WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Reynolds number: 200,000 Max Cl/Cd: 45.32 at α=5.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fxlv152-il-200000-n5.txt Download as CSV file: xf-fxlv152-il-200000-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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.500 -0.9371 0.16719 0.16355 0.0487 1.0005 0.0109
-18.250 -0.9634 0.15511 0.15133 0.0415 1.0005 0.0108
-18.000 -0.9840 0.14520 0.14127 0.0356 1.0005 0.0107
-17.750 -1.0030 0.13601 0.13195 0.0302 1.0005 0.0107
-17.500 -1.0211 0.12741 0.12320 0.0253 1.0005 0.0107
-17.250 -1.0384 0.11925 0.11489 0.0207 1.0005 0.0106
-17.000 -1.0548 0.11154 0.10703 0.0165 1.0005 0.0106
-16.750 -1.0697 0.10437 0.09970 0.0127 1.0005 0.0107
-16.500 -1.0831 0.09766 0.09283 0.0092 1.0005 0.0107
-16.250 -1.0949 0.09145 0.08647 0.0061 1.0005 0.0108
-16.000 -1.1051 0.08575 0.08062 0.0034 1.0005 0.0109
-15.750 -1.1138 0.08047 0.07519 0.0010 1.0005 0.0111
-15.500 -1.1210 0.07560 0.07017 -0.0011 1.0005 0.0113
-15.250 -1.1269 0.07110 0.06552 -0.0029 1.0005 0.0115
-15.000 -1.1318 0.06690 0.06118 -0.0044 1.0005 0.0118
-14.750 -1.1353 0.06308 0.05723 -0.0057 1.0005 0.0121
-14.500 -1.1372 0.05962 0.05364 -0.0067 1.0005 0.0124
-14.250 -1.1382 0.05640 0.05030 -0.0075 1.0005 0.0130
-14.000 -1.1381 0.05340 0.04714 -0.0081 1.0005 0.0136
-13.500 -1.1341 0.04796 0.04144 -0.0089 1.0005 0.0151
-13.250 -1.1304 0.04550 0.03885 -0.0092 1.0005 0.0160
-13.000 -1.1239 0.04338 0.03656 -0.0093 1.0005 0.0170
-12.750 -1.1203 0.04098 0.03407 -0.0095 1.0005 0.0177
-12.500 -1.1140 0.03889 0.03187 -0.0095 1.0005 0.0187
-12.250 -1.1057 0.03702 0.02987 -0.0095 1.0005 0.0198
-12.000 -1.0991 0.03501 0.02779 -0.0094 1.0005 0.0206
-11.750 -1.0899 0.03327 0.02596 -0.0093 1.0005 0.0216
-11.500 -1.0795 0.03168 0.02429 -0.0091 1.0005 0.0227
-11.250 -1.0690 0.03012 0.02269 -0.0089 1.0005 0.0240
-11.000 -1.0566 0.02877 0.02128 -0.0087 1.0005 0.0252
-10.750 -1.0435 0.02751 0.01999 -0.0084 1.0005 0.0266
-10.500 -1.0294 0.02639 0.01882 -0.0080 1.0005 0.0286
-10.250 -1.0147 0.02536 0.01776 -0.0076 1.0005 0.0312
-10.000 -0.9993 0.02444 0.01680 -0.0070 1.0005 0.0341
-9.750 -0.9826 0.02362 0.01592 -0.0063 1.0005 0.0369
-9.500 -0.9641 0.02282 0.01507 -0.0059 1.0005 0.0401
-9.250 -0.9454 0.02199 0.01425 -0.0055 1.0005 0.0438
-9.000 -0.9193 0.02129 0.01347 -0.0064 0.9138 0.0482
-8.750 -0.8984 0.02071 0.01279 -0.0059 0.8737 0.0530
-8.500 -0.8781 0.02021 0.01217 -0.0051 0.8503 0.0588
-8.000 -0.8347 0.01919 0.01095 -0.0040 0.8160 0.0713
-7.750 -0.8128 0.01864 0.01036 -0.0036 0.8024 0.0791
-7.500 -0.7912 0.01804 0.00977 -0.0031 0.7902 0.0917
-7.250 -0.7690 0.01746 0.00922 -0.0028 0.7789 0.1093
-7.000 -0.7461 0.01692 0.00870 -0.0025 0.7697 0.1277
-6.750 -0.7225 0.01643 0.00819 -0.0022 0.7619 0.1454
-6.500 -0.6983 0.01597 0.00770 -0.0020 0.7545 0.1618
-6.250 -0.6747 0.01541 0.00720 -0.0018 0.7465 0.1830
-6.000 -0.6522 0.01477 0.00667 -0.0015 0.7399 0.2259
-5.750 -0.6293 0.01403 0.00620 -0.0013 0.7327 0.2813
-5.500 -0.6055 0.01347 0.00578 -0.0011 0.7266 0.3236
-5.000 -0.5563 0.01263 0.00531 -0.0006 0.7157 0.4195
-4.750 -0.5297 0.01245 0.00518 -0.0005 0.7105 0.4536
-4.500 -0.5028 0.01234 0.00510 -0.0003 0.7059 0.4801
-4.250 -0.4754 0.01232 0.00509 -0.0002 0.7018 0.5020
-4.000 -0.4474 0.01233 0.00508 -0.0002 0.6969 0.5216
-3.750 -0.4193 0.01236 0.00503 -0.0002 0.6922 0.5383
-3.500 -0.3914 0.01239 0.00503 -0.0001 0.6879 0.5516
-3.000 -0.3349 0.01242 0.00494 -0.0002 0.6805 0.5702
-2.750 -0.3063 0.01240 0.00483 -0.0004 0.6766 0.5773
-2.500 -0.2779 0.01241 0.00484 -0.0004 0.6729 0.5832
-2.250 -0.2496 0.01244 0.00480 -0.0004 0.6693 0.5908
-1.750 -0.1926 0.01246 0.00476 -0.0006 0.6620 0.6021
-1.500 -0.1639 0.01246 0.00474 -0.0008 0.6582 0.6072
-1.250 -0.1351 0.01246 0.00468 -0.0010 0.6546 0.6122
-1.000 -0.1065 0.01246 0.00465 -0.0012 0.6511 0.6163
-0.750 -0.0780 0.01249 0.00465 -0.0012 0.6478 0.6205
-0.500 -0.0493 0.01249 0.00467 -0.0014 0.6434 0.6256
-0.250 -0.0206 0.01251 0.00467 -0.0016 0.6388 0.6315
0.000 0.0079 0.01250 0.00468 -0.0017 0.6345 0.6358
0.250 0.0363 0.01250 0.00468 -0.0018 0.6305 0.6399
0.500 0.0650 0.01251 0.00468 -0.0020 0.6266 0.6439
0.750 0.0938 0.01250 0.00470 -0.0022 0.6215 0.6477
1.000 0.1226 0.01250 0.00468 -0.0025 0.6165 0.6514
1.250 0.1510 0.01246 0.00469 -0.0025 0.6120 0.6545
1.500 0.1794 0.01247 0.00472 -0.0026 0.6074 0.6581
1.750 0.2080 0.01246 0.00479 -0.0028 0.6015 0.6620
2.000 0.2365 0.01244 0.00478 -0.0029 0.5954 0.6658
2.250 0.2651 0.01244 0.00474 -0.0030 0.5897 0.6697
2.500 0.2933 0.01241 0.00484 -0.0030 0.5820 0.6729
2.750 0.3214 0.01240 0.00488 -0.0030 0.5754 0.6766
3.000 0.3496 0.01241 0.00493 -0.0030 0.5688 0.6806
3.250 0.3780 0.01241 0.00501 -0.0031 0.5597 0.6847
3.500 0.4061 0.01241 0.00502 -0.0031 0.5501 0.6885
3.750 0.4338 0.01237 0.00507 -0.0030 0.5363 0.6920
4.000 0.4616 0.01234 0.00513 -0.0030 0.5199 0.6961
4.250 0.4892 0.01232 0.00512 -0.0028 0.4988 0.7007
4.500 0.5163 0.01238 0.00511 -0.0027 0.4765 0.7060
4.750 0.5427 0.01248 0.00522 -0.0024 0.4494 0.7105
5.000 0.5686 0.01268 0.00535 -0.0021 0.4122 0.7158
5.250 0.5928 0.01308 0.00554 -0.0018 0.3587 0.7216
5.500 0.6157 0.01364 0.00588 -0.0013 0.3109 0.7272
5.750 0.6389 0.01419 0.00630 -0.0010 0.2656 0.7335
6.000 0.6611 0.01490 0.00679 -0.0006 0.2173 0.7405
6.250 0.6838 0.01550 0.00728 -0.0003 0.1805 0.7466
6.500 0.7067 0.01603 0.00777 0.0001 0.1600 0.7536
6.750 0.7300 0.01655 0.00828 0.0004 0.1420 0.7614
7.000 0.7528 0.01702 0.00878 0.0009 0.1232 0.7692
7.250 0.7752 0.01757 0.00930 0.0013 0.1056 0.7784
7.500 0.7967 0.01812 0.00985 0.0018 0.0902 0.7887
7.750 0.8181 0.01869 0.01042 0.0024 0.0786 0.8005
8.000 0.8393 0.01924 0.01101 0.0030 0.0707 0.8144
8.250 0.8601 0.01974 0.01161 0.0037 0.0646 0.8301
8.500 0.8806 0.02024 0.01221 0.0045 0.0585 0.8498
8.750 0.8995 0.02073 0.01283 0.0056 0.0528 0.8740
9.000 0.9190 0.02129 0.01350 0.0064 0.0482 0.9151
9.250 0.9445 0.02199 0.01426 0.0056 0.0439 0.9995
9.500 0.9626 0.02280 0.01507 0.0061 0.0402 0.9995
9.750 0.9794 0.02363 0.01593 0.0068 0.0366 0.9995
10.000 0.9951 0.02445 0.01680 0.0076 0.0332 0.9995
10.250 1.0104 0.02537 0.01776 0.0082 0.0302 0.9995
10.500 1.0249 0.02640 0.01883 0.0087 0.0279 0.9995
10.750 1.0386 0.02754 0.02001 0.0091 0.0263 0.9995
11.000 1.0516 0.02877 0.02129 0.0094 0.0251 0.9995
11.250 1.0636 0.03011 0.02269 0.0097 0.0241 0.9995
11.500 1.0739 0.03165 0.02426 0.0100 0.0230 0.9995
11.750 1.0841 0.03321 0.02591 0.0102 0.0217 0.9995
12.000 1.0924 0.03496 0.02774 0.0104 0.0207 0.9995
12.250 1.0993 0.03688 0.02973 0.0106 0.0199 0.9995
12.500 1.1070 0.03873 0.03171 0.0107 0.0190 0.9995
12.750 1.1125 0.04083 0.03391 0.0108 0.0180 0.9995
13.000 1.1159 0.04316 0.03633 0.0107 0.0173 0.9995
13.250 1.1218 0.04526 0.03859 0.0107 0.0163 0.9995
13.500 1.1251 0.04767 0.04113 0.0106 0.0155 0.9995
13.750 1.1265 0.05031 0.04388 0.0103 0.0148 0.9995
14.000 1.1282 0.05297 0.04669 0.0100 0.0141 0.9995
14.250 1.1282 0.05588 0.04975 0.0096 0.0134 0.9995
14.500 1.1266 0.05903 0.05303 0.0090 0.0129 0.9995
14.750 1.1243 0.06240 0.05653 0.0081 0.0125 0.9995
15.000 1.1209 0.06607 0.06032 0.0070 0.0121 0.9995
15.250 1.1159 0.07011 0.06451 0.0057 0.0118 0.9995
15.500 1.1098 0.07446 0.06901 0.0041 0.0116 0.9995
15.750 1.1024 0.07914 0.07383 0.0022 0.0114 0.9995
16.000 1.0937 0.08422 0.07906 0.0001 0.0112 0.9995
16.250 1.0834 0.08971 0.08469 -0.0024 0.0111 0.9995
16.500 1.0717 0.09562 0.09074 -0.0052 0.0110 0.9995
16.750 1.0584 0.10204 0.09731 -0.0083 0.0109 0.9995
17.000 1.0436 0.10886 0.10429 -0.0118 0.0109 0.9995
17.250 1.0274 0.11621 0.11178 -0.0156 0.0109 0.9995
17.500 1.0101 0.12398 0.11970 -0.0198 0.0109 0.9995
17.750 0.9919 0.13219 0.12805 -0.0242 0.0109 0.9995
18.000 0.9731 0.14087 0.13687 -0.0291 0.0110 0.9995
18.250 0.9530 0.15019 0.14632 -0.0344 0.0110 0.9995
18.500 0.9294 0.16084 0.15711 -0.0406 0.0111 0.9995
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