HAM-STD HS1-620 AIRFOIL (hs1620-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: HAM-STD HS1-620 AIRFOIL (hs1620-il) Reynolds number: 1,000,000 Max Cl/Cd: 76.25 at α=2.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-hs1620-il-1000000.txt Download as CSV file: xf-hs1620-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -1.0184 0.08674 0.08307 -0.0971 0.9946 0.0368
-19.000 -1.0706 0.07602 0.07219 -0.1030 0.9942 0.0369
-18.750 -1.1363 0.06264 0.05857 -0.1107 0.9936 0.0369
-18.500 -1.1827 0.05117 0.04683 -0.1187 0.9931 0.0370
-18.250 -1.2029 0.04431 0.03979 -0.1239 0.9925 0.0373
-18.000 -1.2225 0.04011 0.03548 -0.1239 0.9896 0.0375
-17.750 -1.2294 0.03696 0.03222 -0.1243 0.9877 0.0378
-17.500 -1.2302 0.03452 0.02970 -0.1243 0.9862 0.0382
-17.250 -1.2263 0.03263 0.02772 -0.1240 0.9849 0.0386
-17.000 -1.2191 0.03108 0.02610 -0.1235 0.9839 0.0390
-16.750 -1.2096 0.02978 0.02472 -0.1228 0.9831 0.0395
-16.500 -1.1971 0.02869 0.02355 -0.1221 0.9823 0.0399
-16.250 -1.1816 0.02778 0.02256 -0.1216 0.9817 0.0403
-16.000 -1.1731 0.02670 0.02142 -0.1200 0.9810 0.0409
-15.750 -1.2036 0.02611 0.02076 -0.1097 0.9747 0.0410
-15.500 -1.1900 0.02523 0.01985 -0.1081 0.9732 0.0417
-15.250 -1.1695 0.02450 0.01910 -0.1076 0.9722 0.0425
-15.000 -1.1473 0.02390 0.01846 -0.1073 0.9714 0.0432
-14.750 -1.1234 0.02337 0.01789 -0.1072 0.9708 0.0439
-14.500 -1.0985 0.02290 0.01736 -0.1072 0.9702 0.0446
-14.250 -1.0730 0.02228 0.01669 -0.1075 0.9697 0.0453
-14.000 -1.0441 0.02154 0.01595 -0.1085 0.9692 0.0464
-13.750 -1.0312 0.02107 0.01545 -0.1058 0.9646 0.0471
-13.500 -1.0038 0.02053 0.01489 -0.1061 0.9624 0.0480
-13.250 -0.9731 0.02007 0.01438 -0.1070 0.9612 0.0490
-13.000 -0.9432 0.01958 0.01386 -0.1078 0.9603 0.0500
-12.750 -0.9149 0.01900 0.01328 -0.1084 0.9595 0.0513
-12.500 -0.8846 0.01855 0.01283 -0.1093 0.9588 0.0525
-12.250 -0.8533 0.01817 0.01242 -0.1103 0.9583 0.0537
-12.000 -0.8217 0.01784 0.01204 -0.1113 0.9579 0.0547
-11.750 -0.7909 0.01730 0.01152 -0.1123 0.9575 0.0564
-11.500 -0.7577 0.01690 0.01112 -0.1138 0.9572 0.0580
-11.250 -0.7229 0.01656 0.01076 -0.1154 0.9570 0.0595
-11.000 -0.6893 0.01612 0.01031 -0.1169 0.9567 0.0613
-10.750 -0.6564 0.01572 0.00993 -0.1182 0.9564 0.0631
-10.500 -0.6232 0.01541 0.00960 -0.1195 0.9560 0.0649
-10.250 -0.5904 0.01505 0.00923 -0.1208 0.9556 0.0669
-10.000 -0.5836 0.01498 0.00917 -0.1162 0.9491 0.0684
-9.750 -0.5512 0.01466 0.00885 -0.1173 0.9480 0.0706
-9.500 -0.5182 0.01432 0.00850 -0.1185 0.9471 0.0728
-9.250 -0.4853 0.01395 0.00816 -0.1197 0.9462 0.0754
-9.000 -0.4518 0.01366 0.00786 -0.1210 0.9454 0.0780
-8.750 -0.4188 0.01330 0.00752 -0.1222 0.9446 0.0811
-8.500 -0.3848 0.01299 0.00722 -0.1236 0.9438 0.0842
-8.250 -0.3505 0.01266 0.00690 -0.1250 0.9429 0.0874
-8.000 -0.3163 0.01235 0.00660 -0.1264 0.9419 0.0910
-7.750 -0.2912 0.01218 0.00644 -0.1258 0.9385 0.0942
-7.500 -0.2653 0.01194 0.00623 -0.1253 0.9350 0.0980
-7.250 -0.2337 0.01170 0.00599 -0.1261 0.9327 0.1016
-7.000 -0.2009 0.01138 0.00571 -0.1272 0.9307 0.1065
-6.750 -0.1671 0.01112 0.00546 -0.1285 0.9287 0.1110
-6.500 -0.1335 0.01085 0.00522 -0.1297 0.9266 0.1165
-6.250 -0.1091 0.01072 0.00509 -0.1289 0.9215 0.1207
-6.000 -0.0795 0.01048 0.00489 -0.1292 0.9173 0.1264
-5.750 -0.0471 0.01026 0.00466 -0.1301 0.9135 0.1314
-5.500 -0.0174 0.01004 0.00449 -0.1304 0.9080 0.1374
-5.250 0.0103 0.00988 0.00432 -0.1302 0.8998 0.1419
-5.000 0.0404 0.00967 0.00413 -0.1307 0.8917 0.1480
-4.750 0.0703 0.00953 0.00397 -0.1310 0.8806 0.1530
-4.500 0.0989 0.00939 0.00381 -0.1310 0.8663 0.1585
-4.250 0.1287 0.00929 0.00368 -0.1313 0.8491 0.1639
-3.750 0.1845 0.00928 0.00349 -0.1311 0.8058 0.1739
-3.500 0.2109 0.00934 0.00346 -0.1307 0.7859 0.1788
-3.250 0.2371 0.00943 0.00345 -0.1302 0.7681 0.1824
-2.750 0.2899 0.00948 0.00343 -0.1295 0.7394 0.1935
-2.500 0.3166 0.00954 0.00344 -0.1291 0.7280 0.1972
-2.250 0.3435 0.00955 0.00342 -0.1289 0.7172 0.2025
-2.000 0.3703 0.00956 0.00342 -0.1286 0.7078 0.2079
-1.750 0.3977 0.00958 0.00343 -0.1285 0.6988 0.2126
-1.500 0.4239 0.00967 0.00345 -0.1280 0.6894 0.2157
-1.250 0.4511 0.00962 0.00343 -0.1279 0.6806 0.2231
-1.000 0.4764 0.00968 0.00346 -0.1273 0.6708 0.2284
-0.750 0.5036 0.00970 0.00347 -0.1271 0.6626 0.2331
-0.500 0.5294 0.00974 0.00349 -0.1266 0.6534 0.2386
-0.250 0.5549 0.00976 0.00351 -0.1261 0.6446 0.2465
0.000 0.5802 0.00980 0.00355 -0.1255 0.6342 0.2529
0.250 0.6042 0.00986 0.00359 -0.1246 0.6240 0.2603
0.500 0.6283 0.00989 0.00363 -0.1238 0.6129 0.2708
0.750 0.6490 0.00995 0.00369 -0.1221 0.6016 0.2832
1.000 0.6677 0.01003 0.00377 -0.1201 0.5876 0.3027
1.250 0.6885 0.00999 0.00388 -0.1187 0.5723 0.3617
1.500 0.7085 0.00979 0.00406 -0.1172 0.5555 0.5043
1.750 0.7283 0.00966 0.00432 -0.1157 0.5348 0.6628
2.000 0.7472 0.00985 0.00457 -0.1139 0.5092 0.7262
2.250 0.7656 0.01006 0.00486 -0.1119 0.4810 0.7876
2.500 0.7816 0.01025 0.00521 -0.1092 0.4530 0.8762
2.750 0.7944 0.01062 0.00557 -0.1057 0.4259 0.9354
3.000 0.8128 0.01104 0.00588 -0.1036 0.3989 0.9703
3.250 0.8394 0.01151 0.00621 -0.1035 0.3727 0.9908
3.500 0.8746 0.01201 0.00656 -0.1055 0.3504 0.9987
3.750 0.8955 0.01229 0.00676 -0.1042 0.3370 1.0000
4.000 0.9125 0.01257 0.00696 -0.1021 0.3259 1.0000
4.250 0.9327 0.01280 0.00715 -0.1007 0.3181 1.0000
4.500 0.9520 0.01312 0.00740 -0.0991 0.3093 1.0000
4.750 0.9743 0.01335 0.00760 -0.0981 0.3036 1.0000
5.000 0.9963 0.01362 0.00783 -0.0970 0.2978 1.0000
5.250 1.0165 0.01396 0.00813 -0.0957 0.2911 1.0000
5.500 1.0388 0.01423 0.00838 -0.0948 0.2865 1.0000
5.750 1.0616 0.01450 0.00863 -0.0940 0.2825 1.0000
6.000 1.0833 0.01481 0.00892 -0.0930 0.2778 1.0000
6.250 1.1037 0.01520 0.00926 -0.0917 0.2721 1.0000
6.500 1.1261 0.01550 0.00955 -0.0909 0.2687 1.0000
6.750 1.1487 0.01579 0.00984 -0.0901 0.2655 1.0000
7.000 1.1703 0.01613 0.01017 -0.0892 0.2616 1.0000
7.250 1.1908 0.01653 0.01053 -0.0881 0.2571 1.0000
7.500 1.2104 0.01696 0.01095 -0.0868 0.2527 1.0000
7.750 1.2332 0.01726 0.01127 -0.0861 0.2504 1.0000
8.000 1.2548 0.01762 0.01162 -0.0853 0.2471 1.0000
8.250 1.2754 0.01803 0.01202 -0.0843 0.2435 1.0000
8.500 1.2947 0.01851 0.01247 -0.0830 0.2391 1.0000
8.750 1.3139 0.01900 0.01296 -0.0819 0.2356 1.0000
9.000 1.3357 0.01937 0.01335 -0.0811 0.2329 1.0000
9.250 1.3563 0.01980 0.01379 -0.0802 0.2297 1.0000
9.500 1.3757 0.02031 0.01427 -0.0791 0.2261 1.0000
9.750 1.3929 0.02092 0.01487 -0.0777 0.2221 1.0000
10.000 1.4117 0.02146 0.01542 -0.0766 0.2193 1.0000
10.250 1.4324 0.02191 0.01589 -0.0758 0.2167 1.0000
10.500 1.4518 0.02244 0.01643 -0.0748 0.2135 1.0000
10.750 1.4692 0.02308 0.01707 -0.0736 0.2101 1.0000
11.000 1.4842 0.02387 0.01784 -0.0720 0.2062 1.0000
11.250 1.5035 0.02443 0.01843 -0.0711 0.2038 1.0000
11.500 1.5226 0.02501 0.01903 -0.0702 0.2009 1.0000
11.750 1.5393 0.02574 0.01976 -0.0690 0.1976 1.0000
12.000 1.5546 0.02657 0.02058 -0.0677 0.1940 1.0000
12.250 1.5692 0.02745 0.02146 -0.0663 0.1906 1.0000
12.500 1.5872 0.02813 0.02218 -0.0654 0.1881 1.0000
12.750 1.6039 0.02891 0.02298 -0.0644 0.1851 1.0000
13.000 1.6181 0.02987 0.02394 -0.0631 0.1818 1.0000
13.250 1.6297 0.03102 0.02508 -0.0616 0.1780 1.0000
13.500 1.6466 0.03183 0.02593 -0.0607 0.1757 1.0000
13.750 1.6617 0.03279 0.02692 -0.0597 0.1731 1.0000
14.000 1.6753 0.03386 0.02800 -0.0586 0.1699 1.0000
14.250 1.6859 0.03518 0.02932 -0.0572 0.1665 1.0000
14.500 1.6988 0.03633 0.03050 -0.0562 0.1638 1.0000
14.750 1.7131 0.03740 0.03161 -0.0553 0.1614 1.0000
15.000 1.7252 0.03866 0.03289 -0.0542 0.1584 1.0000
15.250 1.7349 0.04012 0.03436 -0.0530 0.1552 1.0000
15.500 1.7437 0.04169 0.03595 -0.0518 0.1522 1.0000
15.750 1.7572 0.04289 0.03720 -0.0511 0.1499 1.0000
16.000 1.7674 0.04438 0.03872 -0.0501 0.1471 1.0000
16.250 1.7755 0.04606 0.04041 -0.0491 0.1440 1.0000
16.500 1.7809 0.04801 0.04239 -0.0479 0.1410 1.0000
16.750 1.7927 0.04940 0.04382 -0.0473 0.1388 1.0000
17.000 1.8004 0.05118 0.04564 -0.0464 0.1362 1.0000
17.250 1.8062 0.05313 0.04762 -0.0455 0.1334 1.0000
17.500 1.8081 0.05553 0.05003 -0.0444 0.1304 1.0000
17.750 1.8179 0.05715 0.05172 -0.0439 0.1285 1.0000
18.000 1.8233 0.05925 0.05387 -0.0432 0.1260 1.0000
18.250 1.8268 0.06153 0.05617 -0.0425 0.1235 1.0000
18.500 1.8250 0.06438 0.05905 -0.0416 0.1207 1.0000
18.750 1.8312 0.06643 0.06117 -0.0411 0.1189 1.0000
19.000 1.8347 0.06879 0.06359 -0.0407 0.1167 1.0000
19.250 1.8351 0.07151 0.06634 -0.0402 0.1144 1.0000
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