S809 VENTED AILERON MODEL, 18 IN CHORD --------- Run Conditions: vel=114.3 ft/s Re=1.003x10^6 AOA=-6.00 Flap deflection=-30.00 Totals: Cl=-0.8073 Cdp=0.1456 Cm(c/4)=0.1708 Cs=-0.0604 Ch=-0.0319 Main component: Cl=-0.4445 Cdp=0.0570 Cm=0.0819 Flap component: Cl=-0.3628 Cdp=0.0885 Cm=0.2935 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.5309 0.5871, 0.07930, -0.0721 0.5501, 0.08690, -0.2369 0.5112, 0.09370, -0.2615 0.4731, 0.09830, -0.2923 0.4349, 0.10070, -0.2802 0.3960, 0.10120, -0.2412 0.3566, 0.10020, -0.1744 0.3172, 0.09790, -0.1234 0.2778, 0.09440, -0.0855 0.2393, 0.08960, -0.0246 0.2056, 0.08360, 0.0414 0.1633, 0.07610, 0.1451 0.1261, 0.06710, 0.2608 0.0900, 0.05640, 0.4134 0.0571, 0.04390, 0.6106 0.0283, 0.02940, 0.8595 0.0142, 0.01970, 1.0018 0.0081, 0.01410, 0.9854 0.0026, 0.00780, 0.6782 0.0000, 0.00000, -0.7392 0.0037, -0.00840, -1.6808 0.0112, -0.01420, -1.3677 0.0191, -0.01930, -1.1669 0.0397, -0.03030, -0.9244 0.0706, -0.04420, -0.8332 0.1037, -0.05710, -0.8671 0.1384, -0.06890, -0.8805 0.1741, -0.07950, -0.9111 0.2102, -0.08660, -0.9678 0.2472, -0.09640, -1.0113 0.2844, -0.10270, -1.0066 0.3225, -0.10690, -0.9545 0.3608, -0.10890, -0.8876 0.3991, -0.10830, -0.7398 0.4373, -0.10510, -0.4917 0.4757, -0.09890, -0.2167 0.5137, -0.09070, -0.0726 0.5514, -0.08120, -0.0433 0.5917, -0.06870, -0.0765 0.5917, -0.02380, -0.5237 0.5917, 0.02120, -0.5334 16 Flap element taps 1.0000, 0.00130, -0.4818 0.9365, 0.01390, 0.1937 0.8333, 0.03280, 0.6393 0.7436, 0.04930, 1.0006 0.7049, 0.05670, 0.4085 0.6667, 0.05450, -0.9048 0.6302, 0.03770, -0.8408 0.6083, 0.01980, -0.7625 0.6000, 0.00000, -1.7839 0.6076, -0.01900, -3.0341 0.6285, -0.03060, -1.5052 0.6667, -0.04090, -0.6913 0.7046, -0.04120, -0.5525 0.7429, -0.03210, -0.5045 0.8333, -0.01400, -0.4963 0.9311, -0.00120, -0.5128 --------- Run Conditions: vel=115.6 ft/s Re=1.012x10^6 AOA=0.00 Flap deflection=-30.00 Totals: Cl=-0.7186 Cdp=0.0753 Cm(c/4)=0.1699 Cs=-0.0753 Ch=-0.1280 Main component: Cl=-0.3771 Cdp=-0.0634 Cm=0.0936 Flap component: Cl=-0.3414 Cdp=0.1387 Cm=0.2559 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.3350 0.5871, 0.07930, 0.2460 0.5501, 0.08690, -0.1606 0.5112, 0.09370, -0.1473 0.4731, 0.09830, -0.1778 0.4349, 0.10070, -0.2236 0.3960, 0.10120, -0.2444 0.3566, 0.10020, -0.2143 0.3172, 0.09790, -0.1976 0.2778, 0.09440, -0.1934 0.2393, 0.08960, -0.1649 0.2056, 0.08360, -0.1358 0.1633, 0.07610, -0.0587 0.1261, 0.06710, 0.0211 0.0900, 0.05640, 0.1411 0.0571, 0.04390, 0.3078 0.0283, 0.02940, 0.5656 0.0142, 0.01970, 0.8034 0.0081, 0.01410, 0.9084 0.0026, 0.00780, 0.9789 0.0000, 0.00000, 0.5856 0.0037, -0.00840, -0.2692 0.0112, -0.01420, -0.3629 0.0191, -0.01930, -0.3576 0.0397, -0.03030, -0.3714 0.0706, -0.04420, -0.4620 0.1037, -0.05710, -0.5860 0.1384, -0.06890, -0.6653 0.1741, -0.07950, -0.7633 0.2102, -0.08660, -0.8825 0.2472, -0.09640, -0.9844 0.2844, -0.10270, -1.0491 0.3225, -0.10690, -1.0706 0.3608, -0.10890, -1.0754 0.3991, -0.10830, -0.9925 0.4373, -0.10510, -0.9436 0.4757, -0.09890, -0.8895 0.5137, -0.09070, -0.2211 0.5514, -0.08120, 0.0838 0.5917, -0.06870, 0.3088 0.5917, -0.02380, 0.2972 0.5917, 0.02120, 0.3016 16 Flap element taps 1.0000, 0.00130, -0.4128 0.9365, 0.01390, 0.1579 0.8333, 0.03280, 0.3960 0.7436, 0.04930, 0.3437 0.7049, 0.05670, 0.3308 0.6667, 0.05450, 0.2823 0.6302, 0.03770, 0.2948 0.6083, 0.01980, 0.5448 0.6000, 0.00000, -0.1717 0.6076, -0.01900, -3.1863 0.6285, -0.03060, -1.7911 0.6667, -0.04090, -0.7224 0.7046, -0.04120, -0.4379 0.7429, -0.03210, -0.4319 0.8333, -0.01400, -0.4419 0.9311, -0.00120, -0.4627 --------- Run Conditions: vel=115.9 ft/s Re=1.015x10^6 AOA=3.04 Flap deflection=-30.00 Totals: Cl=-0.5485 Cdp=0.0658 Cm(c/4)=0.1807 Cs=-0.0948 Ch=-0.1413 Main component: Cl=-0.1998 Cdp=-0.0577 Cm=0.0628 Flap component: Cl=-0.3486 Cdp=0.1235 Cm=0.2540 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.3209 0.5871, 0.07930, 0.2333 0.5501, 0.08690, -0.0825 0.5112, 0.09370, -0.2215 0.4731, 0.09830, -0.2468 0.4349, 0.10070, -0.2909 0.3960, 0.10120, -0.3147 0.3566, 0.10020, -0.3148 0.3172, 0.09790, -0.3135 0.2778, 0.09440, -0.3263 0.2393, 0.08960, -0.3150 0.2056, 0.08360, -0.2972 0.1633, 0.07610, -0.2593 0.1261, 0.06710, -0.1988 0.0900, 0.05640, -0.1177 0.0571, 0.04390, 0.0082 0.0283, 0.02940, 0.2249 0.0142, 0.01970, 0.4711 0.0081, 0.01410, 0.6267 0.0026, 0.00780, 0.8689 0.0000, 0.00000, 0.9899 0.0037, -0.00840, 0.4943 0.0112, -0.01420, 0.2601 0.0191, -0.01930, 0.1620 0.0397, -0.03030, 0.0213 0.0706, -0.04420, -0.1418 0.1037, -0.05710, -0.3055 0.1384, -0.06890, -0.4282 0.1741, -0.07950, -0.5504 0.2102, -0.08660, -0.6817 0.2472, -0.09640, -0.8122 0.2844, -0.10270, -0.8961 0.3225, -0.10690, -0.9554 0.3608, -0.10890, -0.9859 0.3991, -0.10830, -0.9457 0.4373, -0.10510, -0.8558 0.4757, -0.09890, -0.8435 0.5137, -0.09070, -0.2301 0.5514, -0.08120, 0.0315 0.5917, -0.06870, 0.2982 0.5917, -0.02380, 0.2932 0.5917, 0.02120, 0.2890 16 Flap element taps 1.0000, 0.00130, -0.4117 0.9365, 0.01390, 0.1072 0.8333, 0.03280, 0.3567 0.7436, 0.04930, 0.3964 0.7049, 0.05670, 0.2877 0.6667, 0.05450, 0.2186 0.6302, 0.03770, 0.2740 0.6083, 0.01980, 0.7365 0.6000, 0.00000, -0.0681 0.6076, -0.01900, -3.2498 0.6285, -0.03060, -1.8500 0.6667, -0.04090, -0.9219 0.7046, -0.04120, -0.4294 0.7429, -0.03210, -0.4231 0.8333, -0.01400, -0.4330 0.9311, -0.00120, -0.4572 --------- Run Conditions: vel=116.0 ft/s Re=1.014x10^6 AOA=6.03 Flap deflection=-30.00 Totals: Cl=-0.3387 Cdp=0.0558 Cm(c/4)=0.1855 Cs=-0.0911 Ch=-0.1405 Main component: Cl=0.0044 Cdp=-0.0478 Cm=0.0233 Flap component: Cl=-0.3431 Cdp=0.1036 Cm=0.2450 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.2925 0.5871, 0.07930, 0.1774 0.5501, 0.08690, 0.0805 0.5112, 0.09370, -0.3322 0.4731, 0.09830, -0.3471 0.4349, 0.10070, -0.3839 0.3960, 0.10120, -0.4035 0.3566, 0.10020, -0.4306 0.3172, 0.09790, -0.4445 0.2778, 0.09440, -0.4754 0.2393, 0.08960, -0.4835 0.2056, 0.08360, -0.4781 0.1633, 0.07610, -0.4830 0.1261, 0.06710, -0.4500 0.0900, 0.05640, -0.4212 0.0571, 0.04390, -0.3546 0.0283, 0.02940, -0.2260 0.0142, 0.01970, -0.0358 0.0081, 0.01410, 0.1062 0.0026, 0.00780, 0.3477 0.0000, 0.00000, 0.8759 0.0037, -0.00840, 0.9183 0.0112, -0.01420, 0.7055 0.0191, -0.01930, 0.5710 0.0397, -0.03030, 0.3636 0.0706, -0.04420, 0.1583 0.1037, -0.05710, -0.0275 0.1384, -0.06890, -0.1869 0.1741, -0.07950, -0.3233 0.2102, -0.08660, -0.4593 0.2472, -0.09640, -0.6102 0.2844, -0.10270, -0.7082 0.3225, -0.10690, -0.7983 0.3608, -0.10890, -0.8464 0.3991, -0.10830, -0.8418 0.4373, -0.10510, -0.7438 0.4757, -0.09890, -0.7106 0.5137, -0.09070, -0.2160 0.5514, -0.08120, 0.0166 0.5917, -0.06870, 0.2765 0.5917, -0.02380, 0.2756 0.5917, 0.02120, 0.2737 16 Flap element taps 1.0000, 0.00130, -0.3803 0.9365, 0.01390, 0.0917 0.8333, 0.03280, 0.3458 0.7436, 0.04930, 0.4101 0.7049, 0.05670, 0.2230 0.6667, 0.05450, 0.1590 0.6302, 0.03770, 0.2473 0.6083, 0.01980, 0.8311 0.6000, 0.00000, -0.0155 0.6076, -0.01900, -3.1307 0.6285, -0.03060, -1.7409 0.6667, -0.04090, -1.0632 0.7046, -0.04120, -0.4135 0.7429, -0.03210, -0.3989 0.8333, -0.01400, -0.4087 0.9311, -0.00120, -0.4386 --------- Run Conditions: vel=115.1 ft/s Re=1.006x10^6 AOA=9.01 Flap deflection=-30.00 Totals: Cl=-0.1346 Cdp=0.0490 Cm(c/4)=0.1945 Cs=-0.0695 Ch=-0.1455 Main component: Cl=0.2076 Cdp=-0.0340 Cm=-0.0141 Flap component: Cl=-0.3423 Cdp=0.0830 Cm=0.2399 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.2654 0.5871, 0.07930, 0.1401 0.5501, 0.08690, 0.0025 0.5112, 0.09370, -0.2179 0.4731, 0.09830, -0.4076 0.4349, 0.10070, -0.4926 0.3960, 0.10120, -0.5034 0.3566, 0.10020, -0.5534 0.3172, 0.09790, -0.5850 0.2778, 0.09440, -0.6348 0.2393, 0.08960, -0.6638 0.2056, 0.08360, -0.6737 0.1633, 0.07610, -0.7268 0.1261, 0.06710, -0.7273 0.0900, 0.05640, -0.7628 0.0571, 0.04390, -0.7819 0.0283, 0.02940, -0.7890 0.0142, 0.01970, -0.7296 0.0081, 0.01410, -0.6761 0.0026, 0.00780, -0.4244 0.0000, 0.00000, 0.1346 0.0037, -0.00840, 0.9938 0.0112, -0.01420, 0.9589 0.0191, -0.01930, 0.8547 0.0397, -0.03030, 0.6445 0.0706, -0.04420, 0.4273 0.1037, -0.05710, 0.2321 0.1384, -0.06890, 0.0467 0.1741, -0.07950, -0.1004 0.2102, -0.08660, -0.2351 0.2472, -0.09640, -0.4036 0.2844, -0.10270, -0.5130 0.3225, -0.10690, -0.6282 0.3608, -0.10890, -0.6907 0.3991, -0.10830, -0.7210 0.4373, -0.10510, -0.6298 0.4757, -0.09890, -0.5754 0.5137, -0.09070, -0.4581 0.5514, -0.08120, 0.0455 0.5917, -0.06870, 0.2517 0.5917, -0.02380, 0.2549 0.5917, 0.02120, 0.2573 16 Flap element taps 1.0000, 0.00130, -0.3544 0.9365, 0.01390, 0.0889 0.8333, 0.03280, 0.3449 0.7436, 0.04930, 0.3938 0.7049, 0.05670, 0.1075 0.6667, 0.05450, 0.1062 0.6302, 0.03770, 0.2262 0.6083, 0.01980, 0.8703 0.6000, 0.00000, 0.0540 0.6076, -0.01900, -2.9645 0.6285, -0.03060, -2.0022 0.6667, -0.04090, -1.1587 0.7046, -0.04120, -0.4051 0.7429, -0.03210, -0.3684 0.8333, -0.01400, -0.3777 0.9311, -0.00120, -0.4118 --------- Run Conditions: vel=115.3 ft/s Re=1.005x10^6 AOA=12.04 Flap deflection=-30.00 Totals: Cl=0.0982 Cdp=0.0423 Cm(c/4)=0.1775 Cs=-0.0209 Ch=-0.1247 Main component: Cl=0.3715 Cdp=-0.0037 Cm=-0.0374 Flap component: Cl=-0.2733 Cdp=0.0460 Cm=0.1886 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.0731 0.5871, 0.07930, 0.0485 0.5501, 0.08690, 0.0290 0.5112, 0.09370, -0.0932 0.4731, 0.09830, -0.2882 0.4349, 0.10070, -0.4245 0.3960, 0.10120, -0.4771 0.3566, 0.10020, -0.5819 0.3172, 0.09790, -0.6399 0.2778, 0.09440, -0.7249 0.2393, 0.08960, -0.7868 0.2056, 0.08360, -0.8313 0.1633, 0.07610, -0.9548 0.1261, 0.06710, -1.0117 0.0900, 0.05640, -1.1270 0.0571, 0.04390, -1.2527 0.0283, 0.02940, -1.4483 0.0142, 0.01970, -1.5890 0.0081, 0.01410, -1.7137 0.0026, 0.00780, -1.5860 0.0000, 0.00000, -1.2955 0.0037, -0.00840, 0.7489 0.0112, -0.01420, 1.0056 0.0191, -0.01930, 0.9914 0.0397, -0.03030, 0.8450 0.0706, -0.04420, 0.6483 0.1037, -0.05710, 0.4592 0.1384, -0.06890, 0.2600 0.1741, -0.07950, 0.1085 0.2102, -0.08660, -0.0231 0.2472, -0.09640, -0.2042 0.2844, -0.10270, -0.3206 0.3225, -0.10690, -0.4584 0.3608, -0.10890, -0.5393 0.3991, -0.10830, -0.5986 0.4373, -0.10510, -0.5377 0.4757, -0.09890, -0.4598 0.5137, -0.09070, -0.4383 0.5514, -0.08120, 0.0280 0.5917, -0.06870, 0.0626 0.5917, -0.02380, 0.0682 0.5917, 0.02120, 0.0690 16 Flap element taps 1.0000, 0.00130, -0.3058 0.9365, 0.01390, 0.0586 0.8333, 0.03280, 0.2036 0.7436, 0.04930, 0.1296 0.7049, 0.05670, -0.2808 0.6667, 0.05450, -0.1958 0.6302, 0.03770, 0.0399 0.6083, 0.01980, 0.8240 0.6000, 0.00000, 0.2489 0.6076, -0.01900, -2.6308 0.6285, -0.03060, -2.2018 0.6667, -0.04090, -1.1873 0.7046, -0.04120, -0.3926 0.7429, -0.03210, -0.3177 0.8333, -0.01400, -0.3302 0.9311, -0.00120, -0.3686 --------- Run Conditions: vel=115.3 ft/s Re=1.005x10^6 AOA=15.01 Flap deflection=-30.00 Totals: Cl=0.3620 Cdp=0.0486 Cm(c/4)=0.1507 Cs=0.0468 Ch=-0.0875 Main component: Cl=0.5556 Cdp=0.0321 Cm=-0.0737 Flap component: Cl=-0.1935 Cdp=0.0166 Cm=0.1338 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.0972 0.5871, 0.07930, -0.1207 0.5501, 0.08690, -0.1227 0.5112, 0.09370, -0.1317 0.4731, 0.09830, -0.2271 0.4349, 0.10070, -0.3802 0.3960, 0.10120, -0.4798 0.3566, 0.10020, -0.6255 0.3172, 0.09790, -0.7215 0.2778, 0.09440, -0.8411 0.2393, 0.08960, -0.9380 0.2056, 0.08360, -1.0159 0.1633, 0.07610, -1.1659 0.1261, 0.06710, -1.2641 0.0900, 0.05640, -1.4584 0.0571, 0.04390, -1.7063 0.0283, 0.02940, -2.1008 0.0142, 0.01970, -2.6536 0.0081, 0.01410, -3.0596 0.0026, 0.00780, -3.0908 0.0000, 0.00000, -3.3077 0.0037, -0.00840, 0.1742 0.0112, -0.01420, 0.8791 0.0191, -0.01930, 0.9973 0.0397, -0.03030, 0.9634 0.0706, -0.04420, 0.8144 0.1037, -0.05710, 0.6434 0.1384, -0.06890, 0.4524 0.1741, -0.07950, 0.3048 0.2102, -0.08660, 0.1726 0.2472, -0.09640, -0.0125 0.2844, -0.10270, -0.1359 0.3225, -0.10690, -0.2826 0.3608, -0.10890, -0.3797 0.3991, -0.10830, -0.4618 0.4373, -0.10510, -0.4326 0.4757, -0.09890, -0.3542 0.5137, -0.09070, -0.3111 0.5514, -0.08120, 0.0221 0.5917, -0.06870, -0.1136 0.5917, -0.02380, -0.1104 0.5917, 0.02120, -0.1079 16 Flap element taps 1.0000, 0.00130, -0.2480 0.9365, 0.01390, 0.0621 0.8333, 0.03280, 0.1108 0.7436, 0.04930, -0.0463 0.7049, 0.05670, -0.5765 0.6667, 0.05450, -0.4772 0.6302, 0.03770, -0.1518 0.6083, 0.01980, 0.7369 0.6000, 0.00000, 0.4213 0.6076, -0.01900, -2.2923 0.6285, -0.03060, -1.8534 0.6667, -0.04090, -1.1319 0.7046, -0.04120, -0.3739 0.7429, -0.03210, -0.2399 0.8333, -0.01400, -0.2736 0.9311, -0.00120, -0.2988 --------- Run Conditions: vel=115.4 ft/s Re=1.006x10^6 AOA=18.00 Flap deflection=-30.00 Totals: Cl=0.3153 Cdp=0.0565 Cm(c/4)=0.1865 Cs=0.0437 Ch=-0.1888 Main component: Cl=0.5842 Cdp=0.0520 Cm=-0.0684 Flap component: Cl=-0.2690 Cdp=0.0045 Cm=0.1756 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1875 0.5871, 0.07930, -0.2100 0.5501, 0.08690, -0.2102 0.5112, 0.09370, -0.2048 0.4731, 0.09830, -0.2170 0.4349, 0.10070, -0.2490 0.3960, 0.10120, -0.3099 0.3566, 0.10020, -0.4677 0.3172, 0.09790, -0.6093 0.2778, 0.09440, -0.7654 0.2393, 0.08960, -0.8961 0.2056, 0.08360, -1.0158 0.1633, 0.07610, -1.1989 0.1261, 0.06710, -1.3498 0.0900, 0.05640, -1.5995 0.0571, 0.04390, -1.9441 0.0283, 0.02940, -2.4940 0.0142, 0.01970, -3.0803 0.0081, 0.01410, -4.1050 0.0026, 0.00780, -4.1849 0.0000, 0.00000, -4.7810 0.0037, -0.00840, -0.3329 0.0112, -0.01420, 0.7113 0.0191, -0.01930, 0.9428 0.0397, -0.03030, 0.9999 0.0706, -0.04420, 0.8888 0.1037, -0.05710, 0.7343 0.1384, -0.06890, 0.5549 0.1741, -0.07950, 0.4034 0.2102, -0.08660, 0.2604 0.2472, -0.09640, 0.0717 0.2844, -0.10270, -0.0665 0.3225, -0.10690, -0.2230 0.3608, -0.10890, -0.3445 0.3991, -0.10830, -0.4482 0.4373, -0.10510, -0.4506 0.4757, -0.09890, -0.3860 0.5137, -0.09070, -0.3246 0.5514, -0.08120, -0.2524 0.5917, -0.06870, -0.2046 0.5917, -0.02380, -0.2041 0.5917, 0.02120, -0.2031 16 Flap element taps 1.0000, 0.00130, 0.1247 0.9365, 0.01390, 0.1631 0.8333, 0.03280, 0.0611 0.7436, 0.04930, -0.1751 0.7049, 0.05670, -0.7275 0.6667, 0.05450, -0.6113 0.6302, 0.03770, -0.2437 0.6083, 0.01980, 0.7219 0.6000, 0.00000, 0.3434 0.6076, -0.01900, -2.8143 0.6285, -0.03060, -2.2726 0.6667, -0.04090, -2.0806 0.7046, -0.04120, -1.9182 0.7429, -0.03210, -0.5868 0.8333, -0.01400, -0.1270 0.9311, -0.00120, 0.0747 --------- Run Conditions: vel=115.6 ft/s Re=1.005x10^6 AOA=20.01 Flap deflection=-30.00 Totals: Cl=0.3125 Cdp=0.0741 Cm(c/4)=0.1885 Cs=0.0373 Ch=-0.2032 Main component: Cl=0.5884 Cdp=0.0856 Cm=-0.0716 Flap component: Cl=-0.2759 Cdp=-0.0115 Cm=0.1803 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.3034 0.5871, 0.07930, -0.3135 0.5501, 0.08690, -0.3098 0.5112, 0.09370, -0.3084 0.4731, 0.09830, -0.3171 0.4349, 0.10070, -0.3344 0.3960, 0.10120, -0.3626 0.3566, 0.10020, -0.4601 0.3172, 0.09790, -0.5706 0.2778, 0.09440, -0.7118 0.2393, 0.08960, -0.8400 0.2056, 0.08360, -0.9732 0.1633, 0.07610, -1.1557 0.1261, 0.06710, -1.3255 0.0900, 0.05640, -1.5939 0.0571, 0.04390, -1.9758 0.0283, 0.02940, -2.5849 0.0142, 0.01970, -3.1977 0.0081, 0.01410, -4.4566 0.0026, 0.00780, -4.5471 0.0000, 0.00000, -5.2977 0.0037, -0.00840, -0.5281 0.0112, -0.01420, 0.6383 0.0191, -0.01930, 0.9163 0.0397, -0.03030, 1.0081 0.0706, -0.04420, 0.9114 0.1037, -0.05710, 0.7626 0.1384, -0.06890, 0.5911 0.1741, -0.07950, 0.4377 0.2102, -0.08660, 0.2832 0.2472, -0.09640, 0.0922 0.2844, -0.10270, -0.0580 0.3225, -0.10690, -0.2179 0.3608, -0.10890, -0.3562 0.3991, -0.10830, -0.4680 0.4373, -0.10510, -0.4860 0.4757, -0.09890, -0.4279 0.5137, -0.09070, -0.3629 0.5514, -0.08120, -0.3223 0.5917, -0.06870, -0.3042 0.5917, -0.02380, -0.3061 0.5917, 0.02120, -0.3064 16 Flap element taps 1.0000, 0.00130, 0.1583 0.9365, 0.01390, 0.1549 0.8333, 0.03280, 0.0493 0.7436, 0.04930, -0.2042 0.7049, 0.05670, -0.8454 0.6667, 0.05450, -0.7505 0.6302, 0.03770, -0.3424 0.6083, 0.01980, 0.6950 0.6000, 0.00000, 0.3340 0.6076, -0.01900, -2.9937 0.6285, -0.03060, -2.4628 0.6667, -0.04090, -2.2943 0.7046, -0.04120, -2.0941 0.7429, -0.03210, -0.6799 0.8333, -0.01400, -0.1098 0.9311, -0.00120, 0.1328 --------- Run Conditions: vel=114.8 ft/s Re=0.997x10^6 AOA=23.97 Flap deflection=-30.00 Totals: Cl=-0.1084 Cdp=0.1869 Cm(c/4)=0.1459 Cs=-0.2148 Ch=-0.2790 Main component: Cl=0.1879 Cdp=0.1999 Cm=-0.0272 Flap component: Cl=-0.2963 Cdp=-0.0130 Cm=0.1788 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.5045 0.5871, 0.07930, -0.4984 0.5501, 0.08690, -0.5125 0.5112, 0.09370, -0.5234 0.4731, 0.09830, -0.5326 0.4349, 0.10070, -0.5265 0.3960, 0.10120, -0.5109 0.3566, 0.10020, -0.5133 0.3172, 0.09790, -0.5219 0.2778, 0.09440, -0.5337 0.2393, 0.08960, -0.5173 0.2056, 0.08360, -0.4992 0.1633, 0.07610, -0.5139 0.1261, 0.06710, -0.5095 0.0900, 0.05640, -0.5142 0.0571, 0.04390, -0.5168 0.0283, 0.02940, -0.5351 0.0142, 0.01970, -0.5347 0.0081, 0.01410, -0.5336 0.0026, 0.00780, -0.5069 0.0000, 0.00000, -0.7915 0.0037, -0.00840, 0.6524 0.0112, -0.01420, 0.9796 0.0191, -0.01930, 1.0204 0.0397, -0.03030, 0.9577 0.0706, -0.04420, 0.8025 0.1037, -0.05710, 0.6335 0.1384, -0.06890, 0.4628 0.1741, -0.07950, 0.2998 0.2102, -0.08660, 0.1280 0.2472, -0.09640, -0.0742 0.2844, -0.10270, -0.2403 0.3225, -0.10690, -0.4112 0.3608, -0.10890, -0.5719 0.3991, -0.10830, -0.6949 0.4373, -0.10510, -0.7224 0.4757, -0.09890, -0.6587 0.5137, -0.09070, -0.5834 0.5514, -0.08120, -0.5310 0.5917, -0.06870, -0.4965 0.5917, -0.02380, -0.4997 0.5917, 0.02120, -0.5055 16 Flap element taps 1.0000, 0.00130, -0.4221 0.9365, 0.01390, -0.5272 0.8333, 0.03280, -0.5512 0.7436, 0.04930, -0.5122 0.7049, 0.05670, -1.1523 0.6667, 0.05450, -1.0037 0.6302, 0.03770, -0.5439 0.6083, 0.01980, 0.6571 0.6000, 0.00000, 0.1972 0.6076, -0.01900, -3.7888 0.6285, -0.03060, -3.1712 0.6667, -0.04090, -3.0436 0.7046, -0.04120, -2.8142 0.7429, -0.03210, -1.1321 0.8333, -0.01400, -0.4827 0.9311, -0.00120, -0.2502 --------- Run Conditions: vel=115.1 ft/s Re=0.998x10^6 AOA=26.91 Flap deflection=-30.00 Totals: Cl=0.0071 Cdp=0.2422 Cm(c/4)=0.1210 Cs=-0.2128 Ch=-0.2611 Main component: Cl=0.2598 Cdp=0.2641 Cm=-0.0566 Flap component: Cl=-0.2527 Cdp=-0.0219 Cm=0.1486 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.6020 0.5871, 0.07930, -0.5992 0.5501, 0.08690, -0.6114 0.5112, 0.09370, -0.6197 0.4731, 0.09830, -0.6289 0.4349, 0.10070, -0.6225 0.3960, 0.10120, -0.6168 0.3566, 0.10020, -0.6067 0.3172, 0.09790, -0.6125 0.2778, 0.09440, -0.6228 0.2393, 0.08960, -0.6101 0.2056, 0.08360, -0.6050 0.1633, 0.07610, -0.6077 0.1261, 0.06710, -0.6046 0.0900, 0.05640, -0.6039 0.0571, 0.04390, -0.6049 0.0283, 0.02940, -0.6167 0.0142, 0.01970, -0.6231 0.0081, 0.01410, -0.6262 0.0026, 0.00780, -0.5872 0.0000, 0.00000, -0.8620 0.0037, -0.00840, 0.4974 0.0112, -0.01420, 0.9202 0.0191, -0.01930, 1.0076 0.0397, -0.03030, 0.9927 0.0706, -0.04420, 0.8667 0.1037, -0.05710, 0.7165 0.1384, -0.06890, 0.5645 0.1741, -0.07950, 0.4076 0.2102, -0.08660, 0.2318 0.2472, -0.09640, 0.0390 0.2844, -0.10270, -0.1313 0.3225, -0.10690, -0.2974 0.3608, -0.10890, -0.4682 0.3991, -0.10830, -0.5985 0.4373, -0.10510, -0.6464 0.4757, -0.09890, -0.6035 0.5137, -0.09070, -0.5263 0.5514, -0.08120, -0.4976 0.5917, -0.06870, -0.5956 0.5917, -0.02380, -0.5969 0.5917, 0.02120, -0.6009 16 Flap element taps 1.0000, 0.00130, -0.5419 0.9365, 0.01390, -0.6591 0.8333, 0.03280, -0.6473 0.7436, 0.04930, -0.6022 0.7049, 0.05670, -1.2961 0.6667, 0.05450, -1.1515 0.6302, 0.03770, -0.6540 0.6083, 0.01980, 0.6029 0.6000, 0.00000, 0.2808 0.6076, -0.01900, -3.5997 0.6285, -0.03060, -3.0652 0.6667, -0.04090, -2.9943 0.7046, -0.04120, -2.7284 0.7429, -0.03210, -1.1403 0.8333, -0.01400, -0.5230 0.9311, -0.00120, -0.3127