WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Xfoil prediction polar at RE=50,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Reynolds number: 50,000 Max Cl/Cd: 27.39 at α=7.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fxlv152-il-50000-n5.txt Download as CSV file: xf-fxlv152-il-50000-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 = 0.050 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-14.250 -0.8270 0.11458 0.10780 0.0031 1.0005 0.0716
-14.000 -0.8625 0.10276 0.09588 -0.0040 1.0005 0.0706
-13.750 -0.8991 0.09231 0.08526 -0.0102 1.0005 0.0695
-13.500 -0.9301 0.08392 0.07662 -0.0146 1.0005 0.0691
-13.250 -0.9526 0.07743 0.06988 -0.0175 1.0005 0.0696
-13.000 -0.9718 0.07181 0.06396 -0.0196 1.0005 0.0706
-12.750 -0.9897 0.06663 0.05840 -0.0210 1.0005 0.0719
-12.500 -0.9825 0.06423 0.05600 -0.0210 1.0005 0.0746
-12.250 -0.9839 0.06079 0.05232 -0.0213 1.0005 0.0769
-12.000 -0.9864 0.05709 0.04820 -0.0213 1.0005 0.0792
-11.750 -0.9694 0.05522 0.04637 -0.0209 1.0005 0.0822
-11.500 -0.9617 0.05258 0.04344 -0.0206 1.0005 0.0860
-11.250 -0.9471 0.05071 0.04154 -0.0201 1.0005 0.0901
-11.000 -0.9340 0.04851 0.03905 -0.0196 1.0005 0.0953
-10.750 -0.9158 0.04699 0.03758 -0.0190 1.0005 0.1003
-10.500 -0.8980 0.04535 0.03579 -0.0184 1.0005 0.1064
-10.250 -0.8828 0.04373 0.03403 -0.0179 1.0005 0.1138
-10.000 -0.8702 0.04214 0.03247 -0.0174 1.0005 0.1220
-9.750 -0.8591 0.04051 0.03082 -0.0170 1.0005 0.1320
-9.500 -0.8474 0.03892 0.02922 -0.0164 1.0005 0.1434
-9.250 -0.8349 0.03738 0.02768 -0.0157 1.0005 0.1559
-9.000 -0.8221 0.03588 0.02623 -0.0149 1.0005 0.1690
-8.750 -0.8106 0.03441 0.02484 -0.0139 1.0005 0.1831
-8.500 -0.7993 0.03293 0.02349 -0.0130 1.0005 0.1995
-8.250 -0.7885 0.03145 0.02214 -0.0120 1.0005 0.2207
-8.000 -0.7784 0.03001 0.02094 -0.0110 1.0005 0.2462
-7.750 -0.7677 0.02867 0.01979 -0.0099 1.0005 0.2805
-7.500 -0.7554 0.02756 0.01898 -0.0086 1.0005 0.3188
-7.250 -0.7393 0.02702 0.01882 -0.0070 1.0005 0.3604
-7.000 -0.7205 0.02693 0.01890 -0.0056 1.0005 0.4020
-6.750 -0.7022 0.02700 0.01903 -0.0041 1.0005 0.4374
-6.500 -0.6894 0.02703 0.01904 -0.0022 1.0005 0.4674
-6.250 -0.6639 0.02773 0.01969 -0.0014 0.9852 0.4938
-6.000 -0.6283 0.02811 0.01981 -0.0032 0.9642 0.5221
-5.250 -0.5225 0.02911 0.02014 -0.0067 0.9221 0.5779
-5.000 -0.4897 0.02970 0.02058 -0.0065 0.9104 0.5912
-4.750 -0.4577 0.03017 0.02090 -0.0063 0.9000 0.6043
-4.500 -0.4321 0.03024 0.02079 -0.0058 0.8881 0.6182
-4.250 -0.4086 0.03013 0.02050 -0.0054 0.8767 0.6313
-4.000 -0.3794 0.03023 0.02048 -0.0049 0.8677 0.6391
-3.750 -0.3591 0.02981 0.01988 -0.0046 0.8571 0.6499
-3.500 -0.3318 0.02970 0.01963 -0.0043 0.8496 0.6560
-3.250 -0.3079 0.02953 0.01935 -0.0040 0.8405 0.6635
-3.000 -0.2852 0.02921 0.01890 -0.0037 0.8330 0.6721
-2.750 -0.2591 0.02921 0.01881 -0.0033 0.8258 0.6785
-2.500 -0.2382 0.02890 0.01839 -0.0031 0.8185 0.6885
-2.250 -0.2104 0.02898 0.01841 -0.0025 0.8130 0.6946
-2.000 -0.1897 0.02881 0.01818 -0.0022 0.8050 0.7048
-1.750 -0.1640 0.02883 0.01814 -0.0016 0.7986 0.7115
-1.500 -0.1400 0.02871 0.01797 -0.0013 0.7930 0.7193
-1.250 -0.1185 0.02853 0.01774 -0.0013 0.7858 0.7263
-1.000 -0.0927 0.02846 0.01764 -0.0010 0.7800 0.7313
-0.750 -0.0690 0.02833 0.01745 -0.0009 0.7743 0.7381
-0.500 -0.0462 0.02825 0.01736 -0.0010 0.7674 0.7446
-0.250 -0.0199 0.02824 0.01735 -0.0008 0.7619 0.7495
0.000 0.0053 0.02817 0.01725 -0.0008 0.7570 0.7556
0.250 0.0272 0.02822 0.01731 -0.0008 0.7495 0.7622
0.500 0.0533 0.02828 0.01740 -0.0006 0.7439 0.7673
0.750 0.0795 0.02828 0.01740 -0.0006 0.7396 0.7734
1.000 0.0999 0.02848 0.01766 -0.0006 0.7317 0.7800
1.250 0.1250 0.02860 0.01783 -0.0003 0.7257 0.7855
1.500 0.1501 0.02864 0.01789 0.0000 0.7205 0.7922
1.750 0.1703 0.02888 0.01821 0.0002 0.7113 0.7988
2.000 0.1969 0.02884 0.01823 0.0007 0.7045 0.8043
2.250 0.2175 0.02902 0.01848 0.0012 0.6944 0.8118
2.500 0.2433 0.02900 0.01852 0.0017 0.6872 0.8182
2.750 0.2659 0.02922 0.01884 0.0022 0.6788 0.8253
3.000 0.2893 0.02937 0.01909 0.0025 0.6712 0.8332
3.250 0.3180 0.02933 0.01914 0.0029 0.6660 0.8396
3.500 0.3361 0.02985 0.01980 0.0032 0.6554 0.8488
3.750 0.3640 0.02985 0.01994 0.0036 0.6491 0.8564
4.000 0.3835 0.03032 0.02058 0.0040 0.6384 0.8668
4.250 0.4126 0.03022 0.02063 0.0044 0.6305 0.8757
4.500 0.4340 0.03042 0.02100 0.0051 0.6170 0.8875
4.750 0.4632 0.03012 0.02085 0.0056 0.6047 0.8982
5.000 0.4955 0.02958 0.02046 0.0059 0.5920 0.9089
5.250 0.5233 0.02939 0.02046 0.0060 0.5758 0.9216
5.500 0.5563 0.02911 0.02039 0.0052 0.5592 0.9336
5.750 0.5916 0.02881 0.02032 0.0041 0.5414 0.9462
6.000 0.6283 0.02836 0.02010 0.0027 0.5202 0.9616
6.250 0.6671 0.02756 0.01949 0.0013 0.4946 0.9798
6.500 0.6936 0.02715 0.01920 0.0013 0.4647 0.9995
6.750 0.7065 0.02693 0.01896 0.0036 0.4362 0.9995
7.000 0.7236 0.02684 0.01881 0.0053 0.4013 0.9995
7.250 0.7406 0.02704 0.01884 0.0068 0.3597 0.9995
7.500 0.7557 0.02760 0.01906 0.0085 0.3185 0.9995
7.750 0.7672 0.02869 0.01987 0.0099 0.2805 0.9995
8.000 0.7772 0.03000 0.02097 0.0112 0.2470 0.9995
8.250 0.7860 0.03143 0.02214 0.0124 0.2220 0.9995
8.500 0.7956 0.03291 0.02343 0.0135 0.2015 0.9995
8.750 0.8059 0.03434 0.02475 0.0146 0.1851 0.9995
9.000 0.8166 0.03580 0.02610 0.0157 0.1712 0.9995
9.250 0.8292 0.03728 0.02755 0.0166 0.1577 0.9995
9.500 0.8412 0.03882 0.02908 0.0174 0.1450 0.9995
9.750 0.8527 0.04040 0.03071 0.0180 0.1335 0.9995
10.000 0.8633 0.04204 0.03239 0.0185 0.1231 0.9995
10.250 0.8754 0.04365 0.03404 0.0190 0.1146 0.9995
10.500 0.8904 0.04513 0.03547 0.0196 0.1080 0.9995
10.750 0.9071 0.04681 0.03738 0.0203 0.1014 0.9995
11.000 0.9231 0.04852 0.03918 0.0210 0.0960 0.9995
11.250 0.9372 0.05033 0.04108 0.0215 0.0910 0.9995
11.500 0.9485 0.05254 0.04348 0.0220 0.0867 0.9995
11.750 0.9607 0.05463 0.04569 0.0225 0.0830 0.9995
12.000 0.9711 0.05717 0.04841 0.0229 0.0802 0.9995
12.250 0.9729 0.06043 0.05197 0.0231 0.0778 0.9995
12.500 0.9785 0.06307 0.05471 0.0232 0.0753 0.9995
12.750 0.9743 0.06661 0.05845 0.0229 0.0732 0.9995
13.000 0.9586 0.07146 0.06362 0.0216 0.0719 0.9995
13.250 0.9429 0.07649 0.06890 0.0200 0.0705 0.9995
13.500 0.9502 0.07853 0.07087 0.0198 0.0674 0.9995
13.750 0.9251 0.08522 0.07784 0.0169 0.0672 0.9995
14.000 0.8979 0.09280 0.08564 0.0131 0.0672 0.9995
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