S809 UNVENTED AILERON, LEGR, CHORD = 18 IN --------- Run Conditions: vel=203.7 ft/s Re=1.994x10^6 AOA=-6.01 Flap deflection=0.00 Totals: Cl=-0.4680 Cdp=0.0332 Cm(c/4)=0.0059 Cs=0.0160 Ch=0.0565 Main component: Cl=-0.4139 Cdp=0.0367 Cm=0.0797 Flap component: Cl=-0.0541 Cdp=-0.0035 Cm=0.0434 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2603 0.6175, -0.04610, -0.2385 0.5841, -0.02440, -0.2205 0.5775, 0.01750, -0.2202 0.5777, 0.04660, -0.2200 0.6274, 0.07170, -0.0997 0.5694, 0.08320, -0.2242 0.5112, 0.09370, -0.4260 0.4731, 0.09830, -0.4729 0.4349, 0.10070, -0.4493 0.3960, 0.10120, -0.3774 0.3566, 0.10020, -0.3191 0.3172, 0.09790, -0.2476 0.2778, 0.09440, -0.1932 0.2393, 0.08960, -0.1376 0.2056, 0.08360, -0.0586 0.1633, 0.07610, 0.0390 0.1261, 0.06710, 0.1722 0.0900, 0.05640, 0.2289 0.0571, 0.04390, 0.5298 0.0283, 0.02940, 0.7979 0.0142, 0.01970, 0.9804 0.0081, 0.01410, 1.0109 0.0026, 0.00780, 0.6948 0.0000, 0.00000, -0.0896 0.0037, -0.00840, -1.3005 0.0112, -0.01420, -1.0678 0.0191, -0.01930, -1.0143 0.0397, -0.03030, -0.8098 0.0706, -0.04420, -0.8132 0.1037, -0.05710, -0.7763 0.1384, -0.06890, -0.8711 0.1741, -0.07950, -0.9055 0.2102, -0.08660, -0.9639 0.2472, -0.09640, -1.0368 0.2844, -0.10270, -1.0485 0.3225, -0.10690, -1.0425 0.3608, -0.10890, -1.0076 0.3991, -0.10830, -0.9056 0.4373, -0.10510, -0.7224 0.4757, -0.09890, -0.4616 0.5137, -0.09070, -0.3103 0.5694, -0.07640, -0.2627 14 Flap element taps 1.0000, 0.00130, -0.0786 0.9365, 0.01390, -0.0325 0.8333, 0.03280, -0.0472 0.7436, 0.04930, -0.0766 0.7049, 0.05670, -0.0728 0.6662, 0.06410, -0.1886 0.6522, 0.01390, -0.2153 0.5969, -0.00020, -0.2222 0.6000, -0.03020, -0.2462 0.6324, -0.04540, -0.2452 0.6667, -0.04880, -0.2514 0.7046, -0.04110, -0.2526 0.7429, -0.03210, -0.2562 0.9311, -0.00120, -0.2038 --------- Run Conditions: vel=205.0 ft/s Re=2.000x10^6 AOA=0.01 Flap deflection=0.00 Totals: Cl=-0.0356 Cdp=-0.0015 Cm(c/4)=-0.0151 Cs=0.0015 Ch=-0.0294 Main component: Cl=-0.0733 Cdp=0.0194 Cm=0.0243 Flap component: Cl=0.0377 Cdp=-0.0209 Cm=-0.0304 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1821 0.6175, -0.04610, -0.1212 0.5841, -0.02440, -0.1190 0.5775, 0.01750, -0.1225 0.5777, 0.04660, -0.1216 0.6274, 0.07170, -0.1607 0.5694, 0.08320, -0.3124 0.5112, 0.09370, -0.5605 0.4731, 0.09830, -0.6449 0.4349, 0.10070, -0.6570 0.3960, 0.10120, -0.6124 0.3566, 0.10020, -0.5843 0.3172, 0.09790, -0.5399 0.2778, 0.09440, -0.5200 0.2393, 0.08960, -0.5021 0.2056, 0.08360, -0.4616 0.1633, 0.07610, -0.4052 0.1261, 0.06710, -0.3135 0.0900, 0.05640, -0.3652 0.0571, 0.04390, -0.0727 0.0283, 0.02940, 0.1772 0.0142, 0.01970, 0.4224 0.0081, 0.01410, 0.6296 0.0026, 0.00780, 0.7759 0.0000, 0.00000, -0.0505 0.0037, -0.00840, 0.5385 0.0112, -0.01420, 0.2997 0.0191, -0.01930, 0.1530 0.0397, -0.03030, 0.0369 0.0706, -0.04420, -0.1300 0.1037, -0.05710, -0.2082 0.1384, -0.06890, -0.3838 0.1741, -0.07950, -0.4854 0.2102, -0.08660, -0.5983 0.2472, -0.09640, -0.7311 0.2844, -0.10270, -0.8051 0.3225, -0.10690, -0.8717 0.3608, -0.10890, -0.9163 0.3991, -0.10830, -0.9093 0.4373, -0.10510, -0.8459 0.4757, -0.09890, -0.6835 0.5137, -0.09070, -0.5491 0.5694, -0.07640, -0.3221 14 Flap element taps 1.0000, 0.00130, 0.1823 0.9365, 0.01390, 0.1081 0.8333, 0.03280, 0.0055 0.7436, 0.04930, -0.0752 0.7049, 0.05670, -0.0966 0.6662, 0.06410, -0.2045 0.6522, 0.01390, -0.1185 0.5969, -0.00020, -0.1207 0.6000, -0.03020, -0.1203 0.6324, -0.04540, -0.1188 0.6667, -0.04880, -0.1026 0.7046, -0.04110, 0.0054 0.7429, -0.03210, 0.0569 0.9311, -0.00120, 0.2229 Wake drag found for this condition, Cdw=0.0121 --------- Run Conditions: vel=205.2 ft/s Re=1.998x10^6 AOA=3.05 Flap deflection=0.00 Totals: Cl=0.2834 Cdp=0.0030 Cm(c/4)=-0.0227 Cs=0.0121 Ch=-0.0515 Main component: Cl=0.2170 Cdp=0.0215 Cm=-0.0413 Flap component: Cl=0.0664 Cdp=-0.0185 Cm=-0.0521 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1445 0.6175, -0.04610, -0.1089 0.5841, -0.02440, -0.1090 0.5775, 0.01750, -0.1100 0.5777, 0.04660, -0.1085 0.6274, 0.07170, -0.2340 0.5694, 0.08320, -0.3964 0.5112, 0.09370, -0.6676 0.4731, 0.09830, -0.7747 0.4349, 0.10070, -0.8084 0.3960, 0.10120, -0.7800 0.3566, 0.10020, -0.7696 0.3172, 0.09790, -0.7438 0.2778, 0.09440, -0.7455 0.2393, 0.08960, -0.7531 0.2056, 0.08360, -0.7403 0.1633, 0.07610, -0.7179 0.1261, 0.06710, -0.6629 0.0900, 0.05640, -0.7967 0.0571, 0.04390, -0.5562 0.0283, 0.02940, -0.4066 0.0142, 0.01970, -0.2210 0.0081, 0.01410, -0.0971 0.0026, 0.00780, 0.1185 0.0000, 0.00000, -0.0197 0.0037, -0.00840, 0.9720 0.0112, -0.01420, 0.7917 0.0191, -0.01930, 0.6366 0.0397, -0.03030, 0.4402 0.0706, -0.04420, 0.2357 0.1037, -0.05710, 0.1136 0.1384, -0.06890, -0.0784 0.1741, -0.07950, -0.2005 0.2102, -0.08660, -0.3260 0.2472, -0.09640, -0.4709 0.2844, -0.10270, -0.5614 0.3225, -0.10690, -0.6473 0.3608, -0.10890, -0.7104 0.3991, -0.10830, -0.7264 0.4373, -0.10510, -0.6924 0.4757, -0.09890, -0.5626 0.5137, -0.09070, -0.4550 0.5694, -0.07640, -0.2568 14 Flap element taps 1.0000, 0.00130, 0.1634 0.9365, 0.01390, 0.0948 0.8333, 0.03280, -0.0204 0.7436, 0.04930, -0.1181 0.7049, 0.05670, -0.1505 0.6662, 0.06410, -0.2488 0.6522, 0.01390, -0.1066 0.5969, -0.00020, -0.1102 0.6000, -0.03020, -0.1090 0.6324, -0.04540, -0.1064 0.6667, -0.04880, -0.0306 0.7046, -0.04110, 0.0880 0.7429, -0.03210, 0.1283 0.9311, -0.00120, 0.2569 Wake drag found for this condition, Cdw=0.0135 --------- Run Conditions: vel=205.3 ft/s Re=1.996x10^6 AOA=6.01 Flap deflection=0.00 Totals: Cl=0.5708 Cdp=0.0203 Cm(c/4)=-0.0255 Cs=0.0395 Ch=-0.0668 Main component: Cl=0.4841 Cdp=0.0313 Cm=-0.1007 Flap component: Cl=0.0867 Cdp=-0.0109 Cm=-0.0673 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.0975 0.6175, -0.04610, -0.0801 0.5841, -0.02440, -0.0811 0.5775, 0.01750, -0.0834 0.5777, 0.04660, -0.0803 0.6274, 0.07170, -0.2896 0.5694, 0.08320, -0.4544 0.5112, 0.09370, -0.7411 0.4731, 0.09830, -0.8726 0.4349, 0.10070, -0.9313 0.3960, 0.10120, -0.9238 0.3566, 0.10020, -0.9347 0.3172, 0.09790, -0.9298 0.2778, 0.09440, -0.9573 0.2393, 0.08960, -0.9932 0.2056, 0.08360, -1.0115 0.1633, 0.07610, -1.0312 0.1261, 0.06710, -1.0207 0.0900, 0.05640, -1.2367 0.0571, 0.04390, -1.0887 0.0283, 0.02940, -1.0901 0.0142, 0.01970, -1.0685 0.0081, 0.01410, -1.0321 0.0026, 0.00780, -0.6955 0.0000, 0.00000, 0.0056 0.0037, -0.00840, 0.9623 0.0112, -0.01420, 0.9967 0.0191, -0.01930, 0.9160 0.0397, -0.03030, 0.7270 0.0706, -0.04420, 0.5179 0.1037, -0.05710, 0.3734 0.1384, -0.06890, 0.1790 0.1741, -0.07950, 0.0458 0.2102, -0.08660, -0.0869 0.2472, -0.09640, -0.2387 0.2844, -0.10270, -0.3411 0.3225, -0.10690, -0.4424 0.3608, -0.10890, -0.5193 0.3991, -0.10830, -0.5553 0.4373, -0.10510, -0.5434 0.4757, -0.09890, -0.4418 0.5137, -0.09070, -0.3571 0.5694, -0.07640, -0.1860 14 Flap element taps 1.0000, 0.00130, 0.1163 0.9365, 0.01390, 0.0657 0.8333, 0.03280, -0.0412 0.7436, 0.04930, -0.1460 0.7049, 0.05670, -0.1876 0.6662, 0.06410, -0.2713 0.6522, 0.01390, -0.0787 0.5969, -0.00020, -0.0837 0.6000, -0.03020, -0.0811 0.6324, -0.04540, -0.0776 0.6667, -0.04880, 0.0899 0.7046, -0.04110, 0.1397 0.7429, -0.03210, 0.1701 0.9311, -0.00120, 0.2630 Wake drag found for this condition, Cdw=0.0167 --------- Run Conditions: vel=204.8 ft/s Re=1.990x10^6 AOA=9.01 Flap deflection=0.00 Totals: Cl=0.7861 Cdp=0.0506 Cm(c/4)=-0.0270 Cs=0.0731 Ch=-0.0895 Main component: Cl=0.6793 Cdp=0.0484 Cm=-0.1389 Flap component: Cl=0.1068 Cdp=0.0023 Cm=-0.0842 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.0684 0.6175, -0.04610, -0.0645 0.5841, -0.02440, -0.0693 0.5775, 0.01750, -0.0704 0.5777, 0.04660, -0.0667 0.6274, 0.07170, -0.3080 0.5694, 0.08320, -0.4493 0.5112, 0.09370, -0.7273 0.4731, 0.09830, -0.8827 0.4349, 0.10070, -0.9702 0.3960, 0.10120, -0.9886 0.3566, 0.10020, -1.0255 0.3172, 0.09790, -1.0451 0.2778, 0.09440, -1.0993 0.2393, 0.08960, -1.1644 0.2056, 0.08360, -1.2155 0.1633, 0.07610, -1.2803 0.1261, 0.06710, -1.3173 0.0900, 0.05640, -1.6033 0.0571, 0.04390, -1.5773 0.0283, 0.02940, -1.7666 0.0142, 0.01970, -1.9632 0.0081, 0.01410, -2.0857 0.0026, 0.00780, -1.7764 0.0000, 0.00000, 0.0174 0.0037, -0.00840, 0.6488 0.0112, -0.01420, 0.9924 0.0191, -0.01930, 1.0091 0.0397, -0.03030, 0.8932 0.0706, -0.04420, 0.7082 0.1037, -0.05710, 0.5576 0.1384, -0.06890, 0.3685 0.1741, -0.07950, 0.2296 0.2102, -0.08660, 0.0938 0.2472, -0.09640, -0.0586 0.2844, -0.10270, -0.1685 0.3225, -0.10690, -0.2824 0.3608, -0.10890, -0.3714 0.3991, -0.10830, -0.4244 0.4373, -0.10510, -0.4313 0.4757, -0.09890, -0.3525 0.5137, -0.09070, -0.2856 0.5694, -0.07640, -0.1386 14 Flap element taps 1.0000, 0.00130, 0.0021 0.9365, 0.01390, -0.0460 0.8333, 0.03280, -0.1082 0.7436, 0.04930, -0.1795 0.7049, 0.05670, -0.2129 0.6662, 0.06410, -0.2657 0.6522, 0.01390, -0.0653 0.5969, -0.00020, -0.0717 0.6000, -0.03020, -0.0680 0.6324, -0.04540, -0.0644 0.6667, -0.04880, 0.1911 0.7046, -0.04110, 0.1596 0.7429, -0.03210, 0.1831 0.9311, -0.00120, 0.2355 Wake drag found for this condition, Cdw=0.0256 --------- Run Conditions: vel=206.1 ft/s Re=2.000x10^6 AOA=12.01 Flap deflection=0.00 Totals: Cl=0.8899 Cdp=0.0898 Cm(c/4)=-0.0311 Cs=0.0974 Ch=-0.1381 Main component: Cl=0.7461 Cdp=0.0630 Cm=-0.1357 Flap component: Cl=0.1438 Cdp=0.0267 Cm=-0.1178 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.0657 0.6175, -0.04610, -0.0828 0.5841, -0.02440, -0.0861 0.5775, 0.01750, -0.0877 0.5777, 0.04660, -0.0837 0.6274, 0.07170, -0.3285 0.5694, 0.08320, -0.3448 0.5112, 0.09370, -0.4447 0.4731, 0.09830, -0.6005 0.4349, 0.10070, -0.7502 0.3960, 0.10120, -0.8362 0.3566, 0.10020, -0.9301 0.3172, 0.09790, -0.9964 0.2778, 0.09440, -1.0915 0.2393, 0.08960, -1.1935 0.2056, 0.08360, -1.2857 0.1633, 0.07610, -1.4005 0.1261, 0.06710, -1.4937 0.0900, 0.05640, -1.8350 0.0571, 0.04390, -1.9445 0.0283, 0.02940, -2.3322 0.0142, 0.01970, -2.7493 0.0081, 0.01410, -3.0783 0.0026, 0.00780, -2.8956 0.0000, 0.00000, 0.0251 0.0037, -0.00840, 0.1818 0.0112, -0.01420, 0.8731 0.0191, -0.01930, 0.9986 0.0397, -0.03030, 0.9750 0.0706, -0.04420, 0.8305 0.1037, -0.05710, 0.6863 0.1384, -0.06890, 0.5079 0.1741, -0.07950, 0.3663 0.2102, -0.08660, 0.2259 0.2472, -0.09640, 0.0680 0.2844, -0.10270, -0.0476 0.3225, -0.10690, -0.1673 0.3608, -0.10890, -0.2668 0.3991, -0.10830, -0.3366 0.4373, -0.10510, -0.3581 0.4757, -0.09890, -0.2995 0.5137, -0.09070, -0.2484 0.5694, -0.07640, -0.1181 14 Flap element taps 1.0000, 0.00130, -0.2136 0.9365, 0.01390, -0.3008 0.8333, 0.03280, -0.3017 0.7436, 0.04930, -0.3140 0.7049, 0.05670, -0.3155 0.6662, 0.06410, -0.3192 0.6522, 0.01390, -0.0820 0.5969, -0.00020, -0.0890 0.6000, -0.03020, -0.0856 0.6324, -0.04540, -0.0818 0.6667, -0.04880, 0.2080 0.7046, -0.04110, 0.1457 0.7429, -0.03210, 0.1623 0.9311, -0.00120, 0.1519 --------- Run Conditions: vel=206.1 ft/s Re=1.994x10^6 AOA=15.02 Flap deflection=0.00 Totals: Cl=0.9397 Cdp=0.1315 Cm(c/4)=-0.0346 Cs=0.1165 Ch=-0.1636 Main component: Cl=0.7714 Cdp=0.0862 Cm=-0.1302 Flap component: Cl=0.1682 Cdp=0.0452 Cm=-0.1399 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.0680 0.6175, -0.04610, -0.1071 0.5841, -0.02440, -0.1092 0.5775, 0.01750, -0.1156 0.5777, 0.04660, -0.1105 0.6274, 0.07170, -0.3948 0.5694, 0.08320, -0.3902 0.5112, 0.09370, -0.3984 0.4731, 0.09830, -0.4305 0.4349, 0.10070, -0.5021 0.3960, 0.10120, -0.6015 0.3566, 0.10020, -0.7212 0.3172, 0.09790, -0.8396 0.2778, 0.09440, -0.9771 0.2393, 0.08960, -1.1226 0.2056, 0.08360, -1.2698 0.1633, 0.07610, -1.4214 0.1261, 0.06710, -1.5794 0.0900, 0.05640, -1.9529 0.0571, 0.04390, -2.1981 0.0283, 0.02940, -2.7559 0.0142, 0.01970, -3.3799 0.0081, 0.01410, -3.9014 0.0026, 0.00780, -3.9036 0.0000, 0.00000, -0.1864 0.0037, -0.00840, -0.3117 0.0112, -0.01420, 0.7056 0.0191, -0.01930, 0.9399 0.0397, -0.03030, 1.0097 0.0706, -0.04420, 0.9052 0.1037, -0.05710, 0.7727 0.1384, -0.06890, 0.6156 0.1741, -0.07950, 0.4729 0.2102, -0.08660, 0.3231 0.2472, -0.09640, 0.1663 0.2844, -0.10270, 0.0369 0.3225, -0.10690, -0.0880 0.3608, -0.10890, -0.1997 0.3991, -0.10830, -0.2866 0.4373, -0.10510, -0.3204 0.4757, -0.09890, -0.2774 0.5137, -0.09070, -0.2374 0.5694, -0.07640, -0.0997 14 Flap element taps 1.0000, 0.00130, -0.3449 0.9365, 0.01390, -0.4275 0.8333, 0.03280, -0.4191 0.7436, 0.04930, -0.4154 0.7049, 0.05670, -0.4082 0.6662, 0.06410, -0.4010 0.6522, 0.01390, -0.1118 0.5969, -0.00020, -0.1171 0.6000, -0.03020, -0.1134 0.6324, -0.04540, -0.1132 0.6667, -0.04880, 0.3017 0.7046, -0.04110, 0.1338 0.7429, -0.03210, 0.1455 0.9311, -0.00120, 0.0968 --------- Run Conditions: vel=203.6 ft/s Re=1.990x10^6 AOA=18.01 Flap deflection=0.00 Totals: Cl=0.7966 Cdp=0.2179 Cm(c/4)=-0.0719 Cs=0.0391 Ch=-0.1920 Main component: Cl=0.5986 Cdp=0.1507 Cm=-0.1111 Flap component: Cl=0.1980 Cdp=0.0672 Cm=-0.1670 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1408 0.6175, -0.04610, -0.1929 0.5841, -0.02440, -0.1982 0.5775, 0.01750, -0.2007 0.5777, 0.04660, -0.1928 0.6274, 0.07170, -0.5908 0.5694, 0.08320, -0.5921 0.5112, 0.09370, -0.5881 0.4731, 0.09830, -0.5873 0.4349, 0.10070, -0.5863 0.3960, 0.10120, -0.5874 0.3566, 0.10020, -0.6073 0.3172, 0.09790, -0.6225 0.2778, 0.09440, -0.6563 0.2393, 0.08960, -0.7077 0.2056, 0.08360, -0.7866 0.1633, 0.07610, -0.8921 0.1261, 0.06710, -1.0273 0.0900, 0.05640, -1.2805 0.0571, 0.04390, -1.5790 0.0283, 0.02940, -2.1394 0.0142, 0.01970, -2.7738 0.0081, 0.01410, -3.2765 0.0026, 0.00780, -3.3681 0.0000, 0.00000, -0.1854 0.0037, -0.00840, -0.2122 0.0112, -0.01420, 0.7239 0.0191, -0.01930, 0.9421 0.0397, -0.03030, 1.0069 0.0706, -0.04420, 0.9054 0.1037, -0.05710, 0.7751 0.1384, -0.06890, 0.6176 0.1741, -0.07950, 0.4735 0.2102, -0.08660, 0.3220 0.2472, -0.09640, 0.1594 0.2844, -0.10270, 0.0241 0.3225, -0.10690, -0.1103 0.3608, -0.10890, -0.2328 0.3991, -0.10830, -0.3293 0.4373, -0.10510, -0.3705 0.4757, -0.09890, -0.3318 0.5137, -0.09070, -0.3021 0.5694, -0.07640, -0.1649 14 Flap element taps 1.0000, 0.00130, -0.5117 0.9365, 0.01390, -0.5829 0.8333, 0.03280, -0.6087 0.7436, 0.04930, -0.6067 0.7049, 0.05670, -0.6035 0.6662, 0.06410, -0.6021 0.6522, 0.01390, -0.1976 0.5969, -0.00020, -0.2045 0.6000, -0.03020, -0.1989 0.6324, -0.04540, -0.1992 0.6667, -0.04880, 0.3280 0.7046, -0.04110, 0.0696 0.7429, -0.03210, 0.0776 0.9311, -0.00120, -0.0021 --------- Run Conditions: vel=204.3 ft/s Re=1.997x10^6 AOA=19.99 Flap deflection=0.00 Totals: Cl=0.7085 Cdp=0.2865 Cm(c/4)=-0.0980 Cs=-0.0270 Ch=-0.2000 Main component: Cl=0.5022 Cdp=0.2080 Cm=-0.1131 Flap component: Cl=0.2063 Cdp=0.0784 Cm=-0.1758 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1614 0.6175, -0.04610, -0.2174 0.5841, -0.02440, -0.2232 0.5775, 0.01750, -0.2269 0.5777, 0.04660, -0.2183 0.6274, 0.07170, -0.6488 0.5694, 0.08320, -0.6541 0.5112, 0.09370, -0.6576 0.4731, 0.09830, -0.6549 0.4349, 0.10070, -0.6629 0.3960, 0.10120, -0.6616 0.3566, 0.10020, -0.6762 0.3172, 0.09790, -0.6886 0.2778, 0.09440, -0.7097 0.2393, 0.08960, -0.7256 0.2056, 0.08360, -0.7428 0.1633, 0.07610, -0.7671 0.1261, 0.06710, -0.7955 0.0900, 0.05640, -0.8071 0.0571, 0.04390, -0.8880 0.0283, 0.02940, -1.1361 0.0142, 0.01970, -1.5591 0.0081, 0.01410, -1.9169 0.0026, 0.00780, -2.0939 0.0000, 0.00000, -0.1732 0.0037, -0.00840, 0.0755 0.0112, -0.01420, 0.7971 0.0191, -0.01930, 0.9651 0.0397, -0.03030, 1.0040 0.0706, -0.04420, 0.9020 0.1037, -0.05710, 0.7771 0.1384, -0.06890, 0.6231 0.1741, -0.07950, 0.4818 0.2102, -0.08660, 0.3335 0.2472, -0.09640, 0.1709 0.2844, -0.10270, 0.0347 0.3225, -0.10690, -0.1029 0.3608, -0.10890, -0.2264 0.3991, -0.10830, -0.3267 0.4373, -0.10510, -0.3732 0.4757, -0.09890, -0.3395 0.5137, -0.09070, -0.3088 0.5694, -0.07640, -0.1810 14 Flap element taps 1.0000, 0.00130, -0.5475 0.9365, 0.01390, -0.6238 0.8333, 0.03280, -0.6694 0.7436, 0.04930, -0.6701 0.7049, 0.05670, -0.6572 0.6662, 0.06410, -0.6635 0.6522, 0.01390, -0.2241 0.5969, -0.00020, -0.2317 0.6000, -0.03020, -0.2259 0.6324, -0.04540, -0.2259 0.6667, -0.04880, 0.3747 0.7046, -0.04110, 0.0485 0.7429, -0.03210, 0.0562 0.9311, -0.00120, -0.0340 --------- Run Conditions: vel=207.7 ft/s Re=2.025x10^6 AOA=23.99 Flap deflection=0.00 Totals: Cl=0.9191 Cdp=0.4310 Cm(c/4)=-0.1290 Cs=-0.0201 Ch=-0.2346 Main component: Cl=0.6818 Cdp=0.3163 Cm=-0.1738 Flap component: Cl=0.2372 Cdp=0.1147 Cm=-0.2089 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1479 0.6175, -0.04610, -0.2184 0.5841, -0.02440, -0.2311 0.5775, 0.01750, -0.2361 0.5777, 0.04660, -0.2233 0.6274, 0.07170, -0.8309 0.5694, 0.08320, -0.8341 0.5112, 0.09370, -0.8494 0.4731, 0.09830, -0.8853 0.4349, 0.10070, -0.9112 0.3960, 0.10120, -0.9222 0.3566, 0.10020, -0.9458 0.3172, 0.09790, -0.9769 0.2778, 0.09440, -1.0304 0.2393, 0.08960, -1.0764 0.2056, 0.08360, -1.1163 0.1633, 0.07610, -1.1636 0.1261, 0.06710, -1.2095 0.0900, 0.05640, -1.2405 0.0571, 0.04390, -1.2987 0.0283, 0.02940, -1.3533 0.0142, 0.01970, -1.4987 0.0081, 0.01410, -1.6621 0.0026, 0.00780, -1.6480 0.0000, 0.00000, -0.1613 0.0037, -0.00840, -0.1629 0.0112, -0.01420, 0.6685 0.0191, -0.01930, 0.8990 0.0397, -0.03030, 1.0093 0.0706, -0.04420, 0.9550 0.1037, -0.05710, 0.8519 0.1384, -0.06890, 0.7148 0.1741, -0.07950, 0.5832 0.2102, -0.08660, 0.4421 0.2472, -0.09640, 0.2829 0.2844, -0.10270, 0.1447 0.3225, -0.10690, -0.0016 0.3608, -0.10890, -0.1353 0.3991, -0.10830, -0.2441 0.4373, -0.10510, -0.3031 0.4757, -0.09890, -0.2865 0.5137, -0.09070, -0.2713 0.5694, -0.07640, -0.1602 14 Flap element taps 1.0000, 0.00130, -0.7019 0.9365, 0.01390, -0.7616 0.8333, 0.03280, -0.7923 0.7436, 0.04930, -0.8120 0.7049, 0.05670, -0.8120 0.6662, 0.06410, -0.7856 0.6522, 0.01390, -0.2333 0.5969, -0.00020, -0.2445 0.6000, -0.03020, -0.2348 0.6324, -0.04540, -0.2427 0.6667, -0.04880, 0.5862 0.7046, -0.04110, 0.0479 0.7429, -0.03210, 0.0540 0.9311, -0.00120, -0.0791 --------- Run Conditions: vel=204.2 ft/s Re=1.988x10^6 AOA=27.01 Flap deflection=0.00 Totals: Cl=0.8296 Cdp=0.4828 Cm(c/4)=-0.1380 Cs=-0.0534 Ch=-0.2364 Main component: Cl=0.5963 Cdp=0.3528 Cm=-0.1662 Flap component: Cl=0.2333 Cdp=0.1300 Cm=-0.2114 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1431 0.6175, -0.04610, -0.2225 0.5841, -0.02440, -0.2351 0.5775, 0.01750, -0.2388 0.5777, 0.04660, -0.2255 0.6274, 0.07170, -0.8291 0.5694, 0.08320, -0.8439 0.5112, 0.09370, -0.8539 0.4731, 0.09830, -0.8556 0.4349, 0.10070, -0.8593 0.3960, 0.10120, -0.8544 0.3566, 0.10020, -0.8740 0.3172, 0.09790, -0.8815 0.2778, 0.09440, -0.8907 0.2393, 0.08960, -0.9055 0.2056, 0.08360, -0.9188 0.1633, 0.07610, -0.9534 0.1261, 0.06710, -0.9810 0.0900, 0.05640, -1.0024 0.0571, 0.04390, -1.0094 0.0283, 0.02940, -1.0265 0.0142, 0.01970, -1.0972 0.0081, 0.01410, -1.1389 0.0026, 0.00780, -1.0177 0.0000, 0.00000, -0.1586 0.0037, -0.00840, -0.0127 0.0112, -0.01420, 0.6914 0.0191, -0.01930, 0.9005 0.0397, -0.03030, 1.0117 0.0706, -0.04420, 0.9708 0.1037, -0.05710, 0.8790 0.1384, -0.06890, 0.7507 0.1741, -0.07950, 0.6259 0.2102, -0.08660, 0.4916 0.2472, -0.09640, 0.3359 0.2844, -0.10270, 0.1998 0.3225, -0.10690, 0.0514 0.3608, -0.10890, -0.0838 0.3991, -0.10830, -0.1976 0.4373, -0.10510, -0.2631 0.4757, -0.09890, -0.2547 0.5137, -0.09070, -0.2487 0.5694, -0.07640, -0.1565 14 Flap element taps 1.0000, 0.00130, -0.7568 0.9365, 0.01390, -0.7901 0.8333, 0.03280, -0.8122 0.7436, 0.04930, -0.8263 0.7049, 0.05670, -0.8218 0.6662, 0.06410, -0.7913 0.6522, 0.01390, -0.2355 0.5969, -0.00020, -0.2480 0.6000, -0.03020, -0.2385 0.6324, -0.04540, -0.2466 0.6667, -0.04880, 0.6516 0.7046, -0.04110, 0.0432 0.7429, -0.03210, 0.0480 0.9311, -0.00120, -0.1065