WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Reynolds number: 100,000 Max Cl/Cd: 38.24 at α=6.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fxlv152-il-100000-n5.txt Download as CSV file: xf-fxlv152-il-100000-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 = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-16.750 -0.8423 0.15607 0.15128 0.0368 1.0005 0.0246
-16.500 -0.9297 0.12703 0.12183 0.0206 1.0005 0.0232
-16.250 -0.9487 0.11809 0.11273 0.0154 1.0005 0.0233
-16.000 -0.9649 0.11016 0.10464 0.0109 1.0005 0.0235
-15.750 -0.9793 0.10291 0.09722 0.0068 1.0005 0.0238
-15.500 -0.9926 0.09620 0.09035 0.0032 1.0005 0.0242
-15.250 -1.0049 0.08992 0.08388 0.0001 1.0005 0.0249
-15.000 -1.0156 0.08421 0.07799 -0.0026 1.0005 0.0256
-14.750 -1.0231 0.07930 0.07298 -0.0050 1.0005 0.0262
-14.500 -1.0300 0.07466 0.06822 -0.0071 1.0005 0.0271
-14.250 -1.0360 0.07032 0.06368 -0.0087 1.0005 0.0284
-14.000 -1.0403 0.06650 0.05974 -0.0101 1.0005 0.0295
-13.750 -1.0430 0.06295 0.05604 -0.0112 1.0005 0.0309
-13.500 -1.0439 0.05966 0.05258 -0.0120 1.0005 0.0327
-13.250 -1.0437 0.05665 0.04944 -0.0128 1.0005 0.0345
-13.000 -1.0415 0.05386 0.04648 -0.0133 1.0005 0.0366
-12.750 -1.0386 0.05128 0.04379 -0.0137 1.0005 0.0384
-12.500 -1.0333 0.04894 0.04128 -0.0137 1.0005 0.0403
-12.250 -1.0283 0.04667 0.03895 -0.0139 1.0005 0.0419
-12.000 -1.0210 0.04461 0.03674 -0.0138 1.0005 0.0440
-11.750 -1.0139 0.04261 0.03470 -0.0138 1.0005 0.0459
-11.500 -1.0049 0.04079 0.03277 -0.0137 1.0005 0.0485
-11.250 -0.9959 0.03903 0.03096 -0.0136 1.0005 0.0508
-11.000 -0.9852 0.03740 0.02922 -0.0133 1.0005 0.0535
-10.750 -0.9748 0.03580 0.02756 -0.0131 1.0005 0.0561
-10.500 -0.9627 0.03435 0.02600 -0.0127 1.0005 0.0597
-10.250 -0.9515 0.03289 0.02450 -0.0124 1.0005 0.0636
-10.000 -0.9397 0.03151 0.02307 -0.0120 1.0005 0.0685
-9.750 -0.9277 0.03019 0.02173 -0.0115 1.0005 0.0741
-9.500 -0.9154 0.02898 0.02051 -0.0108 1.0005 0.0806
-9.250 -0.9022 0.02788 0.01942 -0.0100 1.0005 0.0879
-9.000 -0.8866 0.02683 0.01837 -0.0095 1.0005 0.0960
-8.750 -0.8698 0.02585 0.01738 -0.0090 1.0005 0.1049
-8.500 -0.8524 0.02489 0.01645 -0.0085 1.0005 0.1153
-8.250 -0.8341 0.02397 0.01556 -0.0082 1.0005 0.1270
-8.000 -0.8152 0.02308 0.01471 -0.0079 1.0005 0.1404
-7.500 -0.7633 0.02130 0.01296 -0.0100 0.9213 0.1783
-7.250 -0.7421 0.02041 0.01219 -0.0100 0.8949 0.2066
-7.000 -0.7237 0.01952 0.01147 -0.0093 0.8745 0.2461
-6.750 -0.7053 0.01872 0.01082 -0.0085 0.8587 0.3003
-6.500 -0.6869 0.01803 0.01039 -0.0073 0.8458 0.3522
-6.250 -0.6658 0.01769 0.01026 -0.0063 0.8339 0.4064
-6.000 -0.6418 0.01756 0.01012 -0.0057 0.8239 0.4457
-5.750 -0.6168 0.01756 0.01009 -0.0050 0.8152 0.4721
-5.500 -0.5908 0.01764 0.01014 -0.0044 0.8063 0.4938
-5.250 -0.5650 0.01775 0.01013 -0.0039 0.7975 0.5148
-5.000 -0.5389 0.01785 0.01009 -0.0034 0.7889 0.5337
-4.750 -0.5126 0.01797 0.01009 -0.0029 0.7807 0.5490
-4.500 -0.4863 0.01802 0.00998 -0.0025 0.7742 0.5619
-4.250 -0.4594 0.01808 0.00993 -0.0023 0.7675 0.5736
-4.000 -0.4324 0.01820 0.00997 -0.0018 0.7620 0.5829
-3.750 -0.4060 0.01824 0.00985 -0.0015 0.7574 0.5940
-3.500 -0.3782 0.01839 0.01000 -0.0013 0.7516 0.6021
-3.250 -0.3511 0.01840 0.00988 -0.0012 0.7462 0.6120
-3.000 -0.3239 0.01844 0.00985 -0.0009 0.7415 0.6185
-2.750 -0.2962 0.01842 0.00976 -0.0009 0.7363 0.6242
-2.500 -0.2687 0.01830 0.00952 -0.0012 0.7306 0.6307
-2.250 -0.2412 0.01824 0.00940 -0.0012 0.7259 0.6355
-2.000 -0.2137 0.01824 0.00935 -0.0010 0.7221 0.6405
-1.750 -0.1862 0.01822 0.00927 -0.0012 0.7170 0.6482
-1.500 -0.1589 0.01823 0.00929 -0.0012 0.7117 0.6549
-1.250 -0.1317 0.01826 0.00930 -0.0009 0.7070 0.6610
-1.000 -0.1043 0.01821 0.00916 -0.0009 0.7033 0.6674
-0.750 -0.0765 0.01819 0.00916 -0.0012 0.6985 0.6720
-0.500 -0.0488 0.01821 0.00920 -0.0012 0.6936 0.6760
-0.250 -0.0213 0.01818 0.00916 -0.0012 0.6891 0.6806
0.000 0.0064 0.01814 0.00905 -0.0013 0.6854 0.6855
0.250 0.0343 0.01815 0.00908 -0.0016 0.6807 0.6895
0.500 0.0619 0.01820 0.00919 -0.0017 0.6760 0.6932
0.750 0.0895 0.01824 0.00925 -0.0017 0.6718 0.6979
1.000 0.1172 0.01822 0.00919 -0.0017 0.6675 0.7031
1.250 0.1445 0.01824 0.00926 -0.0018 0.6607 0.7077
1.500 0.1716 0.01824 0.00930 -0.0016 0.6536 0.7115
1.750 0.1990 0.01820 0.00925 -0.0014 0.6482 0.7162
2.000 0.2263 0.01827 0.00940 -0.0016 0.6410 0.7218
2.250 0.2537 0.01832 0.00952 -0.0017 0.6353 0.7265
2.500 0.2811 0.01833 0.00958 -0.0015 0.6306 0.7308
2.750 0.3084 0.01841 0.00976 -0.0016 0.6247 0.7357
3.000 0.3359 0.01846 0.00988 -0.0017 0.6172 0.7412
3.250 0.3632 0.01836 0.00984 -0.0013 0.6109 0.7457
3.500 0.3896 0.01838 0.01000 -0.0011 0.6008 0.7509
3.750 0.4171 0.01822 0.00987 -0.0007 0.5923 0.7570
4.000 0.4435 0.01822 0.01002 -0.0005 0.5819 0.7626
4.250 0.4704 0.01810 0.00998 0.0000 0.5735 0.7677
4.500 0.4965 0.01808 0.01010 0.0003 0.5610 0.7738
4.750 0.5230 0.01794 0.01006 0.0008 0.5477 0.7805
5.000 0.5490 0.01780 0.01002 0.0015 0.5327 0.7878
5.250 0.5747 0.01773 0.01009 0.0019 0.5134 0.7971
5.500 0.5996 0.01764 0.01014 0.0026 0.4918 0.8056
5.750 0.6251 0.01758 0.01012 0.0032 0.4692 0.8153
6.000 0.6492 0.01760 0.01019 0.0041 0.4411 0.8237
6.250 0.6725 0.01774 0.01029 0.0049 0.4012 0.8339
6.500 0.6925 0.01811 0.01045 0.0061 0.3472 0.8447
6.750 0.7101 0.01881 0.01090 0.0073 0.2959 0.8570
7.000 0.7272 0.01961 0.01154 0.0085 0.2432 0.8721
7.250 0.7445 0.02046 0.01225 0.0094 0.2052 0.8924
7.500 0.7647 0.02130 0.01300 0.0097 0.1786 0.9192
7.750 0.7918 0.02225 0.01391 0.0085 0.1577 0.9539
8.000 0.8154 0.02312 0.01476 0.0078 0.1407 0.9995
8.250 0.8339 0.02398 0.01559 0.0082 0.1269 0.9995
8.500 0.8517 0.02487 0.01646 0.0087 0.1151 0.9995
8.750 0.8685 0.02581 0.01737 0.0092 0.1046 0.9995
9.000 0.8842 0.02680 0.01835 0.0099 0.0959 0.9995
9.250 0.8985 0.02785 0.01939 0.0106 0.0880 0.9995
9.500 0.9103 0.02897 0.02049 0.0116 0.0813 0.9995
9.750 0.9223 0.03019 0.02172 0.0122 0.0749 0.9995
10.000 0.9343 0.03148 0.02305 0.0128 0.0691 0.9995
10.250 0.9460 0.03284 0.02446 0.0133 0.0640 0.9995
10.500 0.9572 0.03427 0.02594 0.0137 0.0599 0.9995
10.750 0.9682 0.03575 0.02751 0.0141 0.0566 0.9995
11.000 0.9786 0.03732 0.02916 0.0145 0.0540 0.9995
11.250 0.9884 0.03895 0.03088 0.0148 0.0515 0.9995
11.500 0.9974 0.04067 0.03266 0.0150 0.0490 0.9995
11.750 1.0057 0.04247 0.03455 0.0152 0.0465 0.9995
12.000 1.0129 0.04440 0.03656 0.0153 0.0442 0.9995
12.250 1.0193 0.04645 0.03872 0.0153 0.0422 0.9995
12.500 1.0240 0.04867 0.04098 0.0153 0.0409 0.9995
12.750 1.0295 0.05092 0.04342 0.0155 0.0391 0.9995
13.000 1.0322 0.05342 0.04601 0.0153 0.0375 0.9995
13.250 1.0340 0.05612 0.04887 0.0150 0.0355 0.9995
13.500 1.0340 0.05904 0.05193 0.0143 0.0336 0.9995
13.750 1.0329 0.06221 0.05527 0.0136 0.0318 0.9995
14.000 1.0302 0.06563 0.05884 0.0127 0.0303 0.9995
14.250 1.0259 0.06930 0.06260 0.0114 0.0292 0.9995
14.500 1.0201 0.07346 0.06698 0.0101 0.0279 0.9995
14.750 1.0132 0.07791 0.07157 0.0083 0.0269 0.9995
15.000 1.0057 0.08266 0.07641 0.0061 0.0262 0.9995
15.250 0.9955 0.08804 0.08196 0.0036 0.0255 0.9995
15.500 0.9832 0.09404 0.08815 0.0008 0.0249 0.9995
15.750 0.9697 0.10053 0.09480 -0.0025 0.0244 0.9995
16.000 0.9549 0.10752 0.10195 -0.0063 0.0241 0.9995
16.250 0.9385 0.11519 0.10977 -0.0105 0.0239 0.9995
16.500 0.9188 0.12388 0.11863 -0.0153 0.0237 0.9995
16.750 0.8726 0.14001 0.13507 -0.0244 0.0243 0.9995
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