S809 SPOILER FLAP, LEGR, CHORD = 18 INCHES --------- Run Conditions: vel=103.1 ft/s Re=1.007x10^6 AOA=-6.01 Flap deflection=45.00 Totals: Cl=-0.4112 Cdp=0.3329 Cm(c/4)=-0.0755 Cs=-0.2880 Ch=0.0194 Main component: Cl=-0.5793 Cdp=0.0356 Cm=0.1381 Flap component: Cl=0.1681 Cdp=0.2973 Cm=-0.1026 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1974 0.5905, -0.01667, -0.1886 0.5709, 0.03110, -0.1783 0.5889, 0.07933, -0.1966 0.5500, 0.08689, 0.4595 0.5110, 0.09367, 0.3571 0.4731, 0.09830, 0.2606 0.4349, 0.10070, 0.1840 0.3960, 0.10120, 0.1332 0.3566, 0.10020, 0.1239 0.3172, 0.09790, 0.1278 0.2778, 0.09440, 0.1257 0.2393, 0.08960, 0.1536 0.2056, 0.08360, 0.1868 0.1633, 0.07610, 0.2568 0.1261, 0.06710, 0.3642 0.0900, 0.05640, 0.4694 0.0571, 0.04390, 0.6653 0.0283, 0.02940, 0.8792 0.0142, 0.01970, 0.9977 0.0081, 0.01410, 0.9672 0.0026, 0.00780, 0.5702 0.0000, 0.00000, -0.9284 0.0037, -0.00840, -1.7511 0.0112, -0.01420, -1.4099 0.0191, -0.01930, -1.1240 0.0397, -0.03030, -0.8256 0.0706, -0.04420, -0.8317 0.1037, -0.05710, -0.7938 0.1384, -0.06890, -0.8441 0.1741, -0.07950, -0.8709 0.2102, -0.08660, -0.8968 0.2472, -0.09640, -0.9384 0.2844, -0.10270, -0.9290 0.3225, -0.10690, -0.8708 0.3608, -0.10890, -0.7965 0.3991, -0.10830, -0.6370 0.4373, -0.10510, -0.3958 0.4757, -0.09890, -0.2259 0.5137, -0.09067, -0.1818 0.5611, -0.07859, -0.1916 16 Flap element taps 1.0000, 0.00130, -1.0445 0.9365, 0.01390, -1.0274 0.8333, 0.03280, -1.0287 0.7436, 0.04930, -1.0141 0.7049, 0.05667, -1.0027 0.6662, 0.06411, -1.0028 0.6274, 0.07172, -0.9946 0.6009, 0.07523, -1.0098 0.6069, 0.02889, 0.5431 0.6079, -0.01747, 0.8489 0.6167, -0.06381, -0.1867 0.6558, -0.05300, -0.2103 0.7045, -0.04117, -0.2142 0.7429, -0.03210, -0.2333 0.8333, -0.01400, -0.2010 0.9311, -0.00120, 0.0122 --------- Run Conditions: vel=102.7 ft/s Re=1.002x10^6 AOA=0.00 Flap deflection=45.00 Totals: Cl=0.0332 Cdp=0.3611 Cm(c/4)=-0.0964 Cs=-0.3611 Ch=0.0280 Main component: Cl=-0.1803 Cdp=-0.0107 Cm=0.0579 Flap component: Cl=0.2135 Cdp=0.3718 Cm=-0.1627 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0756 0.5905, -0.01667, 0.0783 0.5709, 0.03110, 0.0885 0.5889, 0.07933, 0.0953 0.5500, 0.08689, 0.3657 0.5110, 0.09367, 0.2810 0.4731, 0.09830, 0.1651 0.4349, 0.10070, 0.0534 0.3960, 0.10120, -0.0341 0.3566, 0.10020, -0.0785 0.3172, 0.09790, -0.1067 0.2778, 0.09440, -0.1445 0.2393, 0.08960, -0.1557 0.2056, 0.08360, -0.1647 0.1633, 0.07610, -0.1356 0.1261, 0.06710, -0.0734 0.0900, 0.05640, -0.0388 0.0571, 0.04390, 0.1200 0.0283, 0.02940, 0.3125 0.0142, 0.01970, 0.5439 0.0081, 0.01410, 0.7066 0.0026, 0.00780, 0.8519 0.0000, 0.00000, 0.9479 0.0037, -0.00840, 0.4019 0.0112, -0.01420, 0.1942 0.0191, -0.01930, 0.1430 0.0397, -0.03030, 0.0994 0.0706, -0.04420, -0.0889 0.1037, -0.05710, -0.1690 0.1384, -0.06890, -0.2881 0.1741, -0.07950, -0.3772 0.2102, -0.08660, -0.4517 0.2472, -0.09640, -0.5403 0.2844, -0.10270, -0.5831 0.3225, -0.10690, -0.5817 0.3608, -0.10890, -0.5759 0.3991, -0.10830, -0.5005 0.4373, -0.10510, -0.3406 0.4757, -0.09890, -0.1288 0.5137, -0.09067, 0.0471 0.5611, -0.07859, 0.0769 16 Flap element taps 1.0000, 0.00130, -1.0358 0.9365, 0.01390, -1.0356 0.8333, 0.03280, -1.0505 0.7436, 0.04930, -1.0362 0.7049, 0.05667, -1.0275 0.6662, 0.06411, -1.0286 0.6274, 0.07172, -1.0216 0.6009, 0.07523, -1.0435 0.6069, 0.02889, 0.4989 0.6079, -0.01747, 0.8200 0.6167, -0.06381, 0.0560 0.6558, -0.05300, 0.0325 0.7045, -0.04117, 0.0203 0.7429, -0.03210, -0.0180 0.8333, -0.01400, 0.1260 0.9311, -0.00120, 0.2249 --------- Run Conditions: vel=102.2 ft/s Re=0.998x10^6 AOA=3.03 Flap deflection=45.00 Totals: Cl=0.2445 Cdp=0.3791 Cm(c/4)=-0.0985 Cs=-0.3657 Ch=0.0356 Main component: Cl=0.0291 Cdp=-0.0264 Cm=0.0150 Flap component: Cl=0.2154 Cdp=0.4055 Cm=-0.1796 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.1976 0.5905, -0.01667, 0.1474 0.5709, 0.03110, 0.1554 0.5889, 0.07933, 0.1872 0.5500, 0.08689, 0.2913 0.5110, 0.09367, 0.2365 0.4731, 0.09830, 0.1251 0.4349, 0.10070, -0.0012 0.3960, 0.10120, -0.1033 0.3566, 0.10020, -0.1815 0.3172, 0.09790, -0.2318 0.2778, 0.09440, -0.2904 0.2393, 0.08960, -0.3251 0.2056, 0.08360, -0.3519 0.1633, 0.07610, -0.3652 0.1261, 0.06710, -0.3295 0.0900, 0.05640, -0.3529 0.0571, 0.04390, -0.2509 0.0283, 0.02940, -0.1423 0.0142, 0.01970, 0.0198 0.0081, 0.01410, 0.2232 0.0026, 0.00780, 0.3389 0.0000, 0.00000, 0.9011 0.0037, -0.00840, 0.8861 0.0112, -0.01420, 0.6836 0.0191, -0.01930, 0.5743 0.0397, -0.03030, 0.4303 0.0706, -0.04420, 0.2151 0.1037, -0.05710, 0.1027 0.1384, -0.06890, -0.0461 0.1741, -0.07950, -0.1564 0.2102, -0.08660, -0.2335 0.2472, -0.09640, -0.3388 0.2844, -0.10270, -0.3968 0.3225, -0.10690, -0.4239 0.3608, -0.10890, -0.4358 0.3991, -0.10830, -0.3917 0.4373, -0.10510, -0.2588 0.4757, -0.09890, -0.0727 0.5137, -0.09067, 0.1340 0.5611, -0.07859, 0.1915 16 Flap element taps 1.0000, 0.00130, -1.0817 0.9365, 0.01390, -1.0816 0.8333, 0.03280, -1.0857 0.7436, 0.04930, -1.0787 0.7049, 0.05667, -1.0663 0.6662, 0.06411, -1.0659 0.6274, 0.07172, -1.0573 0.6009, 0.07523, -1.0800 0.6069, 0.02889, 0.4798 0.6079, -0.01747, 0.8187 0.6167, -0.06381, 0.1268 0.6558, -0.05300, 0.1020 0.7045, -0.04117, 0.0751 0.7429, -0.03210, 0.0562 0.8333, -0.01400, 0.1984 0.9311, -0.00120, 0.2095 --------- Run Conditions: vel=102.5 ft/s Re=1.000x10^6 AOA=6.01 Flap deflection=45.00 Totals: Cl=0.3680 Cdp=0.3885 Cm(c/4)=-0.1325 Cs=-0.3479 Ch=0.0194 Main component: Cl=0.0857 Cdp=-0.0374 Cm=0.0191 Flap component: Cl=0.2823 Cdp=0.4259 Cm=-0.2533 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.2404 0.5905, -0.01667, 0.2262 0.5709, 0.03110, 0.2473 0.5889, 0.07933, 0.2034 0.5500, 0.08689, 0.2404 0.5110, 0.09367, 0.2312 0.4731, 0.09830, 0.2292 0.4349, 0.10070, 0.1868 0.3960, 0.10120, 0.0704 0.3566, 0.10020, -0.0742 0.3172, 0.09790, -0.1779 0.2778, 0.09440, -0.2838 0.2393, 0.08960, -0.3562 0.2056, 0.08360, -0.4138 0.1633, 0.07610, -0.4713 0.1261, 0.06710, -0.4764 0.0900, 0.05640, -0.5583 0.0571, 0.04390, -0.5217 0.0283, 0.02940, -0.5149 0.0142, 0.01970, -0.4594 0.0081, 0.01410, -0.2316 0.0026, 0.00780, -0.1241 0.0000, 0.00000, 0.4733 0.0037, -0.00840, 0.9870 0.0112, -0.01420, 0.8968 0.0191, -0.01930, 0.7940 0.0397, -0.03030, 0.6292 0.0706, -0.04420, 0.4018 0.1037, -0.05710, 0.2676 0.1384, -0.06890, 0.1014 0.1741, -0.07950, -0.0270 0.2102, -0.08660, -0.1203 0.2472, -0.09640, -0.2497 0.2844, -0.10270, -0.3252 0.3225, -0.10690, -0.3770 0.3608, -0.10890, -0.4170 0.3991, -0.10830, -0.4123 0.4373, -0.10510, -0.3247 0.4757, -0.09890, -0.1888 0.5137, -0.09067, 0.0191 0.5611, -0.07859, 0.1848 16 Flap element taps 1.0000, 0.00130, -1.0203 0.9365, 0.01390, -1.0342 0.8333, 0.03280, -1.0385 0.7436, 0.04930, -1.0371 0.7049, 0.05667, -1.0282 0.6662, 0.06411, -1.0241 0.6274, 0.07172, -1.0212 0.6009, 0.07523, -1.0704 0.6069, 0.02889, 0.1153 0.6079, -0.01747, 0.1661 0.6167, -0.06381, 0.1652 0.6558, -0.05300, 0.2184 0.7045, -0.04117, 0.2361 0.7429, -0.03210, 0.2368 0.8333, -0.01400, 0.5078 0.9311, -0.00120, 0.5590 --------- Run Conditions: vel=102.5 ft/s Re=1.000x10^6 AOA=9.05 Flap deflection=45.00 Totals: Cl=0.5967 Cdp=0.4182 Cm(c/4)=-0.1688 Cs=-0.3191 Ch=0.0112 Main component: Cl=0.2521 Cdp=-0.0175 Cm=-0.0110 Flap component: Cl=0.3446 Cdp=0.4357 Cm=-0.3216 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.1341 0.5905, -0.01667, 0.0932 0.5709, 0.03110, 0.1448 0.5889, 0.07933, 0.0785 0.5500, 0.08689, 0.1180 0.5110, 0.09367, 0.0928 0.4731, 0.09830, 0.1029 0.4349, 0.10070, 0.0928 0.3960, 0.10120, 0.0529 0.3566, 0.10020, -0.0706 0.3172, 0.09790, -0.2089 0.2778, 0.09440, -0.3559 0.2393, 0.08960, -0.4666 0.2056, 0.08360, -0.5649 0.1633, 0.07610, -0.6707 0.1261, 0.06710, -0.7260 0.0900, 0.05640, -0.8806 0.0571, 0.04390, -0.9449 0.0283, 0.02940, -1.1072 0.0142, 0.01970, -1.2485 0.0081, 0.01410, -1.0840 0.0026, 0.00780, -1.0747 0.0000, 0.00000, -0.6896 0.0037, -0.00840, 0.8457 0.0112, -0.01420, 0.9960 0.0191, -0.01930, 0.9625 0.0397, -0.03030, 0.8280 0.0706, -0.04420, 0.6204 0.1037, -0.05710, 0.4778 0.1384, -0.06890, 0.3028 0.1741, -0.07950, 0.1697 0.2102, -0.08660, 0.0634 0.2472, -0.09640, -0.0758 0.2844, -0.10270, -0.1704 0.3225, -0.10690, -0.2505 0.3608, -0.10890, -0.3135 0.3991, -0.10830, -0.3428 0.4373, -0.10510, -0.2929 0.4757, -0.09890, -0.2107 0.5137, -0.09067, -0.0385 0.5611, -0.07859, 0.0909 16 Flap element taps 1.0000, 0.00130, -1.0070 0.9365, 0.01390, -1.0259 0.8333, 0.03280, -1.0408 0.7436, 0.04930, -1.0452 0.7049, 0.05667, -1.0321 0.6662, 0.06411, -1.0257 0.6274, 0.07172, -1.0180 0.6009, 0.07523, -1.0827 0.6069, 0.02889, -0.1693 0.6079, -0.01747, -0.6724 0.6167, -0.06381, -0.2640 0.6558, -0.05300, 0.0934 0.7045, -0.04117, 0.3034 0.7429, -0.03210, 0.7373 0.8333, -0.01400, 0.9000 0.9311, -0.00120, 0.4977 --------- Run Conditions: vel=102.8 ft/s Re=1.002x10^6 AOA=12.03 Flap deflection=45.00 Totals: Cl=0.8264 Cdp=0.4246 Cm(c/4)=-0.1827 Cs=-0.2430 Ch=0.0059 Main component: Cl=0.4719 Cdp=0.0023 Cm=-0.0634 Flap component: Cl=0.3545 Cdp=0.4223 Cm=-0.3435 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0828 0.5905, -0.01667, 0.0331 0.5709, 0.03110, 0.0841 0.5889, 0.07933, -0.1211 0.5500, 0.08689, -0.0902 0.5110, 0.09367, -0.1166 0.4731, 0.09830, -0.1172 0.4349, 0.10070, -0.1176 0.3960, 0.10120, -0.1225 0.3566, 0.10020, -0.1833 0.3172, 0.09790, -0.2797 0.2778, 0.09440, -0.4355 0.2393, 0.08960, -0.5811 0.2056, 0.08360, -0.7202 0.1633, 0.07610, -0.8861 0.1261, 0.06710, -0.9995 0.0900, 0.05640, -1.2402 0.0571, 0.04390, -1.4283 0.0283, 0.02940, -1.8046 0.0142, 0.01970, -2.1989 0.0081, 0.01410, -2.2081 0.0026, 0.00780, -2.3333 0.0000, 0.00000, -2.5651 0.0037, -0.00840, 0.3392 0.0112, -0.01420, 0.9110 0.0191, -0.01930, 0.9926 0.0397, -0.03030, 0.9530 0.0706, -0.04420, 0.7920 0.1037, -0.05710, 0.6589 0.1384, -0.06890, 0.4838 0.1741, -0.07950, 0.3500 0.2102, -0.08660, 0.2525 0.2472, -0.09640, 0.1067 0.2844, -0.10270, 0.0062 0.3225, -0.10690, -0.0920 0.3608, -0.10890, -0.1649 0.3991, -0.10830, -0.2147 0.4373, -0.10510, -0.1744 0.4757, -0.09890, -0.1178 0.5137, -0.09067, -0.0757 0.5611, -0.07859, 0.1813 16 Flap element taps 1.0000, 0.00130, -0.9635 0.9365, 0.01390, -0.9856 0.8333, 0.03280, -1.0030 0.7436, 0.04930, -1.0040 0.7049, 0.05667, -0.9932 0.6662, 0.06411, -0.9835 0.6274, 0.07172, -0.9800 0.6009, 0.07523, -1.0435 0.6069, 0.02889, -0.5488 0.6079, -0.01747, -1.0568 0.6167, -0.06381, -0.4832 0.6558, -0.05300, 0.0508 0.7045, -0.04117, 0.4457 0.7429, -0.03210, 0.8794 0.8333, -0.01400, 0.8960 0.9311, -0.00120, 0.5196 --------- Run Conditions: vel=103.4 ft/s Re=1.006x10^6 AOA=15.04 Flap deflection=45.00 Totals: Cl=1.0042 Cdp=0.4042 Cm(c/4)=-0.1940 Cs=-0.1297 Ch=-0.0091 Main component: Cl=0.6620 Cdp=0.0561 Cm=-0.1271 Flap component: Cl=0.3422 Cdp=0.3480 Cm=-0.3356 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0635 0.5905, -0.01667, 0.0089 0.5709, 0.03110, 0.0436 0.5889, 0.07933, -0.4473 0.5500, 0.08689, -0.4079 0.5110, 0.09367, -0.4319 0.4731, 0.09830, -0.4889 0.4349, 0.10070, -0.4902 0.3960, 0.10120, -0.4936 0.3566, 0.10020, -0.5043 0.3172, 0.09790, -0.5302 0.2778, 0.09440, -0.5699 0.2393, 0.08960, -0.6012 0.2056, 0.08360, -0.6881 0.1633, 0.07610, -0.8238 0.1261, 0.06710, -0.9983 0.0900, 0.05640, -1.2860 0.0571, 0.04390, -1.6345 0.0283, 0.02940, -2.2114 0.0142, 0.01970, -2.8655 0.0081, 0.01410, -3.0572 0.0026, 0.00780, -3.3816 0.0000, 0.00000, -4.4004 0.0037, -0.00840, -0.2846 0.0112, -0.01420, 0.7040 0.0191, -0.01930, 0.9312 0.0397, -0.03030, 1.0017 0.0706, -0.04420, 0.9013 0.1037, -0.05710, 0.7808 0.1384, -0.06890, 0.6437 0.1741, -0.07950, 0.5217 0.2102, -0.08660, 0.3987 0.2472, -0.09640, 0.2729 0.2844, -0.10270, 0.1629 0.3225, -0.10690, 0.0714 0.3608, -0.10890, -0.0154 0.3991, -0.10830, -0.0713 0.4373, -0.10510, -0.0575 0.4757, -0.09890, -0.0069 0.5137, -0.09067, 0.0380 0.5611, -0.07859, 0.2079 16 Flap element taps 1.0000, 0.00130, -0.7308 0.9365, 0.01390, -0.7569 0.8333, 0.03280, -0.7710 0.7436, 0.04930, -0.7706 0.7049, 0.05667, -0.7593 0.6662, 0.06411, -0.7601 0.6274, 0.07172, -0.7628 0.6009, 0.07523, -0.8946 0.6069, 0.02889, -1.1249 0.6079, -0.01747, -1.2600 0.6167, -0.06381, -0.6369 0.6558, -0.05300, 0.0550 0.7045, -0.04117, 0.5650 0.7429, -0.03210, 0.9252 0.8333, -0.01400, 0.9060 0.9311, -0.00120, 0.5769 --------- Run Conditions: vel=102.7 ft/s Re=0.998x10^6 AOA=18.00 Flap deflection=45.00 Totals: Cl=0.9720 Cdp=0.5227 Cm(c/4)=-0.2111 Cs=-0.1968 Ch=-0.0022 Main component: Cl=0.6653 Cdp=0.1513 Cm=-0.1597 Flap component: Cl=0.3067 Cdp=0.3715 Cm=-0.3229 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0808 0.5905, -0.01667, 0.0138 0.5709, 0.03110, 0.0687 0.5889, 0.07933, -0.6942 0.5500, 0.08689, -0.6737 0.5110, 0.09367, -0.6837 0.4731, 0.09830, -0.6269 0.4349, 0.10070, -0.7022 0.3960, 0.10120, -0.7462 0.3566, 0.10020, -0.7640 0.3172, 0.09790, -0.7615 0.2778, 0.09440, -0.7623 0.2393, 0.08960, -0.7538 0.2056, 0.08360, -0.7784 0.1633, 0.07610, -0.8096 0.1261, 0.06710, -0.8228 0.0900, 0.05640, -0.8592 0.0571, 0.04390, -0.9781 0.0283, 0.02940, -1.3756 0.0142, 0.01970, -1.9547 0.0081, 0.01410, -2.2432 0.0026, 0.00780, -2.6629 0.0000, 0.00000, -3.7863 0.0037, -0.00840, -0.2190 0.0112, -0.01420, 0.6960 0.0191, -0.01930, 0.9213 0.0397, -0.03030, 1.0032 0.0706, -0.04420, 0.9195 0.1037, -0.05710, 0.8126 0.1384, -0.06890, 0.6834 0.1741, -0.07950, 0.5670 0.2102, -0.08660, 0.4496 0.2472, -0.09640, 0.3264 0.2844, -0.10270, 0.2178 0.3225, -0.10690, 0.1248 0.3608, -0.10890, 0.0369 0.3991, -0.10830, -0.0224 0.4373, -0.10510, -0.0147 0.4757, -0.09890, 0.0306 0.5137, -0.09067, 0.0759 0.5611, -0.07859, 0.1824 16 Flap element taps 1.0000, 0.00130, -0.6953 0.9365, 0.01390, -0.7125 0.8333, 0.03280, -0.7275 0.7436, 0.04930, -0.7419 0.7049, 0.05667, -0.7407 0.6662, 0.06411, -0.7523 0.6274, 0.07172, -0.7724 0.6009, 0.07523, -0.9996 0.6069, 0.02889, -0.9701 0.6079, -0.01747, -0.9544 0.6167, -0.06381, -0.5405 0.6558, -0.05300, 0.0749 0.7045, -0.04117, 0.5813 0.7429, -0.03210, 0.9284 0.8333, -0.01400, 0.9065 0.9311, -0.00120, 0.5875 --------- Run Conditions: vel=103.4 ft/s Re=1.007x10^6 AOA=19.98 Flap deflection=45.00 Totals: Cl=0.9881 Cdp=0.6095 Cm(c/4)=-0.2260 Cs=-0.2352 Ch=0.0000 Main component: Cl=0.6866 Cdp=0.2148 Cm=-0.1783 Flap component: Cl=0.3015 Cdp=0.3947 Cm=-0.3319 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0822 0.5905, -0.01667, 0.0106 0.5709, 0.03110, 0.0637 0.5889, 0.07933, -0.7983 0.5500, 0.08689, -0.7457 0.5110, 0.09367, -0.7717 0.4731, 0.09830, -0.7745 0.4349, 0.10070, -0.7596 0.3960, 0.10120, -0.7711 0.3566, 0.10020, -0.8360 0.3172, 0.09790, -0.8690 0.2778, 0.09440, -0.8936 0.2393, 0.08960, -0.8855 0.2056, 0.08360, -0.8918 0.1633, 0.07610, -0.9092 0.1261, 0.06710, -0.8973 0.0900, 0.05640, -0.9125 0.0571, 0.04390, -0.9377 0.0283, 0.02940, -1.0154 0.0142, 0.01970, -1.2372 0.0081, 0.01410, -1.4963 0.0026, 0.00780, -1.8897 0.0000, 0.00000, -3.0746 0.0037, -0.00840, -0.1148 0.0112, -0.01420, 0.7096 0.0191, -0.01930, 0.9214 0.0397, -0.03030, 1.0073 0.0706, -0.04420, 0.9366 0.1037, -0.05710, 0.8388 0.1384, -0.06890, 0.7137 0.1741, -0.07950, 0.6035 0.2102, -0.08660, 0.4938 0.2472, -0.09640, 0.3706 0.2844, -0.10270, 0.2628 0.3225, -0.10690, 0.1649 0.3608, -0.10890, 0.0770 0.3991, -0.10830, 0.0128 0.4373, -0.10510, 0.0168 0.4757, -0.09890, 0.0541 0.5137, -0.09067, 0.1017 0.5611, -0.07859, 0.1685 16 Flap element taps 1.0000, 0.00130, -0.7306 0.9365, 0.01390, -0.7456 0.8333, 0.03280, -0.7609 0.7436, 0.04930, -0.7768 0.7049, 0.05667, -0.7785 0.6662, 0.06411, -0.7926 0.6274, 0.07172, -0.8184 0.6009, 0.07523, -1.0496 0.6069, 0.02889, -1.0121 0.6079, -0.01747, -0.9650 0.6167, -0.06381, -0.5588 0.6558, -0.05300, 0.0770 0.7045, -0.04117, 0.6024 0.7429, -0.03210, 0.9385 0.8333, -0.01400, 0.9122 0.9311, -0.00120, 0.5898 --------- Run Conditions: vel=102.1 ft/s Re=0.993x10^6 AOA=24.00 Flap deflection=45.00 Totals: Cl=0.9513 Cdp=0.7396 Cm(c/4)=-0.2450 Cs=-0.2888 Ch=0.0027 Main component: Cl=0.6719 Cdp=0.2982 Cm=-0.1930 Flap component: Cl=0.2794 Cdp=0.4414 Cm=-0.3445 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0758 0.5905, -0.01667, -0.0083 0.5709, 0.03110, 0.0334 0.5889, 0.07933, -0.9000 0.5500, 0.08689, -0.8518 0.5110, 0.09367, -0.8792 0.4731, 0.09830, -0.9208 0.4349, 0.10070, -0.9178 0.3960, 0.10120, -0.8498 0.3566, 0.10020, -0.8074 0.3172, 0.09790, -0.8081 0.2778, 0.09440, -0.8419 0.2393, 0.08960, -0.8416 0.2056, 0.08360, -0.8386 0.1633, 0.07610, -0.8559 0.1261, 0.06710, -0.8327 0.0900, 0.05640, -0.8346 0.0571, 0.04390, -0.8292 0.0283, 0.02940, -0.8569 0.0142, 0.01970, -0.8682 0.0081, 0.01410, -0.9358 0.0026, 0.00780, -1.1951 0.0000, 0.00000, -2.4894 0.0037, -0.00840, -0.1022 0.0112, -0.01420, 0.6738 0.0191, -0.01930, 0.8925 0.0397, -0.03030, 1.0041 0.0706, -0.04420, 0.9579 0.1037, -0.05710, 0.8793 0.1384, -0.06890, 0.7625 0.1741, -0.07950, 0.6594 0.2102, -0.08660, 0.5604 0.2472, -0.09640, 0.4397 0.2844, -0.10270, 0.3335 0.3225, -0.10690, 0.2310 0.3608, -0.10890, 0.1394 0.3991, -0.10830, 0.0647 0.4373, -0.10510, 0.0618 0.4757, -0.09890, 0.0865 0.5137, -0.09067, 0.1353 0.5611, -0.07859, 0.1794 16 Flap element taps 1.0000, 0.00130, -0.8096 0.9365, 0.01390, -0.8271 0.8333, 0.03280, -0.8399 0.7436, 0.04930, -0.8617 0.7049, 0.05667, -0.8648 0.6662, 0.06411, -0.8783 0.6274, 0.07172, -0.9021 0.6009, 0.07523, -1.0284 0.6069, 0.02889, -1.0412 0.6079, -0.01747, -0.9847 0.6167, -0.06381, -0.5947 0.6558, -0.05300, 0.0725 0.7045, -0.04117, 0.6143 0.7429, -0.03210, 0.9402 0.8333, -0.01400, 0.9085 0.9311, -0.00120, 0.5810 --------- Run Conditions: vel=103.1 ft/s Re=1.002x10^6 AOA=27.01 Flap deflection=45.00 Totals: Cl=1.0692 Cdp=0.9346 Cm(c/4)=-0.2884 Cs=-0.3471 Ch=0.0070 Main component: Cl=0.7782 Cdp=0.3971 Cm=-0.2345 Flap component: Cl=0.2911 Cdp=0.5374 Cm=-0.3981 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0246 0.5905, -0.01667, -0.0796 0.5709, 0.03110, -0.0344 0.5889, 0.07933, -1.0977 0.5500, 0.08689, -1.0452 0.5110, 0.09367, -1.0784 0.4731, 0.09830, -1.1123 0.4349, 0.10070, -1.1273 0.3960, 0.10120, -1.0579 0.3566, 0.10020, -1.0253 0.3172, 0.09790, -1.0142 0.2778, 0.09440, -1.0426 0.2393, 0.08960, -1.0509 0.2056, 0.08360, -1.0470 0.1633, 0.07610, -1.0643 0.1261, 0.06710, -1.0406 0.0900, 0.05640, -1.0390 0.0571, 0.04390, -1.0338 0.0283, 0.02940, -1.0429 0.0142, 0.01970, -1.0718 0.0081, 0.01410, -1.2436 0.0026, 0.00780, -1.1692 0.0000, 0.00000, -2.2109 0.0037, -0.00840, -0.2869 0.0112, -0.01420, 0.5524 0.0191, -0.01930, 0.8242 0.0397, -0.03030, 0.9927 0.0706, -0.04420, 0.9842 0.1037, -0.05710, 0.9248 0.1384, -0.06890, 0.8200 0.1741, -0.07950, 0.7234 0.2102, -0.08660, 0.6281 0.2472, -0.09640, 0.5077 0.2844, -0.10270, 0.4004 0.3225, -0.10690, 0.2941 0.3608, -0.10890, 0.1925 0.3991, -0.10830, 0.1085 0.4373, -0.10510, 0.0926 0.4757, -0.09890, 0.0996 0.5137, -0.09067, 0.1472 0.5611, -0.07859, 0.1953 16 Flap element taps 1.0000, 0.00130, -1.0815 0.9365, 0.01390, -1.1018 0.8333, 0.03280, -1.1162 0.7436, 0.04930, -1.1355 0.7049, 0.05667, -1.1371 0.6662, 0.06411, -1.1454 0.6274, 0.07172, -1.1645 0.6009, 0.07523, -1.2568 0.6069, 0.02889, -1.2566 0.6079, -0.01747, -1.2199 0.6167, -0.06381, -0.7628 0.6558, -0.05300, 0.0280 0.7045, -0.04117, 0.6225 0.7429, -0.03210, 0.9456 0.8333, -0.01400, 0.9076 0.9311, -0.00120, 0.5556