S809 UNVENTED AILERON, LEGR, CHORD = 18 IN --------- Run Conditions: vel=104.7 ft/s Re=0.997x10^6 AOA=-6.01 Flap deflection=-45.00 Totals: Cl=-1.3728 Cdp=0.2158 Cm(c/4)=0.1254 Cs=-0.0709 Ch=0.2305 Main component: Cl=-1.1999 Cdp=0.0340 Cm=0.3015 Flap component: Cl=-0.1730 Cdp=0.1818 Cm=0.1709 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4928 0.6175, -0.04610, -0.4365 0.5841, -0.02440, -0.5066 0.5775, 0.01750, -0.4984 0.5777, 0.04660, -0.5023 0.6274, 0.07170, 0.5695 0.5694, 0.08320, 0.5026 0.5112, 0.09370, 0.4519 0.4731, 0.09830, 0.2704 0.4349, 0.10070, 0.2948 0.3960, 0.10120, 0.4425 0.3566, 0.10020, 0.4407 0.3172, 0.09790, 0.4590 0.2778, 0.09440, 0.4742 0.2393, 0.08960, 0.5063 0.2056, 0.08360, 0.5350 0.1633, 0.07610, 0.6248 0.1261, 0.06710, 0.7106 0.0900, 0.05640, 0.8173 0.0571, 0.04390, 0.9511 0.0283, 0.02940, 1.0048 0.0142, 0.01970, 0.8110 0.0081, 0.01410, 0.4386 0.0026, 0.00780, -0.5712 0.0000, 0.00000, -0.2149 0.0037, -0.00840, -4.9300 0.0112, -0.01420, -3.3757 0.0191, -0.01930, -2.8462 0.0397, -0.03030, -2.1164 0.0706, -0.04420, -1.8238 0.1037, -0.05710, -1.6416 0.1384, -0.06890, -1.6191 0.1741, -0.07950, -1.6067 0.2102, -0.08660, -1.6554 0.2472, -0.09640, -1.6896 0.2844, -0.10270, -1.6757 0.3225, -0.10690, -1.6213 0.3608, -0.10890, -1.5523 0.3991, -0.10830, -1.3725 0.4373, -0.10510, -1.1548 0.4757, -0.09890, -0.8713 0.5137, -0.09070, -0.5841 0.5694, -0.07640, -0.4900 15 Flap element taps 1.0000, 0.00130, -0.3933 0.9365, 0.01390, 0.1137 0.8333, 0.03280, 0.3472 0.7436, 0.04930, 0.4902 0.7049, 0.05670, 0.5572 0.6662, 0.06410, 0.5052 0.6522, 0.01390, -0.4349 0.5969, -0.00020, -0.3648 0.6000, -0.03020, -0.4712 0.6324, -0.04540, -0.4398 0.6667, -0.04880, -0.4629 0.7046, -0.04110, -0.4117 0.7429, -0.03210, -0.4423 0.8333, -0.01400, -0.4407 0.9311, -0.00120, -0.4675 --------- Run Conditions: vel=105.3 ft/s Re=1.002x10^6 AOA=0.03 Flap deflection=-45.00 Totals: Cl=-1.3996 Cdp=0.2296 Cm(c/4)=0.2258 Cs=-0.2303 Ch=0.3178 Main component: Cl=-1.1342 Cdp=0.0055 Cm=0.3388 Flap component: Cl=-0.2654 Cdp=0.2241 Cm=0.2368 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7039 0.6175, -0.04610, -0.5842 0.5841, -0.02440, -0.5823 0.5775, 0.01750, -0.5932 0.5777, 0.04660, -0.5903 0.6274, 0.07170, 0.6499 0.5694, 0.08320, 0.6604 0.5112, 0.09370, 0.5407 0.4731, 0.09830, 0.4265 0.4349, 0.10070, 0.3508 0.3960, 0.10120, 0.2750 0.3566, 0.10020, 0.2917 0.3172, 0.09790, 0.2969 0.2778, 0.09440, 0.3009 0.2393, 0.08960, 0.3136 0.2056, 0.08360, 0.3035 0.1633, 0.07610, 0.4087 0.1261, 0.06710, 0.4693 0.0900, 0.05640, 0.5648 0.0571, 0.04390, 0.7454 0.0283, 0.02940, 0.9418 0.0142, 0.01970, 1.0099 0.0081, 0.01410, 0.9066 0.0026, 0.00780, 0.4232 0.0000, 0.00000, -0.2297 0.0037, -0.00840, -2.3699 0.0112, -0.01420, -1.7304 0.0191, -0.01930, -1.5468 0.0397, -0.03030, -1.2435 0.0706, -0.04420, -1.2037 0.1037, -0.05710, -1.1628 0.1384, -0.06890, -1.2434 0.1741, -0.07950, -1.3214 0.2102, -0.08660, -1.4748 0.2472, -0.09640, -1.5859 0.2844, -0.10270, -1.6719 0.3225, -0.10690, -1.7026 0.3608, -0.10890, -1.7619 0.3991, -0.10830, -1.7046 0.4373, -0.10510, -1.6445 0.4757, -0.09890, -1.4111 0.5137, -0.09070, -1.2525 0.5694, -0.07640, -0.8980 15 Flap element taps 1.0000, 0.00130, -0.6191 0.9365, 0.01390, 0.1330 0.8333, 0.03280, 0.4762 0.7436, 0.04930, 0.7191 0.7049, 0.05670, 0.7676 0.6662, 0.06410, 0.6633 0.6522, 0.01390, -0.5959 0.5969, -0.00020, -0.6050 0.6000, -0.03020, -0.6365 0.6324, -0.04540, -0.6289 0.6667, -0.04880, -0.6337 0.7046, -0.04110, -0.6178 0.7429, -0.03210, -0.6331 0.8333, -0.01400, -0.6365 0.9311, -0.00120, -0.6145 --------- Run Conditions: vel=106.3 ft/s Re=1.010x10^6 AOA=3.03 Flap deflection=-45.00 Totals: Cl=-1.2631 Cdp=0.1909 Cm(c/4)=0.2324 Cs=-0.2574 Ch=0.3146 Main component: Cl=-0.9932 Cdp=-0.0121 Cm=0.3135 Flap component: Cl=-0.2700 Cdp=0.2030 Cm=0.2317 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7161 0.6175, -0.04610, -0.5865 0.5841, -0.02440, -0.5883 0.5775, 0.01750, -0.5987 0.5777, 0.04660, -0.5984 0.6274, 0.07170, 0.5818 0.5694, 0.08320, 0.6081 0.5112, 0.09370, 0.5477 0.4731, 0.09830, 0.4297 0.4349, 0.10070, 0.3289 0.3960, 0.10120, 0.2247 0.3566, 0.10020, 0.2422 0.3172, 0.09790, 0.2363 0.2778, 0.09440, 0.2311 0.2393, 0.08960, 0.2266 0.2056, 0.08360, 0.1864 0.1633, 0.07610, 0.2972 0.1261, 0.06710, 0.3337 0.0900, 0.05640, 0.4098 0.0571, 0.04390, 0.5937 0.0283, 0.02940, 0.8184 0.0142, 0.01970, 0.9767 0.0081, 0.01410, 0.9488 0.0026, 0.00780, 0.7355 0.0000, 0.00000, -0.2101 0.0037, -0.00840, -1.2584 0.0112, -0.01420, -0.9251 0.0191, -0.01930, -0.9610 0.0397, -0.03030, -0.8154 0.0706, -0.04420, -0.8720 0.1037, -0.05710, -0.8887 0.1384, -0.06890, -0.9947 0.1741, -0.07950, -1.1005 0.2102, -0.08660, -1.2905 0.2472, -0.09640, -1.4141 0.2844, -0.10270, -1.5279 0.3225, -0.10690, -1.5734 0.3608, -0.10890, -1.6586 0.3991, -0.10830, -1.6201 0.4373, -0.10510, -1.5975 0.4757, -0.09890, -1.3845 0.5137, -0.09070, -1.2597 0.5694, -0.07640, -0.9101 15 Flap element taps 1.0000, 0.00130, -0.6191 0.9365, 0.01390, 0.1275 0.8333, 0.03280, 0.4804 0.7436, 0.04930, 0.6664 0.7049, 0.05670, 0.6222 0.6662, 0.06410, 0.5702 0.6522, 0.01390, -0.6078 0.5969, -0.00020, -0.6087 0.6000, -0.03020, -0.6391 0.6324, -0.04540, -0.6381 0.6667, -0.04880, -0.6446 0.7046, -0.04110, -0.6195 0.7429, -0.03210, -0.6398 0.8333, -0.01400, -0.6494 0.9311, -0.00120, -0.6137 --------- Run Conditions: vel=106.3 ft/s Re=1.009x10^6 AOA=6.05 Flap deflection=-45.00 Totals: Cl=-1.0346 Cdp=0.1672 Cm(c/4)=0.2329 Cs=-0.2753 Ch=0.3013 Main component: Cl=-0.7699 Cdp=-0.0101 Cm=0.2661 Flap component: Cl=-0.2647 Cdp=0.1773 Cm=0.2195 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6997 0.6175, -0.04610, -0.5738 0.5841, -0.02440, -0.5783 0.5775, 0.01750, -0.5914 0.5777, 0.04660, -0.5950 0.6274, 0.07170, 0.5000 0.5694, 0.08320, 0.5326 0.5112, 0.09370, 0.5004 0.4731, 0.09830, 0.4133 0.4349, 0.10070, 0.2903 0.3960, 0.10120, 0.1501 0.3566, 0.10020, 0.1526 0.3172, 0.09790, 0.1308 0.2778, 0.09440, 0.1123 0.2393, 0.08960, 0.0874 0.2056, 0.08360, 0.0191 0.1633, 0.07610, 0.1168 0.1261, 0.06710, 0.1255 0.0900, 0.05640, 0.1570 0.0571, 0.04390, 0.3301 0.0283, 0.02940, 0.5538 0.0142, 0.01970, 0.7673 0.0081, 0.01410, 0.8346 0.0026, 0.00780, 0.9814 0.0000, 0.00000, -0.1711 0.0037, -0.00840, -0.0333 0.0112, -0.01420, -0.1535 0.0191, -0.01930, -0.2569 0.0397, -0.03030, -0.2955 0.0706, -0.04420, -0.4465 0.1037, -0.05710, -0.5261 0.1384, -0.06890, -0.6555 0.1741, -0.07950, -0.7930 0.2102, -0.08660, -1.0131 0.2472, -0.09640, -1.1483 0.2844, -0.10270, -1.2888 0.3225, -0.10690, -1.3503 0.3608, -0.10890, -1.4636 0.3991, -0.10830, -1.4468 0.4373, -0.10510, -1.4635 0.4757, -0.09890, -1.2815 0.5137, -0.09070, -1.1976 0.5694, -0.07640, -0.8723 15 Flap element taps 1.0000, 0.00130, -0.6105 0.9365, 0.01390, 0.1161 0.8333, 0.03280, 0.4698 0.7436, 0.04930, 0.5544 0.7049, 0.05670, 0.5041 0.6662, 0.06410, 0.4853 0.6522, 0.01390, -0.5989 0.5969, -0.00020, -0.5977 0.6000, -0.03020, -0.6292 0.6324, -0.04540, -0.6279 0.6667, -0.04880, -0.6354 0.7046, -0.04110, -0.6066 0.7429, -0.03210, -0.6288 0.8333, -0.01400, -0.6436 0.9311, -0.00120, -0.5991 --------- Run Conditions: vel=105.9 ft/s Re=1.005x10^6 AOA=9.03 Flap deflection=-45.00 Totals: Cl=-0.7757 Cdp=0.1471 Cm(c/4)=0.2269 Cs=-0.2670 Ch=0.2797 Main component: Cl=-0.5249 Cdp=-0.0017 Cm=0.2108 Flap component: Cl=-0.2508 Cdp=0.1488 Cm=0.2019 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6544 0.6175, -0.04610, -0.5488 0.5841, -0.02440, -0.5506 0.5775, 0.01750, -0.5644 0.5777, 0.04660, -0.5695 0.6274, 0.07170, 0.4091 0.5694, 0.08320, 0.4463 0.5112, 0.09370, 0.4221 0.4731, 0.09830, 0.3731 0.4349, 0.10070, 0.2548 0.3960, 0.10120, 0.0804 0.3566, 0.10020, 0.0610 0.3172, 0.09790, 0.0219 0.2778, 0.09440, -0.0152 0.2393, 0.08960, -0.0638 0.2056, 0.08360, -0.1609 0.1633, 0.07610, -0.0841 0.1261, 0.06710, -0.1100 0.0900, 0.05640, -0.1425 0.0571, 0.04390, -0.0063 0.0283, 0.02940, 0.1603 0.0142, 0.01970, 0.3527 0.0081, 0.01410, 0.4493 0.0026, 0.00780, 0.6578 0.0000, 0.00000, -0.1511 0.0037, -0.00840, 0.7244 0.0112, -0.01420, 0.4838 0.0191, -0.01930, 0.3130 0.0397, -0.03030, 0.1543 0.0706, -0.04420, -0.0538 0.1037, -0.05710, -0.1920 0.1384, -0.06890, -0.3276 0.1741, -0.07950, -0.4826 0.2102, -0.08660, -0.7248 0.2472, -0.09640, -0.8665 0.2844, -0.10270, -1.0252 0.3225, -0.10690, -1.1012 0.3608, -0.10890, -1.2337 0.3991, -0.10830, -1.2392 0.4373, -0.10510, -1.2896 0.4757, -0.09890, -1.1366 0.5137, -0.09070, -1.0907 0.5694, -0.07640, -0.7986 15 Flap element taps 1.0000, 0.00130, -0.5769 0.9365, 0.01390, 0.1080 0.8333, 0.03280, 0.4388 0.7436, 0.04930, 0.4402 0.7049, 0.05670, 0.4065 0.6662, 0.06410, 0.3935 0.6522, 0.01390, -0.5718 0.5969, -0.00020, -0.5684 0.6000, -0.03020, -0.5975 0.6324, -0.04540, -0.5989 0.6667, -0.04880, -0.6051 0.7046, -0.04110, -0.5719 0.7429, -0.03210, -0.5996 0.8333, -0.01400, -0.6165 0.9311, -0.00120, -0.5633 --------- Run Conditions: vel=106.2 ft/s Re=1.008x10^6 AOA=12.04 Flap deflection=-45.00 Totals: Cl=-0.5200 Cdp=0.1394 Cm(c/4)=0.2220 Cs=-0.2448 Ch=0.2628 Main component: Cl=-0.2818 Cdp=0.0165 Cm=0.1548 Flap component: Cl=-0.2382 Cdp=0.1229 Cm=0.1871 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6147 0.6175, -0.04610, -0.5367 0.5841, -0.02440, -0.5365 0.5775, 0.01750, -0.5508 0.5777, 0.04660, -0.5576 0.6274, 0.07170, 0.2985 0.5694, 0.08320, 0.3384 0.5112, 0.09370, 0.3170 0.4731, 0.09830, 0.2940 0.4349, 0.10070, 0.2177 0.3960, 0.10120, 0.0275 0.3566, 0.10020, -0.0191 0.3172, 0.09790, -0.0837 0.2778, 0.09440, -0.1449 0.2393, 0.08960, -0.2226 0.2056, 0.08360, -0.3518 0.1633, 0.07610, -0.3044 0.1261, 0.06710, -0.3738 0.0900, 0.05640, -0.4757 0.0571, 0.04390, -0.4088 0.0283, 0.02940, -0.3633 0.0142, 0.01970, -0.2269 0.0081, 0.01410, -0.3022 0.0026, 0.00780, 0.0757 0.0000, 0.00000, -0.1254 0.0037, -0.00840, 1.0036 0.0112, -0.01420, 0.8734 0.0191, -0.01930, 0.7185 0.0397, -0.03030, 0.5161 0.0706, -0.04420, 0.2783 0.1037, -0.05710, 0.1083 0.1384, -0.06890, -0.0325 0.1741, -0.07950, -0.2013 0.2102, -0.08660, -0.4589 0.2472, -0.09640, -0.6049 0.2844, -0.10270, -0.7753 0.3225, -0.10690, -0.8637 0.3608, -0.10890, -1.0098 0.3991, -0.10830, -1.0382 0.4373, -0.10510, -1.1192 0.4757, -0.09890, -0.9971 0.5137, -0.09070, -0.9833 0.5694, -0.07640, -0.7271 15 Flap element taps 1.0000, 0.00130, -0.5507 0.9365, 0.01390, 0.1121 0.8333, 0.03280, 0.4060 0.7436, 0.04930, 0.3296 0.7049, 0.05670, 0.2993 0.6662, 0.06410, 0.2846 0.6522, 0.01390, -0.5579 0.5969, -0.00020, -0.5544 0.6000, -0.03020, -0.5804 0.6324, -0.04540, -0.5811 0.6667, -0.04880, -0.5878 0.7046, -0.04110, -0.5514 0.7429, -0.03210, -0.5782 0.8333, -0.01400, -0.5985 0.9311, -0.00120, -0.5382 --------- Run Conditions: vel=106.0 ft/s Re=1.003x10^6 AOA=15.04 Flap deflection=-45.00 Totals: Cl=-0.2507 Cdp=0.1377 Cm(c/4)=0.2039 Cs=-0.1981 Ch=0.2285 Main component: Cl=-0.0434 Cdp=0.0430 Cm=0.0960 Flap component: Cl=-0.2073 Cdp=0.0947 Cm=0.1596 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5470 0.6175, -0.04610, -0.5258 0.5841, -0.02440, -0.5042 0.5775, 0.01750, -0.5258 0.5777, 0.04660, -0.5243 0.6274, 0.07170, 0.1652 0.5694, 0.08320, 0.1705 0.5112, 0.09370, 0.1707 0.4731, 0.09830, 0.1730 0.4349, 0.10070, 0.1560 0.3960, 0.10120, 0.0905 0.3566, 0.10020, -0.0351 0.3172, 0.09790, -0.1475 0.2778, 0.09440, -0.2663 0.2393, 0.08960, -0.3607 0.2056, 0.08360, -0.4577 0.1633, 0.07610, -0.5492 0.1261, 0.06710, -0.6237 0.0900, 0.05640, -0.8316 0.0571, 0.04390, -0.8479 0.0283, 0.02940, -0.9781 0.0142, 0.01970, -1.0373 0.0081, 0.01410, -1.1563 0.0026, 0.00780, -0.7956 0.0000, 0.00000, -0.0961 0.0037, -0.00840, 0.9065 0.0112, -0.01420, 1.0041 0.0191, -0.01930, 0.9612 0.0397, -0.03030, 0.7878 0.0706, -0.04420, 0.5642 0.1037, -0.05710, 0.3989 0.1384, -0.06890, 0.1866 0.1741, -0.07950, 0.0152 0.2102, -0.08660, -0.1604 0.2472, -0.09640, -0.3622 0.2844, -0.10270, -0.5153 0.3225, -0.10690, -0.6565 0.3608, -0.10890, -0.8011 0.3991, -0.10830, -0.8991 0.4373, -0.10510, -0.9258 0.4757, -0.09890, -0.8500 0.5137, -0.09070, -0.7375 0.5694, -0.07640, -0.6281 15 Flap element taps 1.0000, 0.00130, -0.5207 0.9365, 0.01390, 0.1215 0.8333, 0.03280, 0.3240 0.7436, 0.04930, 0.1797 0.7049, 0.05670, 0.1625 0.6662, 0.06410, 0.1682 0.6522, 0.01390, -0.5102 0.5969, -0.00020, -0.4047 0.6000, -0.03020, -0.5378 0.6324, -0.04540, -0.5261 0.6667, -0.04880, -0.5061 0.7046, -0.04110, -0.5197 0.7429, -0.03210, -0.5057 0.8333, -0.01400, -0.5329 0.9311, -0.00120, -0.5068 --------- Run Conditions: vel=105.3 ft/s Re=0.996x10^6 AOA=18.01 Flap deflection=-45.00 Totals: Cl=0.0755 Cdp=0.1365 Cm(c/4)=0.1609 Cs=-0.1065 Ch=0.1603 Main component: Cl=0.2078 Cdp=0.0972 Cm=0.0281 Flap component: Cl=-0.1322 Cdp=0.0393 Cm=0.1043 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5096 0.6175, -0.04610, -0.5486 0.5841, -0.02440, -0.5387 0.5775, 0.01750, -0.5508 0.5777, 0.04660, -0.5497 0.6274, 0.07170, -0.0871 0.5694, 0.08320, -0.0978 0.5112, 0.09370, -0.0887 0.4731, 0.09830, -0.0858 0.4349, 0.10070, -0.0841 0.3960, 0.10120, -0.0821 0.3566, 0.10020, -0.1094 0.3172, 0.09790, -0.1537 0.2778, 0.09440, -0.2628 0.2393, 0.08960, -0.4064 0.2056, 0.08360, -0.5743 0.1633, 0.07610, -0.7380 0.1261, 0.06710, -0.8892 0.0900, 0.05640, -1.1767 0.0571, 0.04390, -1.3553 0.0283, 0.02940, -1.7292 0.0142, 0.01970, -2.0729 0.0081, 0.01410, -2.3930 0.0026, 0.00780, -2.0906 0.0000, 0.00000, -0.0969 0.0037, -0.00840, 0.3730 0.0112, -0.01420, 0.9203 0.0191, -0.01930, 1.0106 0.0397, -0.03030, 0.9597 0.0706, -0.04420, 0.7849 0.1037, -0.05710, 0.6327 0.1384, -0.06890, 0.4386 0.1741, -0.07950, 0.2683 0.2102, -0.08660, 0.1019 0.2472, -0.09640, -0.0996 0.2844, -0.10270, -0.2573 0.3225, -0.10690, -0.4152 0.3608, -0.10890, -0.5712 0.3991, -0.10830, -0.6817 0.4373, -0.10510, -0.7364 0.4757, -0.09890, -0.6975 0.5137, -0.09070, -0.6845 0.5694, -0.07640, -0.5654 15 Flap element taps 1.0000, 0.00130, -0.4471 0.9365, 0.01390, 0.0946 0.8333, 0.03280, 0.0576 0.7436, 0.04930, -0.0964 0.7049, 0.05670, -0.1010 0.6662, 0.06410, -0.0843 0.6522, 0.01390, -0.5323 0.5969, -0.00020, -0.5567 0.6000, -0.03020, -0.5677 0.6324, -0.04540, -0.4873 0.6667, -0.04880, -0.4217 0.7046, -0.04110, -0.4280 0.7429, -0.03210, -0.4319 0.8333, -0.01400, -0.4519 0.9311, -0.00120, -0.4574 --------- Run Conditions: vel=105.2 ft/s Re=0.996x10^6 AOA=20.01 Flap deflection=-45.00 Totals: Cl=0.3146 Cdp=0.1749 Cm(c/4)=0.0807 Cs=-0.0566 Ch=0.0591 Main component: Cl=0.3483 Cdp=0.1931 Cm=-0.0420 Flap component: Cl=-0.0337 Cdp=-0.0182 Cm=0.0339 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5636 0.6175, -0.04610, -0.6981 0.5841, -0.02440, -0.6969 0.5775, 0.01750, -0.7134 0.5777, 0.04660, -0.7124 0.6274, 0.07170, -0.4365 0.5694, 0.08320, -0.4971 0.5112, 0.09370, -0.4964 0.4731, 0.09830, -0.4823 0.4349, 0.10070, -0.4807 0.3960, 0.10120, -0.4759 0.3566, 0.10020, -0.4993 0.3172, 0.09790, -0.5084 0.2778, 0.09440, -0.5279 0.2393, 0.08960, -0.5342 0.2056, 0.08360, -0.5550 0.1633, 0.07610, -0.6197 0.1261, 0.06710, -0.7023 0.0900, 0.05640, -0.8651 0.0571, 0.04390, -1.1771 0.0283, 0.02940, -1.7694 0.0142, 0.01970, -2.3412 0.0081, 0.01410, -2.7842 0.0026, 0.00780, -2.6943 0.0000, 0.00000, -0.0782 0.0037, -0.00840, -0.0257 0.0112, -0.01420, 0.7842 0.0191, -0.01930, 0.9679 0.0397, -0.03030, 1.0015 0.0706, -0.04420, 0.8730 0.1037, -0.05710, 0.7363 0.1384, -0.06890, 0.5572 0.1741, -0.07950, 0.3949 0.2102, -0.08660, 0.2327 0.2472, -0.09640, 0.0379 0.2844, -0.10270, -0.1237 0.3225, -0.10690, -0.2854 0.3608, -0.10890, -0.4518 0.3991, -0.10830, -0.5742 0.4373, -0.10510, -0.6471 0.4757, -0.09890, -0.6318 0.5137, -0.09070, -0.6387 0.5694, -0.07640, -0.5455 15 Flap element taps 1.0000, 0.00130, -0.4169 0.9365, 0.01390, -0.1147 0.8333, 0.03280, -0.3047 0.7436, 0.04930, -0.4578 0.7049, 0.05670, -0.4651 0.6662, 0.06410, -0.4259 0.6522, 0.01390, -0.6939 0.5969, -0.00020, -0.7238 0.6000, -0.03020, -0.7402 0.6324, -0.04540, -0.5757 0.6667, -0.04880, -0.4155 0.7046, -0.04110, -0.4209 0.7429, -0.03210, -0.3979 0.8333, -0.01400, -0.4323 0.9311, -0.00120, -0.3903 --------- Run Conditions: vel=106.9 ft/s Re=1.012x10^6 AOA=23.99 Flap deflection=-45.00 Totals: Cl=0.4833 Cdp=0.2623 Cm(c/4)=0.0221 Cs=-0.0431 Ch=-0.0292 Main component: Cl=0.4363 Cdp=0.3268 Cm=-0.0949 Flap component: Cl=0.0471 Cdp=-0.0645 Cm=-0.0201 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7092 0.6175, -0.04610, -0.9894 0.5841, -0.02440, -0.9786 0.5775, 0.01750, -0.9886 0.5777, 0.04660, -0.9871 0.6274, 0.07170, -0.6463 0.5694, 0.08320, -0.7067 0.5112, 0.09370, -0.7589 0.4731, 0.09830, -0.7745 0.4349, 0.10070, -0.7585 0.3960, 0.10120, -0.7494 0.3566, 0.10020, -0.7709 0.3172, 0.09790, -0.7895 0.2778, 0.09440, -0.8170 0.2393, 0.08960, -0.8527 0.2056, 0.08360, -0.8983 0.1633, 0.07610, -0.9282 0.1261, 0.06710, -0.9523 0.0900, 0.05640, -0.9896 0.0571, 0.04390, -1.0619 0.0283, 0.02940, -1.2582 0.0142, 0.01970, -1.6070 0.0081, 0.01410, -1.9721 0.0026, 0.00780, -2.0668 0.0000, 0.00000, -0.0332 0.0037, -0.00840, -0.1283 0.0112, -0.01420, 0.7083 0.0191, -0.01930, 0.9277 0.0397, -0.03030, 1.0119 0.0706, -0.04420, 0.9217 0.1037, -0.05710, 0.8078 0.1384, -0.06890, 0.6468 0.1741, -0.07950, 0.4945 0.2102, -0.08660, 0.3295 0.2472, -0.09640, 0.1361 0.2844, -0.10270, -0.0311 0.3225, -0.10690, -0.2007 0.3608, -0.10890, -0.3804 0.3991, -0.10830, -0.5206 0.4373, -0.10510, -0.6192 0.4757, -0.09890, -0.6288 0.5137, -0.09070, -0.6754 0.5694, -0.07640, -0.6196 15 Flap element taps 1.0000, 0.00130, -0.5500 0.9365, 0.01390, -0.4711 0.8333, 0.03280, -0.6057 0.7436, 0.04930, -0.6843 0.7049, 0.05670, -0.6801 0.6662, 0.06410, -0.6511 0.6522, 0.01390, -0.9754 0.5969, -0.00020, -0.9985 0.6000, -0.03020, -1.0358 0.6324, -0.04540, -0.8049 0.6667, -0.04880, -0.4548 0.7046, -0.04110, -0.4042 0.7429, -0.03210, -0.3988 0.8333, -0.01400, -0.4143 0.9311, -0.00120, -0.4165 --------- Run Conditions: vel=105.9 ft/s Re=1.003x10^6 AOA=27.01 Flap deflection=-45.00 Totals: Cl=0.4548 Cdp=0.3242 Cm(c/4)=0.0418 Cs=-0.0823 Ch=0.0018 Main component: Cl=0.4410 Cdp=0.3817 Cm=-0.1023 Flap component: Cl=0.0138 Cdp=-0.0575 Cm=0.0060 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7967 0.6175, -0.04610, -1.1292 0.5841, -0.02440, -1.1201 0.5775, 0.01750, -1.1303 0.5777, 0.04660, -1.1283 0.6274, 0.07170, -0.6619 0.5694, 0.08320, -0.7259 0.5112, 0.09370, -0.7730 0.4731, 0.09830, -0.7624 0.4349, 0.10070, -0.7790 0.3960, 0.10120, -0.7877 0.3566, 0.10020, -0.8254 0.3172, 0.09790, -0.8394 0.2778, 0.09440, -0.8675 0.2393, 0.08960, -0.8953 0.2056, 0.08360, -0.9459 0.1633, 0.07610, -0.9958 0.1261, 0.06710, -1.0585 0.0900, 0.05640, -1.1169 0.0571, 0.04390, -1.1834 0.0283, 0.02940, -1.2908 0.0142, 0.01970, -1.5560 0.0081, 0.01410, -1.8181 0.0026, 0.00780, -1.8218 0.0000, 0.00000, 0.0390 0.0037, -0.00840, -0.2060 0.0112, -0.01420, 0.6563 0.0191, -0.01930, 0.8984 0.0397, -0.03030, 1.0150 0.0706, -0.04420, 0.9476 0.1037, -0.05710, 0.8449 0.1384, -0.06890, 0.6961 0.1741, -0.07950, 0.5452 0.2102, -0.08660, 0.3799 0.2472, -0.09640, 0.1876 0.2844, -0.10270, 0.0145 0.3225, -0.10690, -0.1608 0.3608, -0.10890, -0.3520 0.3991, -0.10830, -0.5030 0.4373, -0.10510, -0.6209 0.4757, -0.09890, -0.6438 0.5137, -0.09070, -0.7096 0.5694, -0.07640, -0.6729 15 Flap element taps 1.0000, 0.00130, -0.6211 0.9365, 0.01390, -0.5235 0.8333, 0.03280, -0.6067 0.7436, 0.04930, -0.6475 0.7049, 0.05670, -0.6420 0.6662, 0.06410, -0.6350 0.6522, 0.01390, -1.1164 0.5969, -0.00020, -1.1446 0.6000, -0.03020, -1.1895 0.6324, -0.04540, -1.0166 0.6667, -0.04880, -0.5848 0.7046, -0.04110, -0.5096 0.7429, -0.03210, -0.5039 0.8333, -0.01400, -0.5225 0.9311, -0.00120, -0.5296