FX 75-VG-166/22 (fx75vg166-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 75-VG-166/22 (fx75vg166-il) Reynolds number: 1,000,000 Max Cl/Cd: 103.32 at α=4.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx75vg166-il-1000000-n5.txt Download as CSV file: xf-fx75vg166-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 75-VG-166/22
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
------ -------- --------- --------- -------- -------- --------
-17.750 -0.8954 0.07154 0.06765 -0.0818 0.7266 0.0059
-17.500 -0.9123 0.06438 0.06031 -0.0867 0.7263 0.0057
-17.250 -0.9272 0.05797 0.05375 -0.0910 0.7260 0.0058
-17.000 -0.9408 0.05235 0.04795 -0.0945 0.7256 0.0058
-16.750 -0.9447 0.04837 0.04385 -0.0967 0.7252 0.0059
-16.500 -0.9442 0.04518 0.04052 -0.0984 0.7246 0.0059
-16.250 -0.9400 0.04271 0.03796 -0.0994 0.7243 0.0061
-16.000 -0.9425 0.03978 0.03488 -0.0999 0.7241 0.0059
-15.750 -0.9385 0.03766 0.03266 -0.1001 0.7238 0.0059
-15.500 -0.9372 0.03541 0.03028 -0.0999 0.7235 0.0059
-15.250 -0.9292 0.03386 0.02865 -0.0997 0.7231 0.0060
-15.000 -0.9220 0.03226 0.02696 -0.0993 0.7226 0.0062
-14.750 -0.9076 0.03130 0.02595 -0.0992 0.7221 0.0063
-14.500 -0.9022 0.02960 0.02413 -0.0983 0.7216 0.0062
-14.250 -0.8904 0.02846 0.02290 -0.0978 0.7211 0.0064
-14.000 -0.8745 0.02763 0.02201 -0.0975 0.7206 0.0067
-13.750 -0.8618 0.02658 0.02088 -0.0969 0.7202 0.0066
-13.500 -0.8463 0.02573 0.01996 -0.0964 0.7196 0.0068
-13.250 -0.8325 0.02475 0.01889 -0.0956 0.7190 0.0070
-13.000 -0.8175 0.02389 0.01796 -0.0949 0.7185 0.0070
-12.750 -0.8016 0.02310 0.01708 -0.0942 0.7180 0.0071
-12.500 -0.7843 0.02241 0.01632 -0.0936 0.7174 0.0072
-12.250 -0.7686 0.02164 0.01549 -0.0928 0.7167 0.0073
-12.000 -0.7511 0.02100 0.01479 -0.0921 0.7161 0.0072
-11.750 -0.7365 0.02014 0.01386 -0.0909 0.7152 0.0076
-11.500 -0.7178 0.01959 0.01328 -0.0902 0.7146 0.0078
-11.250 -0.6995 0.01901 0.01265 -0.0894 0.7139 0.0078
-11.000 -0.6794 0.01857 0.01218 -0.0888 0.7132 0.0083
-10.750 -0.6592 0.01812 0.01170 -0.0882 0.7126 0.0087
-10.500 -0.6409 0.01754 0.01105 -0.0873 0.7120 0.0084
-10.250 -0.6199 0.01717 0.01065 -0.0868 0.7114 0.0090
-10.000 -0.5986 0.01682 0.01026 -0.0863 0.7106 0.0094
-9.750 -0.5790 0.01638 0.00978 -0.0854 0.7102 0.0095
-9.500 -0.5597 0.01592 0.00930 -0.0844 0.7098 0.0098
-9.250 -0.5395 0.01554 0.00892 -0.0836 0.7093 0.0104
-9.000 -0.5194 0.01517 0.00853 -0.0828 0.7087 0.0107
-8.750 -0.4980 0.01489 0.00824 -0.0821 0.7081 0.0114
-8.500 -0.4777 0.01454 0.00788 -0.0812 0.7075 0.0117
-8.250 -0.4572 0.01422 0.00753 -0.0803 0.7068 0.0122
-8.000 -0.4367 0.01390 0.00720 -0.0794 0.7061 0.0127
-7.750 -0.4168 0.01357 0.00687 -0.0783 0.7054 0.0134
-7.500 -0.3966 0.01327 0.00657 -0.0773 0.7047 0.0141
-7.250 -0.3766 0.01300 0.00628 -0.0763 0.7040 0.0148
-7.000 -0.3563 0.01278 0.00606 -0.0752 0.7033 0.0156
-6.750 -0.3384 0.01251 0.00577 -0.0737 0.7025 0.0164
-6.500 -0.3204 0.01228 0.00553 -0.0722 0.7018 0.0171
-6.250 -0.3009 0.01207 0.00532 -0.0709 0.7011 0.0182
-6.000 -0.2790 0.01187 0.00511 -0.0701 0.7004 0.0192
-5.750 -0.2569 0.01166 0.00488 -0.0692 0.6997 0.0202
-5.500 -0.2348 0.01144 0.00467 -0.0684 0.6990 0.0219
-5.250 -0.2118 0.01126 0.00447 -0.0678 0.6984 0.0233
-5.000 -0.1887 0.01106 0.00429 -0.0672 0.6977 0.0262
-4.750 -0.1650 0.01090 0.00413 -0.0666 0.6970 0.0296
-4.500 -0.1416 0.01071 0.00398 -0.0661 0.6964 0.0352
-4.250 -0.1179 0.01053 0.00384 -0.0656 0.6957 0.0421
-4.000 -0.0941 0.01034 0.00370 -0.0651 0.6949 0.0519
-3.750 -0.0709 0.01010 0.00356 -0.0645 0.6940 0.0704
-3.250 -0.0245 0.00960 0.00328 -0.0633 0.6918 0.1249
-3.000 -0.0019 0.00928 0.00313 -0.0627 0.6906 0.1695
-2.750 0.0180 0.00881 0.00294 -0.0616 0.6896 0.2465
-2.500 0.0392 0.00838 0.00277 -0.0608 0.6886 0.3184
-2.250 0.0584 0.00781 0.00255 -0.0597 0.6875 0.4174
-2.000 0.0756 0.00708 0.00226 -0.0582 0.6864 0.5403
-1.750 0.0894 0.00635 0.00209 -0.0557 0.6854 0.6873
-1.500 0.1165 0.00640 0.00226 -0.0555 0.6845 0.7285
-1.250 0.1469 0.00672 0.00263 -0.0559 0.6837 0.7438
-1.000 0.1763 0.00689 0.00273 -0.0563 0.6826 0.7635
-0.750 0.2059 0.00709 0.00295 -0.0567 0.6814 0.7677
-0.500 0.2351 0.00719 0.00306 -0.0570 0.6798 0.7709
-0.250 0.2639 0.00725 0.00309 -0.0574 0.6782 0.7740
0.000 0.2924 0.00725 0.00306 -0.0577 0.6768 0.7760
0.250 0.3211 0.00725 0.00306 -0.0580 0.6754 0.7771
0.500 0.3501 0.00725 0.00306 -0.0584 0.6737 0.7779
0.750 0.3790 0.00725 0.00305 -0.0587 0.6720 0.7788
1.000 0.4078 0.00724 0.00302 -0.0591 0.6702 0.7795
1.250 0.4365 0.00726 0.00303 -0.0594 0.6683 0.7803
1.500 0.4649 0.00728 0.00309 -0.0597 0.6660 0.7812
1.750 0.4934 0.00730 0.00313 -0.0600 0.6637 0.7821
2.000 0.5218 0.00731 0.00315 -0.0603 0.6609 0.7831
2.250 0.5501 0.00730 0.00314 -0.0606 0.6580 0.7841
2.500 0.5783 0.00729 0.00311 -0.0608 0.6550 0.7850
2.750 0.6064 0.00730 0.00313 -0.0611 0.6521 0.7859
3.000 0.6344 0.00730 0.00316 -0.0613 0.6479 0.7867
3.250 0.6617 0.00727 0.00311 -0.0613 0.6399 0.7876
3.500 0.6887 0.00727 0.00310 -0.0614 0.6288 0.7884
3.750 0.7139 0.00732 0.00308 -0.0610 0.6132 0.7892
4.000 0.7392 0.00740 0.00312 -0.0607 0.6005 0.7898
4.250 0.7645 0.00749 0.00318 -0.0604 0.5899 0.7904
4.500 0.7873 0.00762 0.00326 -0.0595 0.5661 0.7912
4.750 0.8081 0.00784 0.00340 -0.0584 0.5434 0.7919
5.000 0.8277 0.00812 0.00360 -0.0570 0.5184 0.7926
5.250 0.8429 0.00854 0.00388 -0.0548 0.4837 0.7931
5.500 0.8459 0.00932 0.00438 -0.0503 0.4226 0.7939
5.750 0.8510 0.00996 0.00482 -0.0463 0.3773 0.7946
6.000 0.8501 0.01068 0.00532 -0.0412 0.3312 0.7954
6.250 0.8537 0.01108 0.00565 -0.0368 0.3079 0.7961
6.500 0.8527 0.01167 0.00612 -0.0317 0.2825 0.7971
6.750 0.8495 0.01245 0.00679 -0.0267 0.2541 0.7981
7.000 0.8421 0.01378 0.00799 -0.0220 0.2228 0.7990
7.250 0.8405 0.01499 0.00908 -0.0185 0.1979 0.7997
7.500 0.8483 0.01579 0.00983 -0.0161 0.1829 0.8003
7.750 0.8482 0.01693 0.01080 -0.0128 0.1534 0.8009
8.000 0.8601 0.01761 0.01143 -0.0112 0.1414 0.8013
8.250 0.8645 0.01863 0.01231 -0.0086 0.1157 0.8018
8.500 0.8815 0.01913 0.01283 -0.0077 0.1138 0.8021
8.750 0.8922 0.01992 0.01355 -0.0061 0.0986 0.8024
9.000 0.9041 0.02070 0.01426 -0.0047 0.0847 0.8027
9.250 0.9133 0.02164 0.01509 -0.0031 0.0684 0.8029
9.500 0.9266 0.02239 0.01580 -0.0020 0.0591 0.8032
9.750 0.9394 0.02320 0.01656 -0.0008 0.0481 0.8034
10.000 0.9515 0.02408 0.01738 0.0003 0.0383 0.8035
10.250 0.9655 0.02487 0.01816 0.0012 0.0332 0.8037
10.500 0.9784 0.02575 0.01900 0.0021 0.0265 0.8038
10.750 0.9945 0.02646 0.01972 0.0027 0.0246 0.8040
11.000 1.0085 0.02731 0.02056 0.0035 0.0212 0.8041
11.250 1.0238 0.02815 0.02141 0.0040 0.0198 0.8042
11.500 1.0393 0.02901 0.02229 0.0045 0.0185 0.8043
11.750 1.0552 0.02986 0.02315 0.0049 0.0171 0.8044
12.000 1.0715 0.03070 0.02403 0.0052 0.0162 0.8044
12.250 1.0867 0.03166 0.02501 0.0055 0.0155 0.8045
12.500 1.1006 0.03271 0.02607 0.0059 0.0143 0.8045
12.750 1.1167 0.03363 0.02703 0.0061 0.0134 0.8046
13.000 1.1322 0.03460 0.02804 0.0064 0.0131 0.8046
13.250 1.1463 0.03570 0.02916 0.0066 0.0123 0.8047
13.500 1.1600 0.03685 0.03035 0.0069 0.0119 0.8047
13.750 1.1731 0.03807 0.03159 0.0072 0.0109 0.8047
14.000 1.1872 0.03923 0.03280 0.0073 0.0105 0.8048
14.250 1.1999 0.04050 0.03411 0.0075 0.0103 0.8049
14.500 1.2126 0.04178 0.03544 0.0077 0.0100 0.8050
14.750 1.2241 0.04315 0.03683 0.0080 0.0092 0.8051
15.000 1.2353 0.04464 0.03839 0.0081 0.0093 0.8051
15.250 1.2464 0.04617 0.03994 0.0082 0.0085 0.8052
15.500 1.2555 0.04789 0.04172 0.0083 0.0084 0.8052
15.750 1.2669 0.04945 0.04334 0.0083 0.0083 0.8053
16.000 1.2764 0.05122 0.04517 0.0082 0.0081 0.8054
16.250 1.2867 0.05296 0.04698 0.0080 0.0080 0.8056
16.500 1.2945 0.05490 0.04898 0.0080 0.0076 0.8056
16.750 1.3024 0.05694 0.05110 0.0078 0.0076 0.8059
17.000 1.3104 0.05897 0.05319 0.0075 0.0074 0.8061
17.250 1.3143 0.06140 0.05570 0.0074 0.0073 0.8061
17.500 1.3202 0.06367 0.05804 0.0071 0.0073 0.8062
17.750 1.3255 0.06608 0.06051 0.0067 0.0071 0.8063
18.000 1.3290 0.06869 0.06319 0.0064 0.0069 0.8063
18.250 1.3316 0.07143 0.06601 0.0059 0.0069 0.8063
18.500 1.3323 0.07446 0.06911 0.0054 0.0067 0.8064
18.750 1.3342 0.07732 0.07206 0.0048 0.0067 0.8064
19.000 1.3301 0.08101 0.07584 0.0040 0.0065 0.8064
19.250 1.3272 0.08463 0.07955 0.0032 0.0064 0.8065
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