S809 UNVENTED AILERON, LEGR, CHORD = 18 IN --------- Run Conditions: vel=205.8 ft/s Re=2.010x10^6 AOA=-6.00 Flap deflection=-5.00 Totals: Cl=-0.6079 Cdp=0.0530 Cm(c/4)=0.0314 Cs=0.0108 Ch=0.0850 Main component: Cl=-0.5157 Cdp=0.0391 Cm=0.1093 Flap component: Cl=-0.0922 Cdp=0.0139 Cm=0.0746 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3032 0.6175, -0.04610, -0.2865 0.5841, -0.02440, -0.2558 0.5775, 0.01750, -0.2541 0.5777, 0.04660, -0.2542 0.6274, 0.07170, 0.0550 0.5694, 0.08320, -0.0955 0.5112, 0.09370, -0.3015 0.4731, 0.09830, -0.3539 0.4349, 0.10070, -0.3435 0.3960, 0.10120, -0.2807 0.3566, 0.10020, -0.2266 0.3172, 0.09790, -0.1599 0.2778, 0.09440, -0.1103 0.2393, 0.08960, -0.0550 0.2056, 0.08360, 0.0185 0.1633, 0.07610, 0.1187 0.1261, 0.06710, 0.2480 0.0900, 0.05640, 0.3143 0.0571, 0.04390, 0.6018 0.0283, 0.02940, 0.8538 0.0142, 0.01970, 1.0020 0.0081, 0.01410, 1.0001 0.0026, 0.00780, 0.5954 0.0000, 0.00000, -0.0976 0.0037, -0.00840, -1.6619 0.0112, -0.01420, -1.3118 0.0191, -0.01930, -1.2256 0.0397, -0.03030, -0.9562 0.0706, -0.04420, -0.9285 0.1037, -0.05710, -0.8758 0.1384, -0.06890, -0.9588 0.1741, -0.07950, -0.9880 0.2102, -0.08660, -1.0466 0.2472, -0.09640, -1.1147 0.2844, -0.10270, -1.1250 0.3225, -0.10690, -1.1122 0.3608, -0.10890, -1.0701 0.3991, -0.10830, -0.9563 0.4373, -0.10510, -0.7617 0.4757, -0.09890, -0.4950 0.5137, -0.09070, -0.3500 0.5694, -0.07640, -0.3047 14 Flap element taps 1.0000, 0.00130, -0.2199 0.9365, 0.01390, -0.0822 0.8333, 0.03280, -0.0241 0.7436, 0.04930, 0.0077 0.7049, 0.05670, 0.0465 0.6662, 0.06410, 0.0901 0.6522, 0.01390, -0.2474 0.5969, -0.00020, -0.2644 0.6000, -0.03020, -0.3022 0.6324, -0.04540, -0.2933 0.6667, -0.04880, -0.2897 0.7046, -0.04110, -0.2975 0.7429, -0.03210, -0.3055 0.9311, -0.00120, -0.3193 --------- Run Conditions: vel=205.9 ft/s Re=2.005x10^6 AOA=-0.01 Flap deflection=-5.00 Totals: Cl=-0.2506 Cdp=0.0082 Cm(c/4)=0.0281 Cs=-0.0081 Ch=0.0310 Main component: Cl=-0.2179 Cdp=0.0113 Cm=0.0646 Flap component: Cl=-0.0327 Cdp=-0.0031 Cm=0.0261 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1897 0.6175, -0.04610, -0.1120 0.5841, -0.02440, -0.0982 0.5775, 0.01750, -0.0985 0.5777, 0.04660, -0.0990 0.6274, 0.07170, -0.0018 0.5694, 0.08320, -0.1688 0.5112, 0.09370, -0.4119 0.4731, 0.09830, -0.5008 0.4349, 0.10070, -0.5222 0.3960, 0.10120, -0.4872 0.3566, 0.10020, -0.4589 0.3172, 0.09790, -0.4179 0.2778, 0.09440, -0.3985 0.2393, 0.08960, -0.3769 0.2056, 0.08360, -0.3407 0.1633, 0.07610, -0.2741 0.1261, 0.06710, -0.1822 0.0900, 0.05640, -0.2105 0.0571, 0.04390, 0.0810 0.0283, 0.02940, 0.3432 0.0142, 0.01970, 0.5942 0.0081, 0.01410, 0.7736 0.0026, 0.00780, 0.9088 0.0000, 0.00000, -0.0666 0.0037, -0.00840, 0.2707 0.0112, -0.01420, 0.0751 0.0191, -0.01930, -0.0545 0.0397, -0.03030, -0.1244 0.0706, -0.04420, -0.2719 0.1037, -0.05710, -0.3358 0.1384, -0.06890, -0.5015 0.1741, -0.07950, -0.6002 0.2102, -0.08660, -0.7167 0.2472, -0.09640, -0.8453 0.2844, -0.10270, -0.9212 0.3225, -0.10690, -0.9800 0.3608, -0.10890, -1.0203 0.3991, -0.10830, -1.0030 0.4373, -0.10510, -0.9312 0.4757, -0.09890, -0.7537 0.5137, -0.09070, -0.6060 0.5694, -0.07640, -0.3479 14 Flap element taps 1.0000, 0.00130, 0.0360 0.9365, 0.01390, 0.0429 0.8333, 0.03280, 0.0206 0.7436, 0.04930, 0.0072 0.7049, 0.05670, 0.0243 0.6662, 0.06410, 0.0426 0.6522, 0.01390, -0.0946 0.5969, -0.00020, -0.0988 0.6000, -0.03020, -0.1201 0.6324, -0.04540, -0.1140 0.6667, -0.04880, -0.1155 0.7046, -0.04110, -0.0986 0.7429, -0.03210, -0.0905 0.9311, -0.00120, -0.0474 Wake drag found for this condition, Cdw=0.0219 --------- Run Conditions: vel=205.9 ft/s Re=1.998x10^6 AOA=3.02 Flap deflection=-5.00 Totals: Cl=0.0055 Cdp=0.0042 Cm(c/4)=0.0285 Cs=-0.0039 Ch=0.0130 Main component: Cl=0.0194 Cdp=0.0179 Cm=0.0162 Flap component: Cl=-0.0139 Cdp=-0.0137 Cm=0.0109 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2179 0.6175, -0.04610, -0.1423 0.5841, -0.02440, -0.1293 0.5775, 0.01750, -0.1300 0.5777, 0.04660, -0.1307 0.6274, 0.07170, -0.0465 0.5694, 0.08320, -0.2183 0.5112, 0.09370, -0.4846 0.4731, 0.09830, -0.5954 0.4349, 0.10070, -0.6375 0.3960, 0.10120, -0.6196 0.3566, 0.10020, -0.6083 0.3172, 0.09790, -0.5840 0.2778, 0.09440, -0.5856 0.2393, 0.08960, -0.5877 0.2056, 0.08360, -0.5775 0.1633, 0.07610, -0.5386 0.1261, 0.06710, -0.4801 0.0900, 0.05640, -0.5801 0.0571, 0.04390, -0.3261 0.0283, 0.02940, -0.1347 0.0142, 0.01970, 0.0860 0.0081, 0.01410, 0.2489 0.0026, 0.00780, 0.4007 0.0000, 0.00000, -0.0522 0.0037, -0.00840, 0.8532 0.0112, -0.01420, 0.6192 0.0191, -0.01930, 0.4562 0.0397, -0.03030, 0.2792 0.0706, -0.04420, 0.0820 0.1037, -0.05710, -0.0298 0.1384, -0.06890, -0.2179 0.1741, -0.07950, -0.3403 0.2102, -0.08660, -0.4749 0.2472, -0.09640, -0.6199 0.2844, -0.10270, -0.7174 0.3225, -0.10690, -0.7998 0.3608, -0.10890, -0.8654 0.3991, -0.10830, -0.8760 0.4373, -0.10510, -0.8395 0.4757, -0.09890, -0.6968 0.5137, -0.09070, -0.5824 0.5694, -0.07640, -0.3566 14 Flap element taps 1.0000, 0.00130, 0.1466 0.9365, 0.01390, 0.0970 0.8333, 0.03280, 0.0335 0.7436, 0.04930, -0.0041 0.7049, 0.05670, -0.0011 0.6662, 0.06410, 0.0011 0.6522, 0.01390, -0.1265 0.5969, -0.00020, -0.1309 0.6000, -0.03020, -0.1493 0.6324, -0.04540, -0.1433 0.6667, -0.04880, -0.1444 0.7046, -0.04110, -0.0889 0.7429, -0.03210, -0.0521 0.9311, -0.00120, 0.0879 Wake drag found for this condition, Cdw=0.0148 --------- Run Conditions: vel=207.1 ft/s Re=2.007x10^6 AOA=6.01 Flap deflection=-5.00 Totals: Cl=0.3003 Cdp=0.0132 Cm(c/4)=0.0210 Cs=0.0183 Ch=-0.0133 Main component: Cl=0.2855 Cdp=0.0339 Cm=-0.0424 Flap component: Cl=0.0148 Cdp=-0.0207 Cm=-0.0116 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2098 0.6175, -0.04610, -0.1697 0.5841, -0.02440, -0.1614 0.5775, 0.01750, -0.1612 0.5777, 0.04660, -0.1623 0.6274, 0.07170, -0.1173 0.5694, 0.08320, -0.2793 0.5112, 0.09370, -0.5612 0.4731, 0.09830, -0.6957 0.4349, 0.10070, -0.7624 0.3960, 0.10120, -0.7651 0.3566, 0.10020, -0.7722 0.3172, 0.09790, -0.7685 0.2778, 0.09440, -0.7928 0.2393, 0.08960, -0.8219 0.2056, 0.08360, -0.8433 0.1633, 0.07610, -0.8402 0.1261, 0.06710, -0.8238 0.0900, 0.05640, -1.0055 0.0571, 0.04390, -0.8281 0.0283, 0.02940, -0.7658 0.0142, 0.01970, -0.6674 0.0081, 0.01410, -0.5922 0.0026, 0.00780, -0.2610 0.0000, 0.00000, -0.0333 0.0037, -0.00840, 1.0068 0.0112, -0.01420, 0.9374 0.0191, -0.01930, 0.8159 0.0397, -0.03030, 0.6129 0.0706, -0.04420, 0.3965 0.1037, -0.05710, 0.2548 0.1384, -0.06890, 0.0608 0.1741, -0.07950, -0.0769 0.2102, -0.08660, -0.2228 0.2472, -0.09640, -0.3764 0.2844, -0.10270, -0.4888 0.3225, -0.10690, -0.5881 0.3608, -0.10890, -0.6717 0.3991, -0.10830, -0.7052 0.4373, -0.10510, -0.6973 0.4757, -0.09890, -0.5881 0.5137, -0.09070, -0.5021 0.5694, -0.07640, -0.3128 14 Flap element taps 1.0000, 0.00130, 0.1726 0.9365, 0.01390, 0.1108 0.8333, 0.03280, 0.0245 0.7436, 0.04930, -0.0354 0.7049, 0.05670, -0.0474 0.6662, 0.06410, -0.0652 0.6522, 0.01390, -0.1594 0.5969, -0.00020, -0.1620 0.6000, -0.03020, -0.1731 0.6324, -0.04540, -0.1697 0.6667, -0.04880, -0.1580 0.7046, -0.04110, -0.0663 0.7429, -0.03210, 0.0080 0.9311, -0.00120, 0.2029 Wake drag found for this condition, Cdw=0.0135 --------- Run Conditions: vel=207.1 ft/s Re=2.004x10^6 AOA=9.01 Flap deflection=-5.00 Totals: Cl=0.5889 Cdp=0.0342 Cm(c/4)=0.0131 Cs=0.0585 Ch=-0.0370 Main component: Cl=0.5420 Cdp=0.0555 Cm=-0.0981 Flap component: Cl=0.0469 Cdp=-0.0213 Cm=-0.0356 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1771 0.6175, -0.04610, -0.1839 0.5841, -0.02440, -0.1820 0.5775, 0.01750, -0.1839 0.5777, 0.04660, -0.1849 0.6274, 0.07170, -0.1963 0.5694, 0.08320, -0.3211 0.5112, 0.09370, -0.5972 0.4731, 0.09830, -0.7594 0.4349, 0.10070, -0.8557 0.3960, 0.10120, -0.8852 0.3566, 0.10020, -0.9172 0.3172, 0.09790, -0.9376 0.2778, 0.09440, -0.9894 0.2393, 0.08960, -1.0486 0.2056, 0.08360, -1.1052 0.1633, 0.07610, -1.1475 0.1261, 0.06710, -1.1817 0.0900, 0.05640, -1.4438 0.0571, 0.04390, -1.3876 0.0283, 0.02940, -1.5142 0.0142, 0.01970, -1.6353 0.0081, 0.01410, -1.7076 0.0026, 0.00780, -1.3849 0.0000, 0.00000, -0.0127 0.0037, -0.00840, 0.7847 0.0112, -0.01420, 1.0079 0.0191, -0.01930, 0.9903 0.0397, -0.03030, 0.8449 0.0706, -0.04420, 0.6448 0.1037, -0.05710, 0.4904 0.1384, -0.06890, 0.3029 0.1741, -0.07950, 0.1592 0.2102, -0.08660, 0.0105 0.2472, -0.09640, -0.1453 0.2844, -0.10270, -0.2673 0.3225, -0.10690, -0.3794 0.3608, -0.10890, -0.4758 0.3991, -0.10830, -0.5290 0.4373, -0.10510, -0.5440 0.4757, -0.09890, -0.4636 0.5137, -0.09070, -0.4025 0.5694, -0.07640, -0.2446 14 Flap element taps 1.0000, 0.00130, 0.1322 0.9365, 0.01390, 0.0849 0.8333, 0.03280, -0.0052 0.7436, 0.04930, -0.0841 0.7049, 0.05670, -0.1145 0.6662, 0.06410, -0.1511 0.6522, 0.01390, -0.1804 0.5969, -0.00020, -0.1812 0.6000, -0.03020, -0.1835 0.6324, -0.04540, -0.1829 0.6667, -0.04880, -0.0788 0.7046, -0.04110, -0.0056 0.7429, -0.03210, 0.0737 0.9311, -0.00120, 0.2394 --------- Run Conditions: vel=206.4 ft/s Re=1.994x10^6 AOA=12.02 Flap deflection=-5.00 Totals: Cl=0.7632 Cdp=0.0702 Cm(c/4)=-0.0003 Cs=0.0903 Ch=-0.0868 Main component: Cl=0.6659 Cdp=0.0780 Cm=-0.1140 Flap component: Cl=0.0973 Cdp=-0.0078 Cm=-0.0765 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1771 0.6175, -0.04610, -0.2305 0.5841, -0.02440, -0.2295 0.5775, 0.01750, -0.2312 0.5777, 0.04660, -0.2317 0.6274, 0.07170, -0.2757 0.5694, 0.08320, -0.2989 0.5112, 0.09370, -0.4212 0.4731, 0.09830, -0.5910 0.4349, 0.10070, -0.7386 0.3960, 0.10120, -0.8215 0.3566, 0.10020, -0.8990 0.3172, 0.09790, -0.9571 0.2778, 0.09440, -1.0449 0.2393, 0.08960, -1.1386 0.2056, 0.08360, -1.2344 0.1633, 0.07610, -1.3248 0.1261, 0.06710, -1.4131 0.0900, 0.05640, -1.7379 0.0571, 0.04390, -1.8183 0.0283, 0.02940, -2.1498 0.0142, 0.01970, -2.5014 0.0081, 0.01410, -2.7775 0.0026, 0.00780, -2.5382 0.0000, 0.00000, -0.0063 0.0037, -0.00840, 0.3345 0.0112, -0.01420, 0.9169 0.0191, -0.01930, 1.0066 0.0397, -0.03030, 0.9562 0.0706, -0.04420, 0.7935 0.1037, -0.05710, 0.6429 0.1384, -0.06890, 0.4668 0.1741, -0.07950, 0.3169 0.2102, -0.08660, 0.1631 0.2472, -0.09640, 0.0056 0.2844, -0.10270, -0.1175 0.3225, -0.10690, -0.2384 0.3608, -0.10890, -0.3463 0.3991, -0.10830, -0.4157 0.4373, -0.10510, -0.4502 0.4757, -0.09890, -0.3925 0.5137, -0.09070, -0.3521 0.5694, -0.07640, -0.2185 14 Flap element taps 1.0000, 0.00130, -0.0546 0.9365, 0.01390, -0.1291 0.8333, 0.03280, -0.1903 0.7436, 0.04930, -0.2325 0.7049, 0.05670, -0.2456 0.6662, 0.06410, -0.2647 0.6522, 0.01390, -0.2278 0.5969, -0.00020, -0.2287 0.6000, -0.03020, -0.2306 0.6324, -0.04540, -0.2306 0.6667, -0.04880, 0.0227 0.7046, -0.04110, 0.0021 0.7429, -0.03210, 0.0745 0.9311, -0.00120, 0.1854 --------- Run Conditions: vel=208.6 ft/s Re=2.007x10^6 AOA=15.00 Flap deflection=-5.00 Totals: Cl=0.8052 Cdp=0.1059 Cm(c/4)=-0.0052 Cs=0.1061 Ch=-0.1230 Main component: Cl=0.6762 Cdp=0.0966 Cm=-0.1025 Flap component: Cl=0.1290 Cdp=0.0093 Cm=-0.1040 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1902 0.6175, -0.04610, -0.2748 0.5841, -0.02440, -0.2752 0.5775, 0.01750, -0.2784 0.5777, 0.04660, -0.2794 0.6274, 0.07170, -0.3375 0.5694, 0.08320, -0.3367 0.5112, 0.09370, -0.3356 0.4731, 0.09830, -0.3573 0.4349, 0.10070, -0.4152 0.3960, 0.10120, -0.5047 0.3566, 0.10020, -0.6246 0.3172, 0.09790, -0.7494 0.2778, 0.09440, -0.8933 0.2393, 0.08960, -1.0413 0.2056, 0.08360, -1.1862 0.1633, 0.07610, -1.3362 0.1261, 0.06710, -1.4869 0.0900, 0.05640, -1.8545 0.0571, 0.04390, -2.0693 0.0283, 0.02940, -2.5828 0.0142, 0.01970, -3.1447 0.0081, 0.01410, -3.6102 0.0026, 0.00780, -3.5706 0.0000, 0.00000, -0.1709 0.0037, -0.00840, -0.1495 0.0112, -0.01420, 0.7620 0.0191, -0.01930, 0.9636 0.0397, -0.03030, 1.0019 0.0706, -0.04420, 0.8809 0.1037, -0.05710, 0.7434 0.1384, -0.06890, 0.5788 0.1741, -0.07950, 0.4314 0.2102, -0.08660, 0.2771 0.2472, -0.09640, 0.1122 0.2844, -0.10270, -0.0222 0.3225, -0.10690, -0.1506 0.3608, -0.10890, -0.2676 0.3991, -0.10830, -0.3574 0.4373, -0.10510, -0.4012 0.4757, -0.09890, -0.3616 0.5137, -0.09070, -0.3261 0.5694, -0.07640, -0.2080 14 Flap element taps 1.0000, 0.00130, -0.2570 0.9365, 0.01390, -0.3491 0.8333, 0.03280, -0.3494 0.7436, 0.04930, -0.3495 0.7049, 0.05670, -0.3468 0.6662, 0.06410, -0.3519 0.6522, 0.01390, -0.2733 0.5969, -0.00020, -0.2744 0.6000, -0.03020, -0.2753 0.6324, -0.04540, -0.2776 0.6667, -0.04880, 0.0705 0.7046, -0.04110, -0.0246 0.7429, -0.03210, 0.0432 0.9311, -0.00120, 0.0968 --------- Run Conditions: vel=208.7 ft/s Re=2.005x10^6 AOA=18.00 Flap deflection=-5.00 Totals: Cl=0.6048 Cdp=0.1905 Cm(c/4)=-0.0503 Cs=0.0057 Ch=-0.1512 Main component: Cl=0.4415 Cdp=0.1656 Cm=-0.0767 Flap component: Cl=0.1633 Cdp=0.0249 Cm=-0.1321 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2807 0.6175, -0.04610, -0.3931 0.5841, -0.02440, -0.3922 0.5775, 0.01750, -0.3936 0.5777, 0.04660, -0.3933 0.6274, 0.07170, -0.5211 0.5694, 0.08320, -0.5260 0.5112, 0.09370, -0.5245 0.4731, 0.09830, -0.5210 0.4349, 0.10070, -0.5212 0.3960, 0.10120, -0.5173 0.3566, 0.10020, -0.5251 0.3172, 0.09790, -0.5331 0.2778, 0.09440, -0.5510 0.2393, 0.08960, -0.5742 0.2056, 0.08360, -0.6058 0.1633, 0.07610, -0.6550 0.1261, 0.06710, -0.7244 0.0900, 0.05640, -0.8528 0.0571, 0.04390, -1.1015 0.0283, 0.02940, -1.6439 0.0142, 0.01970, -2.2189 0.0081, 0.01410, -2.6545 0.0026, 0.00780, -2.7163 0.0000, 0.00000, -0.1598 0.0037, -0.00840, 0.0484 0.0112, -0.01420, 0.8104 0.0191, -0.01930, 0.9771 0.0397, -0.03030, 0.9984 0.0706, -0.04420, 0.8779 0.1037, -0.05710, 0.7428 0.1384, -0.06890, 0.5777 0.1741, -0.07950, 0.4296 0.2102, -0.08660, 0.2728 0.2472, -0.09640, 0.1023 0.2844, -0.10270, -0.0381 0.3225, -0.10690, -0.1761 0.3608, -0.10890, -0.3041 0.3991, -0.10830, -0.4067 0.4373, -0.10510, -0.4582 0.4757, -0.09890, -0.4258 0.5137, -0.09070, -0.3969 0.5694, -0.07640, -0.2851 14 Flap element taps 1.0000, 0.00130, -0.4155 0.9365, 0.01390, -0.5047 0.8333, 0.03280, -0.5636 0.7436, 0.04930, -0.5628 0.7049, 0.05670, -0.5547 0.6662, 0.06410, -0.5663 0.6522, 0.01390, -0.3923 0.5969, -0.00020, -0.3940 0.6000, -0.03020, -0.3942 0.6324, -0.04540, -0.3989 0.6667, -0.04880, 0.0910 0.7046, -0.04110, -0.1063 0.7429, -0.03210, -0.0385 0.9311, -0.00120, -0.0122 --------- Run Conditions: vel=208.6 ft/s Re=2.003x10^6 AOA=19.99 Flap deflection=-5.00 Totals: Cl=0.6124 Cdp=0.2460 Cm(c/4)=-0.0674 Cs=-0.0218 Ch=-0.1634 Main component: Cl=0.4369 Cdp=0.2111 Cm=-0.0892 Flap component: Cl=0.1754 Cdp=0.0349 Cm=-0.1430 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3083 0.6175, -0.04610, -0.4335 0.5841, -0.02440, -0.4319 0.5775, 0.01750, -0.4337 0.5777, 0.04660, -0.4329 0.6274, 0.07170, -0.6059 0.5694, 0.08320, -0.6065 0.5112, 0.09370, -0.6048 0.4731, 0.09830, -0.6162 0.4349, 0.10070, -0.6117 0.3960, 0.10120, -0.6031 0.3566, 0.10020, -0.6114 0.3172, 0.09790, -0.6176 0.2778, 0.09440, -0.6314 0.2393, 0.08960, -0.6500 0.2056, 0.08360, -0.6700 0.1633, 0.07610, -0.7020 0.1261, 0.06710, -0.7350 0.0900, 0.05640, -0.7784 0.0571, 0.04390, -0.8975 0.0283, 0.02940, -1.2251 0.0142, 0.01970, -1.7056 0.0081, 0.01410, -2.0889 0.0026, 0.00780, -2.2428 0.0000, 0.00000, -0.1450 0.0037, -0.00840, 0.0897 0.0112, -0.01420, 0.8104 0.0191, -0.01930, 0.9750 0.0397, -0.03030, 1.0017 0.0706, -0.04420, 0.8901 0.1037, -0.05710, 0.7595 0.1384, -0.06890, 0.5975 0.1741, -0.07950, 0.4502 0.2102, -0.08660, 0.2949 0.2472, -0.09640, 0.1228 0.2844, -0.10270, -0.0203 0.3225, -0.10690, -0.1645 0.3608, -0.10890, -0.2971 0.3991, -0.10830, -0.4074 0.4373, -0.10510, -0.4650 0.4757, -0.09890, -0.4366 0.5137, -0.09070, -0.4132 0.5694, -0.07640, -0.3037 14 Flap element taps 1.0000, 0.00130, -0.4829 0.9365, 0.01390, -0.5798 0.8333, 0.03280, -0.6347 0.7436, 0.04930, -0.6333 0.7049, 0.05670, -0.6217 0.6662, 0.06410, -0.6372 0.6522, 0.01390, -0.4307 0.5969, -0.00020, -0.4339 0.6000, -0.03020, -0.4333 0.6324, -0.04540, -0.4389 0.6667, -0.04880, 0.1057 0.7046, -0.04110, -0.1331 0.7429, -0.03210, -0.0652 0.9311, -0.00120, -0.0510 --------- Run Conditions: vel=207.1 ft/s Re=1.984x10^6 AOA=24.00 Flap deflection=-5.00 Totals: Cl=0.8665 Cdp=0.3914 Cm(c/4)=-0.1003 Cs=-0.0052 Ch=-0.2005 Main component: Cl=0.6539 Cdp=0.3261 Cm=-0.1604 Flap component: Cl=0.2126 Cdp=0.0653 Cm=-0.1776 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2909 0.6175, -0.04610, -0.4458 0.5841, -0.02440, -0.4449 0.5775, 0.01750, -0.4504 0.5777, 0.04660, -0.4464 0.6274, 0.07170, -0.7954 0.5694, 0.08320, -0.8147 0.5112, 0.09370, -0.8512 0.4731, 0.09830, -0.8706 0.4349, 0.10070, -0.8829 0.3960, 0.10120, -0.8963 0.3566, 0.10020, -0.9303 0.3172, 0.09790, -0.9806 0.2778, 0.09440, -1.0337 0.2393, 0.08960, -1.0886 0.2056, 0.08360, -1.1369 0.1633, 0.07610, -1.1972 0.1261, 0.06710, -1.2464 0.0900, 0.05640, -1.2856 0.0571, 0.04390, -1.3831 0.0283, 0.02940, -1.4744 0.0142, 0.01970, -1.6474 0.0081, 0.01410, -1.8430 0.0026, 0.00780, -1.9130 0.0000, 0.00000, -0.1477 0.0037, -0.00840, -0.2043 0.0112, -0.01420, 0.6665 0.0191, -0.01930, 0.9049 0.0397, -0.03030, 1.0117 0.0706, -0.04420, 0.9505 0.1037, -0.05710, 0.8427 0.1384, -0.06890, 0.6990 0.1741, -0.07950, 0.5605 0.2102, -0.08660, 0.4123 0.2472, -0.09640, 0.2436 0.2844, -0.10270, 0.0970 0.3225, -0.10690, -0.0601 0.3608, -0.10890, -0.2018 0.3991, -0.10830, -0.3205 0.4373, -0.10510, -0.3907 0.4757, -0.09890, -0.3804 0.5137, -0.09070, -0.3776 0.5694, -0.07640, -0.2761 14 Flap element taps 1.0000, 0.00130, -0.6422 0.9365, 0.01390, -0.7223 0.8333, 0.03280, -0.7665 0.7436, 0.04930, -0.7886 0.7049, 0.05670, -0.7992 0.6662, 0.06410, -0.8117 0.6522, 0.01390, -0.4442 0.5969, -0.00020, -0.4515 0.6000, -0.03020, -0.4488 0.6324, -0.04540, -0.4663 0.6667, -0.04880, 0.2189 0.7046, -0.04110, -0.1263 0.7429, -0.03210, -0.0660 0.9311, -0.00120, -0.0963 --------- Run Conditions: vel=209.0 ft/s Re=2.000x10^6 AOA=26.99 Flap deflection=-5.00 Totals: Cl=0.7234 Cdp=0.4316 Cm(c/4)=-0.1082 Cs=-0.0563 Ch=-0.1958 Main component: Cl=0.5186 Cdp=0.3557 Cm=-0.1440 Flap component: Cl=0.2049 Cdp=0.0759 Cm=-0.1744 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3005 0.6175, -0.04610, -0.4632 0.5841, -0.02440, -0.4646 0.5775, 0.01750, -0.4648 0.5777, 0.04660, -0.4626 0.6274, 0.07170, -0.7848 0.5694, 0.08320, -0.8069 0.5112, 0.09370, -0.8151 0.4731, 0.09830, -0.8224 0.4349, 0.10070, -0.8271 0.3960, 0.10120, -0.8210 0.3566, 0.10020, -0.8390 0.3172, 0.09790, -0.8410 0.2778, 0.09440, -0.8487 0.2393, 0.08960, -0.8580 0.2056, 0.08360, -0.8617 0.1633, 0.07610, -0.8850 0.1261, 0.06710, -0.8983 0.0900, 0.05640, -0.8959 0.0571, 0.04390, -0.9066 0.0283, 0.02940, -0.9234 0.0142, 0.01970, -0.9918 0.0081, 0.01410, -1.0495 0.0026, 0.00780, -0.9568 0.0000, 0.00000, -0.1319 0.0037, -0.00840, 0.0454 0.0112, -0.01420, 0.7192 0.0191, -0.01930, 0.9163 0.0397, -0.03030, 1.0103 0.0706, -0.04420, 0.9592 0.1037, -0.05710, 0.8621 0.1384, -0.06890, 0.7272 0.1741, -0.07950, 0.5965 0.2102, -0.08660, 0.4553 0.2472, -0.09640, 0.2899 0.2844, -0.10270, 0.1450 0.3225, -0.10690, -0.0139 0.3608, -0.10890, -0.1585 0.3991, -0.10830, -0.2827 0.4373, -0.10510, -0.3596 0.4757, -0.09890, -0.3585 0.5137, -0.09070, -0.3634 0.5694, -0.07640, -0.2769 14 Flap element taps 1.0000, 0.00130, -0.7072 0.9365, 0.01390, -0.7500 0.8333, 0.03280, -0.7825 0.7436, 0.04930, -0.7895 0.7049, 0.05670, -0.7933 0.6662, 0.06410, -0.8045 0.6522, 0.01390, -0.4621 0.5969, -0.00020, -0.4679 0.6000, -0.03020, -0.4664 0.6324, -0.04540, -0.4783 0.6667, -0.04880, 0.2535 0.7046, -0.04110, -0.1437 0.7429, -0.03210, -0.0875 0.9311, -0.00120, -0.1401