HQ 3.0/13 AIRFOIL (hq3013-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: HQ 3.0/13 AIRFOIL (hq3013-il) Reynolds number: 1,000,000 Max Cl/Cd: 97.93 at α=5.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-hq3013-il-1000000-n5.txt Download as CSV file: xf-hq3013-il-1000000-n5.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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-15.500 -0.6834 0.10018 0.09797 -0.0474 1.0000 0.0052
-15.250 -0.7287 0.08771 0.08541 -0.0541 1.0000 0.0051
-15.000 -0.8635 0.05768 0.05498 -0.0728 1.0000 0.0049
-14.750 -0.8859 0.04987 0.04701 -0.0784 1.0000 0.0049
-14.500 -0.9124 0.04277 0.03973 -0.0833 1.0000 0.0049
-14.250 -0.9230 0.03856 0.03539 -0.0856 1.0000 0.0049
-14.000 -0.9327 0.03493 0.03162 -0.0871 1.0000 0.0049
-13.750 -0.9287 0.03306 0.02968 -0.0873 1.0000 0.0050
-13.500 -0.9398 0.03025 0.02674 -0.0871 1.0000 0.0050
-13.000 -0.9223 0.02672 0.02300 -0.0889 0.9877 0.0050
-12.750 -0.8995 0.02511 0.02125 -0.0912 0.9822 0.0051
-12.500 -0.8788 0.02307 0.01902 -0.0935 0.9746 0.0053
-12.250 -0.8547 0.02153 0.01733 -0.0953 0.9673 0.0055
-12.000 -0.8295 0.02038 0.01607 -0.0965 0.9578 0.0056
-11.750 -0.8067 0.01946 0.01504 -0.0969 0.9451 0.0057
-11.500 -0.7852 0.01868 0.01414 -0.0967 0.9307 0.0058
-11.250 -0.7647 0.01799 0.01334 -0.0961 0.9170 0.0059
-11.000 -0.7445 0.01733 0.01256 -0.0953 0.9049 0.0061
-10.750 -0.7236 0.01674 0.01186 -0.0946 0.8940 0.0062
-10.250 -0.6803 0.01561 0.01050 -0.0933 0.8738 0.0065
-10.000 -0.6576 0.01511 0.00990 -0.0927 0.8657 0.0066
-9.750 -0.6344 0.01462 0.00932 -0.0922 0.8580 0.0068
-9.500 -0.6107 0.01418 0.00879 -0.0918 0.8511 0.0069
-9.250 -0.5863 0.01375 0.00829 -0.0914 0.8443 0.0071
-8.750 -0.5375 0.01287 0.00724 -0.0907 0.8320 0.0076
-8.500 -0.5127 0.01245 0.00675 -0.0903 0.8257 0.0078
-8.250 -0.4874 0.01207 0.00631 -0.0900 0.8202 0.0082
-8.000 -0.4616 0.01172 0.00592 -0.0898 0.8141 0.0084
-7.750 -0.4358 0.01141 0.00555 -0.0896 0.8084 0.0088
-7.500 -0.4094 0.01112 0.00520 -0.0894 0.8031 0.0091
-7.250 -0.3830 0.01084 0.00487 -0.0892 0.7974 0.0095
-7.000 -0.3565 0.01059 0.00456 -0.0890 0.7922 0.0100
-6.750 -0.3299 0.01029 0.00423 -0.0889 0.7869 0.0112
-6.500 -0.3032 0.01003 0.00394 -0.0888 0.7817 0.0129
-6.250 -0.2767 0.00976 0.00367 -0.0887 0.7768 0.0172
-6.000 -0.2496 0.00952 0.00346 -0.0886 0.7719 0.0233
-5.750 -0.2222 0.00935 0.00328 -0.0886 0.7670 0.0268
-5.500 -0.1947 0.00921 0.00310 -0.0885 0.7623 0.0288
-5.250 -0.1671 0.00903 0.00292 -0.0885 0.7576 0.0315
-5.000 -0.1394 0.00889 0.00276 -0.0885 0.7527 0.0336
-4.500 -0.0839 0.00860 0.00245 -0.0885 0.7431 0.0406
-4.250 -0.0560 0.00848 0.00232 -0.0886 0.7376 0.0439
-4.000 -0.0284 0.00836 0.00218 -0.0885 0.7320 0.0490
-3.750 -0.0004 0.00823 0.00206 -0.0886 0.7251 0.0545
-3.500 0.0271 0.00812 0.00193 -0.0885 0.7178 0.0625
-3.250 0.0552 0.00800 0.00182 -0.0886 0.7108 0.0708
-2.750 0.1107 0.00773 0.00161 -0.0886 0.6990 0.1014
-2.500 0.1385 0.00758 0.00152 -0.0887 0.6929 0.1245
-2.250 0.1660 0.00740 0.00143 -0.0887 0.6874 0.1601
-2.000 0.1937 0.00719 0.00135 -0.0887 0.6815 0.2035
-1.750 0.2209 0.00700 0.00127 -0.0887 0.6742 0.2529
-1.500 0.2483 0.00681 0.00120 -0.0888 0.6659 0.3004
-1.250 0.2741 0.00638 0.00111 -0.0887 0.6578 0.4258
-1.000 0.3015 0.00623 0.00111 -0.0887 0.6489 0.4873
-0.750 0.3292 0.00622 0.00111 -0.0886 0.6396 0.5080
-0.500 0.3570 0.00621 0.00112 -0.0886 0.6299 0.5306
-0.250 0.3849 0.00618 0.00115 -0.0886 0.6224 0.5582
0.000 0.4127 0.00621 0.00117 -0.0885 0.6136 0.5712
0.250 0.4408 0.00625 0.00118 -0.0885 0.6037 0.5785
0.500 0.4684 0.00630 0.00121 -0.0885 0.5918 0.5872
0.750 0.4954 0.00639 0.00125 -0.0883 0.5734 0.5979
1.000 0.5221 0.00650 0.00130 -0.0880 0.5548 0.6080
1.250 0.5490 0.00661 0.00136 -0.0879 0.5375 0.6148
1.500 0.5759 0.00673 0.00142 -0.0877 0.5192 0.6206
2.000 0.6287 0.00702 0.00158 -0.0872 0.4803 0.6311
2.250 0.6548 0.00720 0.00168 -0.0869 0.4587 0.6373
2.500 0.6806 0.00739 0.00179 -0.0865 0.4375 0.6433
2.750 0.7062 0.00759 0.00192 -0.0862 0.4155 0.6500
3.250 0.7569 0.00801 0.00220 -0.0854 0.3718 0.6629
3.500 0.7825 0.00821 0.00234 -0.0850 0.3523 0.6701
3.750 0.8071 0.00846 0.00251 -0.0845 0.3289 0.6777
4.000 0.8315 0.00872 0.00269 -0.0840 0.3056 0.6860
4.250 0.8563 0.00894 0.00286 -0.0835 0.2894 0.6941
4.750 0.9059 0.00937 0.00323 -0.0825 0.2605 0.7119
5.000 0.9307 0.00957 0.00342 -0.0820 0.2486 0.7217
5.250 0.9553 0.00978 0.00361 -0.0815 0.2373 0.7322
5.500 0.9793 0.01000 0.00383 -0.0809 0.2244 0.7427
5.750 1.0029 0.01025 0.00405 -0.0803 0.2102 0.7533
6.000 1.0260 0.01051 0.00428 -0.0795 0.1962 0.7655
6.250 1.0487 0.01079 0.00453 -0.0787 0.1829 0.7783
6.500 1.0705 0.01110 0.00481 -0.0778 0.1672 0.7916
6.750 1.0916 0.01142 0.00510 -0.0767 0.1518 0.8053
7.000 1.1127 0.01173 0.00539 -0.0756 0.1398 0.8204
7.250 1.1329 0.01203 0.00569 -0.0744 0.1275 0.8392
7.500 1.1524 0.01228 0.00598 -0.0729 0.1173 0.8655
7.750 1.1775 0.01254 0.00636 -0.0728 0.1028 1.0000
8.000 1.1957 0.01301 0.00674 -0.0714 0.0887 1.0000
8.250 1.2126 0.01345 0.00712 -0.0696 0.0773 1.0000
8.500 1.2268 0.01397 0.00756 -0.0674 0.0643 1.0000
8.750 1.2419 0.01445 0.00800 -0.0653 0.0551 1.0000
9.000 1.2570 0.01494 0.00846 -0.0634 0.0472 1.0000
9.250 1.2697 0.01558 0.00903 -0.0611 0.0371 1.0000
9.500 1.2843 0.01613 0.00955 -0.0592 0.0314 1.0000
9.750 1.2964 0.01683 0.01021 -0.0570 0.0233 1.0000
10.000 1.3100 0.01746 0.01082 -0.0551 0.0190 1.0000
10.250 1.3222 0.01820 0.01154 -0.0531 0.0139 1.0000
10.500 1.3287 0.01930 0.01260 -0.0505 0.0046 1.0000
10.750 1.3408 0.02010 0.01343 -0.0486 0.0038 1.0000
11.000 1.3543 0.02083 0.01419 -0.0471 0.0034 1.0000
11.250 1.3678 0.02158 0.01499 -0.0456 0.0032 1.0000
11.500 1.3810 0.02237 0.01582 -0.0441 0.0031 1.0000
11.750 1.3934 0.02323 0.01675 -0.0426 0.0030 1.0000
12.000 1.4056 0.02414 0.01770 -0.0412 0.0029 1.0000
12.250 1.4162 0.02517 0.01880 -0.0397 0.0027 1.0000
12.500 1.4263 0.02628 0.01997 -0.0383 0.0026 1.0000
12.750 1.4364 0.02742 0.02117 -0.0369 0.0026 1.0000
13.000 1.4448 0.02871 0.02253 -0.0356 0.0025 1.0000
13.250 1.4523 0.03012 0.02401 -0.0342 0.0024 1.0000
13.500 1.4596 0.03159 0.02555 -0.0330 0.0023 1.0000
13.750 1.4634 0.03340 0.02746 -0.0316 0.0022 1.0000
14.000 1.4713 0.03489 0.02902 -0.0307 0.0021 1.0000
14.250 1.4784 0.03650 0.03069 -0.0298 0.0021 1.0000
14.500 1.4836 0.03835 0.03261 -0.0290 0.0021 1.0000
14.750 1.4872 0.04040 0.03475 -0.0282 0.0020 1.0000
15.000 1.4904 0.04257 0.03701 -0.0275 0.0019 1.0000
15.250 1.4938 0.04480 0.03931 -0.0271 0.0019 1.0000
15.500 1.4960 0.04724 0.04183 -0.0267 0.0019 1.0000
15.750 1.4960 0.05000 0.04469 -0.0265 0.0019 1.0000
16.000 1.4953 0.05297 0.04776 -0.0265 0.0018 1.0000
16.250 1.4944 0.05607 0.05096 -0.0267 0.0018 1.0000
16.500 1.4921 0.05945 0.05444 -0.0271 0.0018 1.0000
16.750 1.4867 0.06338 0.05849 -0.0277 0.0018 1.0000
17.000 1.4833 0.06719 0.06240 -0.0286 0.0017 1.0000
17.250 1.4766 0.07161 0.06693 -0.0298 0.0017 1.0000
17.500 1.4680 0.07646 0.07190 -0.0313 0.0017 1.0000
17.750 1.4583 0.08169 0.07725 -0.0332 0.0017 1.0000
18.000 1.4501 0.08682 0.08250 -0.0352 0.0017 1.0000
18.250 1.4375 0.09285 0.08866 -0.0378 0.0016 1.0000
18.500 1.4249 0.09904 0.09498 -0.0405 0.0017 1.0000
18.750 1.4100 0.10583 0.10190 -0.0437 0.0016 1.0000
19.000 1.3924 0.11331 0.10952 -0.0475 0.0016 1.0000
19.250 1.3764 0.12060 0.11694 -0.0512 0.0016 1.0000
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