UNIVERSITY OF GLASGOW GU25-5(11)8 AIRFOIL (gu255118-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: UNIVERSITY OF GLASGOW GU25-5(11)8 AIRFOIL (gu255118-il) Reynolds number: 1,000,000 Max Cl/Cd: 136.26 at α=9.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-gu255118-il-1000000.txt Download as CSV file: xf-gu255118-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: UNIVERSITY OF GLASGOW GU25-5(11)8 AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-12.250 0.1895 0.07921 0.07549 -0.1569 0.6181 0.0223
-12.000 0.1937 0.07645 0.07274 -0.1576 0.6177 0.0224
-11.750 0.2032 0.07482 0.07112 -0.1580 0.6170 0.0227
-11.500 0.2065 0.07193 0.06824 -0.1588 0.6164 0.0228
-11.250 -0.1886 0.03133 0.02676 -0.1808 0.6193 0.0187
-11.000 -0.1895 0.03054 0.02594 -0.1777 0.6185 0.0189
-10.750 -0.1885 0.02993 0.02532 -0.1744 0.6178 0.0190
-10.500 -0.2037 0.02857 0.02382 -0.1687 0.6172 0.0191
-10.250 -0.1938 0.02809 0.02332 -0.1665 0.6164 0.0192
-10.000 -0.1804 0.02775 0.02296 -0.1649 0.6156 0.0194
-9.750 -0.1661 0.02744 0.02264 -0.1633 0.6148 0.0197
-9.500 -0.1566 0.02668 0.02179 -0.1610 0.6140 0.0200
-9.250 -0.1532 0.02518 0.02010 -0.1579 0.6132 0.0202
-9.000 -0.1485 0.02356 0.01826 -0.1549 0.6124 0.0204
-8.750 -0.1405 0.02207 0.01655 -0.1521 0.6116 0.0206
-8.500 -0.1274 0.02095 0.01525 -0.1501 0.6108 0.0209
-8.250 -0.1123 0.01989 0.01401 -0.1483 0.6101 0.0212
-8.000 -0.0949 0.01905 0.01301 -0.1468 0.6093 0.0215
-7.750 -0.0751 0.01857 0.01240 -0.1456 0.6086 0.0218
-7.500 -0.0546 0.01812 0.01182 -0.1445 0.6077 0.0220
-7.250 -0.0366 0.01670 0.01024 -0.1433 0.6070 0.0225
-7.000 -0.0147 0.01606 0.00957 -0.1426 0.6061 0.0229
-6.750 0.0085 0.01575 0.00922 -0.1421 0.6052 0.0233
-6.500 0.0322 0.01548 0.00891 -0.1417 0.6042 0.0238
-6.250 0.0561 0.01515 0.00854 -0.1412 0.6035 0.0242
-6.000 0.0795 0.01475 0.00810 -0.1406 0.6032 0.0246
-5.750 0.1031 0.01437 0.00768 -0.1401 0.6029 0.0250
-5.500 0.1269 0.01404 0.00731 -0.1395 0.6025 0.0255
-5.250 0.1509 0.01375 0.00699 -0.1390 0.6021 0.0259
-5.000 0.1752 0.01354 0.00674 -0.1386 0.6017 0.0262
-4.750 0.1966 0.01301 0.00619 -0.1376 0.6012 0.0268
-4.500 0.2180 0.01260 0.00578 -0.1366 0.6007 0.0274
-4.250 0.2414 0.01238 0.00557 -0.1360 0.6002 0.0282
-4.000 0.2654 0.01221 0.00539 -0.1355 0.5996 0.0290
-3.750 0.2891 0.01202 0.00518 -0.1349 0.5990 0.0296
-3.500 0.3131 0.01185 0.00500 -0.1344 0.5985 0.0303
-3.250 0.3375 0.01171 0.00484 -0.1339 0.5980 0.0309
-3.000 0.3624 0.01160 0.00472 -0.1336 0.5975 0.0314
-2.750 0.3845 0.01133 0.00442 -0.1327 0.5970 0.0326
-2.500 0.4090 0.01120 0.00429 -0.1323 0.5966 0.0341
-2.250 0.4341 0.01112 0.00420 -0.1320 0.5961 0.0354
-2.000 0.4595 0.01105 0.00413 -0.1318 0.5957 0.0367
-1.750 0.4843 0.01094 0.00401 -0.1314 0.5952 0.0390
-1.500 0.5095 0.01087 0.00395 -0.1312 0.5948 0.0419
-1.250 0.5347 0.01080 0.00390 -0.1309 0.5944 0.0496
-1.000 0.5559 0.01050 0.00385 -0.1299 0.5940 0.1244
-0.750 0.5739 0.01003 0.00383 -0.1284 0.5936 0.2700
-0.500 0.5905 0.00956 0.00384 -0.1267 0.5931 0.4342
0.000 0.6318 0.00920 0.00396 -0.1244 0.5923 0.6062
0.250 0.6529 0.00910 0.00404 -0.1233 0.5919 0.6669
0.500 0.6726 0.00901 0.00412 -0.1218 0.5915 0.7313
0.750 0.6919 0.00891 0.00422 -0.1202 0.5911 0.7957
1.000 0.7975 0.00892 0.00458 -0.1378 0.5908 0.9321
1.250 0.8443 0.00919 0.00484 -0.1421 0.5904 0.9559
1.500 0.8836 0.00945 0.00507 -0.1449 0.5899 0.9638
1.750 0.9167 0.00971 0.00531 -0.1465 0.5892 0.9700
2.000 0.9559 0.00998 0.00557 -0.1495 0.5885 0.9724
2.250 0.9930 0.01011 0.00569 -0.1520 0.5883 0.9757
2.500 1.0240 0.01027 0.00585 -0.1531 0.5881 0.9809
2.750 1.0615 0.01040 0.00597 -0.1557 0.5879 0.9830
3.000 1.1001 0.01052 0.00609 -0.1586 0.5877 0.9848
3.250 1.1373 0.01064 0.00623 -0.1612 0.5874 0.9869
3.500 1.1734 0.01078 0.00637 -0.1636 0.5872 0.9894
3.750 1.2080 0.01092 0.00653 -0.1657 0.5869 0.9922
4.000 1.2432 0.01105 0.00667 -0.1679 0.5866 0.9941
4.250 1.2806 0.01116 0.00679 -0.1706 0.5863 0.9959
4.500 1.3169 0.01126 0.00692 -0.1731 0.5858 0.9979
4.750 1.3530 0.01137 0.00705 -0.1756 0.5854 0.9996
5.000 1.3769 0.01147 0.00718 -0.1754 0.5847 1.0000
5.250 1.3959 0.01157 0.00731 -0.1742 0.5839 1.0000
5.500 1.4150 0.01168 0.00744 -0.1729 0.5832 1.0000
5.750 1.4345 0.01180 0.00759 -0.1718 0.5824 1.0000
6.000 1.4541 0.01193 0.00775 -0.1707 0.5818 1.0000
6.250 1.4739 0.01205 0.00790 -0.1696 0.5811 1.0000
6.500 1.4939 0.01218 0.00805 -0.1686 0.5805 1.0000
6.750 1.5145 0.01228 0.00818 -0.1676 0.5797 1.0000
7.000 1.5358 0.01237 0.00829 -0.1669 0.5789 1.0000
7.250 1.5586 0.01241 0.00835 -0.1664 0.5779 1.0000
7.500 1.5840 0.01242 0.00835 -0.1664 0.5767 1.0000
7.750 1.6107 0.01252 0.00846 -0.1668 0.5752 1.0000
8.000 1.6215 0.01264 0.00862 -0.1638 0.5725 1.0000
8.250 1.6254 0.01266 0.00870 -0.1594 0.5708 1.0000
8.500 1.6234 0.01257 0.00866 -0.1536 0.5682 1.0000
8.750 1.6289 0.01251 0.00861 -0.1494 0.5661 1.0000
9.000 1.6426 0.01234 0.00845 -0.1469 0.5635 1.0000
9.250 1.6664 0.01223 0.00829 -0.1466 0.5594 1.0000
9.500 1.6587 0.01240 0.00854 -0.1401 0.5571 1.0000
9.750 1.6598 0.01264 0.00885 -0.1357 0.5546 1.0000
10.000 1.6621 0.01282 0.00908 -0.1315 0.5503 1.0000
10.250 1.6728 0.01303 0.00929 -0.1291 0.5466 1.0000
10.500 1.6722 0.01365 0.00997 -0.1250 0.5415 1.0000
10.750 1.6719 0.01444 0.01083 -0.1213 0.5353 1.0000
11.000 1.6759 0.01525 0.01166 -0.1185 0.5287 1.0000
11.250 1.6783 0.01633 0.01282 -0.1157 0.5205 1.0000
11.500 1.6766 0.01772 0.01424 -0.1126 0.5085 1.0000
11.750 1.6564 0.02026 0.01674 -0.1073 0.4885 1.0000
12.000 1.6223 0.02389 0.02031 -0.1009 0.4670 1.0000
12.250 1.5887 0.02777 0.02412 -0.0948 0.4494 1.0000
12.500 1.5563 0.03178 0.02808 -0.0893 0.4320 1.0000
12.750 1.5253 0.03589 0.03213 -0.0842 0.4110 1.0000
13.000 1.5009 0.03967 0.03585 -0.0800 0.3928 1.0000
13.250 1.4720 0.04393 0.04002 -0.0756 0.3711 1.0000
13.500 1.4551 0.04733 0.04333 -0.0724 0.3507 1.0000
13.750 1.4358 0.05104 0.04693 -0.0692 0.3287 1.0000
14.000 1.4244 0.05416 0.04998 -0.0668 0.3105 1.0000
14.250 1.4125 0.05734 0.05303 -0.0644 0.2863 1.0000
14.500 1.4016 0.06053 0.05611 -0.0622 0.2653 1.0000
14.750 1.3916 0.06367 0.05911 -0.0601 0.2393 1.0000
15.000 1.3826 0.06678 0.06208 -0.0582 0.2143 1.0000
15.250 1.3720 0.07006 0.06519 -0.0563 0.1861 1.0000
15.500 1.3686 0.07272 0.06772 -0.0549 0.1655 1.0000
15.750 1.3620 0.07578 0.07065 -0.0535 0.1420 1.0000
16.000 1.3518 0.07917 0.07383 -0.0519 0.1130 1.0000
16.250 1.3490 0.08189 0.07644 -0.0508 0.0931 1.0000
16.500 1.3391 0.08544 0.07982 -0.0495 0.0691 1.0000
16.750 1.3301 0.08892 0.08313 -0.0482 0.0452 1.0000
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