WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Reynolds number: 500,000 Max Cl/Cd: 53.94 at α=9.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fxlv152-il-500000-n5.txt Download as CSV file: xf-fxlv152-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX L V-152 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.000 -1.1121 0.11970 0.11591 0.0245 1.0005 0.0051
-17.750 -1.1275 0.11245 0.10854 0.0207 1.0005 0.0051
-17.500 -1.1425 0.10548 0.10144 0.0172 1.0005 0.0051
-17.250 -1.1567 0.09873 0.09456 0.0139 1.0005 0.0051
-17.000 -1.1706 0.09224 0.08793 0.0108 1.0005 0.0051
-16.750 -1.1830 0.08615 0.08172 0.0079 1.0005 0.0051
-16.500 -1.1945 0.08041 0.07585 0.0054 1.0005 0.0051
-16.250 -1.2045 0.07508 0.07040 0.0031 1.0005 0.0051
-16.000 -1.2126 0.07020 0.06540 0.0011 1.0005 0.0052
-15.750 -1.2198 0.06562 0.06070 -0.0006 1.0005 0.0052
-15.500 -1.2253 0.06145 0.05641 -0.0020 1.0005 0.0052
-15.250 -1.2300 0.05755 0.05240 -0.0032 1.0005 0.0052
-15.000 -1.2338 0.05398 0.04872 -0.0041 1.0005 0.0053
-14.750 -1.2364 0.05067 0.04531 -0.0048 1.0005 0.0053
-14.500 -1.2378 0.04759 0.04212 -0.0054 1.0005 0.0054
-14.250 -1.2375 0.04475 0.03917 -0.0058 1.0005 0.0055
-14.000 -1.2355 0.04214 0.03647 -0.0060 1.0005 0.0055
-13.750 -1.2321 0.03971 0.03394 -0.0062 1.0005 0.0056
-13.500 -1.2272 0.03749 0.03163 -0.0063 1.0005 0.0057
-13.250 -1.2208 0.03542 0.02947 -0.0063 1.0005 0.0058
-13.000 -1.2132 0.03349 0.02746 -0.0063 1.0005 0.0059
-12.750 -1.2042 0.03172 0.02560 -0.0063 1.0005 0.0059
-12.500 -1.1941 0.03008 0.02388 -0.0062 1.0005 0.0060
-12.250 -1.1831 0.02855 0.02227 -0.0060 1.0005 0.0061
-12.000 -1.1710 0.02713 0.02078 -0.0059 1.0005 0.0061
-11.750 -1.1581 0.02581 0.01938 -0.0057 1.0005 0.0062
-11.500 -1.1446 0.02459 0.01809 -0.0054 1.0005 0.0063
-11.250 -1.1303 0.02348 0.01691 -0.0051 1.0005 0.0064
-11.000 -1.1157 0.02246 0.01584 -0.0046 1.0005 0.0065
-10.750 -1.0976 0.02168 0.01486 -0.0043 0.8799 0.0068
-10.500 -1.0839 0.02103 0.01403 -0.0029 0.8443 0.0070
-10.250 -1.0662 0.02035 0.01323 -0.0021 0.8193 0.0074
-10.000 -1.0473 0.01968 0.01248 -0.0014 0.7983 0.0079
-9.500 -1.0039 0.01872 0.01136 -0.0006 0.7661 0.0144
-9.250 -0.9811 0.01828 0.01083 -0.0003 0.7563 0.0154
-9.000 -0.9573 0.01790 0.01036 -0.0001 0.7475 0.0164
-8.750 -0.9331 0.01754 0.00991 0.0001 0.7395 0.0171
-8.500 -0.9094 0.01706 0.00939 0.0003 0.7312 0.0179
-8.250 -0.8850 0.01666 0.00892 0.0005 0.7225 0.0187
-8.000 -0.8599 0.01629 0.00849 0.0006 0.7139 0.0195
-7.750 -0.8352 0.01587 0.00801 0.0007 0.7051 0.0205
-7.500 -0.8101 0.01547 0.00757 0.0008 0.6980 0.0216
-7.250 -0.7847 0.01510 0.00714 0.0009 0.6910 0.0230
-7.000 -0.7595 0.01469 0.00672 0.0010 0.6849 0.0254
-6.500 -0.7083 0.01389 0.00594 0.0010 0.6755 0.0428
-6.250 -0.6825 0.01350 0.00559 0.0010 0.6712 0.0529
-6.000 -0.6560 0.01321 0.00528 0.0010 0.6672 0.0640
-5.750 -0.6293 0.01290 0.00499 0.0009 0.6636 0.0727
-5.250 -0.5769 0.01210 0.00436 0.0008 0.6554 0.1122
-5.000 -0.5508 0.01169 0.00406 0.0008 0.6515 0.1399
-4.750 -0.5243 0.01134 0.00378 0.0007 0.6480 0.1652
-4.500 -0.4984 0.01083 0.00345 0.0007 0.6450 0.2037
-4.000 -0.4453 0.00998 0.00294 0.0005 0.6386 0.2895
-3.750 -0.4183 0.00964 0.00271 0.0004 0.6353 0.3219
-3.500 -0.3925 0.00914 0.00246 0.0004 0.6321 0.3818
-3.250 -0.3656 0.00885 0.00232 0.0003 0.6289 0.4305
-3.000 -0.3377 0.00866 0.00223 0.0002 0.6260 0.4645
-2.750 -0.3098 0.00850 0.00218 0.0001 0.6229 0.4891
-2.500 -0.2813 0.00842 0.00217 0.0000 0.6193 0.5094
-2.250 -0.2524 0.00840 0.00214 -0.0002 0.6155 0.5240
-2.000 -0.2235 0.00841 0.00212 -0.0003 0.6118 0.5367
-1.750 -0.1947 0.00839 0.00210 -0.0005 0.6085 0.5467
-1.500 -0.1654 0.00840 0.00209 -0.0007 0.6055 0.5559
-1.250 -0.1364 0.00837 0.00208 -0.0009 0.6025 0.5619
-1.000 -0.1074 0.00835 0.00207 -0.0011 0.5992 0.5676
-0.750 -0.0783 0.00835 0.00204 -0.0014 0.5957 0.5723
-0.500 -0.0491 0.00837 0.00201 -0.0016 0.5922 0.5763
-0.250 -0.0202 0.00835 0.00201 -0.0018 0.5886 0.5806
0.000 0.0089 0.00833 0.00202 -0.0020 0.5839 0.5846
0.250 0.0379 0.00833 0.00202 -0.0022 0.5790 0.5886
0.500 0.0670 0.00835 0.00202 -0.0024 0.5750 0.5926
1.000 0.1252 0.00836 0.00205 -0.0028 0.5654 0.5986
1.250 0.1541 0.00836 0.00207 -0.0030 0.5594 0.6016
1.500 0.1829 0.00839 0.00209 -0.0031 0.5538 0.6051
1.750 0.2121 0.00839 0.00213 -0.0034 0.5458 0.6091
2.000 0.2409 0.00842 0.00212 -0.0035 0.5339 0.6128
2.250 0.2699 0.00842 0.00215 -0.0037 0.5205 0.6160
2.500 0.2984 0.00844 0.00217 -0.0038 0.5038 0.6194
2.750 0.3262 0.00855 0.00219 -0.0038 0.4795 0.6229
3.000 0.3540 0.00870 0.00226 -0.0039 0.4564 0.6262
3.250 0.3816 0.00889 0.00236 -0.0039 0.4231 0.6293
3.500 0.4077 0.00929 0.00252 -0.0038 0.3636 0.6323
3.750 0.4337 0.00969 0.00274 -0.0038 0.3201 0.6353
4.000 0.4600 0.01004 0.00299 -0.0038 0.2861 0.6386
4.250 0.4857 0.01051 0.00326 -0.0037 0.2342 0.6420
4.500 0.5119 0.01090 0.00352 -0.0037 0.1966 0.6454
4.750 0.5373 0.01141 0.00385 -0.0036 0.1597 0.6487
5.000 0.5632 0.01183 0.00414 -0.0036 0.1319 0.6517
5.250 0.5889 0.01222 0.00444 -0.0036 0.1052 0.6549
5.500 0.6148 0.01258 0.00473 -0.0035 0.0855 0.6585
5.750 0.6406 0.01294 0.00504 -0.0034 0.0722 0.6626
6.000 0.6667 0.01328 0.00535 -0.0034 0.0611 0.6668
6.250 0.6923 0.01365 0.00568 -0.0033 0.0466 0.6713
6.500 0.7177 0.01400 0.00604 -0.0032 0.0396 0.6765
6.750 0.7433 0.01433 0.00639 -0.0031 0.0314 0.6819
7.250 0.7924 0.01522 0.00727 -0.0027 0.0215 0.6924
7.500 0.8172 0.01561 0.00771 -0.0025 0.0204 0.6988
7.750 0.8422 0.01597 0.00811 -0.0023 0.0198 0.7056
8.000 0.8669 0.01633 0.00854 -0.0021 0.0190 0.7126
8.250 0.8910 0.01675 0.00901 -0.0019 0.0181 0.7206
8.500 0.9145 0.01719 0.00951 -0.0016 0.0173 0.7284
8.750 0.9387 0.01753 0.00993 -0.0014 0.0165 0.7372
9.000 0.9623 0.01792 0.01038 -0.0011 0.0156 0.7455
9.250 0.9852 0.01833 0.01088 -0.0007 0.0146 0.7548
9.500 1.0082 0.01869 0.01135 -0.0003 0.0133 0.7652
10.000 1.0482 0.01982 0.01260 0.0009 0.0076 0.7995
10.250 1.0663 0.02046 0.01335 0.0018 0.0071 0.8209
10.500 1.0822 0.02110 0.01412 0.0029 0.0068 0.8464
10.750 1.0953 0.02174 0.01495 0.0045 0.0066 0.8854
11.000 1.1123 0.02251 0.01589 0.0050 0.0065 0.9995
11.250 1.1269 0.02352 0.01697 0.0054 0.0064 0.9995
11.500 1.1408 0.02464 0.01815 0.0058 0.0063 0.9995
11.750 1.1541 0.02585 0.01943 0.0062 0.0062 0.9995
12.000 1.1666 0.02716 0.02082 0.0064 0.0061 0.9995
12.250 1.1783 0.02858 0.02231 0.0067 0.0061 0.9995
12.500 1.1889 0.03009 0.02390 0.0069 0.0060 0.9995
12.750 1.1986 0.03171 0.02559 0.0071 0.0059 0.9995
13.000 1.2072 0.03345 0.02742 0.0072 0.0059 0.9995
13.250 1.2145 0.03533 0.02938 0.0073 0.0058 0.9995
13.500 1.2204 0.03736 0.03150 0.0074 0.0057 0.9995
13.750 1.2249 0.03953 0.03376 0.0075 0.0057 0.9995
14.000 1.2280 0.04188 0.03621 0.0074 0.0056 0.9995
14.250 1.2296 0.04442 0.03884 0.0073 0.0055 0.9995
14.500 1.2296 0.04717 0.04169 0.0071 0.0055 0.9995
14.750 1.2280 0.05014 0.04476 0.0068 0.0054 0.9995
15.000 1.2251 0.05333 0.04805 0.0063 0.0054 0.9995
15.250 1.2210 0.05679 0.05162 0.0056 0.0053 0.9995
15.500 1.2158 0.06059 0.05553 0.0045 0.0053 0.9995
15.750 1.2095 0.06470 0.05975 0.0033 0.0052 0.9995
16.000 1.2024 0.06905 0.06423 0.0018 0.0052 0.9995
16.250 1.1941 0.07376 0.06905 0.0001 0.0052 0.9995
16.500 1.1845 0.07877 0.07418 -0.0019 0.0052 0.9995
16.750 1.1734 0.08420 0.07973 -0.0041 0.0052 0.9995
17.000 1.1611 0.08998 0.08564 -0.0066 0.0052 0.9995
17.250 1.1477 0.09610 0.09189 -0.0094 0.0052 0.9995
17.500 1.1329 0.10263 0.09854 -0.0124 0.0052 0.9995
17.750 1.1181 0.10927 0.10531 -0.0156 0.0052 0.9995
18.000 1.1023 0.11624 0.11240 -0.0190 0.0052 0.9995
18.250 1.0866 0.12335 0.11963 -0.0225 0.0052 0.9995
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