XFOIL Version 6.94 Calculated polar for: WHITCOMB INTEGRAL SUPERCRITICAL 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.080 Re = 0.300 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------- -------- --------- --------- -------- ------- ------- 0.000 0.1372 0.01874 0.01448 -0.0583 0.9644 0.7278 0.500 0.1964 0.01861 0.01446 -0.0560 0.9472 0.7387 1.000 0.2871 0.01730 0.01325 -0.0608 0.9236 0.7496 1.500 0.3435 0.01600 0.01206 -0.0586 0.8849 0.7550 2.000 0.4513 0.01691 0.01076 -0.0671 0.3899 0.7596 2.500 0.5178 0.01855 0.01133 -0.0717 0.1824 0.7656 3.000 0.5598 0.01896 0.01132 -0.0688 0.1126 0.7679 3.500 0.6048 0.01949 0.01172 -0.0663 0.0869 0.7712 4.000 0.6602 0.02017 0.01230 -0.0666 0.0735 0.7727 4.500 0.7164 0.02093 0.01301 -0.0670 0.0647 0.7745 5.000 0.7731 0.02184 0.01389 -0.0676 0.0580 0.7767 5.500 0.8325 0.02303 0.01507 -0.0688 0.0530 0.7775 6.000 0.8923 0.02450 0.01651 -0.0701 0.0490 0.7782 6.500 0.9511 0.02577 0.01785 -0.0711 0.0453 0.7800 8.000 1.1180 0.03318 0.02596 -0.0727 0.0393 0.7816 8.500 1.1570 0.03745 0.03106 -0.0704 0.0381 0.7824 9.000 1.1860 0.04252 0.03685 -0.0671 0.0369 0.7835 9.500 1.1741 0.05274 0.04821 -0.0596 0.0375 0.7835 10.000 1.1178 0.06578 0.06219 -0.0499 0.0405 0.7834 10.500 1.1165 0.07000 0.06650 -0.0462 0.0400 0.7835 12.500 0.6474 0.15066 0.14814 -0.0715 0.0513 0.7837 13.000 0.6622 0.15486 0.15234 -0.0720 0.0502 0.7839 13.500 0.6420 0.16281 0.16030 -0.0777 0.0482 0.7841 14.000 0.6469 0.16815 0.16565 -0.0805 0.0458 0.7842 14.500 0.6690 0.17261 0.17012 -0.0807 0.0447 0.7844 15.000 0.6537 0.18001 0.17753 -0.0869 0.0426 0.7846 15.500 0.6618 0.18531 0.18285 -0.0896 0.0408 0.7848 16.000 0.6765 0.19019 0.18773 -0.0910 0.0399 0.7854 16.500 0.6748 0.19688 0.19444 -0.0952 0.0389 0.7861 17.000 0.6804 0.20270 0.20030 -0.0985 0.0368 0.7866 17.500 0.6915 0.20770 0.20532 -0.1006 0.0355 0.7869 18.000 0.7126 0.21362 0.21125 -0.1008 0.0350 0.7873 18.500 0.7031 0.22003 0.21769 -0.1070 0.0333 0.7876 19.000 0.7116 0.22559 0.22328 -0.1097 0.0319 0.7880 19.500 0.7223 0.23080 0.22851 -0.1118 0.0311 0.7884 20.000 0.7352 0.23699 0.23472 -0.1133 0.0307 0.7889 20.500 0.7338 0.24360 0.24136 -0.1182 0.0291 0.7893 21.000 0.7421 0.24930 0.24709 -0.1208 0.0278 0.7898 21.500 0.7517 0.25468 0.25250 -0.1230 0.0270 0.7904 22.000 0.7601 0.26110 0.25894 -0.1252 0.0267 0.7909 22.500 0.7629 0.26799 0.26587 -0.1292 0.0253 0.7915 23.000 0.7703 0.27377 0.27168 -0.1317 0.0239 0.7925 23.500 0.7793 0.27933 0.27728 -0.1337 0.0232 0.7938 24.000 0.7827 0.28678 0.28476 -0.1371 0.0225 0.7946 24.500 0.7891 0.29326 0.29127 -0.1399 0.0206 0.7953 25.000 0.7965 0.29891 0.29695 -0.1422 0.0198 0.7961 25.500 0.8008 0.30637 0.30442 -0.1451 0.0193 0.7969 26.000 0.8061 0.31339 0.31148 -0.1480 0.0176 0.7977 26.500 0.8121 0.31938 0.31749 -0.1505 0.0167 0.7987 27.500 0.8216 0.33350 0.33166 -0.1559 0.0158 0.8007 28.000 0.8264 0.34033 0.33852 -0.1586 0.0148 0.8018 28.500 0.8311 0.34660 0.34481 -0.1612 0.0140 0.8030 29.000 0.8357 0.35256 0.35080 -0.1636 0.0136 0.8041 30.000 0.8428 0.36625 0.36455 -0.1688 0.0132 0.8071 30.500 0.8461 0.37334 0.37168 -0.1714 0.0128 0.8088 31.000 0.8493 0.37992 0.37829 -0.1740 0.0122 0.8107 31.500 0.8521 0.38623 0.38465 -0.1764 0.0116 0.8132 32.000 0.8548 0.39220 0.39065 -0.1788 0.0111 0.8162 32.500 0.8573 0.39785 0.39634 -0.1811 0.0107 0.8192 33.500 0.8608 0.41217 0.41072 -0.1862 0.0103 0.8244 34.000 0.8624 0.41887 0.41746 -0.1886 0.0095 0.8279 34.500 0.8636 0.42494 0.42358 -0.1909 0.0087 0.8321 35.000 0.8644 0.43039 0.42906 -0.1932 0.0083 0.8374 36.000 0.8651 0.44434 0.44309 -0.1977 0.0078 0.8506 36.500 0.8652 0.45069 0.44949 -0.1999 0.0070 0.8622 37.000 0.8647 0.45597 0.45486 -0.2019 0.0064 0.8895 37.500 0.8638 0.46071 0.45964 -0.2040 0.0061 1.0000 38.000 0.8634 0.46804 0.46697 -0.2064 0.0060 1.0000 38.500 0.8631 0.47520 0.47414 -0.2086 0.0057 1.0000 39.000 0.8622 0.48132 0.48028 -0.2109 0.0049 1.0000 39.500 0.8609 0.48650 0.48547 -0.2131 0.0045 1.0000 40.500 0.8571 0.49837 0.49736 -0.2173 0.0042 1.0000 41.000 0.8551 0.50447 0.50347 -0.2192 0.0039 1.0000 41.500 0.8528 0.50994 0.50895 -0.2212 0.0035 1.0000 42.000 0.8501 0.51467 0.51371 -0.2233 0.0031 1.0000 43.000 0.8437 0.52451 0.52358 -0.2273 0.0028 1.0000 43.500 0.8406 0.53015 0.52924 -0.2291 0.0027 1.0000 44.000 0.8371 0.53510 0.53421 -0.2310 0.0024 1.0000 44.500 0.8332 0.53935 0.53848 -0.2328 0.0021 1.0000 45.000 0.8290 0.54300 0.54215 -0.2347 0.0019 1.0000 46.500 0.8153 0.55521 0.55441 -0.2401 0.0017 1.0000 47.000 0.8106 0.55938 0.55860 -0.2418 0.0016 1.0000 47.500 0.8054 0.56266 0.56190 -0.2435 0.0014 1.0000 48.000 0.8000 0.56566 0.56493 -0.2452 0.0012 1.0000 48.500 0.7943 0.56814 0.56742 -0.2469 0.0010 1.0000 49.000 0.7882 0.56993 0.56923 -0.2487 0.0009 1.0000 50.500 0.7699 0.57816 0.57753 -0.2534 0.0009 1.0000 51.000 0.7635 0.58042 0.57980 -0.2549 0.0008 1.0000 51.500 0.7569 0.58223 0.58163 -0.2563 0.0007 1.0000 52.000 0.7500 0.58359 0.58302 -0.2578 0.0006 1.0000 52.500 0.7429 0.58459 0.58403 -0.2593 0.0005 1.0000 53.000 0.7356 0.58522 0.58469 -0.2608 0.0004 1.0000 53.500 0.7281 0.58544 0.58493 -0.2623 0.0004 1.0000 54.000 0.7202 0.58510 0.58461 -0.2638 0.0003 1.0000 55.000 0.7052 0.58729 0.58683 -0.2663 0.0003 1.0000 55.500 0.6973 0.58731 0.58687 -0.2675 0.0002 1.0000 56.000 0.6892 0.58674 0.58633 -0.2688 0.0002 1.0000 56.500 0.6808 0.58568 0.58528 -0.2702 0.0001 1.0000 57.500 0.6642 0.58487 0.58451 -0.2724 0.0001 1.0000 58.000 0.6556 0.58379 0.58344 -0.2736 0.0001 1.0000 58.500 0.6469 0.58240 0.58207 -0.2747 0.0000 1.0000 59.000 0.6381 0.58043 0.58012 -0.2759 0.0000 1.0000