S809 SPOILER FLAP, LEGR, CHORD = 18 INCHES --------- Run Conditions: vel=102.2 ft/s Re=1.003x10^6 AOA=-6.00 Flap deflection=20.00 Totals: Cl=-0.8698 Cdp=0.1076 Cm(c/4)=0.0445 Cs=-0.0161 Ch=-0.0107 Main component: Cl=-0.7818 Cdp=0.0341 Cm=0.1885 Flap component: Cl=-0.0881 Cdp=0.0735 Cm=0.0751 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3547 0.5905, -0.01667, -0.4599 0.5709, 0.03110, -0.2145 0.5889, 0.07933, -0.1317 0.5500, 0.08689, 0.4749 0.5110, 0.09367, 0.3380 0.4731, 0.09830, 0.2279 0.4349, 0.10070, 0.1547 0.3960, 0.10120, 0.0910 0.3566, 0.10020, 0.1177 0.3172, 0.09790, 0.1368 0.2778, 0.09440, 0.1494 0.2393, 0.08960, 0.1934 0.2056, 0.08360, 0.2213 0.1633, 0.07610, 0.3309 0.1261, 0.06710, 0.4337 0.0900, 0.05640, 0.5658 0.0571, 0.04390, 0.7606 0.0283, 0.02940, 0.9585 0.0142, 0.01970, 0.9971 0.0081, 0.01410, 0.8738 0.0026, 0.00780, 0.2446 0.0000, 0.00000, -1.9452 0.0037, -0.00840, -2.7408 0.0112, -0.01420, -2.0980 0.0191, -0.01930, -1.6762 0.0397, -0.03030, -1.2401 0.0706, -0.04420, -1.1929 0.1037, -0.05710, -1.1216 0.1384, -0.06890, -1.1436 0.1741, -0.07950, -1.1596 0.2102, -0.08660, -1.2226 0.2472, -0.09640, -1.2678 0.2844, -0.10270, -1.2610 0.3225, -0.10690, -1.2055 0.3608, -0.10890, -1.1572 0.3991, -0.10830, -0.9830 0.4373, -0.10510, -0.7352 0.4757, -0.09890, -0.5021 0.5137, -0.09067, -0.4004 0.5611, -0.07859, -0.3865 16 Flap element taps 1.0000, 0.00130, -0.5196 0.9365, 0.01390, -0.4768 0.8333, 0.03280, -0.4858 0.7436, 0.04930, -0.4769 0.7049, 0.05667, -0.4680 0.6662, 0.06411, -0.4774 0.6274, 0.07172, -0.4725 0.6009, 0.07523, -0.4715 0.6069, 0.02889, 0.9959 0.6079, -0.01747, -0.1767 0.6167, -0.06381, -0.7167 0.6558, -0.05300, -0.7364 0.7045, -0.04117, -0.7490 0.7429, -0.03210, -0.7610 0.8333, -0.01400, -0.7799 0.9311, -0.00120, -0.4613 --------- Run Conditions: vel=102.2 ft/s Re=1.003x10^6 AOA=0.01 Flap deflection=20.00 Totals: Cl=-0.2220 Cdp=0.1240 Cm(c/4)=-0.0176 Cs=-0.1240 Ch=-0.0074 Main component: Cl=-0.2782 Cdp=-0.0055 Cm=0.0827 Flap component: Cl=0.0561 Cdp=0.1295 Cm=-0.0448 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.0183 0.5905, -0.01667, -0.2834 0.5709, 0.03110, 0.1522 0.5889, 0.07933, 0.2054 0.5500, 0.08689, 0.3146 0.5110, 0.09367, 0.2190 0.4731, 0.09830, 0.0758 0.4349, 0.10070, -0.0478 0.3960, 0.10120, -0.1703 0.3566, 0.10020, -0.1566 0.3172, 0.09790, -0.1715 0.2778, 0.09440, -0.1945 0.2393, 0.08960, -0.1927 0.2056, 0.08360, -0.2209 0.1633, 0.07610, -0.1299 0.1261, 0.06710, -0.0766 0.0900, 0.05640, -0.0018 0.0571, 0.04390, 0.1716 0.0283, 0.02940, 0.3988 0.0142, 0.01970, 0.6354 0.0081, 0.01410, 0.7595 0.0026, 0.00780, 0.9235 0.0000, 0.00000, 0.8679 0.0037, -0.00840, 0.1539 0.0112, -0.01420, -0.0262 0.0191, -0.01930, -0.0519 0.0397, -0.03030, -0.0599 0.0706, -0.04420, -0.2622 0.1037, -0.05710, -0.3429 0.1384, -0.06890, -0.4336 0.1741, -0.07950, -0.5315 0.2102, -0.08660, -0.6663 0.2472, -0.09640, -0.7565 0.2844, -0.10270, -0.8180 0.3225, -0.10690, -0.8166 0.3608, -0.10890, -0.8545 0.3991, -0.10830, -0.7680 0.4373, -0.10510, -0.6318 0.4757, -0.09890, -0.4150 0.5137, -0.09067, -0.1539 0.5611, -0.07859, -0.0575 16 Flap element taps 1.0000, 0.00130, -0.7001 0.9365, 0.01390, -0.6515 0.8333, 0.03280, -0.6634 0.7436, 0.04930, -0.6487 0.7049, 0.05667, -0.6376 0.6662, 0.06411, -0.6523 0.6274, 0.07172, -0.6400 0.6009, 0.07523, -0.6367 0.6069, 0.02889, 0.9751 0.6079, -0.01747, 0.1066 0.6167, -0.06381, -0.4772 0.6558, -0.05300, -0.5046 0.7045, -0.04117, -0.5123 0.7429, -0.03210, -0.5375 0.8333, -0.01400, -0.4554 0.9311, -0.00120, -0.1072 --------- Run Conditions: vel=102.2 ft/s Re=1.003x10^6 AOA=3.02 Flap deflection=20.00 Totals: Cl=0.1140 Cdp=0.1234 Cm(c/4)=-0.0540 Cs=-0.1172 Ch=-0.0020 Main component: Cl=-0.0247 Cdp=-0.0184 Cm=0.0317 Flap component: Cl=0.1387 Cdp=0.1418 Cm=-0.1158 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.1182 0.5905, -0.01667, -0.1377 0.5709, 0.03110, 0.2159 0.5889, 0.07933, 0.1952 0.5500, 0.08689, 0.1588 0.5110, 0.09367, 0.1429 0.4731, 0.09830, 0.0490 0.4349, 0.10070, -0.1118 0.3960, 0.10120, -0.2732 0.3566, 0.10020, -0.2926 0.3172, 0.09790, -0.3335 0.2778, 0.09440, -0.3804 0.2393, 0.08960, -0.4075 0.2056, 0.08360, -0.4646 0.1633, 0.07610, -0.4047 0.1261, 0.06710, -0.3889 0.0900, 0.05640, -0.3743 0.0571, 0.04390, -0.2622 0.0283, 0.02940, -0.1200 0.0142, 0.01970, 0.0542 0.0081, 0.01410, 0.2302 0.0026, 0.00780, 0.4163 0.0000, 0.00000, 0.9590 0.0037, -0.00840, 0.8377 0.0112, -0.01420, 0.6154 0.0191, -0.01930, 0.5018 0.0397, -0.03030, 0.3617 0.0706, -0.04420, 0.1177 0.1037, -0.05710, -0.0061 0.1384, -0.06890, -0.1212 0.1741, -0.07950, -0.2451 0.2102, -0.08660, -0.3982 0.2472, -0.09640, -0.5034 0.2844, -0.10270, -0.5896 0.3225, -0.10690, -0.6146 0.3608, -0.10890, -0.6799 0.3991, -0.10830, -0.6339 0.4373, -0.10510, -0.5496 0.4757, -0.09890, -0.3895 0.5137, -0.09067, -0.1308 0.5611, -0.07859, 0.0508 16 Flap element taps 1.0000, 0.00130, -0.6511 0.9365, 0.01390, -0.6557 0.8333, 0.03280, -0.6790 0.7436, 0.04930, -0.6557 0.7049, 0.05667, -0.6387 0.6662, 0.06411, -0.6547 0.6274, 0.07172, -0.6454 0.6009, 0.07523, -0.6693 0.6069, 0.02889, 0.6240 0.6079, -0.01747, 0.1386 0.6167, -0.06381, -0.2668 0.6558, -0.05300, -0.3071 0.7045, -0.04117, -0.3077 0.7429, -0.03210, -0.2712 0.8333, -0.01400, -0.0926 0.9311, -0.00120, 0.0142 --------- Run Conditions: vel=102.1 ft/s Re=1.002x10^6 AOA=6.01 Flap deflection=20.00 Totals: Cl=0.4471 Cdp=0.1421 Cm(c/4)=-0.1030 Cs=-0.0945 Ch=0.0216 Main component: Cl=0.1894 Cdp=-0.0236 Cm=-0.0038 Flap component: Cl=0.2577 Cdp=0.1657 Cm=-0.2141 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.1384 0.5905, -0.01667, 0.1125 0.5709, 0.03110, 0.1253 0.5889, 0.07933, 0.0708 0.5500, 0.08689, 0.0756 0.5110, 0.09367, 0.0780 0.4731, 0.09830, 0.0293 0.4349, 0.10070, -0.1283 0.3960, 0.10120, -0.3267 0.3566, 0.10020, -0.3960 0.3172, 0.09790, -0.4694 0.2778, 0.09440, -0.5487 0.2393, 0.08960, -0.6092 0.2056, 0.08360, -0.6962 0.1633, 0.07610, -0.6845 0.1261, 0.06710, -0.7121 0.0900, 0.05640, -0.7797 0.0571, 0.04390, -0.7545 0.0283, 0.02940, -0.7618 0.0142, 0.01970, -0.7480 0.0081, 0.01410, -0.5284 0.0026, 0.00780, -0.3743 0.0000, 0.00000, 0.2314 0.0037, -0.00840, 0.9834 0.0112, -0.01420, 0.9377 0.0191, -0.01930, 0.8419 0.0397, -0.03030, 0.6731 0.0706, -0.04420, 0.4238 0.1037, -0.05710, 0.2753 0.1384, -0.06890, 0.1406 0.1741, -0.07950, -0.0011 0.2102, -0.08660, -0.1651 0.2472, -0.09640, -0.2883 0.2844, -0.10270, -0.3916 0.3225, -0.10690, -0.4374 0.3608, -0.10890, -0.5280 0.3991, -0.10830, -0.5230 0.4373, -0.10510, -0.4872 0.4757, -0.09890, -0.3885 0.5137, -0.09067, -0.1799 0.5611, -0.07859, -0.0025 16 Flap element taps 1.0000, 0.00130, -0.6649 0.9365, 0.01390, -0.6792 0.8333, 0.03280, -0.6969 0.7436, 0.04930, -0.6695 0.7049, 0.05667, -0.6555 0.6662, 0.06411, -0.6712 0.6274, 0.07172, -0.6635 0.6009, 0.07523, -0.7212 0.6069, 0.02889, 0.0791 0.6079, -0.01747, 0.1091 0.6167, -0.06381, 0.1220 0.6558, -0.05300, 0.1111 0.7045, -0.04117, 0.1187 0.7429, -0.03210, 0.1182 0.8333, -0.01400, 0.2327 0.9311, -0.00120, 0.1861 --------- Run Conditions: vel=101.8 ft/s Re=0.999x10^6 AOA=9.04 Flap deflection=20.00 Totals: Cl=0.6689 Cdp=0.1715 Cm(c/4)=-0.1185 Cs=-0.0643 Ch=0.0152 Main component: Cl=0.3769 Cdp=-0.0161 Cm=-0.0399 Flap component: Cl=0.2920 Cdp=0.1876 Cm=-0.2505 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.1177 0.5905, -0.01667, 0.1321 0.5709, 0.03110, 0.0375 0.5889, 0.07933, -0.0324 0.5500, 0.08689, -0.0324 0.5110, 0.09367, -0.0374 0.4731, 0.09830, -0.0477 0.4349, 0.10070, -0.1299 0.3960, 0.10120, -0.3170 0.3566, 0.10020, -0.4268 0.3172, 0.09790, -0.5349 0.2778, 0.09440, -0.6468 0.2393, 0.08960, -0.7424 0.2056, 0.08360, -0.8619 0.1633, 0.07610, -0.9029 0.1261, 0.06710, -0.9790 0.0900, 0.05640, -1.1211 0.0571, 0.04390, -1.2017 0.0283, 0.02940, -1.3918 0.0142, 0.01970, -1.5977 0.0081, 0.01410, -1.4812 0.0026, 0.00780, -1.4441 0.0000, 0.00000, -1.1081 0.0037, -0.00840, 0.7605 0.0112, -0.01420, 0.9943 0.0191, -0.01930, 0.9794 0.0397, -0.03030, 0.8604 0.0706, -0.04420, 0.6378 0.1037, -0.05710, 0.4861 0.1384, -0.06890, 0.3434 0.1741, -0.07950, 0.1997 0.2102, -0.08660, 0.0317 0.2472, -0.09640, -0.0977 0.2844, -0.10270, -0.2149 0.3225, -0.10690, -0.2905 0.3608, -0.10890, -0.3918 0.3991, -0.10830, -0.4097 0.4373, -0.10510, -0.3969 0.4757, -0.09890, -0.3325 0.5137, -0.09067, -0.1482 0.5611, -0.07859, 0.0119 16 Flap element taps 1.0000, 0.00130, -0.6673 0.9365, 0.01390, -0.6839 0.8333, 0.03280, -0.7048 0.7436, 0.04930, -0.6797 0.7049, 0.05667, -0.6684 0.6662, 0.06411, -0.6835 0.6274, 0.07172, -0.6757 0.6009, 0.07523, -0.6915 0.6069, 0.02889, -0.0015 0.6079, -0.01747, 0.0312 0.6167, -0.06381, 0.0868 0.6558, -0.05300, 0.0957 0.7045, -0.04117, 0.0963 0.7429, -0.03210, 0.3043 0.8333, -0.01400, 0.5319 0.9311, -0.00120, 0.2133 --------- Run Conditions: vel=101.8 ft/s Re=0.998x10^6 AOA=12.02 Flap deflection=20.00 Totals: Cl=0.8844 Cdp=0.1852 Cm(c/4)=-0.1235 Cs=0.0031 Ch=0.0165 Main component: Cl=0.5829 Cdp=-0.0025 Cm=-0.0860 Flap component: Cl=0.3015 Cdp=0.1877 Cm=-0.2633 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.1345 0.5905, -0.01667, 0.1950 0.5709, 0.03110, -0.0754 0.5889, 0.07933, -0.2205 0.5500, 0.08689, -0.2088 0.5110, 0.09367, -0.2151 0.4731, 0.09830, -0.2113 0.4349, 0.10070, -0.2373 0.3960, 0.10120, -0.3529 0.3566, 0.10020, -0.4398 0.3172, 0.09790, -0.5766 0.2778, 0.09440, -0.7231 0.2393, 0.08960, -0.8574 0.2056, 0.08360, -1.0228 0.1633, 0.07610, -1.1105 0.1261, 0.06710, -1.2500 0.0900, 0.05640, -1.4697 0.0571, 0.04390, -1.6863 0.0283, 0.02940, -2.0912 0.0142, 0.01970, -2.5575 0.0081, 0.01410, -2.6287 0.0026, 0.00780, -2.7290 0.0000, 0.00000, -3.1198 0.0037, -0.00840, 0.1904 0.0112, -0.01420, 0.8749 0.0191, -0.01930, 0.9860 0.0397, -0.03030, 0.9717 0.0706, -0.04420, 0.8012 0.1037, -0.05710, 0.6604 0.1384, -0.06890, 0.5298 0.1741, -0.07950, 0.3891 0.2102, -0.08660, 0.2179 0.2472, -0.09640, 0.0894 0.2844, -0.10270, -0.0353 0.3225, -0.10690, -0.1175 0.3608, -0.10890, -0.2323 0.3991, -0.10830, -0.2652 0.4373, -0.10510, -0.2648 0.4757, -0.09890, -0.2141 0.5137, -0.09067, -0.1512 0.5611, -0.07859, 0.1340 16 Flap element taps 1.0000, 0.00130, -0.6227 0.9365, 0.01390, -0.6370 0.8333, 0.03280, -0.6574 0.7436, 0.04930, -0.6346 0.7049, 0.05667, -0.6203 0.6662, 0.06411, -0.6368 0.6274, 0.07172, -0.6306 0.6009, 0.07523, -0.6660 0.6069, 0.02889, -0.1730 0.6079, -0.01747, -0.0883 0.6167, -0.06381, 0.0320 0.6558, -0.05300, 0.0575 0.7045, -0.04117, 0.2028 0.7429, -0.03210, 0.6459 0.8333, -0.01400, 0.5416 0.9311, -0.00120, 0.2380 --------- Run Conditions: vel=102.1 ft/s Re=1.000x10^6 AOA=15.02 Flap deflection=20.00 Totals: Cl=0.9932 Cdp=0.2109 Cm(c/4)=-0.1309 Cs=0.0537 Ch=0.0151 Main component: Cl=0.6940 Cdp=0.0403 Cm=-0.1211 Flap component: Cl=0.2992 Cdp=0.1705 Cm=-0.2632 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.1274 0.5905, -0.01667, 0.2258 0.5709, 0.03110, -0.2265 0.5889, 0.07933, -0.4957 0.5500, 0.08689, -0.4678 0.5110, 0.09367, -0.4848 0.4731, 0.09830, -0.4877 0.4349, 0.10070, -0.4929 0.3960, 0.10120, -0.5163 0.3566, 0.10020, -0.5255 0.3172, 0.09790, -0.5505 0.2778, 0.09440, -0.6069 0.2393, 0.08960, -0.6895 0.2056, 0.08360, -0.8401 0.1633, 0.07610, -1.0284 0.1261, 0.06710, -1.2380 0.0900, 0.05640, -1.5472 0.0571, 0.04390, -1.9014 0.0283, 0.02940, -2.5020 0.0142, 0.01970, -3.2129 0.0081, 0.01410, -3.4304 0.0026, 0.00780, -3.7459 0.0000, 0.00000, -4.9446 0.0037, -0.00840, -0.4311 0.0112, -0.01420, 0.6607 0.0191, -0.01930, 0.9129 0.0397, -0.03030, 1.0044 0.0706, -0.04420, 0.9054 0.1037, -0.05710, 0.7781 0.1384, -0.06890, 0.6411 0.1741, -0.07950, 0.5049 0.2102, -0.08660, 0.3703 0.2472, -0.09640, 0.2316 0.2844, -0.10270, 0.1095 0.3225, -0.10690, 0.0086 0.3608, -0.10890, -0.0973 0.3991, -0.10830, -0.1592 0.4373, -0.10510, -0.1696 0.4757, -0.09890, -0.1246 0.5137, -0.09067, -0.0633 0.5611, -0.07859, 0.0657 16 Flap element taps 1.0000, 0.00130, -0.5235 0.9365, 0.01390, -0.5442 0.8333, 0.03280, -0.5563 0.7436, 0.04930, -0.5466 0.7049, 0.05667, -0.5324 0.6662, 0.06411, -0.5406 0.6274, 0.07172, -0.5296 0.6009, 0.07523, -0.5492 0.6069, 0.02889, -0.4249 0.6079, -0.01747, -0.2722 0.6167, -0.06381, -0.0457 0.6558, -0.05300, 0.0190 0.7045, -0.04117, 0.4035 0.7429, -0.03210, 0.8819 0.8333, -0.01400, 0.5494 0.9311, -0.00120, 0.2728 --------- Run Conditions: vel=100.8 ft/s Re=0.989x10^6 AOA=17.99 Flap deflection=20.00 Totals: Cl=0.9836 Cdp=0.3547 Cm(c/4)=-0.1845 Cs=-0.0335 Ch=0.0211 Main component: Cl=0.6526 Cdp=0.1667 Cm=-0.1516 Flap component: Cl=0.3310 Cdp=0.1880 Cm=-0.2942 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0735 0.5905, -0.01667, 0.1817 0.5709, 0.03110, -0.4366 0.5889, 0.07933, -0.8148 0.5500, 0.08689, -0.7752 0.5110, 0.09367, -0.7482 0.4731, 0.09830, -0.7360 0.4349, 0.10070, -0.7779 0.3960, 0.10120, -0.8284 0.3566, 0.10020, -0.8149 0.3172, 0.09790, -0.8214 0.2778, 0.09440, -0.8345 0.2393, 0.08960, -0.8298 0.2056, 0.08360, -0.8454 0.1633, 0.07610, -0.8578 0.1261, 0.06710, -0.8831 0.0900, 0.05640, -0.9139 0.0571, 0.04390, -1.0320 0.0283, 0.02940, -1.4293 0.0142, 0.01970, -1.9930 0.0081, 0.01410, -2.3170 0.0026, 0.00780, -2.7076 0.0000, 0.00000, -3.8814 0.0037, -0.00840, -0.2301 0.0112, -0.01420, 0.7036 0.0191, -0.01930, 0.9251 0.0397, -0.03030, 1.0099 0.0706, -0.04420, 0.9174 0.1037, -0.05710, 0.7987 0.1384, -0.06890, 0.6794 0.1741, -0.07950, 0.5431 0.2102, -0.08660, 0.4002 0.2472, -0.09640, 0.2689 0.2844, -0.10270, 0.1404 0.3225, -0.10690, 0.0463 0.3608, -0.10890, -0.0729 0.3991, -0.10830, -0.1368 0.4373, -0.10510, -0.1589 0.4757, -0.09890, -0.1252 0.5137, -0.09067, -0.0573 0.5611, -0.07859, 0.0170 16 Flap element taps 1.0000, 0.00130, -0.6062 0.9365, 0.01390, -0.6238 0.8333, 0.03280, -0.6505 0.7436, 0.04930, -0.6430 0.7049, 0.05667, -0.6299 0.6662, 0.06411, -0.6441 0.6274, 0.07172, -0.6326 0.6009, 0.07523, -0.6486 0.6069, 0.02889, -0.7069 0.6079, -0.01747, -0.5139 0.6167, -0.06381, -0.1818 0.6558, -0.05300, -0.0700 0.7045, -0.04117, 0.6541 0.7429, -0.03210, 0.9001 0.8333, -0.01400, 0.5358 0.9311, -0.00120, 0.2532 --------- Run Conditions: vel=102.1 ft/s Re=1.001x10^6 AOA=19.98 Flap deflection=20.00 Totals: Cl=1.0093 Cdp=0.4379 Cm(c/4)=-0.2036 Cs=-0.0667 Ch=0.0249 Main component: Cl=0.6686 Cdp=0.2287 Cm=-0.1696 Flap component: Cl=0.3406 Cdp=0.2092 Cm=-0.3085 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0787 0.5905, -0.01667, 0.2044 0.5709, 0.03110, -0.4764 0.5889, 0.07933, -0.9135 0.5500, 0.08689, -0.8941 0.5110, 0.09367, -0.8486 0.4731, 0.09830, -0.8243 0.4349, 0.10070, -0.8433 0.3960, 0.10120, -0.9163 0.3566, 0.10020, -0.9012 0.3172, 0.09790, -0.9055 0.2778, 0.09440, -0.9159 0.2393, 0.08960, -0.9178 0.2056, 0.08360, -0.9471 0.1633, 0.07610, -0.9292 0.1261, 0.06710, -0.9496 0.0900, 0.05640, -0.9453 0.0571, 0.04390, -0.9741 0.0283, 0.02940, -1.0679 0.0142, 0.01970, -1.2952 0.0081, 0.01410, -1.6093 0.0026, 0.00780, -1.9720 0.0000, 0.00000, -3.2050 0.0037, -0.00840, -0.1335 0.0112, -0.01420, 0.7113 0.0191, -0.01930, 0.9234 0.0397, -0.03030, 1.0133 0.0706, -0.04420, 0.9278 0.1037, -0.05710, 0.8179 0.1384, -0.06890, 0.7164 0.1741, -0.07950, 0.5848 0.2102, -0.08660, 0.4349 0.2472, -0.09640, 0.3112 0.2844, -0.10270, 0.1786 0.3225, -0.10690, 0.0911 0.3608, -0.10890, -0.0360 0.3991, -0.10830, -0.0970 0.4373, -0.10510, -0.1326 0.4757, -0.09890, -0.1074 0.5137, -0.09067, -0.0390 0.5611, -0.07859, 0.0172 16 Flap element taps 1.0000, 0.00130, -0.6486 0.9365, 0.01390, -0.6720 0.8333, 0.03280, -0.7019 0.7436, 0.04930, -0.6961 0.7049, 0.05667, -0.6796 0.6662, 0.06411, -0.6996 0.6274, 0.07172, -0.6854 0.6009, 0.07523, -0.6973 0.6069, 0.02889, -0.7682 0.6079, -0.01747, -0.5607 0.6167, -0.06381, -0.1933 0.6558, -0.05300, -0.0867 0.7045, -0.04117, 0.7324 0.7429, -0.03210, 0.8953 0.8333, -0.01400, 0.5301 0.9311, -0.00120, 0.2439 --------- Run Conditions: vel=101.3 ft/s Re=0.995x10^6 AOA=24.01 Flap deflection=20.00 Totals: Cl=0.9813 Cdp=0.5460 Cm(c/4)=-0.2197 Cs=-0.0995 Ch=0.0305 Main component: Cl=0.6416 Cdp=0.3009 Cm=-0.1770 Flap component: Cl=0.3397 Cdp=0.2451 Cm=-0.3223 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0598 0.5905, -0.01667, 0.1850 0.5709, 0.03110, -0.5153 0.5889, 0.07933, -0.9278 0.5500, 0.08689, -0.9148 0.5110, 0.09367, -0.9150 0.4731, 0.09830, -0.9012 0.4349, 0.10070, -0.8769 0.3960, 0.10120, -0.8949 0.3566, 0.10020, -0.8297 0.3172, 0.09790, -0.8296 0.2778, 0.09440, -0.8451 0.2393, 0.08960, -0.8437 0.2056, 0.08360, -0.8856 0.1633, 0.07610, -0.8670 0.1261, 0.06710, -0.9027 0.0900, 0.05640, -0.8865 0.0571, 0.04390, -0.8981 0.0283, 0.02940, -0.9180 0.0142, 0.01970, -0.9504 0.0081, 0.01410, -1.0997 0.0026, 0.00780, -1.3017 0.0000, 0.00000, -2.6746 0.0037, -0.00840, -0.1389 0.0112, -0.01420, 0.6700 0.0191, -0.01930, 0.8915 0.0397, -0.03030, 1.0107 0.0706, -0.04420, 0.9504 0.1037, -0.05710, 0.8588 0.1384, -0.06890, 0.7815 0.1741, -0.07950, 0.6547 0.2102, -0.08660, 0.5018 0.2472, -0.09640, 0.3894 0.2844, -0.10270, 0.2528 0.3225, -0.10690, 0.1719 0.3608, -0.10890, 0.0354 0.3991, -0.10830, -0.0282 0.4373, -0.10510, -0.0806 0.4757, -0.09890, -0.0680 0.5137, -0.09067, -0.0006 0.5611, -0.07859, 0.0470 16 Flap element taps 1.0000, 0.00130, -0.7169 0.9365, 0.01390, -0.7200 0.8333, 0.03280, -0.7474 0.7436, 0.04930, -0.7483 0.7049, 0.05667, -0.7368 0.6662, 0.06411, -0.7615 0.6274, 0.07172, -0.7467 0.6009, 0.07523, -0.7557 0.6069, 0.02889, -0.7924 0.6079, -0.01747, -0.5977 0.6167, -0.06381, -0.2211 0.6558, -0.05300, -0.0877 0.7045, -0.04117, 0.8090 0.7429, -0.03210, 0.8887 0.8333, -0.01400, 0.5250 0.9311, -0.00120, 0.2312 --------- Run Conditions: vel=102.4 ft/s Re=1.005x10^6 AOA=27.01 Flap deflection=20.00 Totals: Cl=1.1085 Cdp=0.7155 Cm(c/4)=-0.2689 Cs=-0.1340 Ch=0.0403 Main component: Cl=0.7258 Cdp=0.3952 Cm=-0.2154 Flap component: Cl=0.3827 Cdp=0.3203 Cm=-0.3816 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0425 0.5905, -0.01667, 0.1858 0.5709, 0.03110, -0.6403 0.5889, 0.07933, -1.1098 0.5500, 0.08689, -1.0889 0.5110, 0.09367, -1.1216 0.4731, 0.09830, -1.1234 0.4349, 0.10070, -1.1089 0.3960, 0.10120, -1.1140 0.3566, 0.10020, -1.0165 0.3172, 0.09790, -1.0025 0.2778, 0.09440, -1.0108 0.2393, 0.08960, -1.0121 0.2056, 0.08360, -1.0566 0.1633, 0.07610, -1.0074 0.1261, 0.06710, -1.0239 0.0900, 0.05640, -1.0017 0.0571, 0.04390, -1.0094 0.0283, 0.02940, -1.0088 0.0142, 0.01970, -1.0349 0.0081, 0.01410, -1.2557 0.0026, 0.00780, -1.1619 0.0000, 0.00000, -2.2627 0.0037, -0.00840, -0.2432 0.0112, -0.01420, 0.5809 0.0191, -0.01930, 0.8362 0.0397, -0.03030, 1.0011 0.0706, -0.04420, 0.9689 0.1037, -0.05710, 0.8932 0.1384, -0.06890, 0.8363 0.1741, -0.07950, 0.7177 0.2102, -0.08660, 0.5601 0.2472, -0.09640, 0.4541 0.2844, -0.10270, 0.3146 0.3225, -0.10690, 0.2390 0.3608, -0.10890, 0.0922 0.3991, -0.10830, 0.0229 0.4373, -0.10510, -0.0448 0.4757, -0.09890, -0.0469 0.5137, -0.09067, 0.0164 0.5611, -0.07859, 0.0697 16 Flap element taps 1.0000, 0.00130, -0.9820 0.9365, 0.01390, -0.9837 0.8333, 0.03280, -1.0054 0.7436, 0.04930, -0.9993 0.7049, 0.05667, -0.9836 0.6662, 0.06411, -1.0080 0.6274, 0.07172, -0.9903 0.6009, 0.07523, -0.9995 0.6069, 0.02889, -0.9652 0.6079, -0.01747, -0.7441 0.6167, -0.06381, -0.3030 0.6558, -0.05300, -0.1605 0.7045, -0.04117, 0.9299 0.7429, -0.03210, 0.8616 0.8333, -0.01400, 0.4954 0.9311, -0.00120, 0.1656