S809 VENTED AILERON MODEL, 18 IN CHORD --------- Run Conditions: vel=113.2 ft/s Re=1.008x10^6 AOA=-6.01 Flap deflection=-30.00 Totals: Cl=-0.7490 Cdp=0.1336 Cm(c/4)=0.1634 Cs=-0.0545 Ch=0.0009 Main component: Cl=-0.4083 Cdp=0.0767 Cm=0.0750 Flap component: Cl=-0.3407 Cdp=0.0570 Cm=0.2780 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.5870 0.5871, 0.07930, -0.1736 0.5501, 0.08690, -0.1494 0.5112, 0.09370, -0.2535 0.4731, 0.09830, -0.3029 0.4349, 0.10070, -0.2880 0.3960, 0.10120, -0.2456 0.3566, 0.10020, -0.1782 0.3172, 0.09790, -0.1270 0.2778, 0.09440, -0.0798 0.2393, 0.08960, -0.0308 0.2056, 0.08360, 0.0305 0.1633, 0.07610, 0.1347 0.1261, 0.06710, 0.2516 0.0900, 0.05640, 0.3865 0.0571, 0.04390, 0.5929 0.0283, 0.02940, 0.8512 0.0142, 0.01970, 0.9935 0.0081, 0.01410, 0.9902 0.0026, 0.00780, 0.7023 0.0000, 0.00000, -0.6913 0.0037, -0.00840, -1.4946 0.0112, -0.01420, -1.5796 0.0191, -0.01930, -1.0075 0.0397, -0.03030, -0.8558 0.0706, -0.04420, -0.8100 0.1037, -0.05710, -0.7840 0.1384, -0.06890, -0.8222 0.1741, -0.07950, -0.8446 0.2102, -0.08660, -0.9034 0.2472, -0.09640, -0.9316 0.2844, -0.10270, -0.9174 0.3225, -0.10690, -0.8478 0.3608, -0.10890, -0.7605 0.3991, -0.10830, -0.5684 0.4373, -0.10510, -0.3209 0.4757, -0.09890, -0.1910 0.5137, -0.09070, -0.1618 0.5514, -0.08120, -0.1665 0.5917, -0.06870, -0.2832 0.5917, -0.02380, -0.6370 0.5917, 0.02120, -0.5959 16 Flap element taps 1.0000, 0.00130, -0.4700 0.9365, 0.01390, 0.2060 0.8333, 0.03280, 0.6558 0.7436, 0.04930, 1.0020 0.7049, 0.05670, 0.3690 0.6667, 0.05450, -0.9997 0.6302, 0.03770, -1.0616 0.6083, 0.01980, -1.1831 0.6000, 0.00000, -2.1326 0.6076, -0.01900, -2.6705 0.6285, -0.03060, -1.2822 0.6667, -0.04090, -0.6234 0.7046, -0.04120, -0.5137 0.7429, -0.03210, -0.4670 0.8333, -0.01400, -0.4804 0.9311, -0.00120, -0.4955 --------- Run Conditions: vel=112.9 ft/s Re=1.004x10^6 AOA=0.01 Flap deflection=-30.00 Totals: Cl=-0.3840 Cdp=0.0985 Cm(c/4)=0.1704 Cs=-0.0985 Ch=-0.0349 Main component: Cl=-0.0482 Cdp=0.0200 Cm=0.0008 Flap component: Cl=-0.3358 Cdp=0.0785 Cm=0.2657 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1700 0.5871, 0.07930, -0.1314 0.5501, 0.08690, -0.1851 0.5112, 0.09370, -0.3332 0.4731, 0.09830, -0.4286 0.4349, 0.10070, -0.4504 0.3960, 0.10120, -0.4480 0.3566, 0.10020, -0.4053 0.3172, 0.09790, -0.3777 0.2778, 0.09440, -0.3623 0.2393, 0.08960, -0.3479 0.2056, 0.08360, -0.3303 0.1633, 0.07610, -0.2550 0.1261, 0.06710, -0.1827 0.0900, 0.05640, -0.1112 0.0571, 0.04390, 0.0431 0.0283, 0.02940, 0.2961 0.0142, 0.01970, 0.5201 0.0081, 0.01410, 0.6774 0.0026, 0.00780, 0.8470 0.0000, 0.00000, 0.9684 0.0037, -0.00840, 0.4022 0.0112, -0.01420, 0.0071 0.0191, -0.01930, 0.1206 0.0397, -0.03030, -0.0160 0.0706, -0.04420, -0.1578 0.1037, -0.05710, -0.2410 0.1384, -0.06890, -0.3500 0.1741, -0.07950, -0.4370 0.2102, -0.08660, -0.5523 0.2472, -0.09640, -0.6310 0.2844, -0.10270, -0.6765 0.3225, -0.10690, -0.6638 0.3608, -0.10890, -0.6486 0.3991, -0.10830, -0.5376 0.4373, -0.10510, -0.3376 0.4757, -0.09890, -0.0878 0.5137, -0.09070, 0.0227 0.5514, -0.08120, 0.0202 0.5917, -0.06870, -0.0323 0.5917, -0.02380, -0.1825 0.5917, 0.02120, -0.1792 16 Flap element taps 1.0000, 0.00130, -0.4488 0.9365, 0.01390, 0.1706 0.8333, 0.03280, 0.6371 0.7436, 0.04930, 0.9824 0.7049, 0.05670, -0.1898 0.6667, 0.05450, -0.4480 0.6302, 0.03770, -0.3779 0.6083, 0.01980, -0.4073 0.6000, 0.00000, -1.2144 0.6076, -0.01900, -2.4975 0.6285, -0.03060, -1.2827 0.6667, -0.04090, -0.6246 0.7046, -0.04120, -0.5051 0.7429, -0.03210, -0.4608 0.8333, -0.01400, -0.4730 0.9311, -0.00120, -0.4930 --------- Run Conditions: vel=113.4 ft/s Re=1.005x10^6 AOA=3.04 Flap deflection=-30.00 Totals: Cl=-0.1397 Cdp=0.0811 Cm(c/4)=0.1611 Cs=-0.0884 Ch=-0.0378 Main component: Cl=0.1682 Cdp=0.0082 Cm=-0.0445 Flap component: Cl=-0.3079 Cdp=0.0729 Cm=0.2394 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.0847 0.5871, 0.07930, -0.1245 0.5501, 0.08690, -0.2100 0.5112, 0.09370, -0.3778 0.4731, 0.09830, -0.4994 0.4349, 0.10070, -0.5424 0.3960, 0.10120, -0.5575 0.3566, 0.10020, -0.5340 0.3172, 0.09790, -0.5235 0.2778, 0.09440, -0.5273 0.2393, 0.08960, -0.5358 0.2056, 0.08360, -0.5396 0.1633, 0.07610, -0.4956 0.1261, 0.06710, -0.4539 0.0900, 0.05640, -0.4347 0.0571, 0.04390, -0.3437 0.0283, 0.02940, -0.1589 0.0142, 0.01970, 0.0106 0.0081, 0.01410, 0.1067 0.0026, 0.00780, 0.4030 0.0000, 0.00000, 0.9334 0.0037, -0.00840, 0.8777 0.0112, -0.01420, 0.5780 0.0191, -0.01930, 0.5439 0.0397, -0.03030, 0.3461 0.0706, -0.04420, 0.1468 0.1037, -0.05710, 0.0293 0.1384, -0.06890, -0.1050 0.1741, -0.07950, -0.2122 0.2102, -0.08660, -0.3436 0.2472, -0.09640, -0.4366 0.2844, -0.10270, -0.5020 0.3225, -0.10690, -0.5158 0.3608, -0.10890, -0.5214 0.3991, -0.10830, -0.4482 0.4373, -0.10510, -0.2830 0.4757, -0.09890, -0.0369 0.5137, -0.09070, 0.1149 0.5514, -0.08120, 0.1209 0.5917, -0.06870, 0.1207 0.5917, -0.02380, -0.0606 0.5917, 0.02120, -0.0880 16 Flap element taps 1.0000, 0.00130, -0.4416 0.9365, 0.01390, 0.1658 0.8333, 0.03280, 0.6682 0.7436, 0.04930, 0.4371 0.7049, 0.05670, -0.1950 0.6667, 0.05450, -0.2631 0.6302, 0.03770, -0.1552 0.6083, 0.01980, -0.1574 0.6000, 0.00000, -0.9134 0.6076, -0.01900, -2.2993 0.6285, -0.03060, -1.2460 0.6667, -0.04090, -0.6103 0.7046, -0.04120, -0.4990 0.7429, -0.03210, -0.4519 0.8333, -0.01400, -0.4638 0.9311, -0.00120, -0.4795 --------- Run Conditions: vel=113.7 ft/s Re=1.007x10^6 AOA=6.04 Flap deflection=-30.00 Totals: Cl=-0.1027 Cdp=0.0506 Cm(c/4)=0.1419 Cs=-0.0611 Ch=-0.0951 Main component: Cl=0.1487 Cdp=-0.0167 Cm=-0.0153 Flap component: Cl=-0.2515 Cdp=0.0673 Cm=0.1814 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.1172 0.5871, 0.07930, 0.0819 0.5501, 0.08690, -0.0050 0.5112, 0.09370, -0.1810 0.4731, 0.09830, -0.3502 0.4349, 0.10070, -0.4376 0.3960, 0.10120, -0.4853 0.3566, 0.10020, -0.5001 0.3172, 0.09790, -0.5156 0.2778, 0.09440, -0.5409 0.2393, 0.08960, -0.5732 0.2056, 0.08360, -0.5954 0.1633, 0.07610, -0.5824 0.1261, 0.06710, -0.5677 0.0900, 0.05640, -0.5895 0.0571, 0.04390, -0.5538 0.0283, 0.02940, -0.4299 0.0142, 0.01970, -0.3192 0.0081, 0.01410, -0.2866 0.0026, 0.00780, 0.0761 0.0000, 0.00000, 0.6584 0.0037, -0.00840, 0.9778 0.0112, -0.01420, 0.7706 0.0191, -0.01930, 0.7043 0.0397, -0.03030, 0.4876 0.0706, -0.04420, 0.2655 0.1037, -0.05710, 0.1239 0.1384, -0.06890, -0.0378 0.1741, -0.07950, -0.1683 0.2102, -0.08660, -0.3206 0.2472, -0.09640, -0.4400 0.2844, -0.10270, -0.5363 0.3225, -0.10690, -0.5922 0.3608, -0.10890, -0.6394 0.3991, -0.10830, -0.6232 0.4373, -0.10510, -0.5188 0.4757, -0.09890, -0.3095 0.5137, -0.09070, -0.0434 0.5514, -0.08120, 0.0719 0.5917, -0.06870, 0.0996 0.5917, -0.02380, 0.0893 0.5917, 0.02120, 0.0936 16 Flap element taps 1.0000, 0.00130, -0.3609 0.9365, 0.01390, 0.0996 0.8333, 0.03280, 0.1355 0.7436, 0.04930, 0.1183 0.7049, 0.05670, 0.1088 0.6667, 0.05450, 0.0744 0.6302, 0.03770, 0.0769 0.6083, 0.01980, 0.1754 0.6000, 0.00000, 0.1996 0.6076, -0.01900, -2.7224 0.6285, -0.03060, -1.5775 0.6667, -0.04090, -0.6340 0.7046, -0.04120, -0.3697 0.7429, -0.03210, -0.3592 0.8333, -0.01400, -0.3779 0.9311, -0.00120, -0.3955 --------- Run Conditions: vel=113.7 ft/s Re=1.006x10^6 AOA=9.03 Flap deflection=-30.00 Totals: Cl=-0.1269 Cdp=0.0439 Cm(c/4)=0.1770 Cs=-0.0632 Ch=-0.1365 Main component: Cl=0.1693 Cdp=-0.0157 Cm=-0.0007 Flap component: Cl=-0.2962 Cdp=0.0596 Cm=0.2073 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.0959 0.5871, 0.07930, 0.0810 0.5501, 0.08690, 0.0483 0.5112, 0.09370, -0.0622 0.4731, 0.09830, -0.2416 0.4349, 0.10070, -0.3612 0.3960, 0.10120, -0.4275 0.3566, 0.10020, -0.4774 0.3172, 0.09790, -0.5156 0.2778, 0.09440, -0.5641 0.2393, 0.08960, -0.6163 0.2056, 0.08360, -0.6524 0.1633, 0.07610, -0.6782 0.1261, 0.06710, -0.6893 0.0900, 0.05640, -0.7604 0.0571, 0.04390, -0.7821 0.0283, 0.02940, -0.7452 0.0142, 0.01970, -0.7244 0.0081, 0.01410, -0.7490 0.0026, 0.00780, -0.3546 0.0000, 0.00000, 0.1381 0.0037, -0.00840, 0.9945 0.0112, -0.01420, 0.9250 0.0191, -0.01930, 0.8458 0.0397, -0.03030, 0.6328 0.0706, -0.04420, 0.3999 0.1037, -0.05710, 0.2429 0.1384, -0.06890, 0.0557 0.1741, -0.07950, -0.0919 0.2102, -0.08660, -0.2528 0.2472, -0.09640, -0.3992 0.2844, -0.10270, -0.5145 0.3225, -0.10690, -0.6065 0.3608, -0.10890, -0.6783 0.3991, -0.10830, -0.7100 0.4373, -0.10510, -0.6502 0.4757, -0.09890, -0.4980 0.5137, -0.09070, -0.2892 0.5514, -0.08120, -0.0477 0.5917, -0.06870, 0.0956 0.5917, -0.02380, 0.0911 0.5917, 0.02120, 0.0896 16 Flap element taps 1.0000, 0.00130, -0.3530 0.9365, 0.01390, 0.0749 0.8333, 0.03280, 0.2198 0.7436, 0.04930, 0.1307 0.7049, 0.05670, -0.1980 0.6667, 0.05450, -0.1232 0.6302, 0.03770, 0.0289 0.6083, 0.01980, 0.8483 0.6000, 0.00000, 0.0623 0.6076, -0.01900, -3.0058 0.6285, -0.03060, -2.3745 0.6667, -0.04090, -1.1716 0.7046, -0.04120, -0.3891 0.7429, -0.03210, -0.3416 0.8333, -0.01400, -0.3561 0.9311, -0.00120, -0.3813 --------- Run Conditions: vel=114.0 ft/s Re=1.009x10^6 AOA=12.02 Flap deflection=-30.00 Totals: Cl=0.0936 Cdp=0.0473 Cm(c/4)=0.1678 Cs=-0.0268 Ch=-0.1179 Main component: Cl=0.3472 Cdp=0.0110 Cm=-0.0333 Flap component: Cl=-0.2535 Cdp=0.0363 Cm=0.1757 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.0242 0.5871, 0.07930, -0.0344 0.5501, 0.08690, -0.0427 0.5112, 0.09370, -0.0860 0.4731, 0.09830, -0.2234 0.4349, 0.10070, -0.3606 0.3960, 0.10120, -0.4543 0.3566, 0.10020, -0.5415 0.3172, 0.09790, -0.6087 0.2778, 0.09440, -0.6829 0.2393, 0.08960, -0.7640 0.2056, 0.08360, -0.8265 0.1633, 0.07610, -0.9001 0.1261, 0.06710, -0.9557 0.0900, 0.05640, -1.1025 0.0571, 0.04390, -1.2260 0.0283, 0.02940, -1.3555 0.0142, 0.01970, -1.5428 0.0081, 0.01410, -1.6283 0.0026, 0.00780, -1.3581 0.0000, 0.00000, -1.2803 0.0037, -0.00840, 0.7716 0.0112, -0.01420, 1.0090 0.0191, -0.01930, 0.9867 0.0397, -0.03030, 0.8337 0.0706, -0.04420, 0.6169 0.1037, -0.05710, 0.4565 0.1384, -0.06890, 0.2640 0.1741, -0.07950, 0.1098 0.2102, -0.08660, -0.0498 0.2472, -0.09640, -0.2108 0.2844, -0.10270, -0.3391 0.3225, -0.10690, -0.4573 0.3608, -0.10890, -0.5442 0.3991, -0.10830, -0.6123 0.4373, -0.10510, -0.5738 0.4757, -0.09890, -0.4562 0.5137, -0.09070, -0.2819 0.5514, -0.08120, -0.0543 0.5917, -0.06870, -0.0197 0.5917, -0.02380, -0.0263 0.5917, 0.02120, -0.0264 16 Flap element taps 1.0000, 0.00130, -0.3534 0.9365, 0.01390, 0.0562 0.8333, 0.03280, 0.1676 0.7436, 0.04930, 0.0502 0.7049, 0.05670, -0.4250 0.6667, 0.05450, -0.3456 0.6302, 0.03770, -0.0188 0.6083, 0.01980, 0.8473 0.6000, 0.00000, 0.1951 0.6076, -0.01900, -2.7123 0.6285, -0.03060, -2.2826 0.6667, -0.04090, -1.1678 0.7046, -0.04120, -0.3745 0.7429, -0.03210, -0.3065 0.8333, -0.01400, -0.3232 0.9311, -0.00120, -0.3520 --------- Run Conditions: vel=114.0 ft/s Re=1.005x10^6 AOA=15.04 Flap deflection=-30.00 Totals: Cl=0.3712 Cdp=0.0557 Cm(c/4)=0.1379 Cs=0.0425 Ch=-0.0865 Main component: Cl=0.5408 Cdp=0.0460 Cm=-0.0720 Flap component: Cl=-0.1696 Cdp=0.0097 Cm=0.1166 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1773 0.5871, 0.07930, -0.1835 0.5501, 0.08690, -0.1841 0.5112, 0.09370, -0.1855 0.4731, 0.09830, -0.2249 0.4349, 0.10070, -0.3140 0.3960, 0.10120, -0.4340 0.3566, 0.10020, -0.5639 0.3172, 0.09790, -0.6726 0.2778, 0.09440, -0.7864 0.2393, 0.08960, -0.9023 0.2056, 0.08360, -1.0075 0.1633, 0.07610, -1.1292 0.1261, 0.06710, -1.2439 0.0900, 0.05640, -1.4706 0.0571, 0.04390, -1.7308 0.0283, 0.02940, -2.0796 0.0142, 0.01970, -2.5421 0.0081, 0.01410, -2.8568 0.0026, 0.00780, -2.7385 0.0000, 0.00000, -3.4811 0.0037, -0.00840, 0.1636 0.0112, -0.01420, 0.8889 0.0191, -0.01930, 1.0043 0.0397, -0.03030, 0.9708 0.0706, -0.04420, 0.8002 0.1037, -0.05710, 0.6501 0.1384, -0.06890, 0.4696 0.1741, -0.07950, 0.3206 0.2102, -0.08660, 0.1578 0.2472, -0.09640, -0.0038 0.2844, -0.10270, -0.1392 0.3225, -0.10690, -0.2631 0.3608, -0.10890, -0.3661 0.3991, -0.10830, -0.4504 0.4373, -0.10510, -0.4325 0.4757, -0.09890, -0.3593 0.5137, -0.09070, -0.3024 0.5514, -0.08120, 0.0225 0.5917, -0.06870, -0.1776 0.5917, -0.02380, -0.1885 0.5917, 0.02120, -0.1874 16 Flap element taps 1.0000, 0.00130, -0.2735 0.9365, 0.01390, 0.0259 0.8333, 0.03280, 0.0223 0.7436, 0.04930, -0.1309 0.7049, 0.05670, -0.6842 0.6667, 0.05450, -0.5943 0.6302, 0.03770, -0.1842 0.6083, 0.01980, 0.7673 0.6000, 0.00000, 0.3760 0.6076, -0.01900, -2.3549 0.6285, -0.03060, -1.9223 0.6667, -0.04090, -1.1284 0.7046, -0.04120, -0.3740 0.7429, -0.03210, -0.2432 0.8333, -0.01400, -0.2586 0.9311, -0.00120, -0.2920 --------- Run Conditions: vel=114.1 ft/s Re=1.007x10^6 AOA=18.01 Flap deflection=-30.00 Totals: Cl=0.3828 Cdp=0.1052 Cm(c/4)=0.1433 Cs=0.0183 Ch=-0.0989 Main component: Cl=0.5676 Cdp=0.1010 Cm=-0.0811 Flap component: Cl=-0.1848 Cdp=0.0042 Cm=0.1253 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.3729 0.5871, 0.07930, -0.4076 0.5501, 0.08690, -0.4108 0.5112, 0.09370, -0.4087 0.4731, 0.09830, -0.4122 0.4349, 0.10070, -0.4215 0.3960, 0.10120, -0.4453 0.3566, 0.10020, -0.4839 0.3172, 0.09790, -0.5611 0.2778, 0.09440, -0.6645 0.2393, 0.08960, -0.8028 0.2056, 0.08360, -0.9446 0.1633, 0.07610, -1.0900 0.1261, 0.06710, -1.2512 0.0900, 0.05640, -1.5177 0.0571, 0.04390, -1.8521 0.0283, 0.02940, -2.3184 0.0142, 0.01970, -2.9202 0.0081, 0.01410, -3.3790 0.0026, 0.00780, -3.3474 0.0000, 0.00000, -4.5788 0.0037, -0.00840, -0.2080 0.0112, -0.01420, 0.7679 0.0191, -0.01930, 0.9707 0.0397, -0.03030, 1.0024 0.0706, -0.04420, 0.8586 0.1037, -0.05710, 0.7173 0.1384, -0.06890, 0.5510 0.1741, -0.07950, 0.3997 0.2102, -0.08660, 0.2257 0.2472, -0.09640, 0.0616 0.2844, -0.10270, -0.0866 0.3225, -0.10690, -0.2163 0.3608, -0.10890, -0.3391 0.3991, -0.10830, -0.4379 0.4373, -0.10510, -0.4446 0.4757, -0.09890, -0.3848 0.5137, -0.09070, -0.3121 0.5514, -0.08120, -0.2126 0.5917, -0.06870, -0.3630 0.5917, -0.02380, -0.3745 0.5917, 0.02120, -0.3806 16 Flap element taps 1.0000, 0.00130, -0.2057 0.9365, 0.01390, -0.0178 0.8333, 0.03280, -0.1133 0.7436, 0.04930, -0.3035 0.7049, 0.05670, -0.9666 0.6667, 0.05450, -0.8758 0.6302, 0.03770, -0.3816 0.6083, 0.01980, 0.6981 0.6000, 0.00000, 0.4069 0.6076, -0.01900, -2.5274 0.6285, -0.03060, -1.9954 0.6667, -0.04090, -1.5677 0.7046, -0.04120, -0.9911 0.7429, -0.03210, -0.3918 0.8333, -0.01400, -0.4090 0.9311, -0.00120, -0.3264 --------- Run Conditions: vel=113.5 ft/s Re=1.001x10^6 AOA=20.00 Flap deflection=-30.00 Totals: Cl=0.1440 Cdp=0.1039 Cm(c/4)=0.1768 Cs=-0.0483 Ch=-0.2346 Main component: Cl=0.4308 Cdp=0.1160 Cm=-0.0497 Flap component: Cl=-0.2868 Cdp=-0.0121 Cm=0.1837 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.4138 0.5871, 0.07930, -0.4384 0.5501, 0.08690, -0.4422 0.5112, 0.09370, -0.4396 0.4731, 0.09830, -0.4390 0.4349, 0.10070, -0.4316 0.3960, 0.10120, -0.4376 0.3566, 0.10020, -0.4246 0.3172, 0.09790, -0.4482 0.2778, 0.09440, -0.4957 0.2393, 0.08960, -0.5756 0.2056, 0.08360, -0.6971 0.1633, 0.07610, -0.8227 0.1261, 0.06710, -0.9918 0.0900, 0.05640, -1.2387 0.0571, 0.04390, -1.5712 0.0283, 0.02940, -2.0288 0.0142, 0.01970, -2.5898 0.0081, 0.01410, -3.0174 0.0026, 0.00780, -2.9922 0.0000, 0.00000, -4.0681 0.0037, -0.00840, -0.0677 0.0112, -0.01420, 0.8105 0.0191, -0.01930, 0.9859 0.0397, -0.03030, 0.9994 0.0706, -0.04420, 0.8424 0.1037, -0.05710, 0.6939 0.1384, -0.06890, 0.5275 0.1741, -0.07950, 0.3641 0.2102, -0.08660, 0.1703 0.2472, -0.09640, -0.0034 0.2844, -0.10270, -0.1711 0.3225, -0.10690, -0.3124 0.3608, -0.10890, -0.4583 0.3991, -0.10830, -0.5750 0.4373, -0.10510, -0.5992 0.4757, -0.09890, -0.5399 0.5137, -0.09070, -0.4547 0.5514, -0.08120, -0.3984 0.5917, -0.06870, -0.3961 0.5917, -0.02380, -0.4150 0.5917, 0.02120, -0.4214 16 Flap element taps 1.0000, 0.00130, 0.0623 0.9365, 0.01390, 0.0126 0.8333, 0.03280, -0.1646 0.7436, 0.04930, -0.3370 0.7049, 0.05670, -1.0022 0.6667, 0.05450, -0.9016 0.6302, 0.03770, -0.4004 0.6083, 0.01980, 0.7366 0.6000, 0.00000, 0.1932 0.6076, -0.01900, -3.4487 0.6285, -0.03060, -2.7976 0.6667, -0.04090, -2.5914 0.7046, -0.04120, -2.4561 0.7429, -0.03210, -0.8117 0.8333, -0.01400, -0.1934 0.9311, -0.00120, 0.0573 --------- Run Conditions: vel=114.1 ft/s Re=1.005x10^6 AOA=24.00 Flap deflection=-30.00 Totals: Cl=0.0176 Cdp=0.1541 Cm(c/4)=0.1540 Cs=-0.1336 Ch=-0.2695 Main component: Cl=0.3135 Cdp=0.1727 Cm=-0.0474 Flap component: Cl=-0.2958 Cdp=-0.0186 Cm=0.1817 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.4594 0.5871, 0.07930, -0.4716 0.5501, 0.08690, -0.4937 0.5112, 0.09370, -0.5011 0.4731, 0.09830, -0.5141 0.4349, 0.10070, -0.5143 0.3960, 0.10120, -0.5382 0.3566, 0.10020, -0.5101 0.3172, 0.09790, -0.5150 0.2778, 0.09440, -0.5255 0.2393, 0.08960, -0.5454 0.2056, 0.08360, -0.5722 0.1633, 0.07610, -0.5586 0.1261, 0.06710, -0.5893 0.0900, 0.05640, -0.6002 0.0571, 0.04390, -0.7017 0.0283, 0.02940, -1.1085 0.0142, 0.01970, -1.7106 0.0081, 0.01410, -2.1933 0.0026, 0.00780, -2.3306 0.0000, 0.00000, -3.3890 0.0037, -0.00840, 0.0114 0.0112, -0.01420, 0.8135 0.0191, -0.01930, 0.9836 0.0397, -0.03030, 1.0079 0.0706, -0.04420, 0.8635 0.1037, -0.05710, 0.7229 0.1384, -0.06890, 0.5705 0.1741, -0.07950, 0.4082 0.2102, -0.08660, 0.2060 0.2472, -0.09640, 0.0339 0.2844, -0.10270, -0.1443 0.3225, -0.10690, -0.2891 0.3608, -0.10890, -0.4505 0.3991, -0.10830, -0.5779 0.4373, -0.10510, -0.6179 0.4757, -0.09890, -0.5701 0.5137, -0.09070, -0.4811 0.5514, -0.08120, -0.4339 0.5917, -0.06870, -0.4200 0.5917, -0.02380, -0.4424 0.5917, 0.02120, -0.4501 16 Flap element taps 1.0000, 0.00130, -0.2451 0.9365, 0.01390, -0.3407 0.8333, 0.03280, -0.4245 0.7436, 0.04930, -0.4505 0.7049, 0.05670, -1.0645 0.6667, 0.05450, -0.9355 0.6302, 0.03770, -0.4241 0.6083, 0.01980, 0.7402 0.6000, 0.00000, 0.1412 0.6076, -0.01900, -3.7082 0.6285, -0.03060, -3.0351 0.6667, -0.04090, -2.8765 0.7046, -0.04120, -2.7201 0.7429, -0.03210, -1.0075 0.8333, -0.01400, -0.3722 0.9311, -0.00120, -0.1371 --------- Run Conditions: vel=113.5 ft/s Re=0.999x10^6 AOA=26.98 Flap deflection=-30.00 Totals: Cl=0.0196 Cdp=0.2040 Cm(c/4)=0.1390 Cs=-0.1729 Ch=-0.2701 Main component: Cl=0.3052 Cdp=0.2297 Cm=-0.0607 Flap component: Cl=-0.2856 Cdp=-0.0257 Cm=0.1723 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.5078 0.5871, 0.07930, -0.5007 0.5501, 0.08690, -0.5235 0.5112, 0.09370, -0.5459 0.4731, 0.09830, -0.5581 0.4349, 0.10070, -0.5646 0.3960, 0.10120, -0.5934 0.3566, 0.10020, -0.5579 0.3172, 0.09790, -0.5574 0.2778, 0.09440, -0.5560 0.2393, 0.08960, -0.5580 0.2056, 0.08360, -0.5839 0.1633, 0.07610, -0.5693 0.1261, 0.06710, -0.6076 0.0900, 0.05640, -0.5940 0.0571, 0.04390, -0.6228 0.0283, 0.02940, -0.7511 0.0142, 0.01970, -1.0108 0.0081, 0.01410, -1.3541 0.0026, 0.00780, -1.5915 0.0000, 0.00000, -2.7236 0.0037, -0.00840, 0.0580 0.0112, -0.01420, 0.8015 0.0191, -0.01930, 0.9742 0.0397, -0.03030, 1.0195 0.0706, -0.04420, 0.8959 0.1037, -0.05710, 0.7701 0.1384, -0.06890, 0.6352 0.1741, -0.07950, 0.4798 0.2102, -0.08660, 0.2765 0.2472, -0.09640, 0.1127 0.2844, -0.10270, -0.0680 0.3225, -0.10690, -0.2101 0.3608, -0.10890, -0.3790 0.3991, -0.10830, -0.5130 0.4373, -0.10510, -0.5707 0.4757, -0.09890, -0.5372 0.5137, -0.09070, -0.4467 0.5514, -0.08120, -0.4245 0.5917, -0.06870, -0.4529 0.5917, -0.02380, -0.4777 0.5917, 0.02120, -0.4876 16 Flap element taps 1.0000, 0.00130, -0.4345 0.9365, 0.01390, -0.5061 0.8333, 0.03280, -0.5223 0.7436, 0.04930, -0.5040 0.7049, 0.05670, -1.1460 0.6667, 0.05450, -0.9999 0.6302, 0.03770, -0.4587 0.6083, 0.01980, 0.7298 0.6000, 0.00000, 0.1697 0.6076, -0.01900, -3.6864 0.6285, -0.03060, -3.0495 0.6667, -0.04090, -2.9423 0.7046, -0.04120, -2.7171 0.7429, -0.03210, -1.0775 0.8333, -0.01400, -0.4592 0.9311, -0.00120, -0.2480