S809 SPOILER FLAP, LEGR, CHORD = 18 INCHES --------- Run Conditions: vel=98.9 ft/s Re=0.995x10^6 AOA=-6.01 Flap deflection=90.00 Totals: Cl=0.2015 Cdp=0.6455 Cm(c/4)=-0.0642 Cs=-0.6631 Ch=0.0934 Main component: Cl=0.0081 Cdp=-0.0386 Cm=-0.0228 Flap component: Cl=0.1933 Cdp=0.6841 Cm=-0.0746 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.2626 0.5905, -0.01667, 0.2652 0.5709, 0.03110, 0.2780 0.5889, 0.07933, 0.2710 0.5500, 0.08689, 0.2057 0.5110, 0.09367, 0.0419 0.4731, 0.09830, -0.0807 0.4349, 0.10070, -0.1639 0.3960, 0.10120, -0.2142 0.3566, 0.10020, -0.2280 0.3172, 0.09790, -0.2195 0.2778, 0.09440, -0.2246 0.2393, 0.08960, -0.2078 0.2056, 0.08360, -0.1769 0.1633, 0.07610, -0.1271 0.1261, 0.06710, -0.0269 0.0900, 0.05640, 0.0459 0.0571, 0.04390, 0.2315 0.0283, 0.02940, 0.4751 0.0142, 0.01970, 0.7046 0.0081, 0.01410, 0.8449 0.0026, 0.00780, 0.9362 0.0000, 0.00000, 0.7861 0.0037, -0.00840, 0.1163 0.0112, -0.01420, -0.0134 0.0191, -0.01930, -0.0137 0.0397, -0.03030, 0.0153 0.0706, -0.04420, -0.1037 0.1037, -0.05710, -0.1231 0.1384, -0.06890, -0.2028 0.1741, -0.07950, -0.2288 0.2102, -0.08660, -0.2448 0.2472, -0.09640, -0.2561 0.2844, -0.10270, -0.2200 0.3225, -0.10690, -0.1344 0.3608, -0.10890, -0.0137 0.3991, -0.10830, 0.1558 0.4373, -0.10510, 0.2617 0.4757, -0.09890, 0.2645 0.5137, -0.09067, 0.2735 0.5611, -0.07859, 0.2649 16 Flap element taps 1.0000, 0.00130, -1.3286 0.9365, 0.01390, -1.4676 0.8333, 0.03280, -1.4372 0.7436, 0.04930, -1.4443 0.7049, 0.05667, -1.4385 0.6662, 0.06411, -1.4502 0.6274, 0.07172, -1.4010 0.6009, 0.07523, -1.5862 0.6069, 0.02889, -1.7187 0.6079, -0.01747, -1.6819 0.6167, -0.06381, 0.1730 0.6558, -0.05300, 0.9967 0.7045, -0.04117, 0.8614 0.7429, -0.03210, 0.6383 0.8333, -0.01400, 0.3582 0.9311, -0.00120, 0.3679 --------- Run Conditions: vel=100.5 ft/s Re=1.011x10^6 AOA=-0.01 Flap deflection=90.00 Totals: Cl=0.2232 Cdp=0.5306 Cm(c/4)=-0.0452 Cs=-0.5307 Ch=0.0582 Main component: Cl=0.1046 Cdp=-0.0427 Cm=-0.0211 Flap component: Cl=0.1186 Cdp=0.5733 Cm=-0.0798 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.2815 0.5905, -0.01667, 0.2664 0.5709, 0.03110, 0.2857 0.5889, 0.07933, 0.2571 0.5500, 0.08689, 0.2671 0.5110, 0.09367, 0.2410 0.4731, 0.09830, 0.1372 0.4349, 0.10070, -0.0203 0.3960, 0.10120, -0.1454 0.3566, 0.10020, -0.2177 0.3172, 0.09790, -0.2589 0.2778, 0.09440, -0.3059 0.2393, 0.08960, -0.3317 0.2056, 0.08360, -0.3449 0.1633, 0.07610, -0.3341 0.1261, 0.06710, -0.2826 0.0900, 0.05640, -0.2759 0.0571, 0.04390, -0.1555 0.0283, 0.02940, 0.0081 0.0142, 0.01970, 0.1949 0.0081, 0.01410, 0.3870 0.0026, 0.00780, 0.5477 0.0000, 0.00000, 0.9727 0.0037, -0.00840, 0.7907 0.0112, -0.01420, 0.5818 0.0191, -0.01930, 0.4848 0.0397, -0.03030, 0.3678 0.0706, -0.04420, 0.1829 0.1037, -0.05710, 0.1000 0.1384, -0.06890, -0.0224 0.1741, -0.07950, -0.0955 0.2102, -0.08660, -0.1541 0.2472, -0.09640, -0.2122 0.2844, -0.10270, -0.2268 0.3225, -0.10690, -0.1977 0.3608, -0.10890, -0.1427 0.3991, -0.10830, -0.0179 0.4373, -0.10510, 0.1830 0.4757, -0.09890, 0.2836 0.5137, -0.09067, 0.3016 0.5611, -0.07859, 0.2920 16 Flap element taps 1.0000, 0.00130, -1.1473 0.9365, 0.01390, -1.2443 0.8333, 0.03280, -1.2702 0.7436, 0.04930, -1.2503 0.7049, 0.05667, -1.2435 0.6662, 0.06411, -1.2611 0.6274, 0.07172, -1.2430 0.6009, 0.07523, -1.4706 0.6069, 0.02889, -1.6547 0.6079, -0.01747, -1.7766 0.6167, -0.06381, 0.2336 0.6558, -0.05300, 0.7197 0.7045, -0.04117, 0.3569 0.7429, -0.03210, 0.2991 0.8333, -0.01400, 0.2856 0.9311, -0.00120, 0.3944 --------- Run Conditions: vel=100.0 ft/s Re=1.003x10^6 AOA=3.02 Flap deflection=90.00 Totals: Cl=0.1622 Cdp=0.5481 Cm(c/4)=-0.0514 Cs=-0.5388 Ch=0.0049 Main component: Cl=0.0521 Cdp=-0.0415 Cm=0.0071 Flap component: Cl=0.1101 Cdp=0.5896 Cm=-0.1062 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.2761 0.5905, -0.01667, 0.2739 0.5709, 0.03110, 0.2928 0.5889, 0.07933, 0.2759 0.5500, 0.08689, 0.2894 0.5110, 0.09367, 0.2954 0.4731, 0.09830, 0.2828 0.4349, 0.10070, 0.1971 0.3960, 0.10120, 0.0437 0.3566, 0.10020, -0.0657 0.3172, 0.09790, -0.1401 0.2778, 0.09440, -0.2152 0.2393, 0.08960, -0.2663 0.2056, 0.08360, -0.3067 0.1633, 0.07610, -0.3217 0.1261, 0.06710, -0.2993 0.0900, 0.05640, -0.3220 0.0571, 0.04390, -0.2415 0.0283, 0.02940, -0.1254 0.0142, 0.01970, 0.0193 0.0081, 0.01410, 0.2040 0.0026, 0.00780, 0.3237 0.0000, 0.00000, 0.8915 0.0037, -0.00840, 0.8957 0.0112, -0.01420, 0.7055 0.0191, -0.01930, 0.5978 0.0397, -0.03030, 0.4578 0.0706, -0.04420, 0.2512 0.1037, -0.05710, 0.1484 0.1384, -0.06890, 0.0102 0.1741, -0.07950, -0.0840 0.2102, -0.08660, -0.1640 0.2472, -0.09640, -0.2445 0.2844, -0.10270, -0.2868 0.3225, -0.10690, -0.2877 0.3608, -0.10890, -0.2713 0.3991, -0.10830, -0.1925 0.4373, -0.10510, -0.0274 0.4757, -0.09890, 0.1646 0.5137, -0.09067, 0.2651 0.5611, -0.07859, 0.2751 16 Flap element taps 1.0000, 0.00130, -1.1411 0.9365, 0.01390, -1.2152 0.8333, 0.03280, -1.2780 0.7436, 0.04930, -1.2697 0.7049, 0.05667, -1.2838 0.6662, 0.06411, -1.3165 0.6274, 0.07172, -1.3301 0.6009, 0.07523, -1.5557 0.6069, 0.02889, -1.6872 0.6079, -0.01747, -1.9436 0.6167, -0.06381, -0.5287 0.6558, -0.05300, 0.3339 0.7045, -0.04117, 0.3402 0.7429, -0.03210, 0.2901 0.8333, -0.01400, 0.2796 0.9311, -0.00120, 0.8826 --------- Run Conditions: vel=100.6 ft/s Re=1.007x10^6 AOA=6.01 Flap deflection=90.00 Totals: Cl=0.1509 Cdp=0.6256 Cm(c/4)=-0.0537 Cs=-0.6063 Ch=-0.0013 Main component: Cl=0.0509 Cdp=-0.0442 Cm=0.0217 Flap component: Cl=0.1000 Cdp=0.6697 Cm=-0.1293 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.3242 0.5905, -0.01667, 0.3138 0.5709, 0.03110, 0.3207 0.5889, 0.07933, 0.3040 0.5500, 0.08689, 0.3093 0.5110, 0.09367, 0.3060 0.4731, 0.09830, 0.3081 0.4349, 0.10070, 0.2922 0.3960, 0.10120, 0.1880 0.3566, 0.10020, 0.0616 0.3172, 0.09790, -0.0471 0.2778, 0.09440, -0.1497 0.2393, 0.08960, -0.2244 0.2056, 0.08360, -0.2924 0.1633, 0.07610, -0.3350 0.1261, 0.06710, -0.3444 0.0900, 0.05640, -0.4038 0.0571, 0.04390, -0.3744 0.0283, 0.02940, -0.3264 0.0142, 0.01970, -0.2535 0.0081, 0.01410, -0.0683 0.0026, 0.00780, 0.0432 0.0000, 0.00000, 0.6599 0.0037, -0.00840, 0.9792 0.0112, -0.01420, 0.8517 0.0191, -0.01930, 0.7457 0.0397, -0.03030, 0.5909 0.0706, -0.04420, 0.3734 0.1037, -0.05710, 0.2534 0.1384, -0.06890, 0.1028 0.1741, -0.07950, -0.0062 0.2102, -0.08660, -0.1031 0.2472, -0.09640, -0.2067 0.2844, -0.10270, -0.2661 0.3225, -0.10690, -0.2931 0.3608, -0.10890, -0.3110 0.3991, -0.10830, -0.2786 0.4373, -0.10510, -0.1757 0.4757, -0.09890, -0.0297 0.5137, -0.09067, 0.1588 0.5611, -0.07859, 0.2773 16 Flap element taps 1.0000, 0.00130, -1.1454 0.9365, 0.01390, -1.2305 0.8333, 0.03280, -1.3093 0.7436, 0.04930, -1.3269 0.7049, 0.05667, -1.3878 0.6662, 0.06411, -1.4572 0.6274, 0.07172, -1.5101 0.6009, 0.07523, -1.9902 0.6069, 0.02889, -1.9586 0.6079, -0.01747, -1.9272 0.6167, -0.06381, -0.7522 0.6558, -0.05300, 0.2466 0.7045, -0.04117, 0.3827 0.7429, -0.03210, 0.3849 0.8333, -0.01400, 0.6859 0.9311, -0.00120, 0.9870 --------- Run Conditions: vel=101.1 ft/s Re=1.010x10^6 AOA=9.04 Flap deflection=90.00 Totals: Cl=0.1943 Cdp=0.6372 Cm(c/4)=-0.0449 Cs=-0.5988 Ch=-0.0151 Main component: Cl=0.1311 Cdp=-0.0263 Cm=0.0113 Flap component: Cl=0.0632 Cdp=0.6636 Cm=-0.1293 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.2357 0.5905, -0.01667, 0.2228 0.5709, 0.03110, 0.2222 0.5889, 0.07933, 0.2127 0.5500, 0.08689, 0.2397 0.5110, 0.09367, 0.2376 0.4731, 0.09830, 0.2503 0.4349, 0.10070, 0.2501 0.3960, 0.10120, 0.2124 0.3566, 0.10020, 0.1250 0.3172, 0.09790, -0.0041 0.2778, 0.09440, -0.1369 0.2393, 0.08960, -0.2445 0.2056, 0.08360, -0.3454 0.1633, 0.07610, -0.4251 0.1261, 0.06710, -0.4734 0.0900, 0.05640, -0.5865 0.0571, 0.04390, -0.6267 0.0283, 0.02940, -0.6894 0.0142, 0.01970, -0.7322 0.0081, 0.01410, -0.4865 0.0026, 0.00780, -0.4892 0.0000, 0.00000, 0.0363 0.0037, -0.00840, 0.9587 0.0112, -0.01420, 0.9722 0.0191, -0.01930, 0.8960 0.0397, -0.03030, 0.7433 0.0706, -0.04420, 0.5312 0.1037, -0.05710, 0.3975 0.1384, -0.06890, 0.2399 0.1741, -0.07950, 0.1165 0.2102, -0.08660, 0.0024 0.2472, -0.09640, -0.1101 0.2844, -0.10270, -0.1925 0.3225, -0.10690, -0.2358 0.3608, -0.10890, -0.2724 0.3991, -0.10830, -0.2674 0.4373, -0.10510, -0.1931 0.4757, -0.09890, -0.0803 0.5137, -0.09067, 0.0910 0.5611, -0.07859, 0.2252 16 Flap element taps 1.0000, 0.00130, -1.1658 0.9365, 0.01390, -1.2247 0.8333, 0.03280, -1.2765 0.7436, 0.04930, -1.2832 0.7049, 0.05667, -1.2987 0.6662, 0.06411, -1.3661 0.6274, 0.07172, -1.4304 0.6009, 0.07523, -2.0335 0.6069, 0.02889, -1.8828 0.6079, -0.01747, -1.8121 0.6167, -0.06381, -0.8303 0.6558, -0.05300, 0.1583 0.7045, -0.04117, 0.3736 0.7429, -0.03210, 0.4188 0.8333, -0.01400, 0.7813 0.9311, -0.00120, 0.9820 --------- Run Conditions: vel=100.9 ft/s Re=1.007x10^6 AOA=12.03 Flap deflection=90.00 Totals: Cl=0.2716 Cdp=0.6403 Cm(c/4)=-0.0412 Cs=-0.5696 Ch=-0.0280 Main component: Cl=0.2408 Cdp=-0.0036 Cm=-0.0113 Flap component: Cl=0.0308 Cdp=0.6439 Cm=-0.1297 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.1284 0.5905, -0.01667, 0.1195 0.5709, 0.03110, 0.1193 0.5889, 0.07933, 0.1095 0.5500, 0.08689, 0.1306 0.5110, 0.09367, 0.1254 0.4731, 0.09830, 0.1314 0.4349, 0.10070, 0.1395 0.3960, 0.10120, 0.1282 0.3566, 0.10020, 0.0915 0.3172, 0.09790, 0.0157 0.2778, 0.09440, -0.1226 0.2393, 0.08960, -0.2606 0.2056, 0.08360, -0.3910 0.1633, 0.07610, -0.5204 0.1261, 0.06710, -0.6078 0.0900, 0.05640, -0.7801 0.0571, 0.04390, -0.9032 0.0283, 0.02940, -1.0980 0.0142, 0.01970, -1.3036 0.0081, 0.01410, -1.1978 0.0026, 0.00780, -1.2558 0.0000, 0.00000, -0.9341 0.0037, -0.00840, 0.7707 0.0112, -0.01420, 0.9910 0.0191, -0.01930, 0.9746 0.0397, -0.03030, 0.8635 0.0706, -0.04420, 0.6726 0.1037, -0.05710, 0.5360 0.1384, -0.06890, 0.3659 0.1741, -0.07950, 0.2435 0.2102, -0.08660, 0.1280 0.2472, -0.09640, 0.0032 0.2844, -0.10270, -0.0898 0.3225, -0.10690, -0.1640 0.3608, -0.10890, -0.2110 0.3991, -0.10830, -0.2307 0.4373, -0.10510, -0.1738 0.4757, -0.09890, -0.0864 0.5137, -0.09067, 0.0769 0.5611, -0.07859, 0.2086 16 Flap element taps 1.0000, 0.00130, -1.1654 0.9365, 0.01390, -1.2129 0.8333, 0.03280, -1.2807 0.7436, 0.04930, -1.2888 0.7049, 0.05667, -1.2922 0.6662, 0.06411, -1.3430 0.6274, 0.07172, -1.4030 0.6009, 0.07523, -2.0176 0.6069, 0.02889, -1.8737 0.6079, -0.01747, -1.8045 0.6167, -0.06381, -0.9517 0.6558, -0.05300, 0.0250 0.7045, -0.04117, 0.2724 0.7429, -0.03210, 0.3548 0.8333, -0.01400, 0.7592 0.9311, -0.00120, 0.9786 --------- Run Conditions: vel=100.9 ft/s Re=1.002x10^6 AOA=15.04 Flap deflection=90.00 Totals: Cl=0.3231 Cdp=0.6346 Cm(c/4)=-0.0370 Cs=-0.5290 Ch=-0.0417 Main component: Cl=0.3272 Cdp=0.0361 Cm=-0.0342 Flap component: Cl=-0.0041 Cdp=0.5985 Cm=-0.1219 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.0074 0.5905, -0.01667, -0.0304 0.5709, 0.03110, -0.0417 0.5889, 0.07933, -0.0393 0.5500, 0.08689, -0.0067 0.5110, 0.09367, -0.0287 0.4731, 0.09830, -0.0259 0.4349, 0.10070, -0.0193 0.3960, 0.10120, -0.0149 0.3566, 0.10020, -0.0359 0.3172, 0.09790, -0.0469 0.2778, 0.09440, -0.0949 0.2393, 0.08960, -0.1812 0.2056, 0.08360, -0.3251 0.1633, 0.07610, -0.5110 0.1261, 0.06710, -0.6557 0.0900, 0.05640, -0.8919 0.0571, 0.04390, -1.0968 0.0283, 0.02940, -1.4370 0.0142, 0.01970, -1.8041 0.0081, 0.01410, -1.8113 0.0026, 0.00780, -1.9576 0.0000, 0.00000, -2.0436 0.0037, -0.00840, 0.4532 0.0112, -0.01420, 0.9313 0.0191, -0.01930, 0.9941 0.0397, -0.03030, 0.9362 0.0706, -0.04420, 0.7825 0.1037, -0.05710, 0.6478 0.1384, -0.06890, 0.4732 0.1741, -0.07950, 0.3527 0.2102, -0.08660, 0.2371 0.2472, -0.09640, 0.1022 0.2844, -0.10270, 0.0042 0.3225, -0.10690, -0.0881 0.3608, -0.10890, -0.1522 0.3991, -0.10830, -0.1923 0.4373, -0.10510, -0.1397 0.4757, -0.09890, -0.0829 0.5137, -0.09067, -0.0371 0.5611, -0.07859, 0.1966 16 Flap element taps 1.0000, 0.00130, -1.1156 0.9365, 0.01390, -1.1716 0.8333, 0.03280, -1.2017 0.7436, 0.04930, -1.2176 0.7049, 0.05667, -1.2462 0.6662, 0.06411, -1.2864 0.6274, 0.07172, -1.3559 0.6009, 0.07523, -1.8990 0.6069, 0.02889, -1.7509 0.6079, -0.01747, -1.6842 0.6167, -0.06381, -1.0261 0.6558, -0.05300, -0.1183 0.7045, -0.04117, 0.1708 0.7429, -0.03210, 0.2508 0.8333, -0.01400, 0.7103 0.9311, -0.00120, 0.9870 --------- Run Conditions: vel=101.9 ft/s Re=1.011x10^6 AOA=18.00 Flap deflection=90.00 Totals: Cl=0.3330 Cdp=0.6132 Cm(c/4)=-0.0355 Cs=-0.4803 Ch=-0.0638 Main component: Cl=0.3779 Cdp=0.1098 Cm=-0.0665 Flap component: Cl=-0.0449 Cdp=0.5034 Cm=-0.0955 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1711 0.5905, -0.01667, -0.2268 0.5709, 0.03110, -0.2452 0.5889, 0.07933, -0.2431 0.5500, 0.08689, -0.1754 0.5110, 0.09367, -0.2624 0.4731, 0.09830, -0.2783 0.4349, 0.10070, -0.2523 0.3960, 0.10120, -0.2381 0.3566, 0.10020, -0.2527 0.3172, 0.09790, -0.2618 0.2778, 0.09440, -0.2914 0.2393, 0.08960, -0.2976 0.2056, 0.08360, -0.2991 0.1633, 0.07610, -0.3502 0.1261, 0.06710, -0.4132 0.0900, 0.05640, -0.6217 0.0571, 0.04390, -0.9200 0.0283, 0.02940, -1.3708 0.0142, 0.01970, -1.8443 0.0081, 0.01410, -1.9494 0.0026, 0.00780, -2.1982 0.0000, 0.00000, -2.6093 0.0037, -0.00840, 0.2466 0.0112, -0.01420, 0.8734 0.0191, -0.01930, 0.9883 0.0397, -0.03030, 0.9742 0.0706, -0.04420, 0.8447 0.1037, -0.05710, 0.7198 0.1384, -0.06890, 0.5539 0.1741, -0.07950, 0.4331 0.2102, -0.08660, 0.3131 0.2472, -0.09640, 0.1765 0.2844, -0.10270, 0.0707 0.3225, -0.10690, -0.0275 0.3608, -0.10890, -0.1069 0.3991, -0.10830, -0.1594 0.4373, -0.10510, -0.1256 0.4757, -0.09890, -0.0731 0.5137, -0.09067, -0.0306 0.5611, -0.07859, 0.1822 16 Flap element taps 1.0000, 0.00130, -0.9885 0.9365, 0.01390, -1.0224 0.8333, 0.03280, -1.0404 0.7436, 0.04930, -1.0472 0.7049, 0.05667, -1.0509 0.6662, 0.06411, -1.0568 0.6274, 0.07172, -1.1038 0.6009, 0.07523, -1.4226 0.6069, 0.02889, -1.3813 0.6079, -0.01747, -1.3180 0.6167, -0.06381, -0.9314 0.6558, -0.05300, -0.2505 0.7045, -0.04117, 0.0302 0.7429, -0.03210, 0.1347 0.8333, -0.01400, 0.6561 0.9311, -0.00120, 0.9976 --------- Run Conditions: vel=99.7 ft/s Re=0.990x10^6 AOA=20.00 Flap deflection=90.00 Totals: Cl=0.3396 Cdp=0.6227 Cm(c/4)=-0.0338 Cs=-0.4690 Ch=-0.0761 Main component: Cl=0.4095 Cdp=0.1648 Cm=-0.0864 Flap component: Cl=-0.0699 Cdp=0.4580 Cm=-0.0803 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.2792 0.5905, -0.01667, -0.3574 0.5709, 0.03110, -0.3751 0.5889, 0.07933, -0.3705 0.5500, 0.08689, -0.2864 0.5110, 0.09367, -0.3628 0.4731, 0.09830, -0.4129 0.4349, 0.10070, -0.4071 0.3960, 0.10120, -0.4005 0.3566, 0.10020, -0.3836 0.3172, 0.09790, -0.3859 0.2778, 0.09440, -0.4036 0.2393, 0.08960, -0.3989 0.2056, 0.08360, -0.4139 0.1633, 0.07610, -0.4284 0.1261, 0.06710, -0.4454 0.0900, 0.05640, -0.5004 0.0571, 0.04390, -0.7137 0.0283, 0.02940, -1.1857 0.0142, 0.01970, -1.7267 0.0081, 0.01410, -1.9176 0.0026, 0.00780, -2.2289 0.0000, 0.00000, -2.8179 0.0037, -0.00840, 0.1420 0.0112, -0.01420, 0.8369 0.0191, -0.01930, 0.9829 0.0397, -0.03030, 0.9953 0.0706, -0.04420, 0.8758 0.1037, -0.05710, 0.7570 0.1384, -0.06890, 0.6096 0.1741, -0.07950, 0.4862 0.2102, -0.08660, 0.3524 0.2472, -0.09640, 0.2203 0.2844, -0.10270, 0.1053 0.3225, -0.10690, 0.0152 0.3608, -0.10890, -0.0815 0.3991, -0.10830, -0.1395 0.4373, -0.10510, -0.1232 0.4757, -0.09890, -0.0819 0.5137, -0.09067, -0.0273 0.5611, -0.07859, 0.0923 16 Flap element taps 1.0000, 0.00130, -0.9654 0.9365, 0.01390, -0.9859 0.8333, 0.03280, -0.9889 0.7436, 0.04930, -0.9930 0.7049, 0.05667, -0.9900 0.6662, 0.06411, -0.9930 0.6274, 0.07172, -1.0257 0.6009, 0.07523, -1.2011 0.6069, 0.02889, -1.1803 0.6079, -0.01747, -1.1571 0.6167, -0.06381, -0.9342 0.6558, -0.05300, -0.3679 0.7045, -0.04117, -0.0597 0.7429, -0.03210, 0.0515 0.8333, -0.01400, 0.6101 0.9311, -0.00120, 0.9977 --------- Run Conditions: vel=103.4 ft/s Re=1.026x10^6 AOA=24.01 Flap deflection=90.00 Totals: Cl=0.3675 Cdp=0.6848 Cm(c/4)=-0.0431 Cs=-0.4760 Ch=-0.0869 Main component: Cl=0.4621 Cdp=0.2823 Cm=-0.1250 Flap component: Cl=-0.0945 Cdp=0.4025 Cm=-0.0717 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.4203 0.5905, -0.01667, -0.5358 0.5709, 0.03110, -0.5578 0.5889, 0.07933, -0.5573 0.5500, 0.08689, -0.4665 0.5110, 0.09367, -0.5057 0.4731, 0.09830, -0.5336 0.4349, 0.10070, -0.5732 0.3960, 0.10120, -0.6293 0.3566, 0.10020, -0.6142 0.3172, 0.09790, -0.6180 0.2778, 0.09440, -0.6313 0.2393, 0.08960, -0.6177 0.2056, 0.08360, -0.6278 0.1633, 0.07610, -0.6005 0.1261, 0.06710, -0.6073 0.0900, 0.05640, -0.6067 0.0571, 0.04390, -0.6234 0.0283, 0.02940, -0.6558 0.0142, 0.01970, -0.8465 0.0081, 0.01410, -1.0839 0.0026, 0.00780, -1.4350 0.0000, 0.00000, -2.2918 0.0037, -0.00840, 0.1174 0.0112, -0.01420, 0.7912 0.0191, -0.01930, 0.9595 0.0397, -0.03030, 1.0092 0.0706, -0.04420, 0.9195 0.1037, -0.05710, 0.8188 0.1384, -0.06890, 0.7047 0.1741, -0.07950, 0.5862 0.2102, -0.08660, 0.4433 0.2472, -0.09640, 0.3215 0.2844, -0.10270, 0.1977 0.3225, -0.10690, 0.1145 0.3608, -0.10890, -0.0010 0.3991, -0.10830, -0.0671 0.4373, -0.10510, -0.0794 0.4757, -0.09890, -0.0607 0.5137, -0.09067, -0.0036 0.5611, -0.07859, 0.0399 16 Flap element taps 1.0000, 0.00130, -0.8914 0.9365, 0.01390, -0.9099 0.8333, 0.03280, -0.9119 0.7436, 0.04930, -0.9258 0.7049, 0.05667, -0.9247 0.6662, 0.06411, -0.9318 0.6274, 0.07172, -0.9572 0.6009, 0.07523, -1.0774 0.6069, 0.02889, -1.0599 0.6079, -0.01747, -1.0376 0.6167, -0.06381, -0.9339 0.6558, -0.05300, -0.5010 0.7045, -0.04117, -0.1667 0.7429, -0.03210, -0.0593 0.8333, -0.01400, 0.5524 0.9311, -0.00120, 1.0000 --------- Run Conditions: vel=100.5 ft/s Re=0.996x10^6 AOA=26.99 Flap deflection=90.00 Totals: Cl=0.3700 Cdp=0.7426 Cm(c/4)=-0.0481 Cs=-0.4938 Ch=-0.0949 Main component: Cl=0.4844 Cdp=0.3562 Cm=-0.1449 Flap component: Cl=-0.1143 Cdp=0.3864 Cm=-0.0700 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.5354 0.5905, -0.01667, -0.6678 0.5709, 0.03110, -0.6824 0.5889, 0.07933, -0.6820 0.5500, 0.08689, -0.6291 0.5110, 0.09367, -0.6220 0.4731, 0.09830, -0.6226 0.4349, 0.10070, -0.6316 0.3960, 0.10120, -0.6998 0.3566, 0.10020, -0.6634 0.3172, 0.09790, -0.6780 0.2778, 0.09440, -0.6891 0.2393, 0.08960, -0.6727 0.2056, 0.08360, -0.7069 0.1633, 0.07610, -0.6640 0.1261, 0.06710, -0.6790 0.0900, 0.05640, -0.6590 0.0571, 0.04390, -0.6657 0.0283, 0.02940, -0.6814 0.0142, 0.01970, -0.6847 0.0081, 0.01410, -0.7870 0.0026, 0.00780, -1.0476 0.0000, 0.00000, -2.1115 0.0037, -0.00840, 0.0515 0.0112, -0.01420, 0.7426 0.0191, -0.01930, 0.9360 0.0397, -0.03030, 1.0174 0.0706, -0.04420, 0.9464 0.1037, -0.05710, 0.8589 0.1384, -0.06890, 0.7723 0.1741, -0.07950, 0.6564 0.2102, -0.08660, 0.5005 0.2472, -0.09640, 0.3881 0.2844, -0.10270, 0.2534 0.3225, -0.10690, 0.1846 0.3608, -0.10890, 0.0467 0.3991, -0.10830, -0.0222 0.4373, -0.10510, -0.0575 0.4757, -0.09890, -0.0568 0.5137, -0.09067, -0.0009 0.5611, -0.07859, 0.0220 16 Flap element taps 1.0000, 0.00130, -0.9171 0.9365, 0.01390, -0.9362 0.8333, 0.03280, -0.9457 0.7436, 0.04930, -0.9551 0.7049, 0.05667, -0.9541 0.6662, 0.06411, -0.9633 0.6274, 0.07172, -0.9865 0.6009, 0.07523, -1.0830 0.6069, 0.02889, -1.0692 0.6079, -0.01747, -1.0585 0.6167, -0.06381, -0.9859 0.6558, -0.05300, -0.6025 0.7045, -0.04117, -0.2612 0.7429, -0.03210, -0.1543 0.8333, -0.01400, 0.5020 0.9311, -0.00120, 1.0035