HQ 3.0/13 AIRFOIL (hq3013-il) Xfoil prediction polar at RE=100,000 Ncrit=9
| Details | Polar file |
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Airfoil: HQ 3.0/13 AIRFOIL (hq3013-il) Reynolds number: 100,000 Max Cl/Cd: 55.91 at α=6.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-hq3013-il-100000.txt Download as CSV file: xf-hq3013-il-100000.csv |
XFOIL Version 6.96
Calculated polar for: HQ 3.0/13 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.250 -0.3556 0.09685 0.09220 -0.0430 1.0000 0.1255
-9.000 -0.3699 0.09461 0.09009 -0.0424 1.0000 0.1294
-8.750 -0.4090 0.09327 0.08893 -0.0417 1.0000 0.1318
-8.500 -0.4505 0.09223 0.08807 -0.0395 1.0000 0.1323
-8.250 -0.4882 0.09095 0.08693 -0.0370 1.0000 0.1324
-8.000 -0.4471 0.08733 0.08325 -0.0323 1.0000 0.1372
-7.750 -0.4637 0.08589 0.08189 -0.0292 1.0000 0.1392
-7.500 -0.4896 0.08440 0.08050 -0.0264 1.0000 0.1405
-7.250 -0.5150 0.08170 0.07788 -0.0263 1.0000 0.1425
-7.000 -0.5868 0.07694 0.07279 -0.0354 1.0000 0.1478
-6.500 -0.5561 0.04934 0.04385 -0.0476 0.9912 0.0724
-6.250 -0.5328 0.04344 0.03738 -0.0504 0.9863 0.0687
-6.000 -0.5018 0.03927 0.03256 -0.0532 0.9820 0.0703
-5.750 -0.4746 0.03614 0.02872 -0.0542 0.9766 0.0737
-5.500 -0.4426 0.03289 0.02486 -0.0558 0.9724 0.0772
-5.250 -0.4090 0.03154 0.02337 -0.0577 0.9679 0.0861
-5.000 -0.3811 0.02979 0.02136 -0.0583 0.9624 0.0939
-4.750 -0.3457 0.02875 0.01998 -0.0599 0.9577 0.1044
-4.500 -0.3137 0.02759 0.01881 -0.0612 0.9530 0.1137
-4.250 -0.2855 0.02657 0.01772 -0.0615 0.9471 0.1222
-4.000 -0.2489 0.02587 0.01690 -0.0632 0.9426 0.1335
-3.750 -0.2205 0.02514 0.01628 -0.0637 0.9371 0.1459
-3.500 -0.1919 0.02446 0.01569 -0.0640 0.9309 0.1623
-3.250 -0.1554 0.02368 0.01523 -0.0660 0.9266 0.1975
-3.000 -0.1364 0.02214 0.01468 -0.0655 0.9199 0.3343
-2.750 -0.1148 0.02210 0.01568 -0.0633 0.9138 0.6141
-2.500 -0.0914 0.02266 0.01620 -0.0616 0.9070 0.6678
-2.250 -0.0684 0.02309 0.01661 -0.0599 0.8999 0.7011
-2.000 -0.0379 0.02350 0.01697 -0.0594 0.8944 0.7317
-1.750 -0.0224 0.02379 0.01723 -0.0567 0.8857 0.7544
-1.500 0.0101 0.02402 0.01743 -0.0563 0.8809 0.7822
-1.250 0.0187 0.02426 0.01766 -0.0524 0.8713 0.8065
-1.000 0.0461 0.02428 0.01767 -0.0507 0.8661 0.8367
-0.750 0.0543 0.02438 0.01777 -0.0468 0.8564 0.8582
-0.500 0.0876 0.02427 0.01760 -0.0471 0.8513 0.8797
-0.250 0.1018 0.02436 0.01767 -0.0447 0.8418 0.8993
0.000 0.1437 0.02426 0.01751 -0.0470 0.8368 0.9153
0.250 0.1739 0.02444 0.01766 -0.0481 0.8279 0.9311
0.500 0.2271 0.02440 0.01755 -0.0529 0.8227 0.9448
0.750 0.2877 0.02429 0.01737 -0.0590 0.8187 0.9567
1.000 0.3376 0.02447 0.01753 -0.0640 0.8096 0.9727
1.250 0.4087 0.02390 0.01690 -0.0714 0.8062 0.9809
1.500 0.4630 0.02369 0.01667 -0.0767 0.7962 0.9983
1.750 0.5122 0.02287 0.01580 -0.0800 0.7909 1.0000
2.000 0.5141 0.02301 0.01590 -0.0766 0.7779 1.0000
2.250 0.5395 0.02303 0.01587 -0.0766 0.7677 1.0000
2.500 0.5835 0.02246 0.01527 -0.0789 0.7617 1.0000
2.750 0.6092 0.02252 0.01532 -0.0787 0.7505 1.0000
3.000 0.6561 0.02173 0.01449 -0.0810 0.7452 1.0000
3.250 0.6818 0.02170 0.01446 -0.0805 0.7328 1.0000
3.500 0.7125 0.02143 0.01419 -0.0805 0.7215 1.0000
3.750 0.7576 0.02050 0.01323 -0.0821 0.7143 1.0000
4.000 0.7851 0.02027 0.01300 -0.0816 0.7008 1.0000
4.250 0.8137 0.02001 0.01276 -0.0811 0.6874 1.0000
4.500 0.8432 0.01970 0.01246 -0.0807 0.6736 1.0000
4.750 0.8731 0.01939 0.01215 -0.0803 0.6591 1.0000
5.000 0.9028 0.01908 0.01184 -0.0799 0.6433 1.0000
5.250 0.9323 0.01879 0.01153 -0.0794 0.6263 1.0000
5.500 0.9583 0.01864 0.01137 -0.0785 0.6064 1.0000
5.750 0.9827 0.01857 0.01131 -0.0774 0.5842 1.0000
6.000 1.0075 0.01853 0.01121 -0.0763 0.5605 1.0000
6.250 1.0320 0.01857 0.01115 -0.0752 0.5349 1.0000
6.500 1.0527 0.01883 0.01134 -0.0736 0.5066 1.0000
6.750 1.0730 0.01921 0.01160 -0.0721 0.4777 1.0000
7.000 1.0926 0.01972 0.01198 -0.0705 0.4492 1.0000
7.250 1.1115 0.02035 0.01247 -0.0690 0.4220 1.0000
7.500 1.1307 0.02106 0.01301 -0.0676 0.3969 1.0000
7.750 1.1485 0.02181 0.01368 -0.0660 0.3731 1.0000
8.000 1.1664 0.02260 0.01437 -0.0645 0.3513 1.0000
8.250 1.1835 0.02342 0.01513 -0.0629 0.3308 1.0000
8.500 1.2014 0.02427 0.01587 -0.0615 0.3123 1.0000
8.750 1.2205 0.02520 0.01670 -0.0604 0.2949 1.0000
9.000 1.2365 0.02613 0.01763 -0.0588 0.2783 1.0000
9.250 1.2525 0.02708 0.01857 -0.0572 0.2627 1.0000
9.500 1.2678 0.02804 0.01952 -0.0556 0.2479 1.0000
9.750 1.2827 0.02902 0.02049 -0.0539 0.2340 1.0000
10.000 1.2968 0.03000 0.02146 -0.0522 0.2205 1.0000
10.250 1.3060 0.03093 0.02248 -0.0497 0.2082 1.0000
10.500 1.3141 0.03198 0.02362 -0.0472 0.1962 1.0000
10.750 1.3226 0.03313 0.02483 -0.0448 0.1845 1.0000
11.000 1.3327 0.03439 0.02609 -0.0428 0.1733 1.0000
11.250 1.3443 0.03569 0.02732 -0.0411 0.1622 1.0000
11.500 1.3486 0.03700 0.02876 -0.0385 0.1523 1.0000
11.750 1.3553 0.03861 0.03051 -0.0364 0.1429 1.0000
12.000 1.3684 0.04018 0.03201 -0.0351 0.1339 1.0000
12.250 1.3703 0.04180 0.03384 -0.0327 0.1265 1.0000
12.500 1.3827 0.04365 0.03571 -0.0316 0.1193 1.0000
12.750 1.3865 0.04552 0.03777 -0.0296 0.1133 1.0000
13.000 1.4016 0.04747 0.03969 -0.0289 0.1071 1.0000
13.250 1.3959 0.04969 0.04223 -0.0265 0.1027 1.0000
13.500 1.4071 0.05114 0.04355 -0.0256 0.0968 1.0000
13.750 1.4015 0.05385 0.04657 -0.0237 0.0930 1.0000
14.000 1.3934 0.05650 0.04950 -0.0221 0.0895 1.0000
14.250 1.4060 0.05791 0.05064 -0.0216 0.0831 1.0000
14.500 1.3885 0.06120 0.05433 -0.0202 0.0809 1.0000
14.750 1.3741 0.06461 0.05803 -0.0194 0.0779 1.0000
15.000 1.3716 0.06687 0.06029 -0.0191 0.0737 1.0000
15.250 1.3669 0.07016 0.06364 -0.0189 0.0700 1.0000
15.500 1.3491 0.07478 0.06860 -0.0193 0.0680 1.0000
15.750 1.3323 0.07956 0.07364 -0.0202 0.0658 1.0000
16.000 1.3433 0.08115 0.07495 -0.0201 0.0599 1.0000
16.250 1.3202 0.08718 0.08133 -0.0219 0.0589 1.0000
16.500 1.2965 0.09391 0.08839 -0.0244 0.0579 1.0000
16.750 1.2720 0.10132 0.09610 -0.0278 0.0571 1.0000
17.000 1.2460 0.10966 0.10470 -0.0320 0.0571 1.0000
17.250 1.2157 0.11944 0.11473 -0.0375 0.0579 1.0000
17.500 1.1838 0.13028 0.12576 -0.0440 0.0590 1.0000
17.750 1.1505 0.14233 0.13793 -0.0515 0.0600 1.0000
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