S809 SPOILER FLAP, LEGR, CHORD = 18 INCHES --------- Run Conditions: vel=103.5 ft/s Re=0.997x10^6 AOA=-6.01 Flap deflection=0.00 Totals: Cl=-0.5256 Cdp=0.0319 Cm(c/4)=0.0160 Cs=0.0233 Ch=-0.0152 Main component: Cl=-0.4538 Cdp=0.0483 Cm=0.0944 Flap component: Cl=-0.0718 Cdp=-0.0164 Cm=0.0531 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.2964 0.5905, -0.01667, -0.2883 0.5709, 0.03110, -0.2844 0.5889, 0.07933, -0.2857 0.5500, 0.08689, -0.2883 0.5110, 0.09367, -0.4304 0.4731, 0.09830, -0.4441 0.4349, 0.10070, -0.4298 0.3960, 0.10120, -0.3871 0.3566, 0.10020, -0.3206 0.3172, 0.09790, -0.2593 0.2778, 0.09440, -0.2155 0.2393, 0.08960, -0.1547 0.2056, 0.08360, -0.0784 0.1633, 0.07610, 0.0229 0.1261, 0.06710, 0.1593 0.0900, 0.05640, 0.2884 0.0571, 0.04390, 0.5203 0.0283, 0.02940, 0.7851 0.0142, 0.01970, 0.9669 0.0081, 0.01410, 0.9860 0.0026, 0.00780, 0.7105 0.0000, 0.00000, -0.4872 0.0037, -0.00840, -1.4279 0.0112, -0.01420, -1.2275 0.0191, -0.01930, -1.0107 0.0397, -0.03030, -0.7725 0.0706, -0.04420, -0.8307 0.1037, -0.05710, -0.8237 0.1384, -0.06890, -0.9033 0.1741, -0.07950, -0.9583 0.2102, -0.08660, -1.0202 0.2472, -0.09640, -1.0996 0.2844, -0.10270, -1.1228 0.3225, -0.10690, -1.1243 0.3608, -0.10890, -1.1193 0.3991, -0.10830, -1.0271 0.4373, -0.10510, -0.8678 0.4757, -0.09890, -0.6443 0.5137, -0.09067, -0.4173 0.5611, -0.07859, -0.3182 16 Flap element taps 1.0000, 0.00130, 0.0546 0.9365, 0.01390, 0.0400 0.8333, 0.03280, -0.0107 0.7436, 0.04930, -0.0499 0.7049, 0.05667, -0.0279 0.6662, 0.06411, -0.0460 0.6274, 0.07172, -0.0567 0.6009, 0.07523, -0.2881 0.6069, 0.02889, -0.2883 0.6079, -0.01747, -0.2873 0.6167, -0.06381, -0.2977 0.6558, -0.05300, -0.2913 0.7045, -0.04117, -0.2709 0.7429, -0.03210, -0.2607 0.8333, -0.01400, -0.2225 0.9311, -0.00120, -0.0780 --------- Run Conditions: vel=103.7 ft/s Re=0.997x10^6 AOA=0.00 Flap deflection=0.00 Totals: Cl=-0.0105 Cdp=0.0088 Cm(c/4)=-0.0227 Cs=-0.0088 Ch=0.0052 Main component: Cl=-0.0666 Cdp=0.0422 Cm=0.0244 Flap component: Cl=0.0561 Cdp=-0.0333 Cm=-0.0444 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3060 0.5905, -0.01667, -0.2379 0.5709, 0.03110, -0.2261 0.5889, 0.07933, -0.2395 0.5500, 0.08689, -0.3627 0.5110, 0.09367, -0.5521 0.4731, 0.09830, -0.6138 0.4349, 0.10070, -0.6409 0.3960, 0.10120, -0.6301 0.3566, 0.10020, -0.5933 0.3172, 0.09790, -0.5626 0.2778, 0.09440, -0.5528 0.2393, 0.08960, -0.5300 0.2056, 0.08360, -0.4932 0.1633, 0.07610, -0.4330 0.1261, 0.06710, -0.3449 0.0900, 0.05640, -0.2915 0.0571, 0.04390, -0.1088 0.0283, 0.02940, 0.1070 0.0142, 0.01970, 0.3599 0.0081, 0.01410, 0.5626 0.0026, 0.00780, 0.7548 0.0000, 0.00000, 0.9938 0.0037, -0.00840, 0.5188 0.0112, -0.01420, 0.2747 0.0191, -0.01930, 0.1945 0.0397, -0.03030, 0.1052 0.0706, -0.04420, -0.1172 0.1037, -0.05710, -0.2249 0.1384, -0.06890, -0.3709 0.1741, -0.07950, -0.4907 0.2102, -0.08660, -0.6037 0.2472, -0.09640, -0.7320 0.2844, -0.10270, -0.8117 0.3225, -0.10690, -0.8696 0.3608, -0.10890, -0.9330 0.3991, -0.10830, -0.9199 0.4373, -0.10510, -0.8530 0.4757, -0.09890, -0.7269 0.5137, -0.09067, -0.5045 0.5611, -0.07859, -0.3471 16 Flap element taps 1.0000, 0.00130, 0.1416 0.9365, 0.01390, 0.0890 0.8333, 0.03280, -0.0123 0.7436, 0.04930, -0.0960 0.7049, 0.05667, -0.1279 0.6662, 0.06411, -0.1831 0.6274, 0.07172, -0.2444 0.6009, 0.07523, -0.3114 0.6069, 0.02889, -0.2304 0.6079, -0.01747, -0.2429 0.6167, -0.06381, -0.1345 0.6558, -0.05300, -0.0606 0.7045, -0.04117, 0.0415 0.7429, -0.03210, 0.0688 0.8333, -0.01400, 0.1618 0.9311, -0.00120, 0.2281 Wake drag found for this condition, Cdw=0.0151 --------- Run Conditions: vel=103.8 ft/s Re=0.999x10^6 AOA=3.01 Flap deflection=0.00 Totals: Cl=0.2549 Cdp=0.0142 Cm(c/4)=-0.0263 Cs=-0.0008 Ch=0.0101 Main component: Cl=0.1705 Cdp=0.0396 Cm=-0.0251 Flap component: Cl=0.0844 Cdp=-0.0254 Cm=-0.0651 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3174 0.5905, -0.01667, -0.2318 0.5709, 0.03110, -0.2126 0.5889, 0.07933, -0.2257 0.5500, 0.08689, -0.3792 0.5110, 0.09367, -0.5861 0.4731, 0.09830, -0.6835 0.4349, 0.10070, -0.7351 0.3960, 0.10120, -0.7482 0.3566, 0.10020, -0.7326 0.3172, 0.09790, -0.7231 0.2778, 0.09440, -0.7351 0.2393, 0.08960, -0.7382 0.2056, 0.08360, -0.7287 0.1633, 0.07610, -0.6985 0.1261, 0.06710, -0.6482 0.0900, 0.05640, -0.6572 0.0571, 0.04390, -0.5400 0.0283, 0.02940, -0.4273 0.0142, 0.01970, -0.2730 0.0081, 0.01410, -0.0494 0.0026, 0.00780, 0.1466 0.0000, 0.00000, 0.7885 0.0037, -0.00840, 0.9430 0.0112, -0.01420, 0.7460 0.0191, -0.01930, 0.6274 0.0397, -0.03030, 0.4487 0.0706, -0.04420, 0.2038 0.1037, -0.05710, 0.0632 0.1384, -0.06890, -0.1001 0.1741, -0.07950, -0.2415 0.2102, -0.08660, -0.3620 0.2472, -0.09640, -0.5050 0.2844, -0.10270, -0.5980 0.3225, -0.10690, -0.6744 0.3608, -0.10890, -0.7565 0.3991, -0.10830, -0.7653 0.4373, -0.10510, -0.7243 0.4757, -0.09890, -0.6244 0.5137, -0.09067, -0.4271 0.5611, -0.07859, -0.2901 16 Flap element taps 1.0000, 0.00130, 0.0586 0.9365, 0.01390, 0.0171 0.8333, 0.03280, -0.0645 0.7436, 0.04930, -0.1383 0.7049, 0.05667, -0.1733 0.6662, 0.06411, -0.2222 0.6274, 0.07172, -0.2613 0.6009, 0.07523, -0.3623 0.6069, 0.02889, -0.2191 0.6079, -0.01747, -0.2426 0.6167, -0.06381, -0.0370 0.6558, -0.05300, -0.0098 0.7045, -0.04117, 0.0844 0.7429, -0.03210, 0.0950 0.8333, -0.01400, 0.1761 0.9311, -0.00120, 0.2218 Wake drag found for this condition, Cdw=0.0175 --------- Run Conditions: vel=103.7 ft/s Re=0.996x10^6 AOA=6.04 Flap deflection=0.00 Totals: Cl=0.4694 Cdp=0.0257 Cm(c/4)=-0.0252 Cs=0.0238 Ch=0.0031 Main component: Cl=0.3671 Cdp=0.0350 Cm=-0.0622 Flap component: Cl=0.1023 Cdp=-0.0093 Cm=-0.0803 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.2929 0.5905, -0.01667, -0.1985 0.5709, 0.03110, -0.1779 0.5889, 0.07933, -0.1887 0.5500, 0.08689, -0.3340 0.5110, 0.09367, -0.5474 0.4731, 0.09830, -0.6842 0.4349, 0.10070, -0.7708 0.3960, 0.10120, -0.8108 0.3566, 0.10020, -0.8265 0.3172, 0.09790, -0.8398 0.2778, 0.09440, -0.8809 0.2393, 0.08960, -0.9122 0.2056, 0.08360, -0.9332 0.1633, 0.07610, -0.9425 0.1261, 0.06710, -0.9357 0.0900, 0.05640, -1.0148 0.0571, 0.04390, -0.9833 0.0283, 0.02940, -1.0181 0.0142, 0.01970, -1.0301 0.0081, 0.01410, -0.7706 0.0026, 0.00780, -0.6392 0.0000, 0.00000, -0.0592 0.0037, -0.00840, 0.9693 0.0112, -0.01420, 0.9669 0.0191, -0.01930, 0.8829 0.0397, -0.03030, 0.7018 0.0706, -0.04420, 0.4568 0.1037, -0.05710, 0.2982 0.1384, -0.06890, 0.1262 0.1741, -0.07950, -0.0296 0.2102, -0.08660, -0.1636 0.2472, -0.09640, -0.3153 0.2844, -0.10270, -0.4245 0.3225, -0.10690, -0.5105 0.3608, -0.10890, -0.6036 0.3991, -0.10830, -0.6321 0.4373, -0.10510, -0.6107 0.4757, -0.09890, -0.5352 0.5137, -0.09067, -0.3574 0.5611, -0.07859, -0.2356 16 Flap element taps 1.0000, 0.00130, -0.0786 0.9365, 0.01390, -0.1220 0.8333, 0.03280, -0.1501 0.7436, 0.04930, -0.1718 0.7049, 0.05667, -0.1888 0.6662, 0.06411, -0.2051 0.6274, 0.07172, -0.2252 0.6009, 0.07523, -0.2930 0.6069, 0.02889, -0.1823 0.6079, -0.01747, -0.2123 0.6167, -0.06381, -0.0216 0.6558, -0.05300, 0.0093 0.7045, -0.04117, 0.0989 0.7429, -0.03210, 0.0981 0.8333, -0.01400, 0.1656 0.9311, -0.00120, 0.1837 --------- Run Conditions: vel=104.3 ft/s Re=1.000x10^6 AOA=9.04 Flap deflection=0.00 Totals: Cl=0.6496 Cdp=0.0414 Cm(c/4)=-0.0241 Cs=0.0612 Ch=0.0040 Main component: Cl=0.5251 Cdp=0.0356 Cm=-0.0875 Flap component: Cl=0.1245 Cdp=0.0058 Cm=-0.0986 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3119 0.5905, -0.01667, -0.2067 0.5709, 0.03110, -0.1677 0.5889, 0.07933, -0.1917 0.5500, 0.08689, -0.2646 0.5110, 0.09367, -0.4324 0.4731, 0.09830, -0.6031 0.4349, 0.10070, -0.7338 0.3960, 0.10120, -0.8100 0.3566, 0.10020, -0.8613 0.3172, 0.09790, -0.9106 0.2778, 0.09440, -0.9808 0.2393, 0.08960, -1.0424 0.2056, 0.08360, -1.0956 0.1633, 0.07610, -1.1504 0.1261, 0.06710, -1.1912 0.0900, 0.05640, -1.3464 0.0571, 0.04390, -1.4173 0.0283, 0.02940, -1.6317 0.0142, 0.01970, -1.8534 0.0081, 0.01410, -1.7163 0.0026, 0.00780, -1.6981 0.0000, 0.00000, -1.4359 0.0037, -0.00840, 0.7017 0.0112, -0.01420, 0.9907 0.0191, -0.01930, 0.9907 0.0397, -0.03030, 0.8659 0.0706, -0.04420, 0.6480 0.1037, -0.05710, 0.4895 0.1384, -0.06890, 0.3127 0.1741, -0.07950, 0.1561 0.2102, -0.08660, 0.0180 0.2472, -0.09640, -0.1399 0.2844, -0.10270, -0.2583 0.3225, -0.10690, -0.3672 0.3608, -0.10890, -0.4731 0.3991, -0.10830, -0.5244 0.4373, -0.10510, -0.5178 0.4757, -0.09890, -0.4623 0.5137, -0.09067, -0.3130 0.5611, -0.07859, -0.1761 16 Flap element taps 1.0000, 0.00130, -0.1909 0.9365, 0.01390, -0.2307 0.8333, 0.03280, -0.2258 0.7436, 0.04930, -0.2281 0.7049, 0.05667, -0.2317 0.6662, 0.06411, -0.2343 0.6274, 0.07172, -0.2447 0.6009, 0.07523, -0.2708 0.6069, 0.02889, -0.1736 0.6079, -0.01747, -0.2272 0.6167, -0.06381, 0.0334 0.6558, -0.05300, 0.0348 0.7045, -0.04117, 0.1212 0.7429, -0.03210, 0.1049 0.8333, -0.01400, 0.1585 0.9311, -0.00120, 0.1485 --------- Run Conditions: vel=103.3 ft/s Re=0.991x10^6 AOA=12.02 Flap deflection=0.00 Totals: Cl=0.7828 Cdp=0.0656 Cm(c/4)=-0.0231 Cs=0.0988 Ch=0.0104 Main component: Cl=0.6351 Cdp=0.0432 Cm=-0.1002 Flap component: Cl=0.1477 Cdp=0.0225 Cm=-0.1178 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3807 0.5905, -0.01667, -0.2218 0.5709, 0.03110, -0.1749 0.5889, 0.07933, -0.2610 0.5500, 0.08689, -0.2760 0.5110, 0.09367, -0.3145 0.4731, 0.09830, -0.4303 0.4349, 0.10070, -0.5828 0.3960, 0.10120, -0.7071 0.3566, 0.10020, -0.8159 0.3172, 0.09790, -0.9050 0.2778, 0.09440, -1.0142 0.2393, 0.08960, -1.1093 0.2056, 0.08360, -1.1985 0.1633, 0.07610, -1.3022 0.1261, 0.06710, -1.3943 0.0900, 0.05640, -1.6209 0.0571, 0.04390, -1.8064 0.0283, 0.02940, -2.2076 0.0142, 0.01970, -2.6489 0.0081, 0.01410, -2.6768 0.0026, 0.00780, -2.7734 0.0000, 0.00000, -3.1348 0.0037, -0.00840, 0.2217 0.0112, -0.01420, 0.8912 0.0191, -0.01930, 0.9978 0.0397, -0.03030, 0.9596 0.0706, -0.04420, 0.7881 0.1037, -0.05710, 0.6381 0.1384, -0.06890, 0.4663 0.1741, -0.07950, 0.3095 0.2102, -0.08660, 0.1718 0.2472, -0.09640, 0.0092 0.2844, -0.10270, -0.1144 0.3225, -0.10690, -0.2371 0.3608, -0.10890, -0.3522 0.3991, -0.10830, -0.4215 0.4373, -0.10510, -0.4252 0.4757, -0.09890, -0.3787 0.5137, -0.09067, -0.3071 0.5611, -0.07859, -0.1765 16 Flap element taps 1.0000, 0.00130, -0.2635 0.9365, 0.01390, -0.3088 0.8333, 0.03280, -0.2987 0.7436, 0.04930, -0.2928 0.7049, 0.05667, -0.2941 0.6662, 0.06411, -0.2892 0.6274, 0.07172, -0.2875 0.6009, 0.07523, -0.3000 0.6069, 0.02889, -0.1790 0.6079, -0.01747, -0.2489 0.6167, -0.06381, 0.1538 0.6558, -0.05300, 0.0623 0.7045, -0.04117, 0.1375 0.7429, -0.03210, 0.1126 0.8333, -0.01400, 0.1472 0.9311, -0.00120, 0.1178 --------- Run Conditions: vel=104.6 ft/s Re=0.999x10^6 AOA=15.01 Flap deflection=0.00 Totals: Cl=0.8672 Cdp=0.1015 Cm(c/4)=-0.0305 Cs=0.1266 Ch=0.0169 Main component: Cl=0.6934 Cdp=0.0628 Cm=-0.1068 Flap component: Cl=0.1738 Cdp=0.0386 Cm=-0.1397 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.4137 0.5905, -0.01667, -0.2799 0.5709, 0.03110, -0.2269 0.5889, 0.07933, -0.3798 0.5500, 0.08689, -0.3755 0.5110, 0.09367, -0.3962 0.4731, 0.09830, -0.3968 0.4349, 0.10070, -0.4413 0.3960, 0.10120, -0.5126 0.3566, 0.10020, -0.6297 0.3172, 0.09790, -0.7528 0.2778, 0.09440, -0.8997 0.2393, 0.08960, -1.0399 0.2056, 0.08360, -1.1850 0.1633, 0.07610, -1.3377 0.1261, 0.06710, -1.4942 0.0900, 0.05640, -1.7783 0.0571, 0.04390, -2.0748 0.0283, 0.02940, -2.6554 0.0142, 0.01970, -3.3156 0.0081, 0.01410, -3.4891 0.0026, 0.00780, -3.7688 0.0000, 0.00000, -4.8347 0.0037, -0.00840, -0.3443 0.0112, -0.01420, 0.7059 0.0191, -0.01930, 0.9378 0.0397, -0.03030, 0.9955 0.0706, -0.04420, 0.8730 0.1037, -0.05710, 0.7463 0.1384, -0.06890, 0.5755 0.1741, -0.07950, 0.4344 0.2102, -0.08660, 0.2901 0.2472, -0.09640, 0.1339 0.2844, -0.10270, -0.0019 0.3225, -0.10690, -0.1340 0.3608, -0.10890, -0.2522 0.3991, -0.10830, -0.3417 0.4373, -0.10510, -0.3600 0.4757, -0.09890, -0.3311 0.5137, -0.09067, -0.2605 0.5611, -0.07859, -0.2039 16 Flap element taps 1.0000, 0.00130, -0.3630 0.9365, 0.01390, -0.4060 0.8333, 0.03280, -0.3953 0.7436, 0.04930, -0.3834 0.7049, 0.05667, -0.3739 0.6662, 0.06411, -0.3750 0.6274, 0.07172, -0.3747 0.6009, 0.07523, -0.3784 0.6069, 0.02889, -0.2317 0.6079, -0.01747, -0.3232 0.6167, -0.06381, 0.2237 0.6558, -0.05300, 0.0663 0.7045, -0.04117, 0.1405 0.7429, -0.03210, 0.1095 0.8333, -0.01400, 0.1261 0.9311, -0.00120, 0.0749 --------- Run Conditions: vel=105.0 ft/s Re=1.002x10^6 AOA=17.97 Flap deflection=0.00 Totals: Cl=0.7000 Cdp=0.2019 Cm(c/4)=-0.0734 Cs=0.0239 Ch=0.0226 Main component: Cl=0.4944 Cdp=0.1435 Cm=-0.0880 Flap component: Cl=0.2057 Cdp=0.0583 Cm=-0.1674 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.5203 0.5905, -0.01667, -0.4209 0.5709, 0.03110, -0.3571 0.5889, 0.07933, -0.6383 0.5500, 0.08689, -0.6124 0.5110, 0.09367, -0.5727 0.4731, 0.09830, -0.5564 0.4349, 0.10070, -0.5708 0.3960, 0.10120, -0.5640 0.3566, 0.10020, -0.5750 0.3172, 0.09790, -0.5836 0.2778, 0.09440, -0.5991 0.2393, 0.08960, -0.6074 0.2056, 0.08360, -0.6359 0.1633, 0.07610, -0.6916 0.1261, 0.06710, -0.7605 0.0900, 0.05640, -0.9295 0.0571, 0.04390, -1.2800 0.0283, 0.02940, -1.8850 0.0142, 0.01970, -2.5297 0.0081, 0.01410, -2.7247 0.0026, 0.00780, -3.0382 0.0000, 0.00000, -3.9942 0.0037, -0.00840, -0.1561 0.0112, -0.01420, 0.7502 0.0191, -0.01930, 0.9486 0.0397, -0.03030, 0.9923 0.0706, -0.04420, 0.8709 0.1037, -0.05710, 0.7486 0.1384, -0.06890, 0.5748 0.1741, -0.07950, 0.4336 0.2102, -0.08660, 0.2907 0.2472, -0.09640, 0.1297 0.2844, -0.10270, -0.0114 0.3225, -0.10690, -0.1521 0.3608, -0.10890, -0.2783 0.3991, -0.10830, -0.3771 0.4373, -0.10510, -0.4032 0.4757, -0.09890, -0.3810 0.5137, -0.09067, -0.3093 0.5611, -0.07859, -0.2449 16 Flap element taps 1.0000, 0.00130, -0.4890 0.9365, 0.01390, -0.5542 0.8333, 0.03280, -0.5727 0.7436, 0.04930, -0.5622 0.7049, 0.05667, -0.5413 0.6662, 0.06411, -0.5347 0.6274, 0.07172, -0.5197 0.6009, 0.07523, -0.5097 0.6069, 0.02889, -0.3610 0.6079, -0.01747, -0.4671 0.6167, -0.06381, 0.2053 0.6558, -0.05300, 0.0127 0.7045, -0.04117, 0.0817 0.7429, -0.03210, 0.0452 0.8333, -0.01400, 0.0593 0.9311, -0.00120, -0.0050 --------- Run Conditions: vel=104.7 ft/s Re=0.997x10^6 AOA=19.98 Flap deflection=0.00 Totals: Cl=0.7020 Cdp=0.2675 Cm(c/4)=-0.0953 Cs=-0.0115 Ch=0.0275 Main component: Cl=0.4794 Cdp=0.1960 Cm=-0.1005 Flap component: Cl=0.2226 Cdp=0.0715 Cm=-0.1826 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.5372 0.5905, -0.01667, -0.4744 0.5709, 0.03110, -0.4111 0.5889, 0.07933, -0.7179 0.5500, 0.08689, -0.6973 0.5110, 0.09367, -0.6665 0.4731, 0.09830, -0.6273 0.4349, 0.10070, -0.6399 0.3960, 0.10120, -0.6413 0.3566, 0.10020, -0.6645 0.3172, 0.09790, -0.6704 0.2778, 0.09440, -0.6853 0.2393, 0.08960, -0.6754 0.2056, 0.08360, -0.6847 0.1633, 0.07610, -0.7071 0.1261, 0.06710, -0.7342 0.0900, 0.05640, -0.7721 0.0571, 0.04390, -0.9131 0.0283, 0.02940, -1.3703 0.0142, 0.01970, -1.9663 0.0081, 0.01410, -2.2317 0.0026, 0.00780, -2.6076 0.0000, 0.00000, -3.6105 0.0037, -0.00840, -0.1067 0.0112, -0.01420, 0.7549 0.0191, -0.01930, 0.9477 0.0397, -0.03030, 0.9973 0.0706, -0.04420, 0.8868 0.1037, -0.05710, 0.7700 0.1384, -0.06890, 0.5993 0.1741, -0.07950, 0.4609 0.2102, -0.08660, 0.3193 0.2472, -0.09640, 0.1578 0.2844, -0.10270, 0.0164 0.3225, -0.10690, -0.1306 0.3608, -0.10890, -0.2582 0.3991, -0.10830, -0.3636 0.4373, -0.10510, -0.3928 0.4757, -0.09890, -0.3787 0.5137, -0.09067, -0.3070 0.5611, -0.07859, -0.2378 16 Flap element taps 1.0000, 0.00130, -0.5578 0.9365, 0.01390, -0.6198 0.8333, 0.03280, -0.6431 0.7436, 0.04930, -0.6403 0.7049, 0.05667, -0.6276 0.6662, 0.06411, -0.6191 0.6274, 0.07172, -0.6006 0.6009, 0.07523, -0.5926 0.6069, 0.02889, -0.4168 0.6079, -0.01747, -0.5298 0.6167, -0.06381, 0.1983 0.6558, -0.05300, 0.0026 0.7045, -0.04117, 0.0676 0.7429, -0.03210, 0.0273 0.8333, -0.01400, 0.0403 0.9311, -0.00120, -0.0350 --------- Run Conditions: vel=106.2 ft/s Re=1.010x10^6 AOA=23.98 Flap deflection=0.00 Totals: Cl=0.6918 Cdp=0.3796 Cm(c/4)=-0.1198 Cs=-0.0656 Ch=0.0315 Main component: Cl=0.4575 Cdp=0.2871 Cm=-0.1200 Flap component: Cl=0.2343 Cdp=0.0924 Cm=-0.1964 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.5028 0.5905, -0.01667, -0.5306 0.5709, 0.03110, -0.4698 0.5889, 0.07933, -0.8251 0.5500, 0.08689, -0.7750 0.5110, 0.09367, -0.7438 0.4731, 0.09830, -0.7037 0.4349, 0.10070, -0.7043 0.3960, 0.10120, -0.6916 0.3566, 0.10020, -0.7049 0.3172, 0.09790, -0.7039 0.2778, 0.09440, -0.7175 0.2393, 0.08960, -0.7133 0.2056, 0.08360, -0.7126 0.1633, 0.07610, -0.7267 0.1261, 0.06710, -0.7152 0.0900, 0.05640, -0.7200 0.0571, 0.04390, -0.7209 0.0283, 0.02940, -0.7656 0.0142, 0.01970, -0.8451 0.0081, 0.01410, -1.0451 0.0026, 0.00780, -1.3847 0.0000, 0.00000, -2.4470 0.0037, -0.00840, 0.0540 0.0112, -0.01420, 0.7657 0.0191, -0.01930, 0.9413 0.0397, -0.03030, 0.9992 0.0706, -0.04420, 0.9152 0.1037, -0.05710, 0.8193 0.1384, -0.06890, 0.6627 0.1741, -0.07950, 0.5340 0.2102, -0.08660, 0.4053 0.2472, -0.09640, 0.2480 0.2844, -0.10270, 0.1091 0.3225, -0.10690, -0.0386 0.3608, -0.10890, -0.1693 0.3991, -0.10830, -0.2836 0.4373, -0.10510, -0.3242 0.4757, -0.09890, -0.3245 0.5137, -0.09067, -0.2584 0.5611, -0.07859, -0.1844 16 Flap element taps 1.0000, 0.00130, -0.6225 0.9365, 0.01390, -0.6805 0.8333, 0.03280, -0.7024 0.7436, 0.04930, -0.7051 0.7049, 0.05667, -0.6927 0.6662, 0.06411, -0.6849 0.6274, 0.07172, -0.6681 0.6009, 0.07523, -0.6586 0.6069, 0.02889, -0.4744 0.6079, -0.01747, -0.5814 0.6167, -0.06381, 0.1712 0.6558, -0.05300, 0.0116 0.7045, -0.04117, 0.0679 0.7429, -0.03210, 0.0202 0.8333, -0.01400, 0.0231 0.9311, -0.00120, -0.0581 --------- Run Conditions: vel=105.0 ft/s Re=0.999x10^6 AOA=27.01 Flap deflection=0.00 Totals: Cl=0.7771 Cdp=0.4496 Cm(c/4)=-0.1278 Cs=-0.0476 Ch=0.0362 Main component: Cl=0.5331 Cdp=0.3381 Cm=-0.1432 Flap component: Cl=0.2440 Cdp=0.1115 Cm=-0.2088 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.5110 0.5905, -0.01667, -0.5659 0.5709, 0.03110, -0.5114 0.5889, 0.07933, -0.8253 0.5500, 0.08689, -0.8095 0.5110, 0.09367, -0.8002 0.4731, 0.09830, -0.7676 0.4349, 0.10070, -0.7727 0.3960, 0.10120, -0.7527 0.3566, 0.10020, -0.7760 0.3172, 0.09790, -0.7825 0.2778, 0.09440, -0.8061 0.2393, 0.08960, -0.8037 0.2056, 0.08360, -0.8206 0.1633, 0.07610, -0.8692 0.1261, 0.06710, -0.9375 0.0900, 0.05640, -0.9943 0.0571, 0.04390, -0.9833 0.0283, 0.02940, -1.0247 0.0142, 0.01970, -1.0674 0.0081, 0.01410, -1.2138 0.0026, 0.00780, -1.4167 0.0000, 0.00000, -2.8901 0.0037, -0.00840, -0.2228 0.0112, -0.01420, 0.6401 0.0191, -0.01930, 0.8813 0.0397, -0.03030, 0.9991 0.0706, -0.04420, 0.9479 0.1037, -0.05710, 0.8694 0.1384, -0.06890, 0.7195 0.1741, -0.07950, 0.5987 0.2102, -0.08660, 0.4753 0.2472, -0.09640, 0.3203 0.2844, -0.10270, 0.1819 0.3225, -0.10690, 0.0292 0.3608, -0.10890, -0.1031 0.3991, -0.10830, -0.2241 0.4373, -0.10510, -0.2723 0.4757, -0.09890, -0.2829 0.5137, -0.09067, -0.2229 0.5611, -0.07859, -0.1556 16 Flap element taps 1.0000, 0.00130, -0.7128 0.9365, 0.01390, -0.7423 0.8333, 0.03280, -0.7472 0.7436, 0.04930, -0.7473 0.7049, 0.05667, -0.7398 0.6662, 0.06411, -0.7376 0.6274, 0.07172, -0.7357 0.6009, 0.07523, -0.7430 0.6069, 0.02889, -0.5122 0.6079, -0.01747, -0.6232 0.6167, -0.06381, 0.1961 0.6558, -0.05300, 0.0201 0.7045, -0.04117, 0.0705 0.7429, -0.03210, 0.0213 0.8333, -0.01400, 0.0109 0.9311, -0.00120, -0.0843