WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Reynolds number: 500,000 Max Cl/Cd: 59.92 at α=4.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fxlv152-il-500000.txt Download as CSV file: xf-fxlv152-il-500000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.250 -1.1638 0.11361 0.10988 0.0201 1.0005 0.0087
-18.000 -1.1770 0.10712 0.10327 0.0169 1.0005 0.0087
-17.750 -1.1899 0.10079 0.09682 0.0138 1.0005 0.0087
-17.500 -1.2021 0.09471 0.09062 0.0109 1.0005 0.0087
-17.250 -1.2136 0.08889 0.08467 0.0083 1.0005 0.0088
-17.000 -1.2241 0.08335 0.07901 0.0059 1.0005 0.0088
-16.750 -1.2332 0.07819 0.07373 0.0037 1.0005 0.0088
-16.500 -1.2412 0.07336 0.06878 0.0018 1.0005 0.0089
-16.250 -1.2480 0.06880 0.06411 0.0001 1.0005 0.0089
-16.000 -1.2536 0.06457 0.05977 -0.0014 1.0005 0.0090
-15.750 -1.2582 0.06059 0.05568 -0.0027 1.0005 0.0091
-15.500 -1.2615 0.05694 0.05192 -0.0037 1.0005 0.0091
-15.250 -1.2641 0.05354 0.04841 -0.0045 1.0005 0.0092
-15.000 -1.2660 0.05036 0.04514 -0.0051 1.0005 0.0093
-14.750 -1.2665 0.04741 0.04209 -0.0055 1.0005 0.0094
-14.500 -1.2655 0.04466 0.03924 -0.0058 1.0005 0.0095
-14.250 -1.2633 0.04210 0.03658 -0.0061 1.0005 0.0096
-14.000 -1.2596 0.03972 0.03411 -0.0062 1.0005 0.0097
-13.750 -1.2547 0.03749 0.03180 -0.0063 1.0005 0.0099
-13.500 -1.2479 0.03549 0.02974 -0.0063 1.0005 0.0101
-13.250 -1.2388 0.03372 0.02793 -0.0063 1.0005 0.0104
-13.000 -1.2281 0.03214 0.02629 -0.0063 1.0005 0.0109
-12.750 -1.2168 0.03060 0.02469 -0.0062 1.0005 0.0114
-12.500 -1.2054 0.02910 0.02312 -0.0061 1.0005 0.0120
-12.250 -1.1920 0.02780 0.02179 -0.0060 1.0005 0.0127
-12.000 -1.1784 0.02652 0.02045 -0.0059 1.0005 0.0136
-11.750 -1.1642 0.02533 0.01918 -0.0057 1.0005 0.0146
-11.500 -1.1502 0.02417 0.01797 -0.0054 1.0005 0.0157
-11.250 -1.1334 0.02328 0.01698 -0.0051 1.0005 0.0169
-11.000 -1.1215 0.02205 0.01571 -0.0044 1.0005 0.0179
-10.750 -1.1061 0.02116 0.01476 -0.0037 1.0005 0.0191
-10.500 -1.0890 0.02036 0.01390 -0.0030 1.0005 0.0201
-10.250 -1.0712 0.01950 0.01300 -0.0024 1.0005 0.0213
-10.000 -1.0505 0.01884 0.01229 -0.0020 1.0005 0.0224
-9.750 -1.0300 0.01811 0.01156 -0.0017 1.0005 0.0237
-9.500 -1.0078 0.01750 0.01094 -0.0015 1.0005 0.0252
-9.250 -0.9764 0.01698 0.01035 -0.0030 0.9199 0.0271
-9.000 -0.9563 0.01665 0.00988 -0.0019 0.8700 0.0290
-8.750 -0.9345 0.01631 0.00942 -0.0012 0.8432 0.0319
-8.500 -0.9112 0.01595 0.00896 -0.0007 0.8215 0.0353
-8.250 -0.8875 0.01557 0.00849 -0.0004 0.8038 0.0391
-8.000 -0.8636 0.01515 0.00801 -0.0001 0.7887 0.0438
-7.750 -0.8398 0.01468 0.00755 0.0002 0.7762 0.0527
-7.500 -0.8149 0.01429 0.00715 0.0003 0.7660 0.0644
-7.250 -0.7901 0.01392 0.00674 0.0005 0.7574 0.0739
-7.000 -0.7649 0.01348 0.00635 0.0005 0.7494 0.0865
-6.750 -0.7397 0.01308 0.00598 0.0006 0.7424 0.1035
-6.500 -0.7140 0.01268 0.00564 0.0006 0.7361 0.1225
-6.250 -0.6880 0.01228 0.00531 0.0005 0.7298 0.1420
-6.000 -0.6619 0.01192 0.00498 0.0005 0.7241 0.1610
-5.750 -0.6364 0.01144 0.00461 0.0005 0.7187 0.1885
-5.500 -0.6117 0.01077 0.00420 0.0005 0.7131 0.2418
-5.250 -0.5866 0.01021 0.00385 0.0006 0.7079 0.2992
-5.000 -0.5617 0.00965 0.00348 0.0007 0.7034 0.3514
-4.750 -0.5365 0.00911 0.00326 0.0007 0.6991 0.4218
-4.500 -0.5091 0.00890 0.00312 0.0007 0.6948 0.4558
-4.250 -0.4812 0.00876 0.00301 0.0006 0.6908 0.4777
-4.000 -0.4531 0.00868 0.00295 0.0005 0.6870 0.4965
-3.750 -0.4247 0.00868 0.00294 0.0004 0.6833 0.5140
-3.500 -0.3958 0.00867 0.00294 0.0003 0.6795 0.5295
-3.250 -0.3668 0.00870 0.00292 0.0001 0.6757 0.5413
-3.000 -0.3381 0.00874 0.00293 -0.0001 0.6723 0.5536
-2.750 -0.3094 0.00877 0.00294 -0.0001 0.6688 0.5636
-2.500 -0.2806 0.00885 0.00297 -0.0003 0.6650 0.5724
-2.250 -0.2517 0.00884 0.00295 -0.0005 0.6612 0.5797
-2.000 -0.2229 0.00885 0.00299 -0.0006 0.6572 0.5870
-1.750 -0.1939 0.00892 0.00300 -0.0008 0.6536 0.5944
-1.500 -0.1652 0.00894 0.00303 -0.0009 0.6505 0.6008
-1.250 -0.1363 0.00904 0.00311 -0.0010 0.6472 0.6065
-1.000 -0.1070 0.00906 0.00312 -0.0013 0.6441 0.6121
-0.750 -0.0779 0.00904 0.00310 -0.0015 0.6403 0.6164
-0.500 -0.0489 0.00902 0.00311 -0.0017 0.6365 0.6203
-0.250 -0.0199 0.00904 0.00311 -0.0018 0.6325 0.6246
0.000 0.0090 0.00911 0.00313 -0.0020 0.6281 0.6291
0.250 0.0383 0.00910 0.00312 -0.0022 0.6237 0.6325
0.500 0.0672 0.00902 0.00309 -0.0024 0.6193 0.6363
0.750 0.0962 0.00899 0.00308 -0.0026 0.6149 0.6401
1.000 0.1251 0.00902 0.00307 -0.0027 0.6102 0.6436
1.250 0.1542 0.00899 0.00308 -0.0030 0.6054 0.6471
1.500 0.1834 0.00898 0.00306 -0.0032 0.5999 0.6504
1.750 0.2120 0.00891 0.00299 -0.0033 0.5933 0.6541
2.000 0.2407 0.00886 0.00298 -0.0034 0.5857 0.6579
2.250 0.2694 0.00881 0.00297 -0.0035 0.5780 0.6616
2.500 0.2980 0.00884 0.00296 -0.0036 0.5705 0.6653
2.750 0.3270 0.00879 0.00295 -0.0037 0.5605 0.6688
3.000 0.3554 0.00876 0.00292 -0.0038 0.5509 0.6724
3.250 0.3841 0.00869 0.00294 -0.0039 0.5393 0.6759
3.500 0.4128 0.00867 0.00295 -0.0040 0.5272 0.6795
3.750 0.4414 0.00868 0.00296 -0.0041 0.5128 0.6832
4.000 0.4696 0.00872 0.00298 -0.0042 0.4926 0.6871
4.250 0.4973 0.00881 0.00304 -0.0042 0.4739 0.6910
4.500 0.5249 0.00893 0.00316 -0.0042 0.4517 0.6950
4.750 0.5513 0.00920 0.00331 -0.0041 0.4081 0.6993
5.000 0.5753 0.00982 0.00359 -0.0038 0.3351 0.7037
5.250 0.6000 0.01036 0.00393 -0.0036 0.2893 0.7080
5.500 0.6245 0.01089 0.00428 -0.0035 0.2342 0.7126
5.750 0.6484 0.01154 0.00469 -0.0033 0.1822 0.7179
6.000 0.6735 0.01206 0.00507 -0.0032 0.1554 0.7234
6.250 0.6991 0.01239 0.00539 -0.0031 0.1364 0.7292
6.500 0.7244 0.01278 0.00572 -0.0030 0.1168 0.7360
6.750 0.7495 0.01322 0.00607 -0.0029 0.0969 0.7432
7.000 0.7738 0.01363 0.00645 -0.0026 0.0802 0.7504
7.250 0.7985 0.01404 0.00684 -0.0024 0.0695 0.7583
7.500 0.8232 0.01438 0.00723 -0.0022 0.0605 0.7665
7.750 0.8475 0.01478 0.00762 -0.0019 0.0497 0.7763
8.000 0.8708 0.01523 0.00809 -0.0016 0.0423 0.7880
8.250 0.8943 0.01564 0.00856 -0.0012 0.0379 0.8020
8.500 0.9177 0.01602 0.00901 -0.0008 0.0341 0.8188
8.750 0.9402 0.01637 0.00947 -0.0002 0.0306 0.8394
9.000 0.9612 0.01673 0.00994 0.0007 0.0280 0.8658
9.250 0.9794 0.01707 0.01041 0.0022 0.0261 0.9135
9.500 1.0092 0.01756 0.01100 0.0011 0.0246 0.9995
9.750 1.0304 0.01820 0.01164 0.0014 0.0233 0.9995
10.000 1.0511 0.01884 0.01231 0.0019 0.0220 0.9995
10.250 1.0699 0.01959 0.01310 0.0024 0.0208 0.9995
10.500 1.0871 0.02040 0.01395 0.0032 0.0198 0.9995
10.750 1.1036 0.02114 0.01476 0.0041 0.0187 0.9995
11.000 1.1169 0.02218 0.01584 0.0049 0.0177 0.9995
11.250 1.1318 0.02316 0.01689 0.0054 0.0167 0.9995
11.500 1.1468 0.02418 0.01798 0.0058 0.0155 0.9995
11.750 1.1597 0.02541 0.01926 0.0061 0.0147 0.9995
12.000 1.1742 0.02654 0.02048 0.0064 0.0136 0.9995
12.250 1.1874 0.02781 0.02181 0.0066 0.0128 0.9995
12.500 1.1996 0.02917 0.02321 0.0068 0.0122 0.9995
12.750 1.2105 0.03068 0.02479 0.0070 0.0116 0.9995
13.000 1.2212 0.03221 0.02639 0.0071 0.0111 0.9995
13.250 1.2312 0.03381 0.02804 0.0073 0.0107 0.9995
13.500 1.2403 0.03551 0.02978 0.0074 0.0103 0.9995
13.750 1.2473 0.03742 0.03174 0.0074 0.0101 0.9995
14.000 1.2519 0.03958 0.03399 0.0075 0.0099 0.9995
14.250 1.2551 0.04191 0.03641 0.0075 0.0098 0.9995
14.500 1.2571 0.04440 0.03898 0.0074 0.0097 0.9995
14.750 1.2576 0.04708 0.04175 0.0072 0.0096 0.9995
15.000 1.2568 0.04993 0.04470 0.0069 0.0095 0.9995
15.250 1.2550 0.05296 0.04783 0.0066 0.0094 0.9995
15.500 1.2524 0.05621 0.05119 0.0060 0.0093 0.9995
15.750 1.2489 0.05973 0.05481 0.0051 0.0093 0.9995
16.000 1.2443 0.06354 0.05873 0.0041 0.0092 0.9995
16.250 1.2385 0.06761 0.06291 0.0028 0.0091 0.9995
16.500 1.2316 0.07196 0.06737 0.0014 0.0091 0.9995
16.750 1.2235 0.07661 0.07213 -0.0003 0.0091 0.9995
17.000 1.2142 0.08156 0.07720 -0.0022 0.0090 0.9995
17.250 1.2038 0.08682 0.08258 -0.0043 0.0090 0.9995
17.500 1.1923 0.09237 0.08824 -0.0067 0.0090 0.9995
17.750 1.1800 0.09817 0.09417 -0.0092 0.0090 0.9995
18.000 1.1669 0.10425 0.10037 -0.0120 0.0090 0.9995
18.250 1.1535 0.11046 0.10669 -0.0149 0.0090 0.9995
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