S809 SPOILER FLAP, LEGR, CHORD = 18 INCHES --------- Run Conditions: vel=102.5 ft/s Re=0.998x10^6 AOA=-5.99 Flap deflection=30.00 Totals: Cl=-0.7580 Cdp=0.2110 Cm(c/4)=0.0037 Cs=-0.1308 Ch=-0.0079 Main component: Cl=-0.7586 Cdp=0.0476 Cm=0.1842 Flap component: Cl=0.0007 Cdp=0.1634 Cm=0.0135 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3240 0.5905, -0.01667, -0.5337 0.5709, 0.03110, -0.2976 0.5889, 0.07933, -0.2420 0.5500, 0.08689, 0.5284 0.5110, 0.09367, 0.4136 0.4731, 0.09830, 0.3132 0.4349, 0.10070, 0.2278 0.3960, 0.10120, 0.1585 0.3566, 0.10020, 0.1780 0.3172, 0.09790, 0.1848 0.2778, 0.09440, 0.1879 0.2393, 0.08960, 0.2197 0.2056, 0.08360, 0.2373 0.1633, 0.07610, 0.3483 0.1261, 0.06710, 0.4328 0.0900, 0.05640, 0.5703 0.0571, 0.04390, 0.7527 0.0283, 0.02940, 0.9491 0.0142, 0.01970, 0.9881 0.0081, 0.01410, 0.8690 0.0026, 0.00780, 0.2827 0.0000, 0.00000, -1.8185 0.0037, -0.00840, -2.5900 0.0112, -0.01420, -1.9883 0.0191, -0.01930, -1.5860 0.0397, -0.03030, -1.1760 0.0706, -0.04420, -1.1346 0.1037, -0.05710, -1.0654 0.1384, -0.06890, -1.0831 0.1741, -0.07950, -1.1042 0.2102, -0.08660, -1.1655 0.2472, -0.09640, -1.1915 0.2844, -0.10270, -1.1922 0.3225, -0.10690, -1.1175 0.3608, -0.10890, -1.0696 0.3991, -0.10830, -0.8835 0.4373, -0.10510, -0.6394 0.4757, -0.09890, -0.4282 0.5137, -0.09067, -0.3656 0.5611, -0.07859, -0.3567 16 Flap element taps 1.0000, 0.00130, -0.8565 0.9365, 0.01390, -0.7926 0.8333, 0.03280, -0.7749 0.7436, 0.04930, -0.7591 0.7049, 0.05667, -0.7223 0.6662, 0.06411, -0.7350 0.6274, 0.07172, -0.7249 0.6009, 0.07523, -0.7275 0.6069, 0.02889, 0.8838 0.6079, -0.01747, 0.8748 0.6167, -0.06381, -0.6341 0.6558, -0.05300, -0.6617 0.7045, -0.04117, -0.6818 0.7429, -0.03210, -0.6906 0.8333, -0.01400, -0.7114 0.9311, -0.00120, -0.3566 --------- Run Conditions: vel=102.8 ft/s Re=1.001x10^6 AOA=0.04 Flap deflection=30.00 Totals: Cl=-0.1655 Cdp=0.2370 Cm(c/4)=-0.0486 Cs=-0.2371 Ch=0.0029 Main component: Cl=-0.2815 Cdp=0.0066 Cm=0.0829 Flap component: Cl=0.1160 Cdp=0.2304 Cm=-0.0902 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0047 0.5905, -0.01667, -0.2730 0.5709, 0.03110, -0.0070 0.5889, 0.07933, 0.0560 0.5500, 0.08689, 0.3737 0.5110, 0.09367, 0.2961 0.4731, 0.09830, 0.1791 0.4349, 0.10070, 0.0536 0.3960, 0.10120, -0.0653 0.3566, 0.10020, -0.0651 0.3172, 0.09790, -0.0897 0.2778, 0.09440, -0.1215 0.2393, 0.08960, -0.1312 0.2056, 0.08360, -0.1626 0.1633, 0.07610, -0.0794 0.1261, 0.06710, -0.0401 0.0900, 0.05640, 0.0399 0.0571, 0.04390, 0.2015 0.0283, 0.02940, 0.4254 0.0142, 0.01970, 0.6512 0.0081, 0.01410, 0.7712 0.0026, 0.00780, 0.9346 0.0000, 0.00000, 0.8445 0.0037, -0.00840, 0.1480 0.0112, -0.01420, -0.0233 0.0191, -0.01930, -0.0467 0.0397, -0.03030, -0.0544 0.0706, -0.04420, -0.2483 0.1037, -0.05710, -0.3212 0.1384, -0.06890, -0.4094 0.1741, -0.07950, -0.5046 0.2102, -0.08660, -0.6306 0.2472, -0.09640, -0.6998 0.2844, -0.10270, -0.7634 0.3225, -0.10690, -0.7408 0.3608, -0.10890, -0.7705 0.3991, -0.10830, -0.6707 0.4373, -0.10510, -0.5193 0.4757, -0.09890, -0.2850 0.5137, -0.09067, -0.0763 0.5611, -0.07859, -0.0234 16 Flap element taps 1.0000, 0.00130, -0.9510 0.9365, 0.01390, -0.9156 0.8333, 0.03280, -0.9154 0.7436, 0.04930, -0.8953 0.7049, 0.05667, -0.8706 0.6662, 0.06411, -0.8858 0.6274, 0.07172, -0.8681 0.6009, 0.07523, -0.8638 0.6069, 0.02889, 0.8724 0.6079, -0.01747, 0.8222 0.6167, -0.06381, -0.3779 0.6558, -0.05300, -0.4115 0.7045, -0.04117, -0.4175 0.7429, -0.03210, -0.4432 0.8333, -0.01400, -0.3974 0.9311, -0.00120, -0.0573 --------- Run Conditions: vel=102.4 ft/s Re=0.998x10^6 AOA=2.99 Flap deflection=30.00 Totals: Cl=0.0962 Cdp=0.2411 Cm(c/4)=-0.0636 Cs=-0.2357 Ch=0.0107 Main component: Cl=-0.0537 Cdp=-0.0131 Cm=0.0354 Flap component: Cl=0.1499 Cdp=0.2541 Cm=-0.1262 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.1435 0.5905, -0.01667, -0.1625 0.5709, 0.03110, 0.1390 0.5889, 0.07933, 0.1771 0.5500, 0.08689, 0.2851 0.5110, 0.09367, 0.2370 0.4731, 0.09830, 0.1270 0.4349, 0.10070, -0.0150 0.3960, 0.10120, -0.1558 0.3566, 0.10020, -0.1817 0.3172, 0.09790, -0.2276 0.2778, 0.09440, -0.2797 0.2393, 0.08960, -0.3144 0.2056, 0.08360, -0.3673 0.1633, 0.07610, -0.3156 0.1261, 0.06710, -0.3076 0.0900, 0.05640, -0.2820 0.0571, 0.04390, -0.1731 0.0283, 0.02940, -0.0215 0.0142, 0.01970, 0.1562 0.0081, 0.01410, 0.3292 0.0026, 0.00780, 0.5250 0.0000, 0.00000, 0.9770 0.0037, -0.00840, 0.7908 0.0112, -0.01420, 0.5647 0.0191, -0.01930, 0.4588 0.0397, -0.03030, 0.3270 0.0706, -0.04420, 0.0953 0.1037, -0.05710, -0.0180 0.1384, -0.06890, -0.1301 0.1741, -0.07950, -0.2505 0.2102, -0.08660, -0.3879 0.2472, -0.09640, -0.4729 0.2844, -0.10270, -0.5553 0.3225, -0.10690, -0.5599 0.3608, -0.10890, -0.6107 0.3991, -0.10830, -0.5426 0.4373, -0.10510, -0.4330 0.4757, -0.09890, -0.2350 0.5137, -0.09067, 0.0089 0.5611, -0.07859, 0.1071 16 Flap element taps 1.0000, 0.00130, -0.9241 0.9365, 0.01390, -0.9095 0.8333, 0.03280, -0.9194 0.7436, 0.04930, -0.9094 0.7049, 0.05667, -0.8912 0.6662, 0.06411, -0.9037 0.6274, 0.07172, -0.8895 0.6009, 0.07523, -0.8852 0.6069, 0.02889, 0.8845 0.6079, -0.01747, 0.7165 0.6167, -0.06381, -0.2493 0.6558, -0.05300, -0.2851 0.7045, -0.04117, -0.2876 0.7429, -0.03210, -0.3146 0.8333, -0.01400, -0.2433 0.9311, -0.00120, 0.0438 --------- Run Conditions: vel=102.5 ft/s Re=0.997x10^6 AOA=6.03 Flap deflection=30.00 Totals: Cl=0.4331 Cdp=0.2544 Cm(c/4)=-0.1355 Cs=-0.2075 Ch=0.0278 Main component: Cl=0.1242 Cdp=-0.0349 Cm=0.0132 Flap component: Cl=0.3089 Cdp=0.2893 Cm=-0.2631 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.2008 0.5905, -0.01667, 0.1993 0.5709, 0.03110, 0.2060 0.5889, 0.07933, 0.1548 0.5500, 0.08689, 0.1659 0.5110, 0.09367, 0.1571 0.4731, 0.09830, 0.1500 0.4349, 0.10070, 0.0565 0.3960, 0.10120, -0.1270 0.3566, 0.10020, -0.2280 0.3172, 0.09790, -0.3215 0.2778, 0.09440, -0.4144 0.2393, 0.08960, -0.4880 0.2056, 0.08360, -0.5744 0.1633, 0.07610, -0.5765 0.1261, 0.06710, -0.6124 0.0900, 0.05640, -0.6644 0.0571, 0.04390, -0.6417 0.0283, 0.02940, -0.6298 0.0142, 0.01970, -0.5989 0.0081, 0.01410, -0.3871 0.0026, 0.00780, -0.2270 0.0000, 0.00000, 0.3683 0.0037, -0.00840, 0.9889 0.0112, -0.01420, 0.9167 0.0191, -0.01930, 0.8144 0.0397, -0.03030, 0.6443 0.0706, -0.04420, 0.3995 0.1037, -0.05710, 0.2577 0.1384, -0.06890, 0.1197 0.1741, -0.07950, -0.0186 0.2102, -0.08660, -0.1687 0.2472, -0.09640, -0.2797 0.2844, -0.10270, -0.3823 0.3225, -0.10690, -0.4198 0.3608, -0.10890, -0.5012 0.3991, -0.10830, -0.4867 0.4373, -0.10510, -0.4408 0.4757, -0.09890, -0.3258 0.5137, -0.09067, -0.1191 0.5611, -0.07859, 0.0617 16 Flap element taps 1.0000, 0.00130, -0.8910 0.9365, 0.01390, -0.9001 0.8333, 0.03280, -0.9159 0.7436, 0.04930, -0.9000 0.7049, 0.05667, -0.8773 0.6662, 0.06411, -0.8874 0.6274, 0.07172, -0.8770 0.6009, 0.07523, -0.9052 0.6069, 0.02889, 0.1751 0.6079, -0.01747, 0.1821 0.6167, -0.06381, 0.2072 0.6558, -0.05300, 0.1921 0.7045, -0.04117, 0.1929 0.7429, -0.03210, 0.1784 0.8333, -0.01400, 0.3458 0.9311, -0.00120, 0.3316 --------- Run Conditions: vel=102.2 ft/s Re=0.995x10^6 AOA=9.02 Flap deflection=30.00 Totals: Cl=0.6659 Cdp=0.2887 Cm(c/4)=-0.1548 Cs=-0.1808 Ch=0.0225 Main component: Cl=0.3264 Cdp=-0.0331 Cm=-0.0281 Flap component: Cl=0.3395 Cdp=0.3218 Cm=-0.3024 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.2088 0.5905, -0.01667, 0.2202 0.5709, 0.03110, 0.2525 0.5889, 0.07933, 0.0187 0.5500, 0.08689, 0.0304 0.5110, 0.09367, 0.0265 0.4731, 0.09830, 0.0273 0.4349, 0.10070, -0.0100 0.3960, 0.10120, -0.1390 0.3566, 0.10020, -0.2681 0.3172, 0.09790, -0.3957 0.2778, 0.09440, -0.5223 0.2393, 0.08960, -0.6298 0.2056, 0.08360, -0.7445 0.1633, 0.07610, -0.8008 0.1261, 0.06710, -0.8827 0.0900, 0.05640, -1.0148 0.0571, 0.04390, -1.0927 0.0283, 0.02940, -1.2595 0.0142, 0.01970, -1.4398 0.0081, 0.01410, -1.2991 0.0026, 0.00780, -1.2579 0.0000, 0.00000, -0.8980 0.0037, -0.00840, 0.8089 0.0112, -0.01420, 0.9979 0.0191, -0.01930, 0.9734 0.0397, -0.03030, 0.8425 0.0706, -0.04420, 0.6227 0.1037, -0.05710, 0.4757 0.1384, -0.06890, 0.3260 0.1741, -0.07950, 0.1866 0.2102, -0.08660, 0.0337 0.2472, -0.09640, -0.0859 0.2844, -0.10270, -0.2009 0.3225, -0.10690, -0.2671 0.3608, -0.10890, -0.3590 0.3991, -0.10830, -0.3719 0.4373, -0.10510, -0.3434 0.4757, -0.09890, -0.2606 0.5137, -0.09067, -0.0778 0.5611, -0.07859, 0.0843 16 Flap element taps 1.0000, 0.00130, -0.9029 0.9365, 0.01390, -0.9177 0.8333, 0.03280, -0.9326 0.7436, 0.04930, -0.9249 0.7049, 0.05667, -0.9054 0.6662, 0.06411, -0.9086 0.6274, 0.07172, -0.9002 0.6009, 0.07523, -0.9395 0.6069, 0.02889, 0.0691 0.6079, -0.01747, 0.0903 0.6167, -0.06381, 0.1758 0.6558, -0.05300, 0.1794 0.7045, -0.04117, 0.1982 0.7429, -0.03210, 0.2618 0.8333, -0.01400, 0.7406 0.9311, -0.00120, 0.3097 --------- Run Conditions: vel=102.4 ft/s Re=0.999x10^6 AOA=12.03 Flap deflection=30.00 Totals: Cl=0.8595 Cdp=0.2991 Cm(c/4)=-0.1563 Cs=-0.1133 Ch=0.0219 Main component: Cl=0.5264 Cdp=-0.0216 Cm=-0.0739 Flap component: Cl=0.3331 Cdp=0.3207 Cm=-0.3082 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.1894 0.5905, -0.01667, 0.1966 0.5709, 0.03110, 0.3358 0.5889, 0.07933, -0.1703 0.5500, 0.08689, -0.1553 0.5110, 0.09367, -0.1622 0.4731, 0.09830, -0.1571 0.4349, 0.10070, -0.1703 0.3960, 0.10120, -0.2201 0.3566, 0.10020, -0.3009 0.3172, 0.09790, -0.4284 0.2778, 0.09440, -0.5868 0.2393, 0.08960, -0.7300 0.2056, 0.08360, -0.8834 0.1633, 0.07610, -0.9969 0.1261, 0.06710, -1.1319 0.0900, 0.05640, -1.3439 0.0571, 0.04390, -1.5457 0.0283, 0.02940, -1.9178 0.0142, 0.01970, -2.3402 0.0081, 0.01410, -2.3781 0.0026, 0.00780, -2.4594 0.0000, 0.00000, -2.7383 0.0037, -0.00840, 0.2983 0.0112, -0.01420, 0.9008 0.0191, -0.01930, 0.9876 0.0397, -0.03030, 0.9545 0.0706, -0.04420, 0.7853 0.1037, -0.05710, 0.6484 0.1384, -0.06890, 0.4989 0.1741, -0.07950, 0.3601 0.2102, -0.08660, 0.2169 0.2472, -0.09640, 0.0934 0.2844, -0.10270, -0.0274 0.3225, -0.10690, -0.1091 0.3608, -0.10890, -0.2074 0.3991, -0.10830, -0.2406 0.4373, -0.10510, -0.2220 0.4757, -0.09890, -0.1593 0.5137, -0.09067, -0.1185 0.5611, -0.07859, 0.1763 16 Flap element taps 1.0000, 0.00130, -0.8425 0.9365, 0.01390, -0.8596 0.8333, 0.03280, -0.8712 0.7436, 0.04930, -0.8668 0.7049, 0.05667, -0.8544 0.6662, 0.06411, -0.8571 0.6274, 0.07172, -0.8527 0.6009, 0.07523, -0.9011 0.6069, 0.02889, -0.0794 0.6079, -0.01747, -0.0368 0.6167, -0.06381, 0.1110 0.6558, -0.05300, 0.1283 0.7045, -0.04117, 0.2209 0.7429, -0.03210, 0.5795 0.8333, -0.01400, 0.7242 0.9311, -0.00120, 0.3215 --------- Run Conditions: vel=102.7 ft/s Re=1.002x10^6 AOA=15.03 Flap deflection=30.00 Totals: Cl=1.0391 Cdp=0.3126 Cm(c/4)=-0.1664 Cs=-0.0324 Ch=0.0208 Main component: Cl=0.7106 Cdp=0.0143 Cm=-0.1272 Flap component: Cl=0.3285 Cdp=0.2983 Cm=-0.3103 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.1456 0.5905, -0.01667, 0.1278 0.5709, 0.03110, 0.4496 0.5889, 0.07933, -0.4764 0.5500, 0.08689, -0.4399 0.5110, 0.09367, -0.4731 0.4731, 0.09830, -0.4606 0.4349, 0.10070, -0.4676 0.3960, 0.10120, -0.4758 0.3566, 0.10020, -0.5031 0.3172, 0.09790, -0.5246 0.2778, 0.09440, -0.5893 0.2393, 0.08960, -0.6844 0.2056, 0.08360, -0.8446 0.1633, 0.07610, -1.0420 0.1261, 0.06710, -1.2344 0.0900, 0.05640, -1.5476 0.0571, 0.04390, -1.8872 0.0283, 0.02940, -2.4869 0.0142, 0.01970, -3.1824 0.0081, 0.01410, -3.3791 0.0026, 0.00780, -3.7104 0.0000, 0.00000, -4.8816 0.0037, -0.00840, -0.4207 0.0112, -0.01420, 0.6615 0.0191, -0.01930, 0.9089 0.0397, -0.03030, 0.9979 0.0706, -0.04420, 0.8997 0.1037, -0.05710, 0.7853 0.1384, -0.06890, 0.6351 0.1741, -0.07950, 0.5086 0.2102, -0.08660, 0.3832 0.2472, -0.09640, 0.2454 0.2844, -0.10270, 0.1346 0.3225, -0.10690, 0.0349 0.3608, -0.10890, -0.0587 0.3991, -0.10830, -0.1192 0.4373, -0.10510, -0.1127 0.4757, -0.09890, -0.0680 0.5137, -0.09067, -0.0123 0.5611, -0.07859, 0.1590 16 Flap element taps 1.0000, 0.00130, -0.6980 0.9365, 0.01390, -0.7252 0.8333, 0.03280, -0.7350 0.7436, 0.04930, -0.7319 0.7049, 0.05667, -0.7246 0.6662, 0.06411, -0.7280 0.6274, 0.07172, -0.7307 0.6009, 0.07523, -0.7623 0.6069, 0.02889, -0.3492 0.6079, -0.01747, -0.2063 0.6167, -0.06381, -0.0290 0.6558, -0.05300, 0.1009 0.7045, -0.04117, 0.3874 0.7429, -0.03210, 0.9875 0.8333, -0.01400, 0.7095 0.9311, -0.00120, 0.3610 --------- Run Conditions: vel=102.2 ft/s Re=1.000x10^6 AOA=17.98 Flap deflection=30.00 Totals: Cl=1.0696 Cdp=0.4120 Cm(c/4)=-0.2020 Cs=-0.0617 Ch=0.0159 Main component: Cl=0.7444 Cdp=0.1389 Cm=-0.1774 Flap component: Cl=0.3252 Cdp=0.2732 Cm=-0.3108 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0990 0.5905, -0.01667, 0.0662 0.5709, 0.03110, 0.4225 0.5889, 0.07933, -0.7837 0.5500, 0.08689, -0.7450 0.5110, 0.09367, -0.8040 0.4731, 0.09830, -0.8622 0.4349, 0.10070, -0.8882 0.3960, 0.10120, -0.8847 0.3566, 0.10020, -0.8922 0.3172, 0.09790, -0.8848 0.2778, 0.09440, -0.9027 0.2393, 0.08960, -0.9158 0.2056, 0.08360, -0.9393 0.1633, 0.07610, -0.9828 0.1261, 0.06710, -0.9865 0.0900, 0.05640, -1.0328 0.0571, 0.04390, -1.1463 0.0283, 0.02940, -1.5684 0.0142, 0.01970, -2.1647 0.0081, 0.01410, -2.4761 0.0026, 0.00780, -2.9264 0.0000, 0.00000, -4.2320 0.0037, -0.00840, -0.3618 0.0112, -0.01420, 0.6513 0.0191, -0.01930, 0.8972 0.0397, -0.03030, 1.0021 0.0706, -0.04420, 0.9245 0.1037, -0.05710, 0.8238 0.1384, -0.06890, 0.6796 0.1741, -0.07950, 0.5589 0.2102, -0.08660, 0.4448 0.2472, -0.09640, 0.3077 0.2844, -0.10270, 0.2005 0.3225, -0.10690, 0.0958 0.3608, -0.10890, 0.0016 0.3991, -0.10830, -0.0662 0.4373, -0.10510, -0.0662 0.4757, -0.09890, -0.0330 0.5137, -0.09067, 0.0265 0.5611, -0.07859, 0.1022 16 Flap element taps 1.0000, 0.00130, -0.6133 0.9365, 0.01390, -0.6430 0.8333, 0.03280, -0.6568 0.7436, 0.04930, -0.6581 0.7049, 0.05667, -0.6471 0.6662, 0.06411, -0.6519 0.6274, 0.07172, -0.6518 0.6009, 0.07523, -0.6696 0.6069, 0.02889, -0.7552 0.6079, -0.01747, -0.3890 0.6167, -0.06381, -0.2195 0.6558, -0.05300, 0.0724 0.7045, -0.04117, 0.6322 0.7429, -0.03210, 1.0078 0.8333, -0.01400, 0.7101 0.9311, -0.00120, 0.3838 --------- Run Conditions: vel=102.8 ft/s Re=1.007x10^6 AOA=19.99 Flap deflection=30.00 Totals: Cl=1.0741 Cdp=0.4951 Cm(c/4)=-0.2178 Cs=-0.0980 Ch=0.0185 Main component: Cl=0.7471 Cdp=0.2052 Cm=-0.1919 Flap component: Cl=0.3270 Cdp=0.2899 Cm=-0.3205 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0870 0.5905, -0.01667, 0.0545 0.5709, 0.03110, 0.4323 0.5889, 0.07933, -0.8430 0.5500, 0.08689, -0.8108 0.5110, 0.09367, -0.8412 0.4731, 0.09830, -0.8928 0.4349, 0.10070, -0.9333 0.3960, 0.10120, -0.9595 0.3566, 0.10020, -0.9930 0.3172, 0.09790, -0.9881 0.2778, 0.09440, -1.0064 0.2393, 0.08960, -1.0095 0.2056, 0.08360, -1.0223 0.1633, 0.07610, -1.0508 0.1261, 0.06710, -1.0326 0.0900, 0.05640, -1.0558 0.0571, 0.04390, -1.0612 0.0283, 0.02940, -1.1236 0.0142, 0.01970, -1.3202 0.0081, 0.01410, -1.5921 0.0026, 0.00780, -1.9824 0.0000, 0.00000, -3.2928 0.0037, -0.00840, -0.2026 0.0112, -0.01420, 0.6788 0.0191, -0.01930, 0.9010 0.0397, -0.03030, 1.0018 0.0706, -0.04420, 0.9379 0.1037, -0.05710, 0.8469 0.1384, -0.06890, 0.7075 0.1741, -0.07950, 0.5940 0.2102, -0.08660, 0.4832 0.2472, -0.09640, 0.3492 0.2844, -0.10270, 0.2429 0.3225, -0.10690, 0.1357 0.3608, -0.10890, 0.0400 0.3991, -0.10830, -0.0315 0.4373, -0.10510, -0.0365 0.4757, -0.09890, -0.0105 0.5137, -0.09067, 0.0502 0.5611, -0.07859, 0.0967 16 Flap element taps 1.0000, 0.00130, -0.6476 0.9365, 0.01390, -0.6650 0.8333, 0.03280, -0.6812 0.7436, 0.04930, -0.6896 0.7049, 0.05667, -0.6841 0.6662, 0.06411, -0.6879 0.6274, 0.07172, -0.6892 0.6009, 0.07523, -0.7044 0.6069, 0.02889, -0.8314 0.6079, -0.01747, -0.4251 0.6167, -0.06381, -0.2697 0.6558, -0.05300, 0.0671 0.7045, -0.04117, 0.6967 0.7429, -0.03210, 1.0092 0.8333, -0.01400, 0.7116 0.9311, -0.00120, 0.3831 --------- Run Conditions: vel=102.2 ft/s Re=1.001x10^6 AOA=24.01 Flap deflection=30.00 Totals: Cl=1.0266 Cdp=0.6173 Cm(c/4)=-0.2405 Cs=-0.1462 Ch=0.0225 Main component: Cl=0.7020 Cdp=0.2891 Cm=-0.1990 Flap component: Cl=0.3245 Cdp=0.3282 Cm=-0.3387 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0671 0.5905, -0.01667, 0.0162 0.5709, 0.03110, 0.4131 0.5889, 0.07933, -0.9872 0.5500, 0.08689, -0.9906 0.5110, 0.09367, -1.0030 0.4731, 0.09830, -0.9487 0.4349, 0.10070, -0.9060 0.3960, 0.10120, -0.8783 0.3566, 0.10020, -0.9051 0.3172, 0.09790, -0.9173 0.2778, 0.09440, -0.9326 0.2393, 0.08960, -0.9193 0.2056, 0.08360, -0.9118 0.1633, 0.07610, -0.9270 0.1261, 0.06710, -0.9005 0.0900, 0.05640, -0.9047 0.0571, 0.04390, -0.8946 0.0283, 0.02940, -0.9092 0.0142, 0.01970, -0.9137 0.0081, 0.01410, -0.9761 0.0026, 0.00780, -1.2284 0.0000, 0.00000, -2.5696 0.0037, -0.00840, -0.1379 0.0112, -0.01420, 0.6610 0.0191, -0.01930, 0.8808 0.0397, -0.03030, 1.0000 0.0706, -0.04420, 0.9572 0.1037, -0.05710, 0.8832 0.1384, -0.06890, 0.7564 0.1741, -0.07950, 0.6491 0.2102, -0.08660, 0.5482 0.2472, -0.09640, 0.4164 0.2844, -0.10270, 0.3114 0.3225, -0.10690, 0.2012 0.3608, -0.10890, 0.1020 0.3991, -0.10830, 0.0235 0.4373, -0.10510, 0.0071 0.4757, -0.09890, 0.0203 0.5137, -0.09067, 0.0817 0.5611, -0.07859, 0.1209 16 Flap element taps 1.0000, 0.00130, -0.7082 0.9365, 0.01390, -0.7297 0.8333, 0.03280, -0.7453 0.7436, 0.04930, -0.7613 0.7049, 0.05667, -0.7598 0.6662, 0.06411, -0.7644 0.6274, 0.07172, -0.7633 0.6009, 0.07523, -0.7701 0.6069, 0.02889, -0.9295 0.6079, -0.01747, -0.4863 0.6167, -0.06381, -0.3460 0.6558, -0.05300, 0.0584 0.7045, -0.04117, 0.7768 0.7429, -0.03210, 1.0039 0.8333, -0.01400, 0.7075 0.9311, -0.00120, 0.3727 --------- Run Conditions: vel=103.3 ft/s Re=1.011x10^6 AOA=27.02 Flap deflection=30.00 Totals: Cl=1.1385 Cdp=0.7831 Cm(c/4)=-0.2810 Cs=-0.1804 Ch=0.0308 Main component: Cl=0.7901 Cdp=0.3748 Cm=-0.2338 Flap component: Cl=0.3484 Cdp=0.4083 Cm=-0.3897 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0386 0.5905, -0.01667, -0.0291 0.5709, 0.03110, 0.4178 0.5889, 0.07933, -1.1488 0.5500, 0.08689, -1.1410 0.5110, 0.09367, -1.1635 0.4731, 0.09830, -1.1237 0.4349, 0.10070, -1.0794 0.3960, 0.10120, -1.0427 0.3566, 0.10020, -1.0654 0.3172, 0.09790, -1.0757 0.2778, 0.09440, -1.0904 0.2393, 0.08960, -1.0806 0.2056, 0.08360, -1.0708 0.1633, 0.07610, -1.0927 0.1261, 0.06710, -1.0663 0.0900, 0.05640, -1.0756 0.0571, 0.04390, -1.0651 0.0283, 0.02940, -1.0715 0.0142, 0.01970, -1.0855 0.0081, 0.01410, -1.2665 0.0026, 0.00780, -1.2308 0.0000, 0.00000, -2.3351 0.0037, -0.00840, -0.3084 0.0112, -0.01420, 0.5475 0.0191, -0.01930, 0.8155 0.0397, -0.03030, 0.9877 0.0706, -0.04420, 0.9779 0.1037, -0.05710, 0.9232 0.1384, -0.06890, 0.8065 0.1741, -0.07950, 0.7076 0.2102, -0.08660, 0.6122 0.2472, -0.09640, 0.4811 0.2844, -0.10270, 0.3748 0.3225, -0.10690, 0.2617 0.3608, -0.10890, 0.1557 0.3991, -0.10830, 0.0675 0.4373, -0.10510, 0.0418 0.4757, -0.09890, 0.0408 0.5137, -0.09067, 0.0968 0.5611, -0.07859, 0.1450 16 Flap element taps 1.0000, 0.00130, -0.9494 0.9365, 0.01390, -0.9614 0.8333, 0.03280, -0.9750 0.7436, 0.04930, -0.9899 0.7049, 0.05667, -0.9873 0.6662, 0.06411, -0.9895 0.6274, 0.07172, -0.9907 0.6009, 0.07523, -1.0059 0.6069, 0.02889, -1.0775 0.6079, -0.01747, -0.5756 0.6167, -0.06381, -0.4309 0.6558, -0.05300, 0.0362 0.7045, -0.04117, 0.8175 0.7429, -0.03210, 1.0012 0.8333, -0.01400, 0.6955 0.9311, -0.00120, 0.3309