WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Reynolds number: 1,000,000 Max Cl/Cd: 66.75 at α=9.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fxlv152-il-1000000.txt Download as CSV file: xf-fxlv152-il-1000000.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 = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.500 -1.1881 0.11424 0.11098 0.0221 1.0005 0.0054
-18.250 -1.2023 0.10759 0.10422 0.0188 1.0005 0.0054
-18.000 -1.2175 0.10084 0.09736 0.0156 1.0005 0.0054
-17.750 -1.2317 0.09441 0.09081 0.0126 1.0005 0.0054
-17.500 -1.2448 0.08832 0.08460 0.0098 1.0005 0.0055
-17.250 -1.2572 0.08247 0.07864 0.0072 1.0005 0.0055
-17.000 -1.2682 0.07703 0.07309 0.0050 1.0005 0.0055
-16.750 -1.2776 0.07197 0.06792 0.0030 1.0005 0.0055
-16.500 -1.2863 0.06718 0.06302 0.0012 1.0005 0.0055
-16.250 -1.2935 0.06273 0.05847 -0.0004 1.0005 0.0056
-16.000 -1.2992 0.05862 0.05426 -0.0017 1.0005 0.0056
-15.750 -1.3041 0.05481 0.05035 -0.0027 1.0005 0.0056
-15.500 -1.3076 0.05133 0.04677 -0.0035 1.0005 0.0057
-15.250 -1.3105 0.04809 0.04344 -0.0041 1.0005 0.0057
-15.000 -1.3121 0.04505 0.04031 -0.0045 1.0005 0.0057
-14.750 -1.3122 0.04221 0.03738 -0.0049 1.0005 0.0058
-14.500 -1.3109 0.03958 0.03466 -0.0051 1.0005 0.0058
-14.250 -1.3081 0.03714 0.03214 -0.0052 1.0005 0.0059
-14.000 -1.3037 0.03488 0.02980 -0.0053 1.0005 0.0060
-13.750 -1.2981 0.03275 0.02760 -0.0053 1.0005 0.0060
-13.500 -1.2911 0.03080 0.02556 -0.0053 1.0005 0.0061
-13.250 -1.2828 0.02899 0.02368 -0.0052 1.0005 0.0062
-13.000 -1.2732 0.02733 0.02195 -0.0050 1.0005 0.0062
-12.750 -1.2624 0.02579 0.02034 -0.0049 1.0005 0.0063
-12.500 -1.2508 0.02438 0.01886 -0.0046 1.0005 0.0063
-12.250 -1.2383 0.02309 0.01751 -0.0043 1.0005 0.0064
-12.000 -1.2249 0.02194 0.01630 -0.0039 1.0005 0.0064
-11.750 -1.2116 0.02086 0.01516 -0.0033 1.0005 0.0065
-11.500 -1.1972 0.01993 0.01416 -0.0024 1.0005 0.0066
-11.250 -1.1807 0.01912 0.01330 -0.0016 1.0005 0.0067
-11.000 -1.1617 0.01838 0.01252 -0.0010 1.0005 0.0069
-10.750 -1.1413 0.01770 0.01181 -0.0006 1.0005 0.0071
-10.500 -1.1142 0.01712 0.01114 -0.0013 0.9340 0.0072
-10.250 -1.0955 0.01676 0.01056 -0.0001 0.8667 0.0074
-10.000 -1.0742 0.01632 0.00997 0.0006 0.8357 0.0076
-9.750 -1.0517 0.01588 0.00943 0.0010 0.8108 0.0080
-9.500 -1.0285 0.01543 0.00894 0.0014 0.7876 0.0094
-9.250 -1.0038 0.01512 0.00857 0.0015 0.7700 0.0138
-9.000 -0.9785 0.01486 0.00824 0.0017 0.7578 0.0151
-8.750 -0.9527 0.01459 0.00792 0.0017 0.7481 0.0161
-8.500 -0.9265 0.01438 0.00764 0.0017 0.7389 0.0169
-8.250 -0.9009 0.01401 0.00725 0.0018 0.7304 0.0178
-8.000 -0.8751 0.01370 0.00689 0.0018 0.7221 0.0187
-7.750 -0.8485 0.01342 0.00658 0.0018 0.7147 0.0194
-7.500 -0.8221 0.01312 0.00624 0.0018 0.7068 0.0202
-7.250 -0.7958 0.01280 0.00588 0.0018 0.6999 0.0212
-7.000 -0.7691 0.01251 0.00555 0.0017 0.6933 0.0222
-6.750 -0.7423 0.01225 0.00526 0.0017 0.6870 0.0232
-6.500 -0.7154 0.01197 0.00496 0.0016 0.6815 0.0250
-6.250 -0.6889 0.01161 0.00465 0.0016 0.6765 0.0356
-6.000 -0.6622 0.01131 0.00436 0.0015 0.6716 0.0444
-5.750 -0.6360 0.01094 0.00406 0.0015 0.6664 0.0648
-5.500 -0.6088 0.01063 0.00381 0.0014 0.6631 0.0767
-5.250 -0.5822 0.01021 0.00353 0.0013 0.6597 0.1022
-5.000 -0.5555 0.00983 0.00328 0.0012 0.6562 0.1307
-4.750 -0.5286 0.00948 0.00304 0.0011 0.6526 0.1582
-4.500 -0.5021 0.00910 0.00278 0.0010 0.6487 0.1919
-4.250 -0.4763 0.00854 0.00249 0.0010 0.6456 0.2525
-4.000 -0.4494 0.00812 0.00226 0.0009 0.6425 0.3024
-3.750 -0.4234 0.00757 0.00199 0.0009 0.6393 0.3649
-3.500 -0.3967 0.00717 0.00182 0.0008 0.6359 0.4273
-3.250 -0.3686 0.00701 0.00173 0.0007 0.6326 0.4552
-3.000 -0.3402 0.00692 0.00166 0.0005 0.6290 0.4738
-2.750 -0.3114 0.00680 0.00161 0.0003 0.6267 0.4909
-2.500 -0.2826 0.00672 0.00158 0.0001 0.6242 0.5100
-2.250 -0.2534 0.00667 0.00157 -0.0001 0.6211 0.5257
-2.000 -0.2240 0.00667 0.00156 -0.0004 0.6179 0.5377
-1.750 -0.1950 0.00665 0.00155 -0.0005 0.6141 0.5483
-1.500 -0.1658 0.00671 0.00155 -0.0008 0.6097 0.5567
-1.250 -0.1366 0.00666 0.00153 -0.0010 0.6071 0.5631
-1.000 -0.1073 0.00664 0.00153 -0.0013 0.6043 0.5690
-0.750 -0.0778 0.00666 0.00153 -0.0015 0.6011 0.5758
-0.500 -0.0488 0.00662 0.00153 -0.0017 0.5976 0.5826
-0.250 -0.0197 0.00664 0.00153 -0.0019 0.5942 0.5877
0.000 0.0095 0.00668 0.00155 -0.0021 0.5902 0.5914
0.250 0.0391 0.00667 0.00154 -0.0024 0.5863 0.5945
0.500 0.0684 0.00664 0.00152 -0.0027 0.5809 0.5979
0.750 0.0972 0.00665 0.00152 -0.0028 0.5746 0.6016
1.000 0.1264 0.00666 0.00155 -0.0030 0.5690 0.6055
1.250 0.1558 0.00665 0.00155 -0.0033 0.5620 0.6094
1.500 0.1847 0.00671 0.00156 -0.0034 0.5529 0.6125
1.750 0.2143 0.00669 0.00156 -0.0037 0.5448 0.6148
2.000 0.2432 0.00669 0.00155 -0.0039 0.5343 0.6180
2.250 0.2724 0.00668 0.00157 -0.0041 0.5225 0.6209
2.500 0.3013 0.00671 0.00159 -0.0043 0.5083 0.6239
2.750 0.3299 0.00681 0.00162 -0.0045 0.4877 0.6270
3.000 0.3584 0.00693 0.00168 -0.0046 0.4710 0.6299
3.250 0.3869 0.00706 0.00176 -0.0048 0.4545 0.6322
3.500 0.4147 0.00721 0.00185 -0.0048 0.4243 0.6352
3.750 0.4395 0.00777 0.00207 -0.0046 0.3410 0.6387
4.000 0.4653 0.00824 0.00233 -0.0045 0.2897 0.6423
4.250 0.4909 0.00875 0.00259 -0.0044 0.2281 0.6459
4.500 0.5161 0.00932 0.00290 -0.0043 0.1723 0.6491
4.750 0.5431 0.00965 0.00313 -0.0044 0.1476 0.6519
5.000 0.5693 0.00997 0.00336 -0.0044 0.1203 0.6561
5.500 0.6215 0.01073 0.00389 -0.0043 0.0714 0.6637
5.750 0.6483 0.01103 0.00414 -0.0043 0.0577 0.6673
6.000 0.6742 0.01143 0.00445 -0.0042 0.0407 0.6711
6.250 0.7006 0.01170 0.00472 -0.0042 0.0318 0.6763
6.500 0.7264 0.01206 0.00504 -0.0041 0.0241 0.6813
6.750 0.7531 0.01232 0.00532 -0.0041 0.0226 0.6864
7.000 0.7795 0.01258 0.00563 -0.0040 0.0216 0.6929
7.250 0.8055 0.01290 0.00598 -0.0039 0.0206 0.7002
7.500 0.8317 0.01318 0.00630 -0.0039 0.0197 0.7074
7.750 0.8578 0.01345 0.00662 -0.0038 0.0189 0.7154
8.000 0.8833 0.01380 0.00699 -0.0037 0.0179 0.7233
8.250 0.9089 0.01408 0.00733 -0.0036 0.0171 0.7310
8.500 0.9350 0.01432 0.00760 -0.0035 0.0161 0.7393
8.750 0.9603 0.01461 0.00793 -0.0034 0.0151 0.7475
9.000 0.9857 0.01487 0.00824 -0.0032 0.0142 0.7570
9.250 1.0106 0.01514 0.00858 -0.0030 0.0099 0.7685
9.500 1.0334 0.01559 0.00904 -0.0026 0.0081 0.7844
9.750 1.0561 0.01603 0.00957 -0.0022 0.0077 0.8068
10.000 1.0782 0.01648 0.01012 -0.0016 0.0074 0.8310
10.250 1.0990 0.01690 0.01069 -0.0009 0.0072 0.8607
10.500 1.1162 0.01725 0.01125 0.0007 0.0071 0.9234
10.750 1.1415 0.01780 0.01192 0.0003 0.0069 0.9995
11.000 1.1611 0.01847 0.01262 0.0009 0.0067 0.9995
11.250 1.1789 0.01919 0.01338 0.0017 0.0066 0.9995
11.500 1.1947 0.01996 0.01421 0.0027 0.0065 0.9995
11.750 1.2094 0.02086 0.01516 0.0035 0.0065 0.9995
12.000 1.2232 0.02188 0.01624 0.0041 0.0065 0.9995
12.250 1.2364 0.02303 0.01745 0.0046 0.0064 0.9995
12.500 1.2487 0.02429 0.01878 0.0050 0.0064 0.9995
12.750 1.2602 0.02568 0.02023 0.0053 0.0064 0.9995
13.000 1.2708 0.02719 0.02180 0.0055 0.0063 0.9995
13.250 1.2801 0.02881 0.02350 0.0058 0.0063 0.9995
13.500 1.2884 0.03055 0.02531 0.0060 0.0063 0.9995
13.750 1.2953 0.03244 0.02727 0.0061 0.0063 0.9995
14.000 1.3009 0.03447 0.02938 0.0062 0.0062 0.9995
14.250 1.3052 0.03664 0.03163 0.0063 0.0062 0.9995
14.500 1.3082 0.03895 0.03402 0.0064 0.0062 0.9995
14.750 1.3097 0.04145 0.03660 0.0063 0.0061 0.9995
15.000 1.3099 0.04411 0.03935 0.0062 0.0061 0.9995
15.250 1.3088 0.04696 0.04229 0.0060 0.0061 0.9995
15.500 1.3060 0.05003 0.04545 0.0056 0.0061 0.9995
15.750 1.3023 0.05333 0.04885 0.0051 0.0060 0.9995
16.000 1.2981 0.05686 0.05248 0.0043 0.0060 0.9995
16.250 1.2928 0.06068 0.05639 0.0034 0.0060 0.9995
16.500 1.2864 0.06478 0.06059 0.0021 0.0060 0.9995
16.750 1.2787 0.06917 0.06509 0.0007 0.0060 0.9995
17.000 1.2700 0.07384 0.06987 -0.0009 0.0060 0.9995
17.250 1.2598 0.07885 0.07498 -0.0027 0.0059 0.9995
17.500 1.2479 0.08426 0.08050 -0.0049 0.0059 0.9995
17.750 1.2350 0.08999 0.08635 -0.0072 0.0059 0.9995
18.000 1.2212 0.09596 0.09243 -0.0098 0.0059 0.9995
18.250 1.2059 0.10235 0.09893 -0.0126 0.0059 0.9995
18.500 1.1904 0.10888 0.10558 -0.0156 0.0059 0.9995
18.750 1.1748 0.11549 0.11230 -0.0188 0.0059 0.9995
19.000 1.1595 0.12224 0.11915 -0.0221 0.0059 0.9995
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