S809 UNVENTED AILERON, LEGR, CHORD = 18 IN --------- Run Conditions: vel=103.8 ft/s Re=1.008x10^6 AOA=-5.99 Flap deflection=5.00 Totals: Cl=-0.2083 Cdp=0.0054 Cm(c/4)=-0.0501 Cs=0.0164 Ch=-0.0421 Main component: Cl=-0.2714 Cdp=0.0321 Cm=0.0525 Flap component: Cl=0.0632 Cdp=-0.0267 Cm=-0.0506 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1371 0.6175, -0.04610, -0.1164 0.5841, -0.02440, -0.1238 0.5775, 0.01750, -0.1407 0.5777, 0.04660, -0.1317 0.6274, 0.07170, -0.2280 0.5694, 0.08320, -0.3579 0.5112, 0.09370, -0.5613 0.4731, 0.09830, -0.6063 0.4349, 0.10070, -0.5937 0.3960, 0.10120, -0.5101 0.3566, 0.10020, -0.4575 0.3172, 0.09790, -0.3877 0.2778, 0.09440, -0.3448 0.2393, 0.08960, -0.3000 0.2056, 0.08360, -0.2245 0.1633, 0.07610, -0.1443 0.1261, 0.06710, -0.0151 0.0900, 0.05640, 0.0322 0.0571, 0.04390, 0.3311 0.0283, 0.02940, 0.6115 0.0142, 0.01970, 0.8578 0.0081, 0.01410, 0.9574 0.0026, 0.00780, 0.8744 0.0000, 0.00000, -0.3416 0.0037, -0.00840, -0.5381 0.0112, -0.01420, -0.4846 0.0191, -0.01930, -0.5371 0.0397, -0.03030, -0.4645 0.0706, -0.04420, -0.5354 0.1037, -0.05710, -0.5486 0.1384, -0.06890, -0.6751 0.1741, -0.07950, -0.7428 0.2102, -0.08660, -0.8296 0.2472, -0.09640, -0.9131 0.2844, -0.10270, -0.9540 0.3225, -0.10690, -0.9832 0.3608, -0.10890, -0.9871 0.3991, -0.10830, -0.9469 0.4373, -0.10510, -0.8351 0.4757, -0.09890, -0.6454 0.5137, -0.09070, -0.4678 0.5694, -0.07640, -0.2482 14 Flap element taps 1.0000, 0.00130, 0.1569 0.9365, 0.01390, 0.0909 0.8333, 0.03280, -0.0270 0.7436, 0.04930, -0.1595 0.7049, 0.05670, -0.2379 0.6662, 0.06410, -0.5072 0.6522, 0.01390, -0.1306 0.5969, -0.00020, -0.1400 0.6000, -0.03020, -0.1343 0.6324, -0.04540, -0.1187 0.6667, -0.04880, -0.0700 0.7046, -0.04110, 0.0151 0.7429, -0.03210, 0.0569 0.9311, -0.00120, 0.2257 Wake drag found for this condition, Cdw=0.0182 --------- Run Conditions: vel=103.8 ft/s Re=1.011x10^6 AOA=0.00 Flap deflection=5.00 Totals: Cl=0.3573 Cdp=-0.0118 Cm(c/4)=-0.0611 Cs=0.0118 Ch=-0.0936 Main component: Cl=0.2351 Cdp=-0.0020 Cm=-0.0552 Flap component: Cl=0.1222 Cdp=-0.0098 Cm=-0.0952 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.0570 0.6175, -0.04610, -0.0106 0.5841, -0.02440, -0.0423 0.5775, 0.01750, -0.0682 0.5777, 0.04660, -0.0418 0.6274, 0.07170, -0.2272 0.5694, 0.08320, -0.4339 0.5112, 0.09370, -0.7122 0.4731, 0.09830, -0.8116 0.4349, 0.10070, -0.8484 0.3960, 0.10120, -0.8020 0.3566, 0.10020, -0.7868 0.3172, 0.09790, -0.7522 0.2778, 0.09440, -0.7535 0.2393, 0.08960, -0.7525 0.2056, 0.08360, -0.7273 0.1633, 0.07610, -0.7003 0.1261, 0.06710, -0.6297 0.0900, 0.05640, -0.7275 0.0571, 0.04390, -0.4869 0.0283, 0.02940, -0.3217 0.0142, 0.01970, -0.1044 0.0081, 0.01410, 0.0020 0.0026, 0.00780, 0.2277 0.0000, 0.00000, -0.4858 0.0037, -0.00840, 0.9275 0.0112, -0.01420, 0.7375 0.0191, -0.01930, 0.5850 0.0397, -0.03030, 0.3950 0.0706, -0.04420, 0.2018 0.1037, -0.05710, 0.0800 0.1384, -0.06890, -0.0962 0.1741, -0.07950, -0.2097 0.2102, -0.08660, -0.3309 0.2472, -0.09640, -0.4496 0.2844, -0.10270, -0.5286 0.3225, -0.10690, -0.6015 0.3608, -0.10890, -0.6520 0.3991, -0.10830, -0.6647 0.4373, -0.10510, -0.6088 0.4757, -0.09890, -0.4816 0.5137, -0.09070, -0.3538 0.5694, -0.07640, -0.1612 14 Flap element taps 1.0000, 0.00130, -0.0257 0.9365, 0.01390, -0.0552 0.8333, 0.03280, -0.0880 0.7436, 0.04930, -0.1651 0.7049, 0.05670, -0.2437 0.6662, 0.06410, -0.5195 0.6522, 0.01390, -0.0571 0.5969, -0.00020, -0.0701 0.6000, -0.03020, -0.0525 0.6324, -0.04540, -0.0206 0.6667, -0.04880, 0.1852 0.7046, -0.04110, 0.2504 0.7429, -0.03210, 0.2349 0.9311, -0.00120, 0.2266 Wake drag found for this condition, Cdw=0.0180 --------- Run Conditions: vel=103.1 ft/s Re=1.007x10^6 AOA=3.03 Flap deflection=5.00 Totals: Cl=0.5873 Cdp=0.0000 Cm(c/4)=-0.0574 Cs=0.0310 Ch=-0.1120 Main component: Cl=0.4542 Cdp=-0.0043 Cm=-0.0991 Flap component: Cl=0.1331 Cdp=0.0044 Cm=-0.1050 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.0193 0.6175, -0.04610, 0.0065 0.5841, -0.02440, -0.0267 0.5775, 0.01750, -0.0539 0.5777, 0.04660, -0.0237 0.6274, 0.07170, -0.2008 0.5694, 0.08320, -0.4114 0.5112, 0.09370, -0.7163 0.4731, 0.09830, -0.8522 0.4349, 0.10070, -0.9203 0.3960, 0.10120, -0.9009 0.3566, 0.10020, -0.9095 0.3172, 0.09790, -0.8987 0.2778, 0.09440, -0.9242 0.2393, 0.08960, -0.9531 0.2056, 0.08360, -0.9587 0.1633, 0.07610, -0.9680 0.1261, 0.06710, -0.9417 0.0900, 0.05640, -1.1136 0.0571, 0.04390, -0.9537 0.0283, 0.02940, -0.9272 0.0142, 0.01970, -0.8054 0.0081, 0.01410, -0.9064 0.0026, 0.00780, -0.4179 0.0000, 0.00000, -0.6199 0.0037, -0.00840, 0.9826 0.0112, -0.01420, 0.9682 0.0191, -0.01930, 0.8747 0.0397, -0.03030, 0.6751 0.0706, -0.04420, 0.4641 0.1037, -0.05710, 0.3173 0.1384, -0.06890, 0.1389 0.1741, -0.07950, 0.0066 0.2102, -0.08660, -0.1263 0.2472, -0.09640, -0.2551 0.2844, -0.10270, -0.3455 0.3225, -0.10690, -0.4289 0.3608, -0.10890, -0.4958 0.3991, -0.10830, -0.5282 0.4373, -0.10510, -0.4939 0.4757, -0.09890, -0.3907 0.5137, -0.09070, -0.2801 0.5694, -0.07640, -0.1077 14 Flap element taps 1.0000, 0.00130, -0.1029 0.9365, 0.01390, -0.1394 0.8333, 0.03280, -0.1512 0.7436, 0.04930, -0.1576 0.7049, 0.05670, -0.1910 0.6662, 0.06410, -0.3797 0.6522, 0.01390, -0.0425 0.5969, -0.00020, -0.0551 0.6000, -0.03020, -0.0377 0.6324, -0.04540, -0.0043 0.6667, -0.04880, 0.2682 0.7046, -0.04110, 0.2885 0.7429, -0.03210, 0.2561 0.9311, -0.00120, 0.2117 Wake drag found for this condition, Cdw=0.0229 --------- Run Conditions: vel=103.0 ft/s Re=1.009x10^6 AOA=6.00 Flap deflection=5.00 Totals: Cl=0.7466 Cdp=0.0425 Cm(c/4)=-0.0511 Cs=0.0569 Ch=-0.1402 Main component: Cl=0.5940 Cdp=0.0142 Cm=-0.1144 Flap component: Cl=0.1525 Cdp=0.0283 Cm=-0.1231 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0102 0.6175, -0.04610, 0.0133 0.5841, -0.02440, -0.0286 0.5775, 0.01750, -0.0557 0.5777, 0.04660, -0.0230 0.6274, 0.07170, -0.1876 0.5694, 0.08320, -0.2463 0.5112, 0.09370, -0.4829 0.4731, 0.09830, -0.6867 0.4349, 0.10070, -0.8309 0.3960, 0.10120, -0.8767 0.3566, 0.10020, -0.9250 0.3172, 0.09790, -0.9563 0.2778, 0.09440, -1.0225 0.2393, 0.08960, -1.0865 0.2056, 0.08360, -1.1324 0.1633, 0.07610, -1.1835 0.1261, 0.06710, -1.2094 0.0900, 0.05640, -1.4513 0.0571, 0.04390, -1.4010 0.0283, 0.02940, -1.5388 0.0142, 0.01970, -1.6345 0.0081, 0.01410, -1.7833 0.0026, 0.00780, -1.3911 0.0000, 0.00000, -0.7646 0.0037, -0.00840, 0.7556 0.0112, -0.01420, 1.0068 0.0191, -0.01930, 1.0035 0.0397, -0.03030, 0.8591 0.0706, -0.04420, 0.6618 0.1037, -0.05710, 0.5053 0.1384, -0.06890, 0.3347 0.1741, -0.07950, 0.1925 0.2102, -0.08660, 0.0513 0.2472, -0.09640, -0.0841 0.2844, -0.10270, -0.1922 0.3225, -0.10690, -0.2864 0.3608, -0.10890, -0.3702 0.3991, -0.10830, -0.4253 0.4373, -0.10510, -0.4054 0.4757, -0.09890, -0.3283 0.5137, -0.09070, -0.2236 0.5694, -0.07640, -0.0576 14 Flap element taps 1.0000, 0.00130, -0.1997 0.9365, 0.01390, -0.2535 0.8333, 0.03280, -0.2556 0.7436, 0.04930, -0.2391 0.7049, 0.05670, -0.2349 0.6662, 0.06410, -0.2400 0.6522, 0.01390, -0.0445 0.5969, -0.00020, -0.0576 0.6000, -0.03020, -0.0393 0.6324, -0.04540, -0.0055 0.6667, -0.04880, 0.3266 0.7046, -0.04110, 0.3085 0.7429, -0.03210, 0.2654 0.9311, -0.00120, 0.1808 Wake drag found for this condition, Cdw=0.0309 --------- Run Conditions: vel=102.5 ft/s Re=1.008x10^6 AOA=8.99 Flap deflection=5.00 Totals: Cl=0.8950 Cdp=0.0510 Cm(c/4)=-0.0501 Cs=0.0894 Ch=-0.1580 Main component: Cl=0.7212 Cdp=0.0132 Cm=-0.1325 Flap component: Cl=0.1738 Cdp=0.0379 Cm=-0.1406 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0388 0.6175, -0.04610, -0.0040 0.5841, -0.02440, -0.0545 0.5775, 0.01750, -0.0831 0.5777, 0.04660, -0.0420 0.6274, 0.07170, -0.2597 0.5694, 0.08320, -0.2922 0.5112, 0.09370, -0.3564 0.4731, 0.09830, -0.5018 0.4349, 0.10070, -0.6912 0.3960, 0.10120, -0.8025 0.3566, 0.10020, -0.8975 0.3172, 0.09790, -0.9710 0.2778, 0.09440, -1.0743 0.2393, 0.08960, -1.1749 0.2056, 0.08360, -1.2650 0.1633, 0.07610, -1.3583 0.1261, 0.06710, -1.4395 0.0900, 0.05640, -1.7356 0.0571, 0.04390, -1.8181 0.0283, 0.02940, -2.1494 0.0142, 0.01970, -2.4665 0.0081, 0.01410, -2.8271 0.0026, 0.00780, -2.4827 0.0000, 0.00000, -0.9227 0.0037, -0.00840, 0.3028 0.0112, -0.01420, 0.9140 0.0191, -0.01930, 1.0173 0.0397, -0.03030, 0.9668 0.0706, -0.04420, 0.8030 0.1037, -0.05710, 0.6536 0.1384, -0.06890, 0.4944 0.1741, -0.07950, 0.3484 0.2102, -0.08660, 0.2027 0.2472, -0.09640, 0.0673 0.2844, -0.10270, -0.0530 0.3225, -0.10690, -0.1563 0.3608, -0.10890, -0.2552 0.3991, -0.10830, -0.3187 0.4373, -0.10510, -0.3175 0.4757, -0.09890, -0.2624 0.5137, -0.09070, -0.1836 0.5694, -0.07640, -0.0007 14 Flap element taps 1.0000, 0.00130, -0.2745 0.9365, 0.01390, -0.3284 0.8333, 0.03280, -0.3182 0.7436, 0.04930, -0.3004 0.7049, 0.05670, -0.2914 0.6662, 0.06410, -0.2883 0.6522, 0.01390, -0.0742 0.5969, -0.00020, -0.0868 0.6000, -0.03020, -0.0640 0.6324, -0.04540, -0.0297 0.6667, -0.04880, 0.4481 0.7046, -0.04110, 0.3212 0.7429, -0.03210, 0.2712 0.9311, -0.00120, 0.1591 --------- Run Conditions: vel=102.1 ft/s Re=1.008x10^6 AOA=11.98 Flap deflection=5.00 Totals: Cl=0.9984 Cdp=0.0953 Cm(c/4)=-0.0544 Cs=0.1140 Ch=-0.1773 Main component: Cl=0.8032 Cdp=0.0415 Cm=-0.1440 Flap component: Cl=0.1952 Cdp=0.0539 Cm=-0.1595 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0611 0.6175, -0.04610, -0.0272 0.5841, -0.02440, -0.0880 0.5775, 0.01750, -0.1227 0.5777, 0.04660, -0.0719 0.6274, 0.07170, -0.3597 0.5694, 0.08320, -0.3783 0.5112, 0.09370, -0.3927 0.4731, 0.09830, -0.4143 0.4349, 0.10070, -0.5269 0.3960, 0.10120, -0.6607 0.3566, 0.10020, -0.7874 0.3172, 0.09790, -0.9083 0.2778, 0.09440, -1.0491 0.2393, 0.08960, -1.1854 0.2056, 0.08360, -1.3186 0.1633, 0.07610, -1.4492 0.1261, 0.06710, -1.5874 0.0900, 0.05640, -1.9273 0.0571, 0.04390, -2.1384 0.0283, 0.02940, -2.6588 0.0142, 0.01970, -3.1955 0.0081, 0.01410, -3.7133 0.0026, 0.00780, -3.4969 0.0000, 0.00000, -1.1038 0.0037, -0.00840, -0.2397 0.0112, -0.01420, 0.7356 0.0191, -0.01930, 0.9621 0.0397, -0.03030, 1.0102 0.0706, -0.04420, 0.8909 0.1037, -0.05710, 0.7551 0.1384, -0.06890, 0.6106 0.1741, -0.07950, 0.4711 0.2102, -0.08660, 0.3159 0.2472, -0.09640, 0.1814 0.2844, -0.10270, 0.0554 0.3225, -0.10690, -0.0508 0.3608, -0.10890, -0.1635 0.3991, -0.10830, -0.2345 0.4373, -0.10510, -0.2489 0.4757, -0.09890, -0.2076 0.5137, -0.09070, -0.1371 0.5694, -0.07640, -0.0266 14 Flap element taps 1.0000, 0.00130, -0.3495 0.9365, 0.01390, -0.4108 0.8333, 0.03280, -0.3914 0.7436, 0.04930, -0.3757 0.7049, 0.05670, -0.3706 0.6662, 0.06410, -0.3659 0.6522, 0.01390, -0.1174 0.5969, -0.00020, -0.1272 0.6000, -0.03020, -0.1000 0.6324, -0.04540, -0.0602 0.6667, -0.04880, 0.5396 0.7046, -0.04110, 0.3263 0.7429, -0.03210, 0.2694 0.9311, -0.00120, 0.1340 --------- Run Conditions: vel=100.9 ft/s Re=1.001x10^6 AOA=15.00 Flap deflection=5.00 Totals: Cl=0.9378 Cdp=0.1882 Cm(c/4)=-0.0848 Cs=0.0609 Ch=-0.2128 Main component: Cl=0.7055 Cdp=0.1089 Cm=-0.1305 Flap component: Cl=0.2323 Cdp=0.0793 Cm=-0.1929 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0139 0.6175, -0.04610, -0.1241 0.5841, -0.02440, -0.1911 0.5775, 0.01750, -0.2404 0.5777, 0.04660, -0.1831 0.6274, 0.07170, -0.5823 0.5694, 0.08320, -0.5740 0.5112, 0.09370, -0.5728 0.4731, 0.09830, -0.5641 0.4349, 0.10070, -0.5651 0.3960, 0.10120, -0.5773 0.3566, 0.10020, -0.5929 0.3172, 0.09790, -0.6259 0.2778, 0.09440, -0.6887 0.2393, 0.08960, -0.7937 0.2056, 0.08360, -0.9496 0.1633, 0.07610, -1.1238 0.1261, 0.06710, -1.3149 0.0900, 0.05640, -1.6510 0.0571, 0.04390, -1.9564 0.0283, 0.02940, -2.5151 0.0142, 0.01970, -3.1191 0.0081, 0.01410, -3.6610 0.0026, 0.00780, -3.5562 0.0000, 0.00000, -0.4460 0.0037, -0.00840, -0.3403 0.0112, -0.01420, 0.6881 0.0191, -0.01930, 0.9338 0.0397, -0.03030, 1.0126 0.0706, -0.04420, 0.9072 0.1037, -0.05710, 0.7769 0.1384, -0.06890, 0.6313 0.1741, -0.07950, 0.4936 0.2102, -0.08660, 0.3336 0.2472, -0.09640, 0.1849 0.2844, -0.10270, 0.0534 0.3225, -0.10690, -0.0537 0.3608, -0.10890, -0.1801 0.3991, -0.10830, -0.2521 0.4373, -0.10510, -0.2804 0.4757, -0.09890, -0.2383 0.5137, -0.09070, -0.1879 0.5694, -0.07640, -0.0914 14 Flap element taps 1.0000, 0.00130, -0.5502 0.9365, 0.01390, -0.5794 0.8333, 0.03280, -0.5917 0.7436, 0.04930, -0.5786 0.7049, 0.05670, -0.5714 0.6662, 0.06410, -0.5646 0.6522, 0.01390, -0.2301 0.5969, -0.00020, -0.2398 0.6000, -0.03020, -0.2092 0.6324, -0.04540, -0.1631 0.6667, -0.04880, 0.5632 0.7046, -0.04110, 0.2881 0.7429, -0.03210, 0.2198 0.9311, -0.00120, 0.0476 --------- Run Conditions: vel=100.2 ft/s Re=0.996x10^6 AOA=18.00 Flap deflection=5.00 Totals: Cl=0.8443 Cdp=0.2949 Cm(c/4)=-0.1241 Cs=-0.0196 Ch=-0.2290 Main component: Cl=0.5975 Cdp=0.1970 Cm=-0.1391 Flap component: Cl=0.2468 Cdp=0.0980 Cm=-0.2086 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.0004 0.6175, -0.04610, -0.1661 0.5841, -0.02440, -0.2478 0.5775, 0.01750, -0.3004 0.5777, 0.04660, -0.2335 0.6274, 0.07170, -0.7189 0.5694, 0.08320, -0.7151 0.5112, 0.09370, -0.6987 0.4731, 0.09830, -0.6932 0.4349, 0.10070, -0.7080 0.3960, 0.10120, -0.7373 0.3566, 0.10020, -0.7358 0.3172, 0.09790, -0.7463 0.2778, 0.09440, -0.7621 0.2393, 0.08960, -0.7770 0.2056, 0.08360, -0.8273 0.1633, 0.07610, -0.8476 0.1261, 0.06710, -0.8858 0.0900, 0.05640, -0.9140 0.0571, 0.04390, -1.0440 0.0283, 0.02940, -1.3806 0.0142, 0.01970, -1.9044 0.0081, 0.01410, -2.3995 0.0026, 0.00780, -2.4609 0.0000, 0.00000, -0.5946 0.0037, -0.00840, -0.0944 0.0112, -0.01420, 0.7421 0.0191, -0.01930, 0.9470 0.0397, -0.03030, 1.0106 0.0706, -0.04420, 0.9070 0.1037, -0.05710, 0.7843 0.1384, -0.06890, 0.6594 0.1741, -0.07950, 0.5237 0.2102, -0.08660, 0.3547 0.2472, -0.09640, 0.2146 0.2844, -0.10270, 0.0747 0.3225, -0.10690, -0.0250 0.3608, -0.10890, -0.1622 0.3991, -0.10830, -0.2337 0.4373, -0.10510, -0.2760 0.4757, -0.09890, -0.2414 0.5137, -0.09070, -0.1978 0.5694, -0.07640, -0.1067 14 Flap element taps 1.0000, 0.00130, -0.5848 0.9365, 0.01390, -0.6443 0.8333, 0.03280, -0.6845 0.7436, 0.04930, -0.6642 0.7049, 0.05670, -0.6512 0.6662, 0.06410, -0.6329 0.6522, 0.01390, -0.2962 0.5969, -0.00020, -0.3043 0.6000, -0.03020, -0.2672 0.6324, -0.04540, -0.2194 0.6667, -0.04880, 0.5857 0.7046, -0.04110, 0.2723 0.7429, -0.03210, 0.1993 0.9311, -0.00120, 0.0198 --------- Run Conditions: vel=99.9 ft/s Re=0.995x10^6 AOA=19.99 Flap deflection=5.00 Totals: Cl=0.9865 Cdp=0.3636 Cm(c/4)=-0.1393 Cs=-0.0045 Ch=-0.2476 Main component: Cl=0.7216 Cdp=0.2474 Cm=-0.1753 Flap component: Cl=0.2649 Cdp=0.1162 Cm=-0.2269 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0172 0.6175, -0.04610, -0.1670 0.5841, -0.02440, -0.2604 0.5775, 0.01750, -0.3175 0.5777, 0.04660, -0.2428 0.6274, 0.07170, -0.7633 0.5694, 0.08320, -0.7743 0.5112, 0.09370, -0.7833 0.4731, 0.09830, -0.8014 0.4349, 0.10070, -0.8275 0.3960, 0.10120, -0.8829 0.3566, 0.10020, -0.8677 0.3172, 0.09790, -0.9047 0.2778, 0.09440, -0.9463 0.2393, 0.08960, -0.9870 0.2056, 0.08360, -1.0610 0.1633, 0.07610, -1.0673 0.1261, 0.06710, -1.1826 0.0900, 0.05640, -1.2471 0.0571, 0.04390, -1.3800 0.0283, 0.02940, -1.5639 0.0142, 0.01970, -1.9410 0.0081, 0.01410, -2.3957 0.0026, 0.00780, -2.4428 0.0000, 0.00000, -0.7272 0.0037, -0.00840, -0.3007 0.0112, -0.01420, 0.6453 0.0191, -0.01930, 0.9012 0.0397, -0.03030, 1.0175 0.0706, -0.04420, 0.9409 0.1037, -0.05710, 0.8308 0.1384, -0.06890, 0.7316 0.1741, -0.07950, 0.5974 0.2102, -0.08660, 0.4202 0.2472, -0.09640, 0.2897 0.2844, -0.10270, 0.1452 0.3225, -0.10690, 0.0555 0.3608, -0.10890, -0.0909 0.3991, -0.10830, -0.1609 0.4373, -0.10510, -0.2185 0.4757, -0.09890, -0.1936 0.5137, -0.09070, -0.1564 0.5694, -0.07640, -0.0654 14 Flap element taps 1.0000, 0.00130, -0.6536 0.9365, 0.01390, -0.7069 0.8333, 0.03280, -0.7311 0.7436, 0.04930, -0.7329 0.7049, 0.05670, -0.7271 0.6662, 0.06410, -0.7373 0.6522, 0.01390, -0.3159 0.5969, -0.00020, -0.3191 0.6000, -0.03020, -0.2796 0.6324, -0.04540, -0.2333 0.6667, -0.04880, 0.6571 0.7046, -0.04110, 0.2889 0.7429, -0.03210, 0.2089 0.9311, -0.00120, 0.0157 --------- Run Conditions: vel=100.2 ft/s Re=0.999x10^6 AOA=23.98 Flap deflection=5.00 Totals: Cl=1.0691 Cdp=0.4860 Cm(c/4)=-0.1528 Cs=-0.0095 Ch=-0.2639 Main component: Cl=0.7976 Cdp=0.3400 Cm=-0.2049 Flap component: Cl=0.2715 Cdp=0.1460 Cm=-0.2415 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0046 0.6175, -0.04610, -0.1753 0.5841, -0.02440, -0.2700 0.5775, 0.01750, -0.3201 0.5777, 0.04660, -0.2394 0.6274, 0.07170, -0.7483 0.5694, 0.08320, -0.7664 0.5112, 0.09370, -0.8285 0.4731, 0.09830, -0.8714 0.4349, 0.10070, -0.8715 0.3960, 0.10120, -0.9587 0.3566, 0.10020, -0.9858 0.3172, 0.09790, -1.0685 0.2778, 0.09440, -1.1302 0.2393, 0.08960, -1.2136 0.2056, 0.08360, -1.3437 0.1633, 0.07610, -1.3806 0.1261, 0.06710, -1.4794 0.0900, 0.05640, -1.4697 0.0571, 0.04390, -1.5322 0.0283, 0.02940, -1.5562 0.0142, 0.01970, -1.6203 0.0081, 0.01410, -1.7547 0.0026, 0.00780, -1.5311 0.0000, 0.00000, -0.8742 0.0037, -0.00840, -0.2590 0.0112, -0.01420, 0.5941 0.0191, -0.01930, 0.8587 0.0397, -0.03030, 1.0148 0.0706, -0.04420, 0.9692 0.1037, -0.05710, 0.8788 0.1384, -0.06890, 0.8092 0.1741, -0.07950, 0.6820 0.2102, -0.08660, 0.4984 0.2472, -0.09640, 0.3793 0.2844, -0.10270, 0.2276 0.3225, -0.10690, 0.1460 0.3608, -0.10890, -0.0140 0.3991, -0.10830, -0.0867 0.4373, -0.10510, -0.1601 0.4757, -0.09890, -0.1507 0.5137, -0.09070, -0.1287 0.5694, -0.07640, -0.0322 14 Flap element taps 1.0000, 0.00130, -0.8058 0.9365, 0.01390, -0.8025 0.8333, 0.03280, -0.7983 0.7436, 0.04930, -0.7823 0.7049, 0.05670, -0.7835 0.6662, 0.06410, -0.8014 0.6522, 0.01390, -0.3335 0.5969, -0.00020, -0.3289 0.6000, -0.03020, -0.2894 0.6324, -0.04540, -0.2673 0.6667, -0.04880, 0.7890 0.7046, -0.04110, 0.2856 0.7429, -0.03210, 0.1985 0.9311, -0.00120, -0.0236 --------- Run Conditions: vel=99.6 ft/s Re=0.994x10^6 AOA=26.99 Flap deflection=5.00 Totals: Cl=1.0749 Cdp=0.5917 Cm(c/4)=-0.1821 Cs=-0.0394 Ch=-0.2885 Main component: Cl=0.7835 Cdp=0.4154 Cm=-0.2223 Flap component: Cl=0.2915 Cdp=0.1763 Cm=-0.2664 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0035 0.6175, -0.04610, -0.2326 0.5841, -0.02440, -0.3218 0.5775, 0.01750, -0.3885 0.5777, 0.04660, -0.2943 0.6274, 0.07170, -0.8857 0.5694, 0.08320, -0.8849 0.5112, 0.09370, -0.9091 0.4731, 0.09830, -0.9242 0.4349, 0.10070, -0.9643 0.3960, 0.10120, -1.0614 0.3566, 0.10020, -1.0607 0.3172, 0.09790, -1.1248 0.2778, 0.09440, -1.1878 0.2393, 0.08960, -1.2464 0.2056, 0.08360, -1.3387 0.1633, 0.07610, -1.2912 0.1261, 0.06710, -1.3174 0.0900, 0.05640, -1.2831 0.0571, 0.04390, -1.3380 0.0283, 0.02940, -1.3256 0.0142, 0.01970, -1.3426 0.0081, 0.01410, -1.3976 0.0026, 0.00780, -1.1724 0.0000, 0.00000, -1.0169 0.0037, -0.00840, -0.2200 0.0112, -0.01420, 0.5714 0.0191, -0.01930, 0.8353 0.0397, -0.03030, 1.0099 0.0706, -0.04420, 0.9832 0.1037, -0.05710, 0.9062 0.1384, -0.06890, 0.8590 0.1741, -0.07950, 0.7386 0.2102, -0.08660, 0.5481 0.2472, -0.09640, 0.4397 0.2844, -0.10270, 0.2839 0.3225, -0.10690, 0.2117 0.3608, -0.10890, 0.0416 0.3991, -0.10830, -0.0311 0.4373, -0.10510, -0.1195 0.4757, -0.09890, -0.1188 0.5137, -0.09070, -0.1080 0.5694, -0.07640, -0.0131 14 Flap element taps 1.0000, 0.00130, -0.8889 0.9365, 0.01390, -0.8917 0.8333, 0.03280, -0.9041 0.7436, 0.04930, -0.9032 0.7049, 0.05670, -0.9223 0.6662, 0.06410, -0.9324 0.6522, 0.01390, -0.3955 0.5969, -0.00020, -0.3901 0.6000, -0.03020, -0.3408 0.6324, -0.04540, -0.3389 0.6667, -0.04880, 0.8685 0.7046, -0.04110, 0.2859 0.7429, -0.03210, 0.1883 0.9311, -0.00120, -0.0533