LWK 80-150/K25 (lwk80150k25-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: LWK 80-150/K25 (lwk80150k25-il) Reynolds number: 500,000 Max Cl/Cd: 44.02 at α=8.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-lwk80150k25-il-500000-n5.txt Download as CSV file: xf-lwk80150k25-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0874 0.12483 0.12132 -0.0032 1.0000 0.0143
-19.500 -1.1069 0.11696 0.11332 -0.0075 1.0000 0.0143
-19.250 -1.1249 0.10953 0.10578 -0.0116 1.0000 0.0144
-19.000 -1.1421 0.10239 0.09850 -0.0154 1.0000 0.0144
-18.750 -1.1561 0.09584 0.09183 -0.0190 1.0000 0.0147
-18.500 -1.1712 0.08936 0.08522 -0.0223 1.0000 0.0147
-18.250 -1.1815 0.08375 0.07949 -0.0252 1.0000 0.0149
-18.000 -1.1940 0.07803 0.07363 -0.0279 1.0000 0.0148
-17.750 -1.1995 0.07346 0.06895 -0.0300 1.0000 0.0151
-17.500 -1.2086 0.06864 0.06400 -0.0320 1.0000 0.0150
-17.250 -1.2127 0.06463 0.05987 -0.0335 1.0000 0.0152
-17.000 -1.2152 0.06096 0.05610 -0.0348 1.0000 0.0153
-16.750 -1.2154 0.05772 0.05275 -0.0357 1.0000 0.0156
-16.500 -1.2155 0.05464 0.04955 -0.0364 1.0000 0.0158
-16.250 -1.2152 0.05171 0.04651 -0.0369 1.0000 0.0159
-16.000 -1.2127 0.04912 0.04382 -0.0372 1.0000 0.0160
-15.750 -1.2107 0.04658 0.04117 -0.0373 1.0000 0.0164
-15.500 -1.2052 0.04448 0.03897 -0.0373 1.0000 0.0166
-15.250 -1.2000 0.04241 0.03679 -0.0371 1.0000 0.0168
-14.750 -1.1874 0.03837 0.03261 -0.0364 0.9633 0.0171
-14.500 -1.1638 0.03617 0.03029 -0.0401 0.9359 0.0176
-14.250 -1.1380 0.03434 0.02833 -0.0435 0.9211 0.0180
-14.000 -1.1151 0.03278 0.02665 -0.0458 0.9087 0.0185
-13.750 -1.0937 0.03150 0.02526 -0.0473 0.8985 0.0190
-13.500 -1.0741 0.03030 0.02393 -0.0483 0.8906 0.0196
-13.250 -1.0556 0.02917 0.02268 -0.0489 0.8835 0.0200
-13.000 -1.0377 0.02799 0.02140 -0.0494 0.8777 0.0206
-12.750 -1.0222 0.02682 0.02016 -0.0494 0.8721 0.0209
-12.500 -1.0034 0.02589 0.01917 -0.0497 0.8670 0.0217
-12.000 -0.9656 0.02420 0.01732 -0.0498 0.8582 0.0230
-11.750 -0.9469 0.02342 0.01647 -0.0496 0.8537 0.0238
-11.500 -0.9280 0.02265 0.01562 -0.0494 0.8496 0.0245
-11.250 -0.9092 0.02188 0.01480 -0.0493 0.8462 0.0255
-11.000 -0.8903 0.02121 0.01410 -0.0489 0.8430 0.0267
-10.750 -0.8714 0.02058 0.01341 -0.0484 0.8397 0.0278
-10.500 -0.8520 0.01999 0.01276 -0.0479 0.8363 0.0287
-10.250 -0.8334 0.01936 0.01212 -0.0473 0.8332 0.0303
-10.000 -0.8138 0.01881 0.01153 -0.0468 0.8303 0.0318
-9.750 -0.7938 0.01832 0.01098 -0.0462 0.8274 0.0335
-9.500 -0.7758 0.01777 0.01043 -0.0453 0.8242 0.0354
-9.250 -0.7569 0.01729 0.00993 -0.0445 0.8212 0.0379
-9.000 -0.7376 0.01684 0.00944 -0.0436 0.8184 0.0399
-8.750 -0.7193 0.01636 0.00896 -0.0426 0.8158 0.0432
-8.500 -0.6999 0.01596 0.00852 -0.0417 0.8134 0.0462
-8.250 -0.6816 0.01552 0.00808 -0.0405 0.8110 0.0497
-8.000 -0.6631 0.01514 0.00770 -0.0393 0.8084 0.0531
-7.750 -0.6458 0.01473 0.00731 -0.0379 0.8055 0.0582
-7.500 -0.6275 0.01439 0.00695 -0.0365 0.8028 0.0622
-7.250 -0.6109 0.01400 0.00659 -0.0349 0.8002 0.0690
-7.000 -0.5936 0.01366 0.00626 -0.0332 0.7979 0.0754
-6.750 -0.5762 0.01336 0.00595 -0.0315 0.7958 0.0824
-6.500 -0.5593 0.01307 0.00568 -0.0297 0.7937 0.0901
-6.250 -0.5425 0.01282 0.00545 -0.0278 0.7914 0.0981
-6.000 -0.5264 0.01255 0.00523 -0.0257 0.7888 0.1092
-5.750 -0.5090 0.01225 0.00499 -0.0240 0.7862 0.1230
-5.500 -0.4906 0.01195 0.00476 -0.0224 0.7838 0.1387
-5.250 -0.4728 0.01161 0.00452 -0.0207 0.7817 0.1607
-5.000 -0.4544 0.01129 0.00429 -0.0191 0.7798 0.1862
-4.750 -0.4360 0.01095 0.00406 -0.0175 0.7779 0.2150
-4.500 -0.4187 0.01055 0.00383 -0.0158 0.7758 0.2543
-4.250 -0.4016 0.01014 0.00361 -0.0140 0.7735 0.2965
-4.000 -0.3844 0.00971 0.00338 -0.0122 0.7710 0.3431
-3.750 -0.3692 0.00920 0.00313 -0.0100 0.7688 0.4045
-3.500 -0.3543 0.00868 0.00288 -0.0077 0.7666 0.4694
-3.250 -0.3390 0.00820 0.00269 -0.0053 0.7644 0.5382
-3.000 -0.3196 0.00791 0.00261 -0.0036 0.7624 0.5933
-2.750 -0.2960 0.00781 0.00260 -0.0027 0.7605 0.6273
-2.500 -0.2705 0.00778 0.00262 -0.0022 0.7588 0.6483
-2.250 -0.2445 0.00777 0.00264 -0.0018 0.7568 0.6645
-2.000 -0.2181 0.00777 0.00266 -0.0014 0.7545 0.6777
-1.750 -0.1917 0.00779 0.00268 -0.0011 0.7523 0.6905
-1.500 -0.1645 0.00781 0.00273 -0.0009 0.7502 0.6994
-1.250 -0.1377 0.00784 0.00272 -0.0006 0.7481 0.7084
-1.000 -0.1100 0.00788 0.00279 -0.0005 0.7460 0.7155
-0.750 -0.0826 0.00792 0.00280 -0.0003 0.7440 0.7224
-0.500 -0.0548 0.00795 0.00283 -0.0002 0.7421 0.7279
-0.250 -0.0274 0.00799 0.00291 -0.0001 0.7396 0.7328
0.000 0.0000 0.00800 0.00294 0.0000 0.7366 0.7366
0.250 0.0274 0.00799 0.00291 0.0001 0.7327 0.7396
0.500 0.0548 0.00796 0.00283 0.0002 0.7280 0.7421
0.750 0.0827 0.00792 0.00280 0.0003 0.7225 0.7441
1.000 0.1100 0.00787 0.00279 0.0005 0.7152 0.7460
1.250 0.1377 0.00784 0.00272 0.0006 0.7083 0.7480
1.500 0.1646 0.00781 0.00273 0.0009 0.6993 0.7502
1.750 0.1917 0.00779 0.00268 0.0011 0.6906 0.7523
2.000 0.2181 0.00777 0.00266 0.0014 0.6776 0.7546
2.250 0.2445 0.00777 0.00264 0.0018 0.6645 0.7568
2.500 0.2705 0.00778 0.00262 0.0022 0.6482 0.7589
2.750 0.2958 0.00782 0.00260 0.0028 0.6261 0.7605
3.000 0.3197 0.00791 0.00261 0.0036 0.5937 0.7623
3.250 0.3394 0.00818 0.00269 0.0052 0.5408 0.7644
3.500 0.3545 0.00867 0.00288 0.0076 0.4704 0.7666
3.750 0.3691 0.00920 0.00313 0.0100 0.4040 0.7688
4.000 0.3848 0.00970 0.00337 0.0121 0.3453 0.7710
4.250 0.4014 0.01015 0.00361 0.0140 0.2950 0.7734
4.500 0.4185 0.01056 0.00383 0.0158 0.2534 0.7758
4.750 0.4363 0.01094 0.00405 0.0175 0.2167 0.7779
5.000 0.4544 0.01129 0.00428 0.0191 0.1860 0.7798
5.250 0.4730 0.01161 0.00452 0.0207 0.1612 0.7817
5.750 0.5091 0.01225 0.00499 0.0240 0.1230 0.7862
6.000 0.5266 0.01254 0.00523 0.0257 0.1096 0.7888
6.250 0.5430 0.01280 0.00545 0.0277 0.0991 0.7914
6.500 0.5597 0.01306 0.00568 0.0296 0.0909 0.7937
6.750 0.5763 0.01336 0.00595 0.0315 0.0820 0.7958
7.000 0.5934 0.01368 0.00626 0.0332 0.0746 0.7979
7.250 0.6110 0.01400 0.00659 0.0348 0.0688 0.8002
7.750 0.6460 0.01473 0.00731 0.0378 0.0582 0.8056
8.000 0.6633 0.01514 0.00770 0.0393 0.0535 0.8084
8.250 0.6819 0.01552 0.00808 0.0405 0.0500 0.8110
8.500 0.7004 0.01595 0.00851 0.0416 0.0465 0.8134
8.750 0.7197 0.01635 0.00896 0.0425 0.0434 0.8158
9.000 0.7382 0.01683 0.00943 0.0435 0.0401 0.8184
9.250 0.7575 0.01727 0.00992 0.0444 0.0380 0.8212
9.500 0.7764 0.01775 0.01041 0.0452 0.0354 0.8243
9.750 0.7944 0.01833 0.01099 0.0461 0.0337 0.8274
10.000 0.8144 0.01881 0.01153 0.0467 0.0319 0.8302
10.250 0.8341 0.01936 0.01212 0.0472 0.0304 0.8332
10.500 0.8527 0.01999 0.01276 0.0478 0.0286 0.8363
10.750 0.8726 0.02055 0.01339 0.0482 0.0272 0.8396
11.000 0.8914 0.02120 0.01409 0.0487 0.0263 0.8429
11.250 0.9104 0.02186 0.01478 0.0491 0.0254 0.8462
11.500 0.9290 0.02266 0.01562 0.0493 0.0242 0.8496
11.750 0.9483 0.02341 0.01646 0.0494 0.0234 0.8537
12.000 0.9668 0.02421 0.01733 0.0496 0.0230 0.8580
12.500 1.0047 0.02591 0.01917 0.0494 0.0213 0.8670
12.750 1.0225 0.02693 0.02026 0.0492 0.0209 0.8721
13.000 1.0393 0.02800 0.02139 0.0491 0.0202 0.8775
13.250 1.0577 0.02913 0.02265 0.0486 0.0199 0.8834
13.500 1.0775 0.03017 0.02379 0.0479 0.0192 0.8903
13.750 1.0953 0.03151 0.02526 0.0470 0.0189 0.8983
14.000 1.1157 0.03287 0.02674 0.0455 0.0184 0.9084
14.250 1.1397 0.03432 0.02832 0.0432 0.0180 0.9208
14.500 1.1653 0.03616 0.03026 0.0399 0.0174 0.9354
14.750 1.1882 0.03841 0.03264 0.0362 0.0171 0.9620
15.000 1.1964 0.04043 0.03473 0.0366 0.0167 1.0000
15.250 1.2025 0.04233 0.03674 0.0368 0.0166 1.0000
15.500 1.2071 0.04447 0.03896 0.0370 0.0164 1.0000
15.750 1.2115 0.04667 0.04127 0.0370 0.0162 1.0000
16.000 1.2156 0.04900 0.04369 0.0369 0.0161 1.0000
16.250 1.2167 0.05175 0.04655 0.0366 0.0158 1.0000
16.500 1.2181 0.05456 0.04948 0.0361 0.0157 1.0000
16.750 1.2183 0.05761 0.05263 0.0354 0.0155 1.0000
17.000 1.2169 0.06099 0.05612 0.0344 0.0153 1.0000
17.250 1.2136 0.06476 0.06001 0.0331 0.0152 1.0000
17.500 1.2083 0.06896 0.06432 0.0315 0.0150 1.0000
17.750 1.2010 0.07357 0.06905 0.0296 0.0150 1.0000
18.000 1.1939 0.07835 0.07396 0.0274 0.0149 1.0000
18.250 1.1853 0.08359 0.07931 0.0247 0.0146 1.0000
18.500 1.1742 0.08930 0.08515 0.0218 0.0146 1.0000
18.750 1.1606 0.09559 0.09157 0.0186 0.0145 1.0000
19.000 1.1442 0.10245 0.09857 0.0150 0.0145 1.0000
19.250 1.1289 0.10933 0.10556 0.0112 0.0144 1.0000
|
Polar data table (+)
Polar graphs
<< Back to LWK 80-150/K25 (lwk80150k25-il)