S809 UNVENTED AILERON, CLEAN, CHORD = 18 IN --------- Run Conditions: vel=203.0 ft/s Re=2.002x10^6 AOA=-6.00 Flap deflection=-10.00 Totals: Cl=-0.7869 Cdp=0.0537 Cm(c/4)=0.0550 Cs=0.0289 Ch=0.1060 Main component: Cl=-0.6681 Cdp=0.0275 Cm=0.1555 Flap component: Cl=-0.1187 Cdp=0.0261 Cm=0.0966 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3253 0.6175, -0.04610, -0.3097 0.5841, -0.02440, -0.2565 0.5775, 0.01750, -0.2685 0.5777, 0.04660, -0.2684 0.6274, 0.07170, 0.3227 0.5694, 0.08320, 0.1171 0.5112, 0.09370, -0.1501 0.4731, 0.09830, -0.1920 0.4349, 0.10070, -0.2193 0.3960, 0.10120, -0.1817 0.3566, 0.10020, -0.1396 0.3172, 0.09790, -0.0805 0.2778, 0.09440, -0.0370 0.2393, 0.08960, 0.0177 0.2056, 0.08360, 0.0908 0.1633, 0.07610, 0.1870 0.1261, 0.06710, 0.3132 0.0900, 0.05640, 0.4608 0.0571, 0.04390, 0.6643 0.0283, 0.02940, 0.9025 0.0142, 0.01970, 1.0136 0.0081, 0.01410, 0.9789 0.0026, 0.00780, 0.5550 0.0000, 0.00000, -1.1582 0.0037, -0.00840, -2.2159 0.0112, -0.01420, -1.7937 0.0191, -0.01930, -1.5872 0.0397, -0.03030, -1.0653 0.0706, -0.04420, -1.0194 0.1037, -0.05710, -1.0560 0.1384, -0.06890, -1.0930 0.1741, -0.07950, -1.1176 0.2102, -0.08660, -1.1797 0.2472, -0.09640, -1.2635 0.2844, -0.10270, -1.2719 0.3225, -0.10690, -1.2703 0.3608, -0.10890, -1.2365 0.3991, -0.10830, -1.1276 0.4373, -0.10510, -0.9409 0.4757, -0.09890, -0.6494 0.5137, -0.09070, -0.4022 0.5694, -0.07640, -0.3553 15 Flap element taps 1.0000, 0.00130, -0.2794 0.9365, 0.01390, -0.0703 0.8333, 0.03280, 0.0479 0.7436, 0.04930, 0.1311 0.7049, 0.05670, 0.2086 0.6662, 0.06410, 0.0280 0.6522, 0.01390, -0.2623 0.5969, -0.00020, -0.1873 0.6000, -0.03020, -0.3194 0.6324, -0.04540, -0.3189 0.6667, -0.04880, -0.3120 0.7046, -0.04110, -0.3220 0.7429, -0.03210, -0.3085 0.8333, -0.01400, -0.3438 0.9311, -0.00120, -0.3184 --------- Run Conditions: vel=203.3 ft/s Re=1.999x10^6 AOA=0.01 Flap deflection=-10.00 Totals: Cl=-0.4999 Cdp=0.0190 Cm(c/4)=0.0691 Cs=-0.0191 Ch=0.0744 Main component: Cl=-0.4162 Cdp=0.0181 Cm=0.1275 Flap component: Cl=-0.0837 Cdp=0.0010 Cm=0.0666 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3275 0.6175, -0.04610, -0.2093 0.5841, -0.02440, -0.1576 0.5775, 0.01750, -0.1554 0.5777, 0.04660, -0.1549 0.6274, 0.07170, 0.2929 0.5694, 0.08320, 0.0514 0.5112, 0.09370, -0.2988 0.4731, 0.09830, -0.3383 0.4349, 0.10070, -0.3822 0.3960, 0.10120, -0.3596 0.3566, 0.10020, -0.3430 0.3172, 0.09790, -0.3089 0.2778, 0.09440, -0.2952 0.2393, 0.08960, -0.2723 0.2056, 0.08360, -0.2327 0.1633, 0.07610, -0.1704 0.1261, 0.06710, -0.0793 0.0900, 0.05640, 0.0283 0.0571, 0.04390, 0.2008 0.0283, 0.02940, 0.4556 0.0142, 0.01970, 0.7160 0.0081, 0.01410, 0.8659 0.0026, 0.00780, 1.0025 0.0000, 0.00000, 0.7619 0.0037, -0.00840, -0.0387 0.0112, -0.01420, -0.1965 0.0191, -0.01930, -0.2306 0.0397, -0.03030, -0.2851 0.0706, -0.04420, -0.4013 0.1037, -0.05710, -0.5402 0.1384, -0.06890, -0.6592 0.1741, -0.07950, -0.7704 0.2102, -0.08660, -0.8907 0.2472, -0.09640, -1.0333 0.2844, -0.10270, -1.1129 0.3225, -0.10690, -1.1962 0.3608, -0.10890, -1.2447 0.3991, -0.10830, -1.2430 0.4373, -0.10510, -1.1620 0.4757, -0.09890, -1.0816 0.5137, -0.09070, -0.7409 0.5694, -0.07640, -0.5029 15 Flap element taps 1.0000, 0.00130, -0.0276 0.9365, 0.01390, 0.0535 0.8333, 0.03280, 0.0915 0.7436, 0.04930, 0.1394 0.7049, 0.05670, 0.2077 0.6662, 0.06410, 0.0141 0.6522, 0.01390, -0.1531 0.5969, -0.00020, -0.1744 0.6000, -0.03020, -0.2296 0.6324, -0.04540, -0.2115 0.6667, -0.04880, -0.2303 0.7046, -0.04110, -0.1742 0.7429, -0.03210, -0.1610 0.8333, -0.01400, -0.1551 0.9311, -0.00120, -0.1281 Wake drag found for this condition, Cdw=0.0251 --------- Run Conditions: vel=204.2 ft/s Re=2.002x10^6 AOA=3.04 Flap deflection=-10.00 Totals: Cl=-0.2007 Cdp=0.0151 Cm(c/4)=0.0687 Cs=-0.0257 Ch=0.0620 Main component: Cl=-0.1301 Cdp=0.0212 Cm=0.0625 Flap component: Cl=-0.0706 Cdp=-0.0061 Cm=0.0560 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2989 0.6175, -0.04610, -0.2022 0.5841, -0.02440, -0.1585 0.5775, 0.01750, -0.1572 0.5777, 0.04660, -0.1580 0.6274, 0.07170, 0.2486 0.5694, 0.08320, -0.0167 0.5112, 0.09370, -0.4406 0.4731, 0.09830, -0.4611 0.4349, 0.10070, -0.5144 0.3960, 0.10120, -0.5077 0.3566, 0.10020, -0.5078 0.3172, 0.09790, -0.4897 0.2778, 0.09440, -0.4960 0.2393, 0.08960, -0.4960 0.2056, 0.08360, -0.4814 0.1633, 0.07610, -0.4482 0.1261, 0.06710, -0.3895 0.0900, 0.05640, -0.3263 0.0571, 0.04390, -0.2133 0.0283, 0.02940, -0.0284 0.0142, 0.01970, 0.2135 0.0081, 0.01410, 0.3932 0.0026, 0.00780, 0.6813 0.0000, 0.00000, 1.0085 0.0037, -0.00840, 0.7579 0.0112, -0.01420, 0.5010 0.0191, -0.01930, 0.3735 0.0397, -0.03030, 0.1921 0.0706, -0.04420, 0.0012 0.1037, -0.05710, -0.1758 0.1384, -0.06890, -0.3252 0.1741, -0.07950, -0.4590 0.2102, -0.08660, -0.5982 0.2472, -0.09640, -0.7556 0.2844, -0.10270, -0.8555 0.3225, -0.10690, -0.9582 0.3608, -0.10890, -1.0286 0.3991, -0.10830, -1.0526 0.4373, -0.10510, -1.0007 0.4757, -0.09890, -0.9071 0.5137, -0.09070, -0.6559 0.5694, -0.07640, -0.4452 15 Flap element taps 1.0000, 0.00130, 0.0250 0.9365, 0.01390, 0.0662 0.8333, 0.03280, 0.0775 0.7436, 0.04930, 0.1110 0.7049, 0.05670, 0.1720 0.6662, 0.06410, -0.0045 0.6522, 0.01390, -0.1537 0.5969, -0.00020, -0.1687 0.6000, -0.03020, -0.2231 0.6324, -0.04540, -0.2038 0.6667, -0.04880, -0.2261 0.7046, -0.04110, -0.1579 0.7429, -0.03210, -0.1412 0.8333, -0.01400, -0.1267 0.9311, -0.00120, -0.0785 Wake drag found for this condition, Cdw=0.0206 --------- Run Conditions: vel=204.3 ft/s Re=1.999x10^6 AOA=6.04 Flap deflection=-10.00 Totals: Cl=0.0813 Cdp=0.0108 Cm(c/4)=0.0710 Cs=-0.0022 Ch=0.0461 Main component: Cl=0.1376 Cdp=0.0272 Cm=0.0061 Flap component: Cl=-0.0562 Cdp=-0.0163 Cm=0.0444 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2888 0.6175, -0.04610, -0.2300 0.5841, -0.02440, -0.1893 0.5775, 0.01750, -0.1882 0.5777, 0.04660, -0.1886 0.6274, 0.07170, 0.2000 0.5694, 0.08320, -0.0850 0.5112, 0.09370, -0.3710 0.4731, 0.09830, -0.6024 0.4349, 0.10070, -0.6508 0.3960, 0.10120, -0.6576 0.3566, 0.10020, -0.6736 0.3172, 0.09790, -0.6754 0.2778, 0.09440, -0.7032 0.2393, 0.08960, -0.7300 0.2056, 0.08360, -0.7446 0.1633, 0.07610, -0.7479 0.1261, 0.06710, -0.7320 0.0900, 0.05640, -0.7303 0.0571, 0.04390, -0.7106 0.0283, 0.02940, -0.6558 0.0142, 0.01970, -0.5321 0.0081, 0.01410, -0.4239 0.0026, 0.00780, -0.1442 0.0000, 0.00000, 0.4678 0.0037, -0.00840, 1.0110 0.0112, -0.01420, 0.8960 0.0191, -0.01930, 0.7729 0.0397, -0.03030, 0.5576 0.0706, -0.04420, 0.3349 0.1037, -0.05710, 0.1406 0.1384, -0.06890, -0.0272 0.1741, -0.07950, -0.1752 0.2102, -0.08660, -0.3279 0.2472, -0.09640, -0.4952 0.2844, -0.10270, -0.6118 0.3225, -0.10690, -0.7312 0.3608, -0.10890, -0.8212 0.3991, -0.10830, -0.8695 0.4373, -0.10510, -0.8487 0.4757, -0.09890, -0.7547 0.5137, -0.09070, -0.6833 0.5694, -0.07640, -0.3910 15 Flap element taps 1.0000, 0.00130, 0.1206 0.9365, 0.01390, 0.1004 0.8333, 0.03280, 0.0758 0.7436, 0.04930, 0.0905 0.7049, 0.05670, 0.1426 0.6662, 0.06410, -0.0316 0.6522, 0.01390, -0.1843 0.5969, -0.00020, -0.2012 0.6000, -0.03020, -0.2477 0.6324, -0.04540, -0.2321 0.6667, -0.04880, -0.2639 0.7046, -0.04110, -0.1627 0.7429, -0.03210, -0.1239 0.8333, -0.01400, -0.0761 0.9311, -0.00120, 0.0270 Wake drag found for this condition, Cdw=0.0166 --------- Run Conditions: vel=204.0 ft/s Re=1.991x10^6 AOA=9.02 Flap deflection=-10.00 Totals: Cl=0.3787 Cdp=0.0117 Cm(c/4)=0.0599 Cs=0.0478 Ch=0.0085 Main component: Cl=0.4016 Cdp=0.0402 Cm=-0.0517 Flap component: Cl=-0.0229 Cdp=-0.0286 Cm=0.0176 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2859 0.6175, -0.04610, -0.2926 0.5841, -0.02440, -0.2575 0.5775, 0.01750, -0.2578 0.5777, 0.04660, -0.2603 0.6274, 0.07170, 0.0064 0.5694, 0.08320, -0.1554 0.5112, 0.09370, -0.4555 0.4731, 0.09830, -0.6403 0.4349, 0.10070, -0.7395 0.3960, 0.10120, -0.7651 0.3566, 0.10020, -0.8025 0.3172, 0.09790, -0.8188 0.2778, 0.09440, -0.8659 0.2393, 0.08960, -0.9312 0.2056, 0.08360, -0.9888 0.1633, 0.07610, -1.0444 0.1261, 0.06710, -1.0921 0.0900, 0.05640, -1.1674 0.0571, 0.04390, -1.2712 0.0283, 0.02940, -1.4050 0.0142, 0.01970, -1.4968 0.0081, 0.01410, -1.5432 0.0026, 0.00780, -1.4873 0.0000, 0.00000, -0.9700 0.0037, -0.00840, 0.8460 0.0112, -0.01420, 1.0118 0.0191, -0.01930, 0.9764 0.0397, -0.03030, 0.8139 0.0706, -0.04420, 0.6021 0.1037, -0.05710, 0.4088 0.1384, -0.06890, 0.2356 0.1741, -0.07950, 0.0811 0.2102, -0.08660, -0.0776 0.2472, -0.09640, -0.2501 0.2844, -0.10270, -0.3788 0.3225, -0.10690, -0.5101 0.3608, -0.10890, -0.6157 0.3991, -0.10830, -0.6851 0.4373, -0.10510, -0.6943 0.4757, -0.09890, -0.6164 0.5137, -0.09070, -0.5675 0.5694, -0.07640, -0.3282 15 Flap element taps 1.0000, 0.00130, 0.1841 0.9365, 0.01390, 0.1272 0.8333, 0.03280, 0.0737 0.7436, 0.04930, 0.0596 0.7049, 0.05670, 0.0636 0.6662, 0.06410, 0.0141 0.6522, 0.01390, -0.2536 0.5969, -0.00020, -0.2688 0.6000, -0.03020, -0.3057 0.6324, -0.04540, -0.2929 0.6667, -0.04880, -0.3362 0.7046, -0.04110, -0.1841 0.7429, -0.03210, -0.0643 0.8333, -0.01400, 0.0835 0.9311, -0.00120, 0.1948 Wake drag found for this condition, Cdw=0.0114 --------- Run Conditions: vel=206.2 ft/s Re=2.008x10^6 AOA=12.04 Flap deflection=-10.00 Totals: Cl=0.6943 Cdp=0.0135 Cm(c/4)=0.0437 Cs=0.1317 Ch=-0.0253 Main component: Cl=0.6671 Cdp=0.0450 Cm=-0.1075 Flap component: Cl=0.0273 Cdp=-0.0315 Cm=-0.0192 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2313 0.6175, -0.04610, -0.2906 0.5841, -0.02440, -0.2757 0.5775, 0.01750, -0.2756 0.5777, 0.04660, -0.2778 0.6274, 0.07170, -0.1957 0.5694, 0.08320, -0.2315 0.5112, 0.09370, -0.4148 0.4731, 0.09830, -0.6316 0.4349, 0.10070, -0.7853 0.3960, 0.10120, -0.8581 0.3566, 0.10020, -0.9326 0.3172, 0.09790, -0.9838 0.2778, 0.09440, -1.0671 0.2393, 0.08960, -1.1672 0.2056, 0.08360, -1.2632 0.1633, 0.07610, -1.3589 0.1261, 0.06710, -1.4559 0.0900, 0.05640, -1.6298 0.0571, 0.04390, -1.8817 0.0283, 0.02940, -2.2523 0.0142, 0.01970, -2.6750 0.0081, 0.01410, -3.0880 0.0026, 0.00780, -3.3414 0.0000, 0.00000, -3.3622 0.0037, -0.00840, 0.2174 0.0112, -0.01420, 0.8919 0.0191, -0.01930, 0.9999 0.0397, -0.03030, 0.9651 0.0706, -0.04420, 0.8057 0.1037, -0.05710, 0.6347 0.1384, -0.06890, 0.4689 0.1741, -0.07950, 0.3175 0.2102, -0.08660, 0.1605 0.2472, -0.09640, -0.0097 0.2844, -0.10270, -0.1440 0.3225, -0.10690, -0.2823 0.3608, -0.10890, -0.3977 0.3991, -0.10830, -0.4820 0.4373, -0.10510, -0.5145 0.4757, -0.09890, -0.4608 0.5137, -0.09070, -0.4308 0.5694, -0.07640, -0.2627 15 Flap element taps 1.0000, 0.00130, 0.1584 0.9365, 0.01390, 0.1132 0.8333, 0.03280, 0.0293 0.7436, 0.04930, -0.0765 0.7049, 0.05670, -0.1294 0.6662, 0.06410, -0.1714 0.6522, 0.01390, -0.2730 0.5969, -0.00020, -0.2815 0.6000, -0.03020, -0.2955 0.6324, -0.04540, -0.2898 0.6667, -0.04880, -0.2569 0.7046, -0.04110, -0.1299 0.7429, -0.03210, 0.0067 0.8333, -0.01400, 0.1625 0.9311, -0.00120, 0.2414 Wake drag found for this condition, Cdw=0.0146 --------- Run Conditions: vel=206.5 ft/s Re=2.007x10^6 AOA=15.02 Flap deflection=-10.00 Totals: Cl=0.8734 Cdp=0.0371 Cm(c/4)=0.0155 Cs=0.1906 Ch=-0.0985 Main component: Cl=0.7718 Cdp=0.0524 Cm=-0.1182 Flap component: Cl=0.1016 Cdp=-0.0154 Cm=-0.0796 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2231 0.6175, -0.04610, -0.3390 0.5841, -0.02440, -0.3350 0.5775, 0.01750, -0.3355 0.5777, 0.04660, -0.3382 0.6274, 0.07170, -0.3328 0.5694, 0.08320, -0.3311 0.5112, 0.09370, -0.3378 0.4731, 0.09830, -0.3871 0.4349, 0.10070, -0.5136 0.3960, 0.10120, -0.6567 0.3566, 0.10020, -0.8032 0.3172, 0.09790, -0.9167 0.2778, 0.09440, -1.0499 0.2393, 0.08960, -1.1944 0.2056, 0.08360, -1.3394 0.1633, 0.07610, -1.4906 0.1261, 0.06710, -1.6537 0.0900, 0.05640, -1.9134 0.0571, 0.04390, -2.3024 0.0283, 0.02940, -2.9154 0.0142, 0.01970, -3.5501 0.0081, 0.01410, -4.3508 0.0026, 0.00780, -4.9132 0.0000, 0.00000, -5.6337 0.0037, -0.00840, -0.5272 0.0112, -0.01420, 0.6437 0.0191, -0.01930, 0.9148 0.0397, -0.03030, 1.0087 0.0706, -0.04420, 0.9132 0.1037, -0.05710, 0.7701 0.1384, -0.06890, 0.6162 0.1741, -0.07950, 0.4714 0.2102, -0.08660, 0.3171 0.2472, -0.09640, 0.1487 0.2844, -0.10270, 0.0090 0.3225, -0.10690, -0.1356 0.3608, -0.10890, -0.2609 0.3991, -0.10830, -0.3593 0.4373, -0.10510, -0.4109 0.4757, -0.09890, -0.3776 0.5137, -0.09070, -0.3692 0.5694, -0.07640, -0.2729 15 Flap element taps 1.0000, 0.00130, -0.0646 0.9365, 0.01390, -0.1627 0.8333, 0.03280, -0.2629 0.7436, 0.04930, -0.3141 0.7049, 0.05670, -0.3271 0.6662, 0.06410, -0.3292 0.6522, 0.01390, -0.3322 0.5969, -0.00020, -0.3364 0.6000, -0.03020, -0.3387 0.6324, -0.04540, -0.3369 0.6667, -0.04880, -0.1823 0.7046, -0.04110, -0.1241 0.7429, -0.03210, 0.0067 0.8333, -0.01400, 0.1392 0.9311, -0.00120, 0.1728 --------- Run Conditions: vel=206.2 ft/s Re=2.002x10^6 AOA=17.99 Flap deflection=-10.00 Totals: Cl=0.7630 Cdp=0.0981 Cm(c/4)=-0.0130 Cs=0.1423 Ch=-0.1424 Main component: Cl=0.6217 Cdp=0.0959 Cm=-0.0887 Flap component: Cl=0.1412 Cdp=0.0022 Cm=-0.1133 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3208 0.6175, -0.04610, -0.4724 0.5841, -0.02440, -0.4671 0.5775, 0.01750, -0.4676 0.5777, 0.04660, -0.4702 0.6274, 0.07170, -0.5112 0.5694, 0.08320, -0.4973 0.5112, 0.09370, -0.4911 0.4731, 0.09830, -0.4829 0.4349, 0.10070, -0.4722 0.3960, 0.10120, -0.4610 0.3566, 0.10020, -0.4657 0.3172, 0.09790, -0.4666 0.2778, 0.09440, -0.4976 0.2393, 0.08960, -0.5919 0.2056, 0.08360, -0.7883 0.1633, 0.07610, -1.0381 0.1261, 0.06710, -1.2931 0.0900, 0.05640, -1.6224 0.0571, 0.04390, -2.0803 0.0283, 0.02940, -2.7758 0.0142, 0.01970, -3.4952 0.0081, 0.01410, -4.2986 0.0026, 0.00780, -5.0488 0.0000, 0.00000, -5.9960 0.0037, -0.00840, -0.7073 0.0112, -0.01420, 0.5661 0.0191, -0.01930, 0.8784 0.0397, -0.03030, 1.0110 0.0706, -0.04420, 0.9376 0.1037, -0.05710, 0.8041 0.1384, -0.06890, 0.6527 0.1741, -0.07950, 0.5079 0.2102, -0.08660, 0.3518 0.2472, -0.09640, 0.1782 0.2844, -0.10270, 0.0313 0.3225, -0.10690, -0.1239 0.3608, -0.10890, -0.2614 0.3991, -0.10830, -0.3745 0.4373, -0.10510, -0.4411 0.4757, -0.09890, -0.4206 0.5137, -0.09070, -0.4267 0.5694, -0.07640, -0.3379 15 Flap element taps 1.0000, 0.00130, -0.4172 0.9365, 0.01390, -0.4907 0.8333, 0.03280, -0.5255 0.7436, 0.04930, -0.5309 0.7049, 0.05670, -0.5251 0.6662, 0.06410, -0.5146 0.6522, 0.01390, -0.4653 0.5969, -0.00020, -0.4711 0.6000, -0.03020, -0.4712 0.6324, -0.04540, -0.4701 0.6667, -0.04880, -0.2496 0.7046, -0.04110, -0.2290 0.7429, -0.03210, -0.0978 0.8333, -0.01400, 0.0152 0.9311, -0.00120, -0.0004 --------- Run Conditions: vel=205.9 ft/s Re=1.994x10^6 AOA=20.00 Flap deflection=-10.00 Totals: Cl=0.7254 Cdp=0.1379 Cm(c/4)=-0.0209 Cs=0.1185 Ch=-0.1439 Main component: Cl=0.5832 Cdp=0.1305 Cm=-0.0888 Flap component: Cl=0.1422 Cdp=0.0074 Cm=-0.1143 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3733 0.6175, -0.04610, -0.5278 0.5841, -0.02440, -0.5290 0.5775, 0.01750, -0.5293 0.5777, 0.04660, -0.5317 0.6274, 0.07170, -0.5682 0.5694, 0.08320, -0.5683 0.5112, 0.09370, -0.5588 0.4731, 0.09830, -0.5527 0.4349, 0.10070, -0.5410 0.3960, 0.10120, -0.5274 0.3566, 0.10020, -0.5363 0.3172, 0.09790, -0.5270 0.2778, 0.09440, -0.5242 0.2393, 0.08960, -0.5402 0.2056, 0.08360, -0.6069 0.1633, 0.07610, -0.7743 0.1261, 0.06710, -1.0416 0.0900, 0.05640, -1.4144 0.0571, 0.04390, -1.9128 0.0283, 0.02940, -2.6494 0.0142, 0.01970, -3.4046 0.0081, 0.01410, -4.1943 0.0026, 0.00780, -5.0491 0.0000, 0.00000, -6.0976 0.0037, -0.00840, -0.7797 0.0112, -0.01420, 0.5321 0.0191, -0.01930, 0.8617 0.0397, -0.03030, 1.0112 0.0706, -0.04420, 0.9475 0.1037, -0.05710, 0.8181 0.1384, -0.06890, 0.6673 0.1741, -0.07950, 0.5225 0.2102, -0.08660, 0.3647 0.2472, -0.09640, 0.1875 0.2844, -0.10270, 0.0361 0.3225, -0.10690, -0.1264 0.3608, -0.10890, -0.2700 0.3991, -0.10830, -0.3906 0.4373, -0.10510, -0.4648 0.4757, -0.09890, -0.4489 0.5137, -0.09070, -0.4621 0.5694, -0.07640, -0.3743 15 Flap element taps 1.0000, 0.00130, -0.4996 0.9365, 0.01390, -0.5598 0.8333, 0.03280, -0.5793 0.7436, 0.04930, -0.5820 0.7049, 0.05670, -0.5730 0.6662, 0.06410, -0.5601 0.6522, 0.01390, -0.5245 0.5969, -0.00020, -0.5299 0.6000, -0.03020, -0.5296 0.6324, -0.04540, -0.5291 0.6667, -0.04880, -0.2934 0.7046, -0.04110, -0.2807 0.7429, -0.03210, -0.1467 0.8333, -0.01400, -0.0365 0.9311, -0.00120, -0.0593 --------- Run Conditions: vel=201.8 ft/s Re=1.953x10^6 AOA=23.99 Flap deflection=-10.00 Totals: Cl=0.4387 Cdp=0.2871 Cm(c/4)=-0.0460 Cs=-0.0839 Ch=-0.1335 Main component: Cl=0.3093 Cdp=0.2749 Cm=-0.0713 Flap component: Cl=0.1293 Cdp=0.0122 Cm=-0.1041 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5217 0.6175, -0.04610, -0.6803 0.5841, -0.02440, -0.6761 0.5775, 0.01750, -0.6763 0.5777, 0.04660, -0.6794 0.6274, 0.07170, -0.6586 0.5694, 0.08320, -0.6651 0.5112, 0.09370, -0.6696 0.4731, 0.09830, -0.6627 0.4349, 0.10070, -0.6570 0.3960, 0.10120, -0.6461 0.3566, 0.10020, -0.6558 0.3172, 0.09790, -0.6479 0.2778, 0.09440, -0.6459 0.2393, 0.08960, -0.6433 0.2056, 0.08360, -0.6394 0.1633, 0.07610, -0.6466 0.1261, 0.06710, -0.6426 0.0900, 0.05640, -0.6413 0.0571, 0.04390, -0.6399 0.0283, 0.02940, -0.6489 0.0142, 0.01970, -0.6595 0.0081, 0.01410, -0.6723 0.0026, 0.00780, -0.6918 0.0000, 0.00000, -0.9084 0.0037, -0.00840, 0.4860 0.0112, -0.01420, 0.9096 0.0191, -0.01930, 0.9946 0.0397, -0.03030, 0.9871 0.0706, -0.04420, 0.8747 0.1037, -0.05710, 0.7331 0.1384, -0.06890, 0.5779 0.1741, -0.07950, 0.4320 0.2102, -0.08660, 0.2727 0.2472, -0.09640, 0.0888 0.2844, -0.10270, -0.0674 0.3225, -0.10690, -0.2387 0.3608, -0.10890, -0.3900 0.3991, -0.10830, -0.5210 0.4373, -0.10510, -0.6014 0.4757, -0.09890, -0.5856 0.5137, -0.09070, -0.6023 0.5694, -0.07640, -0.5128 15 Flap element taps 1.0000, 0.00130, -0.6290 0.9365, 0.01390, -0.6684 0.8333, 0.03280, -0.6805 0.7436, 0.04930, -0.6739 0.7049, 0.05670, -0.6650 0.6662, 0.06410, -0.6511 0.6522, 0.01390, -0.6724 0.5969, -0.00020, -0.6787 0.6000, -0.03020, -0.6819 0.6324, -0.04540, -0.6803 0.6667, -0.04880, -0.4704 0.7046, -0.04110, -0.4340 0.7429, -0.03210, -0.2863 0.8333, -0.01400, -0.1675 0.9311, -0.00120, -0.1908 --------- Run Conditions: vel=206.2 ft/s Re=1.991x10^6 AOA=27.00 Flap deflection=-10.00 Totals: Cl=0.5635 Cdp=0.3762 Cm(c/4)=-0.0739 Cs=-0.0794 Ch=-0.1617 Main component: Cl=0.3990 Cdp=0.3465 Cm=-0.1090 Flap component: Cl=0.1645 Cdp=0.0297 Cm=-0.1331 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5098 0.6175, -0.04610, -0.7268 0.5841, -0.02440, -0.7252 0.5775, 0.01750, -0.7249 0.5777, 0.04660, -0.7272 0.6274, 0.07170, -0.7719 0.5694, 0.08320, -0.7831 0.5112, 0.09370, -0.7878 0.4731, 0.09830, -0.7824 0.4349, 0.10070, -0.7771 0.3960, 0.10120, -0.7642 0.3566, 0.10020, -0.7752 0.3172, 0.09790, -0.7664 0.2778, 0.09440, -0.7630 0.2393, 0.08960, -0.7590 0.2056, 0.08360, -0.7509 0.1633, 0.07610, -0.7579 0.1261, 0.06710, -0.7529 0.0900, 0.05640, -0.7560 0.0571, 0.04390, -0.7567 0.0283, 0.02940, -0.7604 0.0142, 0.01970, -0.7653 0.0081, 0.01410, -0.7730 0.0026, 0.00780, -0.8067 0.0000, 0.00000, -0.8176 0.0037, -0.00840, 0.2944 0.0112, -0.01420, 0.8228 0.0191, -0.01930, 0.9602 0.0397, -0.03030, 1.0076 0.0706, -0.04420, 0.9335 0.1037, -0.05710, 0.8150 0.1384, -0.06890, 0.6726 0.1741, -0.07950, 0.5352 0.2102, -0.08660, 0.3840 0.2472, -0.09640, 0.2059 0.2844, -0.10270, 0.0505 0.3225, -0.10690, -0.1225 0.3608, -0.10890, -0.2773 0.3991, -0.10830, -0.4159 0.4373, -0.10510, -0.5082 0.4757, -0.09890, -0.5090 0.5137, -0.09070, -0.5403 0.5694, -0.07640, -0.4698 15 Flap element taps 1.0000, 0.00130, -0.7374 0.9365, 0.01390, -0.7745 0.8333, 0.03280, -0.7862 0.7436, 0.04930, -0.7838 0.7049, 0.05670, -0.7781 0.6662, 0.06410, -0.7661 0.6522, 0.01390, -0.7210 0.5969, -0.00020, -0.7272 0.6000, -0.03020, -0.7259 0.6324, -0.04540, -0.7274 0.6667, -0.04880, -0.3142 0.7046, -0.04110, -0.4090 0.7429, -0.03210, -0.2753 0.8333, -0.01400, -0.1768 0.9311, -0.00120, -0.2227