LWK 80-150/K25 (lwk80150k25-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: LWK 80-150/K25 (lwk80150k25-il) Reynolds number: 1,000,000 Max Cl/Cd: 55.37 at α=8.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-lwk80150k25-il-1000000-n5.txt Download as CSV file: xf-lwk80150k25-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: LWK 80-150/K25
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
------ -------- --------- --------- -------- -------- --------
-19.750 -1.3088 0.08976 0.08615 -0.0172 1.0000 0.0110
-19.500 -1.3265 0.08312 0.07937 -0.0204 1.0000 0.0110
-19.250 -1.3384 0.07757 0.07370 -0.0230 1.0000 0.0111
-19.000 -1.3520 0.07196 0.06796 -0.0254 1.0000 0.0111
-18.750 -1.3565 0.06787 0.06376 -0.0271 1.0000 0.0112
-18.500 -1.3641 0.06347 0.05923 -0.0286 1.0000 0.0112
-18.250 -1.3729 0.05908 0.05474 -0.0299 1.0000 0.0114
-17.750 -1.3806 0.05212 0.04758 -0.0314 1.0000 0.0116
-16.750 -1.3692 0.04211 0.03727 -0.0316 0.9654 0.0122
-16.500 -1.3474 0.03994 0.03496 -0.0350 0.9261 0.0124
-16.250 -1.3324 0.03821 0.03308 -0.0362 0.9038 0.0126
-16.000 -1.3200 0.03657 0.03132 -0.0367 0.8905 0.0127
-15.750 -1.3101 0.03482 0.02945 -0.0370 0.8805 0.0130
-15.500 -1.2971 0.03342 0.02794 -0.0371 0.8732 0.0131
-15.250 -1.2833 0.03207 0.02650 -0.0373 0.8665 0.0133
-15.000 -1.2685 0.03077 0.02510 -0.0376 0.8612 0.0133
-14.750 -1.2517 0.02973 0.02400 -0.0378 0.8568 0.0137
-14.500 -1.2336 0.02869 0.02288 -0.0382 0.8524 0.0139
-14.250 -1.2172 0.02741 0.02151 -0.0387 0.8483 0.0142
-14.000 -1.1989 0.02631 0.02035 -0.0391 0.8447 0.0145
-13.750 -1.1816 0.02534 0.01934 -0.0392 0.8414 0.0148
-13.500 -1.1628 0.02447 0.01841 -0.0393 0.8377 0.0153
-13.250 -1.1429 0.02364 0.01753 -0.0395 0.8340 0.0156
-13.000 -1.1218 0.02286 0.01668 -0.0399 0.8305 0.0161
-12.750 -1.1014 0.02207 0.01583 -0.0401 0.8275 0.0163
-12.500 -1.0802 0.02146 0.01517 -0.0402 0.8247 0.0169
-12.250 -1.0599 0.02074 0.01440 -0.0402 0.8218 0.0168
-12.000 -1.0396 0.02002 0.01365 -0.0402 0.8189 0.0177
-11.750 -1.0180 0.01938 0.01298 -0.0403 0.8161 0.0184
-11.500 -0.9955 0.01880 0.01236 -0.0405 0.8134 0.0191
-11.250 -0.9730 0.01826 0.01178 -0.0406 0.8109 0.0199
-11.000 -0.9513 0.01776 0.01124 -0.0405 0.8085 0.0204
-10.750 -0.9304 0.01719 0.01065 -0.0402 0.8058 0.0212
-10.500 -0.9090 0.01668 0.01012 -0.0400 0.8031 0.0220
-10.250 -0.8870 0.01622 0.00963 -0.0397 0.8003 0.0231
-10.000 -0.8648 0.01579 0.00917 -0.0395 0.7979 0.0240
-9.750 -0.8433 0.01533 0.00869 -0.0391 0.7955 0.0255
-9.500 -0.8218 0.01492 0.00826 -0.0387 0.7934 0.0267
-9.250 -0.8007 0.01452 0.00785 -0.0381 0.7913 0.0280
-9.000 -0.7802 0.01412 0.00745 -0.0373 0.7891 0.0302
-8.750 -0.7597 0.01374 0.00707 -0.0366 0.7866 0.0322
-8.500 -0.7391 0.01341 0.00672 -0.0357 0.7840 0.0342
-8.250 -0.7196 0.01305 0.00636 -0.0346 0.7815 0.0367
-8.000 -0.6995 0.01275 0.00604 -0.0336 0.7792 0.0390
-7.500 -0.6611 0.01214 0.00544 -0.0310 0.7752 0.0455
-7.250 -0.6424 0.01184 0.00517 -0.0295 0.7733 0.0496
-7.000 -0.6230 0.01160 0.00493 -0.0281 0.7712 0.0533
-6.750 -0.6054 0.01135 0.00471 -0.0263 0.7688 0.0586
-6.500 -0.5869 0.01115 0.00451 -0.0246 0.7665 0.0632
-6.250 -0.5677 0.01091 0.00430 -0.0231 0.7642 0.0703
-6.000 -0.5471 0.01069 0.00410 -0.0219 0.7623 0.0769
-5.750 -0.5257 0.01049 0.00391 -0.0208 0.7603 0.0845
-5.500 -0.5044 0.01026 0.00373 -0.0197 0.7586 0.0933
-5.250 -0.4828 0.01003 0.00355 -0.0186 0.7569 0.1039
-5.000 -0.4612 0.00979 0.00338 -0.0175 0.7549 0.1173
-4.750 -0.4398 0.00954 0.00320 -0.0164 0.7527 0.1343
-4.500 -0.4180 0.00930 0.00303 -0.0154 0.7506 0.1530
-4.250 -0.3971 0.00901 0.00285 -0.0142 0.7487 0.1783
-4.000 -0.3765 0.00870 0.00267 -0.0130 0.7468 0.2101
-3.750 -0.3548 0.00844 0.00251 -0.0119 0.7449 0.2391
-3.500 -0.3341 0.00813 0.00234 -0.0106 0.7427 0.2763
-3.250 -0.3142 0.00776 0.00217 -0.0093 0.7409 0.3241
-3.000 -0.2938 0.00740 0.00201 -0.0080 0.7391 0.3733
-2.750 -0.2743 0.00701 0.00183 -0.0065 0.7370 0.4279
-2.500 -0.2548 0.00661 0.00166 -0.0050 0.7349 0.4858
-2.250 -0.2348 0.00625 0.00152 -0.0035 0.7328 0.5429
-2.000 -0.2135 0.00598 0.00143 -0.0022 0.7308 0.5934
-1.750 -0.1894 0.00585 0.00140 -0.0014 0.7287 0.6265
-1.500 -0.1635 0.00579 0.00139 -0.0010 0.7265 0.6460
-1.250 -0.1370 0.00576 0.00139 -0.0007 0.7246 0.6633
-1.000 -0.1095 0.00574 0.00140 -0.0006 0.7225 0.6750
-0.750 -0.0823 0.00572 0.00142 -0.0004 0.7201 0.6843
-0.500 -0.0545 0.00571 0.00141 -0.0004 0.7166 0.6927
-0.250 -0.0275 0.00570 0.00141 -0.0001 0.7118 0.6997
0.000 0.0000 0.00571 0.00140 0.0000 0.7063 0.7060
0.250 0.0275 0.00570 0.00141 0.0001 0.6997 0.7117
0.500 0.0545 0.00572 0.00141 0.0004 0.6924 0.7168
0.750 0.0822 0.00572 0.00141 0.0004 0.6839 0.7201
1.000 0.1095 0.00574 0.00140 0.0006 0.6754 0.7225
1.250 0.1370 0.00576 0.00139 0.0007 0.6633 0.7246
1.500 0.1636 0.00579 0.00139 0.0010 0.6466 0.7265
1.750 0.1893 0.00585 0.00140 0.0015 0.6258 0.7286
2.000 0.2132 0.00600 0.00143 0.0023 0.5902 0.7307
2.250 0.2348 0.00625 0.00152 0.0035 0.5429 0.7328
2.500 0.2548 0.00661 0.00166 0.0050 0.4860 0.7350
2.750 0.2737 0.00703 0.00184 0.0066 0.4245 0.7372
3.000 0.2936 0.00741 0.00201 0.0080 0.3719 0.7392
3.250 0.3135 0.00780 0.00218 0.0094 0.3200 0.7409
3.500 0.3341 0.00813 0.00234 0.0107 0.2760 0.7427
3.750 0.3547 0.00845 0.00251 0.0119 0.2382 0.7448
4.000 0.3760 0.00872 0.00268 0.0130 0.2073 0.7468
4.250 0.3975 0.00899 0.00285 0.0141 0.1809 0.7487
4.750 0.4400 0.00953 0.00319 0.0164 0.1356 0.7527
5.000 0.4612 0.00979 0.00337 0.0175 0.1169 0.7549
5.250 0.4831 0.01002 0.00355 0.0185 0.1052 0.7569
5.500 0.5047 0.01025 0.00372 0.0196 0.0948 0.7586
5.750 0.5254 0.01050 0.00392 0.0208 0.0829 0.7603
6.000 0.5469 0.01070 0.00410 0.0219 0.0764 0.7622
6.250 0.5674 0.01092 0.00431 0.0231 0.0690 0.7643
6.500 0.5868 0.01115 0.00451 0.0246 0.0632 0.7666
6.750 0.6052 0.01135 0.00471 0.0263 0.0581 0.7689
7.000 0.6231 0.01159 0.00493 0.0280 0.0536 0.7712
7.250 0.6426 0.01184 0.00517 0.0294 0.0500 0.7733
7.500 0.6613 0.01214 0.00544 0.0309 0.0457 0.7752
8.000 0.6998 0.01274 0.00604 0.0335 0.0396 0.7792
8.250 0.7200 0.01304 0.00636 0.0346 0.0370 0.7815
8.500 0.7397 0.01339 0.00671 0.0356 0.0345 0.7840
8.750 0.7602 0.01373 0.00707 0.0365 0.0323 0.7866
9.000 0.7806 0.01412 0.00745 0.0373 0.0300 0.7891
9.250 0.8012 0.01452 0.00785 0.0380 0.0281 0.7914
9.500 0.8225 0.01491 0.00825 0.0386 0.0265 0.7934
9.750 0.8439 0.01533 0.00869 0.0390 0.0253 0.7955
10.000 0.8656 0.01578 0.00916 0.0394 0.0240 0.7979
10.250 0.8879 0.01621 0.00963 0.0396 0.0231 0.8003
10.500 0.9098 0.01668 0.01012 0.0398 0.0219 0.8031
10.750 0.9309 0.01722 0.01067 0.0401 0.0207 0.8059
11.000 0.9526 0.01773 0.01121 0.0402 0.0199 0.8085
11.250 0.9744 0.01823 0.01174 0.0404 0.0194 0.8109
11.500 0.9967 0.01880 0.01235 0.0403 0.0189 0.8133
11.750 1.0188 0.01942 0.01301 0.0402 0.0182 0.8160
12.000 1.0408 0.02002 0.01365 0.0400 0.0177 0.8188
12.250 1.0607 0.02079 0.01445 0.0400 0.0169 0.8217
12.500 1.0823 0.02142 0.01513 0.0399 0.0165 0.8247
12.750 1.1026 0.02211 0.01588 0.0398 0.0163 0.8274
13.000 1.1239 0.02283 0.01664 0.0396 0.0158 0.8305
13.250 1.1447 0.02364 0.01752 0.0392 0.0155 0.8339
13.500 1.1647 0.02447 0.01841 0.0389 0.0151 0.8376
13.750 1.1838 0.02534 0.01933 0.0387 0.0148 0.8412
14.000 1.2006 0.02636 0.02040 0.0387 0.0145 0.8446
14.250 1.2197 0.02740 0.02150 0.0382 0.0142 0.8481
14.500 1.2363 0.02867 0.02285 0.0377 0.0138 0.8522
14.750 1.2536 0.02976 0.02403 0.0374 0.0137 0.8566
15.000 1.2693 0.03091 0.02525 0.0373 0.0134 0.8611
15.250 1.2837 0.03223 0.02667 0.0370 0.0133 0.8663
15.500 1.2983 0.03350 0.02803 0.0368 0.0130 0.8728
15.750 1.3114 0.03488 0.02951 0.0366 0.0128 0.8802
16.000 1.3240 0.03640 0.03114 0.0363 0.0127 0.8901
16.250 1.3348 0.03818 0.03304 0.0358 0.0124 0.9034
16.750 1.3716 0.04209 0.03725 0.0312 0.0121 0.9673
17.750 1.3805 0.05235 0.04782 0.0310 0.0115 1.0000
18.000 1.3800 0.05538 0.05094 0.0304 0.0115 1.0000
18.250 1.3712 0.05956 0.05523 0.0294 0.0113 1.0000
18.500 1.3646 0.06369 0.05946 0.0281 0.0112 1.0000
18.750 1.3629 0.06730 0.06318 0.0269 0.0111 1.0000
19.000 1.3534 0.07210 0.06809 0.0249 0.0111 1.0000
19.250 1.3429 0.07723 0.07335 0.0227 0.0111 1.0000
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