S809 UNVENTED AILERON, LEGR, CHORD = 18 IN --------- Run Conditions: vel=102.2 ft/s Re=0.997x10^6 AOA=-5.99 Flap deflection=0.00 Totals: Cl=-0.4753 Cdp=0.0304 Cm(c/4)=0.0050 Cs=0.0193 Ch=0.0478 Main component: Cl=-0.4281 Cdp=0.0338 Cm=0.0864 Flap component: Cl=-0.0472 Cdp=-0.0034 Cm=0.0376 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2210 0.6175, -0.04610, -0.2026 0.5841, -0.02440, -0.1928 0.5775, 0.01750, -0.2022 0.5777, 0.04660, -0.2020 0.6274, 0.07170, -0.0930 0.5694, 0.08320, -0.2148 0.5112, 0.09370, -0.4221 0.4731, 0.09830, -0.4586 0.4349, 0.10070, -0.4526 0.3960, 0.10120, -0.4105 0.3566, 0.10020, -0.3089 0.3172, 0.09790, -0.2397 0.2778, 0.09440, -0.1984 0.2393, 0.08960, -0.1391 0.2056, 0.08360, -0.0997 0.1633, 0.07610, 0.0375 0.1261, 0.06710, 0.1473 0.0900, 0.05640, 0.2512 0.0571, 0.04390, 0.5257 0.0283, 0.02940, 0.8024 0.0142, 0.01970, 0.9817 0.0081, 0.01410, 0.9828 0.0026, 0.00780, 0.7039 0.0000, 0.00000, -0.3645 0.0037, -0.00840, -1.3889 0.0112, -0.01420, -1.0370 0.0191, -0.01930, -0.9891 0.0397, -0.03030, -0.7965 0.0706, -0.04420, -0.8071 0.1037, -0.05710, -0.7789 0.1384, -0.06890, -0.8413 0.1741, -0.07950, -0.8917 0.2102, -0.08660, -0.9875 0.2472, -0.09640, -1.0475 0.2844, -0.10270, -1.0816 0.3225, -0.10690, -1.0533 0.3608, -0.10890, -1.0489 0.3991, -0.10830, -0.9532 0.4373, -0.10510, -0.8157 0.4757, -0.09890, -0.5842 0.5137, -0.09070, -0.3992 0.5694, -0.07640, -0.2377 14 Flap element taps 1.0000, 0.00130, -0.0203 0.9365, 0.01390, 0.0007 0.8333, 0.03280, -0.0348 0.7436, 0.04930, -0.0691 0.7049, 0.05670, -0.0645 0.6662, 0.06410, -0.0955 0.6522, 0.01390, -0.1956 0.5969, -0.00020, -0.1957 0.6000, -0.03020, -0.2078 0.6324, -0.04540, -0.2253 0.6667, -0.04880, -0.2304 0.7046, -0.04110, -0.2201 0.7429, -0.03210, -0.2208 0.9311, -0.00120, -0.1419 Wake drag found for this condition, Cdw=0.0396 --------- Run Conditions: vel=103.0 ft/s Re=1.006x10^6 AOA=0.01 Flap deflection=0.00 Totals: Cl=-0.0204 Cdp=-0.0040 Cm(c/4)=-0.0156 Cs=0.0040 Ch=-0.0321 Main component: Cl=-0.0584 Cdp=0.0155 Cm=0.0205 Flap component: Cl=0.0380 Cdp=-0.0195 Cm=-0.0310 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1656 0.6175, -0.04610, -0.0972 0.5841, -0.02440, -0.1106 0.5775, 0.01750, -0.1214 0.5777, 0.04660, -0.1224 0.6274, 0.07170, -0.1613 0.5694, 0.08320, -0.2968 0.5112, 0.09370, -0.5540 0.4731, 0.09830, -0.6310 0.4349, 0.10070, -0.6606 0.3960, 0.10120, -0.6839 0.3566, 0.10020, -0.5655 0.3172, 0.09790, -0.5305 0.2778, 0.09440, -0.5194 0.2393, 0.08960, -0.4955 0.2056, 0.08360, -0.5293 0.1633, 0.07610, -0.3914 0.1261, 0.06710, -0.3451 0.0900, 0.05640, -0.3343 0.0571, 0.04390, -0.0826 0.0283, 0.02940, 0.1724 0.0142, 0.01970, 0.4122 0.0081, 0.01410, 0.5454 0.0026, 0.00780, 0.7893 0.0000, 0.00000, -0.4726 0.0037, -0.00840, 0.5550 0.0112, -0.01420, 0.3229 0.0191, -0.01930, 0.1843 0.0397, -0.03030, 0.0628 0.0706, -0.04420, -0.1255 0.1037, -0.05710, -0.2145 0.1384, -0.06890, -0.3099 0.1741, -0.07950, -0.4330 0.2102, -0.08660, -0.6138 0.2472, -0.09640, -0.7060 0.2844, -0.10270, -0.8124 0.3225, -0.10690, -0.8140 0.3608, -0.10890, -0.9018 0.3991, -0.10830, -0.8676 0.4373, -0.10510, -0.8350 0.4757, -0.09890, -0.6822 0.5137, -0.09070, -0.5510 0.5694, -0.07640, -0.2873 14 Flap element taps 1.0000, 0.00130, 0.1894 0.9365, 0.01390, 0.1119 0.8333, 0.03280, 0.0005 0.7436, 0.04930, -0.0797 0.7049, 0.05670, -0.1035 0.6662, 0.06410, -0.1360 0.6522, 0.01390, -0.1282 0.5969, -0.00020, -0.1082 0.6000, -0.03020, -0.1092 0.6324, -0.04540, -0.1326 0.6667, -0.04880, -0.1147 0.7046, -0.04110, 0.0122 0.7429, -0.03210, 0.0556 0.9311, -0.00120, 0.2380 Wake drag found for this condition, Cdw=0.0138 --------- Run Conditions: vel=103.1 ft/s Re=1.010x10^6 AOA=3.03 Flap deflection=0.00 Totals: Cl=0.2904 Cdp=-0.0020 Cm(c/4)=-0.0227 Cs=0.0173 Ch=-0.0536 Main component: Cl=0.2247 Cdp=0.0157 Cm=-0.0432 Flap component: Cl=0.0657 Cdp=-0.0177 Cm=-0.0520 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1213 0.6175, -0.04610, -0.0789 0.5841, -0.02440, -0.0969 0.5775, 0.01750, -0.1055 0.5777, 0.04660, -0.1060 0.6274, 0.07170, -0.2246 0.5694, 0.08320, -0.3623 0.5112, 0.09370, -0.6544 0.4731, 0.09830, -0.7517 0.4349, 0.10070, -0.8066 0.3960, 0.10120, -0.8694 0.3566, 0.10020, -0.7403 0.3172, 0.09790, -0.7232 0.2778, 0.09440, -0.7327 0.2393, 0.08960, -0.7374 0.2056, 0.08360, -0.8207 0.1633, 0.07610, -0.6825 0.1261, 0.06710, -0.6900 0.0900, 0.05640, -0.7454 0.0571, 0.04390, -0.5532 0.0283, 0.02940, -0.4027 0.0142, 0.01970, -0.2146 0.0081, 0.01410, -0.2184 0.0026, 0.00780, 0.1402 0.0000, 0.00000, -0.5915 0.0037, -0.00840, 0.9787 0.0112, -0.01420, 0.8097 0.0191, -0.01930, 0.6605 0.0397, -0.03030, 0.4639 0.0706, -0.04420, 0.2247 0.1037, -0.05710, 0.0858 0.1384, -0.06890, 0.0024 0.1741, -0.07950, -0.1423 0.2102, -0.08660, -0.3600 0.2472, -0.09640, -0.4517 0.2844, -0.10270, -0.5829 0.3225, -0.10690, -0.5840 0.3608, -0.10890, -0.7043 0.3991, -0.10830, -0.6813 0.4373, -0.10510, -0.6882 0.4757, -0.09890, -0.5638 0.5137, -0.09070, -0.4616 0.5694, -0.07640, -0.2163 14 Flap element taps 1.0000, 0.00130, 0.1731 0.9365, 0.01390, 0.1017 0.8333, 0.03280, -0.0234 0.7436, 0.04930, -0.1181 0.7049, 0.05670, -0.1543 0.6662, 0.06410, -0.1969 0.6522, 0.01390, -0.1225 0.5969, -0.00020, -0.0937 0.6000, -0.03020, -0.0943 0.6324, -0.04540, -0.1262 0.6667, -0.04880, -0.0485 0.7046, -0.04110, 0.0890 0.7429, -0.03210, 0.1176 0.9311, -0.00120, 0.2795 Wake drag found for this condition, Cdw=0.0147 --------- Run Conditions: vel=103.1 ft/s Re=1.011x10^6 AOA=6.01 Flap deflection=0.00 Totals: Cl=0.5729 Cdp=0.0139 Cm(c/4)=-0.0267 Cs=0.0461 Ch=-0.0715 Main component: Cl=0.4842 Cdp=0.0249 Cm=-0.1001 Flap component: Cl=0.0887 Cdp=-0.0110 Cm=-0.0694 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.0716 0.6175, -0.04610, -0.0557 0.5841, -0.02440, -0.0797 0.5775, 0.01750, -0.0905 0.5777, 0.04660, -0.0909 0.6274, 0.07170, -0.2730 0.5694, 0.08320, -0.4033 0.5112, 0.09370, -0.7196 0.4731, 0.09830, -0.8401 0.4349, 0.10070, -0.9226 0.3960, 0.10120, -1.0249 0.3566, 0.10020, -0.8965 0.3172, 0.09790, -0.9022 0.2778, 0.09440, -0.9335 0.2393, 0.08960, -0.9679 0.2056, 0.08360, -1.0995 0.1633, 0.07610, -0.9798 0.1261, 0.06710, -1.0435 0.0900, 0.05640, -1.1670 0.0571, 0.04390, -1.0737 0.0283, 0.02940, -1.0767 0.0142, 0.01970, -1.0213 0.0081, 0.01410, -1.2391 0.0026, 0.00780, -0.6441 0.0000, 0.00000, -0.7343 0.0037, -0.00840, 0.9672 0.0112, -0.01420, 1.0116 0.0191, -0.01930, 0.9375 0.0397, -0.03030, 0.7515 0.0706, -0.04420, 0.4970 0.1037, -0.05710, 0.3352 0.1384, -0.06890, 0.2694 0.1741, -0.07950, 0.1058 0.2102, -0.08660, -0.1398 0.2472, -0.09640, -0.2299 0.2844, -0.10270, -0.3824 0.3225, -0.10690, -0.3758 0.3608, -0.10890, -0.5214 0.3991, -0.10830, -0.5120 0.4373, -0.10510, -0.5479 0.4757, -0.09890, -0.4492 0.5137, -0.09070, -0.3731 0.5694, -0.07640, -0.1427 14 Flap element taps 1.0000, 0.00130, 0.1157 0.9365, 0.01390, 0.0652 0.8333, 0.03280, -0.0486 0.7436, 0.04930, -0.1476 0.7049, 0.05670, -0.1965 0.6662, 0.06410, -0.2380 0.6522, 0.01390, -0.1103 0.5969, -0.00020, -0.0734 0.6000, -0.03020, -0.0757 0.6324, -0.04540, -0.1115 0.6667, -0.04880, 0.0694 0.7046, -0.04110, 0.1420 0.7429, -0.03210, 0.1571 0.9311, -0.00120, 0.2939 Wake drag found for this condition, Cdw=0.0174 --------- Run Conditions: vel=102.4 ft/s Re=1.006x10^6 AOA=9.01 Flap deflection=0.00 Totals: Cl=0.7830 Cdp=0.0438 Cm(c/4)=-0.0298 Cs=0.0793 Ch=-0.0991 Main component: Cl=0.6697 Cdp=0.0413 Cm=-0.1349 Flap component: Cl=0.1132 Cdp=0.0025 Cm=-0.0900 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.0355 0.6175, -0.04610, -0.0497 0.5841, -0.02440, -0.0727 0.5775, 0.01750, -0.0822 0.5777, 0.04660, -0.0819 0.6274, 0.07170, -0.2819 0.5694, 0.08320, -0.3783 0.5112, 0.09370, -0.6834 0.4731, 0.09830, -0.8348 0.4349, 0.10070, -0.9482 0.3960, 0.10120, -1.0943 0.3566, 0.10020, -0.9767 0.3172, 0.09790, -1.0085 0.2778, 0.09440, -1.0652 0.2393, 0.08960, -1.1306 0.2056, 0.08360, -1.3091 0.1633, 0.07610, -1.2136 0.1261, 0.06710, -1.3350 0.0900, 0.05640, -1.5193 0.0571, 0.04390, -1.5456 0.0283, 0.02940, -1.7268 0.0142, 0.01970, -1.9096 0.0081, 0.01410, -2.2171 0.0026, 0.00780, -1.6863 0.0000, 0.00000, -0.8816 0.0037, -0.00840, 0.6544 0.0112, -0.01420, 1.0091 0.0191, -0.01930, 1.0342 0.0397, -0.03030, 0.9228 0.0706, -0.04420, 0.6873 0.1037, -0.05710, 0.5183 0.1384, -0.06890, 0.4721 0.1741, -0.07950, 0.3018 0.2102, -0.08660, 0.0381 0.2472, -0.09640, -0.0498 0.2844, -0.10270, -0.2221 0.3225, -0.10690, -0.2249 0.3608, -0.10890, -0.3899 0.3991, -0.10830, -0.3961 0.4373, -0.10510, -0.4540 0.4757, -0.09890, -0.3846 0.5137, -0.09070, -0.3245 0.5694, -0.07640, -0.0791 14 Flap element taps 1.0000, 0.00130, -0.0128 0.9365, 0.01390, -0.0674 0.8333, 0.03280, -0.1329 0.7436, 0.04930, -0.1847 0.7049, 0.05670, -0.2244 0.6662, 0.06410, -0.2526 0.6522, 0.01390, -0.1100 0.5969, -0.00020, -0.0675 0.6000, -0.03020, -0.0710 0.6324, -0.04540, -0.1095 0.6667, -0.04880, 0.1702 0.7046, -0.04110, 0.1656 0.7429, -0.03210, 0.1683 0.9311, -0.00120, 0.2681 Wake drag found for this condition, Cdw=0.0269 --------- Run Conditions: vel=102.1 ft/s Re=1.005x10^6 AOA=12.01 Flap deflection=0.00 Totals: Cl=0.8940 Cdp=0.0823 Cm(c/4)=-0.0346 Cs=0.1055 Ch=-0.1455 Main component: Cl=0.7426 Cdp=0.0559 Cm=-0.1337 Flap component: Cl=0.1514 Cdp=0.0264 Cm=-0.1238 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.0224 0.6175, -0.04610, -0.0572 0.5841, -0.02440, -0.0829 0.5775, 0.01750, -0.0911 0.5777, 0.04660, -0.0915 0.6274, 0.07170, -0.3161 0.5694, 0.08320, -0.2904 0.5112, 0.09370, -0.4193 0.4731, 0.09830, -0.5632 0.4349, 0.10070, -0.7378 0.3960, 0.10120, -0.9620 0.3566, 0.10020, -0.8880 0.3172, 0.09790, -0.9660 0.2778, 0.09440, -1.0632 0.2393, 0.08960, -1.1662 0.2056, 0.08360, -1.3945 0.1633, 0.07610, -1.3354 0.1261, 0.06710, -1.5183 0.0900, 0.05640, -1.7508 0.0571, 0.04390, -1.9123 0.0283, 0.02940, -2.2863 0.0142, 0.01970, -2.6939 0.0081, 0.01410, -3.1782 0.0026, 0.00780, -2.7396 0.0000, 0.00000, -1.0662 0.0037, -0.00840, 0.1748 0.0112, -0.01420, 0.8886 0.0191, -0.01930, 1.0241 0.0397, -0.03030, 1.0082 0.0706, -0.04420, 0.8108 0.1037, -0.05710, 0.6502 0.1384, -0.06890, 0.6221 0.1741, -0.07950, 0.4490 0.2102, -0.08660, 0.1734 0.2472, -0.09640, 0.0874 0.2844, -0.10270, -0.0960 0.3225, -0.10690, -0.1035 0.3608, -0.10890, -0.2851 0.3991, -0.10830, -0.2986 0.4373, -0.10510, -0.3799 0.4757, -0.09890, -0.3270 0.5137, -0.09070, -0.2889 0.5694, -0.07640, -0.0825 14 Flap element taps 1.0000, 0.00130, -0.2077 0.9365, 0.01390, -0.2980 0.8333, 0.03280, -0.3185 0.7436, 0.04930, -0.3205 0.7049, 0.05670, -0.3302 0.6662, 0.06410, -0.3330 0.6522, 0.01390, -0.1233 0.5969, -0.00020, -0.0782 0.6000, -0.03020, -0.0831 0.6324, -0.04540, -0.1233 0.6667, -0.04880, 0.2257 0.7046, -0.04110, 0.1543 0.7429, -0.03210, 0.1483 0.9311, -0.00120, 0.1936 --------- Run Conditions: vel=100.0 ft/s Re=1.004x10^6 AOA=15.04 Flap deflection=0.00 Totals: Cl=0.9139 Cdp=0.1317 Cm(c/4)=-0.0342 Cs=0.1099 Ch=-0.1632 Main component: Cl=0.7463 Cdp=0.0869 Cm=-0.1240 Flap component: Cl=0.1676 Cdp=0.0448 Cm=-0.1394 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.0479 0.6175, -0.04610, -0.1073 0.5841, -0.02440, -0.1092 0.5775, 0.01750, -0.1216 0.5777, 0.04660, -0.1267 0.6274, 0.07170, -0.3881 0.5694, 0.08320, -0.3754 0.5112, 0.09370, -0.4013 0.4731, 0.09830, -0.4155 0.4349, 0.10070, -0.4785 0.3960, 0.10120, -0.6020 0.3566, 0.10020, -0.6873 0.3172, 0.09790, -0.8137 0.2778, 0.09440, -0.9501 0.2393, 0.08960, -1.0905 0.2056, 0.08360, -1.2786 0.1633, 0.07610, -1.3771 0.1261, 0.06710, -1.5529 0.0900, 0.05640, -1.8794 0.0571, 0.04390, -2.1367 0.0283, 0.02940, -2.6851 0.0142, 0.01970, -3.2651 0.0081, 0.01410, -3.7960 0.0026, 0.00780, -3.6155 0.0000, 0.00000, -0.2940 0.0037, -0.00840, -0.3135 0.0112, -0.01420, 0.7138 0.0191, -0.01930, 0.9504 0.0397, -0.03030, 1.0217 0.0706, -0.04420, 0.8939 0.1037, -0.05710, 0.7512 0.1384, -0.06890, 0.6348 0.1741, -0.07950, 0.4834 0.2102, -0.08660, 0.2933 0.2472, -0.09640, 0.1639 0.2844, -0.10270, 0.0171 0.3225, -0.10690, -0.0776 0.3608, -0.10890, -0.2207 0.3991, -0.10830, -0.2879 0.4373, -0.10510, -0.3369 0.4757, -0.09890, -0.2972 0.5137, -0.09070, -0.2527 0.5694, -0.07640, -0.1372 14 Flap element taps 1.0000, 0.00130, -0.3470 0.9365, 0.01390, -0.4286 0.8333, 0.03280, -0.4179 0.7436, 0.04930, -0.4118 0.7049, 0.05670, -0.4140 0.6662, 0.06410, -0.4054 0.6522, 0.01390, -0.1243 0.5969, -0.00020, -0.1107 0.6000, -0.03020, -0.1159 0.6324, -0.04540, -0.1248 0.6667, -0.04880, 0.3046 0.7046, -0.04110, 0.1314 0.7429, -0.03210, 0.1299 0.9311, -0.00120, 0.1055 --------- Run Conditions: vel=98.7 ft/s Re=0.989x10^6 AOA=18.03 Flap deflection=0.00 Totals: Cl=0.6967 Cdp=0.2295 Cm(c/4)=-0.0848 Cs=-0.0026 Ch=-0.1921 Main component: Cl=0.4939 Cdp=0.1632 Cm=-0.0982 Flap component: Cl=0.2028 Cdp=0.0664 Cm=-0.1700 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1260 0.6175, -0.04610, -0.1883 0.5841, -0.02440, -0.2000 0.5775, 0.01750, -0.2114 0.5777, 0.04660, -0.2133 0.6274, 0.07170, -0.5781 0.5694, 0.08320, -0.5594 0.5112, 0.09370, -0.5890 0.4731, 0.09830, -0.5863 0.4349, 0.10070, -0.5970 0.3960, 0.10120, -0.6507 0.3566, 0.10020, -0.5869 0.3172, 0.09790, -0.6020 0.2778, 0.09440, -0.6130 0.2393, 0.08960, -0.6320 0.2056, 0.08360, -0.7195 0.1633, 0.07610, -0.6745 0.1261, 0.06710, -0.7591 0.0900, 0.05640, -0.8221 0.0571, 0.04390, -1.0123 0.0283, 0.02940, -1.4624 0.0142, 0.01970, -2.0187 0.0081, 0.01410, -2.6062 0.0026, 0.00780, -2.4916 0.0000, 0.00000, -0.3319 0.0037, -0.00840, 0.0279 0.0112, -0.01420, 0.8073 0.0191, -0.01930, 0.9838 0.0397, -0.03030, 1.0193 0.0706, -0.04420, 0.8759 0.1037, -0.05710, 0.7330 0.1384, -0.06890, 0.6432 0.1741, -0.07950, 0.4884 0.2102, -0.08660, 0.2700 0.2472, -0.09640, 0.1498 0.2844, -0.10270, -0.0154 0.3225, -0.10690, -0.0923 0.3608, -0.10890, -0.2597 0.3991, -0.10830, -0.3242 0.4373, -0.10510, -0.3947 0.4757, -0.09890, -0.3586 0.5137, -0.09070, -0.3246 0.5694, -0.07640, -0.1918 14 Flap element taps 1.0000, 0.00130, -0.4695 0.9365, 0.01390, -0.5588 0.8333, 0.03280, -0.6097 0.7436, 0.04930, -0.6147 0.7049, 0.05670, -0.6160 0.6662, 0.06410, -0.6162 0.6522, 0.01390, -0.2248 0.5969, -0.00020, -0.2016 0.6000, -0.03020, -0.2066 0.6324, -0.04540, -0.2224 0.6667, -0.04880, 0.4170 0.7046, -0.04110, 0.0707 0.7429, -0.03210, 0.0596 0.9311, -0.00120, 0.0254 --------- Run Conditions: vel=99.6 ft/s Re=1.001x10^6 AOA=19.99 Flap deflection=0.00 Totals: Cl=0.7427 Cdp=0.2872 Cm(c/4)=-0.0984 Cs=-0.0160 Ch=-0.2042 Main component: Cl=0.5328 Cdp=0.2087 Cm=-0.1186 Flap component: Cl=0.2099 Cdp=0.0785 Cm=-0.1788 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1365 0.6175, -0.04610, -0.2042 0.5841, -0.02440, -0.2191 0.5775, 0.01750, -0.2290 0.5777, 0.04660, -0.2325 0.6274, 0.07170, -0.6667 0.5694, 0.08320, -0.6411 0.5112, 0.09370, -0.6781 0.4731, 0.09830, -0.6845 0.4349, 0.10070, -0.6935 0.3960, 0.10120, -0.7654 0.3566, 0.10020, -0.6795 0.3172, 0.09790, -0.7021 0.2778, 0.09440, -0.7126 0.2393, 0.08960, -0.7352 0.2056, 0.08360, -0.8462 0.1633, 0.07610, -0.7749 0.1261, 0.06710, -0.8517 0.0900, 0.05640, -0.8406 0.0571, 0.04390, -0.9667 0.0283, 0.02940, -1.2646 0.0142, 0.01970, -1.7563 0.0081, 0.01410, -2.2828 0.0026, 0.00780, -2.2559 0.0000, 0.00000, -0.3720 0.0037, -0.00840, 0.0037 0.0112, -0.01420, 0.7863 0.0191, -0.01930, 0.9735 0.0397, -0.03030, 1.0291 0.0706, -0.04420, 0.8942 0.1037, -0.05710, 0.7558 0.1384, -0.06890, 0.6901 0.1741, -0.07950, 0.5342 0.2102, -0.08660, 0.2991 0.2472, -0.09640, 0.1909 0.2844, -0.10270, 0.0141 0.3225, -0.10690, -0.0499 0.3608, -0.10890, -0.2305 0.3991, -0.10830, -0.2909 0.4373, -0.10510, -0.3766 0.4757, -0.09890, -0.3464 0.5137, -0.09070, -0.3232 0.5694, -0.07640, -0.1874 14 Flap element taps 1.0000, 0.00130, -0.5441 0.9365, 0.01390, -0.6245 0.8333, 0.03280, -0.6659 0.7436, 0.04930, -0.6678 0.7049, 0.05670, -0.6779 0.6662, 0.06410, -0.6789 0.6522, 0.01390, -0.2461 0.5969, -0.00020, -0.2178 0.6000, -0.03020, -0.2235 0.6324, -0.04540, -0.2432 0.6667, -0.04880, 0.3541 0.7046, -0.04110, 0.0628 0.7429, -0.03210, 0.0455 0.9311, -0.00120, -0.0017 --------- Run Conditions: vel=99.7 ft/s Re=1.002x10^6 AOA=24.01 Flap deflection=0.00 Totals: Cl=1.0600 Cdp=0.4426 Cm(c/4)=-0.1224 Cs=0.0270 Ch=-0.2584 Main component: Cl=0.8248 Cdp=0.3232 Cm=-0.1969 Flap component: Cl=0.2352 Cdp=0.1194 Cm=-0.2125 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1034 0.6175, -0.04610, -0.1826 0.5841, -0.02440, -0.1968 0.5775, 0.01750, -0.2072 0.5777, 0.04660, -0.2135 0.6274, 0.07170, -0.7828 0.5694, 0.08320, -0.7692 0.5112, 0.09370, -0.8436 0.4731, 0.09830, -0.8843 0.4349, 0.10070, -0.9001 0.3960, 0.10120, -1.0522 0.3566, 0.10020, -1.0302 0.3172, 0.09790, -1.0887 0.2778, 0.09440, -1.1432 0.2393, 0.08960, -1.2289 0.2056, 0.08360, -1.4105 0.1633, 0.07610, -1.4004 0.1261, 0.06710, -1.5831 0.0900, 0.05640, -1.6613 0.0571, 0.04390, -1.8508 0.0283, 0.02940, -1.9370 0.0142, 0.01970, -2.1475 0.0081, 0.01410, -2.5166 0.0026, 0.00780, -2.2818 0.0000, 0.00000, -0.4502 0.0037, -0.00840, -0.4632 0.0112, -0.01420, 0.5591 0.0191, -0.01930, 0.8604 0.0397, -0.03030, 1.0330 0.0706, -0.04420, 0.9632 0.1037, -0.05710, 0.8528 0.1384, -0.06890, 0.8254 0.1741, -0.07950, 0.6831 0.2102, -0.08660, 0.4378 0.2472, -0.09640, 0.3414 0.2844, -0.10270, 0.1605 0.3225, -0.10690, 0.1041 0.3608, -0.10890, -0.0902 0.3991, -0.10830, -0.1534 0.4373, -0.10510, -0.2621 0.4757, -0.09890, -0.2508 0.5137, -0.09070, -0.2475 0.5694, -0.07640, -0.1225 14 Flap element taps 1.0000, 0.00130, -0.7944 0.9365, 0.01390, -0.8350 0.8333, 0.03280, -0.8563 0.7436, 0.04930, -0.8290 0.7049, 0.05670, -0.8172 0.6662, 0.06410, -0.8145 0.6522, 0.01390, -0.2285 0.5969, -0.00020, -0.1928 0.6000, -0.03020, -0.2016 0.6324, -0.04540, -0.2257 0.6667, -0.04880, 0.0428 0.7046, -0.04110, 0.0917 0.7429, -0.03210, 0.0559 0.9311, -0.00120, -0.0476 --------- Run Conditions: vel=98.9 ft/s Re=0.992x10^6 AOA=27.00 Flap deflection=0.00 Totals: Cl=0.9572 Cdp=0.5003 Cm(c/4)=-0.1230 Cs=-0.0112 Ch=-0.2433 Main component: Cl=0.7435 Cdp=0.3773 Cm=-0.1940 Flap component: Cl=0.2137 Cdp=0.1230 Cm=-0.1990 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1050 0.6175, -0.04610, -0.1889 0.5841, -0.02440, -0.2064 0.5775, 0.01750, -0.2172 0.5777, 0.04660, -0.2241 0.6274, 0.07170, -0.7780 0.5694, 0.08320, -0.7723 0.5112, 0.09370, -0.8538 0.4731, 0.09830, -0.8683 0.4349, 0.10070, -0.8968 0.3960, 0.10120, -1.0135 0.3566, 0.10020, -0.9624 0.3172, 0.09790, -1.0593 0.2778, 0.09440, -1.1028 0.2393, 0.08960, -1.1850 0.2056, 0.08360, -1.3581 0.1633, 0.07610, -1.3121 0.1261, 0.06710, -1.4543 0.0900, 0.05640, -1.4060 0.0571, 0.04390, -1.4259 0.0283, 0.02940, -1.4217 0.0142, 0.01970, -1.4536 0.0081, 0.01410, -1.6073 0.0026, 0.00780, -1.3437 0.0000, 0.00000, -0.5452 0.0037, -0.00840, -0.2192 0.0112, -0.01420, 0.6026 0.0191, -0.01930, 0.8636 0.0397, -0.03030, 1.0286 0.0706, -0.04420, 0.9685 0.1037, -0.05710, 0.8676 0.1384, -0.06890, 0.8606 0.1741, -0.07950, 0.7220 0.2102, -0.08660, 0.4739 0.2472, -0.09640, 0.3864 0.2844, -0.10270, 0.2011 0.3225, -0.10690, 0.1506 0.3608, -0.10890, -0.0503 0.3991, -0.10830, -0.1137 0.4373, -0.10510, -0.2358 0.4757, -0.09890, -0.2320 0.5137, -0.09070, -0.2404 0.5694, -0.07640, -0.1157 14 Flap element taps 1.0000, 0.00130, -0.7953 0.9365, 0.01390, -0.8103 0.8333, 0.03280, -0.8218 0.7436, 0.04930, -0.8082 0.7049, 0.05670, -0.8150 0.6662, 0.06410, -0.8053 0.6522, 0.01390, -0.2399 0.5969, -0.00020, -0.2010 0.6000, -0.03020, -0.2100 0.6324, -0.04540, -0.2362 0.6667, -0.04880, -0.0926 0.7046, -0.04110, 0.0816 0.7429, -0.03210, 0.0385 0.9311, -0.00120, -0.0711