S809 UNVENTED AILERON, LEGR, CHORD = 18 IN --------- Run Conditions: vel=100.6 ft/s Re=1.003x10^6 AOA=-6.01 Flap deflection=-20.00 Totals: Cl=-1.0108 Cdp=0.1180 Cm(c/4)=0.0981 Cs=-0.0115 Ch=0.1656 Main component: Cl=-0.8322 Cdp=0.0395 Cm=0.2014 Flap component: Cl=-0.1786 Cdp=0.0785 Cm=0.1511 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4386 0.6175, -0.04610, -0.3916 0.5841, -0.02440, -0.3799 0.5775, 0.01750, -0.3880 0.5777, 0.04660, -0.3882 0.6274, 0.07170, 0.5014 0.5694, 0.08320, 0.3226 0.5112, 0.09370, 0.0664 0.4731, 0.09830, 0.0138 0.4349, 0.10070, -0.0107 0.3960, 0.10120, -0.0100 0.3566, 0.10020, 0.0491 0.3172, 0.09790, 0.0979 0.2778, 0.09440, 0.1300 0.2393, 0.08960, 0.1849 0.2056, 0.08360, 0.2282 0.1633, 0.07610, 0.3469 0.1261, 0.06710, 0.4473 0.0900, 0.05640, 0.5721 0.0571, 0.04390, 0.7913 0.0283, 0.02940, 0.9850 0.0142, 0.01970, 0.9995 0.0081, 0.01410, 0.8404 0.0026, 0.00780, 0.1326 0.0000, 0.00000, -0.2176 0.0037, -0.00840, -3.0192 0.0112, -0.01420, -2.2324 0.0191, -0.01930, -1.8916 0.0397, -0.03030, -1.4363 0.0706, -0.04420, -1.3222 0.1037, -0.05710, -1.2212 0.1384, -0.06890, -1.2411 0.1741, -0.07950, -1.2668 0.2102, -0.08660, -1.3312 0.2472, -0.09640, -1.3705 0.2844, -0.10270, -1.3702 0.3225, -0.10690, -1.3199 0.3608, -0.10890, -1.2706 0.3991, -0.10830, -1.1096 0.4373, -0.10510, -0.8845 0.4757, -0.09890, -0.6109 0.5137, -0.09070, -0.4811 0.5694, -0.07640, -0.4323 14 Flap element taps 1.0000, 0.00130, -0.4208 0.9365, 0.01390, -0.0655 0.8333, 0.03280, 0.1423 0.7436, 0.04930, 0.3074 0.7049, 0.05670, 0.4277 0.6662, 0.06410, 0.5517 0.6522, 0.01390, -0.3875 0.5969, -0.00020, -0.3927 0.6000, -0.03020, -0.4320 0.6324, -0.04540, -0.4210 0.6667, -0.04880, -0.4260 0.7046, -0.04110, -0.4246 0.7429, -0.03210, -0.4370 0.9311, -0.00120, -0.4328 --------- Run Conditions: vel=100.5 ft/s Re=1.000x10^6 AOA=0.02 Flap deflection=-20.00 Totals: Cl=-0.7926 Cdp=0.0563 Cm(c/4)=0.1160 Cs=-0.0566 Ch=0.1364 Main component: Cl=-0.6394 Cdp=0.0103 Cm=0.1898 Flap component: Cl=-0.1532 Cdp=0.0459 Cm=0.1244 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4080 0.6175, -0.04610, -0.2932 0.5841, -0.02440, -0.2852 0.5775, 0.01750, -0.2884 0.5777, 0.04660, -0.2882 0.6274, 0.07170, 0.3823 0.5694, 0.08320, 0.2658 0.5112, 0.09370, 0.0127 0.4731, 0.09830, -0.0879 0.4349, 0.10070, -0.1375 0.3960, 0.10120, -0.1724 0.3566, 0.10020, -0.1130 0.3172, 0.09790, -0.0873 0.2778, 0.09440, -0.0785 0.2393, 0.08960, -0.0555 0.2056, 0.08360, -0.0577 0.1633, 0.07610, 0.0559 0.1261, 0.06710, 0.1187 0.0900, 0.05640, 0.1937 0.0571, 0.04390, 0.4379 0.0283, 0.02940, 0.7063 0.0142, 0.01970, 0.9105 0.0081, 0.01410, 0.9492 0.0026, 0.00780, 0.8377 0.0000, 0.00000, -0.0868 0.0037, -0.00840, -0.7844 0.0112, -0.01420, -0.6347 0.0191, -0.01930, -0.6914 0.0397, -0.03030, -0.5900 0.0706, -0.04420, -0.6924 0.1037, -0.05710, -0.7174 0.1384, -0.06890, -0.8213 0.1741, -0.07950, -0.9286 0.2102, -0.08660, -1.0785 0.2472, -0.09640, -1.1818 0.2844, -0.10270, -1.2678 0.3225, -0.10690, -1.2911 0.3608, -0.10890, -1.3595 0.3991, -0.10830, -1.3180 0.4373, -0.10510, -1.2502 0.4757, -0.09890, -1.0560 0.5137, -0.09070, -0.8852 0.5694, -0.07640, -0.5745 14 Flap element taps 1.0000, 0.00130, -0.3082 0.9365, 0.01390, -0.0211 0.8333, 0.03280, 0.1476 0.7436, 0.04930, 0.2966 0.7049, 0.05670, 0.3806 0.6662, 0.06410, 0.4073 0.6522, 0.01390, -0.2986 0.5969, -0.00020, -0.2924 0.6000, -0.03020, -0.3383 0.6324, -0.04540, -0.3386 0.6667, -0.04880, -0.3340 0.7046, -0.04110, -0.3160 0.7429, -0.03210, -0.3290 0.9311, -0.00120, -0.3202 --------- Run Conditions: vel=100.6 ft/s Re=1.000x10^6 AOA=3.03 Flap deflection=-20.00 Totals: Cl=-0.5547 Cdp=0.0417 Cm(c/4)=0.1180 Cs=-0.0709 Ch=0.1250 Main component: Cl=-0.4132 Cdp=0.0088 Cm=0.1426 Flap component: Cl=-0.1414 Cdp=0.0329 Cm=0.1133 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3895 0.6175, -0.04610, -0.2736 0.5841, -0.02440, -0.2654 0.5775, 0.01750, -0.2715 0.5777, 0.04660, -0.2708 0.6274, 0.07170, 0.3048 0.5694, 0.08320, 0.2225 0.5112, 0.09370, -0.0393 0.4731, 0.09830, -0.1605 0.4349, 0.10070, -0.2325 0.3960, 0.10120, -0.2898 0.3566, 0.10020, -0.2345 0.3172, 0.09790, -0.2246 0.2778, 0.09440, -0.2336 0.2393, 0.08960, -0.2271 0.2056, 0.08360, -0.2586 0.1633, 0.07610, -0.1545 0.1261, 0.06710, -0.1210 0.0900, 0.05640, -0.0995 0.0571, 0.04390, 0.1306 0.0283, 0.02940, 0.3826 0.0142, 0.01970, 0.6125 0.0081, 0.01410, 0.7265 0.0026, 0.00780, 0.9153 0.0000, 0.00000, -0.0277 0.0037, -0.00840, 0.2699 0.0112, -0.01420, 0.0846 0.0191, -0.01930, -0.0490 0.0397, -0.03030, -0.1236 0.0706, -0.04420, -0.3018 0.1037, -0.05710, -0.3868 0.1384, -0.06890, -0.5113 0.1741, -0.07950, -0.6462 0.2102, -0.08660, -0.8267 0.2472, -0.09640, -0.9430 0.2844, -0.10270, -1.0568 0.3225, -0.10690, -1.0945 0.3608, -0.10890, -1.1925 0.3991, -0.10830, -1.1742 0.4373, -0.10510, -1.1444 0.4757, -0.09890, -0.9788 0.5137, -0.09070, -0.8433 0.5694, -0.07640, -0.5513 14 Flap element taps 1.0000, 0.00130, -0.2802 0.9365, 0.01390, -0.0229 0.8333, 0.03280, 0.1297 0.7436, 0.04930, 0.2703 0.7049, 0.05670, 0.3284 0.6662, 0.06410, 0.3214 0.6522, 0.01390, -0.2870 0.5969, -0.00020, -0.2747 0.6000, -0.03020, -0.3174 0.6324, -0.04540, -0.3238 0.6667, -0.04880, -0.3175 0.7046, -0.04110, -0.2940 0.7429, -0.03210, -0.3090 0.9311, -0.00120, -0.2957 --------- Run Conditions: vel=101.2 ft/s Re=1.006x10^6 AOA=6.04 Flap deflection=-20.00 Totals: Cl=-0.2979 Cdp=0.0363 Cm(c/4)=0.1194 Cs=-0.0674 Ch=0.1150 Main component: Cl=-0.1691 Cdp=0.0158 Cm=0.0901 Flap component: Cl=-0.1288 Cdp=0.0205 Cm=0.1025 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3718 0.6175, -0.04610, -0.2664 0.5841, -0.02440, -0.2617 0.5775, 0.01750, -0.2653 0.5777, 0.04660, -0.2686 0.6274, 0.07170, 0.2137 0.5694, 0.08320, 0.1668 0.5112, 0.09370, -0.0878 0.4731, 0.09830, -0.2328 0.4349, 0.10070, -0.3258 0.3960, 0.10120, -0.4091 0.3566, 0.10020, -0.3667 0.3172, 0.09790, -0.3723 0.2778, 0.09440, -0.4011 0.2393, 0.08960, -0.4179 0.2056, 0.08360, -0.4787 0.1633, 0.07610, -0.3954 0.1261, 0.06710, -0.3974 0.0900, 0.05640, -0.4432 0.0571, 0.04390, -0.2547 0.0283, 0.02940, -0.0769 0.0142, 0.01970, 0.1159 0.0081, 0.01410, 0.2130 0.0026, 0.00780, 0.4352 0.0000, 0.00000, 0.0024 0.0037, -0.00840, 0.8597 0.0112, -0.01420, 0.6348 0.0191, -0.01930, 0.4700 0.0397, -0.03030, 0.2879 0.0706, -0.04420, 0.0607 0.1037, -0.05710, -0.0764 0.1384, -0.06890, -0.2114 0.1741, -0.07950, -0.3664 0.2102, -0.08660, -0.5661 0.2472, -0.09640, -0.6952 0.2844, -0.10270, -0.8292 0.3225, -0.10690, -0.8825 0.3608, -0.10890, -1.0029 0.3991, -0.10830, -1.0077 0.4373, -0.10510, -1.0098 0.4757, -0.09890, -0.8753 0.5137, -0.09070, -0.7712 0.5694, -0.07640, -0.5050 14 Flap element taps 1.0000, 0.00130, -0.2502 0.9365, 0.01390, -0.0222 0.8333, 0.03280, 0.1162 0.7436, 0.04930, 0.2352 0.7049, 0.05670, 0.2593 0.6662, 0.06410, 0.2230 0.6522, 0.01390, -0.2826 0.5969, -0.00020, -0.2633 0.6000, -0.03020, -0.3058 0.6324, -0.04540, -0.3153 0.6667, -0.04880, -0.3027 0.7046, -0.04110, -0.2710 0.7429, -0.03210, -0.2867 0.9311, -0.00120, -0.2793 --------- Run Conditions: vel=100.9 ft/s Re=1.003x10^6 AOA=9.02 Flap deflection=-20.00 Totals: Cl=-0.0379 Cdp=0.0399 Cm(c/4)=0.1177 Cs=-0.0453 Ch=0.1031 Main component: Cl=0.0721 Cdp=0.0330 Cm=0.0374 Flap component: Cl=-0.1100 Cdp=0.0069 Cm=0.0881 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3487 0.6175, -0.04610, -0.2708 0.5841, -0.02440, -0.2670 0.5775, 0.01750, -0.2727 0.5777, 0.04660, -0.2744 0.6274, 0.07170, 0.0976 0.5694, 0.08320, 0.0904 0.5112, 0.09370, -0.1173 0.4731, 0.09830, -0.2800 0.4349, 0.10070, -0.4029 0.3960, 0.10120, -0.5130 0.3566, 0.10020, -0.4883 0.3172, 0.09790, -0.5163 0.2778, 0.09440, -0.5668 0.2393, 0.08960, -0.6122 0.2056, 0.08360, -0.7045 0.1633, 0.07610, -0.6521 0.1261, 0.06710, -0.6974 0.0900, 0.05640, -0.8145 0.0571, 0.04390, -0.7045 0.0283, 0.02940, -0.6607 0.0142, 0.01970, -0.5452 0.0081, 0.01410, -0.6761 0.0026, 0.00780, -0.1603 0.0000, 0.00000, 0.0215 0.0037, -0.00840, 1.0149 0.0112, -0.01420, 0.9427 0.0191, -0.01930, 0.8205 0.0397, -0.03030, 0.6139 0.0706, -0.04420, 0.3643 0.1037, -0.05710, 0.1976 0.1384, -0.06890, 0.0631 0.1741, -0.07950, -0.1103 0.2102, -0.08660, -0.3232 0.2472, -0.09640, -0.4595 0.2844, -0.10270, -0.6047 0.3225, -0.10690, -0.6686 0.3608, -0.10890, -0.8072 0.3991, -0.10830, -0.8346 0.4373, -0.10510, -0.8634 0.4757, -0.09890, -0.7594 0.5137, -0.09070, -0.6859 0.5694, -0.07640, -0.4512 14 Flap element taps 1.0000, 0.00130, -0.2135 0.9365, 0.01390, -0.0118 0.8333, 0.03280, 0.1048 0.7436, 0.04930, 0.1752 0.7049, 0.05670, 0.1499 0.6662, 0.06410, 0.0977 0.6522, 0.01390, -0.2899 0.5969, -0.00020, -0.2682 0.6000, -0.03020, -0.3022 0.6324, -0.04540, -0.3143 0.6667, -0.04880, -0.2817 0.7046, -0.04110, -0.2415 0.7429, -0.03210, -0.2558 0.9311, -0.00120, -0.2557 --------- Run Conditions: vel=101.2 ft/s Re=1.005x10^6 AOA=12.02 Flap deflection=-20.00 Totals: Cl=0.1835 Cdp=0.0526 Cm(c/4)=0.1174 Cs=-0.0133 Ch=0.0959 Main component: Cl=0.2738 Cdp=0.0617 Cm=-0.0050 Flap component: Cl=-0.0903 Cdp=-0.0090 Cm=0.0748 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3505 0.6175, -0.04610, -0.3252 0.5841, -0.02440, -0.3236 0.5775, 0.01750, -0.3282 0.5777, 0.04660, -0.3331 0.6274, 0.07170, -0.0176 0.5694, 0.08320, -0.0095 0.5112, 0.09370, -0.1238 0.4731, 0.09830, -0.2715 0.4349, 0.10070, -0.4224 0.3960, 0.10120, -0.5673 0.3566, 0.10020, -0.5714 0.3172, 0.09790, -0.6253 0.2778, 0.09440, -0.7005 0.2393, 0.08960, -0.7734 0.2056, 0.08360, -0.9014 0.1633, 0.07610, -0.8857 0.1261, 0.06710, -0.9784 0.0900, 0.05640, -1.1645 0.0571, 0.04390, -1.1618 0.0283, 0.02940, -1.2781 0.0142, 0.01970, -1.3519 0.0081, 0.01410, -1.5907 0.0026, 0.00780, -1.0848 0.0000, 0.00000, 0.0466 0.0037, -0.00840, 0.8468 0.0112, -0.01420, 1.0239 0.0191, -0.01930, 0.9936 0.0397, -0.03030, 0.8335 0.0706, -0.04420, 0.5961 0.1037, -0.05710, 0.4196 0.1384, -0.06890, 0.2893 0.1741, -0.07950, 0.1093 0.2102, -0.08660, -0.1142 0.2472, -0.09640, -0.2541 0.2844, -0.10270, -0.4195 0.3225, -0.10690, -0.4956 0.3608, -0.10890, -0.6463 0.3991, -0.10830, -0.7055 0.4373, -0.10510, -0.7500 0.4757, -0.09890, -0.6717 0.5137, -0.09070, -0.6216 0.5694, -0.07640, -0.4062 14 Flap element taps 1.0000, 0.00130, -0.1524 0.9365, 0.01390, 0.0347 0.8333, 0.03280, 0.0994 0.7436, 0.04930, 0.0616 0.7049, 0.05670, 0.0075 0.6662, 0.06410, -0.0299 0.6522, 0.01390, -0.3461 0.5969, -0.00020, -0.3254 0.6000, -0.03020, -0.3525 0.6324, -0.04540, -0.3638 0.6667, -0.04880, -0.2836 0.7046, -0.04110, -0.2117 0.7429, -0.03210, -0.2253 0.9311, -0.00120, -0.2341 --------- Run Conditions: vel=101.5 ft/s Re=1.006x10^6 AOA=15.03 Flap deflection=-20.00 Totals: Cl=0.3569 Cdp=0.0701 Cm(c/4)=0.1067 Cs=0.0249 Ch=0.0591 Main component: Cl=0.4031 Cdp=0.1068 Cm=-0.0275 Flap component: Cl=-0.0462 Cdp=-0.0367 Cm=0.0435 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4333 0.6175, -0.04610, -0.5158 0.5841, -0.02440, -0.5146 0.5775, 0.01750, -0.5187 0.5777, 0.04660, -0.5281 0.6274, 0.07170, -0.1411 0.5694, 0.08320, -0.1184 0.5112, 0.09370, -0.1504 0.4731, 0.09830, -0.1821 0.4349, 0.10070, -0.3056 0.3960, 0.10120, -0.4969 0.3566, 0.10020, -0.5518 0.3172, 0.09790, -0.6455 0.2778, 0.09440, -0.7561 0.2393, 0.08960, -0.8659 0.2056, 0.08360, -1.0317 0.1633, 0.07610, -1.0611 0.1261, 0.06710, -1.2085 0.0900, 0.05640, -1.4516 0.0571, 0.04390, -1.5785 0.0283, 0.02940, -1.8885 0.0142, 0.01970, -2.2007 0.0081, 0.01410, -2.5778 0.0026, 0.00780, -2.1668 0.0000, 0.00000, 0.1682 0.0037, -0.00840, 0.4158 0.0112, -0.01420, 0.9522 0.0191, -0.01930, 1.0250 0.0397, -0.03030, 0.9592 0.0706, -0.04420, 0.7574 0.1037, -0.05710, 0.5849 0.1384, -0.06890, 0.4652 0.1741, -0.07950, 0.2825 0.2102, -0.08660, 0.0566 0.2472, -0.09640, -0.0895 0.2844, -0.10270, -0.2654 0.3225, -0.10690, -0.3632 0.3608, -0.10890, -0.5339 0.3991, -0.10830, -0.6089 0.4373, -0.10510, -0.6849 0.4757, -0.09890, -0.6380 0.5137, -0.09070, -0.6227 0.5694, -0.07640, -0.4442 14 Flap element taps 1.0000, 0.00130, 0.0374 0.9365, 0.01390, 0.1046 0.8333, 0.03280, -0.0085 0.7436, 0.04930, -0.1225 0.7049, 0.05670, -0.1506 0.6662, 0.06410, -0.1568 0.6522, 0.01390, -0.5382 0.5969, -0.00020, -0.5179 0.6000, -0.03020, -0.5415 0.6324, -0.04540, -0.5553 0.6667, -0.04880, -0.4422 0.7046, -0.04110, -0.2161 0.7429, -0.03210, -0.2056 0.9311, -0.00120, -0.0732 --------- Run Conditions: vel=101.2 ft/s Re=1.003x10^6 AOA=18.02 Flap deflection=-20.00 Totals: Cl=0.3792 Cdp=0.1073 Cm(c/4)=0.0786 Cs=0.0152 Ch=-0.0120 Main component: Cl=0.3758 Cdp=0.1567 Cm=-0.0230 Flap component: Cl=0.0034 Cdp=-0.0494 Cm=0.0031 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5857 0.6175, -0.04610, -0.7454 0.5841, -0.02440, -0.7418 0.5775, 0.01750, -0.7458 0.5777, 0.04660, -0.7531 0.6274, 0.07170, -0.3059 0.5694, 0.08320, -0.2907 0.5112, 0.09370, -0.3163 0.4731, 0.09830, -0.2961 0.4349, 0.10070, -0.3001 0.3960, 0.10120, -0.3669 0.3566, 0.10020, -0.3246 0.3172, 0.09790, -0.3716 0.2778, 0.09440, -0.4565 0.2393, 0.08960, -0.5830 0.2056, 0.08360, -0.8097 0.1633, 0.07610, -0.9102 0.1261, 0.06710, -1.1323 0.0900, 0.05640, -1.4138 0.0571, 0.04390, -1.6671 0.0283, 0.02940, -2.1211 0.0142, 0.01970, -2.5879 0.0081, 0.01410, -3.0747 0.0026, 0.00780, -2.8005 0.0000, 0.00000, 0.2658 0.0037, -0.00840, 0.0762 0.0112, -0.01420, 0.8480 0.0191, -0.01930, 1.0021 0.0397, -0.03030, 1.0038 0.0706, -0.04420, 0.8326 0.1037, -0.05710, 0.6687 0.1384, -0.06890, 0.5557 0.1741, -0.07950, 0.3719 0.2102, -0.08660, 0.1398 0.2472, -0.09640, -0.0105 0.2844, -0.10270, -0.1980 0.3225, -0.10690, -0.3054 0.3608, -0.10890, -0.4957 0.3991, -0.10830, -0.5890 0.4373, -0.10510, -0.6898 0.4757, -0.09890, -0.6651 0.5137, -0.09070, -0.6816 0.5694, -0.07640, -0.5417 14 Flap element taps 1.0000, 0.00130, -0.0367 0.9365, 0.01390, -0.0993 0.8333, 0.03280, -0.2629 0.7436, 0.04930, -0.3250 0.7049, 0.05670, -0.3380 0.6662, 0.06410, -0.3301 0.6522, 0.01390, -0.7643 0.5969, -0.00020, -0.7415 0.6000, -0.03020, -0.7807 0.6324, -0.04540, -0.7988 0.6667, -0.04880, -0.8648 0.7046, -0.04110, -0.4600 0.7429, -0.03210, -0.3136 0.9311, -0.00120, 0.0613 --------- Run Conditions: vel=101.1 ft/s Re=1.002x10^6 AOA=19.98 Flap deflection=-20.00 Totals: Cl=0.3594 Cdp=0.1552 Cm(c/4)=0.0566 Cs=-0.0230 Ch=-0.0356 Main component: Cl=0.3391 Cdp=0.2033 Cm=-0.0306 Flap component: Cl=0.0203 Cdp=-0.0481 Cm=-0.0104 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6766 0.6175, -0.04610, -0.8640 0.5841, -0.02440, -0.8626 0.5775, 0.01750, -0.8649 0.5777, 0.04660, -0.8717 0.6274, 0.07170, -0.4536 0.5694, 0.08320, -0.4387 0.5112, 0.09370, -0.4686 0.4731, 0.09830, -0.4616 0.4349, 0.10070, -0.4646 0.3960, 0.10120, -0.5212 0.3566, 0.10020, -0.4555 0.3172, 0.09790, -0.4596 0.2778, 0.09440, -0.4784 0.2393, 0.08960, -0.5101 0.2056, 0.08360, -0.6413 0.1633, 0.07610, -0.6721 0.1261, 0.06710, -0.8759 0.0900, 0.05640, -1.1086 0.0571, 0.04390, -1.4140 0.0283, 0.02940, -1.9118 0.0142, 0.01970, -2.4196 0.0081, 0.01410, -2.9368 0.0026, 0.00780, -2.7316 0.0000, 0.00000, 0.3696 0.0037, -0.00840, 0.0474 0.0112, -0.01420, 0.8312 0.0191, -0.01930, 0.9957 0.0397, -0.03030, 1.0079 0.0706, -0.04420, 0.8462 0.1037, -0.05710, 0.6856 0.1384, -0.06890, 0.5739 0.1741, -0.07950, 0.3895 0.2102, -0.08660, 0.1525 0.2472, -0.09640, -0.0020 0.2844, -0.10270, -0.1963 0.3225, -0.10690, -0.3120 0.3608, -0.10890, -0.5115 0.3991, -0.10830, -0.6151 0.4373, -0.10510, -0.7285 0.4757, -0.09890, -0.7122 0.5137, -0.09070, -0.7412 0.5694, -0.07640, -0.6136 14 Flap element taps 1.0000, 0.00130, -0.2087 0.9365, 0.01390, -0.2909 0.8333, 0.03280, -0.4190 0.7436, 0.04930, -0.4688 0.7049, 0.05670, -0.4758 0.6662, 0.06410, -0.4739 0.6522, 0.01390, -0.8827 0.5969, -0.00020, -0.8671 0.6000, -0.03020, -0.9064 0.6324, -0.04540, -0.9301 0.6667, -0.04880, -1.0551 0.7046, -0.04110, -0.6165 0.7429, -0.03210, -0.4125 0.9311, -0.00120, -0.0205 --------- Run Conditions: vel=100.5 ft/s Re=0.995x10^6 AOA=23.99 Flap deflection=-20.00 Totals: Cl=0.2954 Cdp=0.2401 Cm(c/4)=0.0340 Cs=-0.0993 Ch=-0.0460 Main component: Cl=0.2716 Cdp=0.2831 Cm=-0.0449 Flap component: Cl=0.0237 Cdp=-0.0431 Cm=-0.0130 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7686 0.6175, -0.04610, -0.9939 0.5841, -0.02440, -0.9848 0.5775, 0.01750, -0.9892 0.5777, 0.04660, -0.9965 0.6274, 0.07170, -0.5528 0.5694, 0.08320, -0.5652 0.5112, 0.09370, -0.6016 0.4731, 0.09830, -0.5860 0.4349, 0.10070, -0.5930 0.3960, 0.10120, -0.6540 0.3566, 0.10020, -0.5952 0.3172, 0.09790, -0.5905 0.2778, 0.09440, -0.5935 0.2393, 0.08960, -0.5880 0.2056, 0.08360, -0.6585 0.1633, 0.07610, -0.6101 0.1261, 0.06710, -0.6892 0.0900, 0.05640, -0.7008 0.0571, 0.04390, -0.7916 0.0283, 0.02940, -0.9909 0.0142, 0.01970, -1.3658 0.0081, 0.01410, -1.8276 0.0026, 0.00780, -1.7823 0.0000, 0.00000, 0.4546 0.0037, -0.00840, 0.1584 0.0112, -0.01420, 0.8352 0.0191, -0.01930, 0.9895 0.0397, -0.03030, 1.0166 0.0706, -0.04420, 0.8752 0.1037, -0.05710, 0.7274 0.1384, -0.06890, 0.6270 0.1741, -0.07950, 0.4471 0.2102, -0.08660, 0.2117 0.2472, -0.09640, 0.0566 0.2844, -0.10270, -0.1453 0.3225, -0.10690, -0.2703 0.3608, -0.10890, -0.4815 0.3991, -0.10830, -0.5993 0.4373, -0.10510, -0.7327 0.4757, -0.09890, -0.7316 0.5137, -0.09070, -0.7811 0.5694, -0.07640, -0.6765 14 Flap element taps 1.0000, 0.00130, -0.4160 0.9365, 0.01390, -0.4915 0.8333, 0.03280, -0.5825 0.7436, 0.04930, -0.5882 0.7049, 0.05670, -0.5842 0.6662, 0.06410, -0.5667 0.6522, 0.01390, -1.0077 0.5969, -0.00020, -0.9955 0.6000, -0.03020, -1.0393 0.6324, -0.04540, -1.0698 0.6667, -0.04880, -1.2563 0.7046, -0.04110, -0.7808 0.7429, -0.03210, -0.5436 0.9311, -0.00120, -0.1615 --------- Run Conditions: vel=100.6 ft/s Re=0.997x10^6 AOA=26.97 Flap deflection=-20.00 Totals: Cl=0.4194 Cdp=0.3164 Cm(c/4)=0.0227 Cs=-0.0918 Ch=-0.0536 Main component: Cl=0.3849 Cdp=0.3555 Cm=-0.0866 Flap component: Cl=0.0345 Cdp=-0.0391 Cm=-0.0200 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7430 0.6175, -0.04610, -0.9869 0.5841, -0.02440, -0.9826 0.5775, 0.01750, -0.9865 0.5777, 0.04660, -0.9945 0.6274, 0.07170, -0.6497 0.5694, 0.08320, -0.6395 0.5112, 0.09370, -0.6994 0.4731, 0.09830, -0.7074 0.4349, 0.10070, -0.7254 0.3960, 0.10120, -0.7949 0.3566, 0.10020, -0.7576 0.3172, 0.09790, -0.7749 0.2778, 0.09440, -0.8025 0.2393, 0.08960, -0.8074 0.2056, 0.08360, -0.8860 0.1633, 0.07610, -0.8504 0.1261, 0.06710, -0.9353 0.0900, 0.05640, -0.9448 0.0571, 0.04390, -1.0453 0.0283, 0.02940, -1.1073 0.0142, 0.01970, -1.2979 0.0081, 0.01410, -1.5486 0.0026, 0.00780, -1.3975 0.0000, 0.00000, 0.4953 0.0037, -0.00840, 0.0406 0.0112, -0.01420, 0.7584 0.0191, -0.01930, 0.9492 0.0397, -0.03030, 1.0264 0.0706, -0.04420, 0.9239 0.1037, -0.05710, 0.7964 0.1384, -0.06890, 0.7098 0.1741, -0.07950, 0.5395 0.2102, -0.08660, 0.3148 0.2472, -0.09640, 0.1646 0.2844, -0.10270, -0.0335 0.3225, -0.10690, -0.1624 0.3608, -0.10890, -0.3743 0.3991, -0.10830, -0.5014 0.4373, -0.10510, -0.6432 0.4757, -0.09890, -0.6567 0.5137, -0.09070, -0.7191 0.5694, -0.07640, -0.6361 14 Flap element taps 1.0000, 0.00130, -0.4643 0.9365, 0.01390, -0.5304 0.8333, 0.03280, -0.5997 0.7436, 0.04930, -0.6176 0.7049, 0.05670, -0.6261 0.6662, 0.06410, -0.6217 0.6522, 0.01390, -0.9996 0.5969, -0.00020, -0.9889 0.6000, -0.03020, -1.0305 0.6324, -0.04540, -1.0571 0.6667, -0.04880, -1.2502 0.7046, -0.04110, -0.7794 0.7429, -0.03210, -0.5383 0.9311, -0.00120, -0.1768