WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Reynolds number: 200,000 Max Cl/Cd: 52.25 at α=6.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fxlv152-il-200000.txt Download as CSV file: xf-fxlv152-il-200000.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 = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.500 -0.9356 0.14530 0.14177 0.0309 1.0005 0.0222
-17.250 -0.9693 0.13173 0.12802 0.0220 1.0005 0.0217
-17.000 -1.0068 0.11834 0.11435 0.0131 1.0005 0.0211
-16.750 -1.0416 0.10663 0.10231 0.0056 1.0005 0.0207
-16.500 -1.0668 0.09772 0.09312 0.0003 1.0005 0.0206
-16.250 -1.0828 0.09105 0.08623 -0.0032 1.0005 0.0206
-16.000 -1.0952 0.08529 0.08027 -0.0059 1.0005 0.0207
-15.750 -1.1050 0.08017 0.07497 -0.0081 1.0005 0.0209
-15.500 -1.1133 0.07547 0.07007 -0.0098 1.0005 0.0210
-15.250 -1.1198 0.07118 0.06560 -0.0110 1.0005 0.0212
-15.000 -1.1245 0.06727 0.06149 -0.0119 1.0005 0.0215
-14.750 -1.1274 0.06367 0.05769 -0.0124 1.0005 0.0218
-14.500 -1.1290 0.06028 0.05409 -0.0127 1.0005 0.0222
-14.250 -1.1277 0.05730 0.05094 -0.0127 1.0005 0.0226
-14.000 -1.1210 0.05512 0.04881 -0.0122 1.0005 0.0232
-13.750 -1.1170 0.05265 0.04629 -0.0121 1.0005 0.0239
-13.500 -1.1137 0.05008 0.04360 -0.0120 1.0005 0.0248
-13.250 -1.1104 0.04757 0.04102 -0.0117 1.0005 0.0258
-13.000 -1.1063 0.04524 0.03868 -0.0117 1.0005 0.0270
-12.750 -1.1021 0.04288 0.03619 -0.0114 1.0005 0.0288
-12.500 -1.0966 0.04071 0.03402 -0.0114 1.0005 0.0307
-12.250 -1.0901 0.03863 0.03185 -0.0113 1.0005 0.0333
-12.000 -1.0812 0.03678 0.02985 -0.0112 1.0005 0.0361
-11.750 -1.0730 0.03498 0.02804 -0.0110 1.0005 0.0385
-11.500 -1.0630 0.03332 0.02629 -0.0107 1.0005 0.0410
-11.250 -1.0521 0.03179 0.02471 -0.0105 1.0005 0.0433
-11.000 -1.0408 0.03031 0.02319 -0.0102 1.0005 0.0456
-10.750 -1.0279 0.02900 0.02182 -0.0099 1.0005 0.0481
-10.500 -1.0152 0.02769 0.02049 -0.0095 1.0005 0.0504
-10.250 -1.0004 0.02661 0.01935 -0.0091 1.0005 0.0535
-10.000 -0.9861 0.02553 0.01827 -0.0087 1.0005 0.0567
-9.750 -0.9712 0.02454 0.01723 -0.0080 1.0005 0.0605
-9.500 -0.9554 0.02362 0.01627 -0.0072 1.0005 0.0651
-9.250 -0.9395 0.02257 0.01525 -0.0066 1.0005 0.0705
-9.000 -0.9230 0.02151 0.01423 -0.0061 1.0005 0.0772
-8.750 -0.9048 0.02053 0.01329 -0.0056 1.0005 0.0854
-8.500 -0.8846 0.01965 0.01247 -0.0055 1.0005 0.0956
-8.250 -0.8632 0.01880 0.01171 -0.0057 1.0005 0.1074
-8.000 -0.8373 0.01804 0.01103 -0.0068 0.9804 0.1220
-7.750 -0.8003 0.01726 0.01027 -0.0098 0.9369 0.1429
-7.500 -0.7774 0.01666 0.00965 -0.0096 0.9074 0.1651
-7.250 -0.7593 0.01586 0.00900 -0.0086 0.8866 0.1933
-7.000 -0.7411 0.01503 0.00836 -0.0077 0.8705 0.2375
-6.750 -0.7219 0.01427 0.00779 -0.0069 0.8569 0.2974
-6.500 -0.7023 0.01358 0.00732 -0.0059 0.8452 0.3497
-6.250 -0.6805 0.01315 0.00709 -0.0051 0.8341 0.4088
-6.000 -0.6562 0.01298 0.00701 -0.0046 0.8247 0.4535
-5.750 -0.6308 0.01296 0.00700 -0.0041 0.8164 0.4852
-5.500 -0.6042 0.01310 0.00714 -0.0036 0.8092 0.5087
-5.250 -0.5767 0.01324 0.00721 -0.0034 0.8019 0.5278
-5.000 -0.5497 0.01340 0.00724 -0.0031 0.7959 0.5435
-4.750 -0.5221 0.01356 0.00727 -0.0031 0.7898 0.5585
-4.500 -0.4944 0.01376 0.00748 -0.0027 0.7835 0.5706
-4.250 -0.4671 0.01395 0.00760 -0.0023 0.7781 0.5820
-4.000 -0.4395 0.01417 0.00773 -0.0021 0.7727 0.5940
-3.750 -0.4114 0.01442 0.00802 -0.0018 0.7673 0.6033
-3.500 -0.3840 0.01461 0.00808 -0.0016 0.7626 0.6148
-3.250 -0.3562 0.01481 0.00829 -0.0011 0.7586 0.6217
-3.000 -0.3280 0.01489 0.00831 -0.0013 0.7536 0.6301
-2.750 -0.3000 0.01490 0.00830 -0.0013 0.7483 0.6363
-2.500 -0.2722 0.01498 0.00834 -0.0011 0.7437 0.6426
-2.250 -0.2447 0.01506 0.00827 -0.0011 0.7400 0.6510
-2.000 -0.2164 0.01507 0.00837 -0.0011 0.7353 0.6562
-1.750 -0.1882 0.01509 0.00839 -0.0012 0.7305 0.6616
-1.500 -0.1602 0.01505 0.00826 -0.0014 0.7260 0.6676
-1.250 -0.1324 0.01502 0.00818 -0.0014 0.7221 0.6722
-1.000 -0.1042 0.01507 0.00829 -0.0015 0.7175 0.6767
-0.750 -0.0759 0.01509 0.00831 -0.0017 0.7124 0.6822
-0.500 -0.0478 0.01506 0.00822 -0.0019 0.7077 0.6884
-0.250 -0.0203 0.01508 0.00825 -0.0015 0.7038 0.6926
0.000 0.0076 0.01514 0.00836 -0.0016 0.6984 0.6978
0.250 0.0358 0.01514 0.00834 -0.0018 0.6925 0.7041
0.500 0.0634 0.01507 0.00826 -0.0017 0.6876 0.7088
0.750 0.0911 0.01510 0.00829 -0.0015 0.6832 0.7130
1.000 0.1193 0.01511 0.00836 -0.0018 0.6771 0.7174
1.250 0.1477 0.01508 0.00830 -0.0020 0.6717 0.7223
1.500 0.1759 0.01503 0.00822 -0.0020 0.6674 0.7262
1.750 0.2035 0.01506 0.00835 -0.0021 0.6614 0.7300
2.000 0.2313 0.01505 0.00838 -0.0021 0.6548 0.7347
2.250 0.2595 0.01500 0.00828 -0.0020 0.6492 0.7400
2.500 0.2872 0.01498 0.00832 -0.0021 0.6421 0.7443
2.750 0.3148 0.01491 0.00833 -0.0020 0.6349 0.7482
3.000 0.3429 0.01483 0.00823 -0.0018 0.6292 0.7529
3.250 0.3706 0.01480 0.00830 -0.0019 0.6205 0.7583
3.500 0.3985 0.01460 0.00812 -0.0016 0.6128 0.7630
3.750 0.4256 0.01444 0.00805 -0.0013 0.6029 0.7675
4.000 0.4536 0.01416 0.00776 -0.0009 0.5927 0.7726
4.250 0.4812 0.01397 0.00763 -0.0008 0.5803 0.7782
4.500 0.5086 0.01374 0.00742 -0.0003 0.5697 0.7828
4.750 0.5356 0.01356 0.00734 0.0001 0.5560 0.7886
5.000 0.5630 0.01342 0.00728 0.0002 0.5412 0.7956
5.250 0.5896 0.01324 0.00722 0.0007 0.5246 0.8016
5.500 0.6162 0.01308 0.00713 0.0011 0.5037 0.8090
5.750 0.6424 0.01298 0.00699 0.0016 0.4788 0.8165
6.000 0.6671 0.01302 0.00706 0.0022 0.4471 0.8243
6.250 0.6908 0.01322 0.00716 0.0029 0.4025 0.8342
6.500 0.7109 0.01369 0.00740 0.0040 0.3430 0.8446
6.750 0.7294 0.01442 0.00790 0.0051 0.2891 0.8559
7.000 0.7472 0.01521 0.00846 0.0062 0.2297 0.8694
7.250 0.7643 0.01599 0.00909 0.0074 0.1888 0.8856
7.500 0.7814 0.01669 0.00971 0.0087 0.1635 0.9060
7.750 0.8015 0.01736 0.01035 0.0094 0.1429 0.9340
8.000 0.8366 0.01806 0.01106 0.0069 0.1222 0.9732
8.250 0.8642 0.01887 0.01177 0.0054 0.1075 0.9995
8.500 0.8859 0.01964 0.01249 0.0052 0.0954 0.9995
8.750 0.9055 0.02051 0.01330 0.0055 0.0853 0.9995
9.000 0.9228 0.02149 0.01423 0.0061 0.0772 0.9995
9.250 0.9387 0.02252 0.01524 0.0068 0.0706 0.9995
9.500 0.9540 0.02353 0.01623 0.0075 0.0649 0.9995
9.750 0.9680 0.02448 0.01718 0.0085 0.0603 0.9995
10.000 0.9830 0.02544 0.01817 0.0091 0.0563 0.9995
10.250 0.9975 0.02650 0.01928 0.0096 0.0530 0.9995
10.500 1.0103 0.02770 0.02047 0.0100 0.0504 0.9995
10.750 1.0237 0.02893 0.02179 0.0105 0.0480 0.9995
11.000 1.0351 0.03032 0.02319 0.0109 0.0460 0.9995
11.250 1.0468 0.03174 0.02469 0.0113 0.0435 0.9995
11.500 1.0564 0.03332 0.02626 0.0116 0.0413 0.9995
11.750 1.0668 0.03490 0.02796 0.0120 0.0388 0.9995
12.000 1.0743 0.03669 0.02976 0.0123 0.0366 0.9995
12.250 1.0829 0.03848 0.03169 0.0125 0.0339 0.9995
12.500 1.0892 0.04049 0.03380 0.0128 0.0314 0.9995
12.750 1.0943 0.04261 0.03593 0.0128 0.0295 0.9995
13.000 1.0985 0.04491 0.03836 0.0132 0.0276 0.9995
13.250 1.1023 0.04719 0.04065 0.0133 0.0264 0.9995
13.500 1.1050 0.04965 0.04319 0.0137 0.0253 0.9995
13.750 1.1078 0.05214 0.04579 0.0139 0.0244 0.9995
14.000 1.1112 0.05455 0.04823 0.0141 0.0237 0.9995
14.250 1.1170 0.05668 0.05031 0.0147 0.0231 0.9995
14.500 1.1177 0.05961 0.05342 0.0148 0.0226 0.9995
14.750 1.1163 0.06280 0.05681 0.0147 0.0222 0.9995
15.000 1.1140 0.06617 0.06036 0.0144 0.0219 0.9995
15.250 1.1102 0.06980 0.06416 0.0138 0.0216 0.9995
15.500 1.1049 0.07374 0.06827 0.0129 0.0214 0.9995
15.750 1.0978 0.07808 0.07279 0.0116 0.0212 0.9995
16.000 1.0880 0.08295 0.07785 0.0099 0.0211 0.9995
16.250 1.0750 0.08855 0.08367 0.0075 0.0211 0.9995
16.500 1.0572 0.09524 0.09060 0.0041 0.0211 0.9995
16.750 1.0328 0.10358 0.09921 -0.0006 0.0212 0.9995
17.000 1.0019 0.11389 0.10981 -0.0069 0.0215 0.9995
17.250 0.9657 0.12623 0.12243 -0.0148 0.0220 0.9995
17.500 0.9260 0.14058 0.13699 -0.0241 0.0225 0.9995
17.750 0.8931 0.15421 0.15074 -0.0324 0.0230 0.9995
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