S809 VENTED AILERON MODEL, 18 IN CHORD --------- Run Conditions: vel=105.5 ft/s Re=1.000x10^6 AOA=-6.03 Flap deflection=-10.00 Totals: Cl=-0.4153 Cdp=0.0596 Cm(c/4)=0.0451 Cs=-0.0156 Ch=0.0093 Main component: Cl=-0.2759 Cdp=0.0893 Cm=0.0396 Flap component: Cl=-0.1394 Cdp=-0.0297 Cm=0.1102 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.8733 0.5871, 0.07930, -0.3819 0.5501, 0.08690, -0.3504 0.5112, 0.09370, -0.4672 0.4731, 0.09830, -0.5087 0.4349, 0.10070, -0.4858 0.3960, 0.10120, -0.4267 0.3566, 0.10020, -0.3558 0.3172, 0.09790, -0.2836 0.2778, 0.09440, -0.2319 0.2393, 0.08960, -0.1755 0.2056, 0.08360, -0.1091 0.1633, 0.07610, -0.0036 0.1261, 0.06710, 0.1233 0.0900, 0.05640, 0.2486 0.0571, 0.04390, 0.4592 0.0283, 0.02940, 0.7421 0.0142, 0.01970, 0.9376 0.0081, 0.01410, 0.9830 0.0026, 0.00780, 0.7787 0.0000, 0.00000, -0.1164 0.0037, -0.00840, -0.9658 0.0112, -0.01420, -1.2153 0.0191, -0.01930, -0.7398 0.0397, -0.03030, -0.6656 0.0706, -0.04420, -0.6606 0.1037, -0.05710, -0.6643 0.1384, -0.06890, -0.7187 0.1741, -0.07950, -0.7551 0.2102, -0.08660, -0.8238 0.2472, -0.09640, -0.8787 0.2844, -0.10270, -0.8761 0.3225, -0.10690, -0.8405 0.3608, -0.10890, -0.7834 0.3991, -0.10830, -0.6366 0.4373, -0.10510, -0.4124 0.4757, -0.09890, -0.1858 0.5137, -0.09070, -0.1253 0.5514, -0.08120, -0.1170 0.5917, -0.06870, -0.1437 0.5917, -0.02380, -0.4809 0.5917, 0.02120, -0.8647 16 Flap element taps 1.0000, 0.00130, -0.2594 0.9365, 0.01390, -0.0444 0.8333, 0.03280, 0.1521 0.7436, 0.04930, 0.4321 0.7049, 0.05670, 0.8413 0.6667, 0.05450, -0.2115 0.6302, 0.03770, -1.0809 0.6083, 0.01980, -0.9597 0.6000, 0.00000, -1.0579 0.6076, -0.01900, -0.4336 0.6285, -0.03060, -0.3483 0.6667, -0.04090, -0.3095 0.7046, -0.04120, -0.2870 0.7429, -0.03210, -0.2874 0.8333, -0.01400, -0.2837 0.9311, -0.00120, -0.2877 --------- Run Conditions: vel=106.3 ft/s Re=1.008x10^6 AOA=0.01 Flap deflection=-10.00 Totals: Cl=-0.2323 Cdp=0.0209 Cm(c/4)=0.0584 Cs=-0.0209 Ch=-0.0039 Main component: Cl=-0.1324 Cdp=0.0162 Cm=0.0366 Flap component: Cl=-0.1000 Cdp=0.0047 Cm=0.0799 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.0911 0.5871, 0.07930, -0.1640 0.5501, 0.08690, -0.2568 0.5112, 0.09370, -0.4233 0.4731, 0.09830, -0.5241 0.4349, 0.10070, -0.5466 0.3960, 0.10120, -0.5377 0.3566, 0.10020, -0.4966 0.3172, 0.09790, -0.4567 0.2778, 0.09440, -0.4353 0.2393, 0.08960, -0.4151 0.2056, 0.08360, -0.3931 0.1633, 0.07610, -0.3154 0.1261, 0.06710, -0.2341 0.0900, 0.05640, -0.1684 0.0571, 0.04390, -0.0144 0.0283, 0.02940, 0.2423 0.0142, 0.01970, 0.4783 0.0081, 0.01410, 0.6339 0.0026, 0.00780, 0.8102 0.0000, 0.00000, 0.9781 0.0037, -0.00840, 0.4224 0.0112, -0.01420, 0.0013 0.0191, -0.01930, 0.1058 0.0397, -0.03030, -0.0439 0.0706, -0.04420, -0.1912 0.1037, -0.05710, -0.2917 0.1384, -0.06890, -0.4138 0.1741, -0.07950, -0.5182 0.2102, -0.08660, -0.6559 0.2472, -0.09640, -0.7747 0.2844, -0.10270, -0.8486 0.3225, -0.10690, -0.8933 0.3608, -0.10890, -0.9413 0.3991, -0.10830, -0.9132 0.4373, -0.10510, -0.8238 0.4757, -0.09890, -0.6409 0.5137, -0.09070, -0.4585 0.5514, -0.08120, -0.2372 0.5917, -0.06870, -0.0941 0.5917, -0.02380, -0.1197 0.5917, 0.02120, -0.0843 16 Flap element taps 1.0000, 0.00130, -0.0679 0.9365, 0.01390, 0.0723 0.8333, 0.03280, 0.2356 0.7436, 0.04930, 0.1790 0.7049, 0.05670, -0.0991 0.6667, 0.05450, -0.1183 0.6302, 0.03770, -0.0928 0.6083, 0.01980, -0.0977 0.6000, 0.00000, -0.1328 0.6076, -0.01900, -0.1441 0.6285, -0.03060, -0.1798 0.6667, -0.04090, -0.3767 0.7046, -0.04120, -0.3082 0.7429, -0.03210, -0.1866 0.8333, -0.01400, -0.1526 0.9311, -0.00120, -0.1378 Wake drag found for this condition, Cdw=0.0277 --------- Run Conditions: vel=106.6 ft/s Re=1.010x10^6 AOA=3.05 Flap deflection=-10.00 Totals: Cl=-0.0258 Cdp=0.0139 Cm(c/4)=0.0625 Cs=-0.0153 Ch=-0.0189 Main component: Cl=0.0631 Cdp=0.0153 Cm=0.0002 Flap component: Cl=-0.0889 Cdp=-0.0014 Cm=0.0685 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.0730 0.5871, 0.07930, -0.1641 0.5501, 0.08690, -0.2762 0.5112, 0.09370, -0.4595 0.4731, 0.09830, -0.5822 0.4349, 0.10070, -0.6278 0.3960, 0.10120, -0.6394 0.3566, 0.10020, -0.6141 0.3172, 0.09790, -0.5910 0.2778, 0.09440, -0.5888 0.2393, 0.08960, -0.5928 0.2056, 0.08360, -0.5983 0.1633, 0.07610, -0.5439 0.1261, 0.06710, -0.4975 0.0900, 0.05640, -0.4824 0.0571, 0.04390, -0.3956 0.0283, 0.02940, -0.2079 0.0142, 0.01970, -0.0298 0.0081, 0.01410, 0.0621 0.0026, 0.00780, 0.3772 0.0000, 0.00000, 0.9295 0.0037, -0.00840, 0.8856 0.0112, -0.01420, 0.5609 0.0191, -0.01930, 0.5245 0.0397, -0.03030, 0.3156 0.0706, -0.04420, 0.1097 0.1037, -0.05710, -0.0253 0.1384, -0.06890, -0.1691 0.1741, -0.07950, -0.2953 0.2102, -0.08660, -0.4542 0.2472, -0.09640, -0.5874 0.2844, -0.10270, -0.6843 0.3225, -0.10690, -0.7510 0.3608, -0.10890, -0.8243 0.3991, -0.10830, -0.8222 0.4373, -0.10510, -0.7707 0.4757, -0.09890, -0.6192 0.5137, -0.09070, -0.4674 0.5514, -0.08120, -0.2566 0.5917, -0.06870, -0.0781 0.5917, -0.02380, -0.0942 0.5917, 0.02120, -0.0773 16 Flap element taps 1.0000, 0.00130, 0.0610 0.9365, 0.01390, 0.1359 0.8333, 0.03280, 0.2178 0.7436, 0.04930, 0.0157 0.7049, 0.05670, -0.0907 0.6667, 0.05450, -0.0904 0.6302, 0.03770, -0.0774 0.6083, 0.01980, -0.0749 0.6000, 0.00000, -0.0923 0.6076, -0.01900, -0.1076 0.6285, -0.03060, -0.1479 0.6667, -0.04090, -0.5326 0.7046, -0.04120, -0.5809 0.7429, -0.03210, -0.1670 0.8333, -0.01400, -0.0572 0.9311, -0.00120, -0.0086 Wake drag found for this condition, Cdw=0.0206 --------- Run Conditions: vel=107.1 ft/s Re=1.014x10^6 AOA=6.04 Flap deflection=-10.00 Totals: Cl=0.1888 Cdp=0.0117 Cm(c/4)=0.0609 Cs=0.0082 Ch=-0.0397 Main component: Cl=0.2585 Cdp=0.0159 Cm=-0.0362 Flap component: Cl=-0.0697 Cdp=-0.0042 Cm=0.0499 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.0650 0.5871, 0.07930, -0.1480 0.5501, 0.08690, -0.2738 0.5112, 0.09370, -0.4634 0.4731, 0.09830, -0.6135 0.4349, 0.10070, -0.6844 0.3960, 0.10120, -0.7224 0.3566, 0.10020, -0.7191 0.3172, 0.09790, -0.7180 0.2778, 0.09440, -0.7370 0.2393, 0.08960, -0.7676 0.2056, 0.08360, -0.8041 0.1633, 0.07610, -0.7778 0.1261, 0.06710, -0.7743 0.0900, 0.05640, -0.8224 0.0571, 0.04390, -0.8261 0.0283, 0.02940, -0.7541 0.0142, 0.01970, -0.7016 0.0081, 0.01410, -0.7194 0.0026, 0.00780, -0.2821 0.0000, 0.00000, 0.2550 0.0037, -0.00840, 1.0095 0.0112, -0.01420, 0.8946 0.0191, -0.01930, 0.8147 0.0397, -0.03030, 0.6038 0.0706, -0.04420, 0.3732 0.1037, -0.05710, 0.2134 0.1384, -0.06890, 0.0585 0.1741, -0.07950, -0.0855 0.2102, -0.08660, -0.2599 0.2472, -0.09640, -0.3984 0.2844, -0.10270, -0.5115 0.3225, -0.10690, -0.5921 0.3608, -0.10890, -0.6860 0.3991, -0.10830, -0.7091 0.4373, -0.10510, -0.6888 0.4757, -0.09890, -0.5650 0.5137, -0.09070, -0.4442 0.5514, -0.08120, -0.2480 0.5917, -0.06870, -0.0631 0.5917, -0.02380, -0.0764 0.5917, 0.02120, -0.0692 16 Flap element taps 1.0000, 0.00130, 0.1812 0.9365, 0.01390, 0.1663 0.8333, 0.03280, 0.0843 0.7436, 0.04930, -0.0564 0.7049, 0.05670, -0.0724 0.6667, 0.05450, -0.0755 0.6302, 0.03770, -0.0666 0.6083, 0.01980, -0.0589 0.6000, 0.00000, -0.0678 0.6076, -0.01900, -0.0860 0.6285, -0.03060, -0.0609 0.6667, -0.04090, -0.6431 0.7046, -0.04120, -0.8612 0.7429, -0.03210, -0.2400 0.8333, -0.01400, 0.0379 0.9311, -0.00120, 0.1481 Wake drag found for this condition, Cdw=0.0171 --------- Run Conditions: vel=106.8 ft/s Re=1.010x10^6 AOA=9.05 Flap deflection=-10.00 Totals: Cl=0.3420 Cdp=0.0190 Cm(c/4)=0.0595 Cs=0.0350 Ch=-0.0519 Main component: Cl=0.3851 Cdp=0.0187 Cm=-0.0517 Flap component: Cl=-0.0431 Cdp=0.0003 Cm=0.0260 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.0788 0.5871, 0.07930, -0.1096 0.5501, 0.08690, -0.1783 0.5112, 0.09370, -0.3404 0.4731, 0.09830, -0.5223 0.4349, 0.10070, -0.6354 0.3960, 0.10120, -0.7132 0.3566, 0.10020, -0.7447 0.3172, 0.09790, -0.7713 0.2778, 0.09440, -0.8160 0.2393, 0.08960, -0.8765 0.2056, 0.08360, -0.9442 0.1633, 0.07610, -0.9564 0.1261, 0.06710, -0.9959 0.0900, 0.05640, -1.1069 0.0571, 0.04390, -1.2013 0.0283, 0.02940, -1.2741 0.0142, 0.01970, -1.3942 0.0081, 0.01410, -1.4631 0.0026, 0.00780, -1.0977 0.0000, 0.00000, -0.8642 0.0037, -0.00840, 0.8753 0.0112, -0.01420, 1.0055 0.0191, -0.01930, 0.9586 0.0397, -0.03030, 0.7901 0.0706, -0.04420, 0.5650 0.1037, -0.05710, 0.3966 0.1384, -0.06890, 0.2411 0.1741, -0.07950, 0.0867 0.2102, -0.08660, -0.0980 0.2472, -0.09640, -0.2499 0.2844, -0.10270, -0.3767 0.3225, -0.10690, -0.4773 0.3608, -0.10890, -0.5852 0.3991, -0.10830, -0.6367 0.4373, -0.10510, -0.6298 0.4757, -0.09890, -0.5242 0.5137, -0.09070, -0.4301 0.5514, -0.08120, -0.2490 0.5917, -0.06870, -0.1104 0.5917, -0.02380, -0.0780 0.5917, 0.02120, -0.0726 16 Flap element taps 1.0000, 0.00130, 0.0670 0.9365, 0.01390, -0.0079 0.8333, 0.03280, -0.0563 0.7436, 0.04930, -0.0738 0.7049, 0.05670, -0.0715 0.6667, 0.05450, -0.0795 0.6302, 0.03770, -0.0710 0.6083, 0.01980, -0.0672 0.6000, 0.00000, -0.0948 0.6076, -0.01900, -0.1011 0.6285, -0.03060, 0.1767 0.6667, -0.04090, -0.7099 0.7046, -0.04120, -1.0235 0.7429, -0.03210, -0.2707 0.8333, -0.01400, 0.0418 0.9311, -0.00120, 0.1528 Wake drag found for this condition, Cdw=0.0210 --------- Run Conditions: vel=106.9 ft/s Re=1.011x10^6 AOA=12.06 Flap deflection=-10.00 Totals: Cl=0.4732 Cdp=0.0420 Cm(c/4)=0.0574 Cs=0.0578 Ch=-0.0146 Main component: Cl=0.4640 Cdp=0.0555 Cm=-0.0529 Flap component: Cl=0.0093 Cdp=-0.0135 Cm=-0.0075 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1647 0.5871, 0.07930, -0.1639 0.5501, 0.08690, -0.1789 0.5112, 0.09370, -0.2260 0.4731, 0.09830, -0.3676 0.4349, 0.10070, -0.5175 0.3960, 0.10120, -0.6389 0.3566, 0.10020, -0.7135 0.3172, 0.09790, -0.7757 0.2778, 0.09440, -0.8531 0.2393, 0.08960, -0.9438 0.2056, 0.08360, -1.0475 0.1633, 0.07610, -1.1020 0.1261, 0.06710, -1.1904 0.0900, 0.05640, -1.3685 0.0571, 0.04390, -1.5698 0.0283, 0.02940, -1.8072 0.0142, 0.01970, -2.1288 0.0081, 0.01410, -2.3593 0.0026, 0.00780, -2.0772 0.0000, 0.00000, -2.3936 0.0037, -0.00840, 0.5004 0.0112, -0.01420, 0.9635 0.0191, -0.01930, 1.0027 0.0397, -0.03030, 0.9158 0.0706, -0.04420, 0.7177 0.1037, -0.05710, 0.5520 0.1384, -0.06890, 0.3952 0.1741, -0.07950, 0.2412 0.2102, -0.08660, 0.0539 0.2472, -0.09640, -0.1053 0.2844, -0.10270, -0.2459 0.3225, -0.10690, -0.3647 0.3608, -0.10890, -0.4900 0.3991, -0.10830, -0.5616 0.4373, -0.10510, -0.5868 0.4757, -0.09890, -0.5224 0.5137, -0.09070, -0.4695 0.5514, -0.08120, -0.3633 0.5917, -0.06870, -0.7397 0.5917, -0.02380, -0.3475 0.5917, 0.02120, -0.1996 16 Flap element taps 1.0000, 0.00130, -0.0607 0.9365, 0.01390, -0.0916 0.8333, 0.03280, -0.0867 0.7436, 0.04930, -0.1040 0.7049, 0.05670, -0.1211 0.6667, 0.05450, -0.1589 0.6302, 0.03770, -0.2417 0.6083, 0.01980, -0.4571 0.6000, 0.00000, -1.1715 0.6076, -0.01900, 0.8950 0.6285, -0.03060, 0.2536 0.6667, -0.04090, -0.6510 0.7046, -0.04120, -0.9065 0.7429, -0.03210, -0.1933 0.8333, -0.01400, 0.0328 0.9311, -0.00120, 0.1165 --------- Run Conditions: vel=106.6 ft/s Re=1.008x10^6 AOA=15.04 Flap deflection=-10.00 Totals: Cl=0.6405 Cdp=0.0673 Cm(c/4)=0.0488 Cs=0.1012 Ch=-0.0057 Main component: Cl=0.6023 Cdp=0.0713 Cm=-0.0803 Flap component: Cl=0.0382 Cdp=-0.0040 Cm=-0.0299 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.2997 0.5871, 0.07930, -0.2947 0.5501, 0.08690, -0.3004 0.5112, 0.09370, -0.2993 0.4731, 0.09830, -0.3392 0.4349, 0.10070, -0.4265 0.3960, 0.10120, -0.5431 0.3566, 0.10020, -0.6669 0.3172, 0.09790, -0.7656 0.2778, 0.09440, -0.8760 0.2393, 0.08960, -1.0013 0.2056, 0.08360, -1.1286 0.1633, 0.07610, -1.2468 0.1261, 0.06710, -1.3840 0.0900, 0.05640, -1.6387 0.0571, 0.04390, -1.9600 0.0283, 0.02940, -2.3966 0.0142, 0.01970, -2.9621 0.0081, 0.01410, -3.3908 0.0026, 0.00780, -3.2820 0.0000, 0.00000, -4.4098 0.0037, -0.00840, -0.1274 0.0112, -0.01420, 0.7839 0.0191, -0.01930, 0.9674 0.0397, -0.03030, 0.9915 0.0706, -0.04420, 0.8480 0.1037, -0.05710, 0.6998 0.1384, -0.06890, 0.5432 0.1741, -0.07950, 0.3957 0.2102, -0.08660, 0.2194 0.2472, -0.09640, 0.0553 0.2844, -0.10270, -0.0862 0.3225, -0.10690, -0.2188 0.3608, -0.10890, -0.3472 0.3991, -0.10830, -0.4359 0.4373, -0.10510, -0.4740 0.4757, -0.09890, -0.4288 0.5137, -0.09070, -0.3924 0.5514, -0.08120, -0.3328 0.5917, -0.06870, -0.6866 0.5917, -0.02380, -0.3295 0.5917, 0.02120, -0.3013 16 Flap element taps 1.0000, 0.00130, -0.1529 0.9365, 0.01390, -0.1796 0.8333, 0.03280, -0.1712 0.7436, 0.04930, -0.1922 0.7049, 0.05670, -0.2176 0.6667, 0.05450, -0.2449 0.6302, 0.03770, -0.3961 0.6083, 0.01980, -0.4707 0.6000, 0.00000, -0.9712 0.6076, -0.01900, 0.9282 0.6285, -0.03060, 0.2661 0.6667, -0.04090, -0.6224 0.7046, -0.04120, -0.8961 0.7429, -0.03210, -0.1979 0.8333, -0.01400, 0.0117 0.9311, -0.00120, 0.0734 --------- Run Conditions: vel=105.6 ft/s Re=0.999x10^6 AOA=18.00 Flap deflection=-10.00 Totals: Cl=0.5996 Cdp=0.1377 Cm(c/4)=0.0147 Cs=0.0543 Ch=0.0087 Main component: Cl=0.5117 Cdp=0.1313 Cm=-0.0707 Flap component: Cl=0.0879 Cdp=0.0064 Cm=-0.0677 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.5030 0.5871, 0.07930, -0.5055 0.5501, 0.08690, -0.5149 0.5112, 0.09370, -0.5152 0.4731, 0.09830, -0.5153 0.4349, 0.10070, -0.5209 0.3960, 0.10120, -0.5242 0.3566, 0.10020, -0.5421 0.3172, 0.09790, -0.5422 0.2778, 0.09440, -0.5567 0.2393, 0.08960, -0.6001 0.2056, 0.08360, -0.6966 0.1633, 0.07610, -0.8479 0.1261, 0.06710, -1.0481 0.0900, 0.05640, -1.3514 0.0571, 0.04390, -1.7526 0.0283, 0.02940, -2.2924 0.0142, 0.01970, -2.9407 0.0081, 0.01410, -3.4569 0.0026, 0.00780, -3.4406 0.0000, 0.00000, -4.8303 0.0037, -0.00840, -0.3212 0.0112, -0.01420, 0.7107 0.0191, -0.01930, 0.9407 0.0397, -0.03030, 1.0043 0.0706, -0.04420, 0.8851 0.1037, -0.05710, 0.7458 0.1384, -0.06890, 0.5852 0.1741, -0.07950, 0.4391 0.2102, -0.08660, 0.2668 0.2472, -0.09640, 0.0954 0.2844, -0.10270, -0.0517 0.3225, -0.10690, -0.2002 0.3608, -0.10890, -0.3350 0.3991, -0.10830, -0.4396 0.4373, -0.10510, -0.4891 0.4757, -0.09890, -0.4576 0.5137, -0.09070, -0.4371 0.5514, -0.08120, -0.3655 0.5917, -0.06870, -0.9289 0.5917, -0.02380, -0.4463 0.5917, 0.02120, -0.5611 16 Flap element taps 1.0000, 0.00130, -0.3468 0.9365, 0.01390, -0.3838 0.8333, 0.03280, -0.3749 0.7436, 0.04930, -0.4330 0.7049, 0.05670, -0.4905 0.6667, 0.05450, -0.4133 0.6302, 0.03770, -0.6990 0.6083, 0.01980, -0.6917 0.6000, 0.00000, -1.1175 0.6076, -0.01900, 0.9256 0.6285, -0.03060, 0.2578 0.6667, -0.04090, -0.6866 0.7046, -0.04120, -1.0099 0.7429, -0.03210, -0.2857 0.8333, -0.01400, -0.0775 0.9311, -0.00120, -0.0379 --------- Run Conditions: vel=105.6 ft/s Re=0.997x10^6 AOA=20.00 Flap deflection=-10.00 Totals: Cl=0.5191 Cdp=0.1950 Cm(c/4)=-0.0036 Cs=-0.0057 Ch=0.0112 Main component: Cl=0.4251 Cdp=0.1845 Cm=-0.0697 Flap component: Cl=0.0940 Cdp=0.0105 Cm=-0.0725 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.5960 0.5871, 0.07930, -0.5622 0.5501, 0.08690, -0.5645 0.5112, 0.09370, -0.5707 0.4731, 0.09830, -0.5877 0.4349, 0.10070, -0.5978 0.3960, 0.10120, -0.5905 0.3566, 0.10020, -0.6135 0.3172, 0.09790, -0.6126 0.2778, 0.09440, -0.6163 0.2393, 0.08960, -0.6322 0.2056, 0.08360, -0.6479 0.1633, 0.07610, -0.6838 0.1261, 0.06710, -0.7247 0.0900, 0.05640, -0.8324 0.0571, 0.04390, -1.1019 0.0283, 0.02940, -1.6362 0.0142, 0.01970, -2.2664 0.0081, 0.01410, -2.7681 0.0026, 0.00780, -2.8560 0.0000, 0.00000, -4.0997 0.0037, -0.00840, -0.1691 0.0112, -0.01420, 0.7454 0.0191, -0.01930, 0.9476 0.0397, -0.03030, 1.0014 0.0706, -0.04420, 0.8856 0.1037, -0.05710, 0.7513 0.1384, -0.06890, 0.5918 0.1741, -0.07950, 0.4473 0.2102, -0.08660, 0.2780 0.2472, -0.09640, 0.1042 0.2844, -0.10270, -0.0452 0.3225, -0.10690, -0.1970 0.3608, -0.10890, -0.3375 0.3991, -0.10830, -0.4479 0.4373, -0.10510, -0.5025 0.4757, -0.09890, -0.4754 0.5137, -0.09070, -0.4617 0.5514, -0.08120, -0.3888 0.5917, -0.06870, -1.0191 0.5917, -0.02380, -0.5075 0.5917, 0.02120, -0.6292 16 Flap element taps 1.0000, 0.00130, -0.4128 0.9365, 0.01390, -0.4515 0.8333, 0.03280, -0.4332 0.7436, 0.04930, -0.4831 0.7049, 0.05670, -0.5397 0.6667, 0.05450, -0.4947 0.6302, 0.03770, -0.7752 0.6083, 0.01980, -0.7687 0.6000, 0.00000, -1.1937 0.6076, -0.01900, 0.9196 0.6285, -0.03060, 0.2437 0.6667, -0.04090, -0.7293 0.7046, -0.04120, -1.0756 0.7429, -0.03210, -0.3322 0.8333, -0.01400, -0.1239 0.9311, -0.00120, -0.0877 --------- Run Conditions: vel=105.0 ft/s Re=0.992x10^6 AOA=23.99 Flap deflection=-10.00 Totals: Cl=0.5198 Cdp=0.3116 Cm(c/4)=-0.0350 Cs=-0.0733 Ch=0.0263 Main component: Cl=0.3945 Cdp=0.2940 Cm=-0.0912 Flap component: Cl=0.1253 Cdp=0.0176 Cm=-0.0941 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.8476 0.5871, 0.07930, -0.7439 0.5501, 0.08690, -0.7101 0.5112, 0.09370, -0.6762 0.4731, 0.09830, -0.6877 0.4349, 0.10070, -0.6904 0.3960, 0.10120, -0.6903 0.3566, 0.10020, -0.7105 0.3172, 0.09790, -0.7053 0.2778, 0.09440, -0.7030 0.2393, 0.08960, -0.7028 0.2056, 0.08360, -0.7054 0.1633, 0.07610, -0.7135 0.1261, 0.06710, -0.7208 0.0900, 0.05640, -0.7308 0.0571, 0.04390, -0.7712 0.0283, 0.02940, -0.9211 0.0142, 0.01970, -1.1527 0.0081, 0.01410, -1.4663 0.0026, 0.00780, -1.7375 0.0000, 0.00000, -3.0141 0.0037, -0.00840, -0.0523 0.0112, -0.01420, 0.7434 0.0191, -0.01930, 0.9359 0.0397, -0.03030, 1.0062 0.0706, -0.04420, 0.9167 0.1037, -0.05710, 0.7991 0.1384, -0.06890, 0.6547 0.1741, -0.07950, 0.5191 0.2102, -0.08660, 0.3568 0.2472, -0.09640, 0.1869 0.2844, -0.10270, 0.0373 0.3225, -0.10690, -0.1130 0.3608, -0.10890, -0.2609 0.3991, -0.10830, -0.3803 0.4373, -0.10510, -0.4483 0.4757, -0.09890, -0.4366 0.5137, -0.09070, -0.4380 0.5514, -0.08120, -0.3766 0.5917, -0.06870, -1.2353 0.5917, -0.02380, -0.6788 0.5917, 0.02120, -0.7470 16 Flap element taps 1.0000, 0.00130, -0.4862 0.9365, 0.01390, -0.5352 0.8333, 0.03280, -0.5233 0.7436, 0.04930, -0.5456 0.7049, 0.05670, -0.6153 0.6667, 0.05450, -0.6990 0.6302, 0.03770, -0.9573 0.6083, 0.01980, -0.9616 0.6000, 0.00000, -1.4131 0.6076, -0.01900, 0.9064 0.6285, -0.03060, 0.2769 0.6667, -0.04090, -0.7136 0.7046, -0.04120, -1.0850 0.7429, -0.03210, -0.3520 0.8333, -0.01400, -0.1550 0.9311, -0.00120, -0.1323 --------- Run Conditions: vel=107.1 ft/s Re=1.011x10^6 AOA=26.96 Flap deflection=-10.00 Totals: Cl=0.4902 Cdp=0.3770 Cm(c/4)=-0.0462 Cs=-0.1138 Ch=0.0360 Main component: Cl=0.3505 Cdp=0.3525 Cm=-0.0942 Flap component: Cl=0.1397 Cdp=0.0244 Cm=-0.1039 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.8902 0.5871, 0.07930, -0.7919 0.5501, 0.08690, -0.7424 0.5112, 0.09370, -0.6992 0.4731, 0.09830, -0.6837 0.4349, 0.10070, -0.6777 0.3960, 0.10120, -0.6681 0.3566, 0.10020, -0.6706 0.3172, 0.09790, -0.6619 0.2778, 0.09440, -0.6558 0.2393, 0.08960, -0.6563 0.2056, 0.08360, -0.6617 0.1633, 0.07610, -0.6590 0.1261, 0.06710, -0.6670 0.0900, 0.05640, -0.6866 0.0571, 0.04390, -0.7052 0.0283, 0.02940, -0.7300 0.0142, 0.01970, -0.7465 0.0081, 0.01410, -0.7931 0.0026, 0.00780, -0.7304 0.0000, 0.00000, -1.6466 0.0037, -0.00840, 0.1189 0.0112, -0.01420, 0.7590 0.0191, -0.01930, 0.9338 0.0397, -0.03030, 1.0107 0.0706, -0.04420, 0.9356 0.1037, -0.05710, 0.8323 0.1384, -0.06890, 0.7042 0.1741, -0.07950, 0.5755 0.2102, -0.08660, 0.4133 0.2472, -0.09640, 0.2501 0.2844, -0.10270, 0.0996 0.3225, -0.10690, -0.0481 0.3608, -0.10890, -0.2023 0.3991, -0.10830, -0.3250 0.4373, -0.10510, -0.4049 0.4757, -0.09890, -0.4031 0.5137, -0.09070, -0.4156 0.5514, -0.08120, -0.3633 0.5917, -0.06870, -1.3445 0.5917, -0.02380, -0.7790 0.5917, 0.02120, -0.8094 16 Flap element taps 1.0000, 0.00130, -0.5387 0.9365, 0.01390, -0.5724 0.8333, 0.03280, -0.5500 0.7436, 0.04930, -0.6065 0.7049, 0.05670, -0.6845 0.6667, 0.05450, -0.7830 0.6302, 0.03770, -1.0506 0.6083, 0.01980, -1.0720 0.6000, 0.00000, -1.5655 0.6076, -0.01900, 0.8976 0.6285, -0.03060, 0.2959 0.6667, -0.04090, -0.7010 0.7046, -0.04120, -1.0954 0.7429, -0.03210, -0.3675 0.8333, -0.01400, -0.1742 0.9311, -0.00120, -0.1621