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