S809 UNVENTED AILERON, CLEAN, CHORD = 18 IN --------- Run Conditions: vel=107.7 ft/s Re=1.005x10^6 AOA=-6.01 Flap deflection=-45.00 Totals: Cl=-1.4288 Cdp=0.2511 Cm(c/4)=0.1742 Cs=-0.1002 Ch=0.3152 Main component: Cl=-1.1924 Cdp=0.0026 Cm=0.3025 Flap component: Cl=-0.2364 Cdp=0.2486 Cm=0.2336 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5835 0.6175, -0.04610, -0.5537 0.5841, -0.02440, -0.5505 0.5775, 0.01750, -0.5602 0.5777, 0.04660, -0.5589 0.6274, 0.07170, 0.7064 0.5694, 0.08320, 0.6772 0.5112, 0.09370, 0.5317 0.4731, 0.09830, 0.4970 0.4349, 0.10070, 0.4825 0.3960, 0.10120, 0.4160 0.3566, 0.10020, 0.4651 0.3172, 0.09790, 0.4648 0.2778, 0.09440, 0.4790 0.2393, 0.08960, 0.5090 0.2056, 0.08360, 0.5158 0.1633, 0.07610, 0.6323 0.1261, 0.06710, 0.7073 0.0900, 0.05640, 0.8487 0.0571, 0.04390, 0.9602 0.0283, 0.02940, 1.0122 0.0142, 0.01970, 0.8109 0.0081, 0.01410, 0.3943 0.0026, 0.00780, -0.6974 0.0000, 0.00000, -4.5249 0.0037, -0.00840, -4.8627 0.0112, -0.01420, -4.4997 0.0191, -0.01930, -2.4936 0.0397, -0.03030, -1.9977 0.0706, -0.04420, -1.7220 0.1037, -0.05710, -1.6476 0.1384, -0.06890, -1.5514 0.1741, -0.07950, -1.5372 0.2102, -0.08660, -1.5990 0.2472, -0.09640, -1.6008 0.2844, -0.10270, -1.5857 0.3225, -0.10690, -1.4849 0.3608, -0.10890, -1.4053 0.3991, -0.10830, -1.1767 0.4373, -0.10510, -0.9195 0.4757, -0.09890, -0.6902 0.5137, -0.09070, -0.6227 0.5694, -0.07640, -0.5747 15 Flap element taps 1.0000, 0.00130, -0.5618 0.9365, 0.01390, 0.1764 0.8333, 0.03280, 0.5192 0.7436, 0.04930, 0.7168 0.7049, 0.05670, 0.7567 0.6662, 0.06410, 0.7237 0.6522, 0.01390, -0.5600 0.5969, -0.00020, -0.5679 0.6000, -0.03020, -0.5663 0.6324, -0.04540, -0.5831 0.6667, -0.04880, -0.6010 0.7046, -0.04110, -0.5885 0.7429, -0.03210, -0.5944 0.8333, -0.01400, -0.5976 0.9311, -0.00120, -0.5683 --------- Run Conditions: vel=108.8 ft/s Re=1.018x10^6 AOA=0.01 Flap deflection=-45.00 Totals: Cl=-1.4590 Cdp=0.2064 Cm(c/4)=0.2238 Cs=-0.2067 Ch=0.3187 Main component: Cl=-1.1928 Cdp=-0.0228 Cm=0.3507 Flap component: Cl=-0.2661 Cdp=0.2292 Cm=0.2378 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6880 0.6175, -0.04610, -0.5620 0.5841, -0.02440, -0.5712 0.5775, 0.01750, -0.5807 0.5777, 0.04660, -0.5832 0.6274, 0.07170, 0.7602 0.5694, 0.08320, 0.7342 0.5112, 0.09370, 0.4923 0.4731, 0.09830, 0.3897 0.4349, 0.10070, 0.3667 0.3960, 0.10120, 0.2345 0.3566, 0.10020, 0.3440 0.3172, 0.09790, 0.3296 0.2778, 0.09440, 0.3329 0.2393, 0.08960, 0.3434 0.2056, 0.08360, 0.2836 0.1633, 0.07610, 0.4574 0.1261, 0.06710, 0.4908 0.0900, 0.05640, 0.6638 0.0571, 0.04390, 0.7935 0.0283, 0.02940, 0.9839 0.0142, 0.01970, 1.0116 0.0081, 0.01410, 0.8214 0.0026, 0.00780, 0.3153 0.0000, 0.00000, -1.7557 0.0037, -0.00840, -2.6932 0.0112, -0.01420, -2.1941 0.0191, -0.01930, -2.0859 0.0397, -0.03030, -1.2678 0.0706, -0.04420, -1.2651 0.1037, -0.05710, -1.3328 0.1384, -0.06890, -1.2850 0.1741, -0.07950, -1.3703 0.2102, -0.08660, -1.5791 0.2472, -0.09640, -1.6475 0.2844, -0.10270, -1.7611 0.3225, -0.10690, -1.7364 0.3608, -0.10890, -1.8335 0.3991, -0.10830, -1.7493 0.4373, -0.10510, -1.6982 0.4757, -0.09890, -1.4678 0.5137, -0.09070, -1.2855 0.5694, -0.07640, -0.8886 15 Flap element taps 1.0000, 0.00130, -0.6099 0.9365, 0.01390, 0.1401 0.8333, 0.03280, 0.4764 0.7436, 0.04930, 0.6976 0.7049, 0.05670, 0.7724 0.6662, 0.06410, 0.7647 0.6522, 0.01390, -0.5954 0.5969, -0.00020, -0.5994 0.6000, -0.03020, -0.6251 0.6324, -0.04540, -0.6305 0.6667, -0.04880, -0.6468 0.7046, -0.04110, -0.6204 0.7429, -0.03210, -0.6434 0.8333, -0.01400, -0.6539 0.9311, -0.00120, -0.6046 --------- Run Conditions: vel=108.8 ft/s Re=1.018x10^6 AOA=3.03 Flap deflection=-45.00 Totals: Cl=-1.3096 Cdp=0.1648 Cm(c/4)=0.2260 Cs=-0.2338 Ch=0.2959 Main component: Cl=-1.0495 Cdp=-0.0366 Cm=0.3286 Flap component: Cl=-0.2601 Cdp=0.2015 Cm=0.2222 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6610 0.6175, -0.04610, -0.4994 0.5841, -0.02440, -0.5123 0.5775, 0.01750, -0.5211 0.5777, 0.04660, -0.5234 0.6274, 0.07170, 0.7621 0.5694, 0.08320, 0.7422 0.5112, 0.09370, 0.5411 0.4731, 0.09830, 0.3231 0.4349, 0.10070, 0.3015 0.3960, 0.10120, 0.1253 0.3566, 0.10020, 0.2764 0.3172, 0.09790, 0.2517 0.2778, 0.09440, 0.2525 0.2393, 0.08960, 0.2445 0.2056, 0.08360, 0.1341 0.1633, 0.07610, 0.3470 0.1261, 0.06710, 0.3419 0.0900, 0.05640, 0.5261 0.0571, 0.04390, 0.6414 0.0283, 0.02940, 0.8717 0.0142, 0.01970, 1.0009 0.0081, 0.01410, 0.8880 0.0026, 0.00780, 0.7197 0.0000, 0.00000, -0.4295 0.0037, -0.00840, -1.4705 0.0112, -0.01420, -1.2645 0.0191, -0.01930, -1.0840 0.0397, -0.03030, -0.8940 0.0706, -0.04420, -0.9422 0.1037, -0.05710, -1.0591 0.1384, -0.06890, -1.0044 0.1741, -0.07950, -1.1403 0.2102, -0.08660, -1.4108 0.2472, -0.09640, -1.4755 0.2844, -0.10270, -1.6327 0.3225, -0.10690, -1.6088 0.3608, -0.10890, -1.7450 0.3991, -0.10830, -1.6703 0.4373, -0.10510, -1.6496 0.4757, -0.09890, -1.5679 0.5137, -0.09070, -1.4308 0.5694, -0.07640, -0.8394 15 Flap element taps 1.0000, 0.00130, -0.5302 0.9365, 0.01390, 0.1445 0.8333, 0.03280, 0.4606 0.7436, 0.04930, 0.6845 0.7049, 0.05670, 0.7648 0.6662, 0.06410, 0.7636 0.6522, 0.01390, -0.5474 0.5969, -0.00020, -0.5318 0.6000, -0.03020, -0.5607 0.6324, -0.04540, -0.5731 0.6667, -0.04880, -0.5919 0.7046, -0.04110, -0.5511 0.7429, -0.03210, -0.5830 0.8333, -0.01400, -0.6002 0.9311, -0.00120, -0.5276 --------- Run Conditions: vel=107.8 ft/s Re=1.009x10^6 AOA=6.03 Flap deflection=-45.00 Totals: Cl=-1.0685 Cdp=0.1568 Cm(c/4)=0.2293 Cs=-0.2681 Ch=0.2854 Main component: Cl=-0.8061 Cdp=-0.0247 Cm=0.2754 Flap component: Cl=-0.2624 Cdp=0.1815 Cm=0.2154 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6307 0.6175, -0.04610, -0.4924 0.5841, -0.02440, -0.5086 0.5775, 0.01750, -0.5173 0.5777, 0.04660, -0.5217 0.6274, 0.07170, 0.7217 0.5694, 0.08320, 0.7295 0.5112, 0.09370, 0.4947 0.4731, 0.09830, 0.3088 0.4349, 0.10070, 0.1911 0.3960, 0.10120, -0.0135 0.3566, 0.10020, 0.1683 0.3172, 0.09790, 0.1318 0.2778, 0.09440, 0.1241 0.2393, 0.08960, 0.0960 0.2056, 0.08360, -0.0636 0.1633, 0.07610, 0.1694 0.1261, 0.06710, 0.1237 0.0900, 0.05640, 0.2989 0.0571, 0.04390, 0.3831 0.0283, 0.02940, 0.6178 0.0142, 0.01970, 0.8225 0.0081, 0.01410, 0.7840 0.0026, 0.00780, 1.0059 0.0000, 0.00000, 0.6689 0.0037, -0.00840, -0.1998 0.0112, -0.01420, -0.3229 0.0191, -0.01930, -0.3204 0.0397, -0.03030, -0.3369 0.0706, -0.04420, -0.5106 0.1037, -0.05710, -0.6830 0.1384, -0.06890, -0.6330 0.1741, -0.07950, -0.8008 0.2102, -0.08660, -1.1272 0.2472, -0.09640, -1.1885 0.2844, -0.10270, -1.3810 0.3225, -0.10690, -1.3556 0.3608, -0.10890, -1.5294 0.3991, -0.10830, -1.4706 0.4373, -0.10510, -1.4973 0.4757, -0.09890, -1.3924 0.5137, -0.09070, -1.3719 0.5694, -0.07640, -0.7688 15 Flap element taps 1.0000, 0.00130, -0.5225 0.9365, 0.01390, 0.1204 0.8333, 0.03280, 0.4292 0.7436, 0.04930, 0.6620 0.7049, 0.05670, 0.7391 0.6662, 0.06410, 0.7149 0.6522, 0.01390, -0.5526 0.5969, -0.00020, -0.5241 0.6000, -0.03020, -0.5550 0.6324, -0.04540, -0.5753 0.6667, -0.04880, -0.5969 0.7046, -0.04110, -0.5425 0.7429, -0.03210, -0.5826 0.8333, -0.01400, -0.6034 0.9311, -0.00120, -0.5116 --------- Run Conditions: vel=107.1 ft/s Re=1.003x10^6 AOA=9.01 Flap deflection=-45.00 Totals: Cl=-0.8100 Cdp=0.1499 Cm(c/4)=0.2309 Cs=-0.2749 Ch=0.2758 Main component: Cl=-0.5483 Cdp=-0.0097 Cm=0.2171 Flap component: Cl=-0.2617 Cdp=0.1596 Cm=0.2079 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5894 0.6175, -0.04610, -0.4804 0.5841, -0.02440, -0.5002 0.5775, 0.01750, -0.5099 0.5777, 0.04660, -0.5141 0.6274, 0.07170, 0.6392 0.5694, 0.08320, 0.6878 0.5112, 0.09370, 0.4582 0.4731, 0.09830, 0.3020 0.4349, 0.10070, 0.1571 0.3960, 0.10120, -0.1630 0.3566, 0.10020, 0.0478 0.3172, 0.09790, 0.0015 0.2778, 0.09440, -0.0160 0.2393, 0.08960, -0.0682 0.2056, 0.08360, -0.2743 0.1633, 0.07610, -0.0374 0.1261, 0.06710, -0.1307 0.0900, 0.05640, 0.0191 0.0571, 0.04390, 0.0418 0.0283, 0.02940, 0.2215 0.0142, 0.01970, 0.4217 0.0081, 0.01410, 0.4007 0.0026, 0.00780, 0.8334 0.0000, 0.00000, 1.0688 0.0037, -0.00840, 0.6627 0.0112, -0.01420, 0.3984 0.0191, -0.01930, 0.2947 0.0397, -0.03030, 0.1485 0.0706, -0.04420, -0.1075 0.1037, -0.05710, -0.3217 0.1384, -0.06890, -0.2764 0.1741, -0.07950, -0.4694 0.2102, -0.08660, -0.8374 0.2472, -0.09640, -0.8983 0.2844, -0.10270, -1.1206 0.3225, -0.10690, -1.0934 0.3608, -0.10890, -1.2996 0.3991, -0.10830, -1.2544 0.4373, -0.10510, -1.3330 0.4757, -0.09890, -1.2217 0.5137, -0.09070, -1.1887 0.5694, -0.07640, -0.6818 15 Flap element taps 1.0000, 0.00130, -0.5086 0.9365, 0.01390, 0.1012 0.8333, 0.03280, 0.4062 0.7436, 0.04930, 0.6420 0.7049, 0.05670, 0.6708 0.6662, 0.06410, 0.6077 0.6522, 0.01390, -0.5533 0.5969, -0.00020, -0.5147 0.6000, -0.03020, -0.5460 0.6324, -0.04540, -0.5705 0.6667, -0.04880, -0.5948 0.7046, -0.04110, -0.5307 0.7429, -0.03210, -0.5788 0.8333, -0.01400, -0.6040 0.9311, -0.00120, -0.4975 --------- Run Conditions: vel=106.6 ft/s Re=0.999x10^6 AOA=12.03 Flap deflection=-45.00 Totals: Cl=-0.5625 Cdp=0.1431 Cm(c/4)=0.2323 Cs=-0.2572 Ch=0.2662 Main component: Cl=-0.3054 Cdp=0.0079 Cm=0.1635 Flap component: Cl=-0.2570 Cdp=0.1351 Cm=0.1989 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5515 0.6175, -0.04610, -0.4851 0.5841, -0.02440, -0.5071 0.5775, 0.01750, -0.5154 0.5777, 0.04660, -0.5240 0.6274, 0.07170, 0.5174 0.5694, 0.08320, 0.6011 0.5112, 0.09370, 0.4494 0.4731, 0.09830, 0.2753 0.4349, 0.10070, 0.1109 0.3960, 0.10120, -0.1982 0.3566, 0.10020, -0.0214 0.3172, 0.09790, -0.1474 0.2778, 0.09440, -0.1617 0.2393, 0.08960, -0.2322 0.2056, 0.08360, -0.4830 0.1633, 0.07610, -0.2549 0.1261, 0.06710, -0.3997 0.0900, 0.05640, -0.2934 0.0571, 0.04390, -0.3543 0.0283, 0.02940, -0.2893 0.0142, 0.01970, -0.1765 0.0081, 0.01410, -0.2630 0.0026, 0.00780, 0.1747 0.0000, 0.00000, 0.7780 0.0037, -0.00840, 1.0174 0.0112, -0.01420, 0.8354 0.0191, -0.01930, 0.7177 0.0397, -0.03030, 0.5271 0.0706, -0.04420, 0.2294 0.1037, -0.05710, -0.0033 0.1384, -0.06890, 0.0433 0.1741, -0.07950, -0.1665 0.2102, -0.08660, -0.5667 0.2472, -0.09640, -0.6234 0.2844, -0.10270, -0.8677 0.3225, -0.10690, -0.8410 0.3608, -0.10890, -1.0716 0.3991, -0.10830, -1.0429 0.4373, -0.10510, -1.1656 0.4757, -0.09890, -1.0696 0.5137, -0.09070, -1.0354 0.5694, -0.07640, -0.6538 15 Flap element taps 1.0000, 0.00130, -0.4905 0.9365, 0.01390, 0.0904 0.8333, 0.03280, 0.4009 0.7436, 0.04930, 0.5879 0.7049, 0.05670, 0.5418 0.6662, 0.06410, 0.4834 0.6522, 0.01390, -0.5667 0.5969, -0.00020, -0.5134 0.6000, -0.03020, -0.5499 0.6324, -0.04540, -0.5721 0.6667, -0.04880, -0.5931 0.7046, -0.04110, -0.5192 0.7429, -0.03210, -0.5691 0.8333, -0.01400, -0.6009 0.9311, -0.00120, -0.4806 --------- Run Conditions: vel=106.2 ft/s Re=0.999x10^6 AOA=15.02 Flap deflection=-45.00 Totals: Cl=-0.3149 Cdp=0.1355 Cm(c/4)=0.2290 Cs=-0.2125 Ch=0.2533 Main component: Cl=-0.0732 Cdp=0.0289 Cm=0.1119 Flap component: Cl=-0.2417 Cdp=0.1066 Cm=0.1844 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5002 0.6175, -0.04610, -0.4821 0.5841, -0.02440, -0.5032 0.5775, 0.01750, -0.5136 0.5777, 0.04660, -0.5235 0.6274, 0.07170, 0.3276 0.5694, 0.08320, 0.4324 0.5112, 0.09370, 0.3499 0.4731, 0.09830, 0.2704 0.4349, 0.10070, 0.1113 0.3960, 0.10120, -0.2565 0.3566, 0.10020, -0.0891 0.3172, 0.09790, -0.1814 0.2778, 0.09440, -0.2390 0.2393, 0.08960, -0.3628 0.2056, 0.08360, -0.6952 0.1633, 0.07610, -0.4852 0.1261, 0.06710, -0.6857 0.0900, 0.05640, -0.6378 0.0571, 0.04390, -0.8063 0.0283, 0.02940, -0.9069 0.0142, 0.01970, -0.9703 0.0081, 0.01410, -1.2134 0.0026, 0.00780, -0.7201 0.0000, 0.00000, -0.3145 0.0037, -0.00840, 0.9567 0.0112, -0.01420, 1.0106 0.0191, -0.01930, 0.9588 0.0397, -0.03030, 0.8038 0.0706, -0.04420, 0.5083 0.1037, -0.05710, 0.2724 0.1384, -0.06890, 0.3307 0.1741, -0.07950, 0.1117 0.2102, -0.08660, -0.3100 0.2472, -0.09640, -0.3600 0.2844, -0.10270, -0.6206 0.3225, -0.10690, -0.5947 0.3608, -0.10890, -0.8469 0.3991, -0.10830, -0.8302 0.4373, -0.10510, -0.9917 0.4757, -0.09890, -0.9199 0.5137, -0.09070, -0.9161 0.5694, -0.07640, -0.6998 15 Flap element taps 1.0000, 0.00130, -0.4712 0.9365, 0.01390, 0.1007 0.8333, 0.03280, 0.4062 0.7436, 0.04930, 0.4429 0.7049, 0.05670, 0.3435 0.6662, 0.06410, 0.2907 0.6522, 0.01390, -0.5660 0.5969, -0.00020, -0.5149 0.6000, -0.03020, -0.5475 0.6324, -0.04540, -0.5601 0.6667, -0.04880, -0.5771 0.7046, -0.04110, -0.4978 0.7429, -0.03210, -0.5532 0.8333, -0.01400, -0.5896 0.9311, -0.00120, -0.4578 --------- Run Conditions: vel=106.5 ft/s Re=1.003x10^6 AOA=17.98 Flap deflection=-45.00 Totals: Cl=-0.0135 Cdp=0.1208 Cm(c/4)=0.1990 Cs=-0.1191 Ch=0.2031 Main component: Cl=0.1703 Cdp=0.0646 Cm=0.0512 Flap component: Cl=-0.1838 Cdp=0.0563 Cm=0.1417 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5330 0.6175, -0.04610, -0.5650 0.5841, -0.02440, -0.5878 0.5775, 0.01750, -0.5987 0.5777, 0.04660, -0.6136 0.6274, 0.07170, 0.0979 0.5694, 0.08320, 0.1943 0.5112, 0.09370, 0.1143 0.4731, 0.09830, 0.1114 0.4349, 0.10070, 0.0778 0.3960, 0.10120, -0.2408 0.3566, 0.10020, -0.0827 0.3172, 0.09790, -0.2302 0.2778, 0.09440, -0.3381 0.2393, 0.08960, -0.5017 0.2056, 0.08360, -0.8641 0.1633, 0.07610, -0.6901 0.1261, 0.06710, -0.9603 0.0900, 0.05640, -0.9908 0.0571, 0.04390, -1.2764 0.0283, 0.02940, -1.6725 0.0142, 0.01970, -1.9959 0.0081, 0.01410, -2.5287 0.0026, 0.00780, -2.2516 0.0000, 0.00000, -2.2473 0.0037, -0.00840, 0.4833 0.0112, -0.01420, 0.9583 0.0191, -0.01930, 1.0256 0.0397, -0.03030, 0.9830 0.0706, -0.04420, 0.7284 0.1037, -0.05710, 0.5078 0.1384, -0.06890, 0.5824 0.1741, -0.07950, 0.3635 0.2102, -0.08660, -0.0694 0.2472, -0.09640, -0.1123 0.2844, -0.10270, -0.3871 0.3225, -0.10690, -0.3583 0.3608, -0.10890, -0.6269 0.3991, -0.10830, -0.6279 0.4373, -0.10510, -0.8240 0.4757, -0.09890, -0.7834 0.5137, -0.09070, -0.8223 0.5694, -0.07640, -0.5825 15 Flap element taps 1.0000, 0.00130, -0.4351 0.9365, 0.01390, 0.1245 0.8333, 0.03280, 0.2114 0.7436, 0.04930, 0.0823 0.7049, 0.05670, 0.0655 0.6662, 0.06410, 0.0557 0.6522, 0.01390, -0.6554 0.5969, -0.00020, -0.5978 0.6000, -0.03020, -0.6386 0.6324, -0.04540, -0.5839 0.6667, -0.04880, -0.5482 0.7046, -0.04110, -0.4468 0.7429, -0.03210, -0.5061 0.8333, -0.01400, -0.5486 0.9311, -0.00120, -0.4151 --------- Run Conditions: vel=106.8 ft/s Re=1.007x10^6 AOA=19.99 Flap deflection=-45.00 Totals: Cl=0.2708 Cdp=0.1165 Cm(c/4)=0.1563 Cs=-0.0169 Ch=0.1446 Main component: Cl=0.3898 Cdp=0.0957 Cm=-0.0123 Flap component: Cl=-0.1190 Cdp=0.0208 Cm=0.0950 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4668 0.6175, -0.04610, -0.5261 0.5841, -0.02440, -0.5546 0.5775, 0.01750, -0.5676 0.5777, 0.04660, -0.5827 0.6274, 0.07170, -0.1659 0.5694, 0.08320, -0.0754 0.5112, 0.09370, -0.1482 0.4731, 0.09830, -0.1499 0.4349, 0.10070, -0.1688 0.3960, 0.10120, -0.4488 0.3566, 0.10020, -0.1699 0.3172, 0.09790, -0.2377 0.2778, 0.09440, -0.3303 0.2393, 0.08960, -0.5360 0.2056, 0.08360, -0.9593 0.1633, 0.07610, -0.8272 0.1261, 0.06710, -1.1659 0.0900, 0.05640, -1.2649 0.0571, 0.04390, -1.6901 0.0283, 0.02940, -2.1985 0.0142, 0.01970, -2.7772 0.0081, 0.01410, -3.8923 0.0026, 0.00780, -3.7372 0.0000, 0.00000, -4.2216 0.0037, -0.00840, -0.1664 0.0112, -0.01420, 0.7582 0.0191, -0.01930, 0.9739 0.0397, -0.03030, 1.0504 0.0706, -0.04420, 0.8513 0.1037, -0.05710, 0.6576 0.1384, -0.06890, 0.7560 0.1741, -0.07950, 0.5443 0.2102, -0.08660, 0.1073 0.2472, -0.09640, 0.0807 0.2844, -0.10270, -0.1967 0.3225, -0.10690, -0.1611 0.3608, -0.10890, -0.4387 0.3991, -0.10830, -0.4406 0.4373, -0.10510, -0.6575 0.4757, -0.09890, -0.6380 0.5137, -0.09070, -0.7040 0.5694, -0.07640, -0.4731 15 Flap element taps 1.0000, 0.00130, -0.3683 0.9365, 0.01390, 0.1297 0.8333, 0.03280, 0.0265 0.7436, 0.04930, -0.1863 0.7049, 0.05670, -0.2152 0.6662, 0.06410, -0.2081 0.6522, 0.01390, -0.6227 0.5969, -0.00020, -0.5521 0.6000, -0.03020, -0.6118 0.6324, -0.04540, -0.5723 0.6667, -0.04880, -0.4841 0.7046, -0.04110, -0.3739 0.7429, -0.03210, -0.4392 0.8333, -0.01400, -0.4854 0.9311, -0.00120, -0.3408 --------- Run Conditions: vel=100.6 ft/s Re=1.001x10^6 AOA=24.01 Flap deflection=-45.00 Totals: Cl=0.4349 Cdp=0.2629 Cm(c/4)=-0.0146 Cs=-0.0632 Ch=-0.0739 Main component: Cl=0.3440 Cdp=0.3203 Cm=-0.0848 Flap component: Cl=0.0909 Cdp=-0.0574 Cm=-0.0559 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7035 0.6175, -0.04610, -0.9528 0.5841, -0.02440, -0.9558 0.5775, 0.01750, -0.9602 0.5777, 0.04660, -0.9592 0.6274, 0.07170, -0.7629 0.5694, 0.08320, -0.8239 0.5112, 0.09370, -0.8502 0.4731, 0.09830, -0.8312 0.4349, 0.10070, -0.8227 0.3960, 0.10120, -0.8449 0.3566, 0.10020, -0.7899 0.3172, 0.09790, -0.7838 0.2778, 0.09440, -0.7894 0.2393, 0.08960, -0.7864 0.2056, 0.08360, -0.8246 0.1633, 0.07610, -0.7756 0.1261, 0.06710, -0.7976 0.0900, 0.05640, -0.7678 0.0571, 0.04390, -0.7696 0.0283, 0.02940, -0.7906 0.0142, 0.01970, -0.7971 0.0081, 0.01410, -0.8343 0.0026, 0.00780, -0.7164 0.0000, 0.00000, -1.0512 0.0037, -0.00840, 0.4721 0.0112, -0.01420, 0.9095 0.0191, -0.01930, 1.0026 0.0397, -0.03030, 0.9884 0.0706, -0.04420, 0.8359 0.1037, -0.05710, 0.6932 0.1384, -0.06890, 0.5658 0.1741, -0.07950, 0.4001 0.2102, -0.08660, 0.1910 0.2472, -0.09640, 0.0291 0.2844, -0.10270, -0.1581 0.3225, -0.10690, -0.2938 0.3608, -0.10890, -0.4883 0.3991, -0.10830, -0.6061 0.4373, -0.10510, -0.7008 0.4757, -0.09890, -0.7149 0.5137, -0.09070, -0.7293 0.5694, -0.07640, -0.6230 15 Flap element taps 1.0000, 0.00130, -1.0122 0.9365, 0.01390, -0.7312 0.8333, 0.03280, -0.8604 0.7436, 0.04930, -0.8581 0.7049, 0.05670, -0.8311 0.6662, 0.06410, -0.7702 0.6522, 0.01390, -0.9665 0.5969, -0.00020, -0.9687 0.6000, -0.03020, -0.9395 0.6324, -0.04540, -0.6469 0.6667, -0.04880, -0.5090 0.7046, -0.04110, -0.5002 0.7429, -0.03210, -0.5062 0.8333, -0.01400, -0.5218 0.9311, -0.00120, -0.5365 --------- Run Conditions: vel=106.0 ft/s Re=1.002x10^6 AOA=26.99 Flap deflection=-45.00 Totals: Cl=0.2492 Cdp=0.2990 Cm(c/4)=0.0381 Cs=-0.1534 Ch=-0.0064 Main component: Cl=0.2381 Cdp=0.3524 Cm=-0.0566 Flap component: Cl=0.0111 Cdp=-0.0533 Cm=0.0053 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.9263 0.6175, -0.04610, -1.2762 0.5841, -0.02440, -1.2656 0.5775, 0.01750, -1.2818 0.5777, 0.04660, -1.2874 0.6274, 0.07170, -0.6846 0.5694, 0.08320, -0.7054 0.5112, 0.09370, -0.7210 0.4731, 0.09830, -0.7164 0.4349, 0.10070, -0.7107 0.3960, 0.10120, -0.7220 0.3566, 0.10020, -0.7051 0.3172, 0.09790, -0.6931 0.2778, 0.09440, -0.6924 0.2393, 0.08960, -0.6882 0.2056, 0.08360, -0.7030 0.1633, 0.07610, -0.6866 0.1261, 0.06710, -0.6845 0.0900, 0.05640, -0.6764 0.0571, 0.04390, -0.6801 0.0283, 0.02940, -0.6946 0.0142, 0.01970, -0.6921 0.0081, 0.01410, -0.7127 0.0026, 0.00780, -0.6527 0.0000, 0.00000, -0.9141 0.0037, -0.00840, 0.4142 0.0112, -0.01420, 0.8870 0.0191, -0.01930, 0.9907 0.0397, -0.03030, 1.0045 0.0706, -0.04420, 0.8837 0.1037, -0.05710, 0.7483 0.1384, -0.06890, 0.6102 0.1741, -0.07950, 0.4510 0.2102, -0.08660, 0.2566 0.2472, -0.09640, 0.0703 0.2844, -0.10270, -0.1232 0.3225, -0.10690, -0.2886 0.3608, -0.10890, -0.4898 0.3991, -0.10830, -0.6470 0.4373, -0.10510, -0.7678 0.4757, -0.09890, -0.7911 0.5137, -0.09070, -0.8267 0.5694, -0.07640, -0.8005 15 Flap element taps 1.0000, 0.00130, -0.8104 0.9365, 0.01390, -0.7852 0.8333, 0.03280, -0.7542 0.7436, 0.04930, -0.7291 0.7049, 0.05670, -0.7104 0.6662, 0.06410, -0.6873 0.6522, 0.01390, -1.2718 0.5969, -0.00020, -1.2484 0.6000, -0.03020, -1.3521 0.6324, -0.04540, -1.1753 0.6667, -0.04880, -0.7363 0.7046, -0.04110, -0.6427 0.7429, -0.03210, -0.6404 0.8333, -0.01400, -0.6820 0.9311, -0.00120, -0.7001 --------- Run Conditions: vel=106.0 ft/s Re=1.003x10^6 AOA=29.99 Flap deflection=-45.00 Totals: Cl=0.2129 Cdp=0.3352 Cm(c/4)=0.0545 Cs=-0.1839 Ch=0.0258 Main component: Cl=0.2300 Cdp=0.3877 Cm=-0.0624 Flap component: Cl=-0.0172 Cdp=-0.0525 Cm=0.0288 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.9697 0.6175, -0.04610, -1.3591 0.5841, -0.02440, -1.3522 0.5775, 0.01750, -1.3706 0.5777, 0.04660, -1.3744 0.6274, 0.07170, -0.6791 0.5694, 0.08320, -0.6943 0.5112, 0.09370, -0.7096 0.4731, 0.09830, -0.7065 0.4349, 0.10070, -0.7051 0.3960, 0.10120, -0.7247 0.3566, 0.10020, -0.7028 0.3172, 0.09790, -0.6895 0.2778, 0.09440, -0.6883 0.2393, 0.08960, -0.6843 0.2056, 0.08360, -0.7039 0.1633, 0.07610, -0.6816 0.1261, 0.06710, -0.6845 0.0900, 0.05640, -0.6703 0.0571, 0.04390, -0.6742 0.0283, 0.02940, -0.6860 0.0142, 0.01970, -0.6843 0.0081, 0.01410, -0.7123 0.0026, 0.00780, -0.6471 0.0000, 0.00000, -0.7375 0.0037, -0.00840, 0.3028 0.0112, -0.01420, 0.8275 0.0191, -0.01930, 0.9617 0.0397, -0.03030, 1.0125 0.0706, -0.04420, 0.9171 0.1037, -0.05710, 0.7990 0.1384, -0.06890, 0.6765 0.1741, -0.07950, 0.5238 0.2102, -0.08660, 0.3249 0.2472, -0.09640, 0.1475 0.2844, -0.10270, -0.0511 0.3225, -0.10690, -0.2140 0.3608, -0.10890, -0.4238 0.3991, -0.10830, -0.5872 0.4373, -0.10510, -0.7257 0.4757, -0.09890, -0.7635 0.5137, -0.09070, -0.8460 0.5694, -0.07640, -0.8113 15 Flap element taps 1.0000, 0.00130, -0.7692 0.9365, 0.01390, -0.7327 0.8333, 0.03280, -0.7272 0.7436, 0.04930, -0.7107 0.7049, 0.05670, -0.6963 0.6662, 0.06410, -0.6806 0.6522, 0.01390, -1.3577 0.5969, -0.00020, -1.3830 0.6000, -0.03020, -1.4419 0.6324, -0.04540, -1.3282 0.6667, -0.04880, -0.8325 0.7046, -0.04110, -0.7107 0.7429, -0.03210, -0.7087 0.8333, -0.01400, -0.7472 0.9311, -0.00120, -0.7539 --------- Run Conditions: vel=105.6 ft/s Re=0.999x10^6 AOA=34.98 Flap deflection=-45.00 Totals: Cl=0.2196 Cdp=0.4136 Cm(c/4)=0.0619 Cs=-0.2129 Ch=0.0469 Main component: Cl=0.2590 Cdp=0.4684 Cm=-0.0902 Flap component: Cl=-0.0393 Cdp=-0.0549 Cm=0.0478 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.0104 0.6175, -0.04610, -1.4841 0.5841, -0.02440, -1.4791 0.5775, 0.01750, -1.4969 0.5777, 0.04660, -1.5023 0.6274, 0.07170, -0.7295 0.5694, 0.08320, -0.7389 0.5112, 0.09370, -0.7620 0.4731, 0.09830, -0.7567 0.4349, 0.10070, -0.7550 0.3960, 0.10120, -0.7813 0.3566, 0.10020, -0.7539 0.3172, 0.09790, -0.7430 0.2778, 0.09440, -0.7412 0.2393, 0.08960, -0.7386 0.2056, 0.08360, -0.7656 0.1633, 0.07610, -0.7344 0.1261, 0.06710, -0.7437 0.0900, 0.05640, -0.7274 0.0571, 0.04390, -0.7314 0.0283, 0.02940, -0.7365 0.0142, 0.01970, -0.7347 0.0081, 0.01410, -0.7698 0.0026, 0.00780, -0.6956 0.0000, 0.00000, -0.7459 0.0037, -0.00840, 0.0533 0.0112, -0.01420, 0.6860 0.0191, -0.01930, 0.8850 0.0397, -0.03030, 1.0167 0.0706, -0.04420, 0.9731 0.1037, -0.05710, 0.8877 0.1384, -0.06890, 0.7964 0.1741, -0.07950, 0.6574 0.2102, -0.08660, 0.4673 0.2472, -0.09640, 0.3007 0.2844, -0.10270, 0.1006 0.3225, -0.10690, -0.0575 0.3608, -0.10890, -0.2780 0.3991, -0.10830, -0.4528 0.4373, -0.10510, -0.6155 0.4757, -0.09890, -0.6806 0.5137, -0.09070, -0.7940 0.5694, -0.07640, -0.7987 15 Flap element taps 1.0000, 0.00130, -0.8430 0.9365, 0.01390, -0.7637 0.8333, 0.03280, -0.7676 0.7436, 0.04930, -0.7577 0.7049, 0.05670, -0.7459 0.6662, 0.06410, -0.7319 0.6522, 0.01390, -1.4844 0.5969, -0.00020, -1.5141 0.6000, -0.03020, -1.5777 0.6324, -0.04540, -1.5921 0.6667, -0.04880, -1.0087 0.7046, -0.04110, -0.8206 0.7429, -0.03210, -0.8197 0.8333, -0.01400, -0.8581 0.9311, -0.00120, -0.8408 --------- Run Conditions: vel=106.0 ft/s Re=1.004x10^6 AOA=39.99 Flap deflection=-45.00 Totals: Cl=0.1796 Cdp=0.4966 Cm(c/4)=0.0793 Cs=-0.2650 Ch=0.0827 Main component: Cl=0.2672 Cdp=0.5542 Cm=-0.1167 Flap component: Cl=-0.0877 Cdp=-0.0576 Cm=0.0819 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.0772 0.6175, -0.04610, -1.6490 0.5841, -0.02440, -1.6453 0.5775, 0.01750, -1.6636 0.5777, 0.04660, -1.6691 0.6274, 0.07170, -0.7873 0.5694, 0.08320, -0.7908 0.5112, 0.09370, -0.8086 0.4731, 0.09830, -0.8097 0.4349, 0.10070, -0.8081 0.3960, 0.10120, -0.8428 0.3566, 0.10020, -0.8103 0.3172, 0.09790, -0.7974 0.2778, 0.09440, -0.7949 0.2393, 0.08960, -0.7928 0.2056, 0.08360, -0.8266 0.1633, 0.07610, -0.7885 0.1261, 0.06710, -0.7977 0.0900, 0.05640, -0.7762 0.0571, 0.04390, -0.7809 0.0283, 0.02940, -0.7887 0.0142, 0.01970, -0.7834 0.0081, 0.01410, -0.8246 0.0026, 0.00780, -0.7443 0.0000, 0.00000, -0.7861 0.0037, -0.00840, -0.2031 0.0112, -0.01420, 0.5140 0.0191, -0.01930, 0.7764 0.0397, -0.03030, 0.9888 0.0706, -0.04420, 0.9987 0.1037, -0.05710, 0.9519 0.1384, -0.06890, 0.8928 0.1741, -0.07950, 0.7719 0.2102, -0.08660, 0.5898 0.2472, -0.09640, 0.4424 0.2844, -0.10270, 0.2450 0.3225, -0.10690, 0.0927 0.3608, -0.10890, -0.1346 0.3991, -0.10830, -0.3182 0.4373, -0.10510, -0.5041 0.4757, -0.09890, -0.5985 0.5137, -0.09070, -0.7503 0.5694, -0.07640, -0.8010 15 Flap element taps 1.0000, 0.00130, -0.9833 0.9365, 0.01390, -0.8325 0.8333, 0.03280, -0.8293 0.7436, 0.04930, -0.8192 0.7049, 0.05670, -0.8059 0.6662, 0.06410, -0.7933 0.6522, 0.01390, -1.6515 0.5969, -0.00020, -1.6600 0.6000, -0.03020, -1.7707 0.6324, -0.04540, -1.9872 0.6667, -0.04880, -1.3869 0.7046, -0.04110, -1.0340 0.7429, -0.03210, -1.0169 0.8333, -0.01400, -1.0479 0.9311, -0.00120, -0.9962 --------- Run Conditions: vel=106.3 ft/s Re=1.007x10^6 AOA=45.04 Flap deflection=-45.00 Totals: Cl=0.1214 Cdp=0.5671 Cm(c/4)=0.0993 Cs=-0.3148 Ch=0.1228 Main component: Cl=0.2652 Cdp=0.6374 Cm=-0.1438 Flap component: Cl=-0.1438 Cdp=-0.0703 Cm=0.1213 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.1136 0.6175, -0.04610, -1.7802 0.5841, -0.02440, -1.7772 0.5775, 0.01750, -1.7985 0.5777, 0.04660, -1.8022 0.6274, 0.07170, -0.8329 0.5694, 0.08320, -0.8387 0.5112, 0.09370, -0.8581 0.4731, 0.09830, -0.8554 0.4349, 0.10070, -0.8565 0.3960, 0.10120, -0.8990 0.3566, 0.10020, -0.8617 0.3172, 0.09790, -0.8503 0.2778, 0.09440, -0.8497 0.2393, 0.08960, -0.8492 0.2056, 0.08360, -0.8862 0.1633, 0.07610, -0.8397 0.1261, 0.06710, -0.8564 0.0900, 0.05640, -0.8315 0.0571, 0.04390, -0.8372 0.0283, 0.02940, -0.8424 0.0142, 0.01970, -0.8389 0.0081, 0.01410, -0.8830 0.0026, 0.00780, -0.7948 0.0000, 0.00000, -0.8328 0.0037, -0.00840, -0.4444 0.0112, -0.01420, 0.3250 0.0191, -0.01930, 0.6427 0.0397, -0.03030, 0.9316 0.0706, -0.04420, 0.9985 0.1037, -0.05710, 0.9896 0.1384, -0.06890, 0.9657 0.1741, -0.07950, 0.8656 0.2102, -0.08660, 0.6981 0.2472, -0.09640, 0.5702 0.2844, -0.10270, 0.3803 0.3225, -0.10690, 0.2376 0.3608, -0.10890, 0.0082 0.3991, -0.10830, -0.1794 0.4373, -0.10510, -0.3862 0.4757, -0.09890, -0.5026 0.5137, -0.09070, -0.6805 0.5694, -0.07640, -0.7756 15 Flap element taps 1.0000, 0.00130, -0.9602 0.9365, 0.01390, -0.8392 0.8333, 0.03280, -0.8569 0.7436, 0.04930, -0.8548 0.7049, 0.05670, -0.8473 0.6662, 0.06410, -0.8349 0.6522, 0.01390, -1.7809 0.5969, -0.00020, -1.8156 0.6000, -0.03020, -1.9236 0.6324, -0.04540, -2.3768 0.6667, -0.04880, -1.8268 0.7046, -0.04110, -1.2593 0.7429, -0.03210, -1.2329 0.8333, -0.01400, -1.2299 0.9311, -0.00120, -1.0827 --------- Run Conditions: vel=100.6 ft/s Re=1.002x10^6 AOA=59.99 Flap deflection=-45.00 Totals: Cl=0.3225 Cdp=0.9351 Cm(c/4)=-0.0169 Cs=-0.1884 Ch=-0.0701 Main component: Cl=0.3527 Cdp=0.9960 Cm=-0.2922 Flap component: Cl=-0.0303 Cdp=-0.0609 Cm=0.0325 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8334 0.6175, -0.04610, -1.6650 0.5841, -0.02440, -1.6877 0.5775, 0.01750, -1.6882 0.5777, 0.04660, -1.6871 0.6274, 0.07170, -1.1914 0.5694, 0.08320, -1.1952 0.5112, 0.09370, -1.2547 0.4731, 0.09830, -1.2417 0.4349, 0.10070, -1.2681 0.3960, 0.10120, -1.4154 0.3566, 0.10020, -1.2502 0.3172, 0.09790, -1.2662 0.2778, 0.09440, -1.2635 0.2393, 0.08960, -1.2683 0.2056, 0.08360, -1.3920 0.1633, 0.07610, -1.2075 0.1261, 0.06710, -1.2841 0.0900, 0.05640, -1.1919 0.0571, 0.04390, -1.2106 0.0283, 0.02940, -1.2088 0.0142, 0.01970, -1.2165 0.0081, 0.01410, -1.3391 0.0026, 0.00780, -1.0920 0.0000, 0.00000, -1.1701 0.0037, -0.00840, -1.2454 0.0112, -0.01420, -0.4322 0.0191, -0.01930, 0.0553 0.0397, -0.03030, 0.5854 0.0706, -0.04420, 0.8053 0.1037, -0.05710, 0.9262 0.1384, -0.06890, 1.1069 0.1741, -0.07950, 1.0779 0.2102, -0.08660, 0.9029 0.2472, -0.09640, 0.9073 0.2844, -0.10270, 0.7443 0.3225, -0.10690, 0.7406 0.3608, -0.10890, 0.4932 0.3991, -0.10830, 0.3821 0.4373, -0.10510, 0.1346 0.4757, -0.09890, -0.0374 0.5137, -0.09070, -0.2109 0.5694, -0.07640, -0.3842 15 Flap element taps 1.0000, 0.00130, -1.2605 0.9365, 0.01390, -1.2537 0.8333, 0.03280, -1.2437 0.7436, 0.04930, -1.2320 0.7049, 0.05670, -1.2335 0.6662, 0.06410, -1.2050 0.6522, 0.01390, -1.7147 0.5969, -0.00020, -1.6998 0.6000, -0.03020, -1.7461 0.6324, -0.04540, -2.8259 0.6667, -0.04880, -2.9144 0.7046, -0.04110, -1.6453 0.7429, -0.03210, -1.3040 0.8333, -0.01400, -0.9443 0.9311, -0.00120, -0.7498 --------- Run Conditions: vel=106.8 ft/s Re=1.012x10^6 AOA=70.01 Flap deflection=-45.00 Totals: Cl=0.4395 Cdp=1.2246 Cm(c/4)=-0.1433 Cs=-0.0056 Ch=-0.2182 Main component: Cl=0.3405 Cdp=1.1692 Cm=-0.3730 Flap component: Cl=0.0990 Cdp=0.0554 Cm=-0.0955 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3289 0.6175, -0.04610, -1.1795 0.5841, -0.02440, -1.1507 0.5775, 0.01750, -1.2147 0.5777, 0.04660, -1.2072 0.6274, 0.07170, -1.3432 0.5694, 0.08320, -1.3904 0.5112, 0.09370, -1.4033 0.4731, 0.09830, -1.3207 0.4349, 0.10070, -1.3926 0.3960, 0.10120, -1.4619 0.3566, 0.10020, -1.4615 0.3172, 0.09790, -1.4524 0.2778, 0.09440, -1.4595 0.2393, 0.08960, -1.4496 0.2056, 0.08360, -1.4439 0.1633, 0.07610, -1.4396 0.1261, 0.06710, -1.4234 0.0900, 0.05640, -1.4054 0.0571, 0.04390, -1.3856 0.0283, 0.02940, -1.3811 0.0142, 0.01970, -1.3744 0.0081, 0.01410, -1.3778 0.0026, 0.00780, -1.3117 0.0000, 0.00000, -1.3673 0.0037, -0.00840, -1.5422 0.0112, -0.01420, -0.9850 0.0191, -0.01930, -0.4913 0.0397, -0.03030, 0.1400 0.0706, -0.04420, 0.5335 0.1037, -0.05710, 0.7565 0.1384, -0.06890, 0.8926 0.1741, -0.07950, 0.9692 0.2102, -0.08660, 1.0069 0.2472, -0.09640, 1.0075 0.2844, -0.10270, 0.9813 0.3225, -0.10690, 0.9324 0.3608, -0.10890, 0.8417 0.3991, -0.10830, 0.7273 0.4373, -0.10510, 0.5815 0.4757, -0.09890, 0.4528 0.5137, -0.09070, 0.2275 0.5694, -0.07640, 0.0625 15 Flap element taps 1.0000, 0.00130, -1.4256 0.9365, 0.01390, -1.4428 0.8333, 0.03280, -1.3307 0.7436, 0.04930, -1.3098 0.7049, 0.05670, -1.2781 0.6662, 0.06410, -1.3188 0.6522, 0.01390, -1.1916 0.5969, -0.00020, -0.9100 0.6000, -0.03020, -0.3517 0.6324, -0.04540, -2.0680 0.6667, -0.04880, -2.3807 0.7046, -0.04110, -1.2369 0.7429, -0.03210, -0.7956 0.8333, -0.01400, -0.5975 0.9311, -0.00120, -0.5909 --------- Run Conditions: vel=106.8 ft/s Re=1.011x10^6 AOA=80.00 Flap deflection=-45.00 Totals: Cl=0.4655 Cdp=1.5202 Cm(c/4)=-0.2623 Cs=0.1945 Ch=-0.3356 Main component: Cl=0.2673 Cdp=1.3173 Cm=-0.4409 Flap component: Cl=0.1982 Cdp=0.2029 Cm=-0.2159 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.1102 0.6175, -0.04610, -0.7511 0.5841, -0.02440, -0.6390 0.5775, 0.01750, -0.6509 0.5777, 0.04660, -0.6334 0.6274, 0.07170, -1.5284 0.5694, 0.08320, -1.5799 0.5112, 0.09370, -1.6135 0.4731, 0.09830, -1.6163 0.4349, 0.10070, -1.6179 0.3960, 0.10120, -1.6179 0.3566, 0.10020, -1.6234 0.3172, 0.09790, -1.6140 0.2778, 0.09440, -1.6213 0.2393, 0.08960, -1.6120 0.2056, 0.08360, -1.6035 0.1633, 0.07610, -1.5994 0.1261, 0.06710, -1.5790 0.0900, 0.05640, -1.5674 0.0571, 0.04390, -1.5429 0.0283, 0.02940, -1.5353 0.0142, 0.01970, -1.5271 0.0081, 0.01410, -1.5290 0.0026, 0.00780, -1.4603 0.0000, 0.00000, -1.5233 0.0037, -0.00840, -1.5838 0.0112, -0.01420, -1.4073 0.0191, -0.01930, -0.9555 0.0397, -0.03030, -0.2937 0.0706, -0.04420, 0.1695 0.1037, -0.05710, 0.4552 0.1384, -0.06890, 0.6507 0.1741, -0.07950, 0.7913 0.2102, -0.08660, 0.8962 0.2472, -0.09640, 0.9573 0.2844, -0.10270, 0.9985 0.3225, -0.10690, 1.0106 0.3608, -0.10890, 0.9920 0.3991, -0.10830, 0.9410 0.4373, -0.10510, 0.8557 0.4757, -0.09890, 0.7679 0.5137, -0.09070, 0.6339 0.5694, -0.07640, 0.4504 15 Flap element taps 1.0000, 0.00130, -1.5889 0.9365, 0.01390, -1.5902 0.8333, 0.03280, -1.5650 0.7436, 0.04930, -1.5396 0.7049, 0.05670, -1.5214 0.6662, 0.06410, -1.4899 0.6522, 0.01390, -0.6711 0.5969, -0.00020, -0.6781 0.6000, -0.03020, 0.5122 0.6324, -0.04540, -1.3023 0.6667, -0.04880, -1.6181 0.7046, -0.04110, -0.6983 0.7429, -0.03210, -0.5256 0.8333, -0.01400, -0.4125 0.9311, -0.00120, -0.5568 --------- Run Conditions: vel=105.9 ft/s Re=1.001x10^6 AOA=90.04 Flap deflection=-45.00 Totals: Cl=0.3760 Cdp=1.6941 Cm(c/4)=-0.3476 Cs=0.3772 Ch=-0.4434 Main component: Cl=0.1559 Cdp=1.3516 Cm=-0.4640 Flap component: Cl=0.2201 Cdp=0.3425 Cm=-0.3071 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.5266 0.6175, -0.04610, -0.1077 0.5841, -0.02440, -0.0823 0.5775, 0.01750, -0.0361 0.5777, 0.04660, 0.0180 0.6274, 0.07170, -1.6224 0.5694, 0.08320, -1.6717 0.5112, 0.09370, -1.6784 0.4731, 0.09830, -1.6840 0.4349, 0.10070, -1.6884 0.3960, 0.10120, -1.6753 0.3566, 0.10020, -1.7051 0.3172, 0.09790, -1.6961 0.2778, 0.09440, -1.7068 0.2393, 0.08960, -1.7022 0.2056, 0.08360, -1.6836 0.1633, 0.07610, -1.7076 0.1261, 0.06710, -1.6847 0.0900, 0.05640, -1.6809 0.0571, 0.04390, -1.6541 0.0283, 0.02940, -1.6398 0.0142, 0.01970, -1.6254 0.0081, 0.01410, -1.6129 0.0026, 0.00780, -1.5474 0.0000, 0.00000, -1.6140 0.0037, -0.00840, -1.6285 0.0112, -0.01420, -1.6810 0.0191, -0.01930, -1.3340 0.0397, -0.03030, -0.7136 0.0706, -0.04420, -0.2291 0.1037, -0.05710, 0.0889 0.1384, -0.06890, 0.3114 0.1741, -0.07950, 0.5001 0.2102, -0.08660, 0.6677 0.2472, -0.09640, 0.7723 0.2844, -0.10270, 0.8788 0.3225, -0.10690, 0.9385 0.3608, -0.10890, 0.9986 0.3991, -0.10830, 1.0064 0.4373, -0.10510, 0.9956 0.4757, -0.09890, 0.9664 0.5137, -0.09070, 0.8895 0.5694, -0.07640, 0.7587 15 Flap element taps 1.0000, 0.00130, -1.6795 0.9365, 0.01390, -1.6810 0.8333, 0.03280, -1.6806 0.7436, 0.04930, -1.6558 0.7049, 0.05670, -1.6432 0.6662, 0.06410, -1.6100 0.6522, 0.01390, -0.0991 0.5969, -0.00020, -0.0946 0.6000, -0.03020, 0.6650 0.6324, -0.04540, -0.4941 0.6667, -0.04880, -0.8141 0.7046, -0.04110, -0.5633 0.7429, -0.03210, -0.1637 0.8333, -0.01400, -0.1786 0.9311, -0.00120, -0.4218 --------- Run Conditions: vel=105.7 ft/s Re=0.999x10^6 AOA=120.06 Flap deflection=-45.00 Totals: Cl=-0.0839 Cdp=1.6850 Cm(c/4)=-0.4907 Cs=0.7714 Ch=-0.6903 Main component: Cl=-0.1438 Cdp=0.9880 Cm=-0.3581 Flap component: Cl=0.0599 Cdp=0.6971 Cm=-0.5077 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.9696 0.6175, -0.04610, 0.9837 0.5841, -0.02440, 0.9991 0.5775, 0.01750, 0.9838 0.5777, 0.04660, 0.9883 0.6274, 0.07170, -1.6631 0.5694, 0.08320, -1.7076 0.5112, 0.09370, -1.7327 0.4731, 0.09830, -1.7523 0.4349, 0.10070, -1.7408 0.3960, 0.10120, -1.7133 0.3566, 0.10020, -1.7440 0.3172, 0.09790, -1.7273 0.2778, 0.09440, -1.7417 0.2393, 0.08960, -1.7364 0.2056, 0.08360, -1.7119 0.1633, 0.07610, -1.7483 0.1261, 0.06710, -1.7343 0.0900, 0.05640, -1.7365 0.0571, 0.04390, -1.7135 0.0283, 0.02940, -1.6795 0.0142, 0.01970, -1.6517 0.0081, 0.01410, -1.6251 0.0026, 0.00780, -1.5642 0.0000, 0.00000, -1.6325 0.0037, -0.00840, -1.6198 0.0112, -0.01420, -1.6451 0.0191, -0.01930, -1.7253 0.0397, -0.03030, -1.5518 0.0706, -0.04420, -1.2720 0.1037, -0.05710, -1.0524 0.1384, -0.06890, -0.8757 0.1741, -0.07950, -0.6910 0.2102, -0.08660, -0.4981 0.2472, -0.09640, -0.3725 0.2844, -0.10270, -0.1860 0.3225, -0.10690, -0.0376 0.3608, -0.10890, 0.1431 0.3991, -0.10830, 0.3044 0.4373, -0.10510, 0.4729 0.4757, -0.09890, 0.6472 0.5137, -0.09070, 0.7556 0.5694, -0.07640, 0.8915 15 Flap element taps 1.0000, 0.00130, -1.6514 0.9365, 0.01390, -1.6742 0.8333, 0.03280, -1.6928 0.7436, 0.04930, -1.6734 0.7049, 0.05670, -1.6562 0.6662, 0.06410, -1.6257 0.6522, 0.01390, 0.9941 0.5969, -0.00020, 0.9839 0.6000, -0.03020, 1.0026 0.6324, -0.04540, 0.9769 0.6667, -0.04880, 0.8743 0.7046, -0.04110, 0.8131 0.7429, -0.03210, 0.7647 0.8333, -0.01400, 0.5911 0.9311, -0.00120, 0.2236 --------- Run Conditions: vel=100.8 ft/s Re=1.002x10^6 AOA=150.02 Flap deflection=-45.00 Totals: Cl=-0.1366 Cdp=0.9169 Cm(c/4)=-0.3813 Cs=0.7259 Ch=-0.6658 Main component: Cl=0.0694 Cdp=0.2917 Cm=-0.0732 Flap component: Cl=-0.2061 Cdp=0.6252 Cm=-0.4522 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0872 0.6175, -0.04610, 0.4382 0.5841, -0.02440, 0.4464 0.5775, 0.01750, 0.3762 0.5777, 0.04660, 0.4460 0.6274, 0.07170, -1.2690 0.5694, 0.08320, -1.2915 0.5112, 0.09370, -1.3192 0.4731, 0.09830, -1.3199 0.4349, 0.10070, -1.3257 0.3960, 0.10120, -1.3304 0.3566, 0.10020, -1.3268 0.3172, 0.09790, -1.3278 0.2778, 0.09440, -1.3357 0.2393, 0.08960, -1.3250 0.2056, 0.08360, -1.3244 0.1633, 0.07610, -1.3331 0.1261, 0.06710, -1.3301 0.0900, 0.05640, -1.3462 0.0571, 0.04390, -1.3429 0.0283, 0.02940, -1.2993 0.0142, 0.01970, -1.2809 0.0081, 0.01410, -1.2623 0.0026, 0.00780, -1.1470 0.0000, 0.00000, -1.2589 0.0037, -0.00840, -1.3435 0.0112, -0.01420, -1.6996 0.0191, -0.01930, -1.8239 0.0397, -0.03030, -1.8129 0.0706, -0.04420, -1.7409 0.1037, -0.05710, -1.6898 0.1384, -0.06890, -1.6465 0.1741, -0.07950, -1.5967 0.2102, -0.08660, -1.5328 0.2472, -0.09640, -1.5175 0.2844, -0.10270, -1.4178 0.3225, -0.10690, -1.3366 0.3608, -0.10890, -1.2329 0.3991, -0.10830, -1.0641 0.4373, -0.10510, -0.8429 0.4757, -0.09890, -0.5882 0.5137, -0.09070, -0.3716 0.5694, -0.07640, -0.0595 15 Flap element taps 1.0000, 0.00130, -1.2268 0.9365, 0.01390, -1.2539 0.8333, 0.03280, -1.2720 0.7436, 0.04930, -1.2593 0.7049, 0.05670, -1.2575 0.6662, 0.06410, -1.2460 0.6522, 0.01390, 0.4311 0.5969, -0.00020, 0.3191 0.6000, -0.03020, 0.3267 0.6324, -0.04540, 0.2962 0.6667, -0.04880, 0.6033 0.7046, -0.04110, 0.8872 0.7429, -0.03210, 0.9644 0.8333, -0.01400, 0.9836 0.9311, -0.00120, 0.8204 --------- Run Conditions: vel=106.8 ft/s Re=1.014x10^6 AOA=180.08 Flap deflection=-45.00 Totals: Cl=0.1788 Cdp=0.1577 Cm(c/4)=-0.0615 Cs=0.1575 Ch=-0.3250 Main component: Cl=0.2906 Cdp=-0.1069 Cm=0.1235 Flap component: Cl=-0.1118 Cdp=0.2646 Cm=-0.1403 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.4102 0.6175, -0.04610, -1.1560 0.5841, -0.02440, -1.1544 0.5775, 0.01750, -1.1626 0.5777, 0.04660, -1.1531 0.6274, 0.07170, -0.5014 0.5694, 0.08320, -0.5145 0.5112, 0.09370, -0.5195 0.4731, 0.09830, -0.5175 0.4349, 0.10070, -0.5218 0.3960, 0.10120, -0.5313 0.3566, 0.10020, -0.5364 0.3172, 0.09790, -0.5343 0.2778, 0.09440, -0.5490 0.2393, 0.08960, -0.5471 0.2056, 0.08360, -0.5570 0.1633, 0.07610, -0.5596 0.1261, 0.06710, -0.5630 0.0900, 0.05640, -0.5548 0.0571, 0.04390, -0.5371 0.0283, 0.02940, -0.5132 0.0142, 0.01970, -0.4897 0.0081, 0.01410, -0.4832 0.0026, 0.00780, -0.4332 0.0000, 0.00000, -0.4679 0.0037, -0.00840, -0.4880 0.0112, -0.01420, -0.4765 0.0191, -0.01930, -0.4655 0.0397, -0.03030, -0.4578 0.0706, -0.04420, -0.4552 0.1037, -0.05710, -0.4633 0.1384, -0.06890, -0.5035 0.1741, -0.07950, -0.5940 0.2102, -0.08660, -0.7451 0.2472, -0.09640, -0.9516 0.2844, -0.10270, -1.1324 0.3225, -0.10690, -1.2882 0.3608, -0.10890, -1.4352 0.3991, -0.10830, -1.4919 0.4373, -0.10510, -1.5006 0.4757, -0.09890, -1.3902 0.5137, -0.09070, -1.3206 0.5694, -0.07640, -1.1890 15 Flap element taps 1.0000, 0.00130, -0.4888 0.9365, 0.01390, -0.4849 0.8333, 0.03280, -0.4922 0.7436, 0.04930, -0.4969 0.7049, 0.05670, -0.4963 0.6662, 0.06410, -0.5003 0.6522, 0.01390, -1.1502 0.5969, -0.00020, -1.2154 0.6000, -0.03020, -1.3560 0.6324, -0.04540, -1.5063 0.6667, -0.04880, -1.2405 0.7046, -0.04110, -0.1026 0.7429, -0.03210, 0.3062 0.8333, -0.01400, 0.7057 0.9311, -0.00120, 0.9655 --------- Run Conditions: vel=104.9 ft/s Re=0.997x10^6 AOA=210.10 Flap deflection=-45.00 Totals: Cl=0.4495 Cdp=0.1467 Cm(c/4)=0.2122 Cs=-0.0985 Ch=0.1771 Main component: Cl=0.1278 Cdp=0.1719 Cm=0.1159 Flap component: Cl=0.3217 Cdp=-0.0252 Cm=0.2119 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6408 0.6175, -0.04610, -0.4246 0.5841, -0.02440, -0.4156 0.5775, 0.01750, -0.4246 0.5777, 0.04660, -0.4172 0.6274, 0.07170, 0.7777 0.5694, 0.08320, 0.7079 0.5112, 0.09370, 0.4534 0.4731, 0.09830, 0.2754 0.4349, 0.10070, 0.1299 0.3960, 0.10120, 0.0117 0.3566, 0.10020, -0.0837 0.3172, 0.09790, -0.1780 0.2778, 0.09440, -0.3103 0.2393, 0.08960, -0.4299 0.2056, 0.08360, -0.5817 0.1633, 0.07610, -0.6965 0.1261, 0.06710, -0.8349 0.0900, 0.05640, -0.9784 0.0571, 0.04390, -1.1350 0.0283, 0.02940, -1.1582 0.0142, 0.01970, -0.9048 0.0081, 0.01410, -0.6882 0.0026, 0.00780, -0.5038 0.0000, 0.00000, -0.5257 0.0037, -0.00840, -0.5286 0.0112, -0.01420, -0.5231 0.0191, -0.01930, -0.5172 0.0397, -0.03030, -0.5290 0.0706, -0.04420, -0.5460 0.1037, -0.05710, -0.5513 0.1384, -0.06890, -0.5415 0.1741, -0.07950, -0.5489 0.2102, -0.08660, -0.5614 0.2472, -0.09640, -0.5660 0.2844, -0.10270, -0.5708 0.3225, -0.10690, -0.5471 0.3608, -0.10890, -0.5629 0.3991, -0.10830, -0.5494 0.4373, -0.10510, -0.5651 0.4757, -0.09890, -0.5663 0.5137, -0.09070, -0.5920 0.5694, -0.07640, -0.5993 15 Flap element taps 1.0000, 0.00130, 1.0033 0.9365, 0.01390, 0.4623 0.8333, 0.03280, 0.5620 0.7436, 0.04930, 0.7137 0.7049, 0.05670, 0.7611 0.6662, 0.06410, 0.7652 0.6522, 0.01390, -0.4136 0.5969, -0.00020, -0.4306 0.6000, -0.03020, -0.4704 0.6324, -0.04540, -1.6389 0.6667, -0.04880, -1.8202 0.7046, -0.04110, -0.7494 0.7429, -0.03210, -0.3558 0.8333, -0.01400, -0.0019 0.9311, -0.00120, 0.2743 --------- Run Conditions: vel=106.2 ft/s Re=1.008x10^6 AOA=240.03 Flap deflection=-45.00 Totals: Cl=1.2502 Cdp=1.2370 Cm(c/4)=0.5400 Cs=-0.4651 Ch=0.8052 Main component: Cl=0.5114 Cdp=0.9521 Cm=0.4045 Flap component: Cl=0.7388 Cdp=0.2849 Cm=0.5595 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.6867 0.6175, -0.04610, -1.5730 0.5841, -0.02440, -1.5661 0.5775, 0.01750, -1.5751 0.5777, 0.04660, -1.5696 0.6274, 0.07170, 0.9815 0.5694, 0.08320, 0.9206 0.5112, 0.09370, 0.8091 0.4731, 0.09830, 0.7275 0.4349, 0.10070, 0.6350 0.3960, 0.10120, 0.5212 0.3566, 0.10020, 0.4513 0.3172, 0.09790, 0.3452 0.2778, 0.09440, 0.1998 0.2393, 0.08960, 0.0491 0.2056, 0.08360, -0.1640 0.1633, 0.07610, -0.3389 0.1261, 0.06710, -0.5931 0.0900, 0.05640, -0.8821 0.0571, 0.04390, -1.2688 0.0283, 0.02940, -1.5626 0.0142, 0.01970, -1.5007 0.0081, 0.01410, -1.5061 0.0026, 0.00780, -1.4250 0.0000, 0.00000, -1.4769 0.0037, -0.00840, -1.4949 0.0112, -0.01420, -1.5062 0.0191, -0.01930, -1.5177 0.0397, -0.03030, -1.5718 0.0706, -0.04420, -1.6641 0.1037, -0.05710, -1.7098 0.1384, -0.06890, -1.6853 0.1741, -0.07950, -1.6862 0.2102, -0.08660, -1.7169 0.2472, -0.09640, -1.7399 0.2844, -0.10270, -1.7776 0.3225, -0.10690, -1.7728 0.3608, -0.10890, -1.8316 0.3991, -0.10830, -1.8261 0.4373, -0.10510, -1.8346 0.4757, -0.09890, -1.7908 0.5137, -0.09070, -1.7788 0.5694, -0.07640, -1.7091 15 Flap element taps 1.0000, 0.00130, -1.5089 0.9365, 0.01390, 1.0116 0.8333, 0.03280, 0.9606 0.7436, 0.04930, 0.9497 0.7049, 0.05670, 0.9562 0.6662, 0.06410, 0.9682 0.6522, 0.01390, -1.5540 0.5969, -0.00020, -1.6262 0.6000, -0.03020, -1.6447 0.6324, -0.04540, -1.6526 0.6667, -0.04880, -1.6320 0.7046, -0.04110, -1.6148 0.7429, -0.03210, -1.5960 0.8333, -0.01400, -1.5456 0.9311, -0.00120, -1.5147 --------- Run Conditions: vel=103.7 ft/s Re=0.982x10^6 AOA=269.07 Flap deflection=-45.00 Totals: Cl=0.6426 Cdp=2.1599 Cm(c/4)=0.6161 Cs=-0.6074 Ch=0.9083 Main component: Cl=0.0525 Cdp=1.4521 Cm=0.5118 Flap component: Cl=0.5900 Cdp=0.7078 Cm=0.6468 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -2.0595 0.6175, -0.04610, -1.9957 0.5841, -0.02440, -1.9686 0.5775, 0.01750, -1.9636 0.5777, 0.04660, -1.9557 0.6274, 0.07170, 1.0071 0.5694, 0.08320, 1.0087 0.5112, 0.09370, 0.9856 0.4731, 0.09830, 0.9761 0.4349, 0.10070, 0.9502 0.3960, 0.10120, 0.8692 0.3566, 0.10020, 0.8752 0.3172, 0.09790, 0.8139 0.2778, 0.09440, 0.7262 0.2393, 0.08960, 0.6176 0.2056, 0.08360, 0.4266 0.1633, 0.07610, 0.2994 0.1261, 0.06710, 0.0287 0.0900, 0.05640, -0.2857 0.0571, 0.04390, -0.8073 0.0283, 0.02940, -1.4745 0.0142, 0.01970, -1.8603 0.0081, 0.01410, -1.8435 0.0026, 0.00780, -1.6421 0.0000, 0.00000, -1.6934 0.0037, -0.00840, -1.7139 0.0112, -0.01420, -1.7373 0.0191, -0.01930, -1.7475 0.0397, -0.03030, -1.7790 0.0706, -0.04420, -1.8388 0.1037, -0.05710, -1.8889 0.1384, -0.06890, -1.9081 0.1741, -0.07950, -1.9662 0.2102, -0.08660, -2.0516 0.2472, -0.09640, -2.0528 0.2844, -0.10270, -2.0588 0.3225, -0.10690, -1.9991 0.3608, -0.10890, -2.0338 0.3991, -0.10830, -2.0031 0.4373, -0.10510, -2.0290 0.4757, -0.09890, -2.0330 0.5137, -0.09070, -2.0616 0.5694, -0.07640, -2.0165 15 Flap element taps 1.0000, 0.00130, -1.7814 0.9365, 0.01390, 0.8136 0.8333, 0.03280, 0.9829 0.7436, 0.04930, 0.9988 0.7049, 0.05670, 1.0037 0.6662, 0.06410, 1.0031 0.6522, 0.01390, -1.9940 0.5969, -0.00020, -2.0520 0.6000, -0.03020, -2.1292 0.6324, -0.04540, -2.2161 0.6667, -0.04880, -2.1923 0.7046, -0.04110, -2.0948 0.7429, -0.03210, -2.0532 0.8333, -0.01400, -1.9716 0.9311, -0.00120, -1.8448