S809 SPOILER FLAP, CLEAN, CHORD = 18 INCHES --------- Run Conditions: vel=106.3 ft/s Re=1.003x10^6 AOA=-6.01 Flap deflection=30.00 Totals: Cl=-0.7042 Cdp=0.2130 Cm(c/4)=-0.0160 Cs=-0.1381 Ch=-0.0064 Main component: Cl=-0.7404 Cdp=0.0374 Cm=0.1780 Flap component: Cl=0.0362 Cdp=0.1756 Cm=-0.0134 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.2540 0.5905, -0.01667, -0.4550 0.5709, 0.03110, -0.1854 0.5889, 0.07933, -0.2039 0.5500, 0.08689, 0.5532 0.5110, 0.09367, 0.3604 0.4731, 0.09830, 0.2376 0.4349, 0.10070, 0.2184 0.3960, 0.10120, 0.1769 0.3566, 0.10020, 0.1547 0.3172, 0.09790, 0.1657 0.2778, 0.09440, 0.1705 0.2393, 0.08960, 0.2021 0.2056, 0.08360, 0.2458 0.1633, 0.07610, 0.3198 0.1261, 0.06710, 0.4219 0.0900, 0.05640, 0.5581 0.0571, 0.04390, 0.7312 0.0283, 0.02940, 0.9436 0.0142, 0.01970, 1.0066 0.0081, 0.01410, 0.9149 0.0026, 0.00780, 0.3710 0.0000, 0.00000, -1.5389 0.0037, -0.00840, -2.4292 0.0112, -0.01420, -1.9447 0.0191, -0.01930, -1.8568 0.0397, -0.03030, -1.0854 0.0706, -0.04420, -1.0372 0.1037, -0.05710, -1.0499 0.1384, -0.06890, -1.0670 0.1741, -0.07950, -1.0802 0.2102, -0.08660, -1.1212 0.2472, -0.09640, -1.1746 0.2844, -0.10270, -1.1702 0.3225, -0.10690, -1.1384 0.3608, -0.10890, -1.0651 0.3991, -0.10830, -0.9244 0.4373, -0.10510, -0.6654 0.4757, -0.09890, -0.4054 0.5137, -0.09067, -0.2943 0.5611, -0.07859, -0.2895 16 Flap element taps 1.0000, 0.00130, -0.8708 0.9365, 0.01390, -0.8022 0.8333, 0.03280, -0.7972 0.7436, 0.04930, -0.7921 0.7049, 0.05667, -0.7845 0.6662, 0.06411, -0.7823 0.6274, 0.07172, -0.7749 0.6009, 0.07523, -0.7730 0.6069, 0.02889, 0.8862 0.6079, -0.01747, 0.8440 0.6167, -0.06381, -0.5888 0.6558, -0.05300, -0.6180 0.7045, -0.04117, -0.6321 0.7429, -0.03210, -0.6407 0.8333, -0.01400, -0.6220 0.9311, -0.00120, -0.2437 --------- Run Conditions: vel=106.2 ft/s Re=1.001x10^6 AOA=0.00 Flap deflection=30.00 Totals: Cl=-0.0768 Cdp=0.2456 Cm(c/4)=-0.0920 Cs=-0.2456 Ch=0.0203 Main component: Cl=-0.2915 Cdp=-0.0276 Cm=0.0929 Flap component: Cl=0.2147 Cdp=0.2732 Cm=-0.1658 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.3764 0.5905, -0.01667, -0.0120 0.5709, 0.03110, 0.1907 0.5889, 0.07933, 0.1475 0.5500, 0.08689, 0.5147 0.5110, 0.09367, 0.3559 0.4731, 0.09830, 0.2232 0.4349, 0.10070, -0.0156 0.3960, 0.10120, -0.0385 0.3566, 0.10020, -0.0796 0.3172, 0.09790, -0.1095 0.2778, 0.09440, -0.1443 0.2393, 0.08960, -0.1530 0.2056, 0.08360, -0.1540 0.1633, 0.07610, -0.1249 0.1261, 0.06710, -0.0694 0.0900, 0.05640, 0.0135 0.0571, 0.04390, 0.1420 0.0283, 0.02940, 0.3710 0.0142, 0.01970, 0.6144 0.0081, 0.01410, 0.7485 0.0026, 0.00780, 0.9268 0.0000, 0.00000, 0.9019 0.0037, -0.00840, 0.2873 0.0112, -0.01420, 0.1018 0.0191, -0.01930, 0.0419 0.0397, -0.03030, -0.0439 0.0706, -0.04420, -0.1763 0.1037, -0.05710, -0.3053 0.1384, -0.06890, -0.4086 0.1741, -0.07950, -0.4998 0.2102, -0.08660, -0.5956 0.2472, -0.09640, -0.6958 0.2844, -0.10270, -0.7544 0.3225, -0.10690, -0.7925 0.3608, -0.10890, -0.7899 0.3991, -0.10830, -0.7434 0.4373, -0.10510, -0.6723 0.4757, -0.09890, -0.6760 0.5137, -0.09067, -0.0969 0.5611, -0.07859, 0.1339 16 Flap element taps 1.0000, 0.00130, -0.9384 0.9365, 0.01390, -0.9132 0.8333, 0.03280, -0.9166 0.7436, 0.04930, -0.9034 0.7049, 0.05667, -0.8901 0.6662, 0.06411, -0.8881 0.6274, 0.07172, -0.8822 0.6009, 0.07523, -0.8864 0.6069, 0.02889, 0.8524 0.6079, -0.01747, 0.8744 0.6167, -0.06381, -0.0935 0.6558, -0.05300, -0.1158 0.7045, -0.04117, -0.1302 0.7429, -0.03210, -0.1186 0.8333, -0.01400, 0.0330 0.9311, -0.00120, 0.0727 --------- Run Conditions: vel=106.0 ft/s Re=1.000x10^6 AOA=3.01 Flap deflection=30.00 Totals: Cl=0.1578 Cdp=0.2588 Cm(c/4)=-0.0969 Cs=-0.2502 Ch=0.0259 Main component: Cl=-0.0692 Cdp=-0.0404 Cm=0.0473 Flap component: Cl=0.2270 Cdp=0.2993 Cm=-0.1869 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.4145 0.5905, -0.01667, 0.0573 0.5709, 0.03110, 0.2483 0.5889, 0.07933, 0.2178 0.5500, 0.08689, 0.4758 0.5110, 0.09367, 0.3153 0.4731, 0.09830, 0.1543 0.4349, 0.10070, 0.0021 0.3960, 0.10120, -0.1560 0.3566, 0.10020, -0.2090 0.3172, 0.09790, -0.2445 0.2778, 0.09440, -0.2978 0.2393, 0.08960, -0.3278 0.2056, 0.08360, -0.3409 0.1633, 0.07610, -0.3576 0.1261, 0.06710, -0.3269 0.0900, 0.05640, -0.2949 0.0571, 0.04390, -0.2233 0.0283, 0.02940, -0.0731 0.0142, 0.01970, 0.1323 0.0081, 0.01410, 0.2749 0.0026, 0.00780, 0.5249 0.0000, 0.00000, 0.9353 0.0037, -0.00840, 0.8379 0.0112, -0.01420, 0.6239 0.0191, -0.01930, 0.5065 0.0397, -0.03030, 0.3300 0.0706, -0.04420, 0.1489 0.1037, -0.05710, -0.0064 0.1384, -0.06890, -0.1495 0.1741, -0.07950, -0.2574 0.2102, -0.08660, -0.3552 0.2472, -0.09640, -0.4759 0.2844, -0.10270, -0.5449 0.3225, -0.10690, -0.6135 0.3608, -0.10890, -0.6237 0.3991, -0.10830, -0.6056 0.4373, -0.10510, -0.5155 0.4757, -0.09890, -0.5024 0.5137, -0.09067, -0.0253 0.5611, -0.07859, 0.1813 16 Flap element taps 1.0000, 0.00130, -0.9548 0.9365, 0.01390, -0.9373 0.8333, 0.03280, -0.9373 0.7436, 0.04930, -0.9357 0.7049, 0.05667, -0.9326 0.6662, 0.06411, -0.9235 0.6274, 0.07172, -0.9172 0.6009, 0.07523, -0.9220 0.6069, 0.02889, 0.8436 0.6079, -0.01747, 0.8647 0.6167, -0.06381, -0.0298 0.6558, -0.05300, -0.0534 0.7045, -0.04117, -0.0695 0.7429, -0.03210, -0.0635 0.8333, -0.01400, 0.1073 0.9311, -0.00120, 0.1079 --------- Run Conditions: vel=105.9 ft/s Re=0.997x10^6 AOA=5.99 Flap deflection=30.00 Totals: Cl=0.3856 Cdp=0.2646 Cm(c/4)=-0.0957 Cs=-0.2229 Ch=0.0288 Main component: Cl=0.1573 Cdp=-0.0517 Cm=0.0021 Flap component: Cl=0.2283 Cdp=0.3163 Cm=-0.2006 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.4452 0.5905, -0.01667, 0.1122 0.5709, 0.03110, 0.3077 0.5889, 0.07933, 0.3095 0.5500, 0.08689, 0.4057 0.5110, 0.09367, 0.2839 0.4731, 0.09830, 0.1040 0.4349, 0.10070, -0.0655 0.3960, 0.10120, -0.1496 0.3566, 0.10020, -0.2932 0.3172, 0.09790, -0.4073 0.2778, 0.09440, -0.4619 0.2393, 0.08960, -0.5098 0.2056, 0.08360, -0.5426 0.1633, 0.07610, -0.6093 0.1261, 0.06710, -0.6151 0.0900, 0.05640, -0.6502 0.0571, 0.04390, -0.6669 0.0283, 0.02940, -0.6525 0.0142, 0.01970, -0.5753 0.0081, 0.01410, -0.5112 0.0026, 0.00780, -0.2685 0.0000, 0.00000, 0.2671 0.0037, -0.00840, 0.9731 0.0112, -0.01420, 0.9252 0.0191, -0.01930, 0.8278 0.0397, -0.03030, 0.6381 0.0706, -0.04420, 0.4377 0.1037, -0.05710, 0.2698 0.1384, -0.06890, 0.0985 0.1741, -0.07950, -0.0190 0.2102, -0.08660, -0.1186 0.2472, -0.09640, -0.2540 0.2844, -0.10270, -0.3325 0.3225, -0.10690, -0.4253 0.3608, -0.10890, -0.4455 0.3991, -0.10830, -0.4569 0.4373, -0.10510, -0.3622 0.4757, -0.09890, -0.3383 0.5137, -0.09067, 0.0033 0.5611, -0.07859, 0.2311 16 Flap element taps 1.0000, 0.00130, -0.9362 0.9365, 0.01390, -0.9238 0.8333, 0.03280, -0.9327 0.7436, 0.04930, -0.9262 0.7049, 0.05667, -0.9176 0.6662, 0.06411, -0.9052 0.6274, 0.07172, -0.9051 0.6009, 0.07523, -0.9086 0.6069, 0.02889, 0.8617 0.6079, -0.01747, 0.7987 0.6167, -0.06381, 0.0273 0.6558, -0.05300, 0.0108 0.7045, -0.04117, -0.0104 0.7429, -0.03210, 0.0046 0.8333, -0.01400, 0.1893 0.9311, -0.00120, 0.1384 --------- Run Conditions: vel=106.0 ft/s Re=0.999x10^6 AOA=9.01 Flap deflection=30.00 Totals: Cl=0.6575 Cdp=0.2790 Cm(c/4)=-0.1423 Cs=-0.1726 Ch=0.0314 Main component: Cl=0.3277 Cdp=-0.0529 Cm=-0.0211 Flap component: Cl=0.3299 Cdp=0.3318 Cm=-0.2944 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.2382 0.5905, -0.01667, 0.2769 0.5709, 0.03110, 0.2919 0.5889, 0.07933, 0.1504 0.5500, 0.08689, 0.1697 0.5110, 0.09367, 0.1636 0.4731, 0.09830, 0.1472 0.4349, 0.10070, 0.0282 0.3960, 0.10120, -0.1154 0.3566, 0.10020, -0.3157 0.3172, 0.09790, -0.4240 0.2778, 0.09440, -0.5469 0.2393, 0.08960, -0.6484 0.2056, 0.08360, -0.7178 0.1633, 0.07610, -0.8508 0.1261, 0.06710, -0.9257 0.0900, 0.05640, -1.0387 0.0571, 0.04390, -1.1714 0.0283, 0.02940, -1.3476 0.0142, 0.01970, -1.4764 0.0081, 0.01410, -1.5954 0.0026, 0.00780, -1.4636 0.0000, 0.00000, -1.1924 0.0037, -0.00840, 0.7384 0.0112, -0.01420, 0.9853 0.0191, -0.01930, 0.9745 0.0397, -0.03030, 0.8445 0.0706, -0.04420, 0.6590 0.1037, -0.05710, 0.4923 0.1384, -0.06890, 0.3062 0.1741, -0.07950, 0.1844 0.2102, -0.08660, 0.0798 0.2472, -0.09640, -0.0695 0.2844, -0.10270, -0.1645 0.3225, -0.10690, -0.2824 0.3608, -0.10890, -0.3268 0.3991, -0.10830, -0.3787 0.4373, -0.10510, -0.3125 0.4757, -0.09890, -0.2502 0.5137, -0.09067, -0.2214 0.5611, -0.07859, 0.1436 16 Flap element taps 1.0000, 0.00130, -0.9240 0.9365, 0.01390, -0.9272 0.8333, 0.03280, -0.9291 0.7436, 0.04930, -0.9308 0.7049, 0.05667, -0.9232 0.6662, 0.06411, -0.9081 0.6274, 0.07172, -0.9043 0.6009, 0.07523, -0.9417 0.6069, 0.02889, 0.2109 0.6079, -0.01747, 0.2067 0.6167, -0.06381, 0.2402 0.6558, -0.05300, 0.2374 0.7045, -0.04117, 0.2164 0.7429, -0.03210, 0.2682 0.8333, -0.01400, 0.6677 0.9311, -0.00120, 0.2818 --------- Run Conditions: vel=106.3 ft/s Re=1.002x10^6 AOA=12.01 Flap deflection=30.00 Totals: Cl=0.8772 Cdp=0.2859 Cm(c/4)=-0.1497 Cs=-0.0971 Ch=0.0255 Main component: Cl=0.5461 Cdp=-0.0444 Cm=-0.0716 Flap component: Cl=0.3311 Cdp=0.3303 Cm=-0.3074 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.2268 0.5905, -0.01667, 0.2673 0.5709, 0.03110, 0.3338 0.5889, 0.07933, -0.0923 0.5500, 0.08689, -0.0686 0.5110, 0.09367, -0.0772 0.4731, 0.09830, -0.0709 0.4349, 0.10070, -0.0903 0.3960, 0.10120, -0.1196 0.3566, 0.10020, -0.3183 0.3172, 0.09790, -0.4717 0.2778, 0.09440, -0.6405 0.2393, 0.08960, -0.7825 0.2056, 0.08360, -0.8914 0.1633, 0.07610, -1.0691 0.1261, 0.06710, -1.1818 0.0900, 0.05640, -1.3849 0.0571, 0.04390, -1.6292 0.0283, 0.02940, -2.0144 0.0142, 0.01970, -2.5468 0.0081, 0.01410, -2.9538 0.0026, 0.00780, -2.9956 0.0000, 0.00000, -3.2357 0.0037, -0.00840, 0.1495 0.0112, -0.01420, 0.8500 0.0191, -0.01930, 0.9731 0.0397, -0.03030, 0.9563 0.0706, -0.04420, 0.8192 0.1037, -0.05710, 0.6724 0.1384, -0.06890, 0.4857 0.1741, -0.07950, 0.3651 0.2102, -0.08660, 0.2665 0.2472, -0.09640, 0.1124 0.2844, -0.10270, 0.0141 0.3225, -0.10690, -0.1180 0.3608, -0.10890, -0.1729 0.3991, -0.10830, -0.2458 0.4373, -0.10510, -0.2012 0.4757, -0.09890, -0.1404 0.5137, -0.09067, -0.0983 0.5611, -0.07859, 0.1951 16 Flap element taps 1.0000, 0.00130, -0.8693 0.9365, 0.01390, -0.8799 0.8333, 0.03280, -0.8848 0.7436, 0.04930, -0.8870 0.7049, 0.05667, -0.8844 0.6662, 0.06411, -0.8669 0.6274, 0.07172, -0.8710 0.6009, 0.07523, -0.9226 0.6069, 0.02889, -0.0120 0.6079, -0.01747, 0.0330 0.6167, -0.06381, 0.1578 0.6558, -0.05300, 0.1698 0.7045, -0.04117, 0.2109 0.7429, -0.03210, 0.5146 0.8333, -0.01400, 0.7349 0.9311, -0.00120, 0.3025 --------- Run Conditions: vel=106.5 ft/s Re=1.002x10^6 AOA=14.99 Flap deflection=30.00 Totals: Cl=1.1040 Cdp=0.3073 Cm(c/4)=-0.1613 Cs=-0.0112 Ch=0.0255 Main component: Cl=0.7672 Cdp=-0.0221 Cm=-0.1257 Flap component: Cl=0.3368 Cdp=0.3294 Cm=-0.3221 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.2018 0.5905, -0.01667, 0.1964 0.5709, 0.03110, 0.4048 0.5889, 0.07933, -0.3486 0.5500, 0.08689, -0.3180 0.5110, 0.09367, -0.3398 0.4731, 0.09830, -0.3294 0.4349, 0.10070, -0.3369 0.3960, 0.10120, -0.3422 0.3566, 0.10020, -0.3931 0.3172, 0.09790, -0.4882 0.2778, 0.09440, -0.6693 0.2393, 0.08960, -0.8536 0.2056, 0.08360, -1.0469 0.1633, 0.07610, -1.2454 0.1261, 0.06710, -1.4395 0.0900, 0.05640, -1.7197 0.0571, 0.04390, -2.1163 0.0283, 0.02940, -2.7719 0.0142, 0.01970, -3.4265 0.0081, 0.01410, -4.5153 0.0026, 0.00780, -4.9637 0.0000, 0.00000, -5.7803 0.0037, -0.00840, -0.7242 0.0112, -0.01420, 0.5529 0.0191, -0.01930, 0.8690 0.0397, -0.03030, 1.0028 0.0706, -0.04420, 0.9269 0.1037, -0.05710, 0.8119 0.1384, -0.06890, 0.6673 0.1741, -0.07950, 0.5447 0.2102, -0.08660, 0.4244 0.2472, -0.09640, 0.2929 0.2844, -0.10270, 0.1710 0.3225, -0.10690, 0.0665 0.3608, -0.10890, -0.0249 0.3991, -0.10830, -0.0929 0.4373, -0.10510, -0.0883 0.4757, -0.09890, -0.0496 0.5137, -0.09067, 0.0105 0.5611, -0.07859, 0.1745 16 Flap element taps 1.0000, 0.00130, -0.7931 0.9365, 0.01390, -0.8136 0.8333, 0.03280, -0.8227 0.7436, 0.04930, -0.8173 0.7049, 0.05667, -0.8101 0.6662, 0.06411, -0.8010 0.6274, 0.07172, -0.7987 0.6009, 0.07523, -0.8457 0.6069, 0.02889, -0.2257 0.6079, -0.01747, -0.1210 0.6167, -0.06381, 0.0485 0.6558, -0.05300, 0.1111 0.7045, -0.04117, 0.3514 0.7429, -0.03210, 0.9572 0.8333, -0.01400, 0.7072 0.9311, -0.00120, 0.3395 --------- Run Conditions: vel=103.8 ft/s Re=0.977x10^6 AOA=17.98 Flap deflection=30.00 Totals: Cl=0.9842 Cdp=0.4762 Cm(c/4)=-0.2203 Cs=-0.1491 Ch=0.0160 Main component: Cl=0.6466 Cdp=0.1977 Cm=-0.1696 Flap component: Cl=0.3376 Cdp=0.2785 Cm=-0.3215 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0557 0.5905, -0.01667, 0.0099 0.5709, 0.03110, 0.3981 0.5889, 0.07933, -0.9076 0.5500, 0.08689, -0.8854 0.5110, 0.09367, -0.8474 0.4731, 0.09830, -0.8503 0.4349, 0.10070, -0.9064 0.3960, 0.10120, -0.9258 0.3566, 0.10020, -0.9506 0.3172, 0.09790, -0.9324 0.2778, 0.09440, -0.9299 0.2393, 0.08960, -0.9056 0.2056, 0.08360, -0.8955 0.1633, 0.07610, -0.9131 0.1261, 0.06710, -0.8983 0.0900, 0.05640, -0.8993 0.0571, 0.04390, -0.8973 0.0283, 0.02940, -0.9198 0.0142, 0.01970, -0.9235 0.0081, 0.01410, -0.9060 0.0026, 0.00780, -0.8554 0.0000, 0.00000, -1.2108 0.0037, -0.00840, 0.3990 0.0112, -0.01420, 0.8814 0.0191, -0.01930, 0.9822 0.0397, -0.03030, 0.9822 0.0706, -0.04420, 0.8707 0.1037, -0.05710, 0.7513 0.1384, -0.06890, 0.6053 0.1741, -0.07950, 0.4854 0.2102, -0.08660, 0.3772 0.2472, -0.09640, 0.2445 0.2844, -0.10270, 0.1264 0.3225, -0.10690, 0.0175 0.3608, -0.10890, -0.0706 0.3991, -0.10830, -0.1423 0.4373, -0.10510, -0.1359 0.4757, -0.09890, -0.1003 0.5137, -0.09067, -0.0374 0.5611, -0.07859, 0.0762 16 Flap element taps 1.0000, 0.00130, -0.6809 0.9365, 0.01390, -0.7006 0.8333, 0.03280, -0.7105 0.7436, 0.04930, -0.7156 0.7049, 0.05667, -0.7170 0.6662, 0.06411, -0.7145 0.6274, 0.07172, -0.7158 0.6009, 0.07523, -0.7354 0.6069, 0.02889, -0.9035 0.6079, -0.01747, -0.4253 0.6167, -0.06381, -0.2892 0.6558, -0.05300, 0.0064 0.7045, -0.04117, 0.6447 0.7429, -0.03210, 1.0063 0.8333, -0.01400, 0.6930 0.9311, -0.00120, 0.3512 --------- Run Conditions: vel=106.3 ft/s Re=1.002x10^6 AOA=19.98 Flap deflection=30.00 Totals: Cl=0.9944 Cdp=0.5380 Cm(c/4)=-0.2308 Cs=-0.1658 Ch=0.0190 Main component: Cl=0.6543 Cdp=0.2328 Cm=-0.1761 Flap component: Cl=0.3401 Cdp=0.3052 Cm=-0.3344 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0435 0.5905, -0.01667, 0.0001 0.5709, 0.03110, 0.3851 0.5889, 0.07933, -0.9416 0.5500, 0.08689, -0.9417 0.5110, 0.09367, -0.9141 0.4731, 0.09830, -0.8522 0.4349, 0.10070, -0.8669 0.3960, 0.10120, -0.8932 0.3566, 0.10020, -0.9363 0.3172, 0.09790, -0.9343 0.2778, 0.09440, -0.9388 0.2393, 0.08960, -0.9102 0.2056, 0.08360, -0.8965 0.1633, 0.07610, -0.9049 0.1261, 0.06710, -0.8873 0.0900, 0.05640, -0.8859 0.0571, 0.04390, -0.8859 0.0283, 0.02940, -0.9015 0.0142, 0.01970, -0.9019 0.0081, 0.01410, -0.8859 0.0026, 0.00780, -0.8365 0.0000, 0.00000, -1.1606 0.0037, -0.00840, 0.3244 0.0112, -0.01420, 0.8467 0.0191, -0.01930, 0.9710 0.0397, -0.03030, 0.9963 0.0706, -0.04420, 0.9021 0.1037, -0.05710, 0.7935 0.1384, -0.06890, 0.6538 0.1741, -0.07950, 0.5350 0.2102, -0.08660, 0.4274 0.2472, -0.09640, 0.2951 0.2844, -0.10270, 0.1761 0.3225, -0.10690, 0.0647 0.3608, -0.10890, -0.0282 0.3991, -0.10830, -0.1039 0.4373, -0.10510, -0.1069 0.4757, -0.09890, -0.0787 0.5137, -0.09067, -0.0152 0.5611, -0.07859, 0.0655 16 Flap element taps 1.0000, 0.00130, -0.7329 0.9365, 0.01390, -0.7541 0.8333, 0.03280, -0.7619 0.7436, 0.04930, -0.7645 0.7049, 0.05667, -0.7682 0.6662, 0.06411, -0.7678 0.6274, 0.07172, -0.7679 0.6009, 0.07523, -0.7882 0.6069, 0.02889, -0.9255 0.6079, -0.01747, -0.4352 0.6167, -0.06381, -0.3188 0.6558, -0.05300, 0.0069 0.7045, -0.04117, 0.6934 0.7429, -0.03210, 1.0062 0.8333, -0.01400, 0.6927 0.9311, -0.00120, 0.3458 --------- Run Conditions: vel=105.6 ft/s Re=0.994x10^6 AOA=24.00 Flap deflection=30.00 Totals: Cl=1.0809 Cdp=0.6894 Cm(c/4)=-0.2616 Cs=-0.1902 Ch=0.0266 Main component: Cl=0.7319 Cdp=0.3217 Cm=-0.2100 Flap component: Cl=0.3490 Cdp=0.3677 Cm=-0.3686 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0315 0.5905, -0.01667, -0.0348 0.5709, 0.03110, 0.4003 0.5889, 0.07933, -1.0651 0.5500, 0.08689, -1.0732 0.5110, 0.09367, -1.0911 0.4731, 0.09830, -1.0309 0.4349, 0.10070, -0.9894 0.3960, 0.10120, -0.9678 0.3566, 0.10020, -0.9970 0.3172, 0.09790, -1.0067 0.2778, 0.09440, -1.0245 0.2393, 0.08960, -1.0065 0.2056, 0.08360, -0.9947 0.1633, 0.07610, -1.0028 0.1261, 0.06710, -0.9873 0.0900, 0.05640, -0.9831 0.0571, 0.04390, -0.9813 0.0283, 0.02940, -0.9937 0.0142, 0.01970, -0.9940 0.0081, 0.01410, -0.9816 0.0026, 0.00780, -0.9251 0.0000, 0.00000, -1.0368 0.0037, -0.00840, 0.0589 0.0112, -0.01420, 0.7088 0.0191, -0.01930, 0.9030 0.0397, -0.03030, 1.0016 0.0706, -0.04420, 0.9528 0.1037, -0.05710, 0.8741 0.1384, -0.06890, 0.7517 0.1741, -0.07950, 0.6433 0.2102, -0.08660, 0.5411 0.2472, -0.09640, 0.4133 0.2844, -0.10270, 0.2939 0.3225, -0.10690, 0.1825 0.3608, -0.10890, 0.0777 0.3991, -0.10830, -0.0057 0.4373, -0.10510, -0.0252 0.4757, -0.09890, -0.0161 0.5137, -0.09067, 0.0446 0.5611, -0.07859, 0.0993 16 Flap element taps 1.0000, 0.00130, -0.8723 0.9365, 0.01390, -0.8927 0.8333, 0.03280, -0.9020 0.7436, 0.04930, -0.9093 0.7049, 0.05667, -0.9106 0.6662, 0.06411, -0.9099 0.6274, 0.07172, -0.9105 0.6009, 0.07523, -0.9325 0.6069, 0.02889, -1.0132 0.6079, -0.01747, -0.5081 0.6167, -0.06381, -0.3864 0.6558, -0.05300, 0.0066 0.7045, -0.04117, 0.7856 0.7429, -0.03210, 0.9991 0.8333, -0.01400, 0.6870 0.9311, -0.00120, 0.3269 --------- Run Conditions: vel=105.6 ft/s Re=0.994x10^6 AOA=26.99 Flap deflection=30.00 Totals: Cl=1.2135 Cdp=0.8544 Cm(c/4)=-0.3016 Cs=-0.2106 Ch=0.0339 Main component: Cl=0.8439 Cdp=0.4172 Cm=-0.2542 Flap component: Cl=0.3696 Cdp=0.4372 Cm=-0.4146 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0098 0.5905, -0.01667, -0.0631 0.5709, 0.03110, 0.3719 0.5889, 0.07933, -1.2646 0.5500, 0.08689, -1.2556 0.5110, 0.09367, -1.2824 0.4731, 0.09830, -1.2485 0.4349, 0.10070, -1.2040 0.3960, 0.10120, -1.1620 0.3566, 0.10020, -1.1680 0.3172, 0.09790, -1.1747 0.2778, 0.09440, -1.1970 0.2393, 0.08960, -1.1878 0.2056, 0.08360, -1.1859 0.1633, 0.07610, -1.1904 0.1261, 0.06710, -1.1758 0.0900, 0.05640, -1.1719 0.0571, 0.04390, -1.1682 0.0283, 0.02940, -1.1750 0.0142, 0.01970, -1.1750 0.0081, 0.01410, -1.1650 0.0026, 0.00780, -1.0901 0.0000, 0.00000, -1.1971 0.0037, -0.00840, -0.2355 0.0112, -0.01420, 0.5460 0.0191, -0.01930, 0.8111 0.0397, -0.03030, 0.9857 0.0706, -0.04420, 0.9830 0.1037, -0.05710, 0.9283 0.1384, -0.06890, 0.8266 0.1741, -0.07950, 0.7274 0.2102, -0.08660, 0.6295 0.2472, -0.09640, 0.5084 0.2844, -0.10270, 0.3886 0.3225, -0.10690, 0.2783 0.3608, -0.10890, 0.1689 0.3991, -0.10830, 0.0761 0.4373, -0.10510, 0.0436 0.4757, -0.09890, 0.0345 0.5137, -0.09067, 0.0906 0.5611, -0.07859, 0.1441 16 Flap element taps 1.0000, 0.00130, -1.0627 0.9365, 0.01390, -1.0800 0.8333, 0.03280, -1.0933 0.7436, 0.04930, -1.0991 0.7049, 0.05667, -1.1003 0.6662, 0.06411, -1.1002 0.6274, 0.07172, -1.0990 0.6009, 0.07523, -1.1191 0.6069, 0.02889, -1.1890 0.6079, -0.01747, -0.6188 0.6167, -0.06381, -0.4864 0.6558, -0.05300, 0.0095 0.7045, -0.04117, 0.8511 0.7429, -0.03210, 0.9944 0.8333, -0.01400, 0.6825 0.9311, -0.00120, 0.3046