S809 UNVENTED AILERON, LEGR, CHORD = 18 IN --------- Run Conditions: vel=220.9 ft/s Re=2.008x10^6 AOA=-5.98 Flap deflection=-30.00 Totals: Cl=-1.1686 Cdp=0.1850 Cm(c/4)=0.1376 Cs=-0.0622 Ch=0.2270 Main component: Cl=-0.9505 Cdp=0.0481 Cm=0.2394 Flap component: Cl=-0.2181 Cdp=0.1369 Cm=0.1937 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4964 0.6175, -0.04610, -0.4688 0.5841, -0.02440, -0.4612 0.5775, 0.01750, -0.4648 0.5777, 0.04660, -0.4622 0.6274, 0.07170, 0.5722 0.5694, 0.08320, 0.5152 0.5112, 0.09370, 0.3145 0.4731, 0.09830, 0.2161 0.4349, 0.10070, 0.1776 0.3960, 0.10120, 0.1795 0.3566, 0.10020, 0.2046 0.3172, 0.09790, 0.2346 0.2778, 0.09440, 0.2631 0.2393, 0.08960, 0.3004 0.2056, 0.08360, 0.3491 0.1633, 0.07610, 0.4400 0.1261, 0.06710, 0.5437 0.0900, 0.05640, 0.6329 0.0571, 0.04390, 0.8439 0.0283, 0.02940, 1.0008 0.0142, 0.01970, 0.9756 0.0081, 0.01410, 0.7997 0.0026, 0.00780, 0.0397 0.0000, 0.00000, -0.1466 0.0037, -0.00840, -3.3459 0.0112, -0.01420, -2.4153 0.0191, -0.01930, -2.1335 0.0397, -0.03030, -1.5955 0.0706, -0.04420, -1.4384 0.1037, -0.05710, -1.3183 0.1384, -0.06890, -1.3448 0.1741, -0.07950, -1.3411 0.2102, -0.08660, -1.3934 0.2472, -0.09640, -1.4347 0.2844, -0.10270, -1.4255 0.3225, -0.10690, -1.3736 0.3608, -0.10890, -1.2906 0.3991, -0.10830, -1.1071 0.4373, -0.10510, -0.8383 0.4757, -0.09890, -0.5908 0.5137, -0.09070, -0.5233 0.5694, -0.07640, -0.5053 14 Flap element taps 1.0000, 0.00130, -0.4806 0.9365, 0.01390, 0.0078 0.8333, 0.03280, 0.2933 0.7436, 0.04930, 0.5201 0.7049, 0.05670, 0.6225 0.6662, 0.06410, 0.5892 0.6522, 0.01390, -0.4672 0.5969, -0.00020, -0.4768 0.6000, -0.03020, -0.4847 0.6324, -0.04540, -0.4856 0.6667, -0.04880, -0.4947 0.7046, -0.04110, -0.4984 0.7429, -0.03210, -0.5001 0.9311, -0.00120, -0.4981 --------- Run Conditions: vel=220.3 ft/s Re=1.997x10^6 AOA=0.01 Flap deflection=-30.00 Totals: Cl=-1.0690 Cdp=0.1210 Cm(c/4)=0.1728 Cs=-0.1212 Ch=0.2165 Main component: Cl=-0.8512 Cdp=0.0169 Cm=0.2573 Flap component: Cl=-0.2179 Cdp=0.1041 Cm=0.1827 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5495 0.6175, -0.04610, -0.4405 0.5841, -0.02440, -0.4367 0.5775, 0.01750, -0.4371 0.5777, 0.04660, -0.4302 0.6274, 0.07170, 0.4713 0.5694, 0.08320, 0.4568 0.5112, 0.09370, 0.2765 0.4731, 0.09830, 0.1444 0.4349, 0.10070, 0.0754 0.3960, 0.10120, 0.0502 0.3566, 0.10020, 0.0588 0.3172, 0.09790, 0.0689 0.2778, 0.09440, 0.0747 0.2393, 0.08960, 0.0899 0.2056, 0.08360, 0.1128 0.1633, 0.07610, 0.1876 0.1261, 0.06710, 0.2699 0.0900, 0.05640, 0.3053 0.0571, 0.04390, 0.5578 0.0283, 0.02940, 0.8008 0.0142, 0.01970, 0.9727 0.0081, 0.01410, 1.0007 0.0026, 0.00780, 0.7290 0.0000, 0.00000, -0.1246 0.0037, -0.00840, -1.1802 0.0112, -0.01420, -0.9462 0.0191, -0.01930, -0.9637 0.0397, -0.03030, -0.8176 0.0706, -0.04420, -0.8708 0.1037, -0.05710, -0.8778 0.1384, -0.06890, -1.0123 0.1741, -0.07950, -1.0947 0.2102, -0.08660, -1.2261 0.2472, -0.09640, -1.3565 0.2844, -0.10270, -1.4417 0.3225, -0.10690, -1.4988 0.3608, -0.10890, -1.5504 0.3991, -0.10830, -1.5245 0.4373, -0.10510, -1.4409 0.4757, -0.09890, -1.2220 0.5137, -0.09070, -1.0444 0.5694, -0.07640, -0.7365 14 Flap element taps 1.0000, 0.00130, -0.4558 0.9365, 0.01390, 0.0159 0.8333, 0.03280, 0.2873 0.7436, 0.04930, 0.5027 0.7049, 0.05670, 0.5340 0.6662, 0.06410, 0.4702 0.6522, 0.01390, -0.4358 0.5969, -0.00020, -0.4493 0.6000, -0.03020, -0.4733 0.6324, -0.04540, -0.4687 0.6667, -0.04880, -0.4612 0.7046, -0.04110, -0.4606 0.7429, -0.03210, -0.4650 0.9311, -0.00120, -0.4752 --------- Run Conditions: vel=221.2 ft/s Re=2.004x10^6 AOA=3.03 Flap deflection=-30.00 Totals: Cl=-0.8366 Cdp=0.0895 Cm(c/4)=0.1696 Cs=-0.1336 Ch=0.1975 Main component: Cl=-0.6343 Cdp=0.0070 Cm=0.2113 Flap component: Cl=-0.2023 Cdp=0.0826 Cm=0.1659 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5145 0.6175, -0.04610, -0.4018 0.5841, -0.02440, -0.3959 0.5775, 0.01750, -0.3983 0.5777, 0.04660, -0.3919 0.6274, 0.07170, 0.3959 0.5694, 0.08320, 0.3930 0.5112, 0.09370, 0.2496 0.4731, 0.09830, 0.0983 0.4349, 0.10070, 0.0076 0.3960, 0.10120, -0.0363 0.3566, 0.10020, -0.0417 0.3172, 0.09790, -0.0454 0.2778, 0.09440, -0.0560 0.2393, 0.08960, -0.0583 0.2056, 0.08360, -0.0568 0.1633, 0.07610, 0.0006 0.1261, 0.06710, 0.0610 0.0900, 0.05640, 0.0475 0.0571, 0.04390, 0.2985 0.0283, 0.02940, 0.5422 0.0142, 0.01970, 0.7639 0.0081, 0.01410, 0.8917 0.0026, 0.00780, 0.9808 0.0000, 0.00000, -0.1072 0.0037, -0.00840, -0.0933 0.0112, -0.01420, -0.1761 0.0191, -0.01930, -0.3011 0.0397, -0.03030, -0.3257 0.0706, -0.04420, -0.4673 0.1037, -0.05710, -0.5308 0.1384, -0.06890, -0.6991 0.1741, -0.07950, -0.8112 0.2102, -0.08660, -0.9642 0.2472, -0.09640, -1.1126 0.2844, -0.10270, -1.2199 0.3225, -0.10690, -1.2974 0.3608, -0.10890, -1.3721 0.3991, -0.10830, -1.3714 0.4373, -0.10510, -1.3210 0.4757, -0.09890, -1.1339 0.5137, -0.09070, -0.9838 0.5694, -0.07640, -0.6968 14 Flap element taps 1.0000, 0.00130, -0.4113 0.9365, 0.01390, 0.0136 0.8333, 0.03280, 0.2780 0.7436, 0.04930, 0.4659 0.7049, 0.05670, 0.4586 0.6662, 0.06410, 0.3941 0.6522, 0.01390, -0.3980 0.5969, -0.00020, -0.4087 0.6000, -0.03020, -0.4302 0.6324, -0.04540, -0.4242 0.6667, -0.04880, -0.4173 0.7046, -0.04110, -0.4144 0.7429, -0.03210, -0.4210 0.9311, -0.00120, -0.4263 --------- Run Conditions: vel=222.1 ft/s Re=2.009x10^6 AOA=6.03 Flap deflection=-30.00 Totals: Cl=-0.5833 Cdp=0.0756 Cm(c/4)=0.1701 Cs=-0.1364 Ch=0.1859 Main component: Cl=-0.3930 Cdp=0.0103 Cm=0.1595 Flap component: Cl=-0.1903 Cdp=0.0653 Cm=0.1536 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4952 0.6175, -0.04610, -0.3919 0.5841, -0.02440, -0.3870 0.5775, 0.01750, -0.3885 0.5777, 0.04660, -0.3826 0.6274, 0.07170, 0.3042 0.5694, 0.08320, 0.3085 0.5112, 0.09370, 0.2222 0.4731, 0.09830, 0.0582 0.4349, 0.10070, -0.0628 0.3960, 0.10120, -0.1313 0.3566, 0.10020, -0.1575 0.3172, 0.09790, -0.1799 0.2778, 0.09440, -0.2096 0.2393, 0.08960, -0.2344 0.2056, 0.08360, -0.2572 0.1633, 0.07610, -0.2262 0.1261, 0.06710, -0.1963 0.0900, 0.05640, -0.2770 0.0571, 0.04390, -0.0529 0.0283, 0.02940, 0.1392 0.0142, 0.01970, 0.3457 0.0081, 0.01410, 0.5174 0.0026, 0.00780, 0.6749 0.0000, 0.00000, -0.0896 0.0037, -0.00840, 0.6876 0.0112, -0.01420, 0.4405 0.0191, -0.01930, 0.2813 0.0397, -0.03030, 0.1253 0.0706, -0.04420, -0.0766 0.1037, -0.05710, -0.1904 0.1384, -0.06890, -0.3823 0.1741, -0.07950, -0.5188 0.2102, -0.08660, -0.6880 0.2472, -0.09640, -0.8509 0.2844, -0.10270, -0.9772 0.3225, -0.10690, -1.0754 0.3608, -0.10890, -1.1723 0.3991, -0.10830, -1.1969 0.4373, -0.10510, -1.1798 0.4757, -0.09890, -1.0281 0.5137, -0.09070, -0.9080 0.5694, -0.07640, -0.6545 14 Flap element taps 1.0000, 0.00130, -0.4012 0.9365, 0.01390, 0.0032 0.8333, 0.03280, 0.2635 0.7436, 0.04930, 0.3867 0.7049, 0.05670, 0.3456 0.6662, 0.06410, 0.3021 0.6522, 0.01390, -0.3893 0.5969, -0.00020, -0.3975 0.6000, -0.03020, -0.4207 0.6324, -0.04540, -0.4147 0.6667, -0.04880, -0.4058 0.7046, -0.04110, -0.4025 0.7429, -0.03210, -0.4091 0.9311, -0.00120, -0.4183 --------- Run Conditions: vel=223.1 ft/s Re=2.016x10^6 AOA=9.04 Flap deflection=-30.00 Totals: Cl=-0.3195 Cdp=0.0706 Cm(c/4)=0.1676 Cs=-0.1199 Ch=0.1726 Main component: Cl=-0.1453 Cdp=0.0225 Cm=0.1044 Flap component: Cl=-0.1742 Cdp=0.0481 Cm=0.1393 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4636 0.6175, -0.04610, -0.3823 0.5841, -0.02440, -0.3747 0.5775, 0.01750, -0.3806 0.5777, 0.04660, -0.3764 0.6274, 0.07170, 0.1993 0.5694, 0.08320, 0.2059 0.5112, 0.09370, 0.1654 0.4731, 0.09830, 0.0308 0.4349, 0.10070, -0.1196 0.3960, 0.10120, -0.2169 0.3566, 0.10020, -0.2681 0.3172, 0.09790, -0.3125 0.2778, 0.09440, -0.3665 0.2393, 0.08960, -0.4167 0.2056, 0.08360, -0.4684 0.1633, 0.07610, -0.4714 0.1261, 0.06710, -0.4794 0.0900, 0.05640, -0.6334 0.0571, 0.04390, -0.4723 0.0283, 0.02940, -0.3845 0.0142, 0.01970, -0.2629 0.0081, 0.01410, -0.1776 0.0026, 0.00780, 0.0737 0.0000, 0.00000, -0.0723 0.0037, -0.00840, 0.9990 0.0112, -0.01420, 0.8461 0.0191, -0.01930, 0.6979 0.0397, -0.03030, 0.4906 0.0706, -0.04420, 0.2618 0.1037, -0.05710, 0.1147 0.1384, -0.06890, -0.0866 0.1741, -0.07950, -0.2393 0.2102, -0.08660, -0.4178 0.2472, -0.09640, -0.5903 0.2844, -0.10270, -0.7299 0.3225, -0.10690, -0.8455 0.3608, -0.10890, -0.9593 0.3991, -0.10830, -1.0070 0.4373, -0.10510, -1.0191 0.4757, -0.09890, -0.9016 0.5137, -0.09070, -0.8106 0.5694, -0.07640, -0.5902 14 Flap element taps 1.0000, 0.00130, -0.3830 0.9365, 0.01390, 0.0016 0.8333, 0.03280, 0.2485 0.7436, 0.04930, 0.2814 0.7049, 0.05670, 0.2287 0.6662, 0.06410, 0.1956 0.6522, 0.01390, -0.3793 0.5969, -0.00020, -0.3866 0.6000, -0.03020, -0.4073 0.6324, -0.04540, -0.4014 0.6667, -0.04880, -0.3902 0.7046, -0.04110, -0.3856 0.7429, -0.03210, -0.3914 0.9311, -0.00120, -0.4060 --------- Run Conditions: vel=222.4 ft/s Re=2.007x10^6 AOA=12.02 Flap deflection=-30.00 Totals: Cl=-0.0439 Cdp=0.0749 Cm(c/4)=0.1586 Cs=-0.0824 Ch=0.1524 Main component: Cl=0.1038 Cdp=0.0444 Cm=0.0475 Flap component: Cl=-0.1477 Cdp=0.0305 Cm=0.1180 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4205 0.6175, -0.04610, -0.3684 0.5841, -0.02440, -0.3638 0.5775, 0.01750, -0.3684 0.5777, 0.04660, -0.3652 0.6274, 0.07170, 0.0701 0.5694, 0.08320, 0.0752 0.5112, 0.09370, 0.0644 0.4731, 0.09830, 0.0058 0.4349, 0.10070, -0.1426 0.3960, 0.10120, -0.2767 0.3566, 0.10020, -0.3629 0.3172, 0.09790, -0.4362 0.2778, 0.09440, -0.5188 0.2393, 0.08960, -0.5995 0.2056, 0.08360, -0.6852 0.1633, 0.07610, -0.7319 0.1261, 0.06710, -0.7867 0.0900, 0.05640, -1.0180 0.0571, 0.04390, -0.9597 0.0283, 0.02940, -1.0318 0.0142, 0.01970, -1.0872 0.0081, 0.01410, -1.1112 0.0026, 0.00780, -0.8088 0.0000, 0.00000, -0.0600 0.0037, -0.00840, 0.9259 0.0112, -0.01420, 1.0051 0.0191, -0.01930, 0.9418 0.0397, -0.03030, 0.7629 0.0706, -0.04420, 0.5393 0.1037, -0.05710, 0.3774 0.1384, -0.06890, 0.1811 0.1741, -0.07950, 0.0202 0.2102, -0.08660, -0.1606 0.2472, -0.09640, -0.3355 0.2844, -0.10270, -0.4844 0.3225, -0.10690, -0.6138 0.3608, -0.10890, -0.7406 0.3991, -0.10830, -0.8087 0.4373, -0.10510, -0.8460 0.4757, -0.09890, -0.7623 0.5137, -0.09070, -0.6964 0.5694, -0.07640, -0.5142 14 Flap element taps 1.0000, 0.00130, -0.3605 0.9365, 0.01390, 0.0080 0.8333, 0.03280, 0.2035 0.7436, 0.04930, 0.1289 0.7049, 0.05670, 0.0813 0.6662, 0.06410, 0.0663 0.6522, 0.01390, -0.3676 0.5969, -0.00020, -0.3737 0.6000, -0.03020, -0.3911 0.6324, -0.04540, -0.3846 0.6667, -0.04880, -0.3645 0.7046, -0.04110, -0.3599 0.7429, -0.03210, -0.3665 0.9311, -0.00120, -0.3874 --------- Run Conditions: vel=222.2 ft/s Re=1.998x10^6 AOA=15.06 Flap deflection=-30.00 Totals: Cl=0.1670 Cdp=0.0878 Cm(c/4)=0.1483 Cs=-0.0414 Ch=0.1329 Main component: Cl=0.2890 Cdp=0.0724 Cm=0.0040 Flap component: Cl=-0.1220 Cdp=0.0154 Cm=0.0982 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4005 0.6175, -0.04610, -0.3799 0.5841, -0.02440, -0.3747 0.5775, 0.01750, -0.3762 0.5777, 0.04660, -0.3751 0.6274, 0.07170, -0.0479 0.5694, 0.08320, -0.0509 0.5112, 0.09370, -0.0507 0.4731, 0.09830, -0.0652 0.4349, 0.10070, -0.1539 0.3960, 0.10120, -0.2794 0.3566, 0.10020, -0.4064 0.3172, 0.09790, -0.5098 0.2778, 0.09440, -0.6227 0.2393, 0.08960, -0.7308 0.2056, 0.08360, -0.8337 0.1633, 0.07610, -0.9346 0.1261, 0.06710, -1.0269 0.0900, 0.05640, -1.3212 0.0571, 0.04390, -1.3728 0.0283, 0.02940, -1.6129 0.0142, 0.01970, -1.8682 0.0081, 0.01410, -2.0295 0.0026, 0.00780, -1.7784 0.0000, 0.00000, -0.1296 0.0037, -0.00840, 0.6144 0.0112, -0.01420, 0.9842 0.0191, -0.01930, 1.0110 0.0397, -0.03030, 0.9046 0.0706, -0.04420, 0.7119 0.1037, -0.05710, 0.5507 0.1384, -0.06890, 0.3527 0.1741, -0.07950, 0.1899 0.2102, -0.08660, 0.0227 0.2472, -0.09640, -0.1567 0.2844, -0.10270, -0.3007 0.3225, -0.10690, -0.4477 0.3608, -0.10890, -0.5782 0.3991, -0.10830, -0.6669 0.4373, -0.10510, -0.7136 0.4757, -0.09890, -0.6512 0.5137, -0.09070, -0.6083 0.5694, -0.07640, -0.4602 14 Flap element taps 1.0000, 0.00130, -0.3457 0.9365, 0.01390, 0.0121 0.8333, 0.03280, 0.1308 0.7436, 0.04930, -0.0080 0.7049, 0.05670, -0.0465 0.6662, 0.06410, -0.0516 0.6522, 0.01390, -0.3726 0.5969, -0.00020, -0.3810 0.6000, -0.03020, -0.3961 0.6324, -0.04540, -0.3848 0.6667, -0.04880, -0.3488 0.7046, -0.04110, -0.3433 0.7429, -0.03210, -0.3487 0.9311, -0.00120, -0.3796 --------- Run Conditions: vel=222.4 ft/s Re=1.998x10^6 AOA=18.05 Flap deflection=-30.00 Totals: Cl=0.5152 Cdp=0.1136 Cm(c/4)=0.0953 Cs=0.0516 Ch=0.0489 Main component: Cl=0.5394 Cdp=0.1302 Cm=-0.0618 Flap component: Cl=-0.0242 Cdp=-0.0166 Cm=0.0258 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3700 0.6175, -0.04610, -0.4478 0.5841, -0.02440, -0.4432 0.5775, 0.01750, -0.4416 0.5777, 0.04660, -0.4419 0.6274, 0.07170, -0.3114 0.5694, 0.08320, -0.3154 0.5112, 0.09370, -0.3125 0.4731, 0.09830, -0.3123 0.4349, 0.10070, -0.3263 0.3960, 0.10120, -0.3535 0.3566, 0.10020, -0.4181 0.3172, 0.09790, -0.5168 0.2778, 0.09440, -0.6545 0.2393, 0.08960, -0.8159 0.2056, 0.08360, -0.9818 0.1633, 0.07610, -1.1562 0.1261, 0.06710, -1.3332 0.0900, 0.05640, -1.6982 0.0571, 0.04390, -1.9524 0.0283, 0.02940, -2.4930 0.0142, 0.01970, -3.0858 0.0081, 0.01410, -3.5675 0.0026, 0.00780, -3.5659 0.0000, 0.00000, -0.1118 0.0037, -0.00840, -0.1732 0.0112, -0.01420, 0.7547 0.0191, -0.01930, 0.9601 0.0397, -0.03030, 1.0057 0.0706, -0.04420, 0.8868 0.1037, -0.05710, 0.7457 0.1384, -0.06890, 0.5735 0.1741, -0.07950, 0.4162 0.2102, -0.08660, 0.2537 0.2472, -0.09640, 0.0744 0.2844, -0.10270, -0.0763 0.3225, -0.10690, -0.2254 0.3608, -0.10890, -0.3612 0.3991, -0.10830, -0.4758 0.4373, -0.10510, -0.5358 0.4757, -0.09890, -0.5034 0.5137, -0.09070, -0.4911 0.5694, -0.07640, -0.3733 14 Flap element taps 1.0000, 0.00130, -0.2934 0.9365, 0.01390, -0.0385 0.8333, 0.03280, -0.1425 0.7436, 0.04930, -0.2975 0.7049, 0.05670, -0.3202 0.6662, 0.06410, -0.3161 0.6522, 0.01390, -0.4403 0.5969, -0.00020, -0.4453 0.6000, -0.03020, -0.4519 0.6324, -0.04540, -0.3959 0.6667, -0.04880, -0.2578 0.7046, -0.04110, -0.2406 0.7429, -0.03210, -0.2424 0.9311, -0.00120, -0.2796 --------- Run Conditions: vel=224.0 ft/s Re=2.011x10^6 AOA=20.02 Flap deflection=-30.00 Totals: Cl=0.4742 Cdp=0.1620 Cm(c/4)=0.0640 Cs=0.0101 Ch=0.0221 Main component: Cl=0.4677 Cdp=0.1900 Cm=-0.0655 Flap component: Cl=0.0065 Cdp=-0.0279 Cm=0.0042 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4896 0.6175, -0.04610, -0.6243 0.5841, -0.02440, -0.6195 0.5775, 0.01750, -0.6215 0.5777, 0.04660, -0.6219 0.6274, 0.07170, -0.4989 0.5694, 0.08320, -0.5072 0.5112, 0.09370, -0.5125 0.4731, 0.09830, -0.5161 0.4349, 0.10070, -0.5171 0.3960, 0.10120, -0.5186 0.3566, 0.10020, -0.5361 0.3172, 0.09790, -0.5555 0.2778, 0.09440, -0.5887 0.2393, 0.08960, -0.6410 0.2056, 0.08360, -0.7205 0.1633, 0.07610, -0.8386 0.1261, 0.06710, -0.9977 0.0900, 0.05640, -1.3000 0.0571, 0.04390, -1.6063 0.0283, 0.02940, -2.1588 0.0142, 0.01970, -2.7530 0.0081, 0.01410, -3.2264 0.0026, 0.00780, -3.2639 0.0000, 0.00000, -0.1036 0.0037, -0.00840, -0.1341 0.0112, -0.01420, 0.7582 0.0191, -0.01930, 0.9580 0.0397, -0.03030, 1.0038 0.0706, -0.04420, 0.8881 0.1037, -0.05710, 0.7489 0.1384, -0.06890, 0.5760 0.1741, -0.07950, 0.4181 0.2102, -0.08660, 0.2532 0.2472, -0.09640, 0.0686 0.2844, -0.10270, -0.0881 0.3225, -0.10690, -0.2473 0.3608, -0.10890, -0.3916 0.3991, -0.10830, -0.5179 0.4373, -0.10510, -0.5897 0.4757, -0.09890, -0.5670 0.5137, -0.09070, -0.5652 0.5694, -0.07640, -0.4613 14 Flap element taps 1.0000, 0.00130, -0.4012 0.9365, 0.01390, -0.2115 0.8333, 0.03280, -0.3315 0.7436, 0.04930, -0.4676 0.7049, 0.05670, -0.5079 0.6662, 0.06410, -0.5116 0.6522, 0.01390, -0.6202 0.5969, -0.00020, -0.6249 0.6000, -0.03020, -0.6335 0.6324, -0.04540, -0.5377 0.6667, -0.04880, -0.3592 0.7046, -0.04110, -0.3159 0.7429, -0.03210, -0.3242 0.9311, -0.00120, -0.3685 --------- Run Conditions: vel=222.8 ft/s Re=1.998x10^6 AOA=24.02 Flap deflection=-30.00 Totals: Cl=0.2903 Cdp=0.2449 Cm(c/4)=0.0464 Cs=-0.1056 Ch=0.0171 Main component: Cl=0.2930 Cdp=0.2695 Cm=-0.0545 Flap component: Cl=-0.0027 Cdp=-0.0246 Cm=0.0097 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6528 0.6175, -0.04610, -0.8399 0.5841, -0.02440, -0.8345 0.5775, 0.01750, -0.8349 0.5777, 0.04660, -0.8343 0.6274, 0.07170, -0.5282 0.5694, 0.08320, -0.5812 0.5112, 0.09370, -0.6067 0.4731, 0.09830, -0.5970 0.4349, 0.10070, -0.6006 0.3960, 0.10120, -0.5920 0.3566, 0.10020, -0.6019 0.3172, 0.09790, -0.6066 0.2778, 0.09440, -0.6155 0.2393, 0.08960, -0.6290 0.2056, 0.08360, -0.6394 0.1633, 0.07610, -0.6583 0.1261, 0.06710, -0.6716 0.0900, 0.05640, -0.6973 0.0571, 0.04390, -0.7525 0.0283, 0.02940, -0.8997 0.0142, 0.01970, -1.1986 0.0081, 0.01410, -1.4663 0.0026, 0.00780, -1.6244 0.0000, 0.00000, -0.1038 0.0037, -0.00840, 0.2091 0.0112, -0.01420, 0.8380 0.0191, -0.01930, 0.9792 0.0397, -0.03030, 0.9961 0.0706, -0.04420, 0.8815 0.1037, -0.05710, 0.7477 0.1384, -0.06890, 0.5783 0.1741, -0.07950, 0.4206 0.2102, -0.08660, 0.2536 0.2472, -0.09640, 0.0627 0.2844, -0.10270, -0.1028 0.3225, -0.10690, -0.2737 0.3608, -0.10890, -0.4333 0.3991, -0.10830, -0.5785 0.4373, -0.10510, -0.6692 0.4757, -0.09890, -0.6595 0.5137, -0.09070, -0.6733 0.5694, -0.07640, -0.5895 14 Flap element taps 1.0000, 0.00130, -0.5100 0.9365, 0.01390, -0.4832 0.8333, 0.03280, -0.5615 0.7436, 0.04930, -0.5797 0.7049, 0.05670, -0.5643 0.6662, 0.06410, -0.5384 0.6522, 0.01390, -0.8292 0.5969, -0.00020, -0.8429 0.6000, -0.03020, -0.8520 0.6324, -0.04540, -0.7784 0.6667, -0.04880, -0.5969 0.7046, -0.04110, -0.5346 0.7429, -0.03210, -0.5398 0.9311, -0.00120, -0.5681 --------- Run Conditions: vel=224.6 ft/s Re=2.014x10^6 AOA=27.00 Flap deflection=-30.00 Totals: Cl=0.2486 Cdp=0.2866 Cm(c/4)=0.0745 Cs=-0.1425 Ch=0.0600 Main component: Cl=0.2964 Cdp=0.3146 Cm=-0.0589 Flap component: Cl=-0.0478 Cdp=-0.0279 Cm=0.0455 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7560 0.6175, -0.04610, -0.9930 0.5841, -0.02440, -0.9850 0.5775, 0.01750, -0.9830 0.5777, 0.04660, -0.9820 0.6274, 0.07170, -0.5682 0.5694, 0.08320, -0.6077 0.5112, 0.09370, -0.6330 0.4731, 0.09830, -0.6275 0.4349, 0.10070, -0.6308 0.3960, 0.10120, -0.6323 0.3566, 0.10020, -0.6414 0.3172, 0.09790, -0.6472 0.2778, 0.09440, -0.6618 0.2393, 0.08960, -0.6751 0.2056, 0.08360, -0.7023 0.1633, 0.07610, -0.7527 0.1261, 0.06710, -0.7813 0.0900, 0.05640, -0.8206 0.0571, 0.04390, -0.8952 0.0283, 0.02940, -0.9860 0.0142, 0.01970, -1.1638 0.0081, 0.01410, -1.3412 0.0026, 0.00780, -1.4595 0.0000, 0.00000, -0.0903 0.0037, -0.00840, 0.1227 0.0112, -0.01420, 0.7960 0.0191, -0.01930, 0.9616 0.0397, -0.03030, 1.0068 0.0706, -0.04420, 0.9104 0.1037, -0.05710, 0.7837 0.1384, -0.06890, 0.6187 0.1741, -0.07950, 0.4613 0.2102, -0.08660, 0.2925 0.2472, -0.09640, 0.0965 0.2844, -0.10270, -0.0777 0.3225, -0.10690, -0.2636 0.3608, -0.10890, -0.4378 0.3991, -0.10830, -0.5989 0.4373, -0.10510, -0.7055 0.4757, -0.09890, -0.7127 0.5137, -0.09070, -0.7407 0.5694, -0.07640, -0.6632 14 Flap element taps 1.0000, 0.00130, -0.5887 0.9365, 0.01390, -0.5088 0.8333, 0.03280, -0.5731 0.7436, 0.04930, -0.5927 0.7049, 0.05670, -0.5887 0.6662, 0.06410, -0.5676 0.6522, 0.01390, -0.9848 0.5969, -0.00020, -1.0014 0.6000, -0.03020, -1.0196 0.6324, -0.04540, -0.9860 0.6667, -0.04880, -0.7984 0.7046, -0.04110, -0.7087 0.7429, -0.03210, -0.7160 0.9311, -0.00120, -0.7041