458 0.02698 0.02057 0.0106 0.0821 1.0000
13.000 1.2592 0.02785 0.02150 0.0117 0.0812 1.0000
13.250 1.2722 0.02875 0.02246 0.0128 0.0802 1.0000
13.500 1.2845 0.02973 0.02350 0.0138 0.0792 1.0000
13.750 1.2965 0.03074 0.02455 0.0148 0.0783 1.0000
14.000 1.3078 0.03184 0.02568 0.0158 0.0775 1.0000
14.250 1.3186 0.03303 0.02690 0.0168 0.0767 1.0000
14.500 1.3297 0.03432 0.02821 0.0176 0.0757 1.0000
14.750 1.3417 0.03577 0.02970 0.0184 0.0746 1.0000
15.000 1.3510 0.03706 0.03108 0.0193 0.0742 1.0000
15.250 1.3591 0.03843 0.03255 0.0200 0.0735 1.0000
15.500 1.3673 0.03992 0.03414 0.0206 0.0729 1.0000
15.750 1.3750 0.04148 0.03580 0.0212 0.0722 1.0000
16.000 1.3821 0.04315 0.03755 0.0216 0.0715 1.0000
16.250 1.3888 0.04488 0.03936 0.0220 0.0708 1.0000
16.500 1.3951 0.04667 0.04122 0.0222 0.0701 1.0000
16.750 1.4013 0.04853 0.04314 0.0224 0.0693 1.0000
17.000 1.4078 0.05042 0.04508 0.0224 0.0687 1.0000
17.250 1.4148 0.05232 0.04702 0.0224 0.0681 1.0000
17.500 1.4219 0.05429 0.04901 0.0225 0.0673 1.0000
17.750 1.4256 0.05672 0.05154 0.0225 0.0665 1.0000
18.000 1.4245 0.05957 0.05452 0.0219 0.0661 1.0000
18.250 1.4231 0.06258 0.05767 0.0212 0.0656 1.0000
18.500 1.4217 0.06569 0.06091 0.0203 0.0651 1.0000
18.750 1.4182 0.06916 0.06451 0.0191 0.0644 1.0000
19.000 1.4152 0.07270 0.06817 0.0178 0.0639 1.0000
19.250 1.4115 0.07641 0.07199 0.0162 0.0632 1.0000
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