MH 45 9.85% (mh45-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: MH 45 9.85% (mh45-il) Reynolds number: 200,000 Max Cl/Cd: 58.73 at α=6.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-mh45-il-200000-n5.txt Download as CSV file: xf-mh45-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: MH 45 9.85%
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.250 -0.5924 0.08724 0.08406 0.0082 1.0000 0.0087
-9.000 -0.6010 0.08040 0.07728 0.0039 1.0000 0.0086
-8.750 -0.6126 0.07262 0.06956 -0.0017 1.0000 0.0083
-8.500 -0.6406 0.05876 0.05565 -0.0140 1.0000 0.0078
-8.250 -0.6744 0.04671 0.04303 -0.0196 1.0000 0.0073
-8.000 -0.6773 0.04035 0.03610 -0.0205 1.0000 0.0071
-7.750 -0.6679 0.03620 0.03147 -0.0206 1.0000 0.0070
-7.500 -0.6544 0.03251 0.02733 -0.0205 1.0000 0.0071
-7.250 -0.6369 0.02942 0.02381 -0.0203 1.0000 0.0071
-7.000 -0.6119 0.02668 0.02064 -0.0211 0.9448 0.0072
-6.750 -0.5908 0.02473 0.01832 -0.0203 0.9205 0.0073
-6.500 -0.5708 0.02319 0.01649 -0.0191 0.9026 0.0075
-6.250 -0.5498 0.02185 0.01490 -0.0179 0.8884 0.0078
-6.000 -0.5279 0.02060 0.01343 -0.0167 0.8760 0.0081
-5.750 -0.5053 0.01946 0.01210 -0.0156 0.8649 0.0086
-5.500 -0.4825 0.01842 0.01088 -0.0146 0.8548 0.0091
-5.250 -0.4586 0.01771 0.00997 -0.0136 0.8452 0.0102
-5.000 -0.4349 0.01689 0.00909 -0.0130 0.8358 0.0116
-4.750 -0.4104 0.01627 0.00835 -0.0122 0.8273 0.0134
-4.500 -0.3855 0.01551 0.00744 -0.0115 0.8184 0.0147
-4.250 -0.3605 0.01480 0.00662 -0.0109 0.8099 0.0172
-4.000 -0.3352 0.01418 0.00589 -0.0101 0.8019 0.0232
-3.750 -0.3095 0.01348 0.00520 -0.0097 0.7932 0.0416
-3.500 -0.2859 0.01254 0.00466 -0.0091 0.7856 0.1212
-3.250 -0.2604 0.01197 0.00437 -0.0088 0.7767 0.1962
-3.000 -0.2345 0.01161 0.00413 -0.0084 0.7687 0.2453
-2.750 -0.2088 0.01123 0.00391 -0.0080 0.7602 0.3050
-2.500 -0.1828 0.01090 0.00373 -0.0076 0.7516 0.3605
-2.250 -0.1569 0.01065 0.00355 -0.0070 0.7437 0.4040
-2.000 -0.1303 0.01042 0.00339 -0.0067 0.7343 0.4461
-1.750 -0.1042 0.01020 0.00323 -0.0061 0.7258 0.4897
-1.500 -0.0782 0.00997 0.00311 -0.0056 0.7168 0.5367
-1.250 -0.0523 0.00973 0.00300 -0.0049 0.7075 0.5884
-1.000 -0.0272 0.00949 0.00289 -0.0041 0.6989 0.6448
-0.750 -0.0021 0.00923 0.00283 -0.0031 0.6889 0.7094
-0.500 0.0238 0.00898 0.00279 -0.0021 0.6792 0.7839
-0.250 0.0583 0.00882 0.00276 -0.0028 0.6691 0.8660
0.000 0.1074 0.00878 0.00270 -0.0068 0.6573 0.9306
0.250 0.1512 0.00879 0.00263 -0.0099 0.6447 0.9682
0.500 0.1923 0.00881 0.00256 -0.0126 0.6318 0.9912
0.750 0.2253 0.00886 0.00250 -0.0136 0.6186 1.0000
1.000 0.2512 0.00891 0.00247 -0.0132 0.6053 1.0000
1.250 0.2772 0.00898 0.00245 -0.0127 0.5914 1.0000
1.500 0.3033 0.00906 0.00244 -0.0123 0.5768 1.0000
1.750 0.3295 0.00915 0.00244 -0.0119 0.5614 1.0000
2.000 0.3557 0.00925 0.00247 -0.0115 0.5453 1.0000
2.250 0.3819 0.00938 0.00251 -0.0111 0.5288 1.0000
2.500 0.4081 0.00951 0.00256 -0.0107 0.5116 1.0000
2.750 0.4345 0.00966 0.00264 -0.0104 0.4936 1.0000
3.000 0.4608 0.00982 0.00273 -0.0101 0.4751 1.0000
3.250 0.4870 0.01001 0.00285 -0.0097 0.4566 1.0000
3.500 0.5133 0.01021 0.00299 -0.0094 0.4377 1.0000
3.750 0.5395 0.01042 0.00314 -0.0092 0.4185 1.0000
4.000 0.5657 0.01066 0.00332 -0.0089 0.3994 1.0000
4.250 0.5919 0.01090 0.00351 -0.0086 0.3807 1.0000
4.500 0.6180 0.01116 0.00372 -0.0084 0.3613 1.0000
4.750 0.6440 0.01144 0.00396 -0.0081 0.3424 1.0000
5.000 0.6699 0.01173 0.00423 -0.0079 0.3229 1.0000
5.250 0.6957 0.01204 0.00450 -0.0076 0.3028 1.0000
5.500 0.7213 0.01239 0.00480 -0.0074 0.2828 1.0000
5.750 0.7468 0.01275 0.00513 -0.0071 0.2620 1.0000
6.250 0.7970 0.01357 0.00588 -0.0066 0.2211 1.0000
6.500 0.8217 0.01403 0.00630 -0.0064 0.2017 1.0000
6.750 0.8461 0.01451 0.00675 -0.0061 0.1840 1.0000
7.000 0.8704 0.01500 0.00725 -0.0057 0.1664 1.0000
7.250 0.8944 0.01553 0.00777 -0.0054 0.1509 1.0000
7.500 0.9180 0.01608 0.00832 -0.0050 0.1367 1.0000
7.750 0.9413 0.01667 0.00891 -0.0046 0.1235 1.0000
8.000 0.9642 0.01727 0.00953 -0.0042 0.1121 1.0000
8.250 0.9866 0.01791 0.01022 -0.0037 0.1014 1.0000
8.750 1.0303 0.01925 0.01163 -0.0027 0.0823 1.0000
9.000 1.0514 0.01997 0.01240 -0.0021 0.0740 1.0000
9.250 1.0710 0.02081 0.01324 -0.0015 0.0662 1.0000
9.500 1.0914 0.02152 0.01406 -0.0008 0.0588 1.0000
9.750 1.1097 0.02242 0.01502 0.0000 0.0525 1.0000
10.000 1.1277 0.02329 0.01598 0.0008 0.0465 1.0000
10.250 1.1433 0.02434 0.01710 0.0018 0.0422 1.0000
10.500 1.1588 0.02532 0.01820 0.0028 0.0377 1.0000
10.750 1.1693 0.02664 0.01954 0.0041 0.0338 1.0000
11.000 1.1814 0.02773 0.02080 0.0053 0.0308 1.0000
11.250 1.1877 0.02900 0.02218 0.0071 0.0283 1.0000
11.500 1.1898 0.03067 0.02391 0.0086 0.0263 1.0000
11.750 1.1917 0.03257 0.02595 0.0097 0.0247 1.0000
12.000 1.1964 0.03439 0.02792 0.0104 0.0229 1.0000
12.250 1.2004 0.03635 0.03001 0.0108 0.0212 1.0000
12.500 1.2009 0.03878 0.03255 0.0110 0.0201 1.0000
12.750 1.1970 0.04181 0.03567 0.0108 0.0190 1.0000
13.000 1.1946 0.04484 0.03883 0.0103 0.0181 1.0000
13.250 1.1931 0.04793 0.04211 0.0097 0.0173 1.0000
13.500 1.1910 0.05123 0.04556 0.0088 0.0163 1.0000
13.750 1.1865 0.05499 0.04947 0.0074 0.0155 1.0000
14.000 1.1810 0.05903 0.05365 0.0058 0.0149 1.0000
14.250 1.1736 0.06354 0.05828 0.0037 0.0144 1.0000
14.500 1.1630 0.06870 0.06357 0.0012 0.0139 1.0000
14.750 1.1512 0.07425 0.06923 -0.0015 0.0136 1.0000
15.000 1.1391 0.08004 0.07514 -0.0044 0.0134 1.0000
15.250 1.1276 0.08603 0.08126 -0.0074 0.0131 1.0000
15.500 1.1161 0.09239 0.08782 -0.0109 0.0126 1.0000
15.750 1.1035 0.09888 0.09444 -0.0142 0.0126 1.0000
16.000 1.0899 0.10599 0.10170 -0.0181 0.0123 1.0000
16.250 1.0760 0.11319 0.10905 -0.0219 0.0122 1.0000
16.500 1.0617 0.12079 0.11678 -0.0260 0.0121 1.0000
16.750 1.0462 0.12890 0.12503 -0.0305 0.0120 1.0000
17.000 1.0311 0.13717 0.13342 -0.0350 0.0120 1.0000
17.250 1.0150 0.14599 0.14236 -0.0399 0.0121 1.0000
17.500 0.9956 0.15616 0.15264 -0.0455 0.0122 1.0000
17.750 0.9720 0.16809 0.16467 -0.0520 0.0124 1.0000
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Polar data table (+)
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