HQ 3.0/15 AIRFOIL (hq3015-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: HQ 3.0/15 AIRFOIL (hq3015-il) Reynolds number: 1,000,000 Max Cl/Cd: 111.8 at α=4.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-hq3015-il-1000000.txt Download as CSV file: xf-hq3015-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: HQ 3.0/15 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
------ -------- --------- --------- -------- -------- --------
-18.000 -0.7071 0.12412 0.12187 -0.0425 1.0000 0.0094
-17.750 -0.7481 0.11195 0.10956 -0.0489 1.0000 0.0093
-17.500 -0.7833 0.10144 0.09893 -0.0545 1.0000 0.0093
-17.250 -0.8219 0.09069 0.08804 -0.0605 1.0000 0.0091
-17.000 -0.8592 0.08033 0.07753 -0.0664 1.0000 0.0091
-16.750 -0.8923 0.07076 0.06779 -0.0721 1.0000 0.0090
-16.500 -0.9154 0.06296 0.05985 -0.0769 1.0000 0.0090
-16.250 -0.9360 0.05620 0.05294 -0.0811 1.0000 0.0090
-16.000 -0.9473 0.05135 0.04798 -0.0839 1.0000 0.0091
-15.750 -0.9613 0.04648 0.04298 -0.0864 1.0000 0.0090
-15.500 -0.9706 0.04252 0.03891 -0.0882 1.0000 0.0091
-15.250 -0.9761 0.03925 0.03553 -0.0894 1.0000 0.0091
-15.000 -0.9785 0.03649 0.03268 -0.0901 1.0000 0.0093
-14.750 -0.9820 0.03380 0.02989 -0.0905 1.0000 0.0093
-14.500 -0.9810 0.03173 0.02775 -0.0905 1.0000 0.0094
-14.250 -0.9813 0.02974 0.02567 -0.0900 1.0000 0.0095
-14.000 -0.9824 0.02795 0.02380 -0.0890 1.0000 0.0096
-13.750 -0.9843 0.02654 0.02232 -0.0872 1.0000 0.0097
-13.500 -0.9792 0.02509 0.02079 -0.0867 0.9989 0.0098
-13.250 -0.9541 0.02358 0.01918 -0.0895 0.9925 0.0100
-13.000 -0.9290 0.02235 0.01786 -0.0918 0.9858 0.0101
-12.750 -0.9043 0.02079 0.01618 -0.0943 0.9795 0.0104
-12.500 -0.8776 0.01939 0.01469 -0.0965 0.9726 0.0109
-12.250 -0.8482 0.01838 0.01360 -0.0985 0.9652 0.0112
-12.000 -0.8195 0.01757 0.01271 -0.1000 0.9553 0.0116
-11.750 -0.7972 0.01691 0.01196 -0.0998 0.9411 0.0119
-11.500 -0.7775 0.01635 0.01131 -0.0990 0.9273 0.0123
-11.250 -0.7580 0.01585 0.01070 -0.0980 0.9157 0.0127
-11.000 -0.7387 0.01534 0.01009 -0.0969 0.9056 0.0131
-10.750 -0.7205 0.01473 0.00939 -0.0957 0.8962 0.0139
-10.500 -0.6998 0.01425 0.00886 -0.0948 0.8884 0.0148
-10.250 -0.6780 0.01384 0.00838 -0.0940 0.8809 0.0159
-10.000 -0.6563 0.01337 0.00791 -0.0932 0.8741 0.0181
-9.750 -0.6331 0.01302 0.00754 -0.0926 0.8673 0.0208
-9.500 -0.6079 0.01284 0.00732 -0.0923 0.8614 0.0239
-9.250 -0.5837 0.01252 0.00702 -0.0918 0.8555 0.0267
-9.000 -0.5578 0.01238 0.00683 -0.0916 0.8497 0.0286
-8.750 -0.5327 0.01213 0.00653 -0.0912 0.8441 0.0303
-8.500 -0.5078 0.01183 0.00623 -0.0909 0.8385 0.0322
-8.250 -0.4819 0.01164 0.00601 -0.0906 0.8330 0.0337
-8.000 -0.4554 0.01149 0.00581 -0.0904 0.8279 0.0350
-7.750 -0.4296 0.01124 0.00552 -0.0902 0.8223 0.0361
-7.500 -0.4045 0.01093 0.00517 -0.0898 0.8170 0.0381
-7.250 -0.3782 0.01071 0.00495 -0.0896 0.8119 0.0397
-7.000 -0.3515 0.01052 0.00473 -0.0895 0.8064 0.0411
-6.750 -0.3246 0.01037 0.00453 -0.0893 0.8012 0.0424
-6.500 -0.2984 0.01012 0.00424 -0.0891 0.7962 0.0447
-6.250 -0.2718 0.00988 0.00402 -0.0889 0.7908 0.0478
-6.000 -0.2447 0.00974 0.00384 -0.0888 0.7856 0.0503
-5.750 -0.2174 0.00959 0.00365 -0.0887 0.7806 0.0522
-5.500 -0.1910 0.00930 0.00338 -0.0886 0.7753 0.0577
-5.250 -0.1637 0.00916 0.00321 -0.0885 0.7702 0.0617
-5.000 -0.1368 0.00894 0.00300 -0.0884 0.7653 0.0690
-4.750 -0.1092 0.00878 0.00284 -0.0883 0.7600 0.0754
-4.500 -0.0821 0.00859 0.00266 -0.0882 0.7548 0.0862
-4.250 -0.0549 0.00840 0.00251 -0.0881 0.7495 0.1010
-4.000 -0.0280 0.00814 0.00234 -0.0881 0.7438 0.1250
-3.750 -0.0014 0.00788 0.00218 -0.0880 0.7382 0.1619
-3.500 0.0254 0.00760 0.00205 -0.0879 0.7332 0.2061
-3.250 0.0524 0.00734 0.00193 -0.0879 0.7281 0.2489
-3.000 0.0793 0.00708 0.00180 -0.0879 0.7231 0.2955
-2.750 0.1046 0.00660 0.00164 -0.0877 0.7184 0.3960
-2.500 0.1317 0.00634 0.00159 -0.0876 0.7135 0.4640
-2.250 0.1594 0.00624 0.00156 -0.0876 0.7083 0.5005
-2.000 0.1875 0.00621 0.00154 -0.0876 0.7028 0.5252
-1.750 0.2160 0.00617 0.00153 -0.0877 0.6967 0.5424
-1.500 0.2440 0.00617 0.00151 -0.0876 0.6905 0.5554
-1.250 0.2725 0.00616 0.00151 -0.0877 0.6844 0.5656
-1.000 0.3009 0.00617 0.00150 -0.0877 0.6780 0.5772
-0.750 0.3290 0.00620 0.00152 -0.0877 0.6719 0.5922
-0.500 0.3574 0.00620 0.00154 -0.0877 0.6654 0.6044
-0.250 0.3855 0.00623 0.00155 -0.0877 0.6594 0.6123
0.000 0.4140 0.00625 0.00157 -0.0878 0.6540 0.6195
0.250 0.4425 0.00627 0.00158 -0.0879 0.6478 0.6257
0.500 0.4703 0.00632 0.00161 -0.0878 0.6413 0.6322
0.750 0.4990 0.00634 0.00163 -0.0880 0.6348 0.6389
1.000 0.5265 0.00638 0.00166 -0.0878 0.6269 0.6461
1.250 0.5546 0.00642 0.00170 -0.0878 0.6176 0.6538
1.500 0.5819 0.00647 0.00173 -0.0877 0.6081 0.6602
1.750 0.6097 0.00651 0.00177 -0.0877 0.5990 0.6661
2.000 0.6374 0.00658 0.00181 -0.0876 0.5896 0.6717
2.250 0.6641 0.00665 0.00187 -0.0874 0.5787 0.6772
2.500 0.6915 0.00672 0.00193 -0.0873 0.5675 0.6830
2.750 0.7185 0.00682 0.00199 -0.0871 0.5555 0.6884
3.000 0.7447 0.00691 0.00207 -0.0868 0.5413 0.6940
3.250 0.7707 0.00704 0.00216 -0.0865 0.5252 0.6999
3.500 0.7962 0.00720 0.00226 -0.0860 0.5075 0.7058
3.750 0.8211 0.00736 0.00238 -0.0855 0.4890 0.7119
4.000 0.8455 0.00757 0.00252 -0.0849 0.4694 0.7185
4.250 0.8698 0.00778 0.00267 -0.0843 0.4481 0.7246
4.500 0.8937 0.00800 0.00283 -0.0836 0.4287 0.7314
4.750 0.9172 0.00825 0.00301 -0.0829 0.4090 0.7382
5.000 0.9401 0.00849 0.00320 -0.0820 0.3878 0.7452
5.250 0.9627 0.00878 0.00340 -0.0811 0.3652 0.7526
5.500 0.9843 0.00906 0.00362 -0.0801 0.3437 0.7601
5.750 1.0062 0.00935 0.00385 -0.0791 0.3238 0.7683
6.000 1.0273 0.00963 0.00409 -0.0780 0.3058 0.7763
6.500 1.0696 0.01017 0.00456 -0.0757 0.2782 0.7943
6.750 1.0899 0.01045 0.00482 -0.0744 0.2656 0.8044
7.000 1.1101 0.01070 0.00506 -0.0731 0.2544 0.8157
7.250 1.1296 0.01091 0.00529 -0.0717 0.2438 0.8283
7.500 1.1461 0.01115 0.00554 -0.0696 0.2325 0.8441
7.750 1.1604 0.01138 0.00582 -0.0672 0.2216 0.8684
8.000 1.1878 0.01160 0.00617 -0.0676 0.2060 1.0000
8.250 1.2033 0.01200 0.00650 -0.0656 0.1925 1.0000
8.500 1.2210 0.01234 0.00682 -0.0640 0.1838 1.0000
8.750 1.2371 0.01274 0.00719 -0.0622 0.1750 1.0000
9.000 1.2522 0.01320 0.00759 -0.0603 0.1649 1.0000
9.250 1.2685 0.01362 0.00799 -0.0587 0.1561 1.0000
9.500 1.2832 0.01413 0.00845 -0.0568 0.1480 1.0000
9.750 1.2994 0.01458 0.00889 -0.0553 0.1402 1.0000
10.000 1.3140 0.01512 0.00941 -0.0535 0.1325 1.0000
10.250 1.3289 0.01566 0.00992 -0.0519 0.1252 1.0000
10.500 1.3429 0.01627 0.01051 -0.0502 0.1174 1.0000
10.750 1.3556 0.01696 0.01117 -0.0484 0.1092 1.0000
11.000 1.3698 0.01760 0.01180 -0.0469 0.1025 1.0000
11.250 1.3812 0.01842 0.01257 -0.0451 0.0946 1.0000
11.500 1.3943 0.01916 0.01331 -0.0436 0.0877 1.0000
11.750 1.4052 0.02006 0.01417 -0.0419 0.0800 1.0000
12.000 1.4152 0.02104 0.01512 -0.0402 0.0724 1.0000
12.250 1.4269 0.02195 0.01603 -0.0388 0.0670 1.0000
12.500 1.4357 0.02307 0.01712 -0.0372 0.0605 1.0000
12.750 1.4464 0.02410 0.01815 -0.0358 0.0555 1.0000
13.000 1.4538 0.02538 0.01940 -0.0342 0.0492 1.0000
13.250 1.4622 0.02662 0.02065 -0.0328 0.0445 1.0000
13.500 1.4706 0.02790 0.02193 -0.0316 0.0409 1.0000
13.750 1.4781 0.02929 0.02333 -0.0303 0.0368 1.0000
14.000 1.4852 0.03074 0.02479 -0.0291 0.0335 1.0000
14.250 1.4926 0.03222 0.02629 -0.0280 0.0304 1.0000
14.500 1.4966 0.03401 0.02808 -0.0268 0.0262 1.0000
14.750 1.4973 0.03614 0.03020 -0.0256 0.0205 1.0000
15.000 1.5005 0.03815 0.03222 -0.0247 0.0176 1.0000
15.250 1.5041 0.04018 0.03428 -0.0239 0.0151 1.0000
15.500 1.4948 0.04353 0.03761 -0.0229 0.0079 1.0000
15.750 1.4959 0.04597 0.04011 -0.0224 0.0066 1.0000
16.000 1.4934 0.04889 0.04309 -0.0219 0.0053 1.0000
16.250 1.4958 0.05137 0.04564 -0.0217 0.0051 1.0000
16.500 1.4941 0.05437 0.04872 -0.0216 0.0047 1.0000
16.750 1.4932 0.05738 0.05181 -0.0217 0.0045 1.0000
17.000 1.4922 0.06051 0.05503 -0.0219 0.0044 1.0000
17.250 1.4888 0.06399 0.05861 -0.0223 0.0042 1.0000
17.500 1.4858 0.06754 0.06225 -0.0228 0.0041 1.0000
17.750 1.4814 0.07139 0.06620 -0.0236 0.0040 1.0000
18.000 1.4774 0.07528 0.07018 -0.0245 0.0040 1.0000
18.250 1.4702 0.07971 0.07473 -0.0258 0.0039 1.0000
18.500 1.4655 0.08390 0.07901 -0.0271 0.0039 1.0000
18.750 1.4581 0.08862 0.08385 -0.0287 0.0039 1.0000
19.000 1.4461 0.09416 0.08952 -0.0307 0.0038 1.0000
19.250 1.4382 0.09915 0.09461 -0.0327 0.0038 1.0000
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