GM15 (smoothed) (gm15sm-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: GM15 (smoothed) (gm15sm-il) Reynolds number: 1,000,000 Max Cl/Cd: 119.49 at α=4° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-gm15sm-il-1000000-n5.txt Download as CSV file: xf-gm15sm-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GM15 (smoothed)
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
------ -------- --------- --------- -------- -------- --------
-9.250 -0.3610 0.10570 0.10406 -0.0240 1.0000 0.0057
-9.000 -0.3576 0.10261 0.10098 -0.0247 1.0000 0.0055
-8.750 -0.3558 0.09955 0.09794 -0.0251 1.0000 0.0052
-8.500 -0.3444 0.09532 0.09371 -0.0286 0.9992 0.0050
-8.250 -0.3310 0.09051 0.08889 -0.0332 0.9973 0.0048
-8.000 -0.3248 0.08655 0.08494 -0.0355 0.9816 0.0048
-7.750 -0.3110 0.08174 0.08013 -0.0406 0.9731 0.0047
-7.500 -0.2934 0.07664 0.07503 -0.0471 0.9677 0.0049
-7.000 -0.1825 0.02015 0.01748 -0.1354 0.9507 0.0056
-6.750 -0.1497 0.01613 0.01289 -0.1399 0.9461 0.0057
-6.500 -0.1214 0.01435 0.01080 -0.1411 0.9413 0.0059
-6.250 -0.0918 0.01320 0.00940 -0.1421 0.9371 0.0061
-6.000 -0.0635 0.01212 0.00810 -0.1427 0.9333 0.0063
-5.750 -0.0376 0.01107 0.00681 -0.1426 0.9285 0.0063
-5.500 -0.0101 0.01024 0.00579 -0.1427 0.9239 0.0064
-5.250 0.0175 0.00959 0.00498 -0.1428 0.9198 0.0065
-5.000 0.0437 0.00909 0.00438 -0.1424 0.9146 0.0066
-4.750 0.0711 0.00867 0.00384 -0.1423 0.9095 0.0067
-4.500 0.0977 0.00800 0.00300 -0.1421 0.9041 0.0077
-4.250 0.1246 0.00773 0.00269 -0.1418 0.8977 0.0084
-4.000 0.1520 0.00752 0.00241 -0.1416 0.8916 0.0092
-3.750 0.1789 0.00731 0.00214 -0.1412 0.8838 0.0099
-3.500 0.2059 0.00714 0.00191 -0.1409 0.8753 0.0106
-3.250 0.2328 0.00693 0.00162 -0.1405 0.8649 0.0127
-3.000 0.2594 0.00680 0.00146 -0.1401 0.8520 0.0159
-2.750 0.2857 0.00669 0.00128 -0.1396 0.8359 0.0206
-2.500 0.3117 0.00662 0.00114 -0.1390 0.8161 0.0251
-2.250 0.3370 0.00656 0.00101 -0.1383 0.7938 0.0347
-2.000 0.3618 0.00650 0.00089 -0.1376 0.7687 0.0566
-1.750 0.3862 0.00642 0.00082 -0.1367 0.7413 0.0950
-1.500 0.4108 0.00642 0.00077 -0.1359 0.7146 0.1227
-1.250 0.4358 0.00645 0.00075 -0.1352 0.6903 0.1444
-1.000 0.4610 0.00648 0.00074 -0.1346 0.6682 0.1689
-0.750 0.4865 0.00650 0.00075 -0.1340 0.6480 0.1993
-0.500 0.5120 0.00655 0.00077 -0.1334 0.6296 0.2187
-0.250 0.5380 0.00660 0.00078 -0.1329 0.6121 0.2329
0.000 0.5640 0.00667 0.00081 -0.1324 0.5952 0.2462
0.250 0.5901 0.00673 0.00084 -0.1319 0.5793 0.2588
0.500 0.6160 0.00681 0.00088 -0.1314 0.5623 0.2725
0.750 0.6420 0.00689 0.00092 -0.1310 0.5466 0.2858
1.000 0.6681 0.00697 0.00098 -0.1305 0.5312 0.2993
1.250 0.6941 0.00705 0.00104 -0.1301 0.5158 0.3133
1.500 0.7202 0.00713 0.00111 -0.1296 0.5006 0.3270
1.750 0.7462 0.00722 0.00118 -0.1292 0.4855 0.3421
2.000 0.7721 0.00732 0.00128 -0.1287 0.4699 0.3575
2.250 0.7980 0.00742 0.00137 -0.1282 0.4547 0.3756
2.500 0.8238 0.00753 0.00148 -0.1278 0.4386 0.3940
2.750 0.8495 0.00764 0.00159 -0.1273 0.4226 0.4151
3.000 0.8749 0.00776 0.00172 -0.1268 0.4062 0.4426
3.250 0.9003 0.00787 0.00188 -0.1262 0.3896 0.4778
3.500 0.9254 0.00794 0.00204 -0.1257 0.3725 0.5366
4.000 0.9750 0.00816 0.00261 -0.1250 0.2647 1.0000
4.250 0.9958 0.00885 0.00297 -0.1238 0.1977 1.0000
4.500 1.0184 0.00937 0.00328 -0.1228 0.1546 1.0000
4.750 1.0401 0.00999 0.00365 -0.1218 0.1059 1.0000
5.000 1.0613 0.01067 0.00410 -0.1206 0.0589 1.0000
5.250 1.0839 0.01120 0.00449 -0.1196 0.0330 1.0000
5.500 1.1077 0.01158 0.00482 -0.1189 0.0217 1.0000
5.750 1.1319 0.01191 0.00515 -0.1182 0.0173 1.0000
6.000 1.1559 0.01226 0.00550 -0.1174 0.0132 1.0000
6.250 1.1799 0.01259 0.00584 -0.1167 0.0114 1.0000
6.500 1.2033 0.01298 0.00623 -0.1159 0.0099 1.0000
6.750 1.2263 0.01342 0.00671 -0.1150 0.0085 1.0000
7.000 1.2499 0.01375 0.00709 -0.1142 0.0080 1.0000
7.250 1.2731 0.01413 0.00751 -0.1134 0.0075 1.0000
7.500 1.2959 0.01453 0.00795 -0.1125 0.0069 1.0000
7.750 1.3182 0.01497 0.00841 -0.1116 0.0063 1.0000
8.000 1.3395 0.01552 0.00900 -0.1105 0.0056 1.0000
8.250 1.3597 0.01616 0.00972 -0.1091 0.0051 1.0000
8.500 1.3817 0.01656 0.01016 -0.1082 0.0048 1.0000
8.750 1.4034 0.01699 0.01064 -0.1072 0.0044 1.0000
9.000 1.4241 0.01749 0.01119 -0.1060 0.0040 1.0000
9.250 1.4442 0.01802 0.01176 -0.1048 0.0036 1.0000
9.500 1.4634 0.01861 0.01239 -0.1035 0.0033 1.0000
9.750 1.4812 0.01931 0.01316 -0.1019 0.0031 1.0000
10.000 1.4949 0.02036 0.01432 -0.0996 0.0028 1.0000
10.250 1.5111 0.02109 0.01513 -0.0978 0.0027 1.0000
10.500 1.5267 0.02182 0.01595 -0.0959 0.0026 1.0000
10.750 1.5393 0.02266 0.01688 -0.0935 0.0026 1.0000
11.000 1.5500 0.02347 0.01781 -0.0908 0.0025 1.0000
11.250 1.5583 0.02442 0.01886 -0.0878 0.0024 1.0000
11.500 1.5666 0.02538 0.01992 -0.0849 0.0023 1.0000
11.750 1.5736 0.02643 0.02108 -0.0820 0.0022 1.0000
12.000 1.5786 0.02766 0.02243 -0.0790 0.0022 1.0000
12.250 1.5842 0.02890 0.02377 -0.0763 0.0021 1.0000
12.500 1.5897 0.03019 0.02516 -0.0738 0.0020 1.0000
12.750 1.5925 0.03177 0.02686 -0.0712 0.0020 1.0000
13.000 1.5958 0.03336 0.02857 -0.0689 0.0019 1.0000
13.250 1.5988 0.03507 0.03039 -0.0669 0.0019 1.0000
13.500 1.5993 0.03710 0.03254 -0.0649 0.0018 1.0000
13.750 1.6017 0.03904 0.03459 -0.0633 0.0018 1.0000
14.000 1.6011 0.04140 0.03707 -0.0618 0.0017 1.0000
14.250 1.5977 0.04424 0.04007 -0.0607 0.0017 1.0000
14.500 1.5956 0.04708 0.04302 -0.0600 0.0016 1.0000
14.750 1.5881 0.05079 0.04689 -0.0596 0.0016 1.0000
15.000 1.5821 0.05456 0.05080 -0.0597 0.0016 1.0000
15.250 1.5734 0.05894 0.05532 -0.0603 0.0016 1.0000
15.500 1.5643 0.06363 0.06016 -0.0614 0.0015 1.0000
15.750 1.5514 0.06922 0.06590 -0.0631 0.0015 1.0000
16.000 1.5376 0.07526 0.07211 -0.0653 0.0015 1.0000
16.250 1.5215 0.08207 0.07908 -0.0682 0.0015 1.0000
16.500 1.5044 0.08942 0.08658 -0.0716 0.0015 1.0000
16.750 1.4873 0.09709 0.09441 -0.0754 0.0015 1.0000
17.000 1.4674 0.10576 0.10323 -0.0799 0.0015 1.0000
17.250 1.4481 0.11457 0.11220 -0.0847 0.0015 1.0000
17.500 1.4267 0.12427 0.12205 -0.0903 0.0015 1.0000
17.750 1.4059 0.13415 0.13208 -0.0960 0.0015 1.0000
|
Polar data table (+)
Polar graphs
<< Back to GM15 (smoothed) (gm15sm-il)