S809 UNVENTED AILERON, CLEAN, CHORD = 18 IN --------- Run Conditions: vel=109.4 ft/s Re=1.002x10^6 AOA=-6.01 Flap deflection=-30.00 Totals: Cl=-1.2279 Cdp=0.1613 Cm(c/4)=0.1382 Cs=-0.0318 Ch=0.2248 Main component: Cl=-1.0120 Cdp=0.0214 Cm=0.2554 Flap component: Cl=-0.2159 Cdp=0.1398 Cm=0.1922 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4950 0.6175, -0.04610, -0.4422 0.5841, -0.02440, -0.4381 0.5775, 0.01750, -0.4546 0.5777, 0.04660, -0.4489 0.6274, 0.07170, 0.6491 0.5694, 0.08320, 0.5132 0.5112, 0.09370, 0.2577 0.4731, 0.09830, 0.2518 0.4349, 0.10070, 0.1991 0.3960, 0.10120, 0.1846 0.3566, 0.10020, 0.2232 0.3172, 0.09790, 0.2587 0.2778, 0.09440, 0.2774 0.2393, 0.08960, 0.3224 0.2056, 0.08360, 0.3582 0.1633, 0.07610, 0.4670 0.1261, 0.06710, 0.5690 0.0900, 0.05640, 0.7116 0.0571, 0.04390, 0.8786 0.0283, 0.02940, 1.0157 0.0142, 0.01970, 0.9499 0.0081, 0.01410, 0.7107 0.0026, 0.00780, -0.1173 0.0000, 0.00000, -3.0425 0.0037, -0.00840, -3.6916 0.0112, -0.01420, -3.3178 0.0191, -0.01930, -1.8290 0.0397, -0.03030, -1.6258 0.0706, -0.04420, -1.4584 0.1037, -0.05710, -1.4214 0.1384, -0.06890, -1.4029 0.1741, -0.07950, -1.4033 0.2102, -0.08660, -1.4602 0.2472, -0.09640, -1.5058 0.2844, -0.10270, -1.5030 0.3225, -0.10690, -1.4597 0.3608, -0.10890, -1.4017 0.3991, -0.10830, -1.2447 0.4373, -0.10510, -1.0150 0.4757, -0.09890, -0.7197 0.5137, -0.09070, -0.5688 0.5694, -0.07640, -0.5010 15 Flap element taps 1.0000, 0.00130, -0.4736 0.9365, 0.01390, 0.0160 0.8333, 0.03280, 0.2905 0.7436, 0.04930, 0.4965 0.7049, 0.05670, 0.6170 0.6662, 0.06410, 0.6943 0.6522, 0.01390, -0.4471 0.5969, -0.00020, -0.4551 0.6000, -0.03020, -0.4732 0.6324, -0.04540, -0.4771 0.6667, -0.04880, -0.4770 0.7046, -0.04110, -0.4854 0.7429, -0.03210, -0.4902 0.8333, -0.01400, -0.4987 0.9311, -0.00120, -0.4920 --------- Run Conditions: vel=109.6 ft/s Re=1.005x10^6 AOA=0.02 Flap deflection=-30.00 Totals: Cl=-1.1700 Cdp=0.1032 Cm(c/4)=0.1714 Cs=-0.1036 Ch=0.2136 Main component: Cl=-0.9526 Cdp=-0.0066 Cm=0.2816 Flap component: Cl=-0.2174 Cdp=0.1098 Cm=0.1823 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5688 0.6175, -0.04610, -0.3866 0.5841, -0.02440, -0.3832 0.5775, 0.01750, -0.4012 0.5777, 0.04660, -0.3934 0.6274, 0.07170, 0.6422 0.5694, 0.08320, 0.5094 0.5112, 0.09370, 0.1671 0.4731, 0.09830, 0.1634 0.4349, 0.10070, 0.1149 0.3960, 0.10120, 0.0608 0.3566, 0.10020, 0.1083 0.3172, 0.09790, 0.1215 0.2778, 0.09440, 0.1191 0.2393, 0.08960, 0.1434 0.2056, 0.08360, 0.1427 0.1633, 0.07610, 0.2525 0.1261, 0.06710, 0.3284 0.0900, 0.05640, 0.4677 0.0571, 0.04390, 0.6428 0.0283, 0.02940, 0.8744 0.0142, 0.01970, 0.9993 0.0081, 0.01410, 0.9689 0.0026, 0.00780, 0.6459 0.0000, 0.00000, -0.6541 0.0037, -0.00840, -1.7052 0.0112, -0.01420, -1.4270 0.0191, -0.01930, -1.2161 0.0397, -0.03030, -0.9988 0.0706, -0.04420, -0.9960 0.1037, -0.05710, -1.0702 0.1384, -0.06890, -1.1180 0.1741, -0.07950, -1.2107 0.2102, -0.08660, -1.3569 0.2472, -0.09640, -1.4696 0.2844, -0.10270, -1.5590 0.3225, -0.10690, -1.6030 0.3608, -0.10890, -1.6601 0.3991, -0.10830, -1.6281 0.4373, -0.10510, -1.5378 0.4757, -0.09890, -1.4609 0.5137, -0.09070, -1.0939 0.5694, -0.07640, -0.7546 15 Flap element taps 1.0000, 0.00130, -0.4189 0.9365, 0.01390, 0.0400 0.8333, 0.03280, 0.2883 0.7436, 0.04930, 0.4811 0.7049, 0.05670, 0.5988 0.6662, 0.06410, 0.6831 0.6522, 0.01390, -0.3961 0.5969, -0.00020, -0.4091 0.6000, -0.03020, -0.4537 0.6324, -0.04540, -0.4497 0.6667, -0.04880, -0.4239 0.7046, -0.04110, -0.4240 0.7429, -0.03210, -0.4328 0.8333, -0.01400, -0.4538 0.9311, -0.00120, -0.4583 --------- Run Conditions: vel=110.1 ft/s Re=1.011x10^6 AOA=3.06 Flap deflection=-30.00 Totals: Cl=-0.9071 Cdp=0.0892 Cm(c/4)=0.1692 Cs=-0.1375 Ch=0.1904 Main component: Cl=-0.7043 Cdp=0.0006 Cm=0.2292 Flap component: Cl=-0.2029 Cdp=0.0886 Cm=0.1652 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5244 0.6175, -0.04610, -0.3634 0.5841, -0.02440, -0.3617 0.5775, 0.01750, -0.3800 0.5777, 0.04660, -0.3711 0.6274, 0.07170, 0.6206 0.5694, 0.08320, 0.4720 0.5112, 0.09370, 0.0608 0.4731, 0.09830, 0.0557 0.4349, 0.10070, 0.0114 0.3960, 0.10120, -0.0637 0.3566, 0.10020, -0.0116 0.3172, 0.09790, -0.0144 0.2778, 0.09440, -0.0316 0.2393, 0.08960, -0.0272 0.2056, 0.08360, -0.0564 0.1633, 0.07610, 0.0492 0.1261, 0.06710, 0.0962 0.0900, 0.05640, 0.2206 0.0571, 0.04390, 0.3722 0.0283, 0.02940, 0.6136 0.0142, 0.01970, 0.8252 0.0081, 0.01410, 0.9009 0.0026, 0.00780, 0.9595 0.0000, 0.00000, 0.5606 0.0037, -0.00840, -0.3406 0.0112, -0.01420, -0.4257 0.0191, -0.01930, -0.4033 0.0397, -0.03030, -0.4161 0.0706, -0.04420, -0.5468 0.1037, -0.05710, -0.6786 0.1384, -0.06890, -0.7555 0.1741, -0.07950, -0.8801 0.2102, -0.08660, -1.0637 0.2472, -0.09640, -1.1875 0.2844, -0.10270, -1.3031 0.3225, -0.10690, -1.3599 0.3608, -0.10890, -1.4481 0.3991, -0.10830, -1.4411 0.4373, -0.10510, -1.3821 0.4757, -0.09890, -1.2957 0.5137, -0.09070, -1.2725 0.5694, -0.07640, -0.6728 15 Flap element taps 1.0000, 0.00130, -0.3755 0.9365, 0.01390, 0.0258 0.8333, 0.03280, 0.2588 0.7436, 0.04930, 0.4512 0.7049, 0.05670, 0.5742 0.6662, 0.06410, 0.6725 0.6522, 0.01390, -0.3812 0.5969, -0.00020, -0.3809 0.6000, -0.03020, -0.4278 0.6324, -0.04540, -0.4218 0.6667, -0.04880, -0.3953 0.7046, -0.04110, -0.3874 0.7429, -0.03210, -0.3958 0.8333, -0.01400, -0.4022 0.9311, -0.00120, -0.3972 --------- Run Conditions: vel=109.0 ft/s Re=1.003x10^6 AOA=6.04 Flap deflection=-30.00 Totals: Cl=-0.6426 Cdp=0.0825 Cm(c/4)=0.1720 Cs=-0.1496 Ch=0.1810 Main component: Cl=-0.4444 Cdp=0.0080 Cm=0.1717 Flap component: Cl=-0.1982 Cdp=0.0745 Cm=0.1579 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4928 0.6175, -0.04610, -0.3594 0.5841, -0.02440, -0.3596 0.5775, 0.01750, -0.3775 0.5777, 0.04660, -0.3668 0.6274, 0.07170, 0.5915 0.5694, 0.08320, 0.4246 0.5112, 0.09370, 0.1700 0.4731, 0.09830, -0.0659 0.4349, 0.10070, -0.1076 0.3960, 0.10120, -0.1973 0.3566, 0.10020, -0.1405 0.3172, 0.09790, -0.1594 0.2778, 0.09440, -0.1946 0.2393, 0.08960, -0.2104 0.2056, 0.08360, -0.2734 0.1633, 0.07610, -0.1773 0.1261, 0.06710, -0.1672 0.0900, 0.05640, -0.0767 0.0571, 0.04390, 0.0254 0.0283, 0.02940, 0.2165 0.0142, 0.01970, 0.4313 0.0081, 0.01410, 0.5476 0.0026, 0.00780, 0.8398 0.0000, 0.00000, 1.0300 0.0037, -0.00840, 0.5761 0.0112, -0.01420, 0.3263 0.0191, -0.01930, 0.2351 0.0397, -0.03030, 0.0780 0.0706, -0.04420, -0.1412 0.1037, -0.05710, -0.3154 0.1384, -0.06890, -0.4102 0.1741, -0.07950, -0.5624 0.2102, -0.08660, -0.7756 0.2472, -0.09640, -0.9081 0.2844, -0.10270, -1.0492 0.3225, -0.10690, -1.1158 0.3608, -0.10890, -1.2312 0.3991, -0.10830, -1.2472 0.4373, -0.10510, -1.2263 0.4757, -0.09890, -1.1260 0.5137, -0.09070, -1.0842 0.5694, -0.07640, -0.6013 15 Flap element taps 1.0000, 0.00130, -0.3620 0.9365, 0.01390, 0.0096 0.8333, 0.03280, 0.2296 0.7436, 0.04930, 0.4214 0.7049, 0.05670, 0.5492 0.6662, 0.06410, 0.6422 0.6522, 0.01390, -0.3812 0.5969, -0.00020, -0.3754 0.6000, -0.03020, -0.4245 0.6324, -0.04540, -0.4227 0.6667, -0.04880, -0.3921 0.7046, -0.04110, -0.3789 0.7429, -0.03210, -0.3918 0.8333, -0.01400, -0.3976 0.9311, -0.00120, -0.3888 --------- Run Conditions: vel=109.1 ft/s Re=1.007x10^6 AOA=9.02 Flap deflection=-30.00 Totals: Cl=-0.3716 Cdp=0.0764 Cm(c/4)=0.1721 Cs=-0.1338 Ch=0.1713 Main component: Cl=-0.1810 Cdp=0.0187 Cm=0.1116 Flap component: Cl=-0.1907 Cdp=0.0578 Cm=0.1493 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4595 0.6175, -0.04610, -0.3619 0.5841, -0.02440, -0.3669 0.5775, 0.01750, -0.3829 0.5777, 0.04660, -0.3714 0.6274, 0.07170, 0.5274 0.5694, 0.08320, 0.3879 0.5112, 0.09370, 0.1091 0.4731, 0.09830, -0.0817 0.4349, 0.10070, -0.2374 0.3960, 0.10120, -0.3390 0.3566, 0.10020, -0.2785 0.3172, 0.09790, -0.3103 0.2778, 0.09440, -0.3639 0.2393, 0.08960, -0.4014 0.2056, 0.08360, -0.4989 0.1633, 0.07610, -0.4240 0.1261, 0.06710, -0.4579 0.0900, 0.05640, -0.4156 0.0571, 0.04390, -0.3936 0.0283, 0.02940, -0.3116 0.0142, 0.01970, -0.1766 0.0081, 0.01410, -0.1062 0.0026, 0.00780, 0.1895 0.0000, 0.00000, 0.7907 0.0037, -0.00840, 0.9827 0.0112, -0.01420, 0.7966 0.0191, -0.01930, 0.6822 0.0397, -0.03030, 0.4671 0.0706, -0.04420, 0.2025 0.1037, -0.05710, 0.0068 0.1384, -0.06890, -0.0996 0.1741, -0.07950, -0.2677 0.2102, -0.08660, -0.5032 0.2472, -0.09640, -0.6405 0.2844, -0.10270, -0.8004 0.3225, -0.10690, -0.8752 0.3608, -0.10890, -1.0128 0.3991, -0.10830, -1.0522 0.4373, -0.10510, -1.0682 0.4757, -0.09890, -0.9729 0.5137, -0.09070, -0.9044 0.5694, -0.07640, -0.5087 15 Flap element taps 1.0000, 0.00130, -0.3455 0.9365, 0.01390, -0.0039 0.8333, 0.03280, 0.2051 0.7436, 0.04930, 0.3989 0.7049, 0.05670, 0.5155 0.6662, 0.06410, 0.5505 0.6522, 0.01390, -0.3892 0.5969, -0.00020, -0.3785 0.6000, -0.03020, -0.4249 0.6324, -0.04540, -0.4256 0.6667, -0.04880, -0.3832 0.7046, -0.04110, -0.3664 0.7429, -0.03210, -0.3788 0.8333, -0.01400, -0.3856 0.9311, -0.00120, -0.3771 --------- Run Conditions: vel=109.3 ft/s Re=1.009x10^6 AOA=12.03 Flap deflection=-30.00 Totals: Cl=-0.1284 Cdp=0.0715 Cm(c/4)=0.1777 Cs=-0.0967 Ch=0.1665 Main component: Cl=0.0524 Cdp=0.0366 Cm=0.0640 Flap component: Cl=-0.1808 Cdp=0.0349 Cm=0.1414 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4286 0.6175, -0.04610, -0.3878 0.5841, -0.02440, -0.3907 0.5775, 0.01750, -0.4110 0.5777, 0.04660, -0.3966 0.6274, 0.07170, 0.3072 0.5694, 0.08320, 0.2997 0.5112, 0.09370, 0.0792 0.4731, 0.09830, -0.1074 0.4349, 0.10070, -0.2585 0.3960, 0.10120, -0.3916 0.3566, 0.10020, -0.3474 0.3172, 0.09790, -0.4112 0.2778, 0.09440, -0.5274 0.2393, 0.08960, -0.5928 0.2056, 0.08360, -0.7262 0.1633, 0.07610, -0.6780 0.1261, 0.06710, -0.7642 0.0900, 0.05640, -0.7874 0.0571, 0.04390, -0.8689 0.0283, 0.02940, -0.9533 0.0142, 0.01970, -0.9901 0.0081, 0.01410, -1.0642 0.0026, 0.00780, -0.7303 0.0000, 0.00000, -0.2587 0.0037, -0.00840, 0.9606 0.0112, -0.01420, 1.0044 0.0191, -0.01930, 0.9485 0.0397, -0.03030, 0.7583 0.0706, -0.04420, 0.4898 0.1037, -0.05710, 0.2883 0.1384, -0.06890, 0.1827 0.1741, -0.07950, 0.0052 0.2102, -0.08660, -0.2460 0.2472, -0.09640, -0.3828 0.2844, -0.10270, -0.5584 0.3225, -0.10690, -0.6414 0.3608, -0.10890, -0.7983 0.3991, -0.10830, -0.8587 0.4373, -0.10510, -0.9073 0.4757, -0.09890, -0.8340 0.5137, -0.09070, -0.7682 0.5694, -0.07640, -0.6438 15 Flap element taps 1.0000, 0.00130, -0.3137 0.9365, 0.01390, 0.0003 0.8333, 0.03280, 0.2112 0.7436, 0.04930, 0.4048 0.7049, 0.05670, 0.4225 0.6662, 0.06410, 0.3030 0.6522, 0.01390, -0.4197 0.5969, -0.00020, -0.4037 0.6000, -0.03020, -0.4443 0.6324, -0.04540, -0.4445 0.6667, -0.04880, -0.3656 0.7046, -0.04110, -0.3388 0.7429, -0.03210, -0.3559 0.8333, -0.01400, -0.3681 0.9311, -0.00120, -0.3587 --------- Run Conditions: vel=109.4 ft/s Re=1.015x10^6 AOA=15.02 Flap deflection=-30.00 Totals: Cl=0.1188 Cdp=0.0629 Cm(c/4)=0.1648 Cs=-0.0299 Ch=0.1467 Main component: Cl=0.2557 Cdp=0.0611 Cm=0.0204 Flap component: Cl=-0.1369 Cdp=0.0017 Cm=0.1117 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5000 0.6175, -0.04610, -0.5393 0.5841, -0.02440, -0.5248 0.5775, 0.01750, -0.5338 0.5777, 0.04660, -0.5363 0.6274, 0.07170, 0.0647 0.5694, 0.08320, 0.0580 0.5112, 0.09370, 0.0465 0.4731, 0.09830, -0.0164 0.4349, 0.10070, -0.1873 0.3960, 0.10120, -0.3240 0.3566, 0.10020, -0.4335 0.3172, 0.09790, -0.5211 0.2778, 0.09440, -0.6271 0.2393, 0.08960, -0.7293 0.2056, 0.08360, -0.8359 0.1633, 0.07610, -0.9291 0.1261, 0.06710, -1.0261 0.0900, 0.05640, -1.1487 0.0571, 0.04390, -1.3846 0.0283, 0.02940, -1.7061 0.0142, 0.01970, -1.9576 0.0081, 0.01410, -2.2230 0.0026, 0.00780, -2.1789 0.0000, 0.00000, -2.0556 0.0037, -0.00840, 0.5527 0.0112, -0.01420, 0.9802 0.0191, -0.01930, 1.0131 0.0397, -0.03030, 0.9179 0.0706, -0.04420, 0.7157 0.1037, -0.05710, 0.5298 0.1384, -0.06890, 0.3561 0.1741, -0.07950, 0.1839 0.2102, -0.08660, 0.0055 0.2472, -0.09640, -0.1866 0.2844, -0.10270, -0.3325 0.3225, -0.10690, -0.4838 0.3608, -0.10890, -0.6305 0.3991, -0.10830, -0.7321 0.4373, -0.10510, -0.7828 0.4757, -0.09890, -0.7261 0.5137, -0.09070, -0.6930 0.5694, -0.07640, -0.5787 15 Flap element taps 1.0000, 0.00130, -0.2844 0.9365, 0.01390, 0.0452 0.8333, 0.03280, 0.1826 0.7436, 0.04930, 0.0901 0.7049, 0.05670, 0.0608 0.6662, 0.06410, 0.0611 0.6522, 0.01390, -0.5339 0.5969, -0.00020, -0.5465 0.6000, -0.03020, -0.5685 0.6324, -0.04540, -0.5387 0.6667, -0.04880, -0.3655 0.7046, -0.04110, -0.3125 0.7429, -0.03210, -0.3124 0.8333, -0.01400, -0.3229 0.9311, -0.00120, -0.3594 --------- Run Conditions: vel=108.5 ft/s Re=1.009x10^6 AOA=17.99 Flap deflection=-30.00 Totals: Cl=0.4229 Cdp=0.0662 Cm(c/4)=0.1368 Cs=0.0677 Ch=0.1022 Main component: Cl=0.5068 Cdp=0.0830 Cm=-0.0413 Flap component: Cl=-0.0839 Cdp=-0.0168 Cm=0.0725 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4647 0.6175, -0.04610, -0.5366 0.5841, -0.02440, -0.5275 0.5775, 0.01750, -0.5369 0.5777, 0.04660, -0.5423 0.6274, 0.07170, -0.1990 0.5694, 0.08320, -0.1941 0.5112, 0.09370, -0.1960 0.4731, 0.09830, -0.1904 0.4349, 0.10070, -0.2226 0.3960, 0.10120, -0.3041 0.3566, 0.10020, -0.4161 0.3172, 0.09790, -0.5525 0.2778, 0.09440, -0.7038 0.2393, 0.08960, -0.8548 0.2056, 0.08360, -1.0207 0.1633, 0.07610, -1.1606 0.1261, 0.06710, -1.3382 0.0900, 0.05640, -1.5599 0.0571, 0.04390, -1.9169 0.0283, 0.02940, -2.4629 0.0142, 0.01970, -3.0683 0.0081, 0.01410, -3.9343 0.0026, 0.00780, -4.2580 0.0000, 0.00000, -4.6935 0.0037, -0.00840, -0.2978 0.0112, -0.01420, 0.7274 0.0191, -0.01930, 0.9503 0.0397, -0.03030, 1.0107 0.0706, -0.04420, 0.8798 0.1037, -0.05710, 0.7270 0.1384, -0.06890, 0.5772 0.1741, -0.07950, 0.4148 0.2102, -0.08660, 0.2312 0.2472, -0.09640, 0.0492 0.2844, -0.10270, -0.1022 0.3225, -0.10690, -0.2506 0.3608, -0.10890, -0.4092 0.3991, -0.10830, -0.5225 0.4373, -0.10510, -0.5994 0.4757, -0.09890, -0.5716 0.5137, -0.09070, -0.5738 0.5694, -0.07640, -0.4658 15 Flap element taps 1.0000, 0.00130, -0.1686 0.9365, 0.01390, 0.1022 0.8333, 0.03280, 0.0034 0.7436, 0.04930, -0.1874 0.7049, 0.05670, -0.2173 0.6662, 0.06410, -0.2096 0.6522, 0.01390, -0.5395 0.5969, -0.00020, -0.5434 0.6000, -0.03020, -0.5607 0.6324, -0.04540, -0.5868 0.6667, -0.04880, -0.4359 0.7046, -0.04110, -0.3097 0.7429, -0.03210, -0.3048 0.8333, -0.01400, -0.3197 0.9311, -0.00120, -0.2563 --------- Run Conditions: vel=108.4 ft/s Re=1.008x10^6 AOA=19.97 Flap deflection=-30.00 Totals: Cl=0.4894 Cdp=0.0963 Cm(c/4)=0.1021 Cs=0.0766 Ch=0.0509 Main component: Cl=0.5224 Cdp=0.1378 Cm=-0.0572 Flap component: Cl=-0.0330 Cdp=-0.0415 Cm=0.0361 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5887 0.6175, -0.04610, -0.7578 0.5841, -0.02440, -0.7507 0.5775, 0.01750, -0.7599 0.5777, 0.04660, -0.7644 0.6274, 0.07170, -0.4229 0.5694, 0.08320, -0.4211 0.5112, 0.09370, -0.4335 0.4731, 0.09830, -0.4177 0.4349, 0.10070, -0.4188 0.3960, 0.10120, -0.4372 0.3566, 0.10020, -0.4315 0.3172, 0.09790, -0.4651 0.2778, 0.09440, -0.5430 0.2393, 0.08960, -0.6704 0.2056, 0.08360, -0.8685 0.1633, 0.07610, -1.0383 0.1261, 0.06710, -1.2665 0.0900, 0.05640, -1.5258 0.0571, 0.04390, -1.9428 0.0283, 0.02940, -2.5818 0.0142, 0.01970, -3.2470 0.0081, 0.01410, -4.3197 0.0026, 0.00780, -4.7899 0.0000, 0.00000, -5.4255 0.0037, -0.00840, -0.5810 0.0112, -0.01420, 0.6204 0.0191, -0.01930, 0.9070 0.0397, -0.03030, 1.0216 0.0706, -0.04420, 0.9135 0.1037, -0.05710, 0.7694 0.1384, -0.06890, 0.6349 0.1741, -0.07950, 0.4716 0.2102, -0.08660, 0.2770 0.2472, -0.09640, 0.0978 0.2844, -0.10270, -0.0650 0.3225, -0.10690, -0.2143 0.3608, -0.10890, -0.3881 0.3991, -0.10830, -0.5143 0.4373, -0.10510, -0.6128 0.4757, -0.09890, -0.6020 0.5137, -0.09070, -0.6277 0.5694, -0.07640, -0.5365 15 Flap element taps 1.0000, 0.00130, -0.1759 0.9365, 0.01390, -0.0629 0.8333, 0.03280, -0.2164 0.7436, 0.04930, -0.3879 0.7049, 0.05670, -0.4294 0.6662, 0.06410, -0.4303 0.6522, 0.01390, -0.7612 0.5969, -0.00020, -0.7673 0.6000, -0.03020, -0.7869 0.6324, -0.04540, -0.8318 0.6667, -0.04880, -0.6130 0.7046, -0.04110, -0.3399 0.7429, -0.03210, -0.3257 0.8333, -0.01400, -0.3230 0.9311, -0.00120, -0.2647 --------- Run Conditions: vel=107.2 ft/s Re=0.998x10^6 AOA=23.99 Flap deflection=-30.00 Totals: Cl=-0.0968 Cdp=0.2205 Cm(c/4)=0.1270 Cs=-0.2408 Ch=0.1025 Main component: Cl=0.0346 Cdp=0.2657 Cm=0.0194 Flap component: Cl=-0.1314 Cdp=-0.0452 Cm=0.1073 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.0855 0.6175, -0.04610, -1.3549 0.5841, -0.02440, -1.3417 0.5775, 0.01750, -1.3527 0.5777, 0.04660, -1.3538 0.6274, 0.07170, -0.4655 0.5694, 0.08320, -0.4871 0.5112, 0.09370, -0.5127 0.4731, 0.09830, -0.5058 0.4349, 0.10070, -0.5089 0.3960, 0.10120, -0.5331 0.3566, 0.10020, -0.4823 0.3172, 0.09790, -0.4721 0.2778, 0.09440, -0.4643 0.2393, 0.08960, -0.4587 0.2056, 0.08360, -0.4955 0.1633, 0.07610, -0.4564 0.1261, 0.06710, -0.4801 0.0900, 0.05640, -0.4462 0.0571, 0.04390, -0.4700 0.0283, 0.02940, -0.4847 0.0142, 0.01970, -0.4844 0.0081, 0.01410, -0.5314 0.0026, 0.00780, -0.4509 0.0000, 0.00000, -0.6973 0.0037, -0.00840, 0.6944 0.0112, -0.01420, 0.9916 0.0191, -0.01930, 1.0195 0.0397, -0.03030, 0.9579 0.0706, -0.04420, 0.7773 0.1037, -0.05710, 0.6045 0.1384, -0.06890, 0.4696 0.1741, -0.07950, 0.2844 0.2102, -0.08660, 0.0585 0.2472, -0.09640, -0.1379 0.2844, -0.10270, -0.3307 0.3225, -0.10690, -0.4965 0.3608, -0.10890, -0.7104 0.3991, -0.10830, -0.8610 0.4373, -0.10510, -0.9974 0.4757, -0.09890, -1.0001 0.5137, -0.09070, -1.0518 0.5694, -0.07640, -0.9657 15 Flap element taps 1.0000, 0.00130, -0.5410 0.9365, 0.01390, -0.4733 0.8333, 0.03280, -0.5258 0.7436, 0.04930, -0.5140 0.7049, 0.05670, -0.4923 0.6662, 0.06410, -0.4647 0.6522, 0.01390, -1.3612 0.5969, -0.00020, -1.3772 0.6000, -0.03020, -1.4408 0.6324, -0.04540, -1.5860 0.6667, -0.04880, -1.5009 0.7046, -0.04110, -1.0029 0.7429, -0.03210, -0.9350 0.8333, -0.01400, -0.8488 0.9311, -0.00120, -0.6134 --------- Run Conditions: vel=107.4 ft/s Re=1.000x10^6 AOA=27.00 Flap deflection=-30.00 Totals: Cl=-0.0853 Cdp=0.2421 Cm(c/4)=0.1246 Cs=-0.2544 Ch=0.0776 Main component: Cl=0.0437 Cdp=0.3092 Cm=0.0091 Flap component: Cl=-0.1289 Cdp=-0.0671 Cm=0.1070 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.1944 0.6175, -0.04610, -1.5479 0.5841, -0.02440, -1.5380 0.5775, 0.01750, -1.5463 0.5777, 0.04660, -1.5474 0.6274, 0.07170, -0.5050 0.5694, 0.08320, -0.5182 0.5112, 0.09370, -0.5484 0.4731, 0.09830, -0.5411 0.4349, 0.10070, -0.5404 0.3960, 0.10120, -0.5836 0.3566, 0.10020, -0.5103 0.3172, 0.09790, -0.5020 0.2778, 0.09440, -0.4979 0.2393, 0.08960, -0.5009 0.2056, 0.08360, -0.5528 0.1633, 0.07610, -0.4823 0.1261, 0.06710, -0.5155 0.0900, 0.05640, -0.4738 0.0571, 0.04390, -0.4928 0.0283, 0.02940, -0.5102 0.0142, 0.01970, -0.5101 0.0081, 0.01410, -0.5683 0.0026, 0.00780, -0.4759 0.0000, 0.00000, -0.7297 0.0037, -0.00840, 0.5955 0.0112, -0.01420, 0.9553 0.0191, -0.01930, 1.0150 0.0397, -0.03030, 0.9875 0.0706, -0.04420, 0.8237 0.1037, -0.05710, 0.6621 0.1384, -0.06890, 0.5505 0.1741, -0.07950, 0.3656 0.2102, -0.08660, 0.1217 0.2472, -0.09640, -0.0643 0.2844, -0.10270, -0.2701 0.3225, -0.10690, -0.4296 0.3608, -0.10890, -0.6626 0.3991, -0.10830, -0.8207 0.4373, -0.10510, -0.9854 0.4757, -0.09890, -1.0078 0.5137, -0.09070, -1.0837 0.5694, -0.07640, -1.0221 15 Flap element taps 1.0000, 0.00130, -0.5762 0.9365, 0.01390, -0.5055 0.8333, 0.03280, -0.5690 0.7436, 0.04930, -0.5590 0.7049, 0.05670, -0.5382 0.6662, 0.06410, -0.5092 0.6522, 0.01390, -1.5602 0.5969, -0.00020, -1.5737 0.6000, -0.03020, -1.6456 0.6324, -0.04540, -1.8561 0.6667, -0.04880, -1.9813 0.7046, -0.04110, -1.2027 0.7429, -0.03210, -0.9958 0.8333, -0.01400, -0.7688 0.9311, -0.00120, -0.4929