HQ 3.0/10 AIRFOIL (hq3010-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: HQ 3.0/10 AIRFOIL (hq3010-il) Reynolds number: 1,000,000 Max Cl/Cd: 99.83 at α=5.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-hq3010-il-1000000-n5.txt Download as CSV file: xf-hq3010-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: HQ 3.0/10 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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.500 -0.3796 0.10716 0.10548 -0.0330 1.0000 0.0043
-10.250 -0.3769 0.10346 0.10180 -0.0342 1.0000 0.0042
-10.000 -0.3733 0.10063 0.09898 -0.0352 1.0000 0.0044
-9.750 -0.3674 0.09849 0.09686 -0.0358 1.0000 0.0047
-9.500 -0.3647 0.09537 0.09376 -0.0368 1.0000 0.0050
-9.250 -0.3624 0.09181 0.09022 -0.0383 0.9998 0.0050
-9.000 -0.3559 0.08730 0.08572 -0.0416 0.9866 0.0050
-8.750 -0.3436 0.08250 0.08092 -0.0467 0.9781 0.0054
-8.500 -0.3278 0.07678 0.07519 -0.0540 0.9714 0.0055
-8.250 -0.3082 0.07034 0.06873 -0.0634 0.9622 0.0058
-7.250 -0.2777 0.04554 0.04344 -0.0913 0.8885 0.0067
-7.000 -0.2719 0.04069 0.03841 -0.0925 0.8791 0.0067
-6.750 -0.2812 0.03150 0.02875 -0.0940 0.8688 0.0072
-6.500 -0.2651 0.02876 0.02578 -0.0941 0.8623 0.0075
-6.250 -0.2459 0.02647 0.02329 -0.0942 0.8561 0.0077
-6.000 -0.2253 0.02423 0.02083 -0.0941 0.8498 0.0080
-5.750 -0.2069 0.01844 0.01442 -0.0929 0.8435 0.0058
-5.500 -0.1841 0.01467 0.00996 -0.0918 0.8372 0.0043
-5.250 -0.1574 0.01407 0.00922 -0.0916 0.8316 0.0041
-5.000 -0.1317 0.01294 0.00795 -0.0914 0.8253 0.0039
-4.750 -0.1060 0.01175 0.00657 -0.0910 0.8193 0.0038
-4.500 -0.0796 0.01089 0.00557 -0.0907 0.8126 0.0037
-4.250 -0.0532 0.01021 0.00477 -0.0905 0.8063 0.0036
-4.000 -0.0263 0.00964 0.00411 -0.0903 0.7993 0.0036
-3.750 0.0006 0.00916 0.00352 -0.0901 0.7924 0.0036
-3.500 0.0279 0.00875 0.00303 -0.0900 0.7847 0.0035
-3.250 0.0552 0.00843 0.00263 -0.0898 0.7766 0.0035
-3.000 0.0826 0.00817 0.00228 -0.0897 0.7664 0.0035
-2.750 0.1102 0.00795 0.00199 -0.0896 0.7564 0.0035
-2.500 0.1379 0.00779 0.00174 -0.0895 0.7479 0.0035
-2.250 0.1658 0.00766 0.00154 -0.0894 0.7402 0.0035
-2.000 0.1938 0.00754 0.00138 -0.0894 0.7331 0.0036
-1.750 0.2217 0.00747 0.00124 -0.0894 0.7248 0.0038
-1.500 0.2496 0.00740 0.00112 -0.0893 0.7144 0.0042
-1.250 0.2771 0.00728 0.00102 -0.0892 0.7017 0.0270
-1.000 0.3043 0.00709 0.00095 -0.0892 0.6890 0.0791
-0.750 0.3310 0.00660 0.00088 -0.0894 0.6784 0.2360
-0.500 0.3565 0.00581 0.00083 -0.0895 0.6690 0.5012
-0.250 0.3839 0.00570 0.00086 -0.0895 0.6589 0.5636
0.000 0.4111 0.00564 0.00091 -0.0894 0.6484 0.6177
0.250 0.4385 0.00566 0.00094 -0.0892 0.6351 0.6413
0.500 0.4656 0.00574 0.00096 -0.0891 0.6162 0.6560
0.750 0.4926 0.00584 0.00100 -0.0889 0.5948 0.6664
1.000 0.5196 0.00594 0.00104 -0.0887 0.5750 0.6744
1.250 0.5466 0.00606 0.00109 -0.0886 0.5540 0.6816
1.500 0.5731 0.00622 0.00116 -0.0883 0.5285 0.6894
1.750 0.5994 0.00640 0.00124 -0.0881 0.5016 0.6966
2.000 0.6254 0.00661 0.00135 -0.0878 0.4707 0.7045
2.250 0.6513 0.00683 0.00146 -0.0875 0.4410 0.7125
2.500 0.6772 0.00706 0.00159 -0.0872 0.4125 0.7211
2.750 0.7031 0.00726 0.00172 -0.0869 0.3885 0.7299
3.000 0.7288 0.00749 0.00186 -0.0866 0.3609 0.7388
3.250 0.7545 0.00772 0.00201 -0.0863 0.3347 0.7484
3.500 0.7801 0.00795 0.00218 -0.0860 0.3101 0.7585
3.750 0.8055 0.00819 0.00236 -0.0856 0.2867 0.7685
4.000 0.8312 0.00840 0.00253 -0.0853 0.2690 0.7797
4.250 0.8565 0.00862 0.00271 -0.0850 0.2504 0.7916
4.500 0.8815 0.00886 0.00291 -0.0846 0.2290 0.8048
4.750 0.9055 0.00915 0.00314 -0.0840 0.2026 0.8206
5.000 0.9282 0.00953 0.00340 -0.0832 0.1706 0.8410
5.250 0.9511 0.00971 0.00363 -0.0823 0.1542 0.8752
5.500 0.9793 0.00981 0.00385 -0.0826 0.1410 1.0000
5.750 1.0034 0.01018 0.00413 -0.0821 0.1205 1.0000
6.000 1.0267 0.01063 0.00444 -0.0815 0.0972 1.0000
6.250 1.0494 0.01111 0.00479 -0.0808 0.0754 1.0000
6.500 1.0731 0.01149 0.00512 -0.0802 0.0625 1.0000
6.750 1.0961 0.01193 0.00550 -0.0796 0.0482 1.0000
7.000 1.1190 0.01236 0.00587 -0.0789 0.0375 1.0000
7.250 1.1417 0.01280 0.00626 -0.0782 0.0284 1.0000
7.500 1.1640 0.01326 0.00668 -0.0774 0.0207 1.0000
7.750 1.1861 0.01373 0.00712 -0.0767 0.0156 1.0000
8.000 1.2084 0.01415 0.00753 -0.0759 0.0109 1.0000
8.250 1.2262 0.01500 0.00832 -0.0744 0.0021 1.0000
8.500 1.2477 0.01546 0.00884 -0.0735 0.0016 1.0000
8.750 1.2691 0.01591 0.00934 -0.0726 0.0014 1.0000
9.000 1.2898 0.01639 0.00987 -0.0716 0.0013 1.0000
9.250 1.3097 0.01691 0.01045 -0.0705 0.0012 1.0000
9.500 1.3286 0.01748 0.01108 -0.0692 0.0010 1.0000
9.750 1.3460 0.01813 0.01181 -0.0677 0.0009 1.0000
10.000 1.3610 0.01885 0.01262 -0.0658 0.0008 1.0000
10.250 1.3719 0.01973 0.01361 -0.0632 0.0007 1.0000
10.500 1.3821 0.02064 0.01462 -0.0606 0.0007 1.0000
10.750 1.3939 0.02142 0.01551 -0.0584 0.0006 1.0000
11.000 1.4044 0.02232 0.01649 -0.0561 0.0006 1.0000
11.250 1.4143 0.02327 0.01753 -0.0539 0.0006 1.0000
11.500 1.4229 0.02433 0.01870 -0.0516 0.0006 1.0000
11.750 1.4307 0.02548 0.01994 -0.0494 0.0006 1.0000
12.000 1.4370 0.02678 0.02134 -0.0472 0.0006 1.0000
12.250 1.4421 0.02821 0.02288 -0.0450 0.0006 1.0000
12.500 1.4464 0.02977 0.02455 -0.0430 0.0006 1.0000
12.750 1.4504 0.03140 0.02630 -0.0412 0.0006 1.0000
13.000 1.4509 0.03342 0.02845 -0.0393 0.0006 1.0000
13.250 1.4496 0.03571 0.03087 -0.0376 0.0005 1.0000
13.500 1.4491 0.03802 0.03331 -0.0363 0.0005 1.0000
13.750 1.4489 0.04043 0.03583 -0.0353 0.0006 1.0000
14.000 1.4432 0.04356 0.03911 -0.0344 0.0005 1.0000
14.250 1.4374 0.04692 0.04263 -0.0339 0.0005 1.0000
14.500 1.4325 0.05033 0.04617 -0.0339 0.0005 1.0000
14.750 1.4241 0.05442 0.05041 -0.0342 0.0005 1.0000
15.000 1.4159 0.05876 0.05489 -0.0351 0.0005 1.0000
15.250 1.4055 0.06373 0.06000 -0.0365 0.0005 1.0000
15.500 1.3978 0.06862 0.06502 -0.0382 0.0005 1.0000
15.750 1.3788 0.07574 0.07232 -0.0412 0.0005 1.0000
16.000 1.3666 0.08212 0.07884 -0.0442 0.0005 1.0000
16.250 1.3477 0.09016 0.08704 -0.0482 0.0005 1.0000
16.500 1.3320 0.09786 0.09489 -0.0523 0.0005 1.0000
16.750 1.3144 0.10628 0.10345 -0.0568 0.0005 1.0000
17.000 1.2925 0.11590 0.11322 -0.0621 0.0005 1.0000
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