S809 VENTED AILERON MODEL, 18 IN CHORD --------- Run Conditions: vel=104.1 ft/s Re=1.007x10^6 AOA=-6.02 Flap deflection=-90.00 Totals: Cl=-0.2072 Cdp=0.5432 Cm(c/4)=0.0405 Cs=-0.5185 Ch=0.0750 Main component: Cl=-0.1832 Cdp=-0.0157 Cm=0.0223 Flap component: Cl=-0.0240 Cdp=0.5589 Cm=0.0840 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.1643 0.5871, 0.07930, 0.2443 0.5501, 0.08690, 0.1872 0.5112, 0.09370, 0.0535 0.4731, 0.09830, -0.0610 0.4349, 0.10070, -0.1042 0.3960, 0.10120, -0.0973 0.3566, 0.10020, -0.0952 0.3172, 0.09790, -0.0741 0.2778, 0.09440, -0.0588 0.2393, 0.08960, -0.0339 0.2056, 0.08360, 0.0101 0.1633, 0.07610, 0.0713 0.1261, 0.06710, 0.1748 0.0900, 0.05640, 0.2685 0.0571, 0.04390, 0.4454 0.0283, 0.02940, 0.7087 0.0142, 0.01970, 0.9017 0.0081, 0.01410, 0.9800 0.0026, 0.00780, 0.8153 0.0000, 0.00000, 0.2856 0.0037, -0.00840, -0.4605 0.0112, -0.01420, -0.7311 0.0191, -0.01930, -0.3844 0.0397, -0.03030, -0.3466 0.0706, -0.04420, -0.3587 0.1037, -0.05710, -0.3534 0.1384, -0.06890, -0.4012 0.1741, -0.07950, -0.4227 0.2102, -0.08660, -0.4438 0.2472, -0.09640, -0.4566 0.2844, -0.10270, -0.4037 0.3225, -0.10690, -0.3231 0.3608, -0.10890, -0.1850 0.3991, -0.10830, 0.0132 0.4373, -0.10510, 0.1327 0.4757, -0.09890, 0.1493 0.5137, -0.09070, 0.1310 0.5514, -0.08120, 0.1183 0.5917, -0.06870, 0.1438 0.5917, -0.02380, 0.1656 0.5917, 0.02120, 0.1727 16 Flap element taps 1.0000, 0.00130, -1.1571 0.9365, 0.01390, 0.9622 0.8333, 0.03280, 0.7800 0.7436, 0.04930, 0.2063 0.7049, 0.05670, -0.3053 0.6667, 0.05450, -0.6187 0.6302, 0.03770, -0.8557 0.6083, 0.01980, -1.3006 0.6000, 0.00000, -1.3366 0.6076, -0.01900, -1.3123 0.6285, -0.03060, -1.2954 0.6667, -0.04090, -1.3473 0.7046, -0.04120, -1.3830 0.7429, -0.03210, -1.2846 0.8333, -0.01400, -1.2403 0.9311, -0.00120, -1.2138 --------- Run Conditions: vel=104.7 ft/s Re=1.009x10^6 AOA=0.01 Flap deflection=-90.00 Totals: Cl=0.0283 Cdp=0.5279 Cm(c/4)=0.0505 Cs=-0.5279 Ch=0.0416 Main component: Cl=0.0999 Cdp=-0.0414 Cm=-0.0266 Flap component: Cl=-0.0716 Cdp=0.5693 Cm=0.0699 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.2951 0.5871, 0.07930, 0.2879 0.5501, 0.08690, 0.2384 0.5112, 0.09370, 0.1224 0.4731, 0.09830, -0.0371 0.4349, 0.10070, -0.1367 0.3960, 0.10120, -0.1830 0.3566, 0.10020, -0.2191 0.3172, 0.09790, -0.2382 0.2778, 0.09440, -0.2631 0.2393, 0.08960, -0.2827 0.2056, 0.08360, -0.2804 0.1633, 0.07610, -0.2623 0.1261, 0.06710, -0.2137 0.0900, 0.05640, -0.1956 0.0571, 0.04390, -0.1000 0.0283, 0.02940, 0.0951 0.0142, 0.01970, 0.2823 0.0081, 0.01410, 0.3869 0.0026, 0.00780, 0.6159 0.0000, 0.00000, 1.0014 0.0037, -0.00840, 0.7849 0.0112, -0.01420, 0.4697 0.0191, -0.01930, 0.4657 0.0397, -0.03030, 0.3116 0.0706, -0.04420, 0.1615 0.1037, -0.05710, 0.0823 0.1384, -0.06890, -0.0237 0.1741, -0.07950, -0.0959 0.2102, -0.08660, -0.1648 0.2472, -0.09640, -0.2232 0.2844, -0.10270, -0.2253 0.3225, -0.10690, -0.2040 0.3608, -0.10890, -0.1351 0.3991, -0.10830, -0.0046 0.4373, -0.10510, 0.1932 0.4757, -0.09890, 0.2891 0.5137, -0.09070, 0.3073 0.5514, -0.08120, 0.2945 0.5917, -0.06870, 0.3022 0.5917, -0.02380, 0.3024 0.5917, 0.02120, 0.3071 16 Flap element taps 1.0000, 0.00130, -1.1174 0.9365, 0.01390, 0.9625 0.8333, 0.03280, 0.6548 0.7436, 0.04930, 0.2839 0.7049, 0.05670, 0.0100 0.6667, 0.05450, -0.1750 0.6302, 0.03770, -0.5457 0.6083, 0.01980, -1.2056 0.6000, 0.00000, -1.3155 0.6076, -0.01900, -1.2908 0.6285, -0.03060, -1.2610 0.6667, -0.04090, -1.3013 0.7046, -0.04120, -1.3339 0.7429, -0.03210, -1.2318 0.8333, -0.01400, -1.1986 0.9311, -0.00120, -1.1684 --------- Run Conditions: vel=105.5 ft/s Re=1.014x10^6 AOA=3.05 Flap deflection=-90.00 Totals: Cl=0.0327 Cdp=0.4973 Cm(c/4)=0.0612 Cs=-0.4948 Ch=0.0209 Main component: Cl=0.1322 Cdp=-0.0395 Cm=-0.0194 Flap component: Cl=-0.0995 Cdp=0.5368 Cm=0.0658 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.2512 0.5871, 0.07930, 0.2695 0.5501, 0.08690, 0.2617 0.5112, 0.09370, 0.2503 0.4731, 0.09830, 0.1314 0.4349, 0.10070, -0.0182 0.3960, 0.10120, -0.1267 0.3566, 0.10020, -0.1880 0.3172, 0.09790, -0.2376 0.2778, 0.09440, -0.2870 0.2393, 0.08960, -0.3279 0.2056, 0.08360, -0.3617 0.1633, 0.07610, -0.3549 0.1261, 0.06710, -0.3409 0.0900, 0.05640, -0.3532 0.0571, 0.04390, -0.3060 0.0283, 0.02940, -0.1652 0.0142, 0.01970, -0.0297 0.0081, 0.01410, 0.0265 0.0026, 0.00780, 0.2913 0.0000, 0.00000, 0.8548 0.0037, -0.00840, 0.9506 0.0112, -0.01420, 0.7052 0.0191, -0.01930, 0.6533 0.0397, -0.03030, 0.4708 0.0706, -0.04420, 0.2864 0.1037, -0.05710, 0.1840 0.1384, -0.06890, 0.0668 0.1741, -0.07950, -0.0274 0.2102, -0.08660, -0.1261 0.2472, -0.09640, -0.1996 0.2844, -0.10270, -0.2317 0.3225, -0.10690, -0.2291 0.3608, -0.10890, -0.1947 0.3991, -0.10830, -0.1031 0.4373, -0.10510, 0.0751 0.4757, -0.09890, 0.2561 0.5137, -0.09070, 0.3077 0.5514, -0.08120, 0.2961 0.5917, -0.06870, 0.3028 0.5917, -0.02380, 0.2817 0.5917, 0.02120, 0.2869 16 Flap element taps 1.0000, 0.00130, -1.1232 0.9365, 0.01390, 0.8771 0.8333, 0.03280, 0.2870 0.7436, 0.04930, 0.2718 0.7049, 0.05670, 0.2233 0.6667, 0.05450, 0.1263 0.6302, 0.03770, -0.4468 0.6083, 0.01980, -1.4939 0.6000, 0.00000, -1.6657 0.6076, -0.01900, -1.2543 0.6285, -0.03060, -1.2279 0.6667, -0.04090, -1.2951 0.7046, -0.04120, -1.3151 0.7429, -0.03210, -1.2303 0.8333, -0.01400, -1.1962 0.9311, -0.00120, -1.1722 --------- Run Conditions: vel=104.7 ft/s Re=1.004x10^6 AOA=6.05 Flap deflection=-90.00 Totals: Cl=-0.0030 Cdp=0.5650 Cm(c/4)=0.0379 Cs=-0.5622 Ch=-0.0670 Main component: Cl=0.0854 Cdp=-0.0414 Cm=0.0090 Flap component: Cl=-0.0884 Cdp=0.6064 Cm=0.0148 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.2888 0.5871, 0.07930, 0.3005 0.5501, 0.08690, 0.2966 0.5112, 0.09370, 0.3007 0.4731, 0.09830, 0.2754 0.4349, 0.10070, 0.1916 0.3960, 0.10120, 0.0524 0.3566, 0.10020, -0.0399 0.3172, 0.09790, -0.1278 0.2778, 0.09440, -0.2017 0.2393, 0.08960, -0.2710 0.2056, 0.08360, -0.3307 0.1633, 0.07610, -0.3449 0.1261, 0.06710, -0.3626 0.0900, 0.05640, -0.4066 0.0571, 0.04390, -0.4071 0.0283, 0.02940, -0.3212 0.0142, 0.01970, -0.2395 0.0081, 0.01410, -0.2393 0.0026, 0.00780, 0.0567 0.0000, 0.00000, 0.6303 0.0037, -0.00840, 0.9999 0.0112, -0.01420, 0.8270 0.0191, -0.01930, 0.7583 0.0397, -0.03030, 0.5689 0.0706, -0.04420, 0.3687 0.1037, -0.05710, 0.2477 0.1384, -0.06890, 0.1211 0.1741, -0.07950, 0.0065 0.2102, -0.08660, -0.1183 0.2472, -0.09640, -0.2067 0.2844, -0.10270, -0.2664 0.3225, -0.10690, -0.2921 0.3608, -0.10890, -0.2979 0.3991, -0.10830, -0.2557 0.4373, -0.10510, -0.1422 0.4757, -0.09890, 0.0458 0.5137, -0.09070, 0.2191 0.5514, -0.08120, 0.2757 0.5917, -0.06870, 0.2976 0.5917, -0.02380, 0.2943 0.5917, 0.02120, 0.2998 16 Flap element taps 1.0000, 0.00130, -1.2366 0.9365, 0.01390, 0.3700 0.8333, 0.03280, 0.3054 0.7436, 0.04930, 0.3709 0.7049, 0.05670, 0.7411 0.6667, 0.05450, 0.9499 0.6302, 0.03770, 0.1169 0.6083, 0.01980, -0.9399 0.6000, 0.00000, -1.2083 0.6076, -0.01900, -1.2330 0.6285, -0.03060, -1.2483 0.6667, -0.04090, -1.3212 0.7046, -0.04120, -1.3683 0.7429, -0.03210, -1.3001 0.8333, -0.01400, -1.3078 0.9311, -0.00120, -1.3027 --------- Run Conditions: vel=105.3 ft/s Re=1.006x10^6 AOA=9.03 Flap deflection=-90.00 Totals: Cl=-0.0266 Cdp=0.5804 Cm(c/4)=0.0521 Cs=-0.5774 Ch=-0.0818 Main component: Cl=0.0999 Cdp=-0.0362 Cm=0.0200 Flap component: Cl=-0.1265 Cdp=0.6165 Cm=0.0159 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.2431 0.5871, 0.07930, 0.2698 0.5501, 0.08690, 0.2682 0.5112, 0.09370, 0.2764 0.4731, 0.09830, 0.2630 0.4349, 0.10070, 0.2432 0.3960, 0.10120, 0.1558 0.3566, 0.10020, 0.0552 0.3172, 0.09790, -0.0617 0.2778, 0.09440, -0.1619 0.2393, 0.08960, -0.2576 0.2056, 0.08360, -0.3464 0.1633, 0.07610, -0.3878 0.1261, 0.06710, -0.4411 0.0900, 0.05640, -0.5272 0.0571, 0.04390, -0.5883 0.0283, 0.02940, -0.5868 0.0142, 0.01970, -0.5908 0.0081, 0.01410, -0.6599 0.0026, 0.00780, -0.3239 0.0000, 0.00000, 0.1364 0.0037, -0.00840, 0.9983 0.0112, -0.01420, 0.9506 0.0191, -0.01930, 0.8766 0.0397, -0.03030, 0.6962 0.0706, -0.04420, 0.4860 0.1037, -0.05710, 0.3523 0.1384, -0.06890, 0.2130 0.1741, -0.07950, 0.0831 0.2102, -0.08660, -0.0589 0.2472, -0.09640, -0.1683 0.2844, -0.10270, -0.2475 0.3225, -0.10690, -0.2999 0.3608, -0.10890, -0.3275 0.3991, -0.10830, -0.3319 0.4373, -0.10510, -0.2637 0.4757, -0.09890, -0.1300 0.5137, -0.09070, 0.0175 0.5514, -0.08120, 0.1708 0.5917, -0.06870, 0.2771 0.5917, -0.02380, 0.2701 0.5917, 0.02120, 0.2739 16 Flap element taps 1.0000, 0.00130, -1.2224 0.9365, 0.01390, 0.2852 0.8333, 0.03280, 0.3425 0.7436, 0.04930, 0.6929 0.7049, 0.05670, 0.9665 0.6667, 0.05450, 0.9023 0.6302, 0.03770, 0.1262 0.6083, 0.01980, -0.9055 0.6000, 0.00000, -1.1994 0.6076, -0.01900, -1.2270 0.6285, -0.03060, -1.2401 0.6667, -0.04090, -1.3035 0.7046, -0.04120, -1.3459 0.7429, -0.03210, -1.2851 0.8333, -0.01400, -1.2633 0.9311, -0.00120, -1.2852 --------- Run Conditions: vel=105.5 ft/s Re=1.006x10^6 AOA=12.05 Flap deflection=-90.00 Totals: Cl=0.0545 Cdp=0.5867 Cm(c/4)=0.0537 Cs=-0.5624 Ch=-0.0887 Main component: Cl=0.2019 Cdp=-0.0141 Cm=0.0027 Flap component: Cl=-0.1474 Cdp=0.6008 Cm=0.0070 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.1378 0.5871, 0.07930, 0.1792 0.5501, 0.08690, 0.1712 0.5112, 0.09370, 0.1814 0.4731, 0.09830, 0.1563 0.4349, 0.10070, 0.1552 0.3960, 0.10120, 0.1341 0.3566, 0.10020, 0.0786 0.3172, 0.09790, -0.0397 0.2778, 0.09440, -0.1681 0.2393, 0.08960, -0.2934 0.2056, 0.08360, -0.4129 0.1633, 0.07610, -0.4985 0.1261, 0.06710, -0.5906 0.0900, 0.05640, -0.7355 0.0571, 0.04390, -0.8785 0.0283, 0.02940, -1.0031 0.0142, 0.01970, -1.1578 0.0081, 0.01410, -1.2888 0.0026, 0.00780, -1.0317 0.0000, 0.00000, -0.8695 0.0037, -0.00840, 0.8358 0.0112, -0.01420, 1.0089 0.0191, -0.01930, 0.9769 0.0397, -0.03030, 0.8407 0.0706, -0.04420, 0.6394 0.1037, -0.05710, 0.4987 0.1384, -0.06890, 0.3496 0.1741, -0.07950, 0.2145 0.2102, -0.08660, 0.0679 0.2472, -0.09640, -0.0543 0.2844, -0.10270, -0.1509 0.3225, -0.10690, -0.2294 0.3608, -0.10890, -0.2724 0.3991, -0.10830, -0.3115 0.4373, -0.10510, -0.2654 0.4757, -0.09890, -0.1553 0.5137, -0.09070, -0.0286 0.5514, -0.08120, 0.1178 0.5917, -0.06870, 0.1680 0.5917, -0.02380, 0.1605 0.5917, 0.02120, 0.1623 16 Flap element taps 1.0000, 0.00130, -1.2752 0.9365, 0.01390, 0.1477 0.8333, 0.03280, 0.2874 0.7436, 0.04930, 0.6903 0.7049, 0.05670, 0.9540 0.6667, 0.05450, 0.9358 0.6302, 0.03770, 0.2174 0.6083, 0.01980, -0.8276 0.6000, 0.00000, -1.1547 0.6076, -0.01900, -1.1874 0.6285, -0.03060, -1.2093 0.6667, -0.04090, -1.2631 0.7046, -0.04120, -1.3266 0.7429, -0.03210, -1.2811 0.8333, -0.01400, -1.2811 0.9311, -0.00120, -1.3342 --------- Run Conditions: vel=105.6 ft/s Re=1.004x10^6 AOA=15.02 Flap deflection=-90.00 Totals: Cl=0.1409 Cdp=0.5853 Cm(c/4)=0.0501 Cs=-0.5288 Ch=-0.1025 Main component: Cl=0.3048 Cdp=0.0228 Cm=-0.0214 Flap component: Cl=-0.1639 Cdp=0.5626 Cm=-0.0004 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.0194 0.5871, 0.07930, 0.0184 0.5501, 0.08690, 0.0009 0.5112, 0.09370, 0.0089 0.4731, 0.09830, 0.0016 0.4349, 0.10070, 0.0051 0.3960, 0.10120, 0.0131 0.3566, 0.10020, -0.0039 0.3172, 0.09790, -0.0359 0.2778, 0.09440, -0.1096 0.2393, 0.08960, -0.2459 0.2056, 0.08360, -0.3938 0.1633, 0.07610, -0.5497 0.1261, 0.06710, -0.6908 0.0900, 0.05640, -0.9074 0.0571, 0.04390, -1.1467 0.0283, 0.02940, -1.4263 0.0142, 0.01970, -1.7583 0.0081, 0.01410, -2.0120 0.0026, 0.00780, -1.8963 0.0000, 0.00000, -2.2060 0.0037, -0.00840, 0.4807 0.0112, -0.01420, 0.9523 0.0191, -0.01930, 1.0016 0.0397, -0.03030, 0.9381 0.0706, -0.04420, 0.7667 0.1037, -0.05710, 0.6320 0.1384, -0.06890, 0.4719 0.1741, -0.07950, 0.3386 0.2102, -0.08660, 0.1966 0.2472, -0.09640, 0.0613 0.2844, -0.10270, -0.0430 0.3225, -0.10690, -0.1469 0.3608, -0.10890, -0.1975 0.3991, -0.10830, -0.2656 0.4373, -0.10510, -0.2338 0.4757, -0.09890, -0.1659 0.5137, -0.09070, -0.1096 0.5514, -0.08120, 0.0944 0.5917, -0.06870, 0.0014 0.5917, -0.02380, 0.0010 0.5917, 0.02120, 0.0037 16 Flap element taps 1.0000, 0.00130, -1.2404 0.9365, 0.01390, 0.0153 0.8333, 0.03280, 0.1669 0.7436, 0.04930, 0.6261 0.7049, 0.05670, 0.9126 0.6667, 0.05450, 0.9661 0.6302, 0.03770, 0.3066 0.6083, 0.01980, -0.7731 0.6000, 0.00000, -1.1771 0.6076, -0.01900, -1.2002 0.6285, -0.03060, -1.2078 0.6667, -0.04090, -1.2455 0.7046, -0.04120, -1.2956 0.7429, -0.03210, -1.2601 0.8333, -0.01400, -1.2707 0.9311, -0.00120, -1.2796 --------- Run Conditions: vel=106.6 ft/s Re=1.011x10^6 AOA=18.03 Flap deflection=-90.00 Totals: Cl=0.2324 Cdp=0.5587 Cm(c/4)=0.0266 Cs=-0.4593 Ch=-0.1183 Main component: Cl=0.3771 Cdp=0.1024 Cm=-0.0549 Flap component: Cl=-0.1448 Cdp=0.4563 Cm=-0.0170 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.3077 0.5871, 0.07930, -0.2192 0.5501, 0.08690, -0.2609 0.5112, 0.09370, -0.2768 0.4731, 0.09830, -0.2888 0.4349, 0.10070, -0.2796 0.3960, 0.10120, -0.2586 0.3566, 0.10020, -0.2809 0.3172, 0.09790, -0.2965 0.2778, 0.09440, -0.3075 0.2393, 0.08960, -0.3183 0.2056, 0.08360, -0.3231 0.1633, 0.07610, -0.3913 0.1261, 0.06710, -0.5035 0.0900, 0.05640, -0.7427 0.0571, 0.04390, -1.1066 0.0283, 0.02940, -1.5650 0.0142, 0.01970, -2.0626 0.0081, 0.01410, -2.4296 0.0026, 0.00780, -2.4896 0.0000, 0.00000, -3.2867 0.0037, -0.00840, 0.1118 0.0112, -0.01420, 0.8423 0.0191, -0.01930, 0.9774 0.0397, -0.03030, 0.9839 0.0706, -0.04420, 0.8507 0.1037, -0.05710, 0.7288 0.1384, -0.06890, 0.5643 0.1741, -0.07950, 0.4335 0.2102, -0.08660, 0.2989 0.2472, -0.09640, 0.1525 0.2844, -0.10270, 0.0430 0.3225, -0.10690, -0.0807 0.3608, -0.10890, -0.1422 0.3991, -0.10830, -0.2397 0.4373, -0.10510, -0.2321 0.4757, -0.09890, -0.1841 0.5137, -0.09070, -0.1278 0.5514, -0.08120, -0.1019 0.5917, -0.06870, -0.2568 0.5917, -0.02380, -0.2641 0.5917, 0.02120, -0.2713 16 Flap element taps 1.0000, 0.00130, -1.1122 0.9365, 0.01390, -0.2452 0.8333, 0.03280, -0.0387 0.7436, 0.04930, 0.4950 0.7049, 0.05670, 0.8287 0.6667, 0.05450, 1.0024 0.6302, 0.03770, 0.4625 0.6083, 0.01980, -0.5771 0.6000, 0.00000, -1.0258 0.6076, -0.01900, -1.0406 0.6285, -0.03060, -1.0508 0.6667, -0.04090, -1.0722 0.7046, -0.04120, -1.1095 0.7429, -0.03210, -1.0829 0.8333, -0.01400, -1.0954 0.9311, -0.00120, -1.1110 --------- Run Conditions: vel=107.1 ft/s Re=1.013x10^6 AOA=20.01 Flap deflection=-90.00 Totals: Cl=0.2983 Cdp=0.5638 Cm(c/4)=0.0033 Cs=-0.4277 Ch=-0.1291 Main component: Cl=0.4216 Cdp=0.1853 Cm=-0.0873 Flap component: Cl=-0.1233 Cdp=0.3785 Cm=-0.0277 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.4920 0.5871, 0.07930, -0.3883 0.5501, 0.08690, -0.4361 0.5112, 0.09370, -0.4744 0.4731, 0.09830, -0.5209 0.4349, 0.10070, -0.5183 0.3960, 0.10120, -0.4965 0.3566, 0.10020, -0.4959 0.3172, 0.09790, -0.4968 0.2778, 0.09440, -0.5035 0.2393, 0.08960, -0.5223 0.2056, 0.08360, -0.5339 0.1633, 0.07610, -0.5604 0.1261, 0.06710, -0.5687 0.0900, 0.05640, -0.5938 0.0571, 0.04390, -0.7063 0.0283, 0.02940, -1.0927 0.0142, 0.01970, -1.6555 0.0081, 0.01410, -2.1189 0.0026, 0.00780, -2.3219 0.0000, 0.00000, -3.3071 0.0037, -0.00840, 0.0185 0.0112, -0.01420, 0.7991 0.0191, -0.01930, 0.9650 0.0397, -0.03030, 1.0003 0.0706, -0.04420, 0.8848 0.1037, -0.05710, 0.7725 0.1384, -0.06890, 0.6188 0.1741, -0.07950, 0.4902 0.2102, -0.08660, 0.3510 0.2472, -0.09640, 0.2069 0.2844, -0.10270, 0.0914 0.3225, -0.10690, -0.0329 0.3608, -0.10890, -0.1038 0.3991, -0.10830, -0.2166 0.4373, -0.10510, -0.2231 0.4757, -0.09890, -0.1923 0.5137, -0.09070, -0.1612 0.5514, -0.08120, -0.1229 0.5917, -0.06870, -0.4534 0.5917, -0.02380, -0.4554 0.5917, 0.02120, -0.4643 16 Flap element taps 1.0000, 0.00130, -0.9984 0.9365, 0.01390, -0.4457 0.8333, 0.03280, -0.1917 0.7436, 0.04930, 0.3960 0.7049, 0.05670, 0.7574 0.6667, 0.05450, 1.0088 0.6302, 0.03770, 0.5488 0.6083, 0.01980, -0.4586 0.6000, 0.00000, -0.9350 0.6076, -0.01900, -0.9420 0.6285, -0.03060, -0.9452 0.6667, -0.04090, -0.9495 0.7046, -0.04120, -0.9704 0.7429, -0.03210, -0.9569 0.8333, -0.01400, -0.9719 0.9311, -0.00120, -0.9873 --------- Run Conditions: vel=106.6 ft/s Re=1.006x10^6 AOA=24.00 Flap deflection=-90.00 Totals: Cl=0.4040 Cdp=0.5910 Cm(c/4)=-0.0180 Cs=-0.3756 Ch=-0.1390 Main component: Cl=0.5032 Cdp=0.3055 Cm=-0.1306 Flap component: Cl=-0.0992 Cdp=0.2855 Cm=-0.0398 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.6658 0.5871, 0.07930, -0.5885 0.5501, 0.08690, -0.6109 0.5112, 0.09370, -0.6342 0.4731, 0.09830, -0.6933 0.4349, 0.10070, -0.7167 0.3960, 0.10120, -0.7220 0.3566, 0.10020, -0.7313 0.3172, 0.09790, -0.7433 0.2778, 0.09440, -0.7435 0.2393, 0.08960, -0.7399 0.2056, 0.08360, -0.7291 0.1633, 0.07610, -0.7388 0.1261, 0.06710, -0.7586 0.0900, 0.05640, -0.7763 0.0571, 0.04390, -0.8155 0.0283, 0.02940, -0.9569 0.0142, 0.01970, -1.1132 0.0081, 0.01410, -1.2579 0.0026, 0.00780, -1.4591 0.0000, 0.00000, -2.8474 0.0037, -0.00840, -0.1007 0.0112, -0.01420, 0.7124 0.0191, -0.01930, 0.9218 0.0397, -0.03030, 1.0122 0.0706, -0.04420, 0.9331 0.1037, -0.05710, 0.8427 0.1384, -0.06890, 0.7143 0.1741, -0.07950, 0.5936 0.2102, -0.08660, 0.4547 0.2472, -0.09640, 0.3180 0.2844, -0.10270, 0.1987 0.3225, -0.10690, 0.0771 0.3608, -0.10890, -0.0043 0.3991, -0.10830, -0.1320 0.4373, -0.10510, -0.1643 0.4757, -0.09890, -0.1547 0.5137, -0.09070, -0.1468 0.5514, -0.08120, -0.1288 0.5917, -0.06870, -0.6356 0.5917, -0.02380, -0.6387 0.5917, 0.02120, -0.6391 16 Flap element taps 1.0000, 0.00130, -0.8129 0.9365, 0.01390, -0.6300 0.8333, 0.03280, -0.3471 0.7436, 0.04930, 0.2829 0.7049, 0.05670, 0.6630 0.6667, 0.05450, 1.0097 0.6302, 0.03770, 0.6584 0.6083, 0.01980, -0.2823 0.6000, 0.00000, -0.7892 0.6076, -0.01900, -0.7906 0.6285, -0.03060, -0.7874 0.6667, -0.04090, -0.7875 0.7046, -0.04120, -0.7979 0.7429, -0.03210, -0.7954 0.8333, -0.01400, -0.8054 0.9311, -0.00120, -0.8036 --------- Run Conditions: vel=106.5 ft/s Re=1.002x10^6 AOA=26.98 Flap deflection=-90.00 Totals: Cl=0.3870 Cdp=0.6649 Cm(c/4)=-0.0290 Cs=-0.4170 Ch=-0.1484 Main component: Cl=0.4894 Cdp=0.3939 Cm=-0.1443 Flap component: Cl=-0.1025 Cdp=0.2710 Cm=-0.0463 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.8119 0.5871, 0.07930, -0.7168 0.5501, 0.08690, -0.7193 0.5112, 0.09370, -0.7349 0.4731, 0.09830, -0.7665 0.4349, 0.10070, -0.7805 0.3960, 0.10120, -0.7897 0.3566, 0.10020, -0.7821 0.3172, 0.09790, -0.7854 0.2778, 0.09440, -0.7822 0.2393, 0.08960, -0.7787 0.2056, 0.08360, -0.7771 0.1633, 0.07610, -0.7704 0.1261, 0.06710, -0.7736 0.0900, 0.05640, -0.7663 0.0571, 0.04390, -0.7703 0.0283, 0.02940, -0.7661 0.0142, 0.01970, -0.7718 0.0081, 0.01410, -0.8122 0.0026, 0.00780, -0.7334 0.0000, 0.00000, -1.3174 0.0037, -0.00840, 0.1138 0.0112, -0.01420, 0.7417 0.0191, -0.01930, 0.9260 0.0397, -0.03030, 1.0197 0.0706, -0.04420, 0.9574 0.1037, -0.05710, 0.8803 0.1384, -0.06890, 0.7682 0.1741, -0.07950, 0.6513 0.2102, -0.08660, 0.5114 0.2472, -0.09640, 0.3798 0.2844, -0.10270, 0.2556 0.3225, -0.10690, 0.1349 0.3608, -0.10890, 0.0455 0.3991, -0.10830, -0.0940 0.4373, -0.10510, -0.1421 0.4757, -0.09890, -0.1497 0.5137, -0.09070, -0.1611 0.5514, -0.08120, -0.1609 0.5917, -0.06870, -0.7828 0.5917, -0.02380, -0.7828 0.5917, 0.02120, -0.7866 16 Flap element taps 1.0000, 0.00130, -0.8493 0.9365, 0.01390, -0.7511 0.8333, 0.03280, -0.4568 0.7436, 0.04930, 0.2055 0.7049, 0.05670, 0.6036 0.6667, 0.05450, 1.0087 0.6302, 0.03770, 0.7006 0.6083, 0.01980, -0.2549 0.6000, 0.00000, -0.8270 0.6076, -0.01900, -0.8254 0.6285, -0.03060, -0.8232 0.6667, -0.04090, -0.8249 0.7046, -0.04120, -0.8331 0.7429, -0.03210, -0.8318 0.8333, -0.01400, -0.8453 0.9311, -0.00120, -0.8357