WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Reynolds number: 1,000,000 Max Cl/Cd: 62.59 at α=8.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fxlv152-il-1000000-n5.txt Download as CSV file: xf-fxlv152-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.500 -1.1498 0.12171 0.11852 0.0266 1.0005 0.0034
-18.250 -1.1687 0.11391 0.11060 0.0226 1.0005 0.0034
-18.000 -1.1860 0.10659 0.10316 0.0190 1.0005 0.0034
-17.750 -1.2030 0.09944 0.09589 0.0155 1.0005 0.0034
-17.500 -1.2184 0.09275 0.08908 0.0123 1.0005 0.0034
-17.250 -1.2312 0.08663 0.08285 0.0095 1.0005 0.0034
-17.000 -1.2426 0.08094 0.07704 0.0070 1.0005 0.0034
-16.750 -1.2515 0.07581 0.07180 0.0049 1.0005 0.0034
-16.500 -1.2594 0.07094 0.06683 0.0029 1.0005 0.0034
-16.250 -1.2654 0.06650 0.06229 0.0013 1.0005 0.0034
-16.000 -1.2693 0.06249 0.05818 -0.0002 1.0005 0.0034
-15.750 -1.2721 0.05874 0.05434 -0.0014 1.0005 0.0035
-15.500 -1.2790 0.05466 0.05015 -0.0026 1.0005 0.0035
-15.250 -1.2858 0.05080 0.04618 -0.0034 1.0005 0.0035
-15.000 -1.2913 0.04726 0.04254 -0.0041 1.0005 0.0036
-14.750 -1.2946 0.04401 0.03919 -0.0046 1.0005 0.0036
-14.500 -1.2960 0.04106 0.03615 -0.0049 1.0005 0.0037
-14.250 -1.2946 0.03845 0.03345 -0.0051 1.0005 0.0037
-14.000 -1.2914 0.03606 0.03098 -0.0052 1.0005 0.0038
-13.750 -1.2865 0.03386 0.02871 -0.0053 1.0005 0.0038
-13.500 -1.2800 0.03184 0.02661 -0.0053 1.0005 0.0039
-13.250 -1.2720 0.03000 0.02470 -0.0052 1.0005 0.0039
-13.000 -1.2626 0.02831 0.02295 -0.0051 1.0005 0.0040
-12.750 -1.2521 0.02673 0.02131 -0.0050 1.0005 0.0040
-12.500 -1.2407 0.02529 0.01980 -0.0048 1.0005 0.0041
-12.250 -1.2298 0.02424 0.01847 -0.0040 0.8623 0.0042
-12.000 -1.2174 0.02315 0.01721 -0.0035 0.8299 0.0042
-11.750 -1.2037 0.02213 0.01605 -0.0029 0.8026 0.0043
-11.500 -1.1890 0.02122 0.01500 -0.0023 0.7750 0.0044
-11.250 -1.1734 0.02044 0.01410 -0.0015 0.7615 0.0044
-11.000 -1.1557 0.01975 0.01332 -0.0007 0.7521 0.0045
-10.750 -1.1359 0.01911 0.01259 -0.0002 0.7437 0.0045
-10.500 -1.1149 0.01850 0.01192 0.0002 0.7367 0.0046
-10.250 -1.0932 0.01794 0.01130 0.0005 0.7279 0.0047
-10.000 -1.0707 0.01742 0.01070 0.0008 0.7189 0.0047
-9.750 -1.0476 0.01693 0.01015 0.0011 0.7075 0.0048
-9.500 -1.0240 0.01647 0.00962 0.0013 0.6968 0.0049
-9.000 -0.9756 0.01560 0.00862 0.0017 0.6810 0.0052
-8.750 -0.9509 0.01518 0.00814 0.0018 0.6754 0.0054
-8.500 -0.9258 0.01479 0.00769 0.0019 0.6696 0.0056
-8.250 -0.9005 0.01441 0.00727 0.0020 0.6646 0.0059
-8.000 -0.8747 0.01404 0.00687 0.0020 0.6605 0.0062
-7.750 -0.8489 0.01368 0.00649 0.0021 0.6564 0.0073
-7.500 -0.8228 0.01334 0.00617 0.0021 0.6526 0.0133
-7.250 -0.7958 0.01312 0.00592 0.0020 0.6490 0.0144
-7.000 -0.7689 0.01286 0.00565 0.0019 0.6460 0.0153
-6.750 -0.7417 0.01262 0.00540 0.0018 0.6429 0.0161
-6.500 -0.7143 0.01240 0.00516 0.0017 0.6393 0.0167
-6.250 -0.6869 0.01218 0.00492 0.0016 0.6353 0.0173
-6.000 -0.6596 0.01193 0.00465 0.0015 0.6314 0.0181
-5.750 -0.6322 0.01171 0.00441 0.0014 0.6279 0.0191
-5.500 -0.6044 0.01150 0.00419 0.0012 0.6250 0.0199
-5.250 -0.5767 0.01128 0.00396 0.0011 0.6215 0.0212
-5.000 -0.5491 0.01103 0.00372 0.0010 0.6182 0.0240
-4.750 -0.5220 0.01070 0.00346 0.0009 0.6148 0.0410
-4.500 -0.4950 0.01035 0.00320 0.0008 0.6113 0.0619
-4.250 -0.4671 0.01015 0.00302 0.0006 0.6079 0.0717
-4.000 -0.4402 0.00974 0.00276 0.0005 0.6043 0.1034
-3.750 -0.4133 0.00935 0.00253 0.0004 0.6008 0.1395
-3.500 -0.3855 0.00909 0.00235 0.0003 0.5972 0.1611
-3.250 -0.3587 0.00868 0.00211 0.0002 0.5939 0.2066
-2.750 -0.3040 0.00801 0.00176 -0.0001 0.5884 0.2907
-2.500 -0.2761 0.00775 0.00161 -0.0003 0.5859 0.3209
-2.250 -0.2495 0.00730 0.00142 -0.0003 0.5830 0.3872
-2.000 -0.2219 0.00702 0.00132 -0.0005 0.5798 0.4348
-1.750 -0.1936 0.00689 0.00126 -0.0006 0.5760 0.4638
-1.500 -0.1653 0.00678 0.00121 -0.0007 0.5718 0.4851
-1.000 -0.1073 0.00665 0.00120 -0.0012 0.5667 0.5188
-0.750 -0.0782 0.00662 0.00121 -0.0014 0.5637 0.5346
-0.500 -0.0490 0.00661 0.00122 -0.0016 0.5602 0.5438
-0.250 -0.0198 0.00661 0.00122 -0.0019 0.5570 0.5504
0.000 0.0095 0.00664 0.00122 -0.0021 0.5534 0.5546
0.250 0.0390 0.00664 0.00122 -0.0024 0.5489 0.5575
0.500 0.0683 0.00662 0.00121 -0.0026 0.5409 0.5608
0.750 0.0972 0.00663 0.00121 -0.0028 0.5314 0.5643
1.000 0.1264 0.00664 0.00121 -0.0031 0.5188 0.5686
1.500 0.1835 0.00684 0.00123 -0.0034 0.4739 0.5754
1.750 0.2120 0.00696 0.00128 -0.0035 0.4534 0.5773
2.000 0.2399 0.00713 0.00135 -0.0036 0.4203 0.5800
2.250 0.2665 0.00748 0.00148 -0.0036 0.3590 0.5826
2.500 0.2935 0.00780 0.00165 -0.0036 0.3165 0.5854
2.750 0.3210 0.00806 0.00180 -0.0037 0.2864 0.5885
3.250 0.3745 0.00881 0.00218 -0.0038 0.1906 0.5937
3.750 0.4284 0.00946 0.00259 -0.0038 0.1304 0.5999
4.000 0.4545 0.00988 0.00284 -0.0038 0.0893 0.6039
4.250 0.4814 0.01021 0.00307 -0.0038 0.0684 0.6079
4.500 0.5084 0.01052 0.00330 -0.0039 0.0481 0.6115
5.000 0.5622 0.01111 0.00379 -0.0039 0.0225 0.6182
5.250 0.5895 0.01134 0.00402 -0.0040 0.0206 0.6217
5.500 0.6170 0.01154 0.00424 -0.0040 0.0196 0.6251
5.750 0.6442 0.01177 0.00448 -0.0041 0.0185 0.6287
6.000 0.6713 0.01202 0.00474 -0.0041 0.0176 0.6318
6.250 0.6985 0.01223 0.00496 -0.0041 0.0171 0.6348
6.500 0.7255 0.01243 0.00519 -0.0042 0.0164 0.6383
6.750 0.7524 0.01266 0.00544 -0.0042 0.0156 0.6423
7.000 0.7790 0.01292 0.00571 -0.0042 0.0147 0.6463
7.250 0.8058 0.01315 0.00595 -0.0042 0.0140 0.6499
7.500 0.8320 0.01343 0.00623 -0.0041 0.0079 0.6534
7.750 0.8572 0.01380 0.00660 -0.0040 0.0063 0.6575
8.000 0.8825 0.01415 0.00699 -0.0038 0.0059 0.6618
8.250 0.9076 0.01451 0.00739 -0.0037 0.0056 0.6658
8.500 0.9325 0.01490 0.00781 -0.0035 0.0053 0.6695
8.750 0.9570 0.01529 0.00826 -0.0032 0.0051 0.6744
9.000 0.9813 0.01568 0.00870 -0.0030 0.0050 0.6799
9.250 1.0053 0.01609 0.00918 -0.0028 0.0049 0.6858
9.500 1.0288 0.01652 0.00967 -0.0024 0.0048 0.6938
9.750 1.0518 0.01698 0.01020 -0.0021 0.0047 0.7040
10.000 1.0741 0.01747 0.01077 -0.0017 0.0047 0.7151
10.250 1.0959 0.01800 0.01136 -0.0012 0.0046 0.7249
10.500 1.1168 0.01856 0.01199 -0.0007 0.0045 0.7349
10.750 1.1369 0.01916 0.01266 -0.0002 0.0045 0.7436
11.000 1.1556 0.01980 0.01339 0.0005 0.0044 0.7527
11.250 1.1712 0.02048 0.01416 0.0016 0.0044 0.7627
11.500 1.1872 0.02129 0.01509 0.0023 0.0043 0.7777
11.750 1.2016 0.02221 0.01615 0.0030 0.0042 0.8062
12.000 1.2148 0.02324 0.01732 0.0036 0.0042 0.8337
12.250 1.2264 0.02434 0.01860 0.0043 0.0041 0.8682
12.500 1.2357 0.02541 0.01994 0.0053 0.0040 0.9995
12.750 1.2466 0.02688 0.02146 0.0055 0.0040 0.9995
13.000 1.2566 0.02845 0.02310 0.0057 0.0040 0.9995
13.250 1.2653 0.03014 0.02486 0.0059 0.0039 0.9995
13.500 1.2728 0.03197 0.02676 0.0061 0.0039 0.9995
13.750 1.2790 0.03395 0.02881 0.0062 0.0039 0.9995
14.000 1.2837 0.03609 0.03102 0.0062 0.0038 0.9995
14.250 1.2869 0.03839 0.03340 0.0063 0.0038 0.9995
14.500 1.2888 0.04085 0.03594 0.0062 0.0038 0.9995
14.750 1.2888 0.04354 0.03872 0.0061 0.0038 0.9995
15.000 1.2875 0.04642 0.04169 0.0058 0.0038 0.9995
15.250 1.2846 0.04951 0.04487 0.0055 0.0037 0.9995
15.500 1.2802 0.05287 0.04832 0.0049 0.0037 0.9995
15.750 1.2751 0.05651 0.05206 0.0041 0.0037 0.9995
16.000 1.2693 0.06040 0.05605 0.0031 0.0037 0.9995
16.250 1.2616 0.06471 0.06047 0.0017 0.0037 0.9995
16.500 1.2531 0.06927 0.06513 0.0002 0.0037 0.9995
16.750 1.2429 0.07421 0.07018 -0.0016 0.0036 0.9995
17.000 1.2314 0.07951 0.07559 -0.0036 0.0036 0.9995
17.250 1.2184 0.08521 0.08140 -0.0060 0.0036 0.9995
17.500 1.2042 0.09126 0.08756 -0.0085 0.0036 0.9995
17.750 1.1889 0.09765 0.09407 -0.0114 0.0036 0.9995
18.000 1.1730 0.10427 0.10081 -0.0144 0.0036 0.9995
18.250 1.1559 0.11126 0.10791 -0.0176 0.0036 0.9995
18.500 1.1393 0.11824 0.11501 -0.0210 0.0036 0.9995
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