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