S809 UNVENTED AILERON, CLEAN, CHORD = 18 IN --------- Run Conditions: vel=221.3 ft/s Re=2.008x10^6 AOA=-6.01 Flap deflection=-45.00 Totals: Cl=-1.5013 Cdp=0.2747 Cm(c/4)=0.1898 Cs=-0.1160 Ch=0.3254 Main component: Cl=-1.2570 Cdp=0.0143 Cm=0.3284 Flap component: Cl=-0.2443 Cdp=0.2603 Cm=0.2418 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6512 0.6175, -0.04610, -0.5888 0.5841, -0.02440, -0.5875 0.5775, 0.01750, -0.5882 0.5777, 0.04660, -0.5824 0.6274, 0.07170, 0.8188 0.5694, 0.08320, 0.7400 0.5112, 0.09370, 0.5872 0.4731, 0.09830, 0.4669 0.4349, 0.10070, 0.4381 0.3960, 0.10120, 0.4434 0.3566, 0.10020, 0.4244 0.3172, 0.09790, 0.4417 0.2778, 0.09440, 0.4559 0.2393, 0.08960, 0.4918 0.2056, 0.08360, 0.5546 0.1633, 0.07610, 0.6082 0.1261, 0.06710, 0.7118 0.0900, 0.05640, 0.8142 0.0571, 0.04390, 0.9474 0.0283, 0.02940, 1.0083 0.0142, 0.01970, 0.8346 0.0081, 0.01410, 0.5046 0.0026, 0.00780, -0.5467 0.0000, 0.00000, -4.4302 0.0037, -0.00840, -5.2202 0.0112, -0.01420, -3.3053 0.0191, -0.01930, -2.6535 0.0397, -0.03030, -2.0290 0.0706, -0.04420, -1.7421 0.1037, -0.05710, -1.6767 0.1384, -0.06890, -1.6670 0.1741, -0.07950, -1.6381 0.2102, -0.08660, -1.6540 0.2472, -0.09640, -1.7171 0.2844, -0.10270, -1.6931 0.3225, -0.10690, -1.6731 0.3608, -0.10890, -1.5917 0.3991, -0.10830, -1.4363 0.4373, -0.10510, -1.1652 0.4757, -0.09890, -0.8475 0.5137, -0.09070, -0.6971 0.5694, -0.07640, -0.6564 15 Flap element taps 1.0000, 0.00130, -0.6061 0.9365, 0.01390, 0.1530 0.8333, 0.03280, 0.5040 0.7436, 0.04930, 0.7308 0.7049, 0.05670, 0.8241 0.6662, 0.06410, 0.8348 0.6522, 0.01390, -0.5794 0.5969, -0.00020, -0.6196 0.6000, -0.03020, -0.6133 0.6324, -0.04540, -0.6120 0.6667, -0.04880, -0.6157 0.7046, -0.04110, -0.6221 0.7429, -0.03210, -0.6234 0.8333, -0.01400, -0.6263 0.9311, -0.00120, -0.6267 --------- Run Conditions: vel=213.0 ft/s Re=1.997x10^6 AOA=0.05 Flap deflection=-45.00 Totals: Cl=-1.4386 Cdp=0.2182 Cm(c/4)=0.2276 Cs=-0.2194 Ch=0.3177 Main component: Cl=-1.1731 Cdp=-0.0106 Cm=0.3500 Flap component: Cl=-0.2655 Cdp=0.2288 Cm=0.2371 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7095 0.6175, -0.04610, -0.5901 0.5841, -0.02440, -0.5873 0.5775, 0.01750, -0.5862 0.5777, 0.04660, -0.5840 0.6274, 0.07170, 0.7823 0.5694, 0.08320, 0.7118 0.5112, 0.09370, 0.5464 0.4731, 0.09830, 0.3641 0.4349, 0.10070, 0.3399 0.3960, 0.10120, 0.3158 0.3566, 0.10020, 0.2966 0.3172, 0.09790, 0.2965 0.2778, 0.09440, 0.2988 0.2393, 0.08960, 0.3117 0.2056, 0.08360, 0.3450 0.1633, 0.07610, 0.3999 0.1261, 0.06710, 0.4836 0.0900, 0.05640, 0.5925 0.0571, 0.04390, 0.7538 0.0283, 0.02940, 0.9457 0.0142, 0.01970, 1.0131 0.0081, 0.01410, 0.9490 0.0026, 0.00780, 0.4301 0.0000, 0.00000, -1.4061 0.0037, -0.00840, -2.4534 0.0112, -0.01420, -2.0016 0.0191, -0.01930, -1.6950 0.0397, -0.03030, -1.2114 0.0706, -0.04420, -1.1753 0.1037, -0.05710, -1.2461 0.1384, -0.06890, -1.3196 0.1741, -0.07950, -1.3859 0.2102, -0.08660, -1.4975 0.2472, -0.09640, -1.6448 0.2844, -0.10270, -1.7144 0.3225, -0.10690, -1.7848 0.3608, -0.10890, -1.8282 0.3991, -0.10830, -1.8035 0.4373, -0.10510, -1.7114 0.4757, -0.09890, -1.4665 0.5137, -0.09070, -1.2772 0.5694, -0.07640, -0.9302 15 Flap element taps 1.0000, 0.00130, -0.6277 0.9365, 0.01390, 0.1221 0.8333, 0.03280, 0.4718 0.7436, 0.04930, 0.7089 0.7049, 0.05670, 0.8045 0.6662, 0.06410, 0.8026 0.6522, 0.01390, -0.5791 0.5969, -0.00020, -0.6193 0.6000, -0.03020, -0.6406 0.6324, -0.04540, -0.6186 0.6667, -0.04880, -0.6218 0.7046, -0.04110, -0.6234 0.7429, -0.03210, -0.6257 0.8333, -0.01400, -0.6311 0.9311, -0.00120, -0.6335 --------- Run Conditions: vel=213.6 ft/s Re=1.995x10^6 AOA=3.09 Flap deflection=-45.00 Totals: Cl=-1.2759 Cdp=0.1815 Cm(c/4)=0.2308 Cs=-0.2500 Ch=0.3031 Main component: Cl=-1.0112 Cdp=-0.0232 Cm=0.3206 Flap component: Cl=-0.2647 Cdp=0.2047 Cm=0.2263 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6982 0.6175, -0.04610, -0.5440 0.5841, -0.02440, -0.5408 0.5775, 0.01750, -0.5420 0.5777, 0.04660, -0.5381 0.6274, 0.07170, 0.7440 0.5694, 0.08320, 0.6920 0.5112, 0.09370, 0.5115 0.4731, 0.09830, 0.3508 0.4349, 0.10070, 0.2773 0.3960, 0.10120, 0.2507 0.3566, 0.10020, 0.2209 0.3172, 0.09790, 0.2098 0.2778, 0.09440, 0.1995 0.2393, 0.08960, 0.1989 0.2056, 0.08360, 0.2182 0.1633, 0.07610, 0.2569 0.1261, 0.06710, 0.3267 0.0900, 0.05640, 0.4197 0.0571, 0.04390, 0.5753 0.0283, 0.02940, 0.7965 0.0142, 0.01970, 0.9663 0.0081, 0.01410, 1.0095 0.0026, 0.00780, 0.8132 0.0000, 0.00000, -0.1140 0.0037, -0.00840, -1.1340 0.0112, -0.01420, -1.0166 0.0191, -0.01930, -0.8958 0.0397, -0.03030, -0.7847 0.0706, -0.04420, -0.8204 0.1037, -0.05710, -0.9398 0.1384, -0.06890, -1.0525 0.1741, -0.07950, -1.1712 0.2102, -0.08660, -1.3008 0.2472, -0.09640, -1.4671 0.2844, -0.10270, -1.5634 0.3225, -0.10690, -1.6723 0.3608, -0.10890, -1.7375 0.3991, -0.10830, -1.7527 0.4373, -0.10510, -1.6681 0.4757, -0.09890, -1.5610 0.5137, -0.09070, -1.1815 0.5694, -0.07640, -0.8981 15 Flap element taps 1.0000, 0.00130, -0.5768 0.9365, 0.01390, 0.1176 0.8333, 0.03280, 0.4589 0.7436, 0.04930, 0.7017 0.7049, 0.05670, 0.7909 0.6662, 0.06410, 0.7543 0.6522, 0.01390, -0.5333 0.5969, -0.00020, -0.5716 0.6000, -0.03020, -0.5937 0.6324, -0.04540, -0.5727 0.6667, -0.04880, -0.5740 0.7046, -0.04110, -0.5783 0.7429, -0.03210, -0.5850 0.8333, -0.01400, -0.5943 0.9311, -0.00120, -0.5994 --------- Run Conditions: vel=214.6 ft/s Re=2.000x10^6 AOA=6.06 Flap deflection=-45.00 Totals: Cl=-1.0405 Cdp=0.1714 Cm(c/4)=0.2358 Cs=-0.2803 Ch=0.2954 Main component: Cl=-0.7720 Cdp=-0.0123 Cm=0.2689 Flap component: Cl=-0.2685 Cdp=0.1837 Cm=0.2209 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6775 0.6175, -0.04610, -0.5478 0.5841, -0.02440, -0.5443 0.5775, 0.01750, -0.5484 0.5777, 0.04660, -0.5456 0.6274, 0.07170, 0.6616 0.5694, 0.08320, 0.6515 0.5112, 0.09370, 0.4815 0.4731, 0.09830, 0.3360 0.4349, 0.10070, 0.2200 0.3960, 0.10120, 0.1579 0.3566, 0.10020, 0.1189 0.3172, 0.09790, 0.0939 0.2778, 0.09440, 0.0675 0.2393, 0.08960, 0.0479 0.2056, 0.08360, 0.0485 0.1633, 0.07610, 0.0632 0.1261, 0.06710, 0.1103 0.0900, 0.05640, 0.1721 0.0571, 0.04390, 0.2986 0.0283, 0.02940, 0.5057 0.0142, 0.01970, 0.7323 0.0081, 0.01410, 0.8706 0.0026, 0.00780, 0.9969 0.0000, 0.00000, 0.7978 0.0037, -0.00840, 0.0484 0.0112, -0.01420, -0.1215 0.0191, -0.01930, -0.1675 0.0397, -0.03030, -0.2483 0.0706, -0.04420, -0.3891 0.1037, -0.05710, -0.5564 0.1384, -0.06890, -0.7069 0.1741, -0.07950, -0.8509 0.2102, -0.08660, -1.0004 0.2472, -0.09640, -1.1850 0.2844, -0.10270, -1.3019 0.3225, -0.10690, -1.4326 0.3608, -0.10890, -1.5201 0.3991, -0.10830, -1.5625 0.4373, -0.10510, -1.5095 0.4757, -0.09890, -1.3924 0.5137, -0.09070, -1.1041 0.5694, -0.07640, -0.8429 15 Flap element taps 1.0000, 0.00130, -0.5754 0.9365, 0.01390, 0.0944 0.8333, 0.03280, 0.4396 0.7436, 0.04930, 0.6935 0.7049, 0.05670, 0.7485 0.6662, 0.06410, 0.6626 0.6522, 0.01390, -0.5425 0.5969, -0.00020, -0.5735 0.6000, -0.03020, -0.5971 0.6324, -0.04540, -0.5758 0.6667, -0.04880, -0.5769 0.7046, -0.04110, -0.5793 0.7429, -0.03210, -0.5833 0.8333, -0.01400, -0.5908 0.9311, -0.00120, -0.5934 --------- Run Conditions: vel=215.2 ft/s Re=1.997x10^6 AOA=9.06 Flap deflection=-45.00 Totals: Cl=-0.7940 Cdp=0.1605 Cm(c/4)=0.2388 Cs=-0.2835 Ch=0.2863 Main component: Cl=-0.5274 Cdp=-0.0003 Cm=0.2159 Flap component: Cl=-0.2665 Cdp=0.1608 Cm=0.2126 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6411 0.6175, -0.04610, -0.5426 0.5841, -0.02440, -0.5399 0.5775, 0.01750, -0.5417 0.5777, 0.04660, -0.5388 0.6274, 0.07170, 0.5569 0.5694, 0.08320, 0.5635 0.5112, 0.09370, 0.4745 0.4731, 0.09830, 0.2955 0.4349, 0.10070, 0.1722 0.3960, 0.10120, 0.1187 0.3566, 0.10020, 0.0172 0.3172, 0.09790, -0.0332 0.2778, 0.09440, -0.0725 0.2393, 0.08960, -0.1131 0.2056, 0.08360, -0.1361 0.1633, 0.07610, -0.1523 0.1261, 0.06710, -0.1378 0.0900, 0.05640, -0.1209 0.0571, 0.04390, -0.0545 0.0283, 0.02940, 0.0825 0.0142, 0.01970, 0.2834 0.0081, 0.01410, 0.4429 0.0026, 0.00780, 0.6721 0.0000, 0.00000, 1.0031 0.0037, -0.00840, 0.7728 0.0112, -0.01420, 0.5235 0.0191, -0.01930, 0.3969 0.0397, -0.03030, 0.2065 0.0706, -0.04420, 0.0018 0.1037, -0.05710, -0.1951 0.1384, -0.06890, -0.3724 0.1741, -0.07950, -0.5348 0.2102, -0.08660, -0.6979 0.2472, -0.09640, -0.8940 0.2844, -0.10270, -1.0280 0.3225, -0.10690, -1.1765 0.3608, -0.10890, -1.2833 0.3991, -0.10830, -1.3515 0.4373, -0.10510, -1.3303 0.4757, -0.09890, -1.2142 0.5137, -0.09070, -1.1193 0.5694, -0.07640, -0.7679 15 Flap element taps 1.0000, 0.00130, -0.5615 0.9365, 0.01390, 0.0752 0.8333, 0.03280, 0.4300 0.7436, 0.04930, 0.6664 0.7049, 0.05670, 0.6173 0.6662, 0.06410, 0.5602 0.6522, 0.01390, -0.5389 0.5969, -0.00020, -0.5673 0.6000, -0.03020, -0.5909 0.6324, -0.04540, -0.5707 0.6667, -0.04880, -0.5708 0.7046, -0.04110, -0.5732 0.7429, -0.03210, -0.5760 0.8333, -0.01400, -0.5853 0.9311, -0.00120, -0.5859 --------- Run Conditions: vel=215.5 ft/s Re=1.997x10^6 AOA=12.05 Flap deflection=-45.00 Totals: Cl=-0.5347 Cdp=0.1484 Cm(c/4)=0.2366 Cs=-0.2568 Ch=0.2747 Main component: Cl=-0.2765 Cdp=0.0125 Cm=0.1586 Flap component: Cl=-0.2581 Cdp=0.1359 Cm=0.2009 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6010 0.6175, -0.04610, -0.5364 0.5841, -0.02440, -0.5330 0.5775, 0.01750, -0.5318 0.5777, 0.04660, -0.5316 0.6274, 0.07170, 0.4404 0.5694, 0.08320, 0.4499 0.5112, 0.09370, 0.4341 0.4731, 0.09830, 0.2909 0.4349, 0.10070, 0.1271 0.3960, 0.10120, 0.0401 0.3566, 0.10020, -0.0505 0.3172, 0.09790, -0.1003 0.2778, 0.09440, -0.2171 0.2393, 0.08960, -0.2868 0.2056, 0.08360, -0.3318 0.1633, 0.07610, -0.3842 0.1261, 0.06710, -0.4103 0.0900, 0.05640, -0.4532 0.0571, 0.04390, -0.4752 0.0283, 0.02940, -0.4637 0.0142, 0.01970, -0.3793 0.0081, 0.01410, -0.2903 0.0026, 0.00780, -0.0324 0.0000, 0.00000, 0.5035 0.0037, -0.00840, 1.0087 0.0112, -0.01420, 0.8979 0.0191, -0.01930, 0.7783 0.0397, -0.03030, 0.5613 0.0706, -0.04420, 0.3326 0.1037, -0.05710, 0.1241 0.1384, -0.06890, -0.0684 0.1741, -0.07950, -0.2407 0.2102, -0.08660, -0.4100 0.2472, -0.09640, -0.6140 0.2844, -0.10270, -0.7601 0.3225, -0.10690, -0.9226 0.3608, -0.10890, -1.0444 0.3991, -0.10830, -1.1347 0.4373, -0.10510, -1.1434 0.4757, -0.09890, -1.0440 0.5137, -0.09070, -0.9822 0.5694, -0.07640, -0.6799 15 Flap element taps 1.0000, 0.00130, -0.5438 0.9365, 0.01390, 0.0673 0.8333, 0.03280, 0.4325 0.7436, 0.04930, 0.5842 0.7049, 0.05670, 0.4738 0.6662, 0.06410, 0.4378 0.6522, 0.01390, -0.5238 0.5969, -0.00020, -0.5535 0.6000, -0.03020, -0.5745 0.6324, -0.04540, -0.5521 0.6667, -0.04880, -0.5529 0.7046, -0.04110, -0.5563 0.7429, -0.03210, -0.5579 0.8333, -0.01400, -0.5691 0.9311, -0.00120, -0.5730 --------- Run Conditions: vel=224.0 ft/s Re=2.024x10^6 AOA=15.03 Flap deflection=-45.00 Totals: Cl=-0.2638 Cdp=0.1319 Cm(c/4)=0.2219 Cs=-0.1958 Ch=0.2492 Main component: Cl=-0.0358 Cdp=0.0285 Cm=0.1018 Flap component: Cl=-0.2280 Cdp=0.1034 Cm=0.1752 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5523 0.6175, -0.04610, -0.5250 0.5841, -0.02440, -0.5232 0.5775, 0.01750, -0.5256 0.5777, 0.04660, -0.5224 0.6274, 0.07170, 0.2582 0.5694, 0.08320, 0.2509 0.5112, 0.09370, 0.2632 0.4731, 0.09830, 0.2587 0.4349, 0.10070, 0.1911 0.3960, 0.10120, 0.0728 0.3566, 0.10020, -0.0866 0.3172, 0.09790, -0.1914 0.2778, 0.09440, -0.3063 0.2393, 0.08960, -0.4097 0.2056, 0.08360, -0.4918 0.1633, 0.07610, -0.6010 0.1261, 0.06710, -0.6530 0.0900, 0.05640, -0.8187 0.0571, 0.04390, -0.9510 0.0283, 0.02940, -1.1205 0.0142, 0.01970, -1.2369 0.0081, 0.01410, -1.2951 0.0026, 0.00780, -1.1035 0.0000, 0.00000, -0.8184 0.0037, -0.00840, 0.8582 0.0112, -0.01420, 1.0109 0.0191, -0.01930, 0.9768 0.0397, -0.03030, 0.8120 0.0706, -0.04420, 0.5991 0.1037, -0.05710, 0.3990 0.1384, -0.06890, 0.1904 0.1741, -0.07950, 0.0199 0.2102, -0.08660, -0.1397 0.2472, -0.09640, -0.3504 0.2844, -0.10270, -0.5020 0.3225, -0.10690, -0.6831 0.3608, -0.10890, -0.8164 0.3991, -0.10830, -0.9313 0.4373, -0.10510, -0.9562 0.4757, -0.09890, -0.8849 0.5137, -0.09070, -0.8381 0.5694, -0.07640, -0.5916 15 Flap element taps 1.0000, 0.00130, -0.5366 0.9365, 0.01390, 0.0910 0.8333, 0.03280, 0.3837 0.7436, 0.04930, 0.2836 0.7049, 0.05670, 0.2544 0.6662, 0.06410, 0.2580 0.6522, 0.01390, -0.5147 0.5969, -0.00020, -0.5414 0.6000, -0.03020, -0.5576 0.6324, -0.04540, -0.5368 0.6667, -0.04880, -0.5314 0.7046, -0.04110, -0.5408 0.7429, -0.03210, -0.5405 0.8333, -0.01400, -0.5465 0.9311, -0.00120, -0.5571 --------- Run Conditions: vel=218.5 ft/s Re=2.006x10^6 AOA=18.03 Flap deflection=-45.00 Totals: Cl=0.0649 Cdp=0.1177 Cm(c/4)=0.1892 Cs=-0.0918 Ch=0.1959 Main component: Cl=0.2362 Cdp=0.0538 Cm=0.0333 Flap component: Cl=-0.1713 Cdp=0.0639 Cm=0.1313 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4764 0.6175, -0.04610, -0.5053 0.5841, -0.02440, -0.5040 0.5775, 0.01750, -0.5045 0.5777, 0.04660, -0.5033 0.6274, 0.07170, 0.0174 0.5694, 0.08320, 0.0130 0.5112, 0.09370, 0.0218 0.4731, 0.09830, 0.0282 0.4349, 0.10070, 0.0242 0.3960, 0.10120, 0.0088 0.3566, 0.10020, -0.0742 0.3172, 0.09790, -0.2135 0.2778, 0.09440, -0.3789 0.2393, 0.08960, -0.5368 0.2056, 0.08360, -0.6884 0.1633, 0.07610, -0.8392 0.1261, 0.06710, -0.9828 0.0900, 0.05640, -1.1970 0.0571, 0.04390, -1.4810 0.0283, 0.02940, -1.8900 0.0142, 0.01970, -2.3029 0.0081, 0.01410, -2.7553 0.0026, 0.00780, -2.6983 0.0000, 0.00000, -3.1110 0.0037, -0.00840, 0.2484 0.0112, -0.01420, 0.8960 0.0191, -0.01930, 1.0030 0.0397, -0.03030, 0.9695 0.0706, -0.04420, 0.8085 0.1037, -0.05710, 0.6324 0.1384, -0.06890, 0.4519 0.1741, -0.07950, 0.2847 0.2102, -0.08660, 0.1138 0.2472, -0.09640, -0.0821 0.2844, -0.10270, -0.2437 0.3225, -0.10690, -0.4152 0.3608, -0.10890, -0.5654 0.3991, -0.10830, -0.6854 0.4373, -0.10510, -0.7445 0.4757, -0.09890, -0.7056 0.5137, -0.09070, -0.6866 0.5694, -0.07640, -0.5569 15 Flap element taps 1.0000, 0.00130, -0.5035 0.9365, 0.01390, 0.0898 0.8333, 0.03280, 0.1798 0.7436, 0.04930, 0.0077 0.7049, 0.05670, -0.0061 0.6662, 0.06410, 0.0145 0.6522, 0.01390, -0.5003 0.5969, -0.00020, -0.5152 0.6000, -0.03020, -0.5245 0.6324, -0.04540, -0.5027 0.6667, -0.04880, -0.4925 0.7046, -0.04110, -0.4946 0.7429, -0.03210, -0.5000 0.8333, -0.01400, -0.5093 0.9311, -0.00120, -0.5133 --------- Run Conditions: vel=219.1 ft/s Re=2.007x10^6 AOA=20.04 Flap deflection=-45.00 Totals: Cl=0.3653 Cdp=0.1070 Cm(c/4)=0.1368 Cs=0.0246 Ch=0.1249 Main component: Cl=0.4566 Cdp=0.0892 Cm=-0.0330 Flap component: Cl=-0.0913 Cdp=0.0179 Cm=0.0748 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4130 0.6175, -0.04610, -0.4973 0.5841, -0.02440, -0.4955 0.5775, 0.01750, -0.4975 0.5777, 0.04660, -0.4965 0.6274, 0.07170, -0.2581 0.5694, 0.08320, -0.2795 0.5112, 0.09370, -0.2555 0.4731, 0.09830, -0.2425 0.4349, 0.10070, -0.2415 0.3960, 0.10120, -0.2323 0.3566, 0.10020, -0.2501 0.3172, 0.09790, -0.2777 0.2778, 0.09440, -0.3654 0.2393, 0.08960, -0.5294 0.2056, 0.08360, -0.7350 0.1633, 0.07610, -0.9529 0.1261, 0.06710, -1.1633 0.0900, 0.05640, -1.4632 0.0571, 0.04390, -1.8761 0.0283, 0.02940, -2.5120 0.0142, 0.01970, -3.1626 0.0081, 0.01410, -3.8994 0.0026, 0.00780, -4.0321 0.0000, 0.00000, -5.3028 0.0037, -0.00840, -0.4799 0.0112, -0.01420, 0.6489 0.0191, -0.01930, 0.9164 0.0397, -0.03030, 1.0109 0.0706, -0.04420, 0.9168 0.1037, -0.05710, 0.7730 0.1384, -0.06890, 0.6082 0.1741, -0.07950, 0.4527 0.2102, -0.08660, 0.2924 0.2472, -0.09640, 0.1046 0.2844, -0.10270, -0.0539 0.3225, -0.10690, -0.2252 0.3608, -0.10890, -0.3759 0.3991, -0.10830, -0.5031 0.4373, -0.10510, -0.5752 0.4757, -0.09890, -0.5584 0.5137, -0.09070, -0.5580 0.5694, -0.07640, -0.4556 15 Flap element taps 1.0000, 0.00130, -0.3855 0.9365, 0.01390, 0.0810 0.8333, 0.03280, 0.0138 0.7436, 0.04930, -0.2620 0.7049, 0.05670, -0.2909 0.6662, 0.06410, -0.2459 0.6522, 0.01390, -0.4910 0.5969, -0.00020, -0.5041 0.6000, -0.03020, -0.5028 0.6324, -0.04540, -0.4127 0.6667, -0.04880, -0.3777 0.7046, -0.04110, -0.3760 0.7429, -0.03210, -0.3843 0.8333, -0.01400, -0.3986 0.9311, -0.00120, -0.3964 --------- Run Conditions: vel=221.9 ft/s Re=2.032x10^6 AOA=24.03 Flap deflection=-45.00 Totals: Cl=0.3761 Cdp=0.2692 Cm(c/4)=0.0027 Cs=-0.0927 Ch=-0.0524 Main component: Cl=0.3144 Cdp=0.3210 Cm=-0.0751 Flap component: Cl=0.0617 Cdp=-0.0518 Cm=-0.0355 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7452 0.6175, -0.04610, -1.0128 0.5841, -0.02440, -1.0115 0.5775, 0.01750, -1.0114 0.5777, 0.04660, -1.0100 0.6274, 0.07170, -0.7226 0.5694, 0.08320, -0.7643 0.5112, 0.09370, -0.7807 0.4731, 0.09830, -0.7841 0.4349, 0.10070, -0.7805 0.3960, 0.10120, -0.7596 0.3566, 0.10020, -0.7644 0.3172, 0.09790, -0.7539 0.2778, 0.09440, -0.7506 0.2393, 0.08960, -0.7427 0.2056, 0.08360, -0.7338 0.1633, 0.07610, -0.7372 0.1261, 0.06710, -0.7237 0.0900, 0.05640, -0.7256 0.0571, 0.04390, -0.7241 0.0283, 0.02940, -0.7279 0.0142, 0.01970, -0.7379 0.0081, 0.01410, -0.7455 0.0026, 0.00780, -0.6965 0.0000, 0.00000, -1.0681 0.0037, -0.00840, 0.4243 0.0112, -0.01420, 0.8940 0.0191, -0.01930, 0.9944 0.0397, -0.03030, 0.9932 0.0706, -0.04420, 0.8778 0.1037, -0.05710, 0.7346 0.1384, -0.06890, 0.5713 0.1741, -0.07950, 0.4171 0.2102, -0.08660, 0.2553 0.2472, -0.09640, 0.0597 0.2844, -0.10270, -0.1081 0.3225, -0.10690, -0.2950 0.3608, -0.10890, -0.4650 0.3991, -0.10830, -0.6156 0.4373, -0.10510, -0.7114 0.4757, -0.09890, -0.7149 0.5137, -0.09070, -0.7453 0.5694, -0.07640, -0.6726 15 Flap element taps 1.0000, 0.00130, -0.8647 0.9365, 0.01390, -0.7794 0.8333, 0.03280, -0.8012 0.7436, 0.04930, -0.7896 0.7049, 0.05670, -0.7625 0.6662, 0.06410, -0.7277 0.6522, 0.01390, -1.0041 0.5969, -0.00020, -1.0204 0.6000, -0.03020, -1.0388 0.6324, -0.04540, -0.7728 0.6667, -0.04880, -0.5640 0.7046, -0.04110, -0.5455 0.7429, -0.03210, -0.5544 0.8333, -0.01400, -0.5706 0.9311, -0.00120, -0.5981 --------- Run Conditions: vel=220.2 ft/s Re=2.010x10^6 AOA=27.05 Flap deflection=-45.00 Totals: Cl=0.2978 Cdp=0.3115 Cm(c/4)=0.0296 Cs=-0.1420 Ch=-0.0080 Main component: Cl=0.2801 Cdp=0.3500 Cm=-0.0695 Flap component: Cl=0.0177 Cdp=-0.0386 Cm=-0.0025 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8178 0.6175, -0.04610, -1.1161 0.5841, -0.02440, -1.1151 0.5775, 0.01750, -1.1108 0.5777, 0.04660, -1.1105 0.6274, 0.07170, -0.7078 0.5694, 0.08320, -0.7228 0.5112, 0.09370, -0.7243 0.4731, 0.09830, -0.7268 0.4349, 0.10070, -0.7291 0.3960, 0.10120, -0.7140 0.3566, 0.10020, -0.7226 0.3172, 0.09790, -0.7159 0.2778, 0.09440, -0.7179 0.2393, 0.08960, -0.7114 0.2056, 0.08360, -0.7035 0.1633, 0.07610, -0.7108 0.1261, 0.06710, -0.7007 0.0900, 0.05640, -0.7062 0.0571, 0.04390, -0.7026 0.0283, 0.02940, -0.7085 0.0142, 0.01970, -0.7205 0.0081, 0.01410, -0.7236 0.0026, 0.00780, -0.6691 0.0000, 0.00000, -0.8217 0.0037, -0.00840, 0.3757 0.0112, -0.01420, 0.8634 0.0191, -0.01930, 0.9824 0.0397, -0.03030, 1.0050 0.0706, -0.04420, 0.9097 0.1037, -0.05710, 0.7782 0.1384, -0.06890, 0.6210 0.1741, -0.07950, 0.4698 0.2102, -0.08660, 0.3105 0.2472, -0.09640, 0.1143 0.2844, -0.10270, -0.0569 0.3225, -0.10690, -0.2505 0.3608, -0.10890, -0.4280 0.3991, -0.10830, -0.5906 0.4373, -0.10510, -0.6996 0.4757, -0.09890, -0.7167 0.5137, -0.09070, -0.7729 0.5694, -0.07640, -0.7210 15 Flap element taps 1.0000, 0.00130, -0.8271 0.9365, 0.01390, -0.7940 0.8333, 0.03280, -0.7433 0.7436, 0.04930, -0.7285 0.7049, 0.05670, -0.7168 0.6662, 0.06410, -0.7025 0.6522, 0.01390, -1.0978 0.5969, -0.00020, -1.1173 0.6000, -0.03020, -1.1437 0.6324, -0.04540, -0.9050 0.6667, -0.04880, -0.6765 0.7046, -0.04110, -0.6552 0.7429, -0.03210, -0.6726 0.8333, -0.01400, -0.6818 0.9311, -0.00120, -0.7180