HAM-STD HS1-620 AIRFOIL (hs1620-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: HAM-STD HS1-620 AIRFOIL (hs1620-il) Reynolds number: 500,000 Max Cl/Cd: 57.26 at α=5.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-hs1620-il-500000-n5.txt Download as CSV file: xf-hs1620-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.250 -0.8814 0.08850 0.08406 -0.1014 0.9911 0.0385
-18.000 -0.9192 0.08006 0.07549 -0.1054 0.9899 0.0388
-17.750 -0.9645 0.07037 0.06563 -0.1103 0.9886 0.0389
-17.500 -1.0097 0.05991 0.05494 -0.1163 0.9872 0.0391
-17.250 -1.0405 0.05119 0.04599 -0.1222 0.9857 0.0393
-17.000 -1.0555 0.04545 0.04007 -0.1260 0.9843 0.0396
-16.750 -1.0603 0.04144 0.03590 -0.1285 0.9831 0.0399
-16.500 -1.0589 0.03842 0.03274 -0.1301 0.9820 0.0403
-16.250 -1.0573 0.03583 0.03004 -0.1309 0.9812 0.0407
-16.000 -1.0671 0.03391 0.02804 -0.1282 0.9781 0.0410
-15.750 -1.0709 0.03235 0.02640 -0.1256 0.9753 0.0414
-15.500 -1.0684 0.03102 0.02500 -0.1236 0.9733 0.0419
-15.250 -1.0609 0.02985 0.02376 -0.1220 0.9716 0.0425
-15.000 -1.0517 0.02886 0.02269 -0.1202 0.9704 0.0431
-14.750 -1.0409 0.02800 0.02175 -0.1184 0.9694 0.0438
-14.500 -1.0233 0.02721 0.02088 -0.1176 0.9687 0.0446
-14.250 -1.0279 0.02674 0.02035 -0.1119 0.9639 0.0450
-14.000 -1.0148 0.02599 0.01957 -0.1100 0.9616 0.0457
-13.750 -0.9968 0.02533 0.01887 -0.1089 0.9601 0.0464
-13.500 -0.9756 0.02471 0.01821 -0.1084 0.9590 0.0473
-13.250 -0.9505 0.02410 0.01754 -0.1085 0.9580 0.0482
-13.000 -0.9208 0.02347 0.01685 -0.1095 0.9571 0.0493
-12.750 -0.8893 0.02275 0.01610 -0.1109 0.9564 0.0504
-12.500 -0.8561 0.02206 0.01539 -0.1127 0.9557 0.0517
-12.250 -0.8478 0.02171 0.01500 -0.1088 0.9493 0.0526
-12.000 -0.8224 0.02125 0.01450 -0.1087 0.9475 0.0538
-11.750 -0.7947 0.02077 0.01398 -0.1091 0.9462 0.0550
-11.500 -0.7660 0.02025 0.01345 -0.1097 0.9452 0.0563
-11.250 -0.7357 0.01978 0.01296 -0.1105 0.9443 0.0578
-11.000 -0.7045 0.01935 0.01249 -0.1115 0.9437 0.0595
-10.750 -0.6736 0.01889 0.01202 -0.1125 0.9431 0.0611
-10.500 -0.6416 0.01845 0.01157 -0.1137 0.9426 0.0629
-10.250 -0.6089 0.01804 0.01113 -0.1150 0.9420 0.0647
-10.000 -0.5999 0.01792 0.01099 -0.1110 0.9358 0.0660
-9.750 -0.5734 0.01755 0.01062 -0.1109 0.9334 0.0680
-9.500 -0.5428 0.01719 0.01026 -0.1116 0.9320 0.0703
-9.250 -0.5106 0.01684 0.00988 -0.1127 0.9309 0.0724
-9.000 -0.4779 0.01644 0.00950 -0.1139 0.9299 0.0749
-8.750 -0.4443 0.01609 0.00913 -0.1152 0.9288 0.0776
-8.500 -0.4101 0.01570 0.00875 -0.1168 0.9278 0.0805
-8.250 -0.3755 0.01535 0.00840 -0.1183 0.9268 0.0837
-8.000 -0.3646 0.01529 0.00833 -0.1146 0.9195 0.0857
-7.750 -0.3355 0.01497 0.00803 -0.1149 0.9168 0.0889
-7.500 -0.3025 0.01467 0.00773 -0.1161 0.9148 0.0926
-7.250 -0.2681 0.01432 0.00740 -0.1175 0.9130 0.0964
-7.000 -0.2325 0.01401 0.00708 -0.1193 0.9114 0.1006
-6.750 -0.2207 0.01391 0.00701 -0.1157 0.9023 0.1036
-6.500 -0.1891 0.01364 0.00675 -0.1165 0.8988 0.1082
-6.250 -0.1532 0.01334 0.00647 -0.1183 0.8963 0.1130
-6.000 -0.1358 0.01322 0.00637 -0.1159 0.8872 0.1172
-5.750 -0.1022 0.01295 0.00611 -0.1171 0.8821 0.1221
-5.500 -0.0704 0.01272 0.00589 -0.1179 0.8762 0.1276
-5.250 -0.0416 0.01252 0.00569 -0.1181 0.8673 0.1325
-5.000 -0.0053 0.01228 0.00546 -0.1199 0.8602 0.1385
-4.750 0.0286 0.01208 0.00523 -0.1212 0.8492 0.1438
-4.500 0.0652 0.01187 0.00499 -0.1231 0.8344 0.1500
-4.250 0.1010 0.01173 0.00475 -0.1247 0.8147 0.1554
-4.000 0.1325 0.01167 0.00459 -0.1254 0.7937 0.1613
-3.750 0.1611 0.01168 0.00450 -0.1255 0.7750 0.1663
-3.500 0.1886 0.01168 0.00444 -0.1254 0.7595 0.1714
-3.250 0.2157 0.01170 0.00441 -0.1251 0.7456 0.1767
-2.750 0.2689 0.01174 0.00435 -0.1245 0.7204 0.1861
-2.500 0.2949 0.01178 0.00434 -0.1240 0.7077 0.1913
-2.250 0.3202 0.01184 0.00433 -0.1234 0.6937 0.1960
-2.000 0.3464 0.01186 0.00432 -0.1230 0.6833 0.2007
-1.750 0.3724 0.01187 0.00432 -0.1226 0.6739 0.2060
-1.500 0.3985 0.01190 0.00433 -0.1222 0.6650 0.2111
-1.250 0.4242 0.01194 0.00433 -0.1217 0.6548 0.2154
-1.000 0.4493 0.01196 0.00434 -0.1211 0.6454 0.2211
-0.750 0.4748 0.01198 0.00437 -0.1206 0.6360 0.2271
-0.500 0.4991 0.01205 0.00439 -0.1197 0.6264 0.2325
-0.250 0.5237 0.01209 0.00442 -0.1190 0.6154 0.2377
0.000 0.5464 0.01215 0.00447 -0.1179 0.6037 0.2444
0.250 0.5680 0.01223 0.00452 -0.1165 0.5903 0.2510
0.750 0.6067 0.01242 0.00467 -0.1127 0.5626 0.2661
1.000 0.6244 0.01259 0.00479 -0.1105 0.5442 0.2759
1.250 0.6422 0.01279 0.00495 -0.1084 0.5224 0.2899
1.500 0.6605 0.01302 0.00515 -0.1065 0.4984 0.3125
1.750 0.6789 0.01321 0.00540 -0.1047 0.4736 0.3670
2.000 0.6967 0.01335 0.00570 -0.1029 0.4483 0.4577
2.250 0.7142 0.01334 0.00608 -0.1011 0.4228 0.6175
2.500 0.7323 0.01355 0.00643 -0.0992 0.3978 0.7025
2.750 0.7508 0.01375 0.00677 -0.0974 0.3776 0.7707
3.000 0.7651 0.01390 0.00720 -0.0942 0.3614 0.8772
3.250 0.7836 0.01426 0.00759 -0.0920 0.3467 0.9501
3.500 0.8146 0.01465 0.00791 -0.0929 0.3335 0.9875
3.750 0.8420 0.01499 0.00817 -0.0932 0.3237 1.0000
4.000 0.8621 0.01526 0.00839 -0.0918 0.3162 1.0000
4.250 0.8810 0.01560 0.00866 -0.0902 0.3090 1.0000
4.500 0.9019 0.01588 0.00892 -0.0890 0.3032 1.0000
4.750 0.9227 0.01620 0.00919 -0.0878 0.2970 1.0000
5.000 0.9427 0.01656 0.00950 -0.0865 0.2913 1.0000
5.250 0.9638 0.01689 0.00981 -0.0854 0.2868 1.0000
5.500 0.9854 0.01721 0.01011 -0.0844 0.2822 1.0000
5.750 1.0060 0.01758 0.01044 -0.0832 0.2772 1.0000
6.000 1.0258 0.01799 0.01082 -0.0820 0.2726 1.0000
6.250 1.0468 0.01836 0.01117 -0.0810 0.2688 1.0000
6.500 1.0683 0.01871 0.01152 -0.0800 0.2650 1.0000
6.750 1.0887 0.01912 0.01192 -0.0790 0.2608 1.0000
7.000 1.1085 0.01957 0.01235 -0.0778 0.2569 1.0000
7.250 1.1274 0.02007 0.01281 -0.0765 0.2530 1.0000
7.500 1.1488 0.02045 0.01321 -0.0757 0.2499 1.0000
7.750 1.1691 0.02089 0.01365 -0.0747 0.2464 1.0000
8.000 1.1887 0.02137 0.01413 -0.0736 0.2429 1.0000
8.250 1.2073 0.02191 0.01465 -0.0723 0.2391 1.0000
8.500 1.2255 0.02248 0.01521 -0.0711 0.2357 1.0000
8.750 1.2457 0.02296 0.01571 -0.0702 0.2328 1.0000
9.000 1.2651 0.02349 0.01625 -0.0692 0.2296 1.0000
9.250 1.2836 0.02407 0.01684 -0.0680 0.2261 1.0000
9.500 1.3004 0.02476 0.01751 -0.0667 0.2225 1.0000
9.750 1.3178 0.02543 0.01818 -0.0655 0.2194 1.0000
10.000 1.3371 0.02601 0.01879 -0.0646 0.2164 1.0000
10.250 1.3549 0.02667 0.01947 -0.0636 0.2129 1.0000
10.500 1.3711 0.02744 0.02024 -0.0623 0.2094 1.0000
10.750 1.3864 0.02828 0.02106 -0.0610 0.2061 1.0000
11.000 1.4037 0.02901 0.02183 -0.0600 0.2034 1.0000
11.250 1.4209 0.02977 0.02262 -0.0590 0.2005 1.0000
11.500 1.4371 0.03060 0.02347 -0.0579 0.1972 1.0000
11.750 1.4515 0.03157 0.02445 -0.0567 0.1940 1.0000
12.000 1.4650 0.03262 0.02549 -0.0554 0.1909 1.0000
12.250 1.4817 0.03346 0.02639 -0.0545 0.1883 1.0000
12.500 1.4968 0.03443 0.02739 -0.0535 0.1852 1.0000
12.750 1.5107 0.03550 0.02848 -0.0524 0.1819 1.0000
13.000 1.5222 0.03677 0.02975 -0.0512 0.1787 1.0000
13.250 1.5361 0.03788 0.03089 -0.0502 0.1759 1.0000
13.500 1.5500 0.03901 0.03207 -0.0493 0.1730 1.0000
13.750 1.5625 0.04027 0.03336 -0.0483 0.1698 1.0000
14.000 1.5730 0.04172 0.03482 -0.0472 0.1667 1.0000
14.250 1.5837 0.04316 0.03629 -0.0462 0.1639 1.0000
14.500 1.5964 0.04445 0.03763 -0.0454 0.1611 1.0000
14.750 1.6073 0.04592 0.03914 -0.0445 0.1582 1.0000
15.000 1.6163 0.04757 0.04081 -0.0436 0.1552 1.0000
15.250 1.6235 0.04940 0.04266 -0.0426 0.1525 1.0000
15.500 1.6349 0.05086 0.04419 -0.0419 0.1500 1.0000
15.750 1.6438 0.05258 0.04596 -0.0412 0.1472 1.0000
16.000 1.6512 0.05446 0.04788 -0.0404 0.1443 1.0000
16.250 1.6556 0.05667 0.05011 -0.0395 0.1417 1.0000
16.500 1.6642 0.05847 0.05197 -0.0389 0.1394 1.0000
16.750 1.6710 0.06048 0.05404 -0.0383 0.1367 1.0000
17.000 1.6761 0.06265 0.05626 -0.0377 0.1339 1.0000
17.250 1.6778 0.06524 0.05888 -0.0371 0.1314 1.0000
17.500 1.6825 0.06752 0.06122 -0.0366 0.1291 1.0000
17.750 1.6871 0.06984 0.06361 -0.0362 0.1267 1.0000
18.000 1.6895 0.07242 0.06625 -0.0358 0.1242 1.0000
18.250 1.6889 0.07538 0.06925 -0.0355 0.1217 1.0000
18.500 1.6886 0.07833 0.07226 -0.0352 0.1196 1.0000
18.750 1.6916 0.08090 0.07492 -0.0351 0.1175 1.0000
19.000 1.6905 0.08401 0.07808 -0.0350 0.1150 1.0000
19.250 1.6873 0.08739 0.08152 -0.0351 0.1128 1.0000
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