S809 UNVENTED AILERON, CLEAN, CHORD = 18 IN --------- Run Conditions: vel=102.5 ft/s Re=1.011x10^6 AOA=-6.01 Flap deflection=5.00 Totals: Cl=-0.2632 Cdp=0.0053 Cm(c/4)=-0.0657 Cs=0.0223 Ch=-0.0707 Main component: Cl=-0.3463 Cdp=0.0257 Cm=0.0672 Flap component: Cl=0.0831 Cdp=-0.0204 Cm=-0.0673 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.0857 0.6175, -0.04610, -0.0283 0.5841, -0.02440, -0.0283 0.5775, 0.01750, -0.0338 0.5777, 0.04660, -0.0351 0.6274, 0.07170, -0.2128 0.5694, 0.08320, -0.4563 0.5112, 0.09370, -0.5315 0.4731, 0.09830, -0.6023 0.4349, 0.10070, -0.5894 0.3960, 0.10120, -0.5136 0.3566, 0.10020, -0.4411 0.3172, 0.09790, -0.3660 0.2778, 0.09440, -0.3243 0.2393, 0.08960, -0.2597 0.2056, 0.08360, -0.1929 0.1633, 0.07610, -0.0840 0.1261, 0.06710, 0.0412 0.0900, 0.05640, 0.2028 0.0571, 0.04390, 0.4095 0.0283, 0.02940, 0.6967 0.0142, 0.01970, 0.9152 0.0081, 0.01410, 0.9864 0.0026, 0.00780, 0.8839 0.0000, 0.00000, 0.1140 0.0037, -0.00840, -0.8725 0.0112, -0.01420, -0.8133 0.0191, -0.01930, -0.7148 0.0397, -0.03030, -0.6156 0.0706, -0.04420, -0.6394 0.1037, -0.05710, -0.7097 0.1384, -0.06890, -0.7662 0.1741, -0.07950, -0.8337 0.2102, -0.08660, -0.9176 0.2472, -0.09640, -1.0118 0.2844, -0.10270, -1.0466 0.3225, -0.10690, -1.0668 0.3608, -0.10890, -1.0753 0.3991, -0.10830, -1.0045 0.4373, -0.10510, -0.9427 0.4757, -0.09890, -0.9155 0.5137, -0.09070, -0.4314 0.5694, -0.07640, -0.2354 15 Flap element taps 1.0000, 0.00130, 0.1876 0.9365, 0.01390, 0.1008 0.8333, 0.03280, -0.0233 0.7436, 0.04930, -0.1329 0.7049, 0.05670, -0.1743 0.6662, 0.06410, -0.3067 0.6522, 0.01390, -0.0304 0.5969, -0.00020, -0.0287 0.6000, -0.03020, -0.0262 0.6324, -0.04540, -0.0228 0.6667, -0.04880, -0.0796 0.7046, -0.04110, 0.2047 0.7429, -0.03210, 0.1951 0.8333, -0.01400, 0.2460 0.9311, -0.00120, 0.2946 Wake drag found for this condition, Cdw=0.0110 --------- Run Conditions: vel=102.8 ft/s Re=1.012x10^6 AOA=0.00 Flap deflection=5.00 Totals: Cl=0.4100 Cdp=0.0033 Cm(c/4)=-0.0793 Cs=-0.0033 Ch=-0.1063 Main component: Cl=0.2756 Cdp=0.0070 Cm=-0.0769 Flap component: Cl=0.1343 Cdp=-0.0038 Cm=-0.1048 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0218 0.6175, -0.04610, 0.0653 0.5841, -0.02440, 0.0462 0.5775, 0.01750, 0.0441 0.5777, 0.04660, 0.0515 0.6274, 0.07170, -0.3855 0.5694, 0.08320, -0.8075 0.5112, 0.09370, -0.8234 0.4731, 0.09830, -0.9038 0.4349, 0.10070, -0.9390 0.3960, 0.10120, -0.9125 0.3566, 0.10020, -0.8491 0.3172, 0.09790, -0.8057 0.2778, 0.09440, -0.8036 0.2393, 0.08960, -0.7824 0.2056, 0.08360, -0.7805 0.1633, 0.07610, -0.7047 0.1261, 0.06710, -0.6510 0.0900, 0.05640, -0.5685 0.0571, 0.04390, -0.4737 0.0283, 0.02940, -0.3079 0.0142, 0.01970, -0.1010 0.0081, 0.01410, 0.0474 0.0026, 0.00780, 0.3496 0.0000, 0.00000, 0.8945 0.0037, -0.00840, 0.9321 0.0112, -0.01420, 0.7115 0.0191, -0.01930, 0.5871 0.0397, -0.03030, 0.3936 0.0706, -0.04420, 0.1843 0.1037, -0.05710, 0.0236 0.1384, -0.06890, -0.0820 0.1741, -0.07950, -0.2026 0.2102, -0.08660, -0.3422 0.2472, -0.09640, -0.4611 0.2844, -0.10270, -0.5417 0.3225, -0.10690, -0.5895 0.3608, -0.10890, -0.6510 0.3991, -0.10830, -0.6240 0.4373, -0.10510, -0.5785 0.4757, -0.09890, -0.5147 0.5137, -0.09070, -0.5003 0.5694, -0.07640, -0.0765 15 Flap element taps 1.0000, 0.00130, 0.1814 0.9365, 0.01390, 0.0757 0.8333, 0.03280, -0.0898 0.7436, 0.04930, -0.2383 0.7049, 0.05670, -0.3033 0.6662, 0.06410, -0.4589 0.6522, 0.01390, 0.0405 0.5969, -0.00020, 0.0438 0.6000, -0.03020, 0.0499 0.6324, -0.04540, 0.0613 0.6667, -0.04880, 0.1731 0.7046, -0.04110, 0.2975 0.7429, -0.03210, 0.2715 0.8333, -0.01400, 0.3017 0.9311, -0.00120, 0.3322 Wake drag found for this condition, Cdw=0.0117 --------- Run Conditions: vel=102.2 ft/s Re=1.006x10^6 AOA=3.03 Flap deflection=5.00 Totals: Cl=0.7379 Cdp=0.0008 Cm(c/4)=-0.0822 Cs=0.0382 Ch=-0.1223 Main component: Cl=0.5786 Cdp=-0.0068 Cm=-0.1428 Flap component: Cl=0.1593 Cdp=0.0075 Cm=-0.1236 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0881 0.6175, -0.04610, 0.1060 0.5841, -0.02440, 0.0794 0.5775, 0.01750, 0.0719 0.5777, 0.04660, 0.0836 0.6274, 0.07170, -0.4756 0.5694, 0.08320, -0.6142 0.5112, 0.09370, -0.9984 0.4731, 0.09830, -1.0575 0.4349, 0.10070, -1.1163 0.3960, 0.10120, -1.1171 0.3566, 0.10020, -1.0651 0.3172, 0.09790, -1.0431 0.2778, 0.09440, -1.0635 0.2393, 0.08960, -1.0713 0.2056, 0.08360, -1.1073 0.1633, 0.07610, -1.0620 0.1261, 0.06710, -1.0606 0.0900, 0.05640, -1.0441 0.0571, 0.04390, -1.0602 0.0283, 0.02940, -1.0606 0.0142, 0.01970, -1.0196 0.0081, 0.01410, -1.0129 0.0026, 0.00780, -0.6907 0.0000, 0.00000, -0.1174 0.0037, -0.00840, 0.9878 0.0112, -0.01420, 0.9918 0.0191, -0.01930, 0.9137 0.0397, -0.03030, 0.7227 0.0706, -0.04420, 0.4970 0.1037, -0.05710, 0.3228 0.1384, -0.06890, 0.2076 0.1741, -0.07950, 0.0735 0.2102, -0.08660, -0.0843 0.2472, -0.09640, -0.2073 0.2844, -0.10270, -0.3064 0.3225, -0.10690, -0.3617 0.3608, -0.10890, -0.4449 0.3991, -0.10830, -0.4376 0.4373, -0.10510, -0.4156 0.4757, -0.09890, -0.3410 0.5137, -0.09070, -0.3431 0.5694, -0.07640, 0.0192 15 Flap element taps 1.0000, 0.00130, 0.1793 0.9365, 0.01390, 0.0709 0.8333, 0.03280, -0.1159 0.7436, 0.04930, -0.2849 0.7049, 0.05670, -0.3617 0.6662, 0.06410, -0.5266 0.6522, 0.01390, 0.0690 0.5969, -0.00020, 0.0729 0.6000, -0.03020, 0.0809 0.6324, -0.04540, 0.0926 0.6667, -0.04880, 0.3556 0.7046, -0.04110, 0.3448 0.7429, -0.03210, 0.3125 0.8333, -0.01400, 0.3310 0.9311, -0.00120, 0.3534 Wake drag found for this condition, Cdw=0.0117 --------- Run Conditions: vel=102.4 ft/s Re=1.007x10^6 AOA=6.03 Flap deflection=5.00 Totals: Cl=0.9368 Cdp=0.0117 Cm(c/4)=-0.0731 Cs=0.0868 Ch=-0.1222 Main component: Cl=0.7786 Cdp=-0.0066 Cm=-0.1830 Flap component: Cl=0.1582 Cdp=0.0183 Cm=-0.1233 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.1078 0.6175, -0.04610, 0.1150 0.5841, -0.02440, 0.0879 0.5775, 0.01750, 0.0831 0.5777, 0.04660, 0.0962 0.6274, 0.07170, -0.5104 0.5694, 0.08320, -0.6699 0.5112, 0.09370, -0.9594 0.4731, 0.09830, -1.1190 0.4349, 0.10070, -1.1777 0.3960, 0.10120, -1.1842 0.3566, 0.10020, -1.1464 0.3172, 0.09790, -1.1432 0.2778, 0.09440, -1.1944 0.2393, 0.08960, -1.2455 0.2056, 0.08360, -1.3206 0.1633, 0.07610, -1.3141 0.1261, 0.06710, -1.3657 0.0900, 0.05640, -1.4197 0.0571, 0.04390, -1.5438 0.0283, 0.02940, -1.7333 0.0142, 0.01970, -1.8924 0.0081, 0.01410, -2.0805 0.0026, 0.00780, -1.8984 0.0000, 0.00000, -1.6026 0.0037, -0.00840, 0.6992 0.0112, -0.01420, 1.0042 0.0191, -0.01930, 1.0136 0.0397, -0.03030, 0.8931 0.0706, -0.04420, 0.6816 0.1037, -0.05710, 0.5118 0.1384, -0.06890, 0.3949 0.1741, -0.07950, 0.2531 0.2102, -0.08660, 0.0880 0.2472, -0.09640, -0.0405 0.2844, -0.10270, -0.1526 0.3225, -0.10690, -0.2187 0.3608, -0.10890, -0.3153 0.3991, -0.10830, -0.3225 0.4373, -0.10510, -0.3269 0.4757, -0.09890, -0.2476 0.5137, -0.09070, -0.2361 0.5694, -0.07640, 0.0723 15 Flap element taps 1.0000, 0.00130, 0.0646 0.9365, 0.01390, 0.0222 0.8333, 0.03280, -0.1097 0.7436, 0.04930, -0.2699 0.7049, 0.05670, -0.3599 0.6662, 0.06410, -0.5152 0.6522, 0.01390, 0.0756 0.5969, -0.00020, 0.0816 0.6000, -0.03020, 0.0890 0.6324, -0.04540, 0.1019 0.6667, -0.04880, 0.3986 0.7046, -0.04110, 0.3522 0.7429, -0.03210, 0.3157 0.8333, -0.01400, 0.3194 0.9311, -0.00120, 0.3197 Wake drag found for this condition, Cdw=0.0241 --------- Run Conditions: vel=102.2 ft/s Re=1.005x10^6 AOA=9.02 Flap deflection=5.00 Totals: Cl=1.0488 Cdp=0.0366 Cm(c/4)=-0.0646 Cs=0.1283 Ch=-0.1537 Main component: Cl=0.8876 Cdp=-0.0052 Cm=-0.1931 Flap component: Cl=0.1613 Cdp=0.0418 Cm=-0.1319 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.1139 0.6175, -0.04610, 0.1210 0.5841, -0.02440, 0.0966 0.5775, 0.01750, 0.0907 0.5777, 0.04660, 0.1011 0.6274, 0.07170, -0.3672 0.5694, 0.08320, -0.5265 0.5112, 0.09370, -0.8226 0.4731, 0.09830, -1.0148 0.4349, 0.10070, -1.1184 0.3960, 0.10120, -1.1672 0.3566, 0.10020, -1.1651 0.3172, 0.09790, -1.1923 0.2778, 0.09440, -1.2602 0.2393, 0.08960, -1.3329 0.2056, 0.08360, -1.4399 0.1633, 0.07610, -1.4695 0.1261, 0.06710, -1.5644 0.0900, 0.05640, -1.6871 0.0571, 0.04390, -1.8994 0.0283, 0.02940, -2.3154 0.0142, 0.01970, -2.7236 0.0081, 0.01410, -3.1361 0.0026, 0.00780, -3.1451 0.0000, 0.00000, -3.2343 0.0037, -0.00840, 0.2354 0.0112, -0.01420, 0.9016 0.0191, -0.01930, 1.0139 0.0397, -0.03030, 0.9813 0.0706, -0.04420, 0.8059 0.1037, -0.05710, 0.6468 0.1384, -0.06890, 0.5308 0.1741, -0.07950, 0.3870 0.2102, -0.08660, 0.2173 0.2472, -0.09640, 0.0830 0.2844, -0.10270, -0.0376 0.3225, -0.10690, -0.1144 0.3608, -0.10890, -0.2238 0.3991, -0.10830, -0.2485 0.4373, -0.10510, -0.2716 0.4757, -0.09890, -0.1977 0.5137, -0.09070, -0.1716 0.5694, -0.07640, 0.0531 15 Flap element taps 1.0000, 0.00130, -0.1521 0.9365, 0.01390, -0.2212 0.8333, 0.03280, -0.2421 0.7436, 0.04930, -0.2525 0.7049, 0.05670, -0.2691 0.6662, 0.06410, -0.3141 0.6522, 0.01390, 0.0869 0.5969, -0.00020, 0.0916 0.6000, -0.03020, 0.0984 0.6324, -0.04540, 0.1081 0.6667, -0.04880, 0.3236 0.7046, -0.04110, 0.3434 0.7429, -0.03210, 0.2955 0.8333, -0.01400, 0.2802 0.9311, -0.00120, 0.2426 --------- Run Conditions: vel=101.8 ft/s Re=1.000x10^6 AOA=12.05 Flap deflection=5.00 Totals: Cl=1.1097 Cdp=0.0646 Cm(c/4)=-0.0601 Cs=0.1684 Ch=-0.1846 Main component: Cl=0.9242 Cdp=-0.0007 Cm=-0.1793 Flap component: Cl=0.1856 Cdp=0.0654 Cm=-0.1555 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.1126 0.6175, -0.04610, 0.1036 0.5841, -0.02440, 0.0754 0.5775, 0.01750, 0.0692 0.5777, 0.04660, 0.0803 0.6274, 0.07170, -0.3773 0.5694, 0.08320, -0.3966 0.5112, 0.09370, -0.5354 0.4731, 0.09830, -0.7274 0.4349, 0.10070, -0.8894 0.3960, 0.10120, -1.0045 0.3566, 0.10020, -1.0519 0.3172, 0.09790, -1.1235 0.2778, 0.09440, -1.2252 0.2393, 0.08960, -1.3315 0.2056, 0.08360, -1.4767 0.1633, 0.07610, -1.5538 0.1261, 0.06710, -1.7026 0.0900, 0.05640, -1.8940 0.0571, 0.04390, -2.2318 0.0283, 0.02940, -2.7559 0.0142, 0.01970, -3.3743 0.0081, 0.01410, -4.3145 0.0026, 0.00780, -4.4660 0.0000, 0.00000, -4.9931 0.0037, -0.00840, -0.3612 0.0112, -0.01420, 0.7049 0.0191, -0.01930, 0.9485 0.0397, -0.03030, 1.0191 0.0706, -0.04420, 0.8913 0.1037, -0.05710, 0.7501 0.1384, -0.06890, 0.6395 0.1741, -0.07950, 0.5017 0.2102, -0.08660, 0.3270 0.2472, -0.09640, 0.1908 0.2844, -0.10270, 0.0627 0.3225, -0.10690, -0.0220 0.3608, -0.10890, -0.1431 0.3991, -0.10830, -0.1817 0.4373, -0.10510, -0.2220 0.4757, -0.09890, -0.1592 0.5137, -0.09070, -0.1347 0.5694, -0.07640, -0.0566 15 Flap element taps 1.0000, 0.00130, -0.3120 0.9365, 0.01390, -0.3850 0.8333, 0.03280, -0.3779 0.7436, 0.04930, -0.3726 0.7049, 0.05670, -0.3760 0.6662, 0.06410, -0.3762 0.6522, 0.01390, 0.0638 0.5969, -0.00020, 0.0683 0.6000, -0.03020, 0.0775 0.6324, -0.04540, 0.0874 0.6667, -0.04880, 0.3529 0.7046, -0.04110, 0.3295 0.7429, -0.03210, 0.2747 0.8333, -0.01400, 0.2435 0.9311, -0.00120, 0.1718 --------- Run Conditions: vel=101.5 ft/s Re=0.997x10^6 AOA=15.01 Flap deflection=5.00 Totals: Cl=1.1173 Cdp=0.0993 Cm(c/4)=-0.0616 Cs=0.1934 Ch=-0.2074 Main component: Cl=0.9125 Cdp=0.0119 Cm=-0.1625 Flap component: Cl=0.2048 Cdp=0.0875 Cm=-0.1753 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.1092 0.6175, -0.04610, 0.0819 0.5841, -0.02440, 0.0527 0.5775, 0.01750, 0.0452 0.5777, 0.04660, 0.0599 0.6274, 0.07170, -0.4586 0.5694, 0.08320, -0.4502 0.5112, 0.09370, -0.4551 0.4731, 0.09830, -0.4759 0.4349, 0.10070, -0.5326 0.3960, 0.10120, -0.6605 0.3566, 0.10020, -0.7600 0.3172, 0.09790, -0.8919 0.2778, 0.09440, -1.0504 0.2393, 0.08960, -1.2028 0.2056, 0.08360, -1.3956 0.1633, 0.07610, -1.5215 0.1261, 0.06710, -1.7246 0.0900, 0.05640, -1.9838 0.0571, 0.04390, -2.4114 0.0283, 0.02940, -3.1042 0.0142, 0.01970, -3.8433 0.0081, 0.01410, -5.0360 0.0026, 0.00780, -5.6173 0.0000, 0.00000, -6.4757 0.0037, -0.00840, -0.9106 0.0112, -0.01420, 0.4952 0.0191, -0.01930, 0.8569 0.0397, -0.03030, 1.0256 0.0706, -0.04420, 0.9445 0.1037, -0.05710, 0.8215 0.1384, -0.06890, 0.7199 0.1741, -0.07950, 0.5837 0.2102, -0.08660, 0.4109 0.2472, -0.09640, 0.2727 0.2844, -0.10270, 0.1397 0.3225, -0.10690, 0.0465 0.3608, -0.10890, -0.0832 0.3991, -0.10830, -0.1317 0.4373, -0.10510, -0.1850 0.4757, -0.09890, -0.1349 0.5137, -0.09070, -0.1173 0.5694, -0.07640, -0.0331 15 Flap element taps 1.0000, 0.00130, -0.4553 0.9365, 0.01390, -0.4888 0.8333, 0.03280, -0.4974 0.7436, 0.04930, -0.4861 0.7049, 0.05670, -0.4820 0.6662, 0.06410, -0.4756 0.6522, 0.01390, 0.0398 0.5969, -0.00020, 0.0445 0.6000, -0.03020, 0.0535 0.6324, -0.04540, 0.0682 0.6667, -0.04880, 0.3747 0.7046, -0.04110, 0.3205 0.7429, -0.03210, 0.2579 0.8333, -0.01400, 0.2104 0.9311, -0.00120, 0.1161 --------- Run Conditions: vel=101.8 ft/s Re=0.999x10^6 AOA=18.02 Flap deflection=5.00 Totals: Cl=0.6676 Cdp=0.2856 Cm(c/4)=-0.1166 Cs=-0.0651 Ch=-0.2222 Main component: Cl=0.4487 Cdp=0.1807 Cm=-0.1066 Flap component: Cl=0.2190 Cdp=0.1049 Cm=-0.1908 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.0337 0.6175, -0.04610, -0.0635 0.5841, -0.02440, -0.1016 0.5775, 0.01750, -0.1071 0.5777, 0.04660, -0.0881 0.6274, 0.07170, -0.6625 0.5694, 0.08320, -0.6615 0.5112, 0.09370, -0.6747 0.4731, 0.09830, -0.6822 0.4349, 0.10070, -0.6850 0.3960, 0.10120, -0.7157 0.3566, 0.10020, -0.6817 0.3172, 0.09790, -0.6883 0.2778, 0.09440, -0.7008 0.2393, 0.08960, -0.6978 0.2056, 0.08360, -0.7400 0.1633, 0.07610, -0.6994 0.1261, 0.06710, -0.7182 0.0900, 0.05640, -0.7007 0.0571, 0.04390, -0.7161 0.0283, 0.02940, -0.7407 0.0142, 0.01970, -0.7462 0.0081, 0.01410, -0.7768 0.0026, 0.00780, -0.7052 0.0000, 0.00000, -1.0037 0.0037, -0.00840, 0.6033 0.0112, -0.01420, 0.9601 0.0191, -0.01930, 1.0197 0.0397, -0.03030, 0.9769 0.0706, -0.04420, 0.8181 0.1037, -0.05710, 0.6712 0.1384, -0.06890, 0.5612 0.1741, -0.07950, 0.4162 0.2102, -0.08660, 0.2366 0.2472, -0.09640, 0.0915 0.2844, -0.10270, -0.0484 0.3225, -0.10690, -0.1449 0.3608, -0.10890, -0.2828 0.3991, -0.10830, -0.3329 0.4373, -0.10510, -0.3848 0.4757, -0.09890, -0.3221 0.5137, -0.09070, -0.2953 0.5694, -0.07640, -0.2080 15 Flap element taps 1.0000, 0.00130, -0.6187 0.9365, 0.01390, -0.6533 0.8333, 0.03280, -0.6811 0.7436, 0.04930, -0.6793 0.7049, 0.05670, -0.6767 0.6662, 0.06410, -0.6857 0.6522, 0.01390, -0.1142 0.5969, -0.00020, -0.1111 0.6000, -0.03020, -0.0983 0.6324, -0.04540, -0.0853 0.6667, -0.04880, 0.2898 0.7046, -0.04110, 0.2094 0.7429, -0.03210, 0.1406 0.8333, -0.01400, 0.0853 0.9311, -0.00120, -0.0193 --------- Run Conditions: vel=102.7 ft/s Re=1.008x10^6 AOA=20.01 Flap deflection=5.00 Totals: Cl=0.7134 Cdp=0.3366 Cm(c/4)=-0.1303 Cs=-0.0722 Ch=-0.2374 Main component: Cl=0.4828 Cdp=0.2153 Cm=-0.1222 Flap component: Cl=0.2306 Cdp=0.1213 Cm=-0.2045 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.0289 0.6175, -0.04610, -0.0703 0.5841, -0.02440, -0.1124 0.5775, 0.01750, -0.1169 0.5777, 0.04660, -0.0976 0.6274, 0.07170, -0.7338 0.5694, 0.08320, -0.7251 0.5112, 0.09370, -0.7365 0.4731, 0.09830, -0.7429 0.4349, 0.10070, -0.7436 0.3960, 0.10120, -0.7824 0.3566, 0.10020, -0.7283 0.3172, 0.09790, -0.7289 0.2778, 0.09440, -0.7348 0.2393, 0.08960, -0.7251 0.2056, 0.08360, -0.7727 0.1633, 0.07610, -0.7138 0.1261, 0.06710, -0.7387 0.0900, 0.05640, -0.7095 0.0571, 0.04390, -0.7291 0.0283, 0.02940, -0.7472 0.0142, 0.01970, -0.7580 0.0081, 0.01410, -0.7936 0.0026, 0.00780, -0.7114 0.0000, 0.00000, -1.0105 0.0037, -0.00840, 0.5278 0.0112, -0.01420, 0.9330 0.0191, -0.01930, 1.0162 0.0397, -0.03030, 0.9984 0.0706, -0.04420, 0.8515 0.1037, -0.05710, 0.7116 0.1384, -0.06890, 0.6173 0.1741, -0.07950, 0.4761 0.2102, -0.08660, 0.2824 0.2472, -0.09640, 0.1433 0.2844, -0.10270, -0.0037 0.3225, -0.10690, -0.0940 0.3608, -0.10890, -0.2409 0.3991, -0.10830, -0.2916 0.4373, -0.10510, -0.3557 0.4757, -0.09890, -0.3024 0.5137, -0.09070, -0.2826 0.5694, -0.07640, -0.1793 15 Flap element taps 1.0000, 0.00130, -0.6764 0.9365, 0.01390, -0.7106 0.8333, 0.03280, -0.7441 0.7436, 0.04930, -0.7487 0.7049, 0.05670, -0.7493 0.6662, 0.06410, -0.7572 0.6522, 0.01390, -0.1294 0.5969, -0.00020, -0.1221 0.6000, -0.03020, -0.1109 0.6324, -0.04540, -0.0967 0.6667, -0.04880, 0.3114 0.7046, -0.04110, 0.2079 0.7429, -0.03210, 0.1344 0.8333, -0.01400, 0.0739 0.9311, -0.00120, -0.0385 --------- Run Conditions: vel=102.7 ft/s Re=1.006x10^6 AOA=23.98 Flap deflection=5.00 Totals: Cl=0.8361 Cdp=0.4562 Cm(c/4)=-0.1593 Cs=-0.0771 Ch=-0.2725 Main component: Cl=0.5842 Cdp=0.2975 Cm=-0.1632 Flap component: Cl=0.2519 Cdp=0.1588 Cm=-0.2335 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.0189 0.6175, -0.04610, -0.0616 0.5841, -0.02440, -0.1111 0.5775, 0.01750, -0.1172 0.5777, 0.04660, -0.0913 0.6274, 0.07170, -0.8598 0.5694, 0.08320, -0.8502 0.5112, 0.09370, -0.8658 0.4731, 0.09830, -0.8652 0.4349, 0.10070, -0.8624 0.3960, 0.10120, -0.9075 0.3566, 0.10020, -0.8416 0.3172, 0.09790, -0.8419 0.2778, 0.09440, -0.8436 0.2393, 0.08960, -0.8384 0.2056, 0.08360, -0.8913 0.1633, 0.07610, -0.8239 0.1261, 0.06710, -0.8558 0.0900, 0.05640, -0.8223 0.0571, 0.04390, -0.8355 0.0283, 0.02940, -0.8433 0.0142, 0.01970, -0.8539 0.0081, 0.01410, -0.8994 0.0026, 0.00780, -0.8050 0.0000, 0.00000, -0.9497 0.0037, -0.00840, 0.2814 0.0112, -0.01420, 0.8203 0.0191, -0.01930, 0.9697 0.0397, -0.03030, 1.0247 0.0706, -0.04420, 0.9229 0.1037, -0.05710, 0.8091 0.1384, -0.06890, 0.7400 0.1741, -0.07950, 0.6063 0.2102, -0.08660, 0.4103 0.2472, -0.09640, 0.2831 0.2844, -0.10270, 0.1313 0.3225, -0.10690, 0.0469 0.3608, -0.10890, -0.1104 0.3991, -0.10830, -0.1690 0.4373, -0.10510, -0.2535 0.4757, -0.09890, -0.2169 0.5137, -0.09070, -0.2163 0.5694, -0.07640, -0.0968 15 Flap element taps 1.0000, 0.00130, -0.7980 0.9365, 0.01390, -0.8353 0.8333, 0.03280, -0.8618 0.7436, 0.04930, -0.8672 0.7049, 0.05670, -0.8717 0.6662, 0.06410, -0.8805 0.6522, 0.01390, -0.1325 0.5969, -0.00020, -0.1251 0.6000, -0.03020, -0.1094 0.6324, -0.04540, -0.0951 0.6667, -0.04880, 0.3321 0.7046, -0.04110, 0.2284 0.7429, -0.03210, 0.1448 0.8333, -0.01400, 0.0699 0.9311, -0.00120, -0.0633 --------- Run Conditions: vel=100.8 ft/s Re=0.987x10^6 AOA=26.95 Flap deflection=5.00 Totals: Cl=1.0089 Cdp=0.6018 Cm(c/4)=-0.2038 Cs=-0.0792 Ch=-0.3252 Main component: Cl=0.7152 Cdp=0.3936 Cm=-0.2153 Flap component: Cl=0.2938 Cdp=0.2083 Cm=-0.2815 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.0131 0.6175, -0.04610, -0.0744 0.5841, -0.02440, -0.1310 0.5775, 0.01750, -0.1392 0.5777, 0.04660, -0.1041 0.6274, 0.07170, -1.0525 0.5694, 0.08320, -1.0411 0.5112, 0.09370, -1.0590 0.4731, 0.09830, -1.0595 0.4349, 0.10070, -1.0571 0.3960, 0.10120, -1.1076 0.3566, 0.10020, -1.0311 0.3172, 0.09790, -1.0314 0.2778, 0.09440, -1.0303 0.2393, 0.08960, -1.0238 0.2056, 0.08360, -1.0806 0.1633, 0.07610, -1.0020 0.1261, 0.06710, -1.0353 0.0900, 0.05640, -0.9952 0.0571, 0.04390, -1.0132 0.0283, 0.02940, -1.0171 0.0142, 0.01970, -1.0242 0.0081, 0.01410, -1.0767 0.0026, 0.00780, -0.9687 0.0000, 0.00000, -1.0285 0.0037, -0.00840, -0.0072 0.0112, -0.01420, 0.6704 0.0191, -0.01930, 0.8927 0.0397, -0.03030, 1.0230 0.0706, -0.04420, 0.9679 0.1037, -0.05710, 0.8827 0.1384, -0.06890, 0.8399 0.1741, -0.07950, 0.7164 0.2102, -0.08660, 0.5227 0.2472, -0.09640, 0.4059 0.2844, -0.10270, 0.2538 0.3225, -0.10690, 0.1752 0.3608, -0.10890, 0.0104 0.3991, -0.10830, -0.0499 0.4373, -0.10510, -0.1516 0.4757, -0.09890, -0.1309 0.5137, -0.09070, -0.1556 0.5694, -0.07640, -0.0349 15 Flap element taps 1.0000, 0.00130, -0.9713 0.9365, 0.01390, -1.0070 0.8333, 0.03280, -1.0449 0.7436, 0.04930, -1.0489 0.7049, 0.05670, -1.0582 0.6662, 0.06410, -1.0702 0.6522, 0.01390, -0.1529 0.5969, -0.00020, -0.1463 0.6000, -0.03020, -0.1258 0.6324, -0.04540, -0.1288 0.6667, -0.04880, 0.5604 0.7046, -0.04110, 0.2495 0.7429, -0.03210, 0.1566 0.8333, -0.01400, 0.0642 0.9311, -0.00120, -0.0905