HQ 3.0/14 AIRFOIL (hq3014-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: HQ 3.0/14 AIRFOIL (hq3014-il) Reynolds number: 500,000 Max Cl/Cd: 99.75 at α=5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-hq3014-il-500000.txt Download as CSV file: xf-hq3014-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: HQ 3.0/14 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
------ -------- --------- --------- -------- -------- --------
-12.500 -0.3847 0.11383 0.11145 -0.0472 1.0000 0.0236
-12.250 -0.3790 0.11151 0.10915 -0.0477 1.0000 0.0242
-12.000 -0.8239 0.03358 0.02964 -0.0810 0.9990 0.0133
-11.750 -0.8052 0.03082 0.02662 -0.0851 0.9921 0.0137
-11.500 -0.7831 0.02851 0.02404 -0.0879 0.9859 0.0141
-11.250 -0.7548 0.02663 0.02193 -0.0908 0.9827 0.0144
-11.000 -0.7347 0.02427 0.01934 -0.0923 0.9760 0.0149
-10.750 -0.7053 0.02269 0.01764 -0.0946 0.9726 0.0154
-10.500 -0.6731 0.02157 0.01643 -0.0969 0.9698 0.0160
-10.250 -0.6484 0.02060 0.01536 -0.0974 0.9619 0.0165
-10.000 -0.6190 0.01955 0.01419 -0.0987 0.9569 0.0171
-9.750 -0.5955 0.01870 0.01322 -0.0986 0.9483 0.0177
-9.500 -0.5701 0.01781 0.01218 -0.0988 0.9415 0.0183
-9.250 -0.5512 0.01692 0.01125 -0.0979 0.9320 0.0193
-9.000 -0.5263 0.01640 0.01067 -0.0977 0.9253 0.0205
-8.750 -0.5037 0.01599 0.01018 -0.0969 0.9168 0.0220
-8.500 -0.4812 0.01531 0.00944 -0.0963 0.9102 0.0241
-8.250 -0.4574 0.01502 0.00912 -0.0957 0.9026 0.0270
-8.000 -0.4341 0.01448 0.00851 -0.0951 0.8962 0.0306
-7.750 -0.4086 0.01433 0.00832 -0.0948 0.8893 0.0342
-7.500 -0.3850 0.01387 0.00782 -0.0942 0.8829 0.0376
-7.250 -0.3589 0.01374 0.00765 -0.0940 0.8770 0.0406
-7.000 -0.3327 0.01360 0.00743 -0.0937 0.8706 0.0427
-6.750 -0.3090 0.01304 0.00681 -0.0932 0.8652 0.0456
-6.500 -0.2837 0.01278 0.00654 -0.0928 0.8589 0.0482
-6.250 -0.2574 0.01259 0.00630 -0.0926 0.8532 0.0509
-6.000 -0.2303 0.01248 0.00611 -0.0924 0.8481 0.0532
-5.750 -0.2065 0.01195 0.00560 -0.0920 0.8419 0.0580
-5.500 -0.1800 0.01175 0.00535 -0.0917 0.8366 0.0618
-5.250 -0.1532 0.01158 0.00511 -0.0916 0.8314 0.0646
-5.000 -0.1286 0.01107 0.00461 -0.0911 0.8255 0.0706
-4.750 -0.1018 0.01083 0.00432 -0.0909 0.8205 0.0762
-4.500 -0.0757 0.01051 0.00401 -0.0907 0.8152 0.0856
-4.250 -0.0494 0.01021 0.00374 -0.0905 0.8095 0.0993
-4.000 -0.0230 0.00987 0.00347 -0.0903 0.8045 0.1262
-3.750 0.0022 0.00939 0.00325 -0.0901 0.7990 0.1904
-3.500 0.0276 0.00892 0.00303 -0.0900 0.7932 0.2657
-3.250 0.0520 0.00828 0.00277 -0.0897 0.7881 0.3798
-3.000 0.0773 0.00792 0.00273 -0.0894 0.7820 0.4786
-2.750 0.1046 0.00782 0.00269 -0.0892 0.7764 0.5188
-2.500 0.1326 0.00779 0.00266 -0.0891 0.7716 0.5475
-2.250 0.1602 0.00777 0.00266 -0.0890 0.7658 0.5698
-2.000 0.1882 0.00776 0.00265 -0.0889 0.7605 0.5884
-1.750 0.2165 0.00779 0.00263 -0.0888 0.7558 0.6025
-1.500 0.2444 0.00779 0.00264 -0.0887 0.7499 0.6139
-1.250 0.2724 0.00781 0.00264 -0.0886 0.7445 0.6279
-1.000 0.3001 0.00786 0.00269 -0.0884 0.7387 0.6446
-0.750 0.3276 0.00786 0.00270 -0.0882 0.7315 0.6554
-0.250 0.3833 0.00787 0.00266 -0.0880 0.7172 0.6706
0.000 0.4115 0.00792 0.00263 -0.0879 0.7109 0.6787
0.250 0.4388 0.00790 0.00266 -0.0877 0.7034 0.6862
0.500 0.4668 0.00796 0.00266 -0.0877 0.6971 0.6953
0.750 0.4942 0.00796 0.00271 -0.0875 0.6902 0.7026
1.000 0.5220 0.00800 0.00271 -0.0874 0.6831 0.7099
1.250 0.5495 0.00800 0.00274 -0.0873 0.6757 0.7157
1.500 0.5769 0.00804 0.00275 -0.0871 0.6674 0.7221
1.750 0.6041 0.00806 0.00277 -0.0869 0.6577 0.7285
2.000 0.6310 0.00810 0.00279 -0.0866 0.6485 0.7346
2.250 0.6581 0.00814 0.00284 -0.0865 0.6387 0.7419
2.500 0.6847 0.00817 0.00289 -0.0862 0.6290 0.7483
2.750 0.7114 0.00824 0.00293 -0.0859 0.6189 0.7557
3.000 0.7378 0.00828 0.00300 -0.0856 0.6077 0.7624
3.250 0.7639 0.00835 0.00307 -0.0852 0.5954 0.7702
3.500 0.7896 0.00842 0.00314 -0.0847 0.5821 0.7777
3.750 0.8149 0.00852 0.00323 -0.0842 0.5674 0.7859
4.000 0.8395 0.00863 0.00333 -0.0836 0.5506 0.7938
4.250 0.8637 0.00877 0.00344 -0.0829 0.5328 0.8031
4.750 0.9098 0.00913 0.00373 -0.0811 0.4917 0.8221
5.000 0.9317 0.00934 0.00390 -0.0800 0.4699 0.8332
5.250 0.9527 0.00957 0.00410 -0.0787 0.4467 0.8458
5.500 0.9725 0.00982 0.00432 -0.0772 0.4233 0.8610
5.750 0.9916 0.01005 0.00454 -0.0756 0.4006 0.8824
6.000 1.0144 0.01028 0.00481 -0.0748 0.3753 0.9363
6.250 1.0433 0.01069 0.00511 -0.0755 0.3481 1.0000
6.500 1.0635 0.01111 0.00542 -0.0744 0.3265 1.0000
6.750 1.0832 0.01153 0.00574 -0.0732 0.3068 1.0000
7.000 1.1023 0.01195 0.00609 -0.0718 0.2898 1.0000
7.250 1.1212 0.01237 0.00644 -0.0705 0.2748 1.0000
7.500 1.1393 0.01276 0.00679 -0.0689 0.2615 1.0000
7.750 1.1556 0.01317 0.00714 -0.0670 0.2477 1.0000
8.000 1.1714 0.01360 0.00752 -0.0651 0.2339 1.0000
8.250 1.1870 0.01406 0.00793 -0.0632 0.2203 1.0000
8.500 1.2022 0.01454 0.00835 -0.0613 0.2078 1.0000
8.750 1.2178 0.01502 0.00880 -0.0595 0.1962 1.0000
9.000 1.2339 0.01550 0.00926 -0.0579 0.1860 1.0000
9.250 1.2487 0.01605 0.00980 -0.0561 0.1765 1.0000
9.750 1.2773 0.01725 0.01093 -0.0526 0.1551 1.0000
10.000 1.2914 0.01789 0.01154 -0.0509 0.1449 1.0000
10.250 1.3043 0.01861 0.01223 -0.0492 0.1354 1.0000
10.500 1.3186 0.01927 0.01291 -0.0477 0.1272 1.0000
10.750 1.3319 0.02002 0.01365 -0.0461 0.1191 1.0000
11.000 1.3435 0.02089 0.01449 -0.0445 0.1108 1.0000
11.250 1.3566 0.02170 0.01530 -0.0430 0.1026 1.0000
11.500 1.3677 0.02265 0.01625 -0.0415 0.0949 1.0000
11.750 1.3784 0.02366 0.01724 -0.0399 0.0870 1.0000
12.000 1.3894 0.02468 0.01829 -0.0385 0.0802 1.0000
12.250 1.3975 0.02593 0.01950 -0.0369 0.0725 1.0000
12.500 1.4075 0.02707 0.02066 -0.0356 0.0662 1.0000
12.750 1.4150 0.02844 0.02202 -0.0342 0.0594 1.0000
13.000 1.4231 0.02979 0.02338 -0.0329 0.0544 1.0000
13.250 1.4301 0.03126 0.02487 -0.0317 0.0494 1.0000
13.500 1.4378 0.03273 0.02636 -0.0306 0.0455 1.0000
13.750 1.4428 0.03445 0.02809 -0.0294 0.0414 1.0000
14.000 1.4507 0.03596 0.02969 -0.0285 0.0388 1.0000
14.250 1.4551 0.03784 0.03158 -0.0275 0.0351 1.0000
14.500 1.4603 0.03971 0.03351 -0.0267 0.0324 1.0000
14.750 1.4654 0.04164 0.03549 -0.0261 0.0298 1.0000
15.000 1.4668 0.04401 0.03789 -0.0254 0.0268 1.0000
15.250 1.4701 0.04625 0.04019 -0.0249 0.0230 1.0000
15.500 1.4682 0.04912 0.04308 -0.0245 0.0184 1.0000
15.750 1.4680 0.05191 0.04593 -0.0243 0.0165 1.0000
16.000 1.4618 0.05551 0.04956 -0.0243 0.0126 1.0000
16.250 1.4580 0.05896 0.05310 -0.0245 0.0106 1.0000
16.500 1.4513 0.06292 0.05715 -0.0250 0.0091 1.0000
16.750 1.4478 0.06660 0.06093 -0.0256 0.0086 1.0000
17.000 1.4412 0.07085 0.06527 -0.0265 0.0080 1.0000
17.250 1.4347 0.07520 0.06974 -0.0276 0.0077 1.0000
17.500 1.4273 0.07983 0.07449 -0.0290 0.0074 1.0000
17.750 1.4201 0.08458 0.07937 -0.0306 0.0073 1.0000
18.000 1.4087 0.09013 0.08507 -0.0327 0.0070 1.0000
18.250 1.3992 0.09549 0.09055 -0.0348 0.0069 1.0000
18.500 1.3884 0.10121 0.09641 -0.0372 0.0068 1.0000
18.750 1.3770 0.10716 0.10249 -0.0399 0.0067 1.0000
19.000 1.3651 0.11330 0.10876 -0.0428 0.0066 1.0000
19.250 1.3493 0.12029 0.11589 -0.0463 0.0065 1.0000
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