LWK 80-150/K25 (lwk80150k25-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: LWK 80-150/K25 (lwk80150k25-il) Reynolds number: 100,000 Max Cl/Cd: 26.69 at α=5.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-lwk80150k25-il-100000-n5.txt Download as CSV file: xf-lwk80150k25-il-100000-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 = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-15.500 -0.7611 0.10633 0.10057 -0.0343 1.0000 0.0389
-15.250 -0.8126 0.09190 0.08591 -0.0436 1.0000 0.0383
-15.000 -0.8454 0.08290 0.07670 -0.0487 1.0000 0.0378
-14.750 -0.8750 0.07565 0.06919 -0.0522 1.0000 0.0379
-14.500 -0.9003 0.06965 0.06291 -0.0542 1.0000 0.0381
-14.250 -0.9208 0.06466 0.05765 -0.0551 1.0000 0.0384
-14.000 -0.9367 0.06041 0.05311 -0.0553 1.0000 0.0387
-13.750 -0.9488 0.05669 0.04909 -0.0549 1.0000 0.0391
-13.500 -0.9562 0.05345 0.04557 -0.0541 1.0000 0.0396
-13.250 -0.9511 0.05130 0.04335 -0.0535 1.0000 0.0401
-13.000 -0.9463 0.04933 0.04131 -0.0528 1.0000 0.0409
-12.750 -0.9412 0.04728 0.03913 -0.0520 1.0000 0.0416
-12.500 -0.9365 0.04547 0.03718 -0.0510 1.0000 0.0429
-12.250 -0.9286 0.04352 0.03504 -0.0500 1.0000 0.0439
-12.000 -0.9217 0.04162 0.03284 -0.0488 1.0000 0.0456
-11.750 -0.9090 0.04006 0.03122 -0.0480 1.0000 0.0470
-11.500 -0.8961 0.03874 0.02990 -0.0472 1.0000 0.0483
-11.250 -0.8825 0.03739 0.02847 -0.0463 1.0000 0.0500
-11.000 -0.8683 0.03610 0.02703 -0.0453 1.0000 0.0522
-10.750 -0.8531 0.03484 0.02567 -0.0444 1.0000 0.0544
-10.500 -0.8407 0.03381 0.02466 -0.0432 1.0000 0.0565
-10.250 -0.8282 0.03284 0.02366 -0.0418 1.0000 0.0590
-10.000 -0.8160 0.03196 0.02265 -0.0402 1.0000 0.0620
-9.750 -0.8028 0.03090 0.02164 -0.0391 0.9929 0.0649
-9.500 -0.7772 0.02990 0.02057 -0.0402 0.9787 0.0694
-9.250 -0.7502 0.02881 0.01941 -0.0415 0.9704 0.0742
-9.000 -0.7237 0.02782 0.01840 -0.0427 0.9636 0.0804
-8.750 -0.6974 0.02682 0.01736 -0.0439 0.9577 0.0871
-8.500 -0.6704 0.02597 0.01643 -0.0450 0.9523 0.0958
-8.250 -0.6471 0.02506 0.01556 -0.0456 0.9461 0.1049
-8.000 -0.6215 0.02421 0.01471 -0.0464 0.9412 0.1159
-7.750 -0.6011 0.02350 0.01401 -0.0462 0.9348 0.1285
-7.500 -0.5804 0.02278 0.01335 -0.0460 0.9294 0.1444
-7.250 -0.5604 0.02211 0.01274 -0.0456 0.9247 0.1641
-7.000 -0.5456 0.02153 0.01224 -0.0441 0.9189 0.1874
-6.750 -0.5309 0.02088 0.01176 -0.0427 0.9137 0.2183
-6.500 -0.5190 0.02027 0.01134 -0.0406 0.9085 0.2559
-6.250 -0.5135 0.01975 0.01106 -0.0373 0.9023 0.2988
-6.000 -0.5051 0.01915 0.01073 -0.0344 0.8976 0.3555
-5.750 -0.4957 0.01859 0.01054 -0.0315 0.8936 0.4237
-5.500 -0.4820 0.01841 0.01084 -0.0287 0.8890 0.5013
-5.250 -0.4465 0.01899 0.01173 -0.0286 0.8866 0.5738
-5.000 -0.4206 0.01946 0.01221 -0.0275 0.8833 0.6122
-4.750 -0.4010 0.01976 0.01244 -0.0257 0.8801 0.6394
-4.500 -0.3861 0.02001 0.01261 -0.0232 0.8765 0.6603
-4.250 -0.3711 0.02038 0.01291 -0.0206 0.8719 0.6775
-4.000 -0.3539 0.02070 0.01315 -0.0184 0.8678 0.6931
-3.750 -0.3343 0.02107 0.01343 -0.0165 0.8647 0.7084
-3.500 -0.2949 0.02191 0.01420 -0.0173 0.8633 0.7178
-3.250 -0.2744 0.02230 0.01452 -0.0156 0.8601 0.7292
-3.000 -0.2640 0.02254 0.01472 -0.0125 0.8549 0.7416
-2.750 -0.2274 0.02313 0.01526 -0.0132 0.8526 0.7474
-2.500 -0.2098 0.02326 0.01532 -0.0113 0.8493 0.7576
-2.250 -0.1788 0.02349 0.01550 -0.0116 0.8471 0.7630
-2.000 -0.1482 0.02369 0.01565 -0.0118 0.8448 0.7680
-1.750 -0.1480 0.02371 0.01565 -0.0074 0.8386 0.7780
-1.500 -0.1176 0.02393 0.01585 -0.0077 0.8357 0.7817
-1.250 -0.0915 0.02401 0.01589 -0.0074 0.8326 0.7866
-1.000 -0.0791 0.02382 0.01564 -0.0049 0.8293 0.7949
-0.750 -0.0565 0.02402 0.01586 -0.0041 0.8249 0.7981
-0.500 -0.0369 0.02413 0.01597 -0.0029 0.8202 0.8022
-0.250 -0.0211 0.02405 0.01587 -0.0010 0.8160 0.8083
0.000 0.0000 0.02391 0.01570 0.0000 0.8129 0.8129
0.250 0.0210 0.02405 0.01587 0.0010 0.8082 0.8160
0.500 0.0369 0.02413 0.01597 0.0029 0.8022 0.8202
0.750 0.0567 0.02401 0.01585 0.0041 0.7980 0.8250
1.000 0.0793 0.02382 0.01564 0.0049 0.7949 0.8293
1.250 0.0914 0.02400 0.01589 0.0074 0.7866 0.8326
1.500 0.1172 0.02394 0.01586 0.0077 0.7817 0.8357
1.750 0.1473 0.02373 0.01567 0.0075 0.7781 0.8387
2.000 0.1476 0.02370 0.01566 0.0119 0.7681 0.8451
2.250 0.1791 0.02348 0.01549 0.0115 0.7629 0.8472
2.500 0.2094 0.02326 0.01533 0.0114 0.7573 0.8494
2.750 0.2277 0.02311 0.01524 0.0132 0.7473 0.8526
3.000 0.2613 0.02258 0.01476 0.0129 0.7408 0.8552
3.250 0.2744 0.02229 0.01452 0.0156 0.7292 0.8601
3.500 0.2950 0.02189 0.01419 0.0173 0.7177 0.8633
3.750 0.3342 0.02108 0.01343 0.0165 0.7085 0.8647
4.000 0.3533 0.02074 0.01319 0.0184 0.6934 0.8679
4.250 0.3710 0.02039 0.01292 0.0206 0.6776 0.8720
4.500 0.3860 0.02001 0.01261 0.0232 0.6604 0.8765
4.750 0.4008 0.01976 0.01244 0.0257 0.6391 0.8802
5.000 0.4207 0.01945 0.01220 0.0275 0.6121 0.8834
5.250 0.4465 0.01898 0.01173 0.0287 0.5733 0.8867
5.500 0.4821 0.01841 0.01083 0.0287 0.5009 0.8890
5.750 0.4959 0.01858 0.01054 0.0315 0.4247 0.8936
6.000 0.5053 0.01914 0.01073 0.0344 0.3557 0.8976
6.250 0.5138 0.01975 0.01105 0.0372 0.2992 0.9023
6.500 0.5190 0.02028 0.01134 0.0406 0.2558 0.9085
6.750 0.5311 0.02087 0.01175 0.0426 0.2188 0.9137
7.000 0.5461 0.02152 0.01224 0.0440 0.1877 0.9189
7.250 0.5608 0.02209 0.01273 0.0455 0.1647 0.9247
7.500 0.5806 0.02278 0.01334 0.0460 0.1445 0.9294
7.750 0.6014 0.02350 0.01401 0.0461 0.1286 0.9348
8.000 0.6220 0.02420 0.01472 0.0464 0.1165 0.9412
8.250 0.6475 0.02505 0.01555 0.0455 0.1050 0.9461
8.500 0.6706 0.02597 0.01641 0.0449 0.0961 0.9524
8.750 0.6980 0.02680 0.01735 0.0438 0.0874 0.9577
9.000 0.7242 0.02782 0.01839 0.0427 0.0804 0.9637
9.250 0.7508 0.02879 0.01940 0.0413 0.0743 0.9705
9.500 0.7777 0.02985 0.02054 0.0401 0.0692 0.9789
9.750 0.8031 0.03086 0.02161 0.0390 0.0647 0.9936
10.000 0.8159 0.03193 0.02262 0.0402 0.0618 1.0000
10.250 0.8285 0.03283 0.02365 0.0418 0.0590 1.0000
10.500 0.8407 0.03379 0.02465 0.0432 0.0563 1.0000
10.750 0.8530 0.03484 0.02564 0.0443 0.0542 1.0000
11.000 0.8679 0.03609 0.02704 0.0453 0.0517 1.0000
11.250 0.8826 0.03738 0.02846 0.0462 0.0498 1.0000
11.500 0.8963 0.03872 0.02988 0.0471 0.0482 1.0000
11.750 0.9096 0.04006 0.03122 0.0479 0.0468 1.0000
12.000 0.9229 0.04164 0.03286 0.0487 0.0457 1.0000
12.250 0.9305 0.04357 0.03508 0.0498 0.0441 1.0000
12.500 0.9365 0.04547 0.03718 0.0509 0.0426 1.0000
12.750 0.9421 0.04732 0.03916 0.0519 0.0416 1.0000
13.000 0.9472 0.04923 0.04118 0.0527 0.0407 1.0000
13.250 0.9526 0.05124 0.04327 0.0534 0.0400 1.0000
13.500 0.9578 0.05347 0.04555 0.0540 0.0394 1.0000
13.750 0.9492 0.05674 0.04915 0.0547 0.0390 1.0000
14.000 0.9363 0.06057 0.05329 0.0551 0.0386 1.0000
14.250 0.9208 0.06477 0.05777 0.0549 0.0383 1.0000
14.500 0.8998 0.06983 0.06311 0.0539 0.0379 1.0000
14.750 0.8760 0.07568 0.06922 0.0520 0.0378 1.0000
15.000 0.8440 0.08336 0.07717 0.0482 0.0377 1.0000
15.250 0.8053 0.09357 0.08762 0.0422 0.0382 1.0000
15.500 0.7414 0.11140 0.10571 0.0307 0.0389 1.0000
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