S809 UNVENTED AILERON, CLEAN, CHORD = 18 IN --------- Run Conditions: vel=217.4 ft/s Re=2.003x10^6 AOA=-6.01 Flap deflection=-30.00 Totals: Cl=-1.2062 Cdp=0.1595 Cm(c/4)=0.1352 Cs=-0.0323 Ch=0.2255 Main component: Cl=-0.9891 Cdp=0.0178 Cm=0.2460 Flap component: Cl=-0.2170 Cdp=0.1417 Cm=0.1933 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5032 0.6175, -0.04610, -0.4590 0.5841, -0.02440, -0.4499 0.5775, 0.01750, -0.4552 0.5777, 0.04660, -0.4527 0.6274, 0.07170, 0.6909 0.5694, 0.08320, 0.5171 0.5112, 0.09370, 0.2338 0.4731, 0.09830, 0.2120 0.4349, 0.10070, 0.1731 0.3960, 0.10120, 0.1855 0.3566, 0.10020, 0.2011 0.3172, 0.09790, 0.2345 0.2778, 0.09440, 0.2636 0.2393, 0.08960, 0.3075 0.2056, 0.08360, 0.3692 0.1633, 0.07610, 0.4519 0.1261, 0.06710, 0.5620 0.0900, 0.05640, 0.6943 0.0571, 0.04390, 0.8604 0.0283, 0.02940, 1.0063 0.0142, 0.01970, 0.9614 0.0081, 0.01410, 0.7582 0.0026, 0.00780, -0.0468 0.0000, 0.00000, -2.9532 0.0037, -0.00840, -3.8970 0.0112, -0.01420, -2.9866 0.0191, -0.01930, -2.0441 0.0397, -0.03030, -1.6278 0.0706, -0.04420, -1.4363 0.1037, -0.05710, -1.4119 0.1384, -0.06890, -1.4086 0.1741, -0.07950, -1.4004 0.2102, -0.08660, -1.4372 0.2472, -0.09640, -1.4949 0.2844, -0.10270, -1.4796 0.3225, -0.10690, -1.4443 0.3608, -0.10890, -1.3642 0.3991, -0.10830, -1.1897 0.4373, -0.10510, -0.9115 0.4757, -0.09890, -0.6155 0.5137, -0.09070, -0.5183 0.5694, -0.07640, -0.5055 15 Flap element taps 1.0000, 0.00130, -0.4803 0.9365, 0.01390, 0.0091 0.8333, 0.03280, 0.2863 0.7436, 0.04930, 0.4955 0.7049, 0.05670, 0.6229 0.6662, 0.06410, 0.7393 0.6522, 0.01390, -0.4520 0.5969, -0.00020, -0.4678 0.6000, -0.03020, -0.4801 0.6324, -0.04540, -0.4770 0.6667, -0.04880, -0.4891 0.7046, -0.04110, -0.4922 0.7429, -0.03210, -0.4943 0.8333, -0.01400, -0.5057 0.9311, -0.00120, -0.4976 --------- Run Conditions: vel=218.5 ft/s Re=2.004x10^6 AOA=0.02 Flap deflection=-30.00 Totals: Cl=-1.1358 Cdp=0.1112 Cm(c/4)=0.1717 Cs=-0.1116 Ch=0.2150 Main component: Cl=-0.9164 Cdp=-0.0024 Cm=0.2716 Flap component: Cl=-0.2194 Cdp=0.1136 Cm=0.1840 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5586 0.6175, -0.04610, -0.3980 0.5841, -0.02440, -0.3864 0.5775, 0.01750, -0.3886 0.5777, 0.04660, -0.3825 0.6274, 0.07170, 0.6666 0.5694, 0.08320, 0.4825 0.5112, 0.09370, 0.1427 0.4731, 0.09830, 0.1189 0.4349, 0.10070, 0.0763 0.3960, 0.10120, 0.0695 0.3566, 0.10020, 0.0661 0.3172, 0.09790, 0.0812 0.2778, 0.09440, 0.0891 0.2393, 0.08960, 0.1120 0.2056, 0.08360, 0.1522 0.1633, 0.07610, 0.2137 0.1261, 0.06710, 0.3070 0.0900, 0.05640, 0.4253 0.0571, 0.04390, 0.6025 0.0283, 0.02940, 0.8374 0.0142, 0.01970, 0.9929 0.0081, 0.01410, 1.0100 0.0026, 0.00780, 0.7251 0.0000, 0.00000, -0.4744 0.0037, -0.00840, -1.5490 0.0112, -0.01420, -1.3146 0.0191, -0.01930, -1.1392 0.0397, -0.03030, -0.9471 0.0706, -0.04420, -0.9339 0.1037, -0.05710, -1.0225 0.1384, -0.06890, -1.1110 0.1741, -0.07950, -1.1933 0.2102, -0.08660, -1.3017 0.2472, -0.09640, -1.4417 0.2844, -0.10270, -1.5180 0.3225, -0.10690, -1.5945 0.3608, -0.10890, -1.6391 0.3991, -0.10830, -1.6204 0.4373, -0.10510, -1.5258 0.4757, -0.09890, -1.3263 0.5137, -0.09070, -1.0934 0.5694, -0.07640, -0.7709 15 Flap element taps 1.0000, 0.00130, -0.4433 0.9365, 0.01390, 0.0220 0.8333, 0.03280, 0.2800 0.7436, 0.04930, 0.4812 0.7049, 0.05670, 0.6060 0.6662, 0.06410, 0.7171 0.6522, 0.01390, -0.3819 0.5969, -0.00020, -0.4134 0.6000, -0.03020, -0.4547 0.6324, -0.04540, -0.4498 0.6667, -0.04880, -0.4305 0.7046, -0.04110, -0.4338 0.7429, -0.03210, -0.4433 0.8333, -0.01400, -0.4659 0.9311, -0.00120, -0.4802 --------- Run Conditions: vel=219.3 ft/s Re=2.006x10^6 AOA=3.05 Flap deflection=-30.00 Totals: Cl=-0.9096 Cdp=0.0883 Cm(c/4)=0.1712 Cs=-0.1366 Ch=0.1939 Main component: Cl=-0.7040 Cdp=-0.0032 Cm=0.2294 Flap component: Cl=-0.2056 Cdp=0.0914 Cm=0.1677 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5391 0.6175, -0.04610, -0.3817 0.5841, -0.02440, -0.3736 0.5775, 0.01750, -0.3745 0.5777, 0.04660, -0.3675 0.6274, 0.07170, 0.6358 0.5694, 0.08320, 0.4461 0.5112, 0.09370, 0.2336 0.4731, 0.09830, 0.0279 0.4349, 0.10070, -0.0112 0.3960, 0.10120, -0.0287 0.3566, 0.10020, -0.0456 0.3172, 0.09790, -0.0427 0.2778, 0.09440, -0.0498 0.2393, 0.08960, -0.0438 0.2056, 0.08360, -0.0212 0.1633, 0.07610, 0.0200 0.1261, 0.06710, 0.0930 0.0900, 0.05640, 0.1872 0.0571, 0.04390, 0.3443 0.0283, 0.02940, 0.5822 0.0142, 0.01970, 0.8138 0.0081, 0.01410, 0.9368 0.0026, 0.00780, 0.9776 0.0000, 0.00000, 0.5835 0.0037, -0.00840, -0.2984 0.0112, -0.01420, -0.3958 0.0191, -0.01930, -0.3975 0.0397, -0.03030, -0.4194 0.0706, -0.04420, -0.5243 0.1037, -0.05710, -0.6681 0.1384, -0.06890, -0.7990 0.1741, -0.07950, -0.9190 0.2102, -0.08660, -1.0528 0.2472, -0.09640, -1.2131 0.2844, -0.10270, -1.3134 0.3225, -0.10690, -1.4183 0.3608, -0.10890, -1.4843 0.3991, -0.10830, -1.4990 0.4373, -0.10510, -1.4238 0.4757, -0.09890, -1.3252 0.5137, -0.09070, -0.9833 0.5694, -0.07640, -0.7224 15 Flap element taps 1.0000, 0.00130, -0.3962 0.9365, 0.01390, 0.0156 0.8333, 0.03280, 0.2581 0.7436, 0.04930, 0.4586 0.7049, 0.05670, 0.5846 0.6662, 0.06410, 0.6875 0.6522, 0.01390, -0.3699 0.5969, -0.00020, -0.3897 0.6000, -0.03020, -0.4263 0.6324, -0.04540, -0.4094 0.6667, -0.04880, -0.3982 0.7046, -0.04110, -0.3980 0.7429, -0.03210, -0.3996 0.8333, -0.01400, -0.4108 0.9311, -0.00120, -0.4218 --------- Run Conditions: vel=219.9 ft/s Re=2.006x10^6 AOA=6.04 Flap deflection=-30.00 Totals: Cl=-0.6344 Cdp=0.0821 Cm(c/4)=0.1723 Cs=-0.1484 Ch=0.1829 Main component: Cl=-0.4355 Cdp=0.0060 Cm=0.1692 Flap component: Cl=-0.1989 Cdp=0.0761 Cm=0.1586 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5012 0.6175, -0.04610, -0.3698 0.5841, -0.02440, -0.3617 0.5775, 0.01750, -0.3660 0.5777, 0.04660, -0.3615 0.6274, 0.07170, 0.5878 0.5694, 0.08320, 0.4029 0.5112, 0.09370, 0.1525 0.4731, 0.09830, -0.0742 0.4349, 0.10070, -0.1247 0.3960, 0.10120, -0.1495 0.3566, 0.10020, -0.1798 0.3172, 0.09790, -0.1921 0.2778, 0.09440, -0.2172 0.2393, 0.08960, -0.2316 0.2056, 0.08360, -0.2318 0.1633, 0.07610, -0.2182 0.1261, 0.06710, -0.1749 0.0900, 0.05640, -0.1212 0.0571, 0.04390, -0.0141 0.0283, 0.02940, 0.1703 0.0142, 0.01970, 0.4048 0.0081, 0.01410, 0.5772 0.0026, 0.00780, 0.7955 0.0000, 0.00000, 1.0096 0.0037, -0.00840, 0.6035 0.0112, -0.01420, 0.3532 0.0191, -0.01930, 0.2395 0.0397, -0.03030, 0.0750 0.0706, -0.04420, -0.1110 0.1037, -0.05710, -0.2928 0.1384, -0.06890, -0.4551 0.1741, -0.07950, -0.5983 0.2102, -0.08660, -0.7490 0.2472, -0.09640, -0.9244 0.2844, -0.10270, -1.0434 0.3225, -0.10690, -1.1678 0.3608, -0.10890, -1.2551 0.3991, -0.10830, -1.2958 0.4373, -0.10510, -1.2511 0.4757, -0.09890, -1.1440 0.5137, -0.09070, -0.9112 0.5694, -0.07640, -0.6550 15 Flap element taps 1.0000, 0.00130, -0.3839 0.9365, 0.01390, -0.0040 0.8333, 0.03280, 0.2297 0.7436, 0.04930, 0.4328 0.7049, 0.05670, 0.5599 0.6662, 0.06410, 0.6344 0.6522, 0.01390, -0.3636 0.5969, -0.00020, -0.3797 0.6000, -0.03020, -0.4116 0.6324, -0.04540, -0.3971 0.6667, -0.04880, -0.3852 0.7046, -0.04110, -0.3849 0.7429, -0.03210, -0.3878 0.8333, -0.01400, -0.4002 0.9311, -0.00120, -0.4124 --------- Run Conditions: vel=220.2 ft/s Re=2.002x10^6 AOA=9.02 Flap deflection=-30.00 Totals: Cl=-0.3744 Cdp=0.0757 Cm(c/4)=0.1765 Cs=-0.1335 Ch=0.1758 Main component: Cl=-0.1820 Cdp=0.0174 Cm=0.1148 Flap component: Cl=-0.1924 Cdp=0.0584 Cm=0.1512 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4684 0.6175, -0.04610, -0.3699 0.5841, -0.02440, -0.3629 0.5775, 0.01750, -0.3682 0.5777, 0.04660, -0.3676 0.6274, 0.07170, 0.4448 0.5694, 0.08320, 0.3681 0.5112, 0.09370, 0.0963 0.4731, 0.09830, -0.0841 0.4349, 0.10070, -0.1830 0.3960, 0.10120, -0.2425 0.3566, 0.10020, -0.3155 0.3172, 0.09790, -0.3451 0.2778, 0.09440, -0.3880 0.2393, 0.08960, -0.4257 0.2056, 0.08360, -0.4518 0.1633, 0.07610, -0.4734 0.1261, 0.06710, -0.4692 0.0900, 0.05640, -0.4715 0.0571, 0.04390, -0.4450 0.0283, 0.02940, -0.3705 0.0142, 0.01970, -0.2246 0.0081, 0.01410, -0.0907 0.0026, 0.00780, 0.1424 0.0000, 0.00000, 0.7284 0.0037, -0.00840, 0.9858 0.0112, -0.01420, 0.8114 0.0191, -0.01930, 0.6787 0.0397, -0.03030, 0.4607 0.0706, -0.04420, 0.2364 0.1037, -0.05710, 0.0353 0.1384, -0.06890, -0.1463 0.1741, -0.07950, -0.3042 0.2102, -0.08660, -0.4654 0.2472, -0.09640, -0.6508 0.2844, -0.10270, -0.7843 0.3225, -0.10690, -0.9244 0.3608, -0.10890, -1.0283 0.3991, -0.10830, -1.0930 0.4373, -0.10510, -1.0792 0.4757, -0.09890, -0.9765 0.5137, -0.09070, -0.8996 0.5694, -0.07640, -0.5829 15 Flap element taps 1.0000, 0.00130, -0.3688 0.9365, 0.01390, -0.0169 0.8333, 0.03280, 0.2138 0.7436, 0.04930, 0.4293 0.7049, 0.05670, 0.5178 0.6662, 0.06410, 0.4593 0.6522, 0.01390, -0.3626 0.5969, -0.00020, -0.3758 0.6000, -0.03020, -0.4051 0.6324, -0.04540, -0.3908 0.6667, -0.04880, -0.3763 0.7046, -0.04110, -0.3754 0.7429, -0.03210, -0.3784 0.8333, -0.01400, -0.3891 0.9311, -0.00120, -0.4076 --------- Run Conditions: vel=220.3 ft/s Re=2.001x10^6 AOA=12.03 Flap deflection=-30.00 Totals: Cl=-0.1110 Cdp=0.0698 Cm(c/4)=0.1764 Cs=-0.0914 Ch=0.1714 Main component: Cl=0.0680 Cdp=0.0315 Cm=0.0592 Flap component: Cl=-0.1790 Cdp=0.0383 Cm=0.1407 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4341 0.6175, -0.04610, -0.3775 0.5841, -0.02440, -0.3694 0.5775, 0.01750, -0.3732 0.5777, 0.04660, -0.3712 0.6274, 0.07170, 0.2169 0.5694, 0.08320, 0.2208 0.5112, 0.09370, 0.1128 0.4731, 0.09830, -0.0833 0.4349, 0.10070, -0.2344 0.3960, 0.10120, -0.3069 0.3566, 0.10020, -0.3885 0.3172, 0.09790, -0.4386 0.2778, 0.09440, -0.5050 0.2393, 0.08960, -0.5898 0.2056, 0.08360, -0.6676 0.1633, 0.07610, -0.7370 0.1261, 0.06710, -0.7805 0.0900, 0.05640, -0.8540 0.0571, 0.04390, -0.9389 0.0283, 0.02940, -1.0301 0.0142, 0.01970, -1.0648 0.0081, 0.01410, -1.0781 0.0026, 0.00780, -0.8045 0.0000, 0.00000, -0.3914 0.0037, -0.00840, 0.9404 0.0112, -0.01420, 1.0021 0.0191, -0.01930, 0.9339 0.0397, -0.03030, 0.7453 0.0706, -0.04420, 0.5231 0.1037, -0.05710, 0.3212 0.1384, -0.06890, 0.1314 0.1741, -0.07950, -0.0329 0.2102, -0.08660, -0.1983 0.2472, -0.09640, -0.3886 0.2844, -0.10270, -0.5329 0.3225, -0.10690, -0.6857 0.3608, -0.10890, -0.8039 0.3991, -0.10830, -0.8903 0.4373, -0.10510, -0.9048 0.4757, -0.09890, -0.8211 0.5137, -0.09070, -0.7660 0.5694, -0.07640, -0.4978 15 Flap element taps 1.0000, 0.00130, -0.3531 0.9365, 0.01390, -0.0093 0.8333, 0.03280, 0.2268 0.7436, 0.04930, 0.3822 0.7049, 0.05670, 0.3143 0.6662, 0.06410, 0.2169 0.6522, 0.01390, -0.3671 0.5969, -0.00020, -0.3823 0.6000, -0.03020, -0.4055 0.6324, -0.04540, -0.3908 0.6667, -0.04880, -0.3639 0.7046, -0.04110, -0.3630 0.7429, -0.03210, -0.3643 0.8333, -0.01400, -0.3800 0.9311, -0.00120, -0.4068 --------- Run Conditions: vel=220.2 ft/s Re=1.993x10^6 AOA=15.02 Flap deflection=-30.00 Totals: Cl=0.1689 Cdp=0.0671 Cm(c/4)=0.1607 Cs=-0.0210 Ch=0.1417 Main component: Cl=0.3077 Cdp=0.0466 Cm=0.0056 Flap component: Cl=-0.1388 Cdp=0.0204 Cm=0.1099 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3792 0.6175, -0.04610, -0.3923 0.5841, -0.02440, -0.3817 0.5775, 0.01750, -0.4037 0.5777, 0.04660, -0.3955 0.6274, 0.07170, 0.0253 0.5694, 0.08320, 0.0215 0.5112, 0.09370, 0.0203 0.4731, 0.09830, -0.0060 0.4349, 0.10070, -0.1528 0.3960, 0.10120, -0.3238 0.3566, 0.10020, -0.4486 0.3172, 0.09790, -0.5452 0.2778, 0.09440, -0.6533 0.2393, 0.08960, -0.7669 0.2056, 0.08360, -0.8722 0.1633, 0.07610, -0.9781 0.1261, 0.06710, -1.0778 0.0900, 0.05640, -1.2389 0.0571, 0.04390, -1.4445 0.0283, 0.02940, -1.7727 0.0142, 0.01970, -2.0924 0.0081, 0.01410, -2.3162 0.0026, 0.00780, -2.3590 0.0000, 0.00000, -2.2899 0.0037, -0.00840, 0.5077 0.0112, -0.01420, 0.9683 0.0191, -0.01930, 1.0150 0.0397, -0.03030, 0.9286 0.0706, -0.04420, 0.7419 0.1037, -0.05710, 0.5544 0.1384, -0.06890, 0.3751 0.1741, -0.07950, 0.2088 0.2102, -0.08660, 0.0380 0.2472, -0.09640, -0.1504 0.2844, -0.10270, -0.3037 0.3225, -0.10690, -0.4603 0.3608, -0.10890, -0.5973 0.3991, -0.10830, -0.6994 0.4373, -0.10510, -0.7414 0.4757, -0.09890, -0.6874 0.5137, -0.09070, -0.5663 0.5694, -0.07640, -0.4483 15 Flap element taps 1.0000, 0.00130, -0.3452 0.9365, 0.01390, 0.0290 0.8333, 0.03280, 0.1640 0.7436, 0.04930, 0.0697 0.7049, 0.05670, 0.0330 0.6662, 0.06410, 0.0231 0.6522, 0.01390, -0.3955 0.5969, -0.00020, -0.2667 0.6000, -0.03020, -0.4004 0.6324, -0.04540, -0.4216 0.6667, -0.04880, -0.3658 0.7046, -0.04110, -0.3539 0.7429, -0.03210, -0.3223 0.8333, -0.01400, -0.3801 0.9311, -0.00120, -0.3621 --------- Run Conditions: vel=220.4 ft/s Re=1.995x10^6 AOA=17.99 Flap deflection=-30.00 Totals: Cl=0.4983 Cdp=0.0621 Cm(c/4)=0.1265 Cs=0.0948 Ch=0.0901 Main component: Cl=0.5636 Cdp=0.0746 Cm=-0.0548 Flap component: Cl=-0.0654 Cdp=-0.0124 Cm=0.0580 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3651 0.6175, -0.04610, -0.4531 0.5841, -0.02440, -0.4508 0.5775, 0.01750, -0.4517 0.5777, 0.04660, -0.4508 0.6274, 0.07170, -0.2065 0.5694, 0.08320, -0.2040 0.5112, 0.09370, -0.1985 0.4731, 0.09830, -0.1975 0.4349, 0.10070, -0.2245 0.3960, 0.10120, -0.3047 0.3566, 0.10020, -0.4537 0.3172, 0.09790, -0.6029 0.2778, 0.09440, -0.7596 0.2393, 0.08960, -0.9205 0.2056, 0.08360, -1.0753 0.1633, 0.07610, -1.2417 0.1261, 0.06710, -1.4152 0.0900, 0.05640, -1.6783 0.0571, 0.04390, -2.0529 0.0283, 0.02940, -2.6443 0.0142, 0.01970, -3.2516 0.0081, 0.01410, -4.0033 0.0026, 0.00780, -4.2837 0.0000, 0.00000, -5.1544 0.0037, -0.00840, -0.3864 0.0112, -0.01420, 0.6913 0.0191, -0.01930, 0.9377 0.0397, -0.03030, 1.0091 0.0706, -0.04420, 0.9017 0.1037, -0.05710, 0.7508 0.1384, -0.06890, 0.5881 0.1741, -0.07950, 0.4324 0.2102, -0.08660, 0.2704 0.2472, -0.09640, 0.0885 0.2844, -0.10270, -0.0662 0.3225, -0.10690, -0.2260 0.3608, -0.10890, -0.3695 0.3991, -0.10830, -0.4854 0.4373, -0.10510, -0.5498 0.4757, -0.09890, -0.5259 0.5137, -0.09070, -0.5176 0.5694, -0.07640, -0.4146 15 Flap element taps 1.0000, 0.00130, -0.2747 0.9365, 0.01390, 0.0352 0.8333, 0.03280, 0.0120 0.7436, 0.04930, -0.1829 0.7049, 0.05670, -0.2118 0.6662, 0.06410, -0.2098 0.6522, 0.01390, -0.4500 0.5969, -0.00020, -0.4568 0.6000, -0.03020, -0.4642 0.6324, -0.04540, -0.4293 0.6667, -0.04880, -0.2760 0.7046, -0.04110, -0.2525 0.7429, -0.03210, -0.2555 0.8333, -0.01400, -0.2727 0.9311, -0.00120, -0.3029 --------- Run Conditions: vel=220.3 ft/s Re=1.989x10^6 AOA=19.98 Flap deflection=-30.00 Totals: Cl=0.4856 Cdp=0.0966 Cm(c/4)=0.0759 Cs=0.0751 Ch=0.0163 Main component: Cl=0.4869 Cdp=0.1287 Cm=-0.0553 Flap component: Cl=-0.0013 Cdp=-0.0321 Cm=0.0089 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5069 0.6175, -0.04610, -0.6755 0.5841, -0.02440, -0.6671 0.5775, 0.01750, -0.6660 0.5777, 0.04660, -0.6654 0.6274, 0.07170, -0.4287 0.5694, 0.08320, -0.4426 0.5112, 0.09370, -0.4403 0.4731, 0.09830, -0.4378 0.4349, 0.10070, -0.4348 0.3960, 0.10120, -0.4213 0.3566, 0.10020, -0.4189 0.3172, 0.09790, -0.4172 0.2778, 0.09440, -0.4350 0.2393, 0.08960, -0.4809 0.2056, 0.08360, -0.5796 0.1633, 0.07610, -0.7701 0.1261, 0.06710, -1.0367 0.0900, 0.05640, -1.3873 0.0571, 0.04390, -1.8454 0.0283, 0.02940, -2.5275 0.0142, 0.01970, -3.2218 0.0081, 0.01410, -3.9906 0.0026, 0.00780, -4.4281 0.0000, 0.00000, -5.5386 0.0037, -0.00840, -0.5711 0.0112, -0.01420, 0.6132 0.0191, -0.01930, 0.9019 0.0397, -0.03030, 1.0115 0.0706, -0.04420, 0.9270 0.1037, -0.05710, 0.7873 0.1384, -0.06890, 0.6285 0.1741, -0.07950, 0.4751 0.2102, -0.08660, 0.3134 0.2472, -0.09640, 0.1287 0.2844, -0.10270, -0.0308 0.3225, -0.10690, -0.1995 0.3608, -0.10890, -0.3540 0.3991, -0.10830, -0.4845 0.4373, -0.10510, -0.5655 0.4757, -0.09890, -0.5586 0.5137, -0.09070, -0.5669 0.5694, -0.07640, -0.4862 15 Flap element taps 1.0000, 0.00130, -0.2553 0.9365, 0.01390, -0.2267 0.8333, 0.03280, -0.3421 0.7436, 0.04930, -0.4202 0.7049, 0.05670, -0.4280 0.6662, 0.06410, -0.4191 0.6522, 0.01390, -0.6695 0.5969, -0.00020, -0.6787 0.6000, -0.03020, -0.6949 0.6324, -0.04540, -0.6677 0.6667, -0.04880, -0.4449 0.7046, -0.04110, -0.3390 0.7429, -0.03210, -0.3295 0.8333, -0.01400, -0.3382 0.9311, -0.00120, -0.3091 --------- Run Conditions: vel=221.3 ft/s Re=1.997x10^6 AOA=24.00 Flap deflection=-30.00 Totals: Cl=0.2281 Cdp=0.2551 Cm(c/4)=0.0871 Cs=-0.1403 Ch=0.0804 Main component: Cl=0.2997 Cdp=0.2892 Cm=-0.0554 Flap component: Cl=-0.0716 Cdp=-0.0340 Cm=0.0645 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7982 0.6175, -0.04610, -1.0134 0.5841, -0.02440, -1.0115 0.5775, 0.01750, -1.0143 0.5777, 0.04660, -1.0141 0.6274, 0.07170, -0.6175 0.5694, 0.08320, -0.6404 0.5112, 0.09370, -0.6676 0.4731, 0.09830, -0.6770 0.4349, 0.10070, -0.6846 0.3960, 0.10120, -0.6866 0.3566, 0.10020, -0.6939 0.3172, 0.09790, -0.6991 0.2778, 0.09440, -0.7043 0.2393, 0.08960, -0.7188 0.2056, 0.08360, -0.7239 0.1633, 0.07610, -0.7518 0.1261, 0.06710, -0.7762 0.0900, 0.05640, -0.8463 0.0571, 0.04390, -0.9015 0.0283, 0.02940, -0.9813 0.0142, 0.01970, -1.0470 0.0081, 0.01410, -1.1023 0.0026, 0.00780, -1.1247 0.0000, 0.00000, -1.6357 0.0037, -0.00840, 0.2827 0.0112, -0.01420, 0.8556 0.0191, -0.01930, 0.9829 0.0397, -0.03030, 0.9934 0.0706, -0.04420, 0.8778 0.1037, -0.05710, 0.7295 0.1384, -0.06890, 0.5659 0.1741, -0.07950, 0.4056 0.2102, -0.08660, 0.2348 0.2472, -0.09640, 0.0357 0.2844, -0.10270, -0.1388 0.3225, -0.10690, -0.3263 0.3608, -0.10890, -0.5026 0.3991, -0.10830, -0.6570 0.4373, -0.10510, -0.7590 0.4757, -0.09890, -0.7641 0.5137, -0.09070, -0.7917 0.5694, -0.07640, -0.7200 15 Flap element taps 1.0000, 0.00130, -0.4503 0.9365, 0.01390, -0.3367 0.8333, 0.03280, -0.4586 0.7436, 0.04930, -0.5501 0.7049, 0.05670, -0.5764 0.6662, 0.06410, -0.5880 0.6522, 0.01390, -1.0083 0.5969, -0.00020, -1.0257 0.6000, -0.03020, -1.0599 0.6324, -0.04540, -1.0872 0.6667, -0.04880, -0.8992 0.7046, -0.04110, -0.7128 0.7429, -0.03210, -0.7069 0.8333, -0.01400, -0.7115 0.9311, -0.00120, -0.5570 --------- Run Conditions: vel=224.7 ft/s Re=2.026x10^6 AOA=27.02 Flap deflection=-30.00 Totals: Cl=-0.0666 Cdp=0.2531 Cm(c/4)=0.1337 Cs=-0.2557 Ch=0.1329 Main component: Cl=0.0826 Cdp=0.2900 Cm=-0.0012 Flap component: Cl=-0.1492 Cdp=-0.0369 Cm=0.1209 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.0337 0.6175, -0.04610, -1.3070 0.5841, -0.02440, -1.2984 0.5775, 0.01750, -1.2979 0.5777, 0.04660, -1.2953 0.6274, 0.07170, -0.5107 0.5694, 0.08320, -0.5323 0.5112, 0.09370, -0.5427 0.4731, 0.09830, -0.5361 0.4349, 0.10070, -0.5330 0.3960, 0.10120, -0.5232 0.3566, 0.10020, -0.5228 0.3172, 0.09790, -0.5175 0.2778, 0.09440, -0.5165 0.2393, 0.08960, -0.5139 0.2056, 0.08360, -0.5094 0.1633, 0.07610, -0.5146 0.1261, 0.06710, -0.5131 0.0900, 0.05640, -0.5157 0.0571, 0.04390, -0.5104 0.0283, 0.02940, -0.5185 0.0142, 0.01970, -0.5395 0.0081, 0.01410, -0.5573 0.0026, 0.00780, -0.5387 0.0000, 0.00000, -0.7898 0.0037, -0.00840, 0.5673 0.0112, -0.01420, 0.9394 0.0191, -0.01930, 1.0074 0.0397, -0.03030, 0.9779 0.0706, -0.04420, 0.8455 0.1037, -0.05710, 0.6906 0.1384, -0.06890, 0.5224 0.1741, -0.07950, 0.3571 0.2102, -0.08660, 0.1773 0.2472, -0.09640, -0.0327 0.2844, -0.10270, -0.2197 0.3225, -0.10690, -0.4221 0.3608, -0.10890, -0.6172 0.3991, -0.10830, -0.7912 0.4373, -0.10510, -0.9125 0.4757, -0.09890, -0.9294 0.5137, -0.09070, -0.9760 0.5694, -0.07640, -0.9213 15 Flap element taps 1.0000, 0.00130, -0.6334 0.9365, 0.01390, -0.5360 0.8333, 0.03280, -0.5564 0.7436, 0.04930, -0.5463 0.7049, 0.05670, -0.5295 0.6662, 0.06410, -0.5117 0.6522, 0.01390, -1.2964 0.5969, -0.00020, -1.3208 0.6000, -0.03020, -1.3693 0.6324, -0.04540, -1.4573 0.6667, -0.04880, -1.3100 0.7046, -0.04110, -1.0830 0.7429, -0.03210, -1.0630 0.8333, -0.01400, -1.0248 0.9311, -0.00120, -0.7901