S809 VENTED AILERON MODEL, 18 IN CHORD --------- Run Conditions: vel=111.0 ft/s Re=1.009x10^6 AOA=-6.04 Flap deflection=-45.00 Totals: Cl=-0.6061 Cdp=0.2620 Cm(c/4)=0.1650 Cs=-0.1968 Ch=0.0194 Main component: Cl=-0.2882 Cdp=0.0141 Cm=0.0417 Flap component: Cl=-0.3179 Cdp=0.2479 Cm=0.2809 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.0639 0.5871, 0.07930, 0.0412 0.5501, 0.08690, 0.0032 0.5112, 0.09370, -0.1121 0.4731, 0.09830, -0.1860 0.4349, 0.10070, -0.1967 0.3960, 0.10120, -0.1287 0.3566, 0.10020, -0.1253 0.3172, 0.09790, -0.0851 0.2778, 0.09440, -0.0525 0.2393, 0.08960, -0.0203 0.2056, 0.08360, 0.0679 0.1633, 0.07610, 0.1229 0.1261, 0.06710, 0.2486 0.0900, 0.05640, 0.3485 0.0571, 0.04390, 0.5506 0.0283, 0.02940, 0.8034 0.0142, 0.01970, 0.9680 0.0081, 0.01410, 1.0208 0.0026, 0.00780, 0.7448 0.0000, 0.00000, -0.2981 0.0037, -0.00840, -1.0807 0.0112, -0.01420, -1.2273 0.0191, -0.01930, -0.7403 0.0397, -0.03030, -0.6363 0.0706, -0.04420, -0.5951 0.1037, -0.05710, -0.5687 0.1384, -0.06890, -0.6372 0.1741, -0.07950, -0.6391 0.2102, -0.08660, -0.6428 0.2472, -0.09640, -0.6660 0.2844, -0.10270, -0.6017 0.3225, -0.10690, -0.5255 0.3608, -0.10890, -0.3631 0.3991, -0.10830, -0.1626 0.4373, -0.10510, -0.0096 0.4757, -0.09890, 0.0152 0.5137, -0.09070, 0.0195 0.5514, -0.08120, 0.0119 0.5917, -0.06870, -0.1539 0.5917, -0.02380, -0.0946 0.5917, 0.02120, -0.0753 16 Flap element taps 1.0000, 0.00130, -0.6626 0.9365, 0.01390, 0.3807 0.8333, 0.03280, 0.8869 0.7436, 0.04930, 0.8028 0.7049, 0.05670, -0.1250 0.6667, 0.05450, -0.5053 0.6302, 0.03770, -0.4259 0.6083, 0.01980, -0.7595 0.6000, 0.00000, -1.6476 0.6076, -0.01900, -1.3652 0.6285, -0.03060, -0.9632 0.6667, -0.04090, -0.7530 0.7046, -0.04120, -0.7162 0.7429, -0.03210, -0.6931 0.8333, -0.01400, -0.6958 0.9311, -0.00120, -0.6752 --------- Run Conditions: vel=112.3 ft/s Re=1.018x10^6 AOA=0.03 Flap deflection=-45.00 Totals: Cl=-0.2452 Cdp=0.2079 Cm(c/4)=0.1612 Cs=-0.2081 Ch=-0.0006 Main component: Cl=0.0619 Cdp=-0.0195 Cm=-0.0270 Flap component: Cl=-0.3071 Cdp=0.2274 Cm=0.2495 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.1550 0.5871, 0.07930, 0.0933 0.5501, 0.08690, -0.0066 0.5112, 0.09370, -0.1660 0.4731, 0.09830, -0.2939 0.4349, 0.10070, -0.3454 0.3960, 0.10120, -0.2999 0.3566, 0.10020, -0.3455 0.3172, 0.09790, -0.3328 0.2778, 0.09440, -0.3385 0.2393, 0.08960, -0.3383 0.2056, 0.08360, -0.2792 0.1633, 0.07610, -0.2808 0.1261, 0.06710, -0.1926 0.0900, 0.05640, -0.1736 0.0571, 0.04390, -0.0326 0.0283, 0.02940, 0.1916 0.0142, 0.01970, 0.4029 0.0081, 0.01410, 0.5849 0.0026, 0.00780, 0.7415 0.0000, 0.00000, 0.9887 0.0037, -0.00840, 0.6076 0.0112, -0.01420, 0.2549 0.0191, -0.01930, 0.3008 0.0397, -0.03030, 0.1465 0.0706, -0.04420, 0.0203 0.1037, -0.05710, -0.0533 0.1384, -0.06890, -0.2091 0.1741, -0.07950, -0.2716 0.2102, -0.08660, -0.3150 0.2472, -0.09640, -0.3984 0.2844, -0.10270, -0.3887 0.3225, -0.10690, -0.3930 0.3608, -0.10890, -0.3035 0.3991, -0.10830, -0.1831 0.4373, -0.10510, 0.0597 0.4757, -0.09890, 0.1820 0.5137, -0.09070, 0.1913 0.5514, -0.08120, 0.1876 0.5917, -0.06870, 0.1092 0.5917, -0.02380, 0.1359 0.5917, 0.02120, 0.1449 16 Flap element taps 1.0000, 0.00130, -0.6284 0.9365, 0.01390, 0.3557 0.8333, 0.03280, 0.9292 0.7436, 0.04930, 0.2425 0.7049, 0.05670, -0.0043 0.6667, 0.05450, -0.0797 0.6302, 0.03770, 0.0168 0.6083, 0.01980, -0.1872 0.6000, 0.00000, -1.4319 0.6076, -0.01900, -1.2422 0.6285, -0.03060, -0.7642 0.6667, -0.04090, -0.6701 0.7046, -0.04120, -0.6645 0.7429, -0.03210, -0.6515 0.8333, -0.01400, -0.6531 0.9311, -0.00120, -0.6354 --------- Run Conditions: vel=110.7 ft/s Re=1.002x10^6 AOA=3.05 Flap deflection=-45.00 Totals: Cl=-0.1757 Cdp=0.2114 Cm(c/4)=0.1432 Cs=-0.2205 Ch=-0.0560 Main component: Cl=0.0922 Cdp=-0.0315 Cm=-0.0145 Flap component: Cl=-0.2680 Cdp=0.2430 Cm=0.1987 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.2126 0.5871, 0.07930, 0.1997 0.5501, 0.08690, 0.1461 0.5112, 0.09370, 0.0107 0.4731, 0.09830, -0.1719 0.4349, 0.10070, -0.2757 0.3960, 0.10120, -0.2439 0.3566, 0.10020, -0.3483 0.3172, 0.09790, -0.3643 0.2778, 0.09440, -0.3965 0.2393, 0.08960, -0.4167 0.2056, 0.08360, -0.3592 0.1633, 0.07610, -0.4144 0.1261, 0.06710, -0.3407 0.0900, 0.05640, -0.3723 0.0571, 0.04390, -0.2725 0.0283, 0.02940, -0.1015 0.0142, 0.01970, 0.0675 0.0081, 0.01410, 0.2288 0.0026, 0.00780, 0.4247 0.0000, 0.00000, 0.9233 0.0037, -0.00840, 0.8662 0.0112, -0.01420, 0.5780 0.0191, -0.01930, 0.5454 0.0397, -0.03030, 0.3452 0.0706, -0.04420, 0.1808 0.1037, -0.05710, 0.0806 0.1384, -0.06890, -0.1270 0.1741, -0.07950, -0.2105 0.2102, -0.08660, -0.2566 0.2472, -0.09640, -0.3830 0.2844, -0.10270, -0.3973 0.3225, -0.10690, -0.4599 0.3608, -0.10890, -0.4021 0.3991, -0.10830, -0.3543 0.4373, -0.10510, -0.1431 0.4757, -0.09890, 0.0887 0.5137, -0.09070, 0.1777 0.5514, -0.08120, 0.1905 0.5917, -0.06870, 0.1756 0.5917, -0.02380, 0.1925 0.5917, 0.02120, 0.1960 16 Flap element taps 1.0000, 0.00130, -0.7261 0.9365, 0.01390, 0.1705 0.8333, 0.03280, 0.2829 0.7436, 0.04930, 0.2158 0.7049, 0.05670, 0.0978 0.6667, 0.05450, 0.1176 0.6302, 0.03770, 0.3467 0.6083, 0.01980, 0.7452 0.6000, 0.00000, -0.7941 0.6076, -0.01900, -1.0868 0.6285, -0.03060, -0.8268 0.6667, -0.04090, -0.7457 0.7046, -0.04120, -0.7457 0.7429, -0.03210, -0.7419 0.8333, -0.01400, -0.7499 0.9311, -0.00120, -0.7215 --------- Run Conditions: vel=110.9 ft/s Re=1.002x10^6 AOA=6.04 Flap deflection=-45.00 Totals: Cl=-0.2029 Cdp=0.2413 Cm(c/4)=0.1651 Cs=-0.2613 Ch=-0.0716 Main component: Cl=0.0905 Cdp=-0.0313 Cm=0.0056 Flap component: Cl=-0.2935 Cdp=0.2726 Cm=0.2035 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.2068 0.5871, 0.07930, 0.2001 0.5501, 0.08690, 0.1757 0.5112, 0.09370, 0.1106 0.4731, 0.09830, -0.0630 0.4349, 0.10070, -0.1910 0.3960, 0.10120, -0.1665 0.3566, 0.10020, -0.3147 0.3172, 0.09790, -0.3522 0.2778, 0.09440, -0.4105 0.2393, 0.08960, -0.4477 0.2056, 0.08360, -0.3939 0.1633, 0.07610, -0.4972 0.1261, 0.06710, -0.4400 0.0900, 0.05640, -0.5199 0.0571, 0.04390, -0.4681 0.0283, 0.02940, -0.3610 0.0142, 0.01970, -0.2499 0.0081, 0.01410, -0.1419 0.0026, 0.00780, 0.0861 0.0000, 0.00000, 0.6606 0.0037, -0.00840, 0.9696 0.0112, -0.01420, 0.7744 0.0191, -0.01930, 0.7079 0.0397, -0.03030, 0.4887 0.0706, -0.04420, 0.3033 0.1037, -0.05710, 0.1857 0.1384, -0.06890, -0.0576 0.1741, -0.07950, -0.1627 0.2102, -0.08660, -0.2106 0.2472, -0.09640, -0.3691 0.2844, -0.10270, -0.4033 0.3225, -0.10690, -0.5161 0.3608, -0.10890, -0.4928 0.3991, -0.10830, -0.5152 0.4373, -0.10510, -0.3690 0.4757, -0.09890, -0.1934 0.5137, -0.09070, -0.0224 0.5514, -0.08120, 0.1273 0.5917, -0.06870, 0.1733 0.5917, -0.02380, 0.1903 0.5917, 0.02120, 0.1897 16 Flap element taps 1.0000, 0.00130, -0.9188 0.9365, 0.01390, 0.0221 0.8333, 0.03280, 0.2916 0.7436, 0.04930, 0.2501 0.7049, 0.05670, -0.1450 0.6667, 0.05450, 0.0881 0.6302, 0.03770, 0.8936 0.6083, 0.01980, 0.9034 0.6000, 0.00000, -0.7147 0.6076, -0.01900, -0.8344 0.6285, -0.03060, -0.8648 0.6667, -0.04090, -0.8535 0.7046, -0.04120, -0.8698 0.7429, -0.03210, -0.8701 0.8333, -0.01400, -0.8801 0.9311, -0.00120, -0.8643 --------- Run Conditions: vel=111.0 ft/s Re=1.002x10^6 AOA=9.06 Flap deflection=-45.00 Totals: Cl=-0.0237 Cdp=0.2274 Cm(c/4)=0.1629 Cs=-0.2283 Ch=-0.0649 Main component: Cl=0.2535 Cdp=-0.0134 Cm=-0.0226 Flap component: Cl=-0.2772 Cdp=0.2408 Cm=0.1824 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.1148 0.5871, 0.07930, 0.1048 0.5501, 0.08690, 0.0932 0.5112, 0.09370, 0.0708 0.4731, 0.09830, -0.0488 0.4349, 0.10070, -0.1953 0.3960, 0.10120, -0.1849 0.3566, 0.10020, -0.3764 0.3172, 0.09790, -0.4431 0.2778, 0.09440, -0.5306 0.2393, 0.08960, -0.5925 0.2056, 0.08360, -0.5548 0.1633, 0.07610, -0.7123 0.1261, 0.06710, -0.6897 0.0900, 0.05640, -0.8403 0.0571, 0.04390, -0.8733 0.0283, 0.02940, -0.9019 0.0142, 0.01970, -0.9447 0.0081, 0.01410, -0.9017 0.0026, 0.00780, -0.6668 0.0000, 0.00000, -0.2965 0.0037, -0.00840, 0.9467 0.0112, -0.01420, 0.9843 0.0191, -0.01930, 0.9179 0.0397, -0.03030, 0.7171 0.0706, -0.04420, 0.5304 0.1037, -0.05710, 0.3981 0.1384, -0.06890, 0.1287 0.1741, -0.07950, 0.0111 0.2102, -0.08660, -0.0340 0.2472, -0.09640, -0.2177 0.2844, -0.10270, -0.2604 0.3225, -0.10690, -0.4079 0.3608, -0.10890, -0.3931 0.3991, -0.10830, -0.4544 0.4373, -0.10510, -0.3257 0.4757, -0.09890, -0.1796 0.5137, -0.09070, -0.0341 0.5514, -0.08120, 0.1274 0.5917, -0.06870, 0.0846 0.5917, -0.02380, 0.1043 0.5917, 0.02120, 0.1032 16 Flap element taps 1.0000, 0.00130, -0.9140 0.9365, 0.01390, -0.0159 0.8333, 0.03280, 0.2106 0.7436, 0.04930, 0.1472 0.7049, 0.05670, -0.3196 0.6667, 0.05450, 0.0006 0.6302, 0.03770, 0.8716 0.6083, 0.01980, 0.9285 0.6000, 0.00000, -0.6249 0.6076, -0.01900, -0.8082 0.6285, -0.03060, -0.8438 0.6667, -0.04090, -0.8289 0.7046, -0.04120, -0.8506 0.7429, -0.03210, -0.8505 0.8333, -0.01400, -0.8702 0.9311, -0.00120, -0.8493 --------- Run Conditions: vel=111.5 ft/s Re=1.005x10^6 AOA=12.04 Flap deflection=-45.00 Totals: Cl=0.1780 Cdp=0.2133 Cm(c/4)=0.1535 Cs=-0.1715 Ch=-0.0566 Main component: Cl=0.4235 Cdp=0.0115 Cm=-0.0541 Flap component: Cl=-0.2456 Cdp=0.2018 Cm=0.1530 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.0119 0.5871, 0.07930, -0.0175 0.5501, 0.08690, -0.0258 0.5112, 0.09370, -0.0233 0.4731, 0.09830, -0.0807 0.4349, 0.10070, -0.1886 0.3960, 0.10120, -0.1871 0.3566, 0.10020, -0.4226 0.3172, 0.09790, -0.5224 0.2778, 0.09440, -0.6390 0.2393, 0.08960, -0.7336 0.2056, 0.08360, -0.7206 0.1633, 0.07610, -0.9304 0.1261, 0.06710, -0.9519 0.0900, 0.05640, -1.1838 0.0571, 0.04390, -1.3222 0.0283, 0.02940, -1.5281 0.0142, 0.01970, -1.7923 0.0081, 0.01410, -1.8669 0.0026, 0.00780, -1.7702 0.0000, 0.00000, -1.9121 0.0037, -0.00840, 0.6026 0.0112, -0.01420, 0.9893 0.0191, -0.01930, 1.0065 0.0397, -0.03030, 0.8830 0.0706, -0.04420, 0.7196 0.1037, -0.05710, 0.5872 0.1384, -0.06890, 0.3103 0.1741, -0.07950, 0.1931 0.2102, -0.08660, 0.1493 0.2472, -0.09640, -0.0500 0.2844, -0.10270, -0.1049 0.3225, -0.10690, -0.2762 0.3608, -0.10890, -0.2770 0.3991, -0.10830, -0.3705 0.4373, -0.10510, -0.2643 0.4757, -0.09890, -0.1746 0.5137, -0.09070, -0.0496 0.5514, -0.08120, 0.1466 0.5917, -0.06870, -0.0406 0.5917, -0.02380, -0.0190 0.5917, 0.02120, -0.0217 16 Flap element taps 1.0000, 0.00130, -0.8657 0.9365, 0.01390, -0.0574 0.8333, 0.03280, 0.1305 0.7436, 0.04930, 0.0341 0.7049, 0.05670, -0.5060 0.6667, 0.05450, -0.1439 0.6302, 0.03770, 0.8286 0.6083, 0.01980, 0.9601 0.6000, 0.00000, -0.5062 0.6076, -0.01900, -0.7659 0.6285, -0.03060, -0.8063 0.6667, -0.04090, -0.7871 0.7046, -0.04120, -0.8053 0.7429, -0.03210, -0.8022 0.8333, -0.01400, -0.8166 0.9311, -0.00120, -0.7916 --------- Run Conditions: vel=111.9 ft/s Re=1.009x10^6 AOA=15.04 Flap deflection=-45.00 Totals: Cl=0.4042 Cdp=0.2026 Cm(c/4)=0.1278 Cs=-0.0908 Ch=-0.0396 Main component: Cl=0.5868 Cdp=0.0498 Cm=-0.0886 Flap component: Cl=-0.1825 Cdp=0.1528 Cm=0.1057 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1885 0.5871, 0.07930, -0.1986 0.5501, 0.08690, -0.2105 0.5112, 0.09370, -0.2036 0.4731, 0.09830, -0.2262 0.4349, 0.10070, -0.2492 0.3960, 0.10120, -0.1853 0.3566, 0.10020, -0.4113 0.3172, 0.09790, -0.5401 0.2778, 0.09440, -0.6983 0.2393, 0.08960, -0.8273 0.2056, 0.08360, -0.8567 0.1633, 0.07610, -1.1168 0.1261, 0.06710, -1.1979 0.0900, 0.05640, -1.5041 0.0571, 0.04390, -1.7719 0.0283, 0.02940, -2.1860 0.0142, 0.01970, -2.7160 0.0081, 0.01410, -3.0026 0.0026, 0.00780, -3.0858 0.0000, 0.00000, -4.0519 0.0037, -0.00840, -0.0410 0.0112, -0.01420, 0.8200 0.0191, -0.01930, 0.9852 0.0397, -0.03030, 0.9752 0.0706, -0.04420, 0.8582 0.1037, -0.05710, 0.7411 0.1384, -0.06890, 0.4742 0.1741, -0.07950, 0.3570 0.2102, -0.08660, 0.3132 0.2472, -0.09640, 0.1096 0.2844, -0.10270, 0.0457 0.3225, -0.10690, -0.1363 0.3608, -0.10890, -0.1550 0.3991, -0.10830, -0.2740 0.4373, -0.10510, -0.1842 0.4757, -0.09890, -0.1161 0.5137, -0.09070, -0.0930 0.5514, -0.08120, 0.1602 0.5917, -0.06870, -0.2183 0.5917, -0.02380, -0.1964 0.5917, 0.02120, -0.1996 16 Flap element taps 1.0000, 0.00130, -0.8034 0.9365, 0.01390, -0.1095 0.8333, 0.03280, -0.0157 0.7436, 0.04930, -0.1618 0.7049, 0.05670, -0.8109 0.6667, 0.05450, -0.3828 0.6302, 0.03770, 0.7423 0.6083, 0.01980, 0.9894 0.6000, 0.00000, -0.3312 0.6076, -0.01900, -0.6897 0.6285, -0.03060, -0.7341 0.6667, -0.04090, -0.7119 0.7046, -0.04120, -0.7282 0.7429, -0.03210, -0.7257 0.8333, -0.01400, -0.7424 0.9311, -0.00120, -0.7123 --------- Run Conditions: vel=111.0 ft/s Re=0.998x10^6 AOA=18.02 Flap deflection=-45.00 Totals: Cl=0.7111 Cdp=0.2408 Cm(c/4)=0.0076 Cs=-0.0090 Ch=-0.0039 Main component: Cl=0.6835 Cdp=0.1921 Cm=-0.1466 Flap component: Cl=0.0277 Cdp=0.0487 Cm=-0.0336 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.6459 0.5871, 0.07930, -0.6853 0.5501, 0.08690, -0.7124 0.5112, 0.09370, -0.7094 0.4731, 0.09830, -0.7420 0.4349, 0.10070, -0.7474 0.3960, 0.10120, -0.6337 0.3566, 0.10020, -0.7513 0.3172, 0.09790, -0.7862 0.2778, 0.09440, -0.8393 0.2393, 0.08960, -0.8549 0.2056, 0.08360, -0.7908 0.1633, 0.07610, -0.9777 0.1261, 0.06710, -1.0219 0.0900, 0.05640, -1.2488 0.0571, 0.04390, -1.5465 0.0283, 0.02940, -2.1352 0.0142, 0.01970, -2.8580 0.0081, 0.01410, -3.3781 0.0026, 0.00780, -3.6487 0.0000, 0.00000, -5.3003 0.0037, -0.00840, -0.5560 0.0112, -0.01420, 0.6215 0.0191, -0.01930, 0.9083 0.0397, -0.03030, 1.0007 0.0706, -0.04420, 0.9326 0.1037, -0.05710, 0.8403 0.1384, -0.06890, 0.5943 0.1741, -0.07950, 0.4821 0.2102, -0.08660, 0.4348 0.2472, -0.09640, 0.2343 0.2844, -0.10270, 0.1623 0.3225, -0.10690, -0.0220 0.3608, -0.10890, -0.0608 0.3991, -0.10830, -0.2023 0.4373, -0.10510, -0.1510 0.4757, -0.09890, -0.1091 0.5137, -0.09070, -0.0748 0.5514, -0.08120, -0.0323 0.5917, -0.06870, -0.6552 0.5917, -0.02380, -0.6479 0.5917, 0.02120, -0.6550 16 Flap element taps 1.0000, 0.00130, -0.5897 0.9365, 0.01390, -0.3918 0.8333, 0.03280, -0.5091 0.7436, 0.04930, -0.6752 0.7049, 0.05670, -1.6250 0.6667, 0.05450, -0.9942 0.6302, 0.03770, 0.5154 0.6083, 0.01980, 1.0093 0.6000, 0.00000, -0.0022 0.6076, -0.01900, -0.4950 0.6285, -0.03060, -0.5388 0.6667, -0.04090, -0.5162 0.7046, -0.04120, -0.5300 0.7429, -0.03210, -0.5273 0.8333, -0.01400, -0.5376 0.9311, -0.00120, -0.5154 --------- Run Conditions: vel=111.2 ft/s Re=0.999x10^6 AOA=20.01 Flap deflection=-45.00 Totals: Cl=0.7974 Cdp=0.3131 Cm(c/4)=-0.0493 Cs=-0.0214 Ch=-0.0042 Main component: Cl=0.6921 Cdp=0.2914 Cm=-0.1769 Flap component: Cl=0.1052 Cdp=0.0217 Cm=-0.0864 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.7710 0.5871, 0.07930, -0.8277 0.5501, 0.08690, -0.8870 0.5112, 0.09370, -0.9159 0.4731, 0.09830, -0.9460 0.4349, 0.10070, -0.9566 0.3960, 0.10120, -0.8528 0.3566, 0.10020, -0.9396 0.3172, 0.09790, -0.9586 0.2778, 0.09440, -0.9969 0.2393, 0.08960, -1.0042 0.2056, 0.08360, -0.9356 0.1633, 0.07610, -1.0707 0.1261, 0.06710, -1.0492 0.0900, 0.05640, -1.1308 0.0571, 0.04390, -1.1564 0.0283, 0.02940, -1.4153 0.0142, 0.01970, -1.8352 0.0081, 0.01410, -2.2253 0.0026, 0.00780, -2.6390 0.0000, 0.00000, -4.3013 0.0037, -0.00840, -0.4117 0.0112, -0.01420, 0.6423 0.0191, -0.01930, 0.9119 0.0397, -0.03030, 1.0061 0.0706, -0.04420, 0.9444 0.1037, -0.05710, 0.8607 0.1384, -0.06890, 0.6374 0.1741, -0.07950, 0.5282 0.2102, -0.08660, 0.4701 0.2472, -0.09640, 0.2804 0.2844, -0.10270, 0.2020 0.3225, -0.10690, 0.0275 0.3608, -0.10890, -0.0216 0.3991, -0.10830, -0.1647 0.4373, -0.10510, -0.1286 0.4757, -0.09890, -0.0984 0.5137, -0.09070, -0.0723 0.5514, -0.08120, -0.0262 0.5917, -0.06870, -0.7596 0.5917, -0.02380, -0.7540 0.5917, 0.02120, -0.7713 16 Flap element taps 1.0000, 0.00130, -0.5521 0.9365, 0.01390, -0.6096 0.8333, 0.03280, -0.7514 0.7436, 0.04930, -0.8350 0.7049, 0.05670, -1.8578 0.6667, 0.05450, -1.1686 0.6302, 0.03770, 0.4508 0.6083, 0.01980, 1.0106 0.6000, 0.00000, 0.0739 0.6076, -0.01900, -0.4589 0.6285, -0.03060, -0.5001 0.6667, -0.04090, -0.4808 0.7046, -0.04120, -0.4928 0.7429, -0.03210, -0.4902 0.8333, -0.01400, -0.4931 0.9311, -0.00120, -0.4739 --------- Run Conditions: vel=110.4 ft/s Re=0.992x10^6 AOA=24.00 Flap deflection=-45.00 Totals: Cl=0.7294 Cdp=0.4052 Cm(c/4)=-0.0826 Cs=-0.0735 Ch=-0.0117 Main component: Cl=0.5740 Cdp=0.3881 Cm=-0.1680 Flap component: Cl=0.1554 Cdp=0.0171 Cm=-0.1223 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.8737 0.5871, 0.07930, -0.8213 0.5501, 0.08690, -0.8570 0.5112, 0.09370, -0.8751 0.4731, 0.09830, -0.9080 0.4349, 0.10070, -0.9140 0.3960, 0.10120, -0.8191 0.3566, 0.10020, -0.8867 0.3172, 0.09790, -0.8928 0.2778, 0.09440, -0.9058 0.2393, 0.08960, -0.8931 0.2056, 0.08360, -0.8097 0.1633, 0.07610, -0.8964 0.1261, 0.06710, -0.8540 0.0900, 0.05640, -0.8969 0.0571, 0.04390, -0.8761 0.0283, 0.02940, -0.8949 0.0142, 0.01970, -0.9243 0.0081, 0.01410, -0.8842 0.0026, 0.00780, -0.8908 0.0000, 0.00000, -1.9248 0.0037, -0.00840, -0.0083 0.0112, -0.01420, 0.7245 0.0191, -0.01930, 0.9325 0.0397, -0.03030, 1.0117 0.0706, -0.04420, 0.9598 0.1037, -0.05710, 0.8896 0.1384, -0.06890, 0.6902 0.1741, -0.07950, 0.5872 0.2102, -0.08660, 0.5252 0.2472, -0.09640, 0.3458 0.2844, -0.10270, 0.2599 0.3225, -0.10690, 0.0931 0.3608, -0.10890, 0.0340 0.3991, -0.10830, -0.1169 0.4373, -0.10510, -0.0962 0.4757, -0.09890, -0.0805 0.5137, -0.09070, -0.0652 0.5514, -0.08120, -0.0229 0.5917, -0.06870, -0.8444 0.5917, -0.02380, -0.8394 0.5917, 0.02120, -0.8714 16 Flap element taps 1.0000, 0.00130, -0.5372 0.9365, 0.01390, -0.8664 0.8333, 0.03280, -0.9243 0.7436, 0.04930, -0.9279 0.7049, 0.05670, -1.9988 0.6667, 0.05450, -1.2846 0.6302, 0.03770, 0.3978 0.6083, 0.01980, 1.0064 0.6000, 0.00000, 0.1197 0.6076, -0.01900, -0.4620 0.6285, -0.03060, -0.4981 0.6667, -0.04090, -0.4863 0.7046, -0.04120, -0.4958 0.7429, -0.03210, -0.4978 0.8333, -0.01400, -0.5041 0.9311, -0.00120, -0.4836 --------- Run Conditions: vel=110.7 ft/s Re=0.993x10^6 AOA=26.98 Flap deflection=-45.00 Totals: Cl=0.6873 Cdp=0.4654 Cm(c/4)=-0.0744 Cs=-0.1029 Ch=-0.0160 Main component: Cl=0.5554 Cdp=0.4324 Cm=-0.1707 Flap component: Cl=0.1319 Cdp=0.0330 Cm=-0.1096 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.8761 0.5871, 0.07930, -0.8428 0.5501, 0.08690, -0.8643 0.5112, 0.09370, -0.8712 0.4731, 0.09830, -0.8924 0.4349, 0.10070, -0.8975 0.3960, 0.10120, -0.8138 0.3566, 0.10020, -0.8719 0.3172, 0.09790, -0.8807 0.2778, 0.09440, -0.9018 0.2393, 0.08960, -0.8964 0.2056, 0.08360, -0.8233 0.1633, 0.07610, -0.8955 0.1261, 0.06710, -0.8576 0.0900, 0.05640, -0.8883 0.0571, 0.04390, -0.8626 0.0283, 0.02940, -0.8735 0.0142, 0.01970, -0.8889 0.0081, 0.01410, -0.8446 0.0026, 0.00780, -0.7802 0.0000, 0.00000, -1.2329 0.0037, -0.00840, 0.0147 0.0112, -0.01420, 0.6946 0.0191, -0.01930, 0.9098 0.0397, -0.03030, 1.0087 0.0706, -0.04420, 0.9725 0.1037, -0.05710, 0.9119 0.1384, -0.06890, 0.7296 0.1741, -0.07950, 0.6298 0.2102, -0.08660, 0.5619 0.2472, -0.09640, 0.3889 0.2844, -0.10270, 0.2976 0.3225, -0.10690, 0.1338 0.3608, -0.10890, 0.0666 0.3991, -0.10830, -0.0901 0.4373, -0.10510, -0.0810 0.4757, -0.09890, -0.0717 0.5137, -0.09070, -0.0644 0.5514, -0.08120, -0.0268 0.5917, -0.06870, -0.8754 0.5917, -0.02380, -0.8692 0.5917, 0.02120, -0.8822 16 Flap element taps 1.0000, 0.00130, -0.5978 0.9365, 0.01390, -0.9014 0.8333, 0.03280, -0.9243 0.7436, 0.04930, -0.9398 0.7049, 0.05670, -2.0194 0.6667, 0.05450, -1.3105 0.6302, 0.03770, 0.3880 0.6083, 0.01980, 1.0061 0.6000, 0.00000, 0.0838 0.6076, -0.01900, -0.5520 0.6285, -0.03060, -0.5859 0.6667, -0.04090, -0.5733 0.7046, -0.04120, -0.5772 0.7429, -0.03210, -0.5773 0.8333, -0.01400, -0.5821 0.9311, -0.00120, -0.5633