HAM-STD HS1-620 AIRFOIL (hs1620-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: HAM-STD HS1-620 AIRFOIL (hs1620-il) Reynolds number: 1,000,000 Max Cl/Cd: 70.65 at α=6° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-hs1620-il-1000000-n5.txt Download as CSV file: xf-hs1620-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: HAM-STD HS1-620 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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.500 -0.8873 0.09298 0.08932 -0.1104 0.9913 0.0316
-19.250 -0.9593 0.08010 0.07624 -0.1168 0.9901 0.0316
-19.000 -1.1191 0.05379 0.04941 -0.1312 0.9880 0.0311
-18.750 -1.1547 0.04460 0.03997 -0.1377 0.9865 0.0313
-18.500 -1.1649 0.03982 0.03505 -0.1408 0.9853 0.0315
-18.250 -1.1660 0.03645 0.03156 -0.1427 0.9843 0.0318
-18.000 -1.1615 0.03383 0.02884 -0.1442 0.9835 0.0321
-17.750 -1.1535 0.03173 0.02665 -0.1451 0.9827 0.0323
-17.500 -1.1463 0.02978 0.02462 -0.1455 0.9820 0.0327
-17.250 -1.1376 0.02812 0.02289 -0.1455 0.9812 0.0331
-17.000 -1.1334 0.02683 0.02154 -0.1438 0.9792 0.0335
-16.750 -1.1296 0.02576 0.02041 -0.1415 0.9764 0.0339
-16.500 -1.1204 0.02479 0.01939 -0.1399 0.9746 0.0344
-16.250 -1.1089 0.02393 0.01847 -0.1383 0.9731 0.0349
-16.000 -1.0961 0.02315 0.01764 -0.1368 0.9719 0.0354
-15.750 -1.0823 0.02244 0.01688 -0.1352 0.9708 0.0359
-15.500 -1.0676 0.02181 0.01619 -0.1336 0.9697 0.0363
-15.250 -1.0513 0.02114 0.01548 -0.1323 0.9688 0.0369
-15.000 -1.0360 0.02060 0.01491 -0.1306 0.9673 0.0375
-14.750 -1.0221 0.02016 0.01444 -0.1285 0.9652 0.0380
-14.500 -1.0040 0.01972 0.01397 -0.1271 0.9635 0.0387
-14.250 -0.9833 0.01929 0.01351 -0.1262 0.9622 0.0393
-14.000 -0.9609 0.01888 0.01307 -0.1256 0.9611 0.0400
-13.750 -0.9371 0.01846 0.01262 -0.1252 0.9601 0.0407
-13.500 -0.9124 0.01797 0.01211 -0.1251 0.9589 0.0416
-13.250 -0.8859 0.01749 0.01162 -0.1252 0.9575 0.0426
-13.000 -0.8585 0.01705 0.01115 -0.1254 0.9561 0.0436
-12.750 -0.8332 0.01669 0.01076 -0.1252 0.9541 0.0444
-12.500 -0.8108 0.01639 0.01043 -0.1243 0.9515 0.0451
-12.250 -0.7866 0.01603 0.01006 -0.1238 0.9495 0.0461
-12.000 -0.7607 0.01568 0.00970 -0.1237 0.9477 0.0472
-11.750 -0.7337 0.01536 0.00936 -0.1237 0.9461 0.0485
-11.500 -0.7057 0.01505 0.00903 -0.1239 0.9444 0.0496
-11.250 -0.6775 0.01469 0.00866 -0.1242 0.9429 0.0509
-11.000 -0.6484 0.01436 0.00833 -0.1247 0.9414 0.0523
-10.750 -0.6225 0.01413 0.00808 -0.1244 0.9395 0.0536
-10.500 -0.5964 0.01391 0.00785 -0.1241 0.9375 0.0547
-10.250 -0.5699 0.01363 0.00759 -0.1240 0.9355 0.0565
-10.000 -0.5423 0.01338 0.00734 -0.1240 0.9335 0.0583
-9.750 -0.5138 0.01315 0.00709 -0.1242 0.9314 0.0598
-9.500 -0.4847 0.01287 0.00682 -0.1246 0.9295 0.0617
-9.250 -0.4546 0.01262 0.00656 -0.1252 0.9277 0.0637
-9.000 -0.4248 0.01241 0.00634 -0.1257 0.9259 0.0657
-8.750 -0.3986 0.01220 0.00616 -0.1254 0.9232 0.0680
-8.500 -0.3712 0.01201 0.00597 -0.1253 0.9202 0.0704
-8.250 -0.3427 0.01181 0.00578 -0.1255 0.9171 0.0724
-8.000 -0.3130 0.01158 0.00556 -0.1259 0.9141 0.0753
-7.750 -0.2818 0.01137 0.00534 -0.1267 0.9113 0.0782
-7.500 -0.2549 0.01119 0.00519 -0.1265 0.9072 0.0810
-7.250 -0.2269 0.01103 0.00503 -0.1265 0.9025 0.0840
-7.000 -0.1970 0.01083 0.00484 -0.1270 0.8978 0.0871
-6.750 -0.1676 0.01065 0.00467 -0.1273 0.8926 0.0910
-6.500 -0.1391 0.01049 0.00451 -0.1274 0.8848 0.0943
-6.250 -0.1091 0.01031 0.00433 -0.1278 0.8769 0.0986
-6.000 -0.0799 0.01017 0.00417 -0.1281 0.8649 0.1027
-5.750 -0.0508 0.01004 0.00400 -0.1283 0.8474 0.1074
-5.500 -0.0232 0.00999 0.00385 -0.1281 0.8215 0.1118
-5.000 0.0266 0.01009 0.00370 -0.1266 0.7678 0.1209
-4.750 0.0518 0.01011 0.00366 -0.1260 0.7483 0.1263
-4.250 0.1046 0.01011 0.00357 -0.1253 0.7189 0.1360
-4.000 0.1313 0.01012 0.00354 -0.1250 0.7078 0.1409
-3.750 0.1581 0.01011 0.00351 -0.1247 0.6957 0.1460
-3.500 0.1848 0.01011 0.00348 -0.1245 0.6847 0.1513
-3.250 0.2110 0.01013 0.00347 -0.1241 0.6726 0.1558
-3.000 0.2377 0.01013 0.00345 -0.1238 0.6613 0.1613
-2.750 0.2636 0.01017 0.00345 -0.1233 0.6500 0.1659
-2.500 0.2908 0.01017 0.00343 -0.1231 0.6408 0.1704
-2.250 0.3169 0.01019 0.00344 -0.1227 0.6307 0.1753
-2.000 0.3436 0.01020 0.00344 -0.1224 0.6223 0.1799
-1.750 0.3703 0.01023 0.00344 -0.1221 0.6132 0.1838
-1.500 0.3958 0.01026 0.00346 -0.1216 0.6042 0.1893
-1.250 0.4216 0.01030 0.00348 -0.1211 0.5926 0.1944
-1.000 0.4462 0.01038 0.00351 -0.1203 0.5803 0.1977
-0.750 0.4689 0.01047 0.00356 -0.1192 0.5652 0.2025
-0.500 0.4907 0.01054 0.00361 -0.1178 0.5502 0.2076
-0.250 0.5108 0.01067 0.00368 -0.1161 0.5329 0.2122
0.000 0.5302 0.01087 0.00378 -0.1142 0.5109 0.2157
0.250 0.5493 0.01110 0.00391 -0.1123 0.4861 0.2214
0.500 0.5697 0.01134 0.00406 -0.1107 0.4610 0.2265
0.750 0.5912 0.01159 0.00422 -0.1094 0.4368 0.2315
1.000 0.6125 0.01189 0.00440 -0.1081 0.4100 0.2355
1.250 0.6335 0.01221 0.00461 -0.1067 0.3830 0.2422
1.500 0.6556 0.01249 0.00481 -0.1056 0.3615 0.2491
2.000 0.7014 0.01295 0.00519 -0.1038 0.3322 0.2670
2.500 0.7486 0.01332 0.00558 -0.1023 0.3120 0.3048
2.750 0.7731 0.01338 0.00579 -0.1018 0.3048 0.3699
3.000 0.7981 0.01337 0.00599 -0.1015 0.2989 0.4513
3.250 0.8225 0.01315 0.00630 -0.1012 0.2927 0.6424
3.500 0.8463 0.01322 0.00656 -0.1005 0.2870 0.7131
3.750 0.8701 0.01325 0.00680 -0.0998 0.2822 0.7795
4.000 0.8898 0.01326 0.00713 -0.0980 0.2774 0.8859
4.250 0.9063 0.01344 0.00743 -0.0954 0.2726 0.9560
4.500 0.9333 0.01367 0.00765 -0.0953 0.2684 0.9854
4.750 0.9625 0.01386 0.00782 -0.0959 0.2644 1.0000
5.000 0.9848 0.01411 0.00805 -0.0950 0.2603 1.0000
5.250 1.0062 0.01441 0.00831 -0.0939 0.2557 1.0000
5.500 1.0286 0.01469 0.00856 -0.0930 0.2518 1.0000
5.750 1.0518 0.01494 0.00880 -0.0922 0.2490 1.0000
6.000 1.0746 0.01521 0.00906 -0.0915 0.2455 1.0000
6.250 1.0964 0.01554 0.00936 -0.0905 0.2415 1.0000
6.500 1.1173 0.01590 0.00969 -0.0894 0.2373 1.0000
6.750 1.1397 0.01620 0.00999 -0.0886 0.2347 1.0000
7.000 1.1622 0.01651 0.01029 -0.0878 0.2318 1.0000
7.250 1.1841 0.01684 0.01061 -0.0870 0.2283 1.0000
7.500 1.2048 0.01724 0.01098 -0.0859 0.2246 1.0000
7.750 1.2249 0.01766 0.01139 -0.0848 0.2210 1.0000
8.000 1.2465 0.01802 0.01175 -0.0840 0.2186 1.0000
8.250 1.2681 0.01839 0.01213 -0.0831 0.2156 1.0000
8.500 1.2887 0.01881 0.01254 -0.0822 0.2119 1.0000
8.750 1.3078 0.01931 0.01302 -0.0810 0.2082 1.0000
9.000 1.3271 0.01981 0.01350 -0.0798 0.2047 1.0000
9.250 1.3479 0.02024 0.01394 -0.0789 0.2020 1.0000
9.500 1.3679 0.02071 0.01441 -0.0780 0.1987 1.0000
9.750 1.3863 0.02126 0.01496 -0.0768 0.1955 1.0000
10.000 1.4041 0.02187 0.01555 -0.0755 0.1921 1.0000
10.250 1.4234 0.02240 0.01609 -0.0745 0.1895 1.0000
10.500 1.4425 0.02295 0.01666 -0.0735 0.1865 1.0000
10.750 1.4601 0.02359 0.01730 -0.0723 0.1834 1.0000
11.000 1.4771 0.02428 0.01798 -0.0711 0.1802 1.0000
11.250 1.4941 0.02498 0.01868 -0.0699 0.1770 1.0000
11.500 1.5117 0.02566 0.01938 -0.0688 0.1743 1.0000
11.750 1.5284 0.02639 0.02013 -0.0677 0.1711 1.0000
12.000 1.5441 0.02720 0.02093 -0.0664 0.1677 1.0000
12.250 1.5585 0.02811 0.02184 -0.0650 0.1645 1.0000
12.500 1.5752 0.02888 0.02264 -0.0640 0.1619 1.0000
12.750 1.5909 0.02975 0.02351 -0.0629 0.1589 1.0000
13.000 1.6045 0.03077 0.02454 -0.0616 0.1556 1.0000
13.250 1.6180 0.03180 0.02558 -0.0603 0.1525 1.0000
13.500 1.6329 0.03278 0.02658 -0.0593 0.1501 1.0000
13.750 1.6471 0.03380 0.02763 -0.0582 0.1474 1.0000
14.000 1.6595 0.03499 0.02883 -0.0570 0.1442 1.0000
14.250 1.6707 0.03628 0.03012 -0.0557 0.1412 1.0000
14.500 1.6843 0.03739 0.03127 -0.0548 0.1389 1.0000
14.750 1.6963 0.03866 0.03257 -0.0537 0.1363 1.0000
15.000 1.7073 0.04003 0.03395 -0.0526 0.1334 1.0000
15.250 1.7160 0.04161 0.03555 -0.0514 0.1305 1.0000
15.500 1.7281 0.04293 0.03690 -0.0506 0.1282 1.0000
15.750 1.7378 0.04448 0.03848 -0.0496 0.1257 1.0000
16.000 1.7467 0.04610 0.04012 -0.0486 0.1229 1.0000
16.250 1.7532 0.04796 0.04201 -0.0475 0.1202 1.0000
16.500 1.7632 0.04951 0.04360 -0.0467 0.1181 1.0000
16.750 1.7703 0.05137 0.04550 -0.0458 0.1156 1.0000
17.000 1.7767 0.05329 0.04744 -0.0449 0.1131 1.0000
17.250 1.7807 0.05549 0.04968 -0.0440 0.1107 1.0000
17.500 1.7884 0.05734 0.05157 -0.0434 0.1087 1.0000
17.750 1.7931 0.05953 0.05381 -0.0427 0.1065 1.0000
18.000 1.7962 0.06187 0.05618 -0.0419 0.1040 1.0000
18.250 1.7976 0.06441 0.05876 -0.0412 0.1019 1.0000
18.500 1.8022 0.06666 0.06107 -0.0407 0.1002 1.0000
18.750 1.8046 0.06916 0.06362 -0.0402 0.0982 1.0000
19.000 1.8045 0.07196 0.06647 -0.0397 0.0961 1.0000
19.250 1.8029 0.07496 0.06951 -0.0393 0.0940 1.0000
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