S809 UNVENTED AILERON, CLEAN, CHORD = 18 IN --------- Run Conditions: vel=212.2 ft/s Re=2.011x10^6 AOA=-6.02 Flap deflection=-5.00 Totals: Cl=-0.6699 Cdp=0.0387 Cm(c/4)=0.0376 Cs=0.0318 Ch=0.0856 Main component: Cl=-0.5790 Cdp=0.0318 Cm=0.1321 Flap component: Cl=-0.0909 Cdp=0.0069 Cm=0.0730 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2972 0.6175, -0.04610, -0.2665 0.5841, -0.02440, -0.2157 0.5775, 0.01750, -0.2130 0.5777, 0.04660, -0.2128 0.6274, 0.07170, 0.1841 0.5694, 0.08320, 0.0048 0.5112, 0.09370, -0.2648 0.4731, 0.09830, -0.3344 0.4349, 0.10070, -0.3393 0.3960, 0.10120, -0.2763 0.3566, 0.10020, -0.2271 0.3172, 0.09790, -0.1642 0.2778, 0.09440, -0.1184 0.2393, 0.08960, -0.0631 0.2056, 0.08360, 0.0134 0.1633, 0.07610, 0.1102 0.1261, 0.06710, 0.2393 0.0900, 0.05640, 0.3901 0.0571, 0.04390, 0.5979 0.0283, 0.02940, 0.8528 0.0142, 0.01970, 1.0014 0.0081, 0.01410, 1.0018 0.0026, 0.00780, 0.6462 0.0000, 0.00000, -0.7376 0.0037, -0.00840, -1.8083 0.0112, -0.01420, -1.4844 0.0191, -0.01930, -1.2820 0.0397, -0.03030, -0.9476 0.0706, -0.04420, -0.8993 0.1037, -0.05710, -0.9517 0.1384, -0.06890, -1.0020 0.1741, -0.07950, -1.0365 0.2102, -0.08660, -1.1048 0.2472, -0.09640, -1.1939 0.2844, -0.10270, -1.2098 0.3225, -0.10690, -1.2176 0.3608, -0.10890, -1.1958 0.3991, -0.10830, -1.1056 0.4373, -0.10510, -0.9511 0.4757, -0.09890, -0.6852 0.5137, -0.09070, -0.4710 0.5694, -0.07640, -0.3176 15 Flap element taps 1.0000, 0.00130, -0.1469 0.9365, 0.01390, -0.0208 0.8333, 0.03280, 0.0223 0.7436, 0.04930, 0.0530 0.7049, 0.05670, 0.1027 0.6662, 0.06410, -0.0964 0.6522, 0.01390, -0.2108 0.5969, -0.00020, -0.2267 0.6000, -0.03020, -0.2880 0.6324, -0.04540, -0.2762 0.6667, -0.04880, -0.2664 0.7046, -0.04110, -0.2682 0.7429, -0.03210, -0.2722 0.8333, -0.01400, -0.2731 0.9311, -0.00120, -0.2490 --------- Run Conditions: vel=211.4 ft/s Re=1.998x10^6 AOA=0.01 Flap deflection=-5.00 Totals: Cl=-0.2703 Cdp=0.0056 Cm(c/4)=0.0267 Cs=-0.0057 Ch=0.0076 Main component: Cl=-0.2499 Cdp=0.0300 Cm=0.0811 Flap component: Cl=-0.0204 Cdp=-0.0244 Cm=0.0131 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3054 0.6175, -0.04610, -0.2209 0.5841, -0.02440, -0.1833 0.5775, 0.01750, -0.1811 0.5777, 0.04660, -0.1821 0.6274, 0.07170, 0.1334 0.5694, 0.08320, -0.0836 0.5112, 0.09370, -0.4358 0.4731, 0.09830, -0.4862 0.4349, 0.10070, -0.5304 0.3960, 0.10120, -0.4974 0.3566, 0.10020, -0.4759 0.3172, 0.09790, -0.4402 0.2778, 0.09440, -0.4275 0.2393, 0.08960, -0.4079 0.2056, 0.08360, -0.3696 0.1633, 0.07610, -0.3128 0.1261, 0.06710, -0.2251 0.0900, 0.05640, -0.1239 0.0571, 0.04390, 0.0359 0.0283, 0.02940, 0.2778 0.0142, 0.01970, 0.5463 0.0081, 0.01410, 0.7215 0.0026, 0.00780, 0.9220 0.0000, 0.00000, 0.9501 0.0037, -0.00840, 0.3310 0.0112, -0.01420, 0.1079 0.0191, -0.01930, 0.0276 0.0397, -0.03030, -0.0861 0.0706, -0.04420, -0.2338 0.1037, -0.05710, -0.3821 0.1384, -0.06890, -0.5108 0.1741, -0.07950, -0.6291 0.2102, -0.08660, -0.7518 0.2472, -0.09640, -0.8940 0.2844, -0.10270, -0.9763 0.3225, -0.10690, -1.0624 0.3608, -0.10890, -1.1135 0.3991, -0.10830, -1.1198 0.4373, -0.10510, -1.0512 0.4757, -0.09890, -0.9695 0.5137, -0.09070, -0.6590 0.5694, -0.07640, -0.4482 15 Flap element taps 1.0000, 0.00130, 0.1826 0.9365, 0.01390, 0.1248 0.8333, 0.03280, 0.0743 0.7436, 0.04930, 0.0564 0.7049, 0.05670, 0.0877 0.6662, 0.06410, -0.1276 0.6522, 0.01390, -0.1791 0.5969, -0.00020, -0.1894 0.6000, -0.03020, -0.2409 0.6324, -0.04540, -0.2266 0.6667, -0.04880, -0.2560 0.7046, -0.04110, -0.1650 0.7429, -0.03210, -0.0599 0.8333, -0.01400, 0.0807 0.9311, -0.00120, 0.1800 Wake drag found for this condition, Cdw=0.0106 --------- Run Conditions: vel=213.3 ft/s Re=2.013x10^6 AOA=3.04 Flap deflection=-5.00 Totals: Cl=0.0704 Cdp=0.0021 Cm(c/4)=0.0188 Cs=0.0017 Ch=-0.0142 Main component: Cl=0.0644 Cdp=0.0276 Cm=0.0080 Flap component: Cl=0.0060 Cdp=-0.0255 Cm=-0.0068 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2469 0.6175, -0.04610, -0.1884 0.5841, -0.02440, -0.1590 0.5775, 0.01750, -0.1600 0.5777, 0.04660, -0.1604 0.6274, 0.07170, 0.0726 0.5694, 0.08320, -0.1766 0.5112, 0.09370, -0.5970 0.4731, 0.09830, -0.6323 0.4349, 0.10070, -0.6895 0.3960, 0.10120, -0.6733 0.3566, 0.10020, -0.6672 0.3172, 0.09790, -0.6491 0.2778, 0.09440, -0.6580 0.2393, 0.08960, -0.6628 0.2056, 0.08360, -0.6524 0.1633, 0.07610, -0.6289 0.1261, 0.06710, -0.5792 0.0900, 0.05640, -0.5309 0.0571, 0.04390, -0.4472 0.0283, 0.02940, -0.3043 0.0142, 0.01970, -0.0967 0.0081, 0.01410, 0.0700 0.0026, 0.00780, 0.3434 0.0000, 0.00000, 0.8838 0.0037, -0.00840, 0.9330 0.0112, -0.01420, 0.7117 0.0191, -0.01930, 0.5766 0.0397, -0.03030, 0.3700 0.0706, -0.04420, 0.1630 0.1037, -0.05710, -0.0174 0.1384, -0.06890, -0.1717 0.1741, -0.07950, -0.3094 0.2102, -0.08660, -0.4481 0.2472, -0.09640, -0.6019 0.2844, -0.10270, -0.7022 0.3225, -0.10690, -0.8049 0.3608, -0.10890, -0.8752 0.3991, -0.10830, -0.9043 0.4373, -0.10510, -0.8637 0.4757, -0.09890, -0.7745 0.5137, -0.09070, -0.5848 0.5694, -0.07640, -0.3591 15 Flap element taps 1.0000, 0.00130, 0.1912 0.9365, 0.01390, 0.1154 0.8333, 0.03280, 0.0444 0.7436, 0.04930, 0.0124 0.7049, 0.05670, 0.0365 0.6662, 0.06410, -0.1700 0.6522, 0.01390, -0.1569 0.5969, -0.00020, -0.1643 0.6000, -0.03020, -0.2015 0.6324, -0.04540, -0.1916 0.6667, -0.04880, -0.2110 0.7046, -0.04110, -0.1171 0.7429, -0.03210, -0.0102 0.8333, -0.01400, 0.1326 0.9311, -0.00120, 0.2218 Wake drag found for this condition, Cdw=0.0087 --------- Run Conditions: vel=213.1 ft/s Re=2.009x10^6 AOA=6.02 Flap deflection=-5.00 Totals: Cl=0.4035 Cdp=0.0006 Cm(c/4)=0.0119 Cs=0.0418 Ch=-0.0357 Main component: Cl=0.3694 Cdp=0.0250 Cm=-0.0607 Flap component: Cl=0.0341 Cdp=-0.0244 Cm=-0.0277 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1835 0.6175, -0.04610, -0.1560 0.5841, -0.02440, -0.1383 0.5775, 0.01750, -0.1403 0.5777, 0.04660, -0.1407 0.6274, 0.07170, -0.0080 0.5694, 0.08320, -0.2812 0.5112, 0.09370, -0.5849 0.4731, 0.09830, -0.7833 0.4349, 0.10070, -0.8504 0.3960, 0.10120, -0.8480 0.3566, 0.10020, -0.8597 0.3172, 0.09790, -0.8628 0.2778, 0.09440, -0.8953 0.2393, 0.08960, -0.9282 0.2056, 0.08360, -0.9509 0.1633, 0.07610, -0.9682 0.1261, 0.06710, -0.9673 0.0900, 0.05640, -0.9899 0.0571, 0.04390, -1.0192 0.0283, 0.02940, -1.0410 0.0142, 0.01970, -1.0045 0.0081, 0.01410, -0.9648 0.0026, 0.00780, -0.6923 0.0000, 0.00000, -0.1436 0.0037, -0.00840, 0.9809 0.0112, -0.01420, 0.9864 0.0191, -0.01930, 0.8999 0.0397, -0.03030, 0.7016 0.0706, -0.04420, 0.4834 0.1037, -0.05710, 0.2943 0.1384, -0.06890, 0.1274 0.1741, -0.07950, -0.0197 0.2102, -0.08660, -0.1664 0.2472, -0.09640, -0.3272 0.2844, -0.10270, -0.4393 0.3225, -0.10690, -0.5544 0.3608, -0.10890, -0.6398 0.3991, -0.10830, -0.6886 0.4373, -0.10510, -0.6758 0.4757, -0.09890, -0.5914 0.5137, -0.09070, -0.5297 0.5694, -0.07640, -0.2619 15 Flap element taps 1.0000, 0.00130, 0.1919 0.9365, 0.01390, 0.1072 0.8333, 0.03280, 0.0174 0.7436, 0.04930, -0.0319 0.7049, 0.05670, -0.0217 0.6662, 0.06410, -0.2191 0.6522, 0.01390, -0.1364 0.5969, -0.00020, -0.1417 0.6000, -0.03020, -0.1640 0.6324, -0.04540, -0.1569 0.6667, -0.04880, -0.1550 0.7046, -0.04110, -0.0517 0.7429, -0.03210, 0.0520 0.8333, -0.01400, 0.1856 0.9311, -0.00120, 0.2584 Wake drag found for this condition, Cdw=0.0086 --------- Run Conditions: vel=213.3 ft/s Re=2.005x10^6 AOA=9.01 Flap deflection=-5.00 Totals: Cl=0.7001 Cdp=0.0075 Cm(c/4)=0.0060 Cs=0.1022 Ch=-0.0519 Main component: Cl=0.6386 Cdp=0.0294 Cm=-0.1197 Flap component: Cl=0.0615 Cdp=-0.0219 Cm=-0.0475 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1376 0.6175, -0.04610, -0.1690 0.5841, -0.02440, -0.1637 0.5775, 0.01750, -0.1676 0.5777, 0.04660, -0.1686 0.6274, 0.07170, -0.1838 0.5694, 0.08320, -0.3484 0.5112, 0.09370, -0.6369 0.4731, 0.09830, -0.8292 0.4349, 0.10070, -0.9354 0.3960, 0.10120, -0.9572 0.3566, 0.10020, -0.9937 0.3172, 0.09790, -1.0164 0.2778, 0.09440, -1.0728 0.2393, 0.08960, -1.1472 0.2056, 0.08360, -1.2115 0.1633, 0.07610, -1.2746 0.1261, 0.06710, -1.3239 0.0900, 0.05640, -1.4321 0.0571, 0.04390, -1.6074 0.0283, 0.02940, -1.8836 0.0142, 0.01970, -2.1040 0.0081, 0.01410, -2.2657 0.0026, 0.00780, -2.2638 0.0000, 0.00000, -2.0491 0.0037, -0.00840, 0.5896 0.0112, -0.01420, 0.9840 0.0191, -0.01930, 1.0093 0.0397, -0.03030, 0.9044 0.0706, -0.04420, 0.7174 0.1037, -0.05710, 0.5384 0.1384, -0.06890, 0.3714 0.1741, -0.07950, 0.2223 0.2102, -0.08660, 0.0735 0.2472, -0.09640, -0.0890 0.2844, -0.10270, -0.2104 0.3225, -0.10690, -0.3354 0.3608, -0.10890, -0.4330 0.3991, -0.10830, -0.4992 0.4373, -0.10510, -0.5109 0.4757, -0.09890, -0.4422 0.5137, -0.09070, -0.3914 0.5694, -0.07640, -0.1747 15 Flap element taps 1.0000, 0.00130, 0.1547 0.9365, 0.01390, 0.0954 0.8333, 0.03280, -0.0040 0.7436, 0.04930, -0.0811 0.7049, 0.05670, -0.1117 0.6662, 0.06410, -0.1759 0.6522, 0.01390, -0.1645 0.5969, -0.00020, -0.1668 0.6000, -0.03020, -0.1684 0.6324, -0.04540, -0.1673 0.6667, -0.04880, -0.0190 0.7046, -0.04110, 0.0233 0.7429, -0.03210, 0.1114 0.8333, -0.01400, 0.2238 0.9311, -0.00120, 0.2745 Wake drag found for this condition, Cdw=0.0116 --------- Run Conditions: vel=212.8 ft/s Re=1.999x10^6 AOA=12.01 Flap deflection=-5.00 Totals: Cl=0.9254 Cdp=0.0263 Cm(c/4)=-0.0088 Cs=0.1669 Ch=-0.0945 Main component: Cl=0.8124 Cdp=0.0358 Cm=-0.1486 Flap component: Cl=0.1130 Cdp=-0.0096 Cm=-0.0878 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1177 0.6175, -0.04610, -0.2083 0.5841, -0.02440, -0.2069 0.5775, 0.01750, -0.2065 0.5777, 0.04660, -0.2067 0.6274, 0.07170, -0.2879 0.5694, 0.08320, -0.3348 0.5112, 0.09370, -0.5148 0.4731, 0.09830, -0.7257 0.4349, 0.10070, -0.8834 0.3960, 0.10120, -0.9546 0.3566, 0.10020, -1.0301 0.3172, 0.09790, -1.0883 0.2778, 0.09440, -1.1793 0.2393, 0.08960, -1.2871 0.2056, 0.08360, -1.3917 0.1633, 0.07610, -1.5055 0.1261, 0.06710, -1.6185 0.0900, 0.05640, -1.8166 0.0571, 0.04390, -2.1170 0.0283, 0.02940, -2.5811 0.0142, 0.01970, -3.0513 0.0081, 0.01410, -3.6892 0.0026, 0.00780, -3.8026 0.0000, 0.00000, -4.2724 0.0037, -0.00840, -0.0672 0.0112, -0.01420, 0.8062 0.0191, -0.01930, 0.9793 0.0397, -0.03030, 0.9929 0.0706, -0.04420, 0.8606 0.1037, -0.05710, 0.7039 0.1384, -0.06890, 0.5446 0.1741, -0.07950, 0.3991 0.2102, -0.08660, 0.2516 0.2472, -0.09640, 0.0889 0.2844, -0.10270, -0.0380 0.3225, -0.10690, -0.1707 0.3608, -0.10890, -0.2788 0.3991, -0.10830, -0.3593 0.4373, -0.10510, -0.3906 0.4757, -0.09890, -0.3412 0.5137, -0.09070, -0.3100 0.5694, -0.07640, -0.1439 15 Flap element taps 1.0000, 0.00130, 0.0156 0.9365, 0.01390, -0.0594 0.8333, 0.03280, -0.1551 0.7436, 0.04930, -0.2223 0.7049, 0.05670, -0.2491 0.6662, 0.06410, -0.2722 0.6522, 0.01390, -0.2029 0.5969, -0.00020, -0.2071 0.6000, -0.03020, -0.2065 0.6324, -0.04540, -0.2084 0.6667, -0.04880, 0.2012 0.7046, -0.04110, 0.0529 0.7429, -0.03210, 0.1290 0.8333, -0.01400, 0.2187 0.9311, -0.00120, 0.2392 --------- Run Conditions: vel=212.4 ft/s Re=1.994x10^6 AOA=15.00 Flap deflection=-5.00 Totals: Cl=0.9567 Cdp=0.0510 Cm(c/4)=-0.0123 Cs=0.1984 Ch=-0.1388 Main component: Cl=0.8098 Cdp=0.0378 Cm=-0.1281 Flap component: Cl=0.1469 Cdp=0.0132 Cm=-0.1185 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1336 0.6175, -0.04610, -0.2432 0.5841, -0.02440, -0.2413 0.5775, 0.01750, -0.2454 0.5777, 0.04660, -0.2467 0.6274, 0.07170, -0.3542 0.5694, 0.08320, -0.3520 0.5112, 0.09370, -0.3499 0.4731, 0.09830, -0.3804 0.4349, 0.10070, -0.4700 0.3960, 0.10120, -0.5915 0.3566, 0.10020, -0.7429 0.3172, 0.09790, -0.8747 0.2778, 0.09440, -1.0255 0.2393, 0.08960, -1.1846 0.2056, 0.08360, -1.3412 0.1633, 0.07610, -1.5103 0.1261, 0.06710, -1.6876 0.0900, 0.05640, -1.9619 0.0571, 0.04390, -2.3779 0.0283, 0.02940, -3.0378 0.0142, 0.01970, -3.7313 0.0081, 0.01410, -4.5582 0.0026, 0.00780, -5.0251 0.0000, 0.00000, -6.0914 0.0037, -0.00840, -0.6897 0.0112, -0.01420, 0.5829 0.0191, -0.01930, 0.8898 0.0397, -0.03030, 1.0112 0.0706, -0.04420, 0.9326 0.1037, -0.05710, 0.7979 0.1384, -0.06890, 0.6483 0.1741, -0.07950, 0.5067 0.2102, -0.08660, 0.3599 0.2472, -0.09640, 0.1963 0.2844, -0.10270, 0.0626 0.3225, -0.10690, -0.0782 0.3608, -0.10890, -0.1970 0.3991, -0.10830, -0.2919 0.4373, -0.10510, -0.3396 0.4757, -0.09890, -0.3070 0.5137, -0.09070, -0.2909 0.5694, -0.07640, -0.1877 15 Flap element taps 1.0000, 0.00130, -0.2516 0.9365, 0.01390, -0.3471 0.8333, 0.03280, -0.3612 0.7436, 0.04930, -0.3561 0.7049, 0.05670, -0.3554 0.6662, 0.06410, -0.3539 0.6522, 0.01390, -0.2403 0.5969, -0.00020, -0.2441 0.6000, -0.03020, -0.2442 0.6324, -0.04540, -0.2457 0.6667, -0.04880, 0.1873 0.7046, -0.04110, 0.0099 0.7429, -0.03210, 0.0790 0.8333, -0.01400, 0.1451 0.9311, -0.00120, 0.1182 --------- Run Conditions: vel=215.9 ft/s Re=2.026x10^6 AOA=17.99 Flap deflection=-5.00 Totals: Cl=0.8846 Cdp=0.1202 Cm(c/4)=-0.0399 Cs=0.1589 Ch=-0.1708 Main component: Cl=0.7033 Cdp=0.0880 Cm=-0.1117 Flap component: Cl=0.1812 Cdp=0.0323 Cm=-0.1477 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2011 0.6175, -0.04610, -0.3376 0.5841, -0.02440, -0.3364 0.5775, 0.01750, -0.3406 0.5777, 0.04660, -0.3402 0.6274, 0.07170, -0.5436 0.5694, 0.08320, -0.5343 0.5112, 0.09370, -0.5225 0.4731, 0.09830, -0.5188 0.4349, 0.10070, -0.5181 0.3960, 0.10120, -0.5110 0.3566, 0.10020, -0.5256 0.3172, 0.09790, -0.5396 0.2778, 0.09440, -0.5938 0.2393, 0.08960, -0.7103 0.2056, 0.08360, -0.8993 0.1633, 0.07610, -1.1381 0.1261, 0.06710, -1.3871 0.0900, 0.05640, -1.7164 0.0571, 0.04390, -2.1878 0.0283, 0.02940, -2.9163 0.0142, 0.01970, -3.6808 0.0081, 0.01410, -4.5035 0.0026, 0.00780, -5.1309 0.0000, 0.00000, -6.4214 0.0037, -0.00840, -0.8474 0.0112, -0.01420, 0.5132 0.0191, -0.01930, 0.8563 0.0397, -0.03030, 1.0117 0.0706, -0.04420, 0.9504 0.1037, -0.05710, 0.8242 0.1384, -0.06890, 0.6771 0.1741, -0.07950, 0.5356 0.2102, -0.08660, 0.3868 0.2472, -0.09640, 0.2187 0.2844, -0.10270, 0.0784 0.3225, -0.10690, -0.0717 0.3608, -0.10890, -0.2009 0.3991, -0.10830, -0.3075 0.4373, -0.10510, -0.3672 0.4757, -0.09890, -0.3438 0.5137, -0.09070, -0.3369 0.5694, -0.07640, -0.2396 15 Flap element taps 1.0000, 0.00130, -0.4748 0.9365, 0.01390, -0.5427 0.8333, 0.03280, -0.5529 0.7436, 0.04930, -0.5541 0.7049, 0.05670, -0.5494 0.6662, 0.06410, -0.5427 0.6522, 0.01390, -0.3355 0.5969, -0.00020, -0.3407 0.6000, -0.03020, -0.3396 0.6324, -0.04540, -0.3450 0.6667, -0.04880, 0.2110 0.7046, -0.04110, -0.0578 0.7429, -0.03210, 0.0086 0.8333, -0.01400, 0.0624 0.9311, -0.00120, 0.0071 --------- Run Conditions: vel=212.7 ft/s Re=1.994x10^6 AOA=20.00 Flap deflection=-5.00 Totals: Cl=0.5715 Cdp=0.2820 Cm(c/4)=-0.0935 Cs=-0.0695 Ch=-0.1860 Main component: Cl=0.3762 Cdp=0.2382 Cm=-0.0911 Flap component: Cl=0.1953 Cdp=0.0439 Cm=-0.1607 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3105 0.6175, -0.04610, -0.4646 0.5841, -0.02440, -0.4609 0.5775, 0.01750, -0.4610 0.5777, 0.04660, -0.4609 0.6274, 0.07170, -0.7110 0.5694, 0.08320, -0.7103 0.5112, 0.09370, -0.7100 0.4731, 0.09830, -0.7061 0.4349, 0.10070, -0.6969 0.3960, 0.10120, -0.6755 0.3566, 0.10020, -0.6740 0.3172, 0.09790, -0.6624 0.2778, 0.09440, -0.6572 0.2393, 0.08960, -0.6502 0.2056, 0.08360, -0.6402 0.1633, 0.07610, -0.6408 0.1261, 0.06710, -0.6312 0.0900, 0.05640, -0.6275 0.0571, 0.04390, -0.6241 0.0283, 0.02940, -0.6277 0.0142, 0.01970, -0.6344 0.0081, 0.01410, -0.6441 0.0026, 0.00780, -0.6346 0.0000, 0.00000, -1.0087 0.0037, -0.00840, 0.4523 0.0112, -0.01420, 0.9028 0.0191, -0.01930, 0.9941 0.0397, -0.03030, 0.9848 0.0706, -0.04420, 0.8690 0.1037, -0.05710, 0.7275 0.1384, -0.06890, 0.5750 0.1741, -0.07950, 0.4303 0.2102, -0.08660, 0.2789 0.2472, -0.09640, 0.1049 0.2844, -0.10270, -0.0386 0.3225, -0.10690, -0.1943 0.3608, -0.10890, -0.3286 0.3991, -0.10830, -0.4400 0.4373, -0.10510, -0.5011 0.4757, -0.09890, -0.4723 0.5137, -0.09070, -0.4633 0.5694, -0.07640, -0.3633 15 Flap element taps 1.0000, 0.00130, -0.6417 0.9365, 0.01390, -0.6929 0.8333, 0.03280, -0.7255 0.7436, 0.04930, -0.7261 0.7049, 0.05670, -0.7160 0.6662, 0.06410, -0.7005 0.6522, 0.01390, -0.4597 0.5969, -0.00020, -0.4647 0.6000, -0.03020, -0.4643 0.6324, -0.04540, -0.4671 0.6667, -0.04880, 0.0910 0.7046, -0.04110, -0.1697 0.7429, -0.03210, -0.0985 0.8333, -0.01400, -0.0449 0.9311, -0.00120, -0.1117 --------- Run Conditions: vel=213.7 ft/s Re=2.002x10^6 AOA=23.98 Flap deflection=-5.00 Totals: Cl=0.5820 Cdp=0.3368 Cm(c/4)=-0.0893 Cs=-0.0712 Ch=-0.1773 Main component: Cl=0.3930 Cdp=0.2843 Cm=-0.0998 Flap component: Cl=0.1889 Cdp=0.0525 Cm=-0.1566 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3554 0.6175, -0.04610, -0.5245 0.5841, -0.02440, -0.5233 0.5775, 0.01750, -0.5263 0.5777, 0.04660, -0.5237 0.6274, 0.07170, -0.7178 0.5694, 0.08320, -0.7246 0.5112, 0.09370, -0.7244 0.4731, 0.09830, -0.7200 0.4349, 0.10070, -0.7191 0.3960, 0.10120, -0.7087 0.3566, 0.10020, -0.7147 0.3172, 0.09790, -0.7079 0.2778, 0.09440, -0.7077 0.2393, 0.08960, -0.7058 0.2056, 0.08360, -0.7011 0.1633, 0.07610, -0.7098 0.1261, 0.06710, -0.7054 0.0900, 0.05640, -0.7018 0.0571, 0.04390, -0.7034 0.0283, 0.02940, -0.7105 0.0142, 0.01970, -0.7213 0.0081, 0.01410, -0.7313 0.0026, 0.00780, -0.7015 0.0000, 0.00000, -0.9136 0.0037, -0.00840, 0.4288 0.0112, -0.01420, 0.8868 0.0191, -0.01930, 0.9890 0.0397, -0.03030, 0.9961 0.0706, -0.04420, 0.8954 0.1037, -0.05710, 0.7638 0.1384, -0.06890, 0.6163 0.1741, -0.07950, 0.4749 0.2102, -0.08660, 0.3243 0.2472, -0.09640, 0.1498 0.2844, -0.10270, 0.0022 0.3225, -0.10690, -0.1593 0.3608, -0.10890, -0.3013 0.3991, -0.10830, -0.4220 0.4373, -0.10510, -0.4944 0.4757, -0.09890, -0.4756 0.5137, -0.09070, -0.4747 0.5694, -0.07640, -0.3799 15 Flap element taps 1.0000, 0.00130, -0.6786 0.9365, 0.01390, -0.7153 0.8333, 0.03280, -0.7295 0.7436, 0.04930, -0.7262 0.7049, 0.05670, -0.7218 0.6662, 0.06410, -0.7159 0.6522, 0.01390, -0.5225 0.5969, -0.00020, -0.5288 0.6000, -0.03020, -0.5273 0.6324, -0.04540, -0.5349 0.6667, -0.04880, 0.1624 0.7046, -0.04110, -0.2009 0.7429, -0.03210, -0.1304 0.8333, -0.01400, -0.0823 0.9311, -0.00120, -0.1514 --------- Run Conditions: vel=215.8 ft/s Re=2.018x10^6 AOA=27.02 Flap deflection=-5.00 Totals: Cl=0.7816 Cdp=0.4710 Cm(c/4)=-0.1356 Cs=-0.0645 Ch=-0.2342 Main component: Cl=0.5420 Cdp=0.3773 Cm=-0.1572 Flap component: Cl=0.2396 Cdp=0.0936 Cm=-0.2059 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3431 0.6175, -0.04610, -0.5153 0.5841, -0.02440, -0.5171 0.5775, 0.01750, -0.5200 0.5777, 0.04660, -0.5147 0.6274, 0.07170, -0.9297 0.5694, 0.08320, -0.9423 0.5112, 0.09370, -0.9396 0.4731, 0.09830, -0.9359 0.4349, 0.10070, -0.9312 0.3960, 0.10120, -0.9175 0.3566, 0.10020, -0.9222 0.3172, 0.09790, -0.9135 0.2778, 0.09440, -0.9127 0.2393, 0.08960, -0.9091 0.2056, 0.08360, -0.9021 0.1633, 0.07610, -0.9088 0.1261, 0.06710, -0.9031 0.0900, 0.05640, -0.9015 0.0571, 0.04390, -0.9021 0.0283, 0.02940, -0.9077 0.0142, 0.01970, -0.9144 0.0081, 0.01410, -0.9192 0.0026, 0.00780, -0.8884 0.0000, 0.00000, -0.9473 0.0037, -0.00840, 0.1450 0.0112, -0.01420, 0.7531 0.0191, -0.01930, 0.9280 0.0397, -0.03030, 1.0090 0.0706, -0.04420, 0.9577 0.1037, -0.05710, 0.8540 0.1384, -0.06890, 0.7241 0.1741, -0.07950, 0.5944 0.2102, -0.08660, 0.4541 0.2472, -0.09640, 0.2870 0.2844, -0.10270, 0.1413 0.3225, -0.10690, -0.0201 0.3608, -0.10890, -0.1652 0.3991, -0.10830, -0.2934 0.4373, -0.10510, -0.3789 0.4757, -0.09890, -0.3797 0.5137, -0.09070, -0.3962 0.5694, -0.07640, -0.3221 15 Flap element taps 1.0000, 0.00130, -0.8907 0.9365, 0.01390, -0.9217 0.8333, 0.03280, -0.9367 0.7436, 0.04930, -0.9381 0.7049, 0.05670, -0.9348 0.6662, 0.06410, -0.9269 0.6522, 0.01390, -0.5160 0.5969, -0.00020, -0.5238 0.6000, -0.03020, -0.5206 0.6324, -0.04540, -0.5430 0.6667, -0.04880, 0.2550 0.7046, -0.04110, -0.1854 0.7429, -0.03210, -0.1217 0.8333, -0.01400, -0.1002 0.9311, -0.00120, -0.2099