S809 UNVENTED AILERON, CLEAN, CHORD = 18 IN --------- Run Conditions: vel=101.9 ft/s Re=1.001x10^6 AOA=-5.99 Flap deflection=-20.00 Totals: Cl=-1.0371 Cdp=0.1001 Cm(c/4)=0.0976 Cs=0.0087 Ch=0.1629 Main component: Cl=-0.8632 Cdp=0.0231 Cm=0.2106 Flap component: Cl=-0.1739 Cdp=0.0770 Cm=0.1475 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4146 0.6175, -0.04610, -0.3723 0.5841, -0.02440, -0.3525 0.5775, 0.01750, -0.3622 0.5777, 0.04660, -0.3620 0.6274, 0.07170, 0.5010 0.5694, 0.08320, 0.3077 0.5112, 0.09370, 0.0662 0.4731, 0.09830, 0.0392 0.4349, 0.10070, -0.0077 0.3960, 0.10120, 0.0097 0.3566, 0.10020, 0.0443 0.3172, 0.09790, 0.0985 0.2778, 0.09440, 0.1294 0.2393, 0.08960, 0.1815 0.2056, 0.08360, 0.2363 0.1633, 0.07610, 0.3400 0.1261, 0.06710, 0.4522 0.0900, 0.05640, 0.6001 0.0571, 0.04390, 0.7821 0.0283, 0.02940, 0.9732 0.0142, 0.01970, 1.0075 0.0081, 0.01410, 0.8594 0.0026, 0.00780, 0.1881 0.0000, 0.00000, -2.1052 0.0037, -0.00840, -2.9753 0.0112, -0.01420, -2.4698 0.0191, -0.01930, -2.2733 0.0397, -0.03030, -1.3522 0.0706, -0.04420, -1.2476 0.1037, -0.05710, -1.2472 0.1384, -0.06890, -1.2587 0.1741, -0.07950, -1.2742 0.2102, -0.08660, -1.3398 0.2472, -0.09640, -1.4008 0.2844, -0.10270, -1.4109 0.3225, -0.10690, -1.3847 0.3608, -0.10890, -1.3399 0.3991, -0.10830, -1.2125 0.4373, -0.10510, -1.0098 0.4757, -0.09890, -0.7067 0.5137, -0.09070, -0.5214 0.5694, -0.07640, -0.4306 15 Flap element taps 1.0000, 0.00130, -0.3913 0.9365, 0.01390, -0.0468 0.8333, 0.03280, 0.1471 0.7436, 0.04930, 0.3112 0.7049, 0.05670, 0.4340 0.6662, 0.06410, 0.5475 0.6522, 0.01390, -0.3556 0.5969, -0.00020, -0.3744 0.6000, -0.03020, -0.3967 0.6324, -0.04540, -0.3834 0.6667, -0.04880, -0.3899 0.7046, -0.04110, -0.3942 0.7429, -0.03210, -0.4049 0.8333, -0.01400, -0.4292 0.9311, -0.00120, -0.4106 --------- Run Conditions: vel=102.2 ft/s Re=1.003x10^6 AOA=0.02 Flap deflection=-20.00 Totals: Cl=-0.8661 Cdp=0.0569 Cm(c/4)=0.1227 Cs=-0.0572 Ch=0.1374 Main component: Cl=-0.7111 Cdp=0.0103 Cm=0.2134 Flap component: Cl=-0.1550 Cdp=0.0466 Cm=0.1258 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4494 0.6175, -0.04610, -0.2930 0.5841, -0.02440, -0.2719 0.5775, 0.01750, -0.2785 0.5777, 0.04660, -0.2748 0.6274, 0.07170, 0.4708 0.5694, 0.08320, 0.3137 0.5112, 0.09370, -0.0383 0.4731, 0.09830, -0.0492 0.4349, 0.10070, -0.1029 0.3960, 0.10120, -0.1276 0.3566, 0.10020, -0.1029 0.3172, 0.09790, -0.0709 0.2778, 0.09440, -0.0604 0.2393, 0.08960, -0.0378 0.2056, 0.08360, -0.0190 0.1633, 0.07610, 0.0747 0.1261, 0.06710, 0.1528 0.0900, 0.05640, 0.2829 0.0571, 0.04390, 0.4542 0.0283, 0.02940, 0.7106 0.0142, 0.01970, 0.9258 0.0081, 0.01410, 0.9688 0.0026, 0.00780, 0.8989 0.0000, 0.00000, 0.1362 0.0037, -0.00840, -0.8617 0.0112, -0.01420, -0.8241 0.0191, -0.01930, -0.7407 0.0397, -0.03030, -0.6547 0.0706, -0.04420, -0.7098 0.1037, -0.05710, -0.8146 0.1384, -0.06890, -0.8941 0.1741, -0.07950, -0.9927 0.2102, -0.08660, -1.1362 0.2472, -0.09640, -1.2554 0.2844, -0.10270, -1.3442 0.3225, -0.10690, -1.3951 0.3608, -0.10890, -1.4438 0.3991, -0.10830, -1.4227 0.4373, -0.10510, -1.3425 0.4757, -0.09890, -1.2684 0.5137, -0.09070, -1.0689 0.5694, -0.07640, -0.6334 15 Flap element taps 1.0000, 0.00130, -0.2708 0.9365, 0.01390, 0.0169 0.8333, 0.03280, 0.1644 0.7436, 0.04930, 0.3070 0.7049, 0.05670, 0.4188 0.6662, 0.06410, 0.5226 0.6522, 0.01390, -0.2727 0.5969, -0.00020, -0.2934 0.6000, -0.03020, -0.3517 0.6324, -0.04540, -0.3332 0.6667, -0.04880, -0.3110 0.7046, -0.04110, -0.2779 0.7429, -0.03210, -0.2837 0.8333, -0.01400, -0.3050 0.9311, -0.00120, -0.2984 --------- Run Conditions: vel=102.7 ft/s Re=1.006x10^6 AOA=3.04 Flap deflection=-20.00 Totals: Cl=-0.5937 Cdp=0.0523 Cm(c/4)=0.1251 Cs=-0.0837 Ch=0.1270 Main component: Cl=-0.4470 Cdp=0.0168 Cm=0.1555 Flap component: Cl=-0.1466 Cdp=0.0355 Cm=0.1171 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4227 0.6175, -0.04610, -0.2884 0.5841, -0.02440, -0.2661 0.5775, 0.01750, -0.2761 0.5777, 0.04660, -0.2748 0.6274, 0.07170, 0.4319 0.5694, 0.08320, 0.2795 0.5112, 0.09370, -0.1584 0.4731, 0.09830, -0.1658 0.4349, 0.10070, -0.2148 0.3960, 0.10120, -0.2606 0.3566, 0.10020, -0.2455 0.3172, 0.09790, -0.2281 0.2778, 0.09440, -0.2337 0.2393, 0.08960, -0.2297 0.2056, 0.08360, -0.2386 0.1633, 0.07610, -0.1613 0.1261, 0.06710, -0.1136 0.0900, 0.05640, -0.0122 0.0571, 0.04390, 0.1196 0.0283, 0.02940, 0.3514 0.0142, 0.01970, 0.6098 0.0081, 0.01410, 0.7312 0.0026, 0.00780, 0.9530 0.0000, 0.00000, 0.9300 0.0037, -0.00840, 0.2632 0.0112, -0.01420, 0.0458 0.0191, -0.01930, -0.0253 0.0397, -0.03030, -0.1211 0.0706, -0.04420, -0.2810 0.1037, -0.05710, -0.4365 0.1384, -0.06890, -0.5483 0.1741, -0.07950, -0.6741 0.2102, -0.08660, -0.8449 0.2472, -0.09640, -0.9772 0.2844, -0.10270, -1.0917 0.3225, -0.10690, -1.1614 0.3608, -0.10890, -1.2327 0.3991, -0.10830, -1.2400 0.4373, -0.10510, -1.1879 0.4757, -0.09890, -1.0904 0.5137, -0.09070, -1.0823 0.5694, -0.07640, -0.5697 15 Flap element taps 1.0000, 0.00130, -0.2514 0.9365, 0.01390, 0.0029 0.8333, 0.03280, 0.1371 0.7436, 0.04930, 0.2748 0.7049, 0.05670, 0.3834 0.6662, 0.06410, 0.4897 0.6522, 0.01390, -0.2685 0.5969, -0.00020, -0.2884 0.6000, -0.03020, -0.3475 0.6324, -0.04540, -0.3332 0.6667, -0.04880, -0.3102 0.7046, -0.04110, -0.2644 0.7429, -0.03210, -0.2751 0.8333, -0.01400, -0.2973 0.9311, -0.00120, -0.2843 --------- Run Conditions: vel=103.1 ft/s Re=1.007x10^6 AOA=6.05 Flap deflection=-20.00 Totals: Cl=-0.3166 Cdp=0.0484 Cm(c/4)=0.1249 Cs=-0.0815 Ch=0.1191 Main component: Cl=-0.1778 Cdp=0.0232 Cm=0.0927 Flap component: Cl=-0.1387 Cdp=0.0252 Cm=0.1096 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3931 0.6175, -0.04610, -0.2859 0.5841, -0.02440, -0.2631 0.5775, 0.01750, -0.2723 0.5777, 0.04660, -0.2708 0.6274, 0.07170, 0.3924 0.5694, 0.08320, 0.2015 0.5112, 0.09370, -0.2574 0.4731, 0.09830, -0.2955 0.4349, 0.10070, -0.3370 0.3960, 0.10120, -0.3944 0.3566, 0.10020, -0.3915 0.3172, 0.09790, -0.3913 0.2778, 0.09440, -0.4091 0.2393, 0.08960, -0.4291 0.2056, 0.08360, -0.4635 0.1633, 0.07610, -0.4128 0.1261, 0.06710, -0.3996 0.0900, 0.05640, -0.3455 0.0571, 0.04390, -0.2776 0.0283, 0.02940, -0.1303 0.0142, 0.01970, 0.0841 0.0081, 0.01410, 0.2031 0.0026, 0.00780, 0.5065 0.0000, 0.00000, 0.9679 0.0037, -0.00840, 0.8668 0.0112, -0.01420, 0.6216 0.0191, -0.01930, 0.4881 0.0397, -0.03030, 0.2998 0.0706, -0.04420, 0.0825 0.1037, -0.05710, -0.1042 0.1384, -0.06890, -0.2385 0.1741, -0.07950, -0.3818 0.2102, -0.08660, -0.5716 0.2472, -0.09640, -0.7141 0.2844, -0.10270, -0.8479 0.3225, -0.10690, -0.9352 0.3608, -0.10890, -1.0250 0.3991, -0.10830, -1.0561 0.4373, -0.10510, -1.0387 0.4757, -0.09890, -0.9285 0.5137, -0.09070, -0.9109 0.5694, -0.07640, -0.5038 15 Flap element taps 1.0000, 0.00130, -0.2300 0.9365, 0.01390, -0.0001 0.8333, 0.03280, 0.1150 0.7436, 0.04930, 0.2466 0.7049, 0.05670, 0.3540 0.6662, 0.06410, 0.4600 0.6522, 0.01390, -0.2666 0.5969, -0.00020, -0.2881 0.6000, -0.03020, -0.3424 0.6324, -0.04540, -0.3305 0.6667, -0.04880, -0.3042 0.7046, -0.04110, -0.2476 0.7429, -0.03210, -0.2576 0.8333, -0.01400, -0.2866 0.9311, -0.00120, -0.2764 --------- Run Conditions: vel=103.1 ft/s Re=1.006x10^6 AOA=9.02 Flap deflection=-20.00 Totals: Cl=-0.0492 Cdp=0.0435 Cm(c/4)=0.1269 Cs=-0.0507 Ch=0.1105 Main component: Cl=0.0793 Cdp=0.0309 Cm=0.0363 Flap component: Cl=-0.1285 Cdp=0.0126 Cm=0.1011 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3651 0.6175, -0.04610, -0.2984 0.5841, -0.02440, -0.2747 0.5775, 0.01750, -0.2869 0.5777, 0.04660, -0.2888 0.6274, 0.07170, 0.3432 0.5694, 0.08320, 0.1408 0.5112, 0.09370, -0.1584 0.4731, 0.09830, -0.3721 0.4349, 0.10070, -0.4733 0.3960, 0.10120, -0.5321 0.3566, 0.10020, -0.5416 0.3172, 0.09790, -0.5555 0.2778, 0.09440, -0.5923 0.2393, 0.08960, -0.6366 0.2056, 0.08360, -0.6982 0.1633, 0.07610, -0.6828 0.1261, 0.06710, -0.7134 0.0900, 0.05640, -0.7201 0.0571, 0.04390, -0.7476 0.0283, 0.02940, -0.7437 0.0142, 0.01970, -0.6617 0.0081, 0.01410, -0.6420 0.0026, 0.00780, -0.3611 0.0000, 0.00000, 0.2531 0.0037, -0.00840, 1.0040 0.0112, -0.01420, 0.9360 0.0191, -0.01930, 0.8274 0.0397, -0.03030, 0.6279 0.0706, -0.04420, 0.3915 0.1037, -0.05710, 0.1928 0.1384, -0.06890, 0.0425 0.1741, -0.07950, -0.1120 0.2102, -0.08660, -0.3128 0.2472, -0.09640, -0.4622 0.2844, -0.10270, -0.6111 0.3225, -0.10690, -0.7141 0.3608, -0.10890, -0.8194 0.3991, -0.10830, -0.8765 0.4373, -0.10510, -0.8913 0.4757, -0.09890, -0.7881 0.5137, -0.09070, -0.7511 0.5694, -0.07640, -0.4240 15 Flap element taps 1.0000, 0.00130, -0.1814 0.9365, 0.01390, 0.0075 0.8333, 0.03280, 0.1027 0.7436, 0.04930, 0.2252 0.7049, 0.05670, 0.3260 0.6662, 0.06410, 0.3975 0.6522, 0.01390, -0.2797 0.5969, -0.00020, -0.3008 0.6000, -0.03020, -0.3476 0.6324, -0.04540, -0.3398 0.6667, -0.04880, -0.3005 0.7046, -0.04110, -0.2248 0.7429, -0.03210, -0.2323 0.8333, -0.01400, -0.2626 0.9311, -0.00120, -0.2513 --------- Run Conditions: vel=103.1 ft/s Re=1.005x10^6 AOA=12.02 Flap deflection=-20.00 Totals: Cl=0.1814 Cdp=0.0380 Cm(c/4)=0.1323 Cs=0.0006 Ch=0.1061 Main component: Cl=0.2924 Cdp=0.0499 Cm=-0.0042 Flap component: Cl=-0.1110 Cdp=-0.0119 Cm=0.0901 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3606 0.6175, -0.04610, -0.3745 0.5841, -0.02440, -0.3581 0.5775, 0.01750, -0.3722 0.5777, 0.04660, -0.3724 0.6274, 0.07170, 0.0918 0.5694, 0.08320, 0.0671 0.5112, 0.09370, -0.1539 0.4731, 0.09830, -0.3533 0.4349, 0.10070, -0.4892 0.3960, 0.10120, -0.5750 0.3566, 0.10020, -0.6249 0.3172, 0.09790, -0.6533 0.2778, 0.09440, -0.7169 0.2393, 0.08960, -0.7937 0.2056, 0.08360, -0.8946 0.1633, 0.07610, -0.9388 0.1261, 0.06710, -1.0336 0.0900, 0.05640, -1.1163 0.0571, 0.04390, -1.2591 0.0283, 0.02940, -1.4511 0.0142, 0.01970, -1.5761 0.0081, 0.01410, -1.7565 0.0026, 0.00780, -1.6426 0.0000, 0.00000, -1.2480 0.0037, -0.00840, 0.7636 0.0112, -0.01420, 0.9997 0.0191, -0.01930, 0.9827 0.0397, -0.03030, 0.8517 0.0706, -0.04420, 0.6324 0.1037, -0.05710, 0.4396 0.1384, -0.06890, 0.2816 0.1741, -0.07950, 0.1241 0.2102, -0.08660, -0.0801 0.2472, -0.09640, -0.2350 0.2844, -0.10270, -0.3937 0.3225, -0.10690, -0.5120 0.3608, -0.10890, -0.6306 0.3991, -0.10830, -0.7098 0.4373, -0.10510, -0.7546 0.4757, -0.09890, -0.6765 0.5137, -0.09070, -0.6536 0.5694, -0.07640, -0.5532 15 Flap element taps 1.0000, 0.00130, -0.0826 0.9365, 0.01390, 0.0616 0.8333, 0.03280, 0.1325 0.7436, 0.04930, 0.1953 0.7049, 0.05670, 0.1779 0.6662, 0.06410, 0.0984 0.6522, 0.01390, -0.3642 0.5969, -0.00020, -0.3742 0.6000, -0.03020, -0.4137 0.6324, -0.04540, -0.4043 0.6667, -0.04880, -0.3386 0.7046, -0.04110, -0.2016 0.7429, -0.03210, -0.2021 0.8333, -0.01400, -0.2248 0.9311, -0.00120, -0.1877 --------- Run Conditions: vel=103.7 ft/s Re=1.007x10^6 AOA=15.00 Flap deflection=-20.00 Totals: Cl=0.4529 Cdp=0.0207 Cm(c/4)=0.0819 Cs=0.0973 Ch=0.0098 Main component: Cl=0.4692 Cdp=0.0293 Cm=-0.0418 Flap component: Cl=-0.0163 Cdp=-0.0086 Cm=0.0131 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1739 0.6175, -0.04610, -0.1976 0.5841, -0.02440, -0.3372 0.5775, 0.01750, -0.1567 0.5777, 0.04660, -0.2417 0.6274, 0.07170, -0.0746 0.5694, 0.08320, -0.0232 0.5112, 0.09370, -0.0936 0.4731, 0.09830, -0.0797 0.4349, 0.10070, -0.1211 0.3960, 0.10120, -0.4713 0.3566, 0.10020, -0.6013 0.3172, 0.09790, -0.6865 0.2778, 0.09440, -0.7934 0.2393, 0.08960, -0.9080 0.2056, 0.08360, -1.0154 0.1633, 0.07610, -1.1312 0.1261, 0.06710, -1.2450 0.0900, 0.05640, -1.4219 0.0571, 0.04390, -1.6635 0.0283, 0.02940, -2.0661 0.0142, 0.01970, -2.5577 0.0081, 0.01410, -2.9120 0.0026, 0.00780, -3.1607 0.0000, 0.00000, -3.1190 0.0037, -0.00840, 0.2428 0.0112, -0.01420, 0.9060 0.0191, -0.01930, 1.0055 0.0397, -0.03030, 0.9675 0.0706, -0.04420, 0.7923 0.1037, -0.05710, 0.6185 0.1384, -0.06890, 0.4422 0.1741, -0.07950, 0.2807 0.2102, -0.08660, 0.1073 0.2472, -0.09640, -0.0845 0.2844, -0.10270, -0.2310 0.3225, -0.10690, -0.3850 0.3608, -0.10890, -0.5331 0.3991, -0.10830, -0.6352 0.4373, -0.10510, -0.6872 0.4757, -0.09890, -0.6535 0.5137, -0.09070, -0.1167 0.5694, -0.07640, -0.1824 15 Flap element taps 1.0000, 0.00130, -0.0133 0.9365, 0.01390, 0.0420 0.8333, 0.03280, -0.0227 0.7436, 0.04930, -0.0670 0.7049, 0.05670, -0.0584 0.6662, 0.06410, -0.0410 0.6522, 0.01390, -0.2256 0.5969, -0.00020, -0.1262 0.6000, -0.03020, -0.0490 0.6324, -0.04540, -0.2387 0.6667, -0.04880, -0.3554 0.7046, -0.04110, -0.1348 0.7429, -0.03210, -0.0830 0.8333, -0.01400, -0.0104 0.9311, -0.00120, 0.0025 --------- Run Conditions: vel=103.5 ft/s Re=1.005x10^6 AOA=18.00 Flap deflection=-20.00 Totals: Cl=0.5621 Cdp=0.0568 Cm(c/4)=0.0845 Cs=0.1197 Ch=-0.0076 Main component: Cl=0.5642 Cdp=0.1120 Cm=-0.0617 Flap component: Cl=-0.0021 Cdp=-0.0552 Cm=0.0082 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5424 0.6175, -0.04610, -0.6937 0.5841, -0.02440, -0.6819 0.5775, 0.01750, -0.6845 0.5777, 0.04660, -0.6911 0.6274, 0.07170, -0.3101 0.5694, 0.08320, -0.3167 0.5112, 0.09370, -0.3098 0.4731, 0.09830, -0.3102 0.4349, 0.10070, -0.3545 0.3960, 0.10120, -0.4240 0.3566, 0.10020, -0.5546 0.3172, 0.09790, -0.6613 0.2778, 0.09440, -0.7927 0.2393, 0.08960, -0.9319 0.2056, 0.08360, -1.0696 0.1633, 0.07610, -1.2308 0.1261, 0.06710, -1.3940 0.0900, 0.05640, -1.6410 0.0571, 0.04390, -1.9995 0.0283, 0.02940, -2.5752 0.0142, 0.01970, -3.1857 0.0081, 0.01410, -4.1808 0.0026, 0.00780, -4.6394 0.0000, 0.00000, -5.0133 0.0037, -0.00840, -0.4092 0.0112, -0.01420, 0.6902 0.0191, -0.01930, 0.9346 0.0397, -0.03030, 1.0108 0.0706, -0.04420, 0.8939 0.1037, -0.05710, 0.7464 0.1384, -0.06890, 0.5793 0.1741, -0.07950, 0.4225 0.2102, -0.08660, 0.2553 0.2472, -0.09640, 0.0648 0.2844, -0.10270, -0.0859 0.3225, -0.10690, -0.2478 0.3608, -0.10890, -0.4030 0.3991, -0.10830, -0.5201 0.4373, -0.10510, -0.5920 0.4757, -0.09890, -0.5765 0.5137, -0.09070, -0.5868 0.5694, -0.07640, -0.5026 15 Flap element taps 1.0000, 0.00130, 0.1306 0.9365, 0.01390, 0.0665 0.8333, 0.03280, -0.1086 0.7436, 0.04930, -0.2454 0.7049, 0.05670, -0.2861 0.6662, 0.06410, -0.3135 0.6522, 0.01390, -0.6792 0.5969, -0.00020, -0.6906 0.6000, -0.03020, -0.7172 0.6324, -0.04540, -0.7282 0.6667, -0.04880, -0.8557 0.7046, -0.04110, -0.4317 0.7429, -0.03210, -0.2054 0.8333, -0.01400, 0.0299 0.9311, -0.00120, 0.1521 --------- Run Conditions: vel=103.0 ft/s Re=0.997x10^6 AOA=19.98 Flap deflection=-20.00 Totals: Cl=0.5413 Cdp=0.0943 Cm(c/4)=0.0590 Cs=0.0964 Ch=-0.0530 Main component: Cl=0.5085 Cdp=0.1411 Cm=-0.0548 Flap component: Cl=0.0328 Cdp=-0.0469 Cm=-0.0214 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6201 0.6175, -0.04610, -0.7991 0.5841, -0.02440, -0.7833 0.5775, 0.01750, -0.7854 0.5777, 0.04660, -0.7927 0.6274, 0.07170, -0.4433 0.5694, 0.08320, -0.4567 0.5112, 0.09370, -0.4498 0.4731, 0.09830, -0.4316 0.4349, 0.10070, -0.4194 0.3960, 0.10120, -0.3946 0.3566, 0.10020, -0.4228 0.3172, 0.09790, -0.4444 0.2778, 0.09440, -0.5270 0.2393, 0.08960, -0.6680 0.2056, 0.08360, -0.8326 0.1633, 0.07610, -1.0338 0.1261, 0.06710, -1.2327 0.0900, 0.05640, -1.5115 0.0571, 0.04390, -1.9063 0.0283, 0.02940, -2.5384 0.0142, 0.01970, -3.1722 0.0081, 0.01410, -4.3315 0.0026, 0.00780, -4.8459 0.0000, 0.00000, -5.3279 0.0037, -0.00840, -0.5551 0.0112, -0.01420, 0.6306 0.0191, -0.01930, 0.9083 0.0397, -0.03030, 1.0144 0.0706, -0.04420, 0.9151 0.1037, -0.05710, 0.7737 0.1384, -0.06890, 0.6047 0.1741, -0.07950, 0.4490 0.2102, -0.08660, 0.2837 0.2472, -0.09640, 0.0865 0.2844, -0.10270, -0.0680 0.3225, -0.10690, -0.2416 0.3608, -0.10890, -0.4023 0.3991, -0.10830, -0.5345 0.4373, -0.10510, -0.6142 0.4757, -0.09890, -0.6115 0.5137, -0.09070, -0.6335 0.5694, -0.07640, -0.5602 15 Flap element taps 1.0000, 0.00130, -0.1396 0.9365, 0.01390, -0.2448 0.8333, 0.03280, -0.3631 0.7436, 0.04930, -0.4219 0.7049, 0.05670, -0.4329 0.6662, 0.06410, -0.4395 0.6522, 0.01390, -0.7810 0.5969, -0.00020, -0.7954 0.6000, -0.03020, -0.8247 0.6324, -0.04540, -0.8359 0.6667, -0.04880, -0.9989 0.7046, -0.04110, -0.5524 0.7429, -0.03210, -0.3126 0.8333, -0.01400, -0.0765 0.9311, -0.00120, 0.0179 --------- Run Conditions: vel=104.1 ft/s Re=1.007x10^6 AOA=23.97 Flap deflection=-20.00 Totals: Cl=0.1493 Cdp=0.2205 Cm(c/4)=0.0382 Cs=-0.1408 Ch=-0.0440 Main component: Cl=0.1399 Cdp=0.2665 Cm=-0.0151 Flap component: Cl=0.0094 Cdp=-0.0460 Cm=-0.0032 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8742 0.6175, -0.04610, -1.0890 0.5841, -0.02440, -1.0682 0.5775, 0.01750, -1.0711 0.5777, 0.04660, -1.0774 0.6274, 0.07170, -0.5338 0.5694, 0.08320, -0.5594 0.5112, 0.09370, -0.5670 0.4731, 0.09830, -0.5533 0.4349, 0.10070, -0.5495 0.3960, 0.10120, -0.5227 0.3566, 0.10020, -0.5474 0.3172, 0.09790, -0.5363 0.2778, 0.09440, -0.5340 0.2393, 0.08960, -0.5325 0.2056, 0.08360, -0.5193 0.1633, 0.07610, -0.5404 0.1261, 0.06710, -0.5298 0.0900, 0.05640, -0.5337 0.0571, 0.04390, -0.5328 0.0283, 0.02940, -0.5546 0.0142, 0.01970, -0.5500 0.0081, 0.01410, -0.5448 0.0026, 0.00780, -0.5558 0.0000, 0.00000, -0.8044 0.0037, -0.00840, 0.6070 0.0112, -0.01420, 0.9638 0.0191, -0.01930, 1.0116 0.0397, -0.03030, 0.9688 0.0706, -0.04420, 0.8225 0.1037, -0.05710, 0.6689 0.1384, -0.06890, 0.4898 0.1741, -0.07950, 0.3292 0.2102, -0.08660, 0.1605 0.2472, -0.09640, -0.0507 0.2844, -0.10270, -0.2130 0.3225, -0.10690, -0.4066 0.3608, -0.10890, -0.5806 0.3991, -0.10830, -0.7301 0.4373, -0.10510, -0.8248 0.4757, -0.09890, -0.8256 0.5137, -0.09070, -0.8595 0.5694, -0.07640, -0.7904 15 Flap element taps 1.0000, 0.00130, -0.5176 0.9365, 0.01390, -0.5593 0.8333, 0.03280, -0.5870 0.7436, 0.04930, -0.5692 0.7049, 0.05670, -0.5518 0.6662, 0.06410, -0.5399 0.6522, 0.01390, -1.0662 0.5969, -0.00020, -1.0853 0.6000, -0.03020, -1.1316 0.6324, -0.04540, -1.1478 0.6667, -0.04880, -1.3882 0.7046, -0.04110, -0.8765 0.7429, -0.03210, -0.5935 0.8333, -0.01400, -0.3313 0.9311, -0.00120, -0.2609 --------- Run Conditions: vel=103.4 ft/s Re=0.999x10^6 AOA=26.99 Flap deflection=-20.00 Totals: Cl=0.2324 Cdp=0.2738 Cm(c/4)=0.0223 Cs=-0.1385 Ch=-0.0601 Main component: Cl=0.2031 Cdp=0.3143 Cm=-0.0430 Flap component: Cl=0.0293 Cdp=-0.0405 Cm=-0.0176 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8576 0.6175, -0.04610, -1.1012 0.5841, -0.02440, -1.0810 0.5775, 0.01750, -1.0841 0.5777, 0.04660, -1.0906 0.6274, 0.07170, -0.6110 0.5694, 0.08320, -0.6410 0.5112, 0.09370, -0.6464 0.4731, 0.09830, -0.6333 0.4349, 0.10070, -0.6281 0.3960, 0.10120, -0.5945 0.3566, 0.10020, -0.6226 0.3172, 0.09790, -0.6086 0.2778, 0.09440, -0.6049 0.2393, 0.08960, -0.5970 0.2056, 0.08360, -0.5781 0.1633, 0.07610, -0.6051 0.1261, 0.06710, -0.5934 0.0900, 0.05640, -0.6032 0.0571, 0.04390, -0.5995 0.0283, 0.02940, -0.6142 0.0142, 0.01970, -0.6086 0.0081, 0.01410, -0.6030 0.0026, 0.00780, -0.6162 0.0000, 0.00000, -0.8409 0.0037, -0.00840, 0.4580 0.0112, -0.01420, 0.9048 0.0191, -0.01930, 0.9962 0.0397, -0.03030, 0.9984 0.0706, -0.04420, 0.8866 0.1037, -0.05710, 0.7516 0.1384, -0.06890, 0.5786 0.1741, -0.07950, 0.4269 0.2102, -0.08660, 0.2669 0.2472, -0.09640, 0.0586 0.2844, -0.10270, -0.1045 0.3225, -0.10690, -0.3037 0.3608, -0.10890, -0.4785 0.3991, -0.10830, -0.6418 0.4373, -0.10510, -0.7432 0.4757, -0.09890, -0.7583 0.5137, -0.09070, -0.8059 0.5694, -0.07640, -0.7544 15 Flap element taps 1.0000, 0.00130, -0.5967 0.9365, 0.01390, -0.6315 0.8333, 0.03280, -0.6564 0.7436, 0.04930, -0.6440 0.7049, 0.05670, -0.6282 0.6662, 0.06410, -0.6141 0.6522, 0.01390, -1.0760 0.5969, -0.00020, -1.0979 0.6000, -0.03020, -1.1340 0.6324, -0.04540, -1.1485 0.6667, -0.04880, -1.3863 0.7046, -0.04110, -0.8833 0.7429, -0.03210, -0.6020 0.8333, -0.01400, -0.3460 0.9311, -0.00120, -0.2945