S809 SPOILER FLAP, LEGR, CHORD = 18 INCHES --------- Run Conditions: vel=102.7 ft/s Re=1.001x10^6 AOA=-6.01 Flap deflection=5.00 Totals: Cl=-0.1823 Cdp=-0.0019 Cm(c/4)=-0.0434 Cs=0.0209 Ch=0.0547 Main component: Cl=-0.2363 Cdp=-0.0024 Cm=0.0360 Flap component: Cl=0.0539 Cdp=0.0006 Cm=-0.0341 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.0837 0.5905, -0.01667, 0.0942 0.5709, 0.03110, 0.0095 0.5889, 0.07933, 0.0066 0.5500, 0.08689, -0.2544 0.5110, 0.09367, -0.5022 0.4731, 0.09830, -0.5593 0.4349, 0.10070, -0.5688 0.3960, 0.10120, -0.5243 0.3566, 0.10020, -0.4735 0.3172, 0.09790, -0.4069 0.2778, 0.09440, -0.3579 0.2393, 0.08960, -0.3050 0.2056, 0.08360, -0.2317 0.1633, 0.07610, -0.1352 0.1261, 0.06710, -0.0070 0.0900, 0.05640, 0.1122 0.0571, 0.04390, 0.3504 0.0283, 0.02940, 0.6264 0.0142, 0.01970, 0.8624 0.0081, 0.01410, 0.9633 0.0026, 0.00780, 0.8679 0.0000, 0.00000, 0.2449 0.0037, -0.00840, -0.6541 0.0112, -0.01420, -0.6616 0.0191, -0.01930, -0.5798 0.0397, -0.03030, -0.4371 0.0706, -0.04420, -0.5496 0.1037, -0.05710, -0.5753 0.1384, -0.06890, -0.6683 0.1741, -0.07950, -0.7239 0.2102, -0.08660, -0.7817 0.2472, -0.09640, -0.8548 0.2844, -0.10270, -0.8759 0.3225, -0.10690, -0.8824 0.3608, -0.10890, -0.8528 0.3991, -0.10830, -0.7722 0.4373, -0.10510, -0.5923 0.4757, -0.09890, -0.3672 0.5137, -0.09067, -0.1676 0.5611, -0.07859, -0.1047 16 Flap element taps 1.0000, 0.00130, -0.0143 0.9365, 0.01390, -0.0438 0.8333, 0.03280, -0.1415 0.7436, 0.04930, -0.2556 0.7049, 0.05667, -0.2935 0.6662, 0.06411, -0.4251 0.6274, 0.07172, -0.8769 0.6009, 0.07523, -1.0921 0.6069, 0.02889, -0.0057 0.6079, -0.01747, 0.0591 0.6167, -0.06381, -0.1221 0.6558, -0.05300, -0.1374 0.7045, -0.04117, -0.1406 0.7429, -0.03210, -0.1281 0.8333, -0.01400, -0.1467 0.9311, -0.00120, -0.1264 Wake drag found for this condition, Cdw=0.0337 --------- Run Conditions: vel=102.8 ft/s Re=1.002x10^6 AOA=0.01 Flap deflection=5.00 Totals: Cl=0.2146 Cdp=-0.0027 Cm(c/4)=-0.0684 Cs=0.0028 Ch=0.0596 Main component: Cl=0.0596 Cdp=0.0032 Cm=-0.0075 Flap component: Cl=0.1550 Cdp=-0.0059 Cm=-0.1145 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.0388 0.5905, -0.01667, -0.0355 0.5709, 0.03110, -0.0316 0.5889, 0.07933, -0.0436 0.5500, 0.08689, -0.2277 0.5110, 0.09367, -0.5075 0.4731, 0.09830, -0.6323 0.4349, 0.10070, -0.6918 0.3960, 0.10120, -0.6899 0.3566, 0.10020, -0.6786 0.3172, 0.09790, -0.6483 0.2778, 0.09440, -0.6396 0.2393, 0.08960, -0.6263 0.2056, 0.08360, -0.5944 0.1633, 0.07610, -0.5447 0.1261, 0.06710, -0.4660 0.0900, 0.05640, -0.4293 0.0571, 0.04390, -0.2603 0.0283, 0.02940, -0.0689 0.0142, 0.01970, 0.1588 0.0081, 0.01410, 0.3874 0.0026, 0.00780, 0.5611 0.0000, 0.00000, 0.9835 0.0037, -0.00840, 0.7159 0.0112, -0.01420, 0.4719 0.0191, -0.01930, 0.3685 0.0397, -0.03030, 0.2444 0.0706, -0.04420, 0.0170 0.1037, -0.05710, -0.0993 0.1384, -0.06890, -0.2514 0.1741, -0.07950, -0.3654 0.2102, -0.08660, -0.4697 0.2472, -0.09640, -0.5906 0.2844, -0.10270, -0.6653 0.3225, -0.10690, -0.7338 0.3608, -0.10890, -0.7720 0.3991, -0.10830, -0.7727 0.4373, -0.10510, -0.6871 0.4757, -0.09890, -0.5591 0.5137, -0.09067, -0.3422 0.5611, -0.07859, -0.1645 16 Flap element taps 1.0000, 0.00130, 0.1176 0.9365, 0.01390, 0.0475 0.8333, 0.03280, -0.1099 0.7436, 0.04930, -0.3031 0.7049, 0.05667, -0.4298 0.6662, 0.06411, -0.6147 0.6274, 0.07172, -0.9362 0.6009, 0.07523, -1.2286 0.6069, 0.02889, -0.0395 0.6079, -0.01747, -0.0380 0.6167, -0.06381, -0.0240 0.6558, -0.05300, -0.0364 0.7045, -0.04117, 0.0171 0.7429, -0.03210, 0.0926 0.8333, -0.01400, 0.1993 0.9311, -0.00120, 0.2505 Wake drag found for this condition, Cdw=0.0274 --------- Run Conditions: vel=103.0 ft/s Re=1.002x10^6 AOA=3.00 Flap deflection=5.00 Totals: Cl=0.4575 Cdp=0.0188 Cm(c/4)=-0.0830 Cs=0.0052 Ch=0.0465 Main component: Cl=0.2576 Cdp=0.0097 Cm=-0.0448 Flap component: Cl=0.1999 Cdp=0.0091 Cm=-0.1527 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.0715 0.5905, -0.01667, -0.0968 0.5709, 0.03110, -0.0889 0.5889, 0.07933, -0.0969 0.5500, 0.08689, -0.2186 0.5110, 0.09367, -0.4837 0.4731, 0.09830, -0.6459 0.4349, 0.10070, -0.7400 0.3960, 0.10120, -0.7661 0.3566, 0.10020, -0.7828 0.3172, 0.09790, -0.7760 0.2778, 0.09440, -0.7913 0.2393, 0.08960, -0.8057 0.2056, 0.08360, -0.8035 0.1633, 0.07610, -0.7846 0.1261, 0.06710, -0.7452 0.0900, 0.05640, -0.7719 0.0571, 0.04390, -0.6697 0.0283, 0.02940, -0.5926 0.0142, 0.01970, -0.4814 0.0081, 0.01410, -0.2207 0.0026, 0.00780, -0.0443 0.0000, 0.00000, 0.6043 0.0037, -0.00840, 0.9802 0.0112, -0.01420, 0.8340 0.0191, -0.01930, 0.7182 0.0397, -0.03030, 0.5415 0.0706, -0.04420, 0.2954 0.1037, -0.05710, 0.1494 0.1384, -0.06890, -0.0166 0.1741, -0.07950, -0.1494 0.2102, -0.08660, -0.2636 0.2472, -0.09640, -0.4024 0.2844, -0.10270, -0.4862 0.3225, -0.10690, -0.5686 0.3608, -0.10890, -0.6285 0.3991, -0.10830, -0.6556 0.4373, -0.10510, -0.5957 0.4757, -0.09890, -0.5007 0.5137, -0.09067, -0.3046 0.5611, -0.07859, -0.1542 16 Flap element taps 1.0000, 0.00130, -0.0195 0.9365, 0.01390, -0.1018 0.8333, 0.03280, -0.2705 0.7436, 0.04930, -0.3948 0.7049, 0.05667, -0.4802 0.6662, 0.06411, -0.5780 0.6274, 0.07172, -0.7489 0.6009, 0.07523, -0.9858 0.6069, 0.02889, -0.0962 0.6079, -0.01747, -0.0973 0.6167, -0.06381, -0.0737 0.6558, -0.05300, -0.0198 0.7045, -0.04117, 0.1665 0.7429, -0.03210, 0.2481 0.8333, -0.01400, 0.2587 0.9311, -0.00120, 0.2362 Wake drag found for this condition, Cdw=0.0363 --------- Run Conditions: vel=103.1 ft/s Re=1.002x10^6 AOA=6.04 Flap deflection=5.00 Totals: Cl=0.5929 Cdp=0.0378 Cm(c/4)=-0.0688 Cs=0.0248 Ch=0.0175 Main component: Cl=0.4050 Cdp=0.0160 Cm=-0.0687 Flap component: Cl=0.1879 Cdp=0.0218 Cm=-0.1485 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.0990 0.5905, -0.01667, -0.1337 0.5709, 0.03110, -0.1243 0.5889, 0.07933, -0.1329 0.5500, 0.08689, -0.2026 0.5110, 0.09367, -0.4124 0.4731, 0.09830, -0.5967 0.4349, 0.10070, -0.7228 0.3960, 0.10120, -0.7822 0.3566, 0.10020, -0.8268 0.3172, 0.09790, -0.8483 0.2778, 0.09440, -0.8914 0.2393, 0.08960, -0.9348 0.2056, 0.08360, -0.9631 0.1633, 0.07610, -0.9820 0.1261, 0.06710, -0.9840 0.0900, 0.05640, -1.0744 0.0571, 0.04390, -1.0564 0.0283, 0.02940, -1.1187 0.0142, 0.01970, -1.1611 0.0081, 0.01410, -0.9029 0.0026, 0.00780, -0.8097 0.0000, 0.00000, -0.2665 0.0037, -0.00840, 0.9416 0.0112, -0.01420, 0.9815 0.0191, -0.01930, 0.9108 0.0397, -0.03030, 0.7396 0.0706, -0.04420, 0.5007 0.1037, -0.05710, 0.3417 0.1384, -0.06890, 0.1694 0.1741, -0.07950, 0.0244 0.2102, -0.08660, -0.1063 0.2472, -0.09640, -0.2508 0.2844, -0.10270, -0.3578 0.3225, -0.10690, -0.4516 0.3608, -0.10890, -0.5240 0.3991, -0.10830, -0.5695 0.4373, -0.10510, -0.5307 0.4757, -0.09890, -0.4562 0.5137, -0.09067, -0.2770 0.5611, -0.07859, -0.1470 16 Flap element taps 1.0000, 0.00130, -0.2045 0.9365, 0.01390, -0.3100 0.8333, 0.03280, -0.3164 0.7436, 0.04930, -0.3410 0.7049, 0.05667, -0.3586 0.6662, 0.06411, -0.3864 0.6274, 0.07172, -0.4651 0.6009, 0.07523, -0.6266 0.6069, 0.02889, -0.1318 0.6079, -0.01747, -0.1352 0.6167, -0.06381, -0.1059 0.6558, -0.05300, -0.0129 0.7045, -0.04117, 0.2585 0.7429, -0.03210, 0.2776 0.8333, -0.01400, 0.2280 0.9311, -0.00120, 0.1692 --------- Run Conditions: vel=103.1 ft/s Re=1.001x10^6 AOA=9.02 Flap deflection=5.00 Totals: Cl=0.7537 Cdp=0.0537 Cm(c/4)=-0.0581 Cs=0.0651 Ch=0.0168 Main component: Cl=0.5655 Cdp=0.0288 Cm=-0.0972 Flap component: Cl=0.1881 Cdp=0.0249 Cm=-0.1491 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1301 0.5905, -0.01667, -0.2103 0.5709, 0.03110, -0.1961 0.5889, 0.07933, -0.2084 0.5500, 0.08689, -0.2422 0.5110, 0.09367, -0.3711 0.4731, 0.09830, -0.5510 0.4349, 0.10070, -0.7050 0.3960, 0.10120, -0.7967 0.3566, 0.10020, -0.8727 0.3172, 0.09790, -0.9245 0.2778, 0.09440, -0.9959 0.2393, 0.08960, -1.0685 0.2056, 0.08360, -1.1304 0.1633, 0.07610, -1.1882 0.1261, 0.06710, -1.2430 0.0900, 0.05640, -1.4012 0.0571, 0.04390, -1.4882 0.0283, 0.02940, -1.7260 0.0142, 0.01970, -1.9734 0.0081, 0.01410, -1.8681 0.0026, 0.00780, -1.8489 0.0000, 0.00000, -1.6783 0.0037, -0.00840, 0.6429 0.0112, -0.01420, 0.9863 0.0191, -0.01930, 0.9979 0.0397, -0.03030, 0.8887 0.0706, -0.04420, 0.6793 0.1037, -0.05710, 0.5191 0.1384, -0.06890, 0.3448 0.1741, -0.07950, 0.1966 0.2102, -0.08660, 0.0613 0.2472, -0.09640, -0.0873 0.2844, -0.10270, -0.2039 0.3225, -0.10690, -0.3182 0.3608, -0.10890, -0.4077 0.3991, -0.10830, -0.4738 0.4373, -0.10510, -0.4522 0.4757, -0.09890, -0.3997 0.5137, -0.09067, -0.2702 0.5611, -0.07859, -0.1054 16 Flap element taps 1.0000, 0.00130, -0.2792 0.9365, 0.01390, -0.3384 0.8333, 0.03280, -0.3249 0.7436, 0.04930, -0.3215 0.7049, 0.05667, -0.3288 0.6662, 0.06411, -0.3358 0.6274, 0.07172, -0.3698 0.6009, 0.07523, -0.4719 0.6069, 0.02889, -0.2012 0.6079, -0.01747, -0.2084 0.6167, -0.06381, -0.1630 0.6558, -0.05300, 0.1078 0.7045, -0.04117, 0.3616 0.7429, -0.03210, 0.2863 0.8333, -0.01400, 0.2224 0.9311, -0.00120, 0.1470 --------- Run Conditions: vel=102.8 ft/s Re=0.999x10^6 AOA=12.02 Flap deflection=5.00 Totals: Cl=0.9115 Cdp=0.0772 Cm(c/4)=-0.0558 Cs=0.1144 Ch=0.0251 Main component: Cl=0.7079 Cdp=0.0469 Cm=-0.1222 Flap component: Cl=0.2036 Cdp=0.0303 Cm=-0.1605 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1411 0.5905, -0.01667, -0.3006 0.5709, 0.03110, -0.2794 0.5889, 0.07933, -0.3048 0.5500, 0.08689, -0.3181 0.5110, 0.09367, -0.3658 0.4731, 0.09830, -0.4717 0.4349, 0.10070, -0.6268 0.3960, 0.10120, -0.7560 0.3566, 0.10020, -0.8704 0.3172, 0.09790, -0.9596 0.2778, 0.09440, -1.0618 0.2393, 0.08960, -1.1660 0.2056, 0.08360, -1.2667 0.1633, 0.07610, -1.3672 0.1261, 0.06710, -1.4746 0.0900, 0.05640, -1.7033 0.0571, 0.04390, -1.9107 0.0283, 0.02940, -2.3461 0.0142, 0.01970, -2.8300 0.0081, 0.01410, -2.8787 0.0026, 0.00780, -3.0269 0.0000, 0.00000, -3.5413 0.0037, -0.00840, 0.1042 0.0112, -0.01420, 0.8580 0.0191, -0.01930, 0.9888 0.0397, -0.03030, 0.9756 0.0706, -0.04420, 0.8116 0.1037, -0.05710, 0.6638 0.1384, -0.06890, 0.4985 0.1741, -0.07950, 0.3526 0.2102, -0.08660, 0.2167 0.2472, -0.09640, 0.0648 0.2844, -0.10270, -0.0576 0.3225, -0.10690, -0.1796 0.3608, -0.10890, -0.2792 0.3991, -0.10830, -0.3578 0.4373, -0.10510, -0.3500 0.4757, -0.09890, -0.3044 0.5137, -0.09067, -0.2370 0.5611, -0.07859, -0.1160 16 Flap element taps 1.0000, 0.00130, -0.3155 0.9365, 0.01390, -0.3628 0.8333, 0.03280, -0.3515 0.7436, 0.04930, -0.3457 0.7049, 0.05667, -0.3454 0.6662, 0.06411, -0.3429 0.6274, 0.07172, -0.3523 0.6009, 0.07523, -0.3842 0.6069, 0.02889, -0.2877 0.6079, -0.01747, -0.3000 0.6167, -0.06381, -0.2307 0.6558, -0.05300, 0.3723 0.7045, -0.04117, 0.3753 0.7429, -0.03210, 0.2907 0.8333, -0.01400, 0.2253 0.9311, -0.00120, 0.1363 --------- Run Conditions: vel=104.4 ft/s Re=1.012x10^6 AOA=15.02 Flap deflection=5.00 Totals: Cl=0.9838 Cdp=0.1173 Cm(c/4)=-0.0612 Cs=0.1417 Ch=0.0314 Main component: Cl=0.7576 Cdp=0.0737 Cm=-0.1273 Flap component: Cl=0.2263 Cdp=0.0436 Cm=-0.1790 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1631 0.5905, -0.01667, -0.4032 0.5709, 0.03110, -0.3740 0.5889, 0.07933, -0.4156 0.5500, 0.08689, -0.4091 0.5110, 0.09367, -0.4183 0.4731, 0.09830, -0.4353 0.4349, 0.10070, -0.4770 0.3960, 0.10120, -0.5643 0.3566, 0.10020, -0.6872 0.3172, 0.09790, -0.8107 0.2778, 0.09440, -0.9576 0.2393, 0.08960, -1.1021 0.2056, 0.08360, -1.2446 0.1633, 0.07610, -1.4010 0.1261, 0.06710, -1.5578 0.0900, 0.05640, -1.8542 0.0571, 0.04390, -2.1655 0.0283, 0.02940, -2.7679 0.0142, 0.01970, -3.4640 0.0081, 0.01410, -3.6583 0.0026, 0.00780, -3.9476 0.0000, 0.00000, -5.1237 0.0037, -0.00840, -0.4527 0.0112, -0.01420, 0.6678 0.0191, -0.01930, 0.9162 0.0397, -0.03030, 1.0019 0.0706, -0.04420, 0.8953 0.1037, -0.05710, 0.7619 0.1384, -0.06890, 0.6060 0.1741, -0.07950, 0.4673 0.2102, -0.08660, 0.3233 0.2472, -0.09640, 0.1682 0.2844, -0.10270, 0.0393 0.3225, -0.10690, -0.0792 0.3608, -0.10890, -0.1930 0.3991, -0.10830, -0.2804 0.4373, -0.10510, -0.2908 0.4757, -0.09890, -0.2607 0.5137, -0.09067, -0.1933 0.5611, -0.07859, -0.1447 16 Flap element taps 1.0000, 0.00130, -0.4005 0.9365, 0.01390, -0.4362 0.8333, 0.03280, -0.4265 0.7436, 0.04930, -0.4184 0.7049, 0.05667, -0.4072 0.6662, 0.06411, -0.4120 0.6274, 0.07172, -0.4091 0.6009, 0.07523, -0.4121 0.6069, 0.02889, -0.3818 0.6079, -0.01747, -0.3901 0.6167, -0.06381, -0.2955 0.6558, -0.05300, 0.4919 0.7045, -0.04117, 0.3779 0.7429, -0.03210, 0.2824 0.8333, -0.01400, 0.2115 0.9311, -0.00120, 0.1094 --------- Run Conditions: vel=102.7 ft/s Re=0.994x10^6 AOA=17.99 Flap deflection=5.00 Totals: Cl=0.8193 Cdp=0.2211 Cm(c/4)=-0.1052 Cs=0.0428 Ch=0.0403 Main component: Cl=0.5546 Cdp=0.1575 Cm=-0.1061 Flap component: Cl=0.2647 Cdp=0.0635 Cm=-0.2109 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.2616 0.5905, -0.01667, -0.5826 0.5709, 0.03110, -0.5410 0.5889, 0.07933, -0.6110 0.5500, 0.08689, -0.5844 0.5110, 0.09367, -0.5811 0.4731, 0.09830, -0.5807 0.4349, 0.10070, -0.5868 0.3960, 0.10120, -0.5959 0.3566, 0.10020, -0.6068 0.3172, 0.09790, -0.6227 0.2778, 0.09440, -0.6545 0.2393, 0.08960, -0.6726 0.2056, 0.08360, -0.6979 0.1633, 0.07610, -0.7642 0.1261, 0.06710, -0.8599 0.0900, 0.05640, -1.0516 0.0571, 0.04390, -1.3825 0.0283, 0.02940, -1.9906 0.0142, 0.01970, -2.6617 0.0081, 0.01410, -2.8825 0.0026, 0.00780, -3.2041 0.0000, 0.00000, -4.2529 0.0037, -0.00840, -0.2461 0.0112, -0.01420, 0.7210 0.0191, -0.01930, 0.9321 0.0397, -0.03030, 1.0010 0.0706, -0.04420, 0.8930 0.1037, -0.05710, 0.7633 0.1384, -0.06890, 0.6067 0.1741, -0.07950, 0.4674 0.2102, -0.08660, 0.3207 0.2472, -0.09640, 0.1621 0.2844, -0.10270, 0.0286 0.3225, -0.10690, -0.0976 0.3608, -0.10890, -0.2194 0.3991, -0.10830, -0.3162 0.4373, -0.10510, -0.3348 0.4757, -0.09890, -0.3128 0.5137, -0.09067, -0.2401 0.5611, -0.07859, -0.1861 16 Flap element taps 1.0000, 0.00130, -0.5219 0.9365, 0.01390, -0.5804 0.8333, 0.03280, -0.6000 0.7436, 0.04930, -0.5906 0.7049, 0.05667, -0.5727 0.6662, 0.06411, -0.5766 0.6274, 0.07172, -0.5713 0.6009, 0.07523, -0.5711 0.6069, 0.02889, -0.5529 0.6079, -0.01747, -0.5637 0.6167, -0.06381, -0.4368 0.6558, -0.05300, 0.5476 0.7045, -0.04117, 0.3401 0.7429, -0.03210, 0.2355 0.8333, -0.01400, 0.1563 0.9311, -0.00120, 0.0383 --------- Run Conditions: vel=103.5 ft/s Re=1.001x10^6 AOA=19.98 Flap deflection=5.00 Totals: Cl=0.7860 Cdp=0.2897 Cm(c/4)=-0.1255 Cs=-0.0036 Ch=0.0456 Main component: Cl=0.5099 Cdp=0.2155 Cm=-0.1141 Flap component: Cl=0.2761 Cdp=0.0742 Cm=-0.2208 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.2964 0.5905, -0.01667, -0.6610 0.5709, 0.03110, -0.6138 0.5889, 0.07933, -0.6902 0.5500, 0.08689, -0.6636 0.5110, 0.09367, -0.6584 0.4731, 0.09830, -0.6574 0.4349, 0.10070, -0.6642 0.3960, 0.10120, -0.6733 0.3566, 0.10020, -0.6785 0.3172, 0.09790, -0.6772 0.2778, 0.09440, -0.6889 0.2393, 0.08960, -0.7071 0.2056, 0.08360, -0.7178 0.1633, 0.07610, -0.7400 0.1261, 0.06710, -0.7468 0.0900, 0.05640, -0.7907 0.0571, 0.04390, -0.9341 0.0283, 0.02940, -1.3706 0.0142, 0.01970, -1.9529 0.0081, 0.01410, -2.2258 0.0026, 0.00780, -2.5950 0.0000, 0.00000, -3.6098 0.0037, -0.00840, -0.1219 0.0112, -0.01420, 0.7458 0.0191, -0.01930, 0.9364 0.0397, -0.03030, 0.9992 0.0706, -0.04420, 0.8955 0.1037, -0.05710, 0.7720 0.1384, -0.06890, 0.6196 0.1741, -0.07950, 0.4833 0.2102, -0.08660, 0.3384 0.2472, -0.09640, 0.1804 0.2844, -0.10270, 0.0460 0.3225, -0.10690, -0.0812 0.3608, -0.10890, -0.2063 0.3991, -0.10830, -0.3077 0.4373, -0.10510, -0.3309 0.4757, -0.09890, -0.3131 0.5137, -0.09067, -0.2431 0.5611, -0.07859, -0.1816 16 Flap element taps 1.0000, 0.00130, -0.5770 0.9365, 0.01390, -0.6203 0.8333, 0.03280, -0.6450 0.7436, 0.04930, -0.6457 0.7049, 0.05667, -0.6316 0.6662, 0.06411, -0.6375 0.6274, 0.07172, -0.6373 0.6009, 0.07523, -0.6354 0.6069, 0.02889, -0.6203 0.6079, -0.01747, -0.6342 0.6167, -0.06381, -0.4845 0.6558, -0.05300, 0.5832 0.7045, -0.04117, 0.3281 0.7429, -0.03210, 0.2211 0.8333, -0.01400, 0.1377 0.9311, -0.00120, 0.0132 --------- Run Conditions: vel=103.8 ft/s Re=1.003x10^6 AOA=23.97 Flap deflection=5.00 Totals: Cl=0.8824 Cdp=0.4269 Cm(c/4)=-0.1583 Cs=-0.0316 Ch=0.0551 Main component: Cl=0.5756 Cdp=0.3163 Cm=-0.1516 Flap component: Cl=0.3068 Cdp=0.1105 Cm=-0.2517 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.2755 0.5905, -0.01667, -0.7294 0.5709, 0.03110, -0.6781 0.5889, 0.07933, -0.7729 0.5500, 0.08689, -0.7647 0.5110, 0.09367, -0.7833 0.4731, 0.09830, -0.7782 0.4349, 0.10070, -0.7911 0.3960, 0.10120, -0.8023 0.3566, 0.10020, -0.8131 0.3172, 0.09790, -0.8311 0.2778, 0.09440, -0.8604 0.2393, 0.08960, -0.8831 0.2056, 0.08360, -0.9126 0.1633, 0.07610, -0.9443 0.1261, 0.06710, -0.9553 0.0900, 0.05640, -0.9807 0.0571, 0.04390, -1.0146 0.0283, 0.02940, -1.0677 0.0142, 0.01970, -1.1557 0.0081, 0.01410, -1.3799 0.0026, 0.00780, -1.7164 0.0000, 0.00000, -3.0688 0.0037, -0.00840, -0.1781 0.0112, -0.01420, 0.6762 0.0191, -0.01930, 0.8941 0.0397, -0.03030, 0.9994 0.0706, -0.04420, 0.9348 0.1037, -0.05710, 0.8351 0.1384, -0.06890, 0.7012 0.1741, -0.07950, 0.5754 0.2102, -0.08660, 0.4388 0.2472, -0.09640, 0.2869 0.2844, -0.10270, 0.1526 0.3225, -0.10690, 0.0249 0.3608, -0.10890, -0.1049 0.3991, -0.10830, -0.2149 0.4373, -0.10510, -0.2517 0.4757, -0.09890, -0.2505 0.5137, -0.09067, -0.1877 0.5611, -0.07859, -0.1200 16 Flap element taps 1.0000, 0.00130, -0.6976 0.9365, 0.01390, -0.7309 0.8333, 0.03280, -0.7581 0.7436, 0.04930, -0.7618 0.7049, 0.05667, -0.7532 0.6662, 0.06411, -0.7639 0.6274, 0.07172, -0.7717 0.6009, 0.07523, -0.7865 0.6069, 0.02889, -0.6964 0.6079, -0.01747, -0.7085 0.6167, -0.06381, -0.5219 0.6558, -0.05300, 0.6374 0.7045, -0.04117, 0.3311 0.7429, -0.03210, 0.2240 0.8333, -0.01400, 0.1285 0.9311, -0.00120, -0.0198 --------- Run Conditions: vel=104.9 ft/s Re=1.012x10^6 AOA=27.00 Flap deflection=5.00 Totals: Cl=0.7947 Cdp=0.4683 Cm(c/4)=-0.1558 Cs=-0.0565 Ch=0.0538 Main component: Cl=0.5044 Cdp=0.3504 Cm=-0.1445 Flap component: Cl=0.2903 Cdp=0.1179 Cm=-0.2415 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.2518 0.5905, -0.01667, -0.7354 0.5709, 0.03110, -0.6832 0.5889, 0.07933, -0.7702 0.5500, 0.08689, -0.7473 0.5110, 0.09367, -0.7364 0.4731, 0.09830, -0.7335 0.4349, 0.10070, -0.7311 0.3960, 0.10120, -0.7327 0.3566, 0.10020, -0.7336 0.3172, 0.09790, -0.7301 0.2778, 0.09440, -0.7371 0.2393, 0.08960, -0.7391 0.2056, 0.08360, -0.7440 0.1633, 0.07610, -0.7784 0.1261, 0.06710, -0.8100 0.0900, 0.05640, -0.8358 0.0571, 0.04390, -0.8196 0.0283, 0.02940, -0.8339 0.0142, 0.01970, -0.8569 0.0081, 0.01410, -0.9559 0.0026, 0.00780, -1.1495 0.0000, 0.00000, -2.4458 0.0037, -0.00840, -0.0886 0.0112, -0.01420, 0.6857 0.0191, -0.01930, 0.8938 0.0397, -0.03030, 1.0049 0.0706, -0.04420, 0.9532 0.1037, -0.05710, 0.8642 0.1384, -0.06890, 0.7375 0.1741, -0.07950, 0.6174 0.2102, -0.08660, 0.4869 0.2472, -0.09640, 0.3383 0.2844, -0.10270, 0.2050 0.3225, -0.10690, 0.0755 0.3608, -0.10890, -0.0549 0.3991, -0.10830, -0.1693 0.4373, -0.10510, -0.2113 0.4757, -0.09890, -0.2175 0.5137, -0.09067, -0.1567 0.5611, -0.07859, -0.0938 16 Flap element taps 1.0000, 0.00130, -0.6770 0.9365, 0.01390, -0.6945 0.8333, 0.03280, -0.7131 0.7436, 0.04930, -0.7219 0.7049, 0.05667, -0.7129 0.6662, 0.06411, -0.7188 0.6274, 0.07172, -0.7185 0.6009, 0.07523, -0.7150 0.6069, 0.02889, -0.6938 0.6079, -0.01747, -0.7107 0.6167, -0.06381, -0.5240 0.6558, -0.05300, 0.6652 0.7045, -0.04117, 0.3384 0.7429, -0.03210, 0.2286 0.8333, -0.01400, 0.1323 0.9311, -0.00120, -0.0162