FX 78-K-140/20 (fx78k140-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 78-K-140/20 (fx78k140-il) Reynolds number: 1,000,000 Max Cl/Cd: 153.09 at α=5.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx78k140-il-1000000-n5.txt Download as CSV file: xf-fx78k140-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 78-K-140/20
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
------ -------- --------- --------- -------- -------- --------
-11.750 -0.6656 0.03387 0.03065 -0.0931 0.7088 0.0024
-11.500 -0.7067 0.02775 0.02394 -0.0865 0.7076 0.0021
-11.250 -0.6871 0.02732 0.02348 -0.0858 0.7066 0.0022
-11.000 -0.6831 0.02515 0.02107 -0.0832 0.7056 0.0023
-10.750 -0.6746 0.02350 0.01920 -0.0810 0.7045 0.0023
-10.500 -0.6551 0.02286 0.01851 -0.0800 0.7035 0.0025
-10.250 -0.6455 0.02121 0.01659 -0.0777 0.7025 0.0024
-10.000 -0.6265 0.02050 0.01579 -0.0767 0.7014 0.0026
-9.750 -0.6077 0.01971 0.01488 -0.0755 0.7004 0.0028
-9.500 -0.5867 0.01919 0.01428 -0.0747 0.6994 0.0030
-9.250 -0.5694 0.01819 0.01309 -0.0732 0.6983 0.0030
-9.000 -0.5476 0.01769 0.01250 -0.0724 0.6972 0.0032
-8.750 -0.5278 0.01692 0.01159 -0.0713 0.6962 0.0033
-8.500 -0.5095 0.01586 0.01032 -0.0698 0.6954 0.0035
-8.250 -0.4862 0.01546 0.00986 -0.0693 0.6946 0.0035
-8.000 -0.4653 0.01471 0.00897 -0.0682 0.6936 0.0037
-7.750 -0.4399 0.01457 0.00881 -0.0681 0.6927 0.0038
-7.500 -0.4190 0.01378 0.00788 -0.0669 0.6916 0.0041
-7.250 -0.3956 0.01331 0.00736 -0.0663 0.6904 0.0047
-7.000 -0.3714 0.01295 0.00695 -0.0658 0.6894 0.0048
-6.750 -0.3455 0.01283 0.00682 -0.0657 0.6883 0.0055
-6.500 -0.3219 0.01238 0.00629 -0.0650 0.6874 0.0057
-6.250 -0.2971 0.01209 0.00593 -0.0646 0.6865 0.0060
-6.000 -0.2724 0.01178 0.00556 -0.0641 0.6855 0.0063
-5.750 -0.2479 0.01148 0.00518 -0.0637 0.6845 0.0064
-5.500 -0.2246 0.01102 0.00465 -0.0629 0.6835 0.0076
-5.250 -0.1998 0.01072 0.00434 -0.0625 0.6824 0.0082
-5.000 -0.1743 0.01051 0.00410 -0.0621 0.6816 0.0089
-4.750 -0.1488 0.01030 0.00386 -0.0618 0.6806 0.0097
-4.500 -0.1236 0.01005 0.00355 -0.0614 0.6796 0.0099
-4.250 -0.0985 0.00979 0.00329 -0.0610 0.6785 0.0121
-4.000 -0.0728 0.00961 0.00310 -0.0607 0.6773 0.0139
-3.750 -0.0469 0.00945 0.00292 -0.0605 0.6762 0.0155
-3.500 -0.0210 0.00928 0.00272 -0.0602 0.6752 0.0179
-3.250 0.0047 0.00911 0.00257 -0.0600 0.6742 0.0225
-3.000 0.0306 0.00896 0.00242 -0.0597 0.6731 0.0284
-2.750 0.0566 0.00882 0.00229 -0.0595 0.6721 0.0350
-2.500 0.0825 0.00869 0.00217 -0.0593 0.6709 0.0452
-2.250 0.1085 0.00857 0.00207 -0.0591 0.6697 0.0554
-2.000 0.1347 0.00845 0.00198 -0.0590 0.6686 0.0665
-1.750 0.1609 0.00833 0.00190 -0.0588 0.6675 0.0800
-1.500 0.1867 0.00819 0.00183 -0.0586 0.6662 0.1038
-1.250 0.2118 0.00801 0.00177 -0.0583 0.6650 0.1398
-1.000 0.2351 0.00771 0.00170 -0.0576 0.6636 0.2137
-0.750 0.2595 0.00751 0.00165 -0.0572 0.6623 0.2688
-0.500 0.2829 0.00725 0.00160 -0.0565 0.6610 0.3432
-0.250 0.3049 0.00694 0.00156 -0.0556 0.6598 0.4356
0.000 0.3232 0.00649 0.00149 -0.0539 0.6584 0.5700
0.250 0.3306 0.00584 0.00149 -0.0496 0.6569 0.7718
0.500 0.3536 0.00572 0.00153 -0.0486 0.6556 0.8267
0.750 0.3814 0.00562 0.00159 -0.0487 0.6543 0.8748
1.000 0.4163 0.00558 0.00163 -0.0504 0.6526 0.9042
1.250 0.4625 0.00557 0.00168 -0.0547 0.6508 0.9307
1.750 0.5377 0.00561 0.00171 -0.0596 0.6466 0.9431
2.000 0.5724 0.00563 0.00172 -0.0614 0.6446 0.9459
2.250 0.6041 0.00567 0.00174 -0.0625 0.6424 0.9509
2.500 0.6368 0.00570 0.00180 -0.0639 0.6401 0.9537
2.750 0.6714 0.00574 0.00185 -0.0658 0.6377 0.9554
3.000 0.7050 0.00578 0.00190 -0.0673 0.6350 0.9572
3.250 0.7374 0.00582 0.00195 -0.0687 0.6326 0.9596
3.500 0.7678 0.00588 0.00200 -0.0695 0.6294 0.9627
3.750 0.7955 0.00593 0.00209 -0.0698 0.6269 0.9668
4.000 0.8288 0.00598 0.00218 -0.0714 0.6235 0.9680
4.250 0.8611 0.00604 0.00226 -0.0727 0.6202 0.9695
4.500 0.8928 0.00611 0.00236 -0.0739 0.6169 0.9712
4.750 0.9240 0.00618 0.00247 -0.0750 0.6129 0.9733
5.000 0.9540 0.00625 0.00258 -0.0759 0.6078 0.9760
5.250 0.9798 0.00640 0.00267 -0.0758 0.5882 0.9799
5.500 1.0099 0.00664 0.00286 -0.0769 0.5629 0.9816
5.750 1.0316 0.00756 0.00345 -0.0768 0.4933 0.9859
6.000 1.0484 0.00894 0.00444 -0.0764 0.4130 0.9914
6.250 1.0470 0.01215 0.00684 -0.0752 0.2640 1.0000
6.500 1.0249 0.01325 0.00789 -0.0673 0.2471 1.0000
6.750 0.9959 0.01536 0.00968 -0.0594 0.1870 1.0000
7.000 0.9850 0.01713 0.01118 -0.0546 0.1348 1.0000
7.250 0.9806 0.01875 0.01256 -0.0510 0.0863 1.0000
7.500 0.9685 0.02093 0.01436 -0.0467 0.0178 1.0000
7.750 0.9836 0.02163 0.01507 -0.0456 0.0149 1.0000
8.000 0.9957 0.02253 0.01596 -0.0442 0.0081 1.0000
8.250 1.0092 0.02336 0.01679 -0.0430 0.0051 1.0000
8.500 1.0234 0.02416 0.01764 -0.0419 0.0046 1.0000
8.750 1.0393 0.02485 0.01833 -0.0412 0.0045 1.0000
9.000 1.0536 0.02567 0.01919 -0.0401 0.0044 1.0000
9.250 1.0649 0.02669 0.02024 -0.0388 0.0035 1.0000
9.500 1.0775 0.02768 0.02127 -0.0377 0.0031 1.0000
9.750 1.0928 0.02849 0.02210 -0.0370 0.0029 1.0000
10.000 1.1067 0.02942 0.02307 -0.0361 0.0022 1.0000
10.250 1.1173 0.03063 0.02436 -0.0348 0.0027 1.0000
10.500 1.1310 0.03160 0.02534 -0.0340 0.0020 1.0000
10.750 1.1384 0.03308 0.02688 -0.0326 0.0017 1.0000
11.000 1.1499 0.03429 0.02814 -0.0317 0.0018 1.0000
11.250 1.1573 0.03582 0.02974 -0.0303 0.0017 1.0000
11.500 1.1739 0.03662 0.03057 -0.0299 0.0019 1.0000
11.750 1.1754 0.03870 0.03274 -0.0282 0.0016 1.0000
12.000 1.1763 0.04087 0.03502 -0.0266 0.0015 1.0000
12.250 1.1846 0.04244 0.03666 -0.0256 0.0016 1.0000
12.500 1.2009 0.04333 0.03756 -0.0254 0.0017 1.0000
12.750 1.1970 0.04604 0.04041 -0.0235 0.0016 1.0000
13.000 1.2084 0.04742 0.04186 -0.0229 0.0015 1.0000
13.250 1.2171 0.04904 0.04354 -0.0222 0.0015 1.0000
13.500 1.2287 0.05042 0.04496 -0.0218 0.0015 1.0000
13.750 1.2208 0.05361 0.04832 -0.0197 0.0015 1.0000
14.000 1.2345 0.05489 0.04965 -0.0196 0.0014 1.0000
14.250 1.2307 0.05776 0.05266 -0.0180 0.0015 1.0000
14.500 1.2453 0.05901 0.05392 -0.0183 0.0015 1.0000
14.750 1.2445 0.06168 0.05673 -0.0171 0.0014 1.0000
15.000 1.2500 0.06385 0.05900 -0.0165 0.0013 1.0000
15.250 1.2425 0.06727 0.06263 -0.0146 0.0014 1.0000
15.500 1.2556 0.06887 0.06425 -0.0153 0.0012 1.0000
15.750 1.2641 0.07087 0.06630 -0.0157 0.0013 1.0000
16.000 1.2663 0.07358 0.06912 -0.0154 0.0012 1.0000
16.250 1.2638 0.07682 0.07251 -0.0149 0.0012 1.0000
16.500 1.2645 0.07983 0.07563 -0.0149 0.0012 1.0000
16.750 1.2552 0.08413 0.08013 -0.0144 0.0012 1.0000
17.000 1.2430 0.08893 0.08514 -0.0142 0.0013 1.0000
17.250 1.2213 0.09540 0.09190 -0.0142 0.0013 1.0000
17.500 1.2467 0.09534 0.09171 -0.0159 0.0012 1.0000
17.750 1.2587 0.09721 0.09356 -0.0171 0.0011 1.0000
18.000 1.2114 0.10781 0.10462 -0.0178 0.0012 1.0000
18.250 1.1838 0.11619 0.11328 -0.0198 0.0012 1.0000
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