ONERA HOR20 AIRFOIL (hor20-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: ONERA HOR20 AIRFOIL (hor20-il) Reynolds number: 1,000,000 Max Cl/Cd: 112.42 at α=9.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-hor20-il-1000000.txt Download as CSV file: xf-hor20-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: ONERA HOR20 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
------ -------- --------- --------- -------- -------- --------
-17.750 -1.1522 0.08405 0.08036 -0.0371 1.0000 0.0552
-17.500 -1.1680 0.07861 0.07487 -0.0399 1.0000 0.0560
-17.250 -1.1834 0.07325 0.06945 -0.0427 1.0000 0.0569
-17.000 -1.1982 0.06807 0.06418 -0.0454 1.0000 0.0578
-16.750 -1.2109 0.06322 0.05925 -0.0479 1.0000 0.0586
-16.500 -1.2255 0.05833 0.05426 -0.0504 1.0000 0.0593
-16.250 -1.2526 0.05221 0.04806 -0.0536 1.0000 0.0600
-16.000 -1.2783 0.04632 0.04208 -0.0567 1.0000 0.0606
-15.750 -1.3030 0.04054 0.03620 -0.0599 1.0000 0.0612
-15.500 -1.3224 0.03525 0.03081 -0.0630 1.0000 0.0618
-15.250 -1.3390 0.02981 0.02525 -0.0671 1.0000 0.0625
-15.000 -1.3394 0.02466 0.01993 -0.0737 1.0000 0.0635
-14.750 -1.3226 0.02334 0.01853 -0.0745 1.0000 0.0645
-14.500 -1.3070 0.02193 0.01708 -0.0750 1.0000 0.0658
-14.250 -1.2876 0.02093 0.01606 -0.0752 1.0000 0.0672
-14.000 -1.2658 0.02016 0.01526 -0.0753 1.0000 0.0685
-13.750 -1.2423 0.01955 0.01461 -0.0753 1.0000 0.0698
-13.500 -1.2192 0.01888 0.01391 -0.0753 1.0000 0.0711
-13.250 -1.1959 0.01820 0.01324 -0.0754 1.0000 0.0727
-13.000 -1.1697 0.01765 0.01268 -0.0757 0.9965 0.0742
-12.750 -1.1345 0.01718 0.01217 -0.0776 0.9776 0.0759
-12.500 -1.1031 0.01666 0.01161 -0.0787 0.9601 0.0776
-12.250 -1.0786 0.01620 0.01111 -0.0784 0.9397 0.0792
-12.000 -1.0543 0.01583 0.01069 -0.0778 0.9173 0.0808
-11.750 -1.0293 0.01554 0.01030 -0.0773 0.8950 0.0823
-11.500 -1.0037 0.01521 0.00987 -0.0770 0.8730 0.0840
-11.250 -0.9777 0.01483 0.00943 -0.0768 0.8525 0.0859
-11.000 -0.9507 0.01454 0.00906 -0.0767 0.8337 0.0878
-10.750 -0.9229 0.01431 0.00874 -0.0766 0.8165 0.0896
-10.500 -0.8952 0.01398 0.00835 -0.0767 0.8025 0.0918
-10.250 -0.8674 0.01369 0.00800 -0.0767 0.7890 0.0941
-10.000 -0.8385 0.01344 0.00771 -0.0769 0.7782 0.0965
-9.750 -0.8099 0.01321 0.00741 -0.0770 0.7659 0.0987
-9.500 -0.7812 0.01289 0.00709 -0.0771 0.7558 0.1015
-9.250 -0.7521 0.01267 0.00682 -0.0773 0.7450 0.1040
-9.000 -0.7227 0.01248 0.00657 -0.0775 0.7353 0.1064
-8.750 -0.6935 0.01219 0.00628 -0.0777 0.7255 0.1098
-8.500 -0.6641 0.01202 0.00605 -0.0778 0.7142 0.1132
-8.250 -0.6344 0.01179 0.00580 -0.0781 0.7053 0.1165
-8.000 -0.6048 0.01157 0.00556 -0.0783 0.6952 0.1203
-7.750 -0.5748 0.01143 0.00537 -0.0785 0.6857 0.1235
-7.500 -0.5450 0.01119 0.00514 -0.0788 0.6759 0.1278
-7.250 -0.5151 0.01105 0.00495 -0.0790 0.6646 0.1319
-7.000 -0.4849 0.01087 0.00476 -0.0792 0.6562 0.1361
-6.750 -0.4548 0.01071 0.00458 -0.0795 0.6458 0.1410
-6.500 -0.4245 0.01060 0.00443 -0.0797 0.6361 0.1453
-6.250 -0.3943 0.01042 0.00425 -0.0800 0.6259 0.1512
-6.000 -0.3639 0.01035 0.00413 -0.0803 0.6155 0.1558
-5.750 -0.3335 0.01017 0.00397 -0.0806 0.6067 0.1619
-5.500 -0.3031 0.01010 0.00385 -0.0808 0.5959 0.1669
-5.250 -0.2725 0.00998 0.00372 -0.0811 0.5867 0.1722
-5.000 -0.2420 0.00989 0.00361 -0.0814 0.5767 0.1778
-4.750 -0.2114 0.00984 0.00351 -0.0817 0.5677 0.1825
-4.500 -0.1807 0.00972 0.00341 -0.0820 0.5599 0.1888
-4.250 -0.1501 0.00969 0.00334 -0.0822 0.5511 0.1942
-4.000 -0.1194 0.00962 0.00326 -0.0825 0.5437 0.2000
-3.750 -0.0887 0.00955 0.00320 -0.0828 0.5363 0.2061
-3.500 -0.0580 0.00956 0.00315 -0.0831 0.5284 0.2108
-3.250 -0.0273 0.00948 0.00309 -0.0834 0.5225 0.2177
-3.000 0.0036 0.00944 0.00305 -0.0836 0.5167 0.2231
-2.750 0.0343 0.00947 0.00303 -0.0839 0.5100 0.2269
-2.500 0.0648 0.00943 0.00298 -0.0842 0.5027 0.2339
-2.250 0.0958 0.00938 0.00296 -0.0845 0.4983 0.2391
-2.000 0.1266 0.00939 0.00294 -0.0847 0.4927 0.2430
-1.750 0.1572 0.00938 0.00290 -0.0850 0.4867 0.2484
-1.500 0.1878 0.00937 0.00289 -0.0852 0.4806 0.2541
-1.250 0.2188 0.00933 0.00287 -0.0855 0.4767 0.2591
-1.000 0.2496 0.00935 0.00286 -0.0858 0.4715 0.2625
-0.750 0.2802 0.00930 0.00282 -0.0861 0.4660 0.2698
-0.500 0.3107 0.00932 0.00283 -0.0863 0.4598 0.2756
-0.250 0.3416 0.00930 0.00282 -0.0866 0.4559 0.2803
0.000 0.3724 0.00928 0.00280 -0.0869 0.4506 0.2869
0.250 0.4029 0.00928 0.00281 -0.0871 0.4450 0.2946
0.500 0.4332 0.00933 0.00284 -0.0873 0.4390 0.3009
0.750 0.4640 0.00928 0.00285 -0.0876 0.4351 0.3114
1.000 0.4946 0.00929 0.00287 -0.0879 0.4300 0.3210
1.250 0.5249 0.00931 0.00291 -0.0881 0.4244 0.3336
1.500 0.5551 0.00939 0.00297 -0.0883 0.4186 0.3440
1.750 0.5858 0.00937 0.00301 -0.0885 0.4151 0.3567
2.000 0.6162 0.00940 0.00306 -0.0888 0.4104 0.3669
2.250 0.6463 0.00946 0.00313 -0.0889 0.4049 0.3783
2.500 0.6762 0.00957 0.00321 -0.0891 0.3985 0.3861
2.750 0.7067 0.00958 0.00327 -0.0893 0.3946 0.3972
3.000 0.7368 0.00965 0.00334 -0.0895 0.3893 0.4057
3.250 0.7666 0.00975 0.00343 -0.0896 0.3833 0.4128
3.500 0.7964 0.00984 0.00353 -0.0897 0.3779 0.4209
3.750 0.8266 0.00990 0.00361 -0.0899 0.3733 0.4281
4.000 0.8563 0.01001 0.00370 -0.0900 0.3679 0.4335
4.250 0.8855 0.01013 0.00381 -0.0901 0.3619 0.4409
4.500 0.9154 0.01021 0.00392 -0.0902 0.3577 0.4475
4.750 0.9451 0.01031 0.00402 -0.0903 0.3529 0.4531
5.000 0.9742 0.01045 0.00413 -0.0904 0.3468 0.4590
5.250 1.0031 0.01058 0.00427 -0.0904 0.3406 0.4655
5.500 1.0326 0.01067 0.00438 -0.0905 0.3356 0.4714
5.750 1.0614 0.01083 0.00452 -0.0905 0.3296 0.4764
6.000 1.0897 0.01101 0.00468 -0.0904 0.3229 0.4828
6.250 1.1188 0.01110 0.00481 -0.0905 0.3181 0.4897
6.500 1.1471 0.01128 0.00497 -0.0904 0.3118 0.4957
6.750 1.1749 0.01150 0.00515 -0.0902 0.3054 0.5004
7.000 1.2035 0.01161 0.00530 -0.0902 0.3002 0.5075
7.250 1.2310 0.01181 0.00549 -0.0901 0.2934 0.5143
7.500 1.2584 0.01202 0.00569 -0.0899 0.2873 0.5212
7.750 1.2862 0.01218 0.00587 -0.0897 0.2821 0.5294
8.000 1.3130 0.01240 0.00609 -0.0895 0.2763 0.5385
8.250 1.3396 0.01263 0.00632 -0.0892 0.2709 0.5460
8.500 1.3667 0.01279 0.00653 -0.0890 0.2661 0.5584
8.750 1.3925 0.01304 0.00680 -0.0886 0.2604 0.5742
9.000 1.4181 0.01327 0.00708 -0.0882 0.2550 0.5990
9.250 1.4444 0.01336 0.00734 -0.0879 0.2507 0.6553
9.500 1.4637 0.01302 0.00765 -0.0861 0.2460 1.0000
9.750 1.4872 0.01342 0.00800 -0.0854 0.2402 1.0000
10.000 1.5129 0.01365 0.00824 -0.0850 0.2366 1.0000
10.250 1.5368 0.01397 0.00854 -0.0843 0.2316 1.0000
10.500 1.5582 0.01441 0.00894 -0.0833 0.2257 1.0000
10.750 1.5817 0.01470 0.00924 -0.0825 0.2217 1.0000
11.000 1.6033 0.01507 0.00960 -0.0815 0.2170 1.0000
11.250 1.6217 0.01556 0.01006 -0.0801 0.2118 1.0000
11.500 1.6408 0.01595 0.01046 -0.0787 0.2075 1.0000
11.750 1.6560 0.01644 0.01094 -0.0767 0.2025 1.0000
12.000 1.6684 0.01713 0.01161 -0.0745 0.1973 1.0000
12.250 1.6849 0.01769 0.01218 -0.0730 0.1934 1.0000
12.500 1.6995 0.01838 0.01288 -0.0714 0.1887 1.0000
12.750 1.7107 0.01934 0.01382 -0.0696 0.1836 1.0000
13.000 1.7258 0.02011 0.01462 -0.0683 0.1798 1.0000
13.250 1.7383 0.02110 0.01561 -0.0670 0.1754 1.0000
13.500 1.7472 0.02242 0.01692 -0.0655 0.1706 1.0000
13.750 1.7607 0.02346 0.01800 -0.0645 0.1674 1.0000
14.000 1.7716 0.02475 0.01931 -0.0634 0.1636 1.0000
14.250 1.7788 0.02639 0.02096 -0.0623 0.1598 1.0000
14.500 1.7878 0.02795 0.02255 -0.0614 0.1566 1.0000
14.750 1.7965 0.02955 0.02418 -0.0606 0.1532 1.0000
15.000 1.8007 0.03159 0.02625 -0.0597 0.1495 1.0000
15.250 1.8033 0.03383 0.02850 -0.0589 0.1460 1.0000
15.500 1.8102 0.03567 0.03040 -0.0582 0.1431 1.0000
15.750 1.8123 0.03800 0.03276 -0.0575 0.1398 1.0000
16.000 1.8095 0.04085 0.03564 -0.0568 0.1366 1.0000
16.250 1.8100 0.04342 0.03827 -0.0563 0.1341 1.0000
16.500 1.8103 0.04606 0.04096 -0.0558 0.1314 1.0000
16.750 1.8073 0.04910 0.04404 -0.0554 0.1287 1.0000
17.000 1.8002 0.05265 0.04763 -0.0551 0.1259 1.0000
17.250 1.7982 0.05572 0.05077 -0.0549 0.1238 1.0000
17.500 1.7955 0.05892 0.05402 -0.0549 0.1215 1.0000
17.750 1.7897 0.06249 0.05764 -0.0548 0.1190 1.0000
18.000 1.7797 0.06657 0.06177 -0.0550 0.1165 1.0000
18.250 1.7737 0.07026 0.06552 -0.0551 0.1145 1.0000
18.500 1.7710 0.07355 0.06887 -0.0553 0.1122 1.0000
18.750 1.7623 0.07762 0.07299 -0.0556 0.1098 1.0000
19.000 1.7494 0.08223 0.07766 -0.0561 0.1074 1.0000
19.250 1.7448 0.08583 0.08131 -0.0565 0.1053 1.0000
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