S809 SPOILER FLAP, CLEAN, CHORD = 18 INCHES --------- Run Conditions: vel=103.4 ft/s Re=1.000x10^6 AOA=-6.06 Flap deflection=90.00 Totals: Cl=0.0276 Cdp=0.6433 Cm(c/4)=-0.0686 Cs=-0.6427 Ch=0.0830 Main component: Cl=-0.1728 Cdp=-0.0823 Cm=0.0190 Flap component: Cl=0.2004 Cdp=0.7257 Cm=-0.0775 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.5148 0.5905, -0.01667, 0.5396 0.5709, 0.03110, 0.5494 0.5889, 0.07933, 0.5354 0.5500, 0.08689, 0.4268 0.5110, 0.09367, 0.1785 0.4731, 0.09830, 0.0230 0.4349, 0.10070, 0.0022 0.3960, 0.10120, -0.0657 0.3566, 0.10020, -0.0680 0.3172, 0.09790, -0.0714 0.2778, 0.09440, -0.0803 0.2393, 0.08960, -0.0650 0.2056, 0.08360, -0.0471 0.1633, 0.07610, 0.0318 0.1261, 0.06710, 0.1123 0.0900, 0.05640, 0.2431 0.0571, 0.04390, 0.4053 0.0283, 0.02940, 0.6539 0.0142, 0.01970, 0.8653 0.0081, 0.01410, 0.9398 0.0026, 0.00780, 0.9257 0.0000, 0.00000, 0.4483 0.0037, -0.00840, -0.3636 0.0112, -0.01420, -0.3732 0.0191, -0.01930, -0.3200 0.0397, -0.03030, -0.2647 0.0706, -0.04420, -0.2983 0.1037, -0.05710, -0.3442 0.1384, -0.06890, -0.3736 0.1741, -0.07950, -0.4036 0.2102, -0.08660, -0.4423 0.2472, -0.09640, -0.4470 0.2844, -0.10270, -0.4294 0.3225, -0.10690, -0.3485 0.3608, -0.10890, -0.3236 0.3991, -0.10830, -0.2719 0.4373, -0.10510, 0.1396 0.4757, -0.09890, 0.3297 0.5137, -0.09067, 0.4788 0.5611, -0.07859, 0.5142 16 Flap element taps 1.0000, 0.00130, -1.2986 0.9365, 0.01390, -1.4573 0.8333, 0.03280, -1.4143 0.7436, 0.04930, -1.4521 0.7049, 0.05667, -1.4510 0.6662, 0.06411, -1.4769 0.6274, 0.07172, -1.4222 0.6009, 0.07523, -1.6347 0.6069, 0.02889, -1.6484 0.6079, -0.01747, -1.6058 0.6167, -0.06381, 0.1068 0.6558, -0.05300, 0.9844 0.7045, -0.04117, 0.8993 0.7429, -0.03210, 0.7313 0.8333, -0.01400, 0.5772 0.9311, -0.00120, 0.5505 --------- Run Conditions: vel=103.8 ft/s Re=1.003x10^6 AOA=0.03 Flap deflection=90.00 Totals: Cl=0.1158 Cdp=0.6135 Cm(c/4)=-0.0504 Cs=-0.6134 Ch=0.0413 Main component: Cl=-0.0150 Cdp=-0.0904 Cm=0.0119 Flap component: Cl=0.1308 Cdp=0.7040 Cm=-0.0913 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.5861 0.5905, -0.01667, 0.5765 0.5709, 0.03110, 0.5873 0.5889, 0.07933, 0.5569 0.5500, 0.08689, 0.5399 0.5110, 0.09367, 0.4173 0.4731, 0.09830, 0.2481 0.4349, 0.10070, 0.0207 0.3960, 0.10120, -0.1280 0.3566, 0.10020, -0.1090 0.3172, 0.09790, -0.1543 0.2778, 0.09440, -0.2006 0.2393, 0.08960, -0.2283 0.2056, 0.08360, -0.2742 0.1633, 0.07610, -0.2105 0.1261, 0.06710, -0.1931 0.0900, 0.05640, -0.1034 0.0571, 0.04390, -0.0145 0.0283, 0.02940, 0.1700 0.0142, 0.01970, 0.3901 0.0081, 0.01410, 0.5039 0.0026, 0.00780, 0.7815 0.0000, 0.00000, 1.0035 0.0037, -0.00840, 0.6855 0.0112, -0.01420, 0.4714 0.0191, -0.01930, 0.3822 0.0397, -0.03030, 0.2568 0.0706, -0.04420, 0.0991 0.1037, -0.05710, -0.0161 0.1384, -0.06890, -0.0753 0.1741, -0.07950, -0.1571 0.2102, -0.08660, -0.2615 0.2472, -0.09640, -0.3008 0.2844, -0.10270, -0.3395 0.3225, -0.10690, -0.2892 0.3608, -0.10890, -0.2743 0.3991, -0.10830, -0.2056 0.4373, -0.10510, -0.2077 0.4757, -0.09890, 0.1990 0.5137, -0.09067, 0.3894 0.5611, -0.07859, 0.5353 16 Flap element taps 1.0000, 0.00130, -1.2508 0.9365, 0.01390, -1.3721 0.8333, 0.03280, -1.4128 0.7436, 0.04930, -1.3847 0.7049, 0.05667, -1.3922 0.6662, 0.06411, -1.4489 0.6274, 0.07172, -1.4226 0.6009, 0.07523, -1.6266 0.6069, 0.02889, -1.6988 0.6079, -0.01747, -1.7281 0.6167, -0.06381, -0.1363 0.6558, -0.05300, 0.6405 0.7045, -0.04117, 0.6196 0.7429, -0.03210, 0.5953 0.8333, -0.01400, 0.5965 0.9311, -0.00120, 0.7522 --------- Run Conditions: vel=103.3 ft/s Re=0.998x10^6 AOA=3.04 Flap deflection=90.00 Totals: Cl=0.1165 Cdp=0.6414 Cm(c/4)=-0.0450 Cs=-0.6343 Ch=0.0269 Main component: Cl=0.0102 Cdp=-0.0854 Cm=0.0216 Flap component: Cl=0.1062 Cdp=0.7268 Cm=-0.1042 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.5758 0.5905, -0.01667, 0.5484 0.5709, 0.03110, 0.5590 0.5889, 0.07933, 0.5217 0.5500, 0.08689, 0.5312 0.5110, 0.09367, 0.4896 0.4731, 0.09830, 0.3519 0.4349, 0.10070, 0.1786 0.3960, 0.10120, -0.0174 0.3566, 0.10020, -0.0980 0.3172, 0.09790, -0.1396 0.2778, 0.09440, -0.1892 0.2393, 0.08960, -0.2406 0.2056, 0.08360, -0.3289 0.1633, 0.07610, -0.2636 0.1261, 0.06710, -0.2879 0.0900, 0.05640, -0.2192 0.0571, 0.04390, -0.1811 0.0283, 0.02940, -0.0522 0.0142, 0.01970, 0.1282 0.0081, 0.01410, 0.2085 0.0026, 0.00780, 0.5146 0.0000, 0.00000, 0.9421 0.0037, -0.00840, 0.8886 0.0112, -0.01420, 0.6901 0.0191, -0.01930, 0.5824 0.0397, -0.03030, 0.4216 0.0706, -0.04420, 0.2280 0.1037, -0.05710, 0.0896 0.1384, -0.06890, 0.0338 0.1741, -0.07950, -0.0682 0.2102, -0.08660, -0.2116 0.2472, -0.09640, -0.2595 0.2844, -0.10270, -0.3292 0.3225, -0.10690, -0.2852 0.3608, -0.10890, -0.3096 0.3991, -0.10830, -0.2193 0.4373, -0.10510, -0.2185 0.4757, -0.09890, 0.0041 0.5137, -0.09067, 0.2892 0.5611, -0.07859, 0.4562 16 Flap element taps 1.0000, 0.00130, -1.2098 0.9365, 0.01390, -1.3095 0.8333, 0.03280, -1.3978 0.7436, 0.04930, -1.4021 0.7049, 0.05667, -1.4178 0.6662, 0.06411, -1.5246 0.6274, 0.07172, -1.5301 0.6009, 0.07523, -1.7603 0.6069, 0.02889, -1.7540 0.6079, -0.01747, -1.7679 0.6167, -0.06381, -0.4116 0.6558, -0.05300, 0.5217 0.7045, -0.04117, 0.6233 0.7429, -0.03210, 0.5786 0.8333, -0.01400, 0.6646 0.9311, -0.00120, 0.9870 --------- Run Conditions: vel=103.0 ft/s Re=0.995x10^6 AOA=6.07 Flap deflection=90.00 Totals: Cl=0.1836 Cdp=0.6538 Cm(c/4)=-0.0368 Cs=-0.6308 Ch=0.0195 Main component: Cl=0.1102 Cdp=-0.0761 Cm=0.0102 Flap component: Cl=0.0734 Cdp=0.7300 Cm=-0.1099 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.5273 0.5905, -0.01667, 0.4991 0.5709, 0.03110, 0.5075 0.5889, 0.07933, 0.4652 0.5500, 0.08689, 0.4747 0.5110, 0.09367, 0.4648 0.4731, 0.09830, 0.3966 0.4349, 0.10070, 0.2115 0.3960, 0.10120, -0.0153 0.3566, 0.10020, -0.0131 0.3172, 0.09790, -0.2002 0.2778, 0.09440, -0.2565 0.2393, 0.08960, -0.3133 0.2056, 0.08360, -0.4400 0.1633, 0.07610, -0.3840 0.1261, 0.06710, -0.4539 0.0900, 0.05640, -0.4211 0.0571, 0.04390, -0.4518 0.0283, 0.02940, -0.4169 0.0142, 0.01970, -0.3211 0.0081, 0.01410, -0.3112 0.0026, 0.00780, -0.0197 0.0000, 0.00000, 0.5437 0.0037, -0.00840, 0.9916 0.0112, -0.01420, 0.8962 0.0191, -0.01930, 0.7971 0.0397, -0.03030, 0.6245 0.0706, -0.04420, 0.4078 0.1037, -0.05710, 0.2532 0.1384, -0.06890, 0.1978 0.1741, -0.07950, 0.0817 0.2102, -0.08660, -0.0939 0.2472, -0.09640, -0.1459 0.2844, -0.10270, -0.2423 0.3225, -0.10690, -0.2051 0.3608, -0.10890, -0.2627 0.3991, -0.10830, -0.1791 0.4373, -0.10510, -0.1660 0.4757, -0.09890, -0.1733 0.5137, -0.09067, 0.2647 0.5611, -0.07859, 0.4060 16 Flap element taps 1.0000, 0.00130, -1.1944 0.9365, 0.01390, -1.2794 0.8333, 0.03280, -1.3846 0.7436, 0.04930, -1.3913 0.7049, 0.05667, -1.4071 0.6662, 0.06411, -1.5189 0.6274, 0.07172, -1.5261 0.6009, 0.07523, -1.8429 0.6069, 0.02889, -1.7847 0.6079, -0.01747, -1.7583 0.6167, -0.06381, -0.4990 0.6558, -0.05300, 0.4643 0.7045, -0.04117, 0.5823 0.7429, -0.03210, 0.5457 0.8333, -0.01400, 0.7674 0.9311, -0.00120, 1.0020 --------- Run Conditions: vel=103.0 ft/s Re=0.995x10^6 AOA=9.02 Flap deflection=90.00 Totals: Cl=0.2541 Cdp=0.6475 Cm(c/4)=-0.0324 Cs=-0.5996 Ch=0.0037 Main component: Cl=0.2108 Cdp=-0.0579 Cm=-0.0053 Flap component: Cl=0.0433 Cdp=0.7054 Cm=-0.1152 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.4325 0.5905, -0.01667, 0.3975 0.5709, 0.03110, 0.4107 0.5889, 0.07933, 0.3580 0.5500, 0.08689, 0.3657 0.5110, 0.09367, 0.3653 0.4731, 0.09830, 0.3782 0.4349, 0.10070, 0.2825 0.3960, 0.10120, 0.0330 0.3566, 0.10020, -0.0044 0.3172, 0.09790, -0.1206 0.2778, 0.09440, -0.2263 0.2393, 0.08960, -0.3820 0.2056, 0.08360, -0.5478 0.1633, 0.07610, -0.5010 0.1261, 0.06710, -0.6146 0.0900, 0.05640, -0.6249 0.0571, 0.04390, -0.7338 0.0283, 0.02940, -0.8136 0.0142, 0.01970, -0.8377 0.0081, 0.01410, -0.9511 0.0026, 0.00780, -0.6470 0.0000, 0.00000, -0.1898 0.0037, -0.00840, 0.9379 0.0112, -0.01420, 0.9896 0.0191, -0.01930, 0.9336 0.0397, -0.03030, 0.7833 0.0706, -0.04420, 0.5613 0.1037, -0.05710, 0.3988 0.1384, -0.06890, 0.3459 0.1741, -0.07950, 0.2184 0.2102, -0.08660, 0.0184 0.2472, -0.09640, -0.0400 0.2844, -0.10270, -0.1554 0.3225, -0.10690, -0.1289 0.3608, -0.10890, -0.2123 0.3991, -0.10830, -0.1464 0.4373, -0.10510, -0.1235 0.4757, -0.09890, -0.1243 0.5137, -0.09067, 0.2392 0.5611, -0.07859, 0.3580 16 Flap element taps 1.0000, 0.00130, -1.1947 0.9365, 0.01390, -1.2484 0.8333, 0.03280, -1.3547 0.7436, 0.04930, -1.3224 0.7049, 0.05667, -1.3410 0.6662, 0.06411, -1.4610 0.6274, 0.07172, -1.4926 0.6009, 0.07523, -1.8363 0.6069, 0.02889, -1.7894 0.6079, -0.01747, -1.7620 0.6167, -0.06381, -0.6338 0.6558, -0.05300, 0.3390 0.7045, -0.04117, 0.4998 0.7429, -0.03210, 0.4888 0.8333, -0.01400, 0.8058 0.9311, -0.00120, 1.0024 --------- Run Conditions: vel=103.3 ft/s Re=0.998x10^6 AOA=12.05 Flap deflection=90.00 Totals: Cl=0.3188 Cdp=0.6394 Cm(c/4)=-0.0340 Cs=-0.5587 Ch=-0.0164 Main component: Cl=0.2934 Cdp=-0.0257 Cm=-0.0182 Flap component: Cl=0.0254 Cdp=0.6651 Cm=-0.1271 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.2681 0.5905, -0.01667, 0.2337 0.5709, 0.03110, 0.2388 0.5889, 0.07933, 0.2047 0.5500, 0.08689, 0.2260 0.5110, 0.09367, 0.2283 0.4731, 0.09830, 0.2557 0.4349, 0.10070, 0.2394 0.3960, 0.10120, 0.0919 0.3566, 0.10020, 0.0781 0.3172, 0.09790, -0.0781 0.2778, 0.09440, -0.2250 0.2393, 0.08960, -0.3715 0.2056, 0.08360, -0.5774 0.1633, 0.07610, -0.5680 0.1261, 0.06710, -0.7210 0.0900, 0.05640, -0.8205 0.0571, 0.04390, -1.0166 0.0283, 0.02940, -1.2303 0.0142, 0.01970, -1.3977 0.0081, 0.01410, -1.6357 0.0026, 0.00780, -1.4366 0.0000, 0.00000, -1.2210 0.0037, -0.00840, 0.7176 0.0112, -0.01420, 0.9873 0.0191, -0.01930, 0.9947 0.0397, -0.03030, 0.8949 0.0706, -0.04420, 0.6886 0.1037, -0.05710, 0.5280 0.1384, -0.06890, 0.4711 0.1741, -0.07950, 0.3372 0.2102, -0.08660, 0.1266 0.2472, -0.09640, 0.0603 0.2844, -0.10270, -0.0719 0.3225, -0.10690, -0.0596 0.3608, -0.10890, -0.1617 0.3991, -0.10830, -0.1222 0.4373, -0.10510, -0.1043 0.4757, -0.09890, -0.0812 0.5137, -0.09067, 0.0253 0.5611, -0.07859, 0.2981 16 Flap element taps 1.0000, 0.00130, -1.1605 0.9365, 0.01390, -1.1929 0.8333, 0.03280, -1.2922 0.7436, 0.04930, -1.2614 0.7049, 0.05667, -1.2532 0.6662, 0.06411, -1.3846 0.6274, 0.07172, -1.4269 0.6009, 0.07523, -1.9306 0.6069, 0.02889, -1.8684 0.6079, -0.01747, -1.7906 0.6167, -0.06381, -0.8099 0.6558, -0.05300, 0.1528 0.7045, -0.04117, 0.3908 0.7429, -0.03210, 0.4133 0.8333, -0.01400, 0.7956 0.9311, -0.00120, 1.0102 --------- Run Conditions: vel=103.1 ft/s Re=0.999x10^6 AOA=15.04 Flap deflection=90.00 Totals: Cl=0.3785 Cdp=0.6386 Cm(c/4)=-0.0388 Cs=-0.5185 Ch=-0.0306 Main component: Cl=0.3691 Cdp=0.0073 Cm=-0.0345 Flap component: Cl=0.0094 Cdp=0.6313 Cm=-0.1371 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0825 0.5905, -0.01667, 0.0715 0.5709, 0.03110, 0.0729 0.5889, 0.07933, 0.0592 0.5500, 0.08689, 0.0945 0.5110, 0.09367, 0.0788 0.4731, 0.09830, 0.0931 0.4349, 0.10070, 0.0889 0.3960, 0.10120, 0.0874 0.3566, 0.10020, 0.0582 0.3172, 0.09790, -0.0049 0.2778, 0.09440, -0.1585 0.2393, 0.08960, -0.3363 0.2056, 0.08360, -0.4977 0.1633, 0.07610, -0.6637 0.1261, 0.06710, -0.8024 0.0900, 0.05640, -0.9959 0.0571, 0.04390, -1.2200 0.0283, 0.02940, -1.6096 0.0142, 0.01970, -2.0158 0.0081, 0.01410, -2.3528 0.0026, 0.00780, -2.3317 0.0000, 0.00000, -2.4766 0.0037, -0.00840, 0.3523 0.0112, -0.01420, 0.9112 0.0191, -0.01930, 0.9915 0.0397, -0.03030, 0.9530 0.0706, -0.04420, 0.8069 0.1037, -0.05710, 0.6646 0.1384, -0.06890, 0.5027 0.1741, -0.07950, 0.3798 0.2102, -0.08660, 0.2672 0.2472, -0.09640, 0.1284 0.2844, -0.10270, 0.0386 0.3225, -0.10690, -0.0520 0.3608, -0.10890, -0.1185 0.3991, -0.10830, -0.1494 0.4373, -0.10510, -0.0986 0.4757, -0.09890, -0.0489 0.5137, -0.09067, -0.0175 0.5611, -0.07859, 0.2544 16 Flap element taps 1.0000, 0.00130, -1.1126 0.9365, 0.01390, -1.1737 0.8333, 0.03280, -1.2424 0.7436, 0.04930, -1.2535 0.7049, 0.05667, -1.2692 0.6662, 0.06411, -1.3393 0.6274, 0.07172, -1.4353 0.6009, 0.07523, -2.1014 0.6069, 0.02889, -1.9270 0.6079, -0.01747, -1.8554 0.6167, -0.06381, -1.0212 0.6558, -0.05300, -0.0283 0.7045, -0.04117, 0.2390 0.7429, -0.03210, 0.3231 0.8333, -0.01400, 0.7489 0.9311, -0.00120, 0.9907 --------- Run Conditions: vel=103.5 ft/s Re=1.004x10^6 AOA=18.00 Flap deflection=90.00 Totals: Cl=0.4000 Cdp=0.6247 Cm(c/4)=-0.0246 Cs=-0.4705 Ch=-0.0476 Main component: Cl=0.4449 Cdp=0.0491 Cm=-0.0579 Flap component: Cl=-0.0449 Cdp=0.5756 Cm=-0.1101 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.0577 0.5905, -0.01667, -0.0868 0.5709, 0.03110, -0.0890 0.5889, 0.07933, -0.0828 0.5500, 0.08689, -0.0434 0.5110, 0.09367, -0.0818 0.4731, 0.09830, -0.0821 0.4349, 0.10070, -0.0729 0.3960, 0.10120, -0.0587 0.3566, 0.10020, -0.0859 0.3172, 0.09790, -0.0884 0.2778, 0.09440, -0.1234 0.2393, 0.08960, -0.2188 0.2056, 0.08360, -0.3927 0.1633, 0.07610, -0.6266 0.1261, 0.06710, -0.8179 0.0900, 0.05640, -1.0782 0.0571, 0.04390, -1.3976 0.0283, 0.02940, -1.8931 0.0142, 0.01970, -2.4188 0.0081, 0.01410, -3.1876 0.0026, 0.00780, -3.2093 0.0000, 0.00000, -3.7245 0.0037, -0.00840, -0.0784 0.0112, -0.01420, 0.7684 0.0191, -0.01930, 0.9442 0.0397, -0.03030, 0.9819 0.0706, -0.04420, 0.8758 0.1037, -0.05710, 0.7502 0.1384, -0.06890, 0.5828 0.1741, -0.07950, 0.4619 0.2102, -0.08660, 0.3559 0.2472, -0.09640, 0.2077 0.2844, -0.10270, 0.1129 0.3225, -0.10690, 0.0048 0.3608, -0.10890, -0.0685 0.3991, -0.10830, -0.1213 0.4373, -0.10510, -0.0883 0.4757, -0.09890, -0.0355 0.5137, -0.09067, 0.0093 0.5611, -0.07859, 0.2326 16 Flap element taps 1.0000, 0.00130, -1.0948 0.9365, 0.01390, -1.1390 0.8333, 0.03280, -1.1888 0.7436, 0.04930, -1.2081 0.7049, 0.05667, -1.2073 0.6662, 0.06411, -1.2414 0.6274, 0.07172, -1.3070 0.6009, 0.07523, -1.7152 0.6069, 0.02889, -1.6323 0.6079, -0.01747, -1.5468 0.6167, -0.06381, -0.9988 0.6558, -0.05300, -0.1681 0.7045, -0.04117, 0.1141 0.7429, -0.03210, 0.2206 0.8333, -0.01400, 0.6958 0.9311, -0.00120, 0.9834 --------- Run Conditions: vel=104.0 ft/s Re=1.008x10^6 AOA=20.00 Flap deflection=90.00 Totals: Cl=0.4199 Cdp=0.6186 Cm(c/4)=-0.0250 Cs=-0.4377 Ch=-0.0616 Main component: Cl=0.4838 Cdp=0.0898 Cm=-0.0753 Flap component: Cl=-0.0639 Cdp=0.5289 Cm=-0.1013 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1545 0.5905, -0.01667, -0.2087 0.5709, 0.03110, -0.2119 0.5889, 0.07933, -0.2120 0.5500, 0.08689, -0.1447 0.5110, 0.09367, -0.2130 0.4731, 0.09830, -0.2214 0.4349, 0.10070, -0.2047 0.3960, 0.10120, -0.1829 0.3566, 0.10020, -0.1998 0.3172, 0.09790, -0.1972 0.2778, 0.09440, -0.2069 0.2393, 0.08960, -0.2208 0.2056, 0.08360, -0.2897 0.1633, 0.07610, -0.5000 0.1261, 0.06710, -0.7351 0.0900, 0.05640, -1.0424 0.0571, 0.04390, -1.4218 0.0283, 0.02940, -2.0071 0.0142, 0.01970, -2.5574 0.0081, 0.01410, -3.6315 0.0026, 0.00780, -3.6971 0.0000, 0.00000, -4.4246 0.0037, -0.00840, -0.3463 0.0112, -0.01420, 0.6712 0.0191, -0.01930, 0.9082 0.0397, -0.03030, 0.9958 0.0706, -0.04420, 0.9156 0.1037, -0.05710, 0.8015 0.1384, -0.06890, 0.6383 0.1741, -0.07950, 0.5188 0.2102, -0.08660, 0.4105 0.2472, -0.09640, 0.2622 0.2844, -0.10270, 0.1637 0.3225, -0.10690, 0.0514 0.3608, -0.10890, -0.0329 0.3991, -0.10830, -0.0960 0.4373, -0.10510, -0.0767 0.4757, -0.09890, -0.0342 0.5137, -0.09067, 0.0222 0.5611, -0.07859, 0.1734 16 Flap element taps 1.0000, 0.00130, -1.0550 0.9365, 0.01390, -1.0903 0.8333, 0.03280, -1.1240 0.7436, 0.04930, -1.1333 0.7049, 0.05667, -1.1341 0.6662, 0.06411, -1.1549 0.6274, 0.07172, -1.1977 0.6009, 0.07523, -1.5446 0.6069, 0.02889, -1.5017 0.6079, -0.01747, -1.4157 0.6167, -0.06381, -1.0144 0.6558, -0.05300, -0.2754 0.7045, -0.04117, 0.0280 0.7429, -0.03210, 0.1436 0.8333, -0.01400, 0.6582 0.9311, -0.00120, 0.9866 --------- Run Conditions: vel=102.2 ft/s Re=0.992x10^6 AOA=24.01 Flap deflection=90.00 Totals: Cl=0.3652 Cdp=0.7863 Cm(c/4)=-0.0566 Cs=-0.5697 Ch=-0.0940 Main component: Cl=0.4628 Cdp=0.3348 Cm=-0.1339 Flap component: Cl=-0.0976 Cdp=0.4515 Cm=-0.0861 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.6035 0.5905, -0.01667, -0.7386 0.5709, 0.03110, -0.7412 0.5889, 0.07933, -0.7513 0.5500, 0.08689, -0.6585 0.5110, 0.09367, -0.6455 0.4731, 0.09830, -0.6743 0.4349, 0.10070, -0.7284 0.3960, 0.10120, -0.7656 0.3566, 0.10020, -0.7671 0.3172, 0.09790, -0.7449 0.2778, 0.09440, -0.7336 0.2393, 0.08960, -0.7168 0.2056, 0.08360, -0.7077 0.1633, 0.07610, -0.7070 0.1261, 0.06710, -0.6966 0.0900, 0.05640, -0.6907 0.0571, 0.04390, -0.6882 0.0283, 0.02940, -0.7038 0.0142, 0.01970, -0.7001 0.0081, 0.01410, -0.7047 0.0026, 0.00780, -0.6705 0.0000, 0.00000, -0.9438 0.0037, -0.00840, 0.4119 0.0112, -0.01420, 0.8774 0.0191, -0.01930, 0.9774 0.0397, -0.03030, 0.9906 0.0706, -0.04420, 0.8923 0.1037, -0.05710, 0.7790 0.1384, -0.06890, 0.6346 0.1741, -0.07950, 0.5142 0.2102, -0.08660, 0.3893 0.2472, -0.09640, 0.2419 0.2844, -0.10270, 0.1267 0.3225, -0.10690, 0.0161 0.3608, -0.10890, -0.0943 0.3991, -0.10830, -0.1719 0.4373, -0.10510, -0.1809 0.4757, -0.09890, -0.1635 0.5137, -0.09067, -0.0930 0.5611, -0.07859, -0.0460 16 Flap element taps 1.0000, 0.00130, -1.0690 0.9365, 0.01390, -1.1105 0.8333, 0.03280, -1.1482 0.7436, 0.04930, -1.1811 0.7049, 0.05667, -1.1787 0.6662, 0.06411, -1.1968 0.6274, 0.07172, -1.2299 0.6009, 0.07523, -1.4485 0.6069, 0.02889, -1.3910 0.6079, -0.01747, -1.3268 0.6167, -0.06381, -1.2006 0.6558, -0.05300, -0.7080 0.7045, -0.04117, -0.3382 0.7429, -0.03210, -0.1963 0.8333, -0.01400, 0.4853 0.9311, -0.00120, 0.9817 --------- Run Conditions: vel=102.4 ft/s Re=0.994x10^6 AOA=27.00 Flap deflection=90.00 Totals: Cl=0.3991 Cdp=0.8760 Cm(c/4)=-0.0630 Cs=-0.5994 Ch=-0.0965 Main component: Cl=0.5239 Cdp=0.4175 Cm=-0.1631 Flap component: Cl=-0.1249 Cdp=0.4585 Cm=-0.0882 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.7218 0.5905, -0.01667, -0.8863 0.5709, 0.03110, -0.8917 0.5889, 0.07933, -0.9059 0.5500, 0.08689, -0.8154 0.5110, 0.09367, -0.7969 0.4731, 0.09830, -0.7937 0.4349, 0.10070, -0.8258 0.3960, 0.10120, -0.8873 0.3566, 0.10020, -0.8803 0.3172, 0.09790, -0.8709 0.2778, 0.09440, -0.8571 0.2393, 0.08960, -0.8416 0.2056, 0.08360, -0.8505 0.1633, 0.07610, -0.8184 0.1261, 0.06710, -0.8200 0.0900, 0.05640, -0.8031 0.0571, 0.04390, -0.8060 0.0283, 0.02940, -0.8166 0.0142, 0.01970, -0.8112 0.0081, 0.01410, -0.8371 0.0026, 0.00780, -0.7776 0.0000, 0.00000, -0.8714 0.0037, -0.00840, 0.2168 0.0112, -0.01420, 0.7843 0.0191, -0.01930, 0.9361 0.0397, -0.03030, 1.0035 0.0706, -0.04420, 0.9317 0.1037, -0.05710, 0.8357 0.1384, -0.06890, 0.7240 0.1741, -0.07950, 0.6028 0.2102, -0.08660, 0.4592 0.2472, -0.09640, 0.3239 0.2844, -0.10270, 0.1981 0.3225, -0.10690, 0.0997 0.3608, -0.10890, -0.0347 0.3991, -0.10830, -0.1131 0.4373, -0.10510, -0.1513 0.4757, -0.09890, -0.1532 0.5137, -0.09067, -0.0880 0.5611, -0.07859, -0.0662 16 Flap element taps 1.0000, 0.00130, -1.1473 0.9365, 0.01390, -1.1864 0.8333, 0.03280, -1.2474 0.7436, 0.04930, -1.2849 0.7049, 0.05667, -1.2894 0.6662, 0.06411, -1.3130 0.6274, 0.07172, -1.3547 0.6009, 0.07523, -1.6392 0.6069, 0.02889, -1.4932 0.6079, -0.01747, -1.4114 0.6167, -0.06381, -1.2754 0.6558, -0.05300, -0.8192 0.7045, -0.04117, -0.4359 0.7429, -0.03210, -0.2956 0.8333, -0.01400, 0.4281 0.9311, -0.00120, 0.9740 --------- Run Conditions: vel=103.0 ft/s Re=0.998x10^6 AOA=30.02 Flap deflection=90.00 Totals: Cl=0.4765 Cdp=0.8536 Cm(c/4)=-0.0625 Cs=-0.5007 Ch=-0.1051 Main component: Cl=0.5913 Cdp=0.5049 Cm=-0.1993 Flap component: Cl=-0.1148 Cdp=0.3487 Cm=-0.0732 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.7732 0.5905, -0.01667, -0.9750 0.5709, 0.03110, -0.9918 0.5889, 0.07933, -0.9977 0.5500, 0.08689, -0.9860 0.5110, 0.09367, -0.9899 0.4731, 0.09830, -0.9406 0.4349, 0.10070, -0.9282 0.3960, 0.10120, -0.9506 0.3566, 0.10020, -0.9626 0.3172, 0.09790, -0.9621 0.2778, 0.09440, -0.9537 0.2393, 0.08960, -0.9379 0.2056, 0.08360, -0.9438 0.1633, 0.07610, -0.9214 0.1261, 0.06710, -0.9157 0.0900, 0.05640, -0.9015 0.0571, 0.04390, -0.8990 0.0283, 0.02940, -0.9011 0.0142, 0.01970, -0.9010 0.0081, 0.01410, -0.9168 0.0026, 0.00780, -0.8608 0.0000, 0.00000, -0.9256 0.0037, -0.00840, -0.0142 0.0112, -0.01420, 0.6518 0.0191, -0.01930, 0.8677 0.0397, -0.03030, 0.9975 0.0706, -0.04420, 0.9731 0.1037, -0.05710, 0.9017 0.1384, -0.06890, 0.8043 0.1741, -0.07950, 0.6962 0.2102, -0.08660, 0.5701 0.2472, -0.09640, 0.4438 0.2844, -0.10270, 0.3184 0.3225, -0.10690, 0.2134 0.3608, -0.10890, 0.0824 0.3991, -0.10830, 0.0039 0.4373, -0.10510, -0.0496 0.4757, -0.09890, -0.0637 0.5137, -0.09067, -0.0091 0.5611, -0.07859, -0.0262 16 Flap element taps 1.0000, 0.00130, -0.9090 0.9365, 0.01390, -0.9143 0.8333, 0.03280, -0.9466 0.7436, 0.04930, -0.9549 0.7049, 0.05667, -0.9530 0.6662, 0.06411, -0.9712 0.6274, 0.07172, -0.9811 0.6009, 0.07523, -1.1994 0.6069, 0.02889, -1.1615 0.6079, -0.01747, -1.0823 0.6167, -0.06381, -1.0196 0.6558, -0.05300, -0.7539 0.7045, -0.04117, -0.4109 0.7429, -0.03210, -0.3240 0.8333, -0.01400, 0.4014 0.9311, -0.00120, 0.9842 --------- Run Conditions: vel=101.3 ft/s Re=0.981x10^6 AOA=34.99 Flap deflection=90.00 Totals: Cl=0.4972 Cdp=0.9449 Cm(c/4)=-0.0663 Cs=-0.4890 Ch=-0.1091 Main component: Cl=0.6368 Cdp=0.6361 Cm=-0.2394 Flap component: Cl=-0.1396 Cdp=0.3088 Cm=-0.0642 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.8940 0.5905, -0.01667, -1.1374 0.5709, 0.03110, -1.1651 0.5889, 0.07933, -1.1781 0.5500, 0.08689, -1.1429 0.5110, 0.09367, -1.1516 0.4731, 0.09830, -1.1125 0.4349, 0.10070, -1.0933 0.3960, 0.10120, -1.1062 0.3566, 0.10020, -1.1050 0.3172, 0.09790, -1.0992 0.2778, 0.09440, -1.0867 0.2393, 0.08960, -1.0713 0.2056, 0.08360, -1.0845 0.1633, 0.07610, -1.0566 0.1261, 0.06710, -1.0461 0.0900, 0.05640, -1.0227 0.0571, 0.04390, -1.0116 0.0283, 0.02940, -1.0122 0.0142, 0.01970, -1.0066 0.0081, 0.01410, -1.0260 0.0026, 0.00780, -0.9634 0.0000, 0.00000, -1.0205 0.0037, -0.00840, -0.3391 0.0112, -0.01420, 0.4447 0.0191, -0.01930, 0.7350 0.0397, -0.03030, 0.9587 0.0706, -0.04420, 0.9937 0.1037, -0.05710, 0.9590 0.1384, -0.06890, 0.8904 0.1741, -0.07950, 0.8001 0.2102, -0.08660, 0.6825 0.2472, -0.09640, 0.5688 0.2844, -0.10270, 0.4445 0.3225, -0.10690, 0.3439 0.3608, -0.10890, 0.2045 0.3991, -0.10830, 0.1160 0.4373, -0.10510, 0.0399 0.4757, -0.09890, 0.0040 0.5137, -0.09067, 0.0350 0.5611, -0.07859, -0.0197 16 Flap element taps 1.0000, 0.00130, -0.8959 0.9365, 0.01390, -0.8935 0.8333, 0.03280, -0.9241 0.7436, 0.04930, -0.9349 0.7049, 0.05667, -0.9295 0.6662, 0.06411, -0.9511 0.6274, 0.07172, -0.9611 0.6009, 0.07523, -1.0858 0.6069, 0.02889, -1.0714 0.6079, -0.01747, -1.0211 0.6167, -0.06381, -0.9863 0.6558, -0.05300, -0.8131 0.7045, -0.04117, -0.4968 0.7429, -0.03210, -0.4059 0.8333, -0.01400, 0.3386 0.9311, -0.00120, 0.9658 --------- Run Conditions: vel=101.9 ft/s Re=0.985x10^6 AOA=39.97 Flap deflection=90.00 Totals: Cl=0.5116 Cdp=1.0544 Cm(c/4)=-0.0748 Cs=-0.4794 Ch=-0.1152 Main component: Cl=0.6735 Cdp=0.7698 Cm=-0.2800 Flap component: Cl=-0.1619 Cdp=0.2846 Cm=-0.0621 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.9851 0.5905, -0.01667, -1.2656 0.5709, 0.03110, -1.2904 0.5889, 0.07933, -1.3025 0.5500, 0.08689, -1.2949 0.5110, 0.09367, -1.2971 0.4731, 0.09830, -1.2778 0.4349, 0.10070, -1.2668 0.3960, 0.10120, -1.2854 0.3566, 0.10020, -1.2718 0.3172, 0.09790, -1.2582 0.2778, 0.09440, -1.2448 0.2393, 0.08960, -1.2284 0.2056, 0.08360, -1.2492 0.1633, 0.07610, -1.2208 0.1261, 0.06710, -1.2115 0.0900, 0.05640, -1.1783 0.0571, 0.04390, -1.1645 0.0283, 0.02940, -1.1577 0.0142, 0.01970, -1.1528 0.0081, 0.01410, -1.1742 0.0026, 0.00780, -1.0995 0.0000, 0.00000, -1.1527 0.0037, -0.00840, -0.6868 0.0112, -0.01420, 0.1924 0.0191, -0.01930, 0.5586 0.0397, -0.03030, 0.8781 0.0706, -0.04420, 0.9784 0.1037, -0.05710, 0.9861 0.1384, -0.06890, 0.9526 0.1741, -0.07950, 0.8811 0.2102, -0.08660, 0.7760 0.2472, -0.09640, 0.6775 0.2844, -0.10270, 0.5596 0.3225, -0.10690, 0.4631 0.3608, -0.10890, 0.3204 0.3991, -0.10830, 0.2238 0.4373, -0.10510, 0.1295 0.4757, -0.09890, 0.0715 0.5137, -0.09067, 0.0848 0.5611, -0.07859, -0.0085 16 Flap element taps 1.0000, 0.00130, -0.9280 0.9365, 0.01390, -0.9243 0.8333, 0.03280, -0.9540 0.7436, 0.04930, -0.9614 0.7049, 0.05667, -0.9560 0.6662, 0.06411, -0.9740 0.6274, 0.07172, -0.9794 0.6009, 0.07523, -1.0888 0.6069, 0.02889, -1.0883 0.6079, -0.01747, -1.0367 0.6167, -0.06381, -1.0150 0.6558, -0.05300, -0.8972 0.7045, -0.04117, -0.5735 0.7429, -0.03210, -0.4981 0.8333, -0.01400, 0.2788 0.9311, -0.00120, 0.9520 --------- Run Conditions: vel=101.8 ft/s Re=0.985x10^6 AOA=44.98 Flap deflection=90.00 Totals: Cl=0.4778 Cdp=1.1407 Cm(c/4)=-0.0803 Cs=-0.4691 Ch=-0.1180 Main component: Cl=0.6597 Cdp=0.8834 Cm=-0.3081 Flap component: Cl=-0.1818 Cdp=0.2572 Cm=-0.0583 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -1.0427 0.5905, -0.01667, -1.3635 0.5709, 0.03110, -1.3893 0.5889, 0.07933, -1.4149 0.5500, 0.08689, -1.3709 0.5110, 0.09367, -1.3888 0.4731, 0.09830, -1.3762 0.4349, 0.10070, -1.3548 0.3960, 0.10120, -1.3587 0.3566, 0.10020, -1.3389 0.3172, 0.09790, -1.3350 0.2778, 0.09440, -1.3350 0.2393, 0.08960, -1.3259 0.2056, 0.08360, -1.3436 0.1633, 0.07610, -1.3100 0.1261, 0.06710, -1.3024 0.0900, 0.05640, -1.2688 0.0571, 0.04390, -1.2627 0.0283, 0.02940, -1.2507 0.0142, 0.01970, -1.2435 0.0081, 0.01410, -1.2684 0.0026, 0.00780, -1.1857 0.0000, 0.00000, -1.2393 0.0037, -0.00840, -0.9755 0.0112, -0.01420, -0.0438 0.0191, -0.01930, 0.3816 0.0397, -0.03030, 0.7860 0.0706, -0.04420, 0.9484 0.1037, -0.05710, 0.9936 0.1384, -0.06890, 0.9933 0.1741, -0.07950, 0.9462 0.2102, -0.08660, 0.8554 0.2472, -0.09640, 0.7756 0.2844, -0.10270, 0.6637 0.3225, -0.10690, 0.5744 0.3608, -0.10890, 0.4329 0.3991, -0.10830, 0.3346 0.4373, -0.10510, 0.2241 0.4757, -0.09890, 0.1486 0.5137, -0.09067, 0.1459 0.5611, -0.07859, 0.0229 16 Flap element taps 1.0000, 0.00130, -0.9388 0.9365, 0.01390, -0.9337 0.8333, 0.03280, -0.9600 0.7436, 0.04930, -0.9641 0.7049, 0.05667, -0.9581 0.6662, 0.06411, -0.9792 0.6274, 0.07172, -0.9822 0.6009, 0.07523, -1.0827 0.6069, 0.02889, -1.0593 0.6079, -0.01747, -1.0149 0.6167, -0.06381, -1.0180 0.6558, -0.05300, -0.9399 0.7045, -0.04117, -0.6302 0.7429, -0.03210, -0.5540 0.8333, -0.01400, 0.2331 0.9311, -0.00120, 0.9362 --------- Run Conditions: vel=105.2 ft/s Re=1.010x10^6 AOA=60.00 Flap deflection=90.00 Totals: Cl=0.1570 Cdp=1.3043 Cm(c/4)=-0.0982 Cs=-0.5162 Ch=-0.1177 Main component: Cl=0.4597 Cdp=1.0636 Cm=-0.3397 Flap component: Cl=-0.3027 Cdp=0.2406 Cm=-0.0606 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -1.0148 0.5905, -0.01667, -1.3982 0.5709, 0.03110, -1.4067 0.5889, 0.07933, -1.4117 0.5500, 0.08689, -1.3529 0.5110, 0.09367, -1.3655 0.4731, 0.09830, -1.3485 0.4349, 0.10070, -1.3456 0.3960, 0.10120, -1.3391 0.3566, 0.10020, -1.3379 0.3172, 0.09790, -1.3304 0.2778, 0.09440, -1.3364 0.2393, 0.08960, -1.3214 0.2056, 0.08360, -1.3237 0.1633, 0.07610, -1.3256 0.1261, 0.06710, -1.3325 0.0900, 0.05640, -1.3219 0.0571, 0.04390, -1.3199 0.0283, 0.02940, -1.3124 0.0142, 0.01970, -1.3214 0.0081, 0.01410, -1.3216 0.0026, 0.00780, -1.2640 0.0000, 0.00000, -1.3251 0.0037, -0.00840, -1.4264 0.0112, -0.01420, -0.6358 0.0191, -0.01930, -0.1379 0.0397, -0.03030, 0.4284 0.0706, -0.04420, 0.7473 0.1037, -0.05710, 0.9018 0.1384, -0.06890, 0.9694 0.1741, -0.07950, 0.9923 0.2102, -0.08660, 0.9893 0.2472, -0.09640, 0.9585 0.2844, -0.10270, 0.9007 0.3225, -0.10690, 0.8269 0.3608, -0.10890, 0.7272 0.3991, -0.10830, 0.6188 0.4373, -0.10510, 0.5049 0.4757, -0.09890, 0.4006 0.5137, -0.09067, 0.3444 0.5611, -0.07859, 0.1680 16 Flap element taps 1.0000, 0.00130, -1.1879 0.9365, 0.01390, -1.1957 0.8333, 0.03280, -1.2069 0.7436, 0.04930, -1.2181 0.7049, 0.05667, -1.2300 0.6662, 0.06411, -1.2429 0.6274, 0.07172, -1.2544 0.6009, 0.07523, -1.3073 0.6069, 0.02889, -1.2290 0.6079, -0.01747, -1.2141 0.6167, -0.06381, -1.2329 0.6558, -0.05300, -1.0413 0.7045, -0.04117, -0.6880 0.7429, -0.03210, -0.5903 0.8333, -0.01400, 0.1981 0.9311, -0.00120, 0.9133 --------- Run Conditions: vel=107.1 ft/s Re=1.026x10^6 AOA=70.02 Flap deflection=90.00 Totals: Cl=-0.0260 Cdp=1.3132 Cm(c/4)=-0.1088 Cs=-0.4732 Ch=-0.1152 Main component: Cl=0.2937 Cdp=1.1424 Cm=-0.3593 Flap component: Cl=-0.3198 Cdp=0.1708 Cm=-0.0558 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.9702 0.5905, -0.01667, -1.4123 0.5709, 0.03110, -1.4237 0.5889, 0.07933, -1.4257 0.5500, 0.08689, -1.3594 0.5110, 0.09367, -1.3702 0.4731, 0.09830, -1.3627 0.4349, 0.10070, -1.3651 0.3960, 0.10120, -1.3647 0.3566, 0.10020, -1.3630 0.3172, 0.09790, -1.3499 0.2778, 0.09440, -1.3519 0.2393, 0.08960, -1.3342 0.2056, 0.08360, -1.3353 0.1633, 0.07610, -1.3362 0.1261, 0.06710, -1.3368 0.0900, 0.05640, -1.3288 0.0571, 0.04390, -1.3296 0.0283, 0.02940, -1.3213 0.0142, 0.01970, -1.3298 0.0081, 0.01410, -1.3281 0.0026, 0.00780, -1.2688 0.0000, 0.00000, -1.3309 0.0037, -0.00840, -1.4965 0.0112, -0.01420, -0.9497 0.0191, -0.01930, -0.4651 0.0397, -0.03030, 0.1449 0.0706, -0.04420, 0.5327 0.1037, -0.05710, 0.7453 0.1384, -0.06890, 0.8692 0.1741, -0.07950, 0.9426 0.2102, -0.08660, 0.9860 0.2472, -0.09640, 0.9977 0.2844, -0.10270, 0.9813 0.3225, -0.10690, 0.9436 0.3608, -0.10890, 0.8752 0.3991, -0.10830, 0.7892 0.4373, -0.10510, 0.6848 0.4757, -0.09890, 0.5745 0.5137, -0.09067, 0.4952 0.5611, -0.07859, 0.2912 16 Flap element taps 1.0000, 0.00130, -1.1485 0.9365, 0.01390, -1.1508 0.8333, 0.03280, -1.1608 0.7436, 0.04930, -1.1700 0.7049, 0.05667, -1.1762 0.6662, 0.06411, -1.1862 0.6274, 0.07172, -1.2005 0.6009, 0.07523, -1.2324 0.6069, 0.02889, -1.1603 0.6079, -0.01747, -1.1525 0.6167, -0.06381, -1.1890 0.6558, -0.05300, -1.0238 0.7045, -0.04117, -0.6882 0.7429, -0.03210, -0.5982 0.8333, -0.01400, 0.1554 0.9311, -0.00120, 0.8720 --------- Run Conditions: vel=106.0 ft/s Re=1.016x10^6 AOA=80.00 Flap deflection=90.00 Totals: Cl=-0.2129 Cdp=1.2595 Cm(c/4)=-0.1156 Cs=-0.4284 Ch=-0.1078 Main component: Cl=0.1112 Cdp=1.1576 Cm=-0.3673 Flap component: Cl=-0.3241 Cdp=0.1019 Cm=-0.0491 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.8871 0.5905, -0.01667, -1.3894 0.5709, 0.03110, -1.4082 0.5889, 0.07933, -1.4106 0.5500, 0.08689, -1.3348 0.5110, 0.09367, -1.3511 0.4731, 0.09830, -1.3400 0.4349, 0.10070, -1.3465 0.3960, 0.10120, -1.3463 0.3566, 0.10020, -1.3515 0.3172, 0.09790, -1.3409 0.2778, 0.09440, -1.3446 0.2393, 0.08960, -1.3210 0.2056, 0.08360, -1.3130 0.1633, 0.07610, -1.3159 0.1261, 0.06710, -1.3147 0.0900, 0.05640, -1.3056 0.0571, 0.04390, -1.3053 0.0283, 0.02940, -1.2967 0.0142, 0.01970, -1.3008 0.0081, 0.01410, -1.3000 0.0026, 0.00780, -1.2457 0.0000, 0.00000, -1.3055 0.0037, -0.00840, -1.3801 0.0112, -0.01420, -1.1594 0.0191, -0.01930, -0.7302 0.0397, -0.03030, -0.1267 0.0706, -0.04420, 0.2955 0.1037, -0.05710, 0.5466 0.1384, -0.06890, 0.7125 0.1741, -0.07950, 0.8307 0.2102, -0.08660, 0.9160 0.2472, -0.09640, 0.9712 0.2844, -0.10270, 0.9956 0.3225, -0.10690, 0.9966 0.3608, -0.10890, 0.9669 0.3991, -0.10830, 0.9120 0.4373, -0.10510, 0.8286 0.4757, -0.09890, 0.7277 0.5137, -0.09067, 0.6395 0.5611, -0.07859, 0.4217 16 Flap element taps 1.0000, 0.00130, -1.0865 0.9365, 0.01390, -1.0889 0.8333, 0.03280, -1.0978 0.7436, 0.04930, -1.1072 0.7049, 0.05667, -1.1140 0.6662, 0.06411, -1.1259 0.6274, 0.07172, -1.1427 0.6009, 0.07523, -1.1581 0.6069, 0.02889, -1.0667 0.6079, -0.01747, -1.0566 0.6167, -0.06381, -1.0989 0.6558, -0.05300, -0.9702 0.7045, -0.04117, -0.6566 0.7429, -0.03210, -0.5826 0.8333, -0.01400, 0.1225 0.9311, -0.00120, 0.8231 --------- Run Conditions: vel=108.7 ft/s Re=1.041x10^6 AOA=90.04 Flap deflection=90.00 Totals: Cl=-0.6215 Cdp=0.9884 Cm(c/4)=-0.1149 Cs=-0.6208 Ch=-0.0806 Main component: Cl=-0.0583 Cdp=0.9186 Cm=-0.2987 Flap component: Cl=-0.5632 Cdp=0.0698 Cm=-0.0634 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.5301 0.5905, -0.01667, -0.9569 0.5709, 0.03110, -0.9644 0.5889, 0.07933, -0.9652 0.5500, 0.08689, -0.9038 0.5110, 0.09367, -0.9147 0.4731, 0.09830, -0.9035 0.4349, 0.10070, -0.9045 0.3960, 0.10120, -0.9025 0.3566, 0.10020, -0.9148 0.3172, 0.09790, -0.9088 0.2778, 0.09440, -0.9150 0.2393, 0.08960, -0.9019 0.2056, 0.08360, -0.8979 0.1633, 0.07610, -0.9037 0.1261, 0.06710, -0.9014 0.0900, 0.05640, -0.8947 0.0571, 0.04390, -0.8916 0.0283, 0.02940, -0.8851 0.0142, 0.01970, -0.8919 0.0081, 0.01410, -0.8890 0.0026, 0.00780, -0.8581 0.0000, 0.00000, -0.8995 0.0037, -0.00840, -0.9130 0.0112, -0.01420, -0.9060 0.0191, -0.01930, -0.6170 0.0397, -0.03030, -0.1433 0.0706, -0.04420, 0.2210 0.1037, -0.05710, 0.4520 0.1384, -0.06890, 0.6136 0.1741, -0.07950, 0.7395 0.2102, -0.08660, 0.8463 0.2472, -0.09640, 0.9176 0.2844, -0.10270, 0.9685 0.3225, -0.10690, 0.9918 0.3608, -0.10890, 0.9927 0.3991, -0.10830, 0.9633 0.4373, -0.10510, 0.9064 0.4757, -0.09890, 0.8290 0.5137, -0.09067, 0.7489 0.5611, -0.07859, 0.5610 16 Flap element taps 1.0000, 0.00130, -1.5936 0.9365, 0.01390, -1.5961 0.8333, 0.03280, -1.6168 0.7436, 0.04930, -1.6380 0.7049, 0.05667, -1.6450 0.6662, 0.06411, -1.6627 0.6274, 0.07172, -1.7416 0.6009, 0.07523, -1.8037 0.6069, 0.02889, -1.4701 0.6079, -0.01747, -1.4550 0.6167, -0.06381, -1.3754 0.6558, -0.05300, -0.8594 0.7045, -0.04117, -0.4580 0.7429, -0.03210, -0.3470 0.8333, -0.01400, 0.2627 0.9311, -0.00120, 0.8441 --------- Run Conditions: vel=107.4 ft/s Re=1.028x10^6 AOA=120.02 Flap deflection=90.00 Totals: Cl=-0.3480 Cdp=0.9997 Cm(c/4)=-0.2233 Cs=0.1988 Ch=-0.0045 Main component: Cl=-0.3960 Cdp=0.7180 Cm=-0.3047 Flap component: Cl=0.0479 Cdp=0.2817 Cm=-0.1785 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3706 0.5905, -0.01667, -1.2086 0.5709, 0.03110, -1.2210 0.5889, 0.07933, -1.2233 0.5500, 0.08689, -1.1103 0.5110, 0.09367, -1.1273 0.4731, 0.09830, -1.1185 0.4349, 0.10070, -1.1248 0.3960, 0.10120, -1.1229 0.3566, 0.10020, -1.1454 0.3172, 0.09790, -1.1396 0.2778, 0.09440, -1.1467 0.2393, 0.08960, -1.1306 0.2056, 0.08360, -1.1179 0.1633, 0.07610, -1.1267 0.1261, 0.06710, -1.1156 0.0900, 0.05640, -1.1069 0.0571, 0.04390, -1.0980 0.0283, 0.02940, -1.0886 0.0142, 0.01970, -1.0914 0.0081, 0.01410, -1.0826 0.0026, 0.00780, -1.0471 0.0000, 0.00000, -1.0976 0.0037, -0.00840, -1.0886 0.0112, -0.01420, -1.1325 0.0191, -0.01930, -1.1727 0.0397, -0.03030, -0.9463 0.0706, -0.04420, -0.6681 0.1037, -0.05710, -0.4562 0.1384, -0.06890, -0.2746 0.1741, -0.07950, -0.1007 0.2102, -0.08660, 0.0739 0.2472, -0.09640, 0.2135 0.2844, -0.10270, 0.3760 0.3225, -0.10690, 0.5191 0.3608, -0.10890, 0.6689 0.3991, -0.10830, 0.7966 0.4373, -0.10510, 0.9068 0.4757, -0.09890, 0.9769 0.5137, -0.09067, 1.0033 0.5611, -0.07859, 0.9053 16 Flap element taps 1.0000, 0.00130, 0.6112 0.9365, 0.01390, 0.5424 0.8333, 0.03280, 0.2017 0.7436, 0.04930, -0.1143 0.7049, 0.05667, -0.2099 0.6662, 0.06411, -0.4748 0.6274, 0.07172, -0.8720 0.6009, 0.07523, -1.8503 0.6069, 0.02889, -1.8748 0.6079, -0.01747, -1.8783 0.6167, -0.06381, -1.7446 0.6558, -0.05300, -1.1219 0.7045, -0.04117, -0.6881 0.7429, -0.03210, -0.5703 0.8333, -0.01400, 0.0183 0.9311, -0.00120, -0.3475 --------- Run Conditions: vel=105.7 ft/s Re=1.011x10^6 AOA=150.00 Flap deflection=90.00 Totals: Cl=-0.0013 Cdp=0.7345 Cm(c/4)=-0.1344 Cs=0.6355 Ch=-0.0168 Main component: Cl=-0.1796 Cdp=0.1479 Cm=-0.1067 Flap component: Cl=0.1784 Cdp=0.5866 Cm=-0.1197 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -1.1503 0.5905, -0.01667, -1.1312 0.5709, 0.03110, -1.1380 0.5889, 0.07933, -1.1556 0.5500, 0.08689, -1.1061 0.5110, 0.09367, -1.1154 0.4731, 0.09830, -1.1147 0.4349, 0.10070, -1.1157 0.3960, 0.10120, -1.1226 0.3566, 0.10020, -1.1219 0.3172, 0.09790, -1.1144 0.2778, 0.09440, -1.1291 0.2393, 0.08960, -1.1260 0.2056, 0.08360, -1.1281 0.1633, 0.07610, -1.1403 0.1261, 0.06710, -1.1298 0.0900, 0.05640, -1.1357 0.0571, 0.04390, -1.1418 0.0283, 0.02940, -1.1367 0.0142, 0.01970, -1.1269 0.0081, 0.01410, -1.1270 0.0026, 0.00780, -1.0528 0.0000, 0.00000, -1.1126 0.0037, -0.00840, -1.2372 0.0112, -0.01420, -1.6229 0.0191, -0.01930, -1.6925 0.0397, -0.03030, -1.6006 0.0706, -0.04420, -1.4648 0.1037, -0.05710, -1.3642 0.1384, -0.06890, -1.2550 0.1741, -0.07950, -1.1464 0.2102, -0.08660, -1.0105 0.2472, -0.09640, -0.8930 0.2844, -0.10270, -0.6838 0.3225, -0.10690, -0.4340 0.3608, -0.10890, -0.1181 0.3991, -0.10830, 0.2428 0.4373, -0.10510, 0.4187 0.4757, -0.09890, 0.0522 0.5137, -0.09067, -0.6120 0.5611, -0.07859, -0.9907 16 Flap element taps 1.0000, 0.00130, -0.7977 0.9365, 0.01390, 0.9842 0.8333, 0.03280, 0.9401 0.7436, 0.04930, 0.7405 0.7049, 0.05667, 0.6309 0.6662, 0.06411, 0.4171 0.6274, 0.07172, 0.0531 0.6009, 0.07523, -1.1305 0.6069, 0.02889, -1.1504 0.6079, -0.01747, -1.1748 0.6167, -0.06381, -1.1410 0.6558, -0.05300, -1.0998 0.7045, -0.04117, -1.0612 0.7429, -0.03210, -1.0609 0.8333, -0.01400, -0.7722 0.9311, -0.00120, -0.8580 --------- Run Conditions: vel=106.2 ft/s Re=1.015x10^6 AOA=180.04 Flap deflection=90.00 Totals: Cl=-0.1906 Cdp=0.7195 Cm(c/4)=-0.0971 Cs=0.7196 Ch=-0.0711 Main component: Cl=-0.0518 Cdp=-0.0391 Cm=-0.0151 Flap component: Cl=-0.1388 Cdp=0.7586 Cm=-0.1296 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -1.6028 0.5905, -0.01667, -1.6255 0.5709, 0.03110, -1.5831 0.5889, 0.07933, -1.6476 0.5500, 0.08689, -1.4714 0.5110, 0.09367, -1.4999 0.4731, 0.09830, -1.5555 0.4349, 0.10070, -1.5985 0.3960, 0.10120, -1.6498 0.3566, 0.10020, -1.6604 0.3172, 0.09790, -1.6245 0.2778, 0.09440, -1.5734 0.2393, 0.08960, -1.4790 0.2056, 0.08360, -1.3971 0.1633, 0.07610, -1.3188 0.1261, 0.06710, -1.2339 0.0900, 0.05640, -1.1973 0.0571, 0.04390, -1.2629 0.0283, 0.02940, -1.4209 0.0142, 0.01970, -1.5981 0.0081, 0.01410, -1.7377 0.0026, 0.00780, -1.7865 0.0000, 0.00000, -2.1575 0.0037, -0.00840, -1.5059 0.0112, -0.01420, -1.2258 0.0191, -0.01930, -1.1273 0.0397, -0.03030, -1.0565 0.0706, -0.04420, -1.0983 0.1037, -0.05710, -1.1884 0.1384, -0.06890, -1.3088 0.1741, -0.07950, -1.3983 0.2102, -0.08660, -1.4619 0.2472, -0.09640, -1.5274 0.2844, -0.10270, -1.5430 0.3225, -0.10690, -1.5297 0.3608, -0.10890, -1.5054 0.3991, -0.10830, -1.4750 0.4373, -0.10510, -1.4389 0.4757, -0.09890, -1.4230 0.5137, -0.09067, -1.4074 0.5611, -0.07859, -1.4509 16 Flap element taps 1.0000, 0.00130, -1.2303 0.9365, 0.01390, 0.6278 0.8333, 0.03280, 0.9468 0.7436, 0.04930, 0.9904 0.7049, 0.05667, 0.9629 0.6662, 0.06411, 0.8589 0.6274, 0.07172, 0.5763 0.6009, 0.07523, -1.2433 0.6069, 0.02889, -1.2650 0.6079, -0.01747, -1.3082 0.6167, -0.06381, -1.2922 0.6558, -0.05300, -1.2748 0.7045, -0.04117, -1.2965 0.7429, -0.03210, -1.3376 0.8333, -0.01400, -1.3434 0.9311, -0.00120, -1.2571 --------- Run Conditions: vel=106.6 ft/s Re=1.019x10^6 AOA=210.00 Flap deflection=90.00 Totals: Cl=-0.1411 Cdp=0.6163 Cm(c/4)=-0.0518 Cs=0.6043 Ch=-0.0997 Main component: Cl=0.3255 Cdp=0.1726 Cm=0.1625 Flap component: Cl=-0.4666 Cdp=0.4437 Cm=-0.1678 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -1.0264 0.5905, -0.01667, -1.1784 0.5709, 0.03110, -1.5998 0.5889, 0.07933, -1.3772 0.5500, 0.08689, 0.9829 0.5110, 0.09367, 0.7188 0.4731, 0.09830, 0.4047 0.4349, 0.10070, 0.1431 0.3960, 0.10120, -0.0616 0.3566, 0.10020, -0.2482 0.3172, 0.09790, -0.3895 0.2778, 0.09440, -0.5622 0.2393, 0.08960, -0.7015 0.2056, 0.08360, -0.8504 0.1633, 0.07610, -0.9917 0.1261, 0.06710, -1.0881 0.0900, 0.05640, -1.1732 0.0571, 0.04390, -1.1311 0.0283, 0.02940, -1.0791 0.0142, 0.01970, -1.0860 0.0081, 0.01410, -1.0927 0.0026, 0.00780, -1.0242 0.0000, 0.00000, -1.0887 0.0037, -0.00840, -1.0823 0.0112, -0.01420, -1.0678 0.0191, -0.01930, -1.0622 0.0397, -0.03030, -1.0644 0.0706, -0.04420, -1.0584 0.1037, -0.05710, -1.0467 0.1384, -0.06890, -1.0562 0.1741, -0.07950, -1.0562 0.2102, -0.08660, -1.0441 0.2472, -0.09640, -1.0466 0.2844, -0.10270, -1.0458 0.3225, -0.10690, -1.0444 0.3608, -0.10890, -1.0459 0.3991, -0.10830, -1.0517 0.4373, -0.10510, -1.0462 0.4757, -0.09890, -1.0431 0.5137, -0.09067, -1.0252 0.5611, -0.07859, -1.0191 16 Flap element taps 1.0000, 0.00130, -0.7478 0.9365, 0.01390, 0.2575 0.8333, 0.03280, 0.6461 0.7436, 0.04930, 0.8585 0.7049, 0.05667, 0.9468 0.6662, 0.06411, 0.9996 0.6274, 0.07172, 0.9522 0.6009, 0.07523, -1.7271 0.6069, 0.02889, -1.7982 0.6079, -0.01747, -1.4212 0.6167, -0.06381, -0.9839 0.6558, -0.05300, -0.9917 0.7045, -0.04117, -1.0039 0.7429, -0.03210, -1.0132 0.8333, -0.01400, -1.1290 0.9311, -0.00120, -1.1080 --------- Run Conditions: vel=106.3 ft/s Re=1.016x10^6 AOA=239.98 Flap deflection=90.00 Totals: Cl=0.3358 Cdp=1.0329 Cm(c/4)=0.1693 Cs=0.2260 Ch=-0.0448 Main component: Cl=0.4930 Cdp=0.7843 Cm=0.3353 Flap component: Cl=-0.1571 Cdp=0.2486 Cm=0.0996 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -1.4787 0.5905, -0.01667, -1.5395 0.5709, 0.03110, -1.4903 0.5889, 0.07933, -1.5505 0.5500, 0.08689, 0.9134 0.5110, 0.09367, 0.9995 0.4731, 0.09830, 0.9657 0.4349, 0.10070, 0.8741 0.3960, 0.10120, 0.7653 0.3566, 0.10020, 0.6240 0.3172, 0.09790, 0.4935 0.2778, 0.09440, 0.3271 0.2393, 0.08960, 0.1645 0.2056, 0.08360, -0.0315 0.1633, 0.07610, -0.2714 0.1261, 0.06710, -0.5097 0.0900, 0.05640, -0.8229 0.0571, 0.04390, -1.2079 0.0283, 0.02940, -1.4637 0.0142, 0.01970, -1.3656 0.0081, 0.01410, -1.3575 0.0026, 0.00780, -1.2876 0.0000, 0.00000, -1.3848 0.0037, -0.00840, -1.3953 0.0112, -0.01420, -1.3982 0.0191, -0.01930, -1.4062 0.0397, -0.03030, -1.4383 0.0706, -0.04420, -1.4661 0.1037, -0.05710, -1.4746 0.1384, -0.06890, -1.4745 0.1741, -0.07950, -1.4827 0.2102, -0.08660, -1.4756 0.2472, -0.09640, -1.4916 0.2844, -0.10270, -1.5071 0.3225, -0.10690, -1.5262 0.3608, -0.10890, -1.5429 0.3991, -0.10830, -1.5517 0.4373, -0.10510, -1.5366 0.4757, -0.09890, -1.5085 0.5137, -0.09067, -1.4572 0.5611, -0.07859, -1.4323 16 Flap element taps 1.0000, 0.00130, -0.5963 0.9365, 0.01390, -0.3279 0.8333, 0.03280, -0.1339 0.7436, 0.04930, -0.2158 0.7049, 0.05667, -0.5841 0.6662, 0.06411, -0.7114 0.6274, 0.07172, -0.6811 0.6009, 0.07523, -0.6633 0.6069, 0.02889, 0.9769 0.6079, -0.01747, 0.6542 0.6167, -0.06381, -1.3852 0.6558, -0.05300, -1.4155 0.7045, -0.04117, -1.4346 0.7429, -0.03210, -1.4773 0.8333, -0.01400, -1.0738 0.9311, -0.00120, -0.5375 --------- Run Conditions: vel=105.5 ft/s Re=1.007x10^6 AOA=268.99 Flap deflection=90.00 Totals: Cl=0.5553 Cdp=1.1527 Cm(c/4)=0.1982 Cs=-0.5349 Ch=0.0965 Main component: Cl=0.0941 Cdp=0.9775 Cm=0.3221 Flap component: Cl=0.4612 Cdp=0.1752 Cm=0.1666 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -1.2090 0.5905, -0.01667, -1.2134 0.5709, 0.03110, -1.1937 0.5889, 0.07933, -1.2260 0.5500, 0.08689, 0.5916 0.5110, 0.09367, 0.7885 0.4731, 0.09830, 0.9180 0.4349, 0.10070, 0.9790 0.3960, 0.10120, 1.0073 0.3566, 0.10020, 0.9855 0.3172, 0.09790, 0.9611 0.2778, 0.09440, 0.9000 0.2393, 0.08960, 0.8365 0.2056, 0.08360, 0.7343 0.1633, 0.07610, 0.5646 0.1261, 0.06710, 0.3829 0.0900, 0.05640, 0.0978 0.0571, 0.04390, -0.3282 0.0283, 0.02940, -0.8764 0.0142, 0.01970, -1.2292 0.0081, 0.01410, -1.2167 0.0026, 0.00780, -1.0632 0.0000, 0.00000, -1.1253 0.0037, -0.00840, -1.1257 0.0112, -0.01420, -1.1148 0.0191, -0.01930, -1.1152 0.0397, -0.03030, -1.1237 0.0706, -0.04420, -1.1327 0.1037, -0.05710, -1.1334 0.1384, -0.06890, -1.1553 0.1741, -0.07950, -1.1617 0.2102, -0.08660, -1.1471 0.2472, -0.09640, -1.1585 0.2844, -0.10270, -1.1597 0.3225, -0.10690, -1.1739 0.3608, -0.10890, -1.1752 0.3991, -0.10830, -1.1846 0.4373, -0.10510, -1.1765 0.4757, -0.09890, -1.1725 0.5137, -0.09067, -1.1599 0.5611, -0.07859, -1.1573 16 Flap element taps 1.0000, 0.00130, -1.6702 0.9365, 0.01390, -1.7339 0.8333, 0.03280, -1.7300 0.7436, 0.04930, -1.7018 0.7049, 0.05667, -1.6995 0.6662, 0.06411, -1.6898 0.6274, 0.07172, -1.6909 0.6009, 0.07523, -1.6972 0.6069, 0.02889, 0.7259 0.6079, -0.01747, 0.9689 0.6167, -0.06381, -0.4427 0.6558, -0.05300, -0.4890 0.7045, -0.04117, 0.0584 0.7429, -0.03210, -0.2034 0.8333, -0.01400, -0.6081 0.9311, -0.00120, -0.8323