HAM-STD HS1-620 AIRFOIL (hs1620-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: HAM-STD HS1-620 AIRFOIL (hs1620-il) Reynolds number: 500,000 Max Cl/Cd: 72.24 at α=2.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-hs1620-il-500000.txt Download as CSV file: xf-hs1620-il-500000.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 = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.500 -0.8851 0.12299 0.11934 -0.0659 1.0000 0.0433
-19.250 -0.9376 0.11114 0.10725 -0.0720 1.0000 0.0438
-19.000 -0.9778 0.10182 0.09774 -0.0765 1.0000 0.0441
-18.750 -1.0128 0.09369 0.08943 -0.0802 1.0000 0.0444
-18.500 -1.0449 0.08618 0.08176 -0.0835 1.0000 0.0447
-18.250 -1.0745 0.07923 0.07464 -0.0865 1.0000 0.0449
-18.000 -1.0918 0.07463 0.06999 -0.0875 1.0000 0.0452
-17.750 -1.1088 0.06998 0.06529 -0.0886 1.0000 0.0456
-17.500 -1.1282 0.06492 0.06015 -0.0901 1.0000 0.0458
-17.250 -1.1475 0.06000 0.05513 -0.0914 1.0000 0.0461
-17.000 -1.1657 0.05550 0.05053 -0.0923 1.0000 0.0464
-16.750 -1.1832 0.05153 0.04646 -0.0923 1.0000 0.0467
-16.500 -1.1996 0.04811 0.04293 -0.0916 1.0000 0.0470
-16.250 -1.2154 0.04516 0.03988 -0.0900 1.0000 0.0473
-16.000 -1.2146 0.04244 0.03704 -0.0908 0.9985 0.0479
-15.750 -1.2124 0.04017 0.03464 -0.0909 0.9965 0.0484
-15.500 -1.2098 0.03832 0.03265 -0.0901 0.9947 0.0490
-15.250 -1.2030 0.03686 0.03101 -0.0894 0.9930 0.0495
-15.000 -1.2074 0.03529 0.02937 -0.0860 0.9893 0.0500
-14.750 -1.2029 0.03402 0.02808 -0.0836 0.9861 0.0506
-14.500 -1.1848 0.03303 0.02705 -0.0833 0.9841 0.0513
-14.250 -1.1612 0.03216 0.02613 -0.0838 0.9825 0.0522
-14.000 -1.1336 0.03139 0.02528 -0.0849 0.9814 0.0532
-13.750 -1.1196 0.03057 0.02435 -0.0830 0.9770 0.0541
-13.500 -1.0989 0.02968 0.02338 -0.0826 0.9741 0.0550
-13.250 -1.0748 0.02878 0.02250 -0.0829 0.9721 0.0561
-13.000 -1.0456 0.02813 0.02182 -0.0839 0.9707 0.0572
-12.750 -1.0148 0.02752 0.02116 -0.0851 0.9697 0.0585
-12.500 -0.9821 0.02699 0.02051 -0.0867 0.9689 0.0597
-12.250 -0.9727 0.02623 0.01974 -0.0835 0.9632 0.0607
-12.000 -0.9462 0.02559 0.01911 -0.0838 0.9607 0.0620
-11.750 -0.9153 0.02508 0.01857 -0.0849 0.9591 0.0635
-11.500 -0.8827 0.02463 0.01803 -0.0862 0.9579 0.0652
-11.250 -0.8515 0.02396 0.01736 -0.0874 0.9569 0.0668
-11.000 -0.8177 0.02345 0.01686 -0.0890 0.9561 0.0686
-10.750 -0.7995 0.02309 0.01646 -0.0873 0.9511 0.0701
-10.500 -0.7714 0.02272 0.01601 -0.0875 0.9479 0.0718
-10.250 -0.7408 0.02207 0.01540 -0.0884 0.9460 0.0739
-10.000 -0.7069 0.02166 0.01498 -0.0899 0.9447 0.0762
-9.750 -0.6714 0.02131 0.01455 -0.0916 0.9438 0.0784
-9.500 -0.6371 0.02071 0.01401 -0.0933 0.9429 0.0810
-9.250 -0.6004 0.02032 0.01361 -0.0953 0.9422 0.0838
-9.000 -0.5832 0.02005 0.01330 -0.0931 0.9356 0.0860
-8.750 -0.5519 0.01956 0.01286 -0.0940 0.9330 0.0890
-8.500 -0.5167 0.01920 0.01246 -0.0956 0.9315 0.0922
-8.250 -0.4816 0.01871 0.01201 -0.0973 0.9303 0.0957
-8.000 -0.4448 0.01834 0.01163 -0.0992 0.9293 0.0996
-7.750 -0.4076 0.01788 0.01119 -0.1013 0.9285 0.1036
-7.500 -0.3689 0.01748 0.01081 -0.1036 0.9279 0.1081
-7.250 -0.3298 0.01703 0.01037 -0.1061 0.9274 0.1128
-7.000 -0.3154 0.01684 0.01021 -0.1031 0.9188 0.1164
-6.750 -0.2795 0.01646 0.00982 -0.1048 0.9170 0.1214
-6.500 -0.2419 0.01605 0.00946 -0.1069 0.9159 0.1269
-6.250 -0.2029 0.01562 0.00904 -0.1092 0.9150 0.1327
-6.000 -0.1624 0.01522 0.00867 -0.1119 0.9143 0.1389
-5.750 -0.1209 0.01479 0.00828 -0.1149 0.9137 0.1452
-5.500 -0.0796 0.01444 0.00794 -0.1177 0.9129 0.1517
-5.250 -0.0387 0.01402 0.00755 -0.1205 0.9119 0.1582
-5.000 -0.0233 0.01386 0.00742 -0.1176 0.9021 0.1628
-4.750 0.0150 0.01351 0.00705 -0.1197 0.8995 0.1688
-4.500 0.0566 0.01307 0.00667 -0.1226 0.8969 0.1755
-4.250 0.0781 0.01287 0.00645 -0.1210 0.8863 0.1803
-4.000 0.1174 0.01245 0.00605 -0.1233 0.8808 0.1867
-3.750 0.1428 0.01226 0.00587 -0.1226 0.8689 0.1920
-3.500 0.1833 0.01204 0.00558 -0.1252 0.8613 0.1976
-3.250 0.2143 0.01176 0.00532 -0.1258 0.8484 0.2039
-3.000 0.2479 0.01161 0.00514 -0.1270 0.8350 0.2097
-2.750 0.2825 0.01153 0.00497 -0.1283 0.8212 0.2148
-2.500 0.3145 0.01138 0.00477 -0.1292 0.8056 0.2213
-2.250 0.3452 0.01135 0.00467 -0.1297 0.7901 0.2273
-2.000 0.3734 0.01139 0.00463 -0.1297 0.7765 0.2327
-1.750 0.4015 0.01136 0.00457 -0.1297 0.7651 0.2387
-1.500 0.4296 0.01135 0.00452 -0.1298 0.7536 0.2456
-1.250 0.4563 0.01136 0.00452 -0.1295 0.7427 0.2518
-1.000 0.4843 0.01140 0.00448 -0.1295 0.7325 0.2585
-0.750 0.5102 0.01134 0.00448 -0.1291 0.7230 0.2674
-0.500 0.5373 0.01139 0.00447 -0.1289 0.7130 0.2756
-0.250 0.5629 0.01134 0.00447 -0.1284 0.7034 0.2870
0.000 0.5887 0.01135 0.00447 -0.1279 0.6932 0.3008
0.250 0.6138 0.01128 0.00450 -0.1274 0.6839 0.3266
0.500 0.6375 0.01105 0.00454 -0.1266 0.6741 0.4097
0.750 0.6575 0.01043 0.00467 -0.1253 0.6647 0.6350
1.000 0.6783 0.01026 0.00480 -0.1236 0.6538 0.7375
1.250 0.6981 0.01018 0.00497 -0.1215 0.6434 0.8169
1.500 0.7157 0.01024 0.00520 -0.1187 0.6319 0.8935
1.750 0.7375 0.01044 0.00543 -0.1169 0.6200 0.9386
2.000 0.7625 0.01073 0.00564 -0.1161 0.6058 0.9646
2.250 0.7941 0.01108 0.00592 -0.1168 0.5886 0.9822
2.500 0.8316 0.01154 0.00627 -0.1191 0.5683 0.9927
2.750 0.8712 0.01206 0.00666 -0.1218 0.5421 0.9989
3.000 0.8766 0.01231 0.00678 -0.1171 0.5172 1.0000
3.250 0.8782 0.01258 0.00690 -0.1115 0.4911 1.0000
3.500 0.8811 0.01295 0.00710 -0.1063 0.4641 1.0000
3.750 0.8901 0.01336 0.00736 -0.1025 0.4366 1.0000
4.000 0.9005 0.01385 0.00768 -0.0991 0.4102 1.0000
4.250 0.9130 0.01435 0.00803 -0.0961 0.3876 1.0000
4.500 0.9285 0.01482 0.00838 -0.0939 0.3694 1.0000
4.750 0.9456 0.01525 0.00872 -0.0919 0.3555 1.0000
5.000 0.9624 0.01573 0.00910 -0.0900 0.3443 1.0000
5.250 0.9820 0.01612 0.00945 -0.0885 0.3351 1.0000
5.500 0.9992 0.01662 0.00986 -0.0867 0.3264 1.0000
5.750 1.0204 0.01696 0.01019 -0.0857 0.3200 1.0000
6.000 1.0393 0.01741 0.01059 -0.0842 0.3135 1.0000
6.250 1.0569 0.01793 0.01106 -0.0826 0.3071 1.0000
6.500 1.0791 0.01826 0.01139 -0.0817 0.3024 1.0000
6.750 1.0989 0.01869 0.01181 -0.0805 0.2973 1.0000
7.000 1.1169 0.01922 0.01229 -0.0790 0.2923 1.0000
7.250 1.1356 0.01974 0.01278 -0.0777 0.2875 1.0000
7.500 1.1574 0.02010 0.01317 -0.0769 0.2836 1.0000
7.750 1.1772 0.02056 0.01363 -0.0758 0.2793 1.0000
8.000 1.1951 0.02113 0.01416 -0.0744 0.2752 1.0000
8.250 1.2113 0.02180 0.01478 -0.0728 0.2704 1.0000
8.500 1.2330 0.02218 0.01522 -0.0720 0.2673 1.0000
8.750 1.2530 0.02266 0.01571 -0.0711 0.2638 1.0000
9.000 1.2713 0.02323 0.01628 -0.0699 0.2600 1.0000
9.250 1.2879 0.02391 0.01693 -0.0684 0.2560 1.0000
9.500 1.3050 0.02459 0.01760 -0.0671 0.2521 1.0000
9.750 1.3248 0.02511 0.01816 -0.0662 0.2491 1.0000
10.000 1.3435 0.02570 0.01878 -0.0652 0.2455 1.0000
10.250 1.3607 0.02638 0.01946 -0.0640 0.2419 1.0000
10.500 1.3753 0.02723 0.02027 -0.0625 0.2381 1.0000
10.750 1.3921 0.02796 0.02103 -0.0614 0.2349 1.0000
11.000 1.4107 0.02859 0.02172 -0.0605 0.2319 1.0000
11.250 1.4281 0.02932 0.02247 -0.0595 0.2287 1.0000
11.500 1.4432 0.03019 0.02334 -0.0582 0.2253 1.0000
11.750 1.4564 0.03121 0.02433 -0.0568 0.2216 1.0000
12.000 1.4725 0.03206 0.02523 -0.0557 0.2187 1.0000
12.250 1.4894 0.03287 0.02610 -0.0549 0.2158 1.0000
12.500 1.5050 0.03377 0.02703 -0.0539 0.2125 1.0000
12.750 1.5180 0.03488 0.02813 -0.0527 0.2092 1.0000
13.000 1.5286 0.03614 0.02936 -0.0512 0.2055 1.0000
13.250 1.5447 0.03708 0.03038 -0.0504 0.2029 1.0000
13.500 1.5597 0.03810 0.03147 -0.0496 0.1998 1.0000
13.750 1.5727 0.03929 0.03268 -0.0486 0.1965 1.0000
14.000 1.5829 0.04071 0.03409 -0.0474 0.1933 1.0000
14.250 1.5938 0.04208 0.03548 -0.0463 0.1901 1.0000
14.500 1.6077 0.04327 0.03675 -0.0456 0.1873 1.0000
14.750 1.6200 0.04458 0.03811 -0.0448 0.1842 1.0000
15.000 1.6292 0.04617 0.03971 -0.0438 0.1812 1.0000
15.250 1.6360 0.04794 0.04146 -0.0426 0.1779 1.0000
15.500 1.6477 0.04937 0.04298 -0.0419 0.1754 1.0000
15.750 1.6589 0.05086 0.04454 -0.0412 0.1724 1.0000
16.000 1.6671 0.05264 0.04635 -0.0405 0.1694 1.0000
16.250 1.6727 0.05464 0.04836 -0.0395 0.1665 1.0000
16.500 1.6792 0.05659 0.05035 -0.0387 0.1638 1.0000
16.750 1.6888 0.05830 0.05215 -0.0382 0.1610 1.0000
17.000 1.6955 0.06029 0.05420 -0.0376 0.1581 1.0000
17.250 1.6994 0.06257 0.05649 -0.0370 0.1553 1.0000
17.500 1.7008 0.06507 0.05900 -0.0362 0.1524 1.0000
17.750 1.7086 0.06705 0.06109 -0.0359 0.1500 1.0000
18.000 1.7136 0.06934 0.06345 -0.0355 0.1472 1.0000
18.250 1.7158 0.07191 0.06606 -0.0351 0.1446 1.0000
18.500 1.7139 0.07491 0.06906 -0.0346 0.1419 1.0000
18.750 1.7180 0.07732 0.07156 -0.0344 0.1395 1.0000
19.000 1.7202 0.07998 0.07432 -0.0343 0.1370 1.0000
19.250 1.7207 0.08285 0.07724 -0.0342 0.1344 1.0000
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