S809 UNVENTED AILERON, LEGR, CHORD = 18 IN --------- Run Conditions: vel=103.7 ft/s Re=1.006x10^6 AOA=-5.98 Flap deflection=-10.00 Totals: Cl=-0.7786 Cdp=0.0677 Cm(c/4)=0.0566 Cs=0.0138 Ch=0.1102 Main component: Cl=-0.6570 Cdp=0.0405 Cm=0.1528 Flap component: Cl=-0.1217 Cdp=0.0272 Cm=0.0993 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3531 0.6175, -0.04610, -0.3340 0.5841, -0.02440, -0.2791 0.5775, 0.01750, -0.2987 0.5777, 0.04660, -0.2944 0.6274, 0.07170, 0.2343 0.5694, 0.08320, 0.0546 0.5112, 0.09370, -0.1617 0.4731, 0.09830, -0.2194 0.4349, 0.10070, -0.2175 0.3960, 0.10120, -0.1773 0.3566, 0.10020, -0.1305 0.3172, 0.09790, -0.0733 0.2778, 0.09440, -0.0262 0.2393, 0.08960, 0.0298 0.2056, 0.08360, 0.0958 0.1633, 0.07610, 0.2009 0.1261, 0.06710, 0.3183 0.0900, 0.05640, 0.4220 0.0571, 0.04390, 0.6775 0.0283, 0.02940, 0.9120 0.0142, 0.01970, 1.0107 0.0081, 0.01410, 0.9562 0.0026, 0.00780, 0.4523 0.0000, 0.00000, -0.3138 0.0037, -0.00840, -2.2933 0.0112, -0.01420, -1.6664 0.0191, -0.01930, -1.4368 0.0397, -0.03030, -1.1208 0.0706, -0.04420, -1.0707 0.1037, -0.05710, -1.0078 0.1384, -0.06890, -1.0765 0.1741, -0.07950, -1.1070 0.2102, -0.08660, -1.1742 0.2472, -0.09640, -1.2342 0.2844, -0.10270, -1.2377 0.3225, -0.10690, -1.2332 0.3608, -0.10890, -1.2043 0.3991, -0.10830, -1.0960 0.4373, -0.10510, -0.9182 0.4757, -0.09890, -0.6581 0.5137, -0.09070, -0.4650 0.5694, -0.07640, -0.3720 14 Flap element taps 1.0000, 0.00130, -0.3161 0.9365, 0.01390, -0.0910 0.8333, 0.03280, 0.0236 0.7436, 0.04930, 0.1126 0.7049, 0.05670, 0.1976 0.6662, 0.06410, 0.1265 0.6522, 0.01390, -0.2822 0.5969, -0.00020, -0.3062 0.6000, -0.03020, -0.3603 0.6324, -0.04540, -0.3409 0.6667, -0.04880, -0.3321 0.7046, -0.04110, -0.3349 0.7429, -0.03210, -0.3425 0.9311, -0.00120, -0.3668 --------- Run Conditions: vel=103.8 ft/s Re=1.007x10^6 AOA=0.00 Flap deflection=-10.00 Totals: Cl=-0.4262 Cdp=0.0157 Cm(c/4)=0.0546 Cs=-0.0157 Ch=0.0609 Main component: Cl=-0.3570 Cdp=0.0094 Cm=0.1059 Flap component: Cl=-0.0692 Cdp=0.0063 Cm=0.0553 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2492 0.6175, -0.04610, -0.1693 0.5841, -0.02440, -0.1348 0.5775, 0.01750, -0.1534 0.5777, 0.04660, -0.1515 0.6274, 0.07170, 0.1502 0.5694, 0.08320, -0.0146 0.5112, 0.09370, -0.2623 0.4731, 0.09830, -0.3543 0.4349, 0.10070, -0.3837 0.3960, 0.10120, -0.3761 0.3566, 0.10020, -0.3400 0.3172, 0.09790, -0.3068 0.2778, 0.09440, -0.2875 0.2393, 0.08960, -0.2635 0.2056, 0.08360, -0.2424 0.1633, 0.07610, -0.1580 0.1261, 0.06710, -0.0816 0.0900, 0.05640, -0.0535 0.0571, 0.04390, 0.2105 0.0283, 0.02940, 0.4790 0.0142, 0.01970, 0.7213 0.0081, 0.01410, 0.8475 0.0026, 0.00780, 0.9620 0.0000, 0.00000, -0.3242 0.0037, -0.00840, -0.0394 0.0112, -0.01420, -0.1363 0.0191, -0.01930, -0.2505 0.0397, -0.03030, -0.2592 0.0706, -0.04420, -0.3999 0.1037, -0.05710, -0.4579 0.1384, -0.06890, -0.6002 0.1741, -0.07950, -0.6995 0.2102, -0.08660, -0.8338 0.2472, -0.09640, -0.9469 0.2844, -0.10270, -1.0185 0.3225, -0.10690, -1.0713 0.3608, -0.10890, -1.1221 0.3991, -0.10830, -1.0972 0.4373, -0.10510, -1.0213 0.4757, -0.09890, -0.8434 0.5137, -0.09070, -0.6920 0.5694, -0.07640, -0.4184 14 Flap element taps 1.0000, 0.00130, -0.1252 0.9365, 0.01390, -0.0132 0.8333, 0.03280, 0.0366 0.7436, 0.04930, 0.0939 0.7049, 0.05670, 0.1526 0.6662, 0.06410, 0.0980 0.6522, 0.01390, -0.1418 0.5969, -0.00020, -0.1535 0.6000, -0.03020, -0.1849 0.6324, -0.04540, -0.1776 0.6667, -0.04880, -0.1743 0.7046, -0.04110, -0.1576 0.7429, -0.03210, -0.1569 0.9311, -0.00120, -0.1683 Wake drag found for this condition, Cdw=0.0311 --------- Run Conditions: vel=103.1 ft/s Re=1.000x10^6 AOA=3.01 Flap deflection=-10.00 Totals: Cl=-0.1759 Cdp=0.0082 Cm(c/4)=0.0550 Cs=-0.0174 Ch=0.0473 Main component: Cl=-0.1228 Cdp=0.0095 Cm=0.0565 Flap component: Cl=-0.0531 Cdp=-0.0013 Cm=0.0423 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2411 0.6175, -0.04610, -0.1538 0.5841, -0.02440, -0.1264 0.5775, 0.01750, -0.1452 0.5777, 0.04660, -0.1431 0.6274, 0.07170, 0.0932 0.5694, 0.08320, -0.0653 0.5112, 0.09370, -0.3322 0.4731, 0.09830, -0.4441 0.4349, 0.10070, -0.4930 0.3960, 0.10120, -0.5109 0.3566, 0.10020, -0.4790 0.3172, 0.09790, -0.4602 0.2778, 0.09440, -0.4605 0.2393, 0.08960, -0.4569 0.2056, 0.08360, -0.4679 0.1633, 0.07610, -0.3951 0.1261, 0.06710, -0.3538 0.0900, 0.05640, -0.3862 0.0571, 0.04390, -0.1524 0.0283, 0.02940, 0.0623 0.0142, 0.01970, 0.2872 0.0081, 0.01410, 0.4434 0.0026, 0.00780, 0.6549 0.0000, 0.00000, -0.3587 0.0037, -0.00840, 0.6964 0.0112, -0.01420, 0.4560 0.0191, -0.01930, 0.2977 0.0397, -0.03030, 0.1581 0.0706, -0.04420, -0.0406 0.1037, -0.05710, -0.1540 0.1384, -0.06890, -0.3070 0.1741, -0.07950, -0.4339 0.2102, -0.08660, -0.5965 0.2472, -0.09640, -0.7193 0.2844, -0.10270, -0.8153 0.3225, -0.10690, -0.8810 0.3608, -0.10890, -0.9586 0.3991, -0.10830, -0.9556 0.4373, -0.10510, -0.9162 0.4757, -0.09890, -0.7679 0.5137, -0.09070, -0.6467 0.5694, -0.07640, -0.3984 14 Flap element taps 1.0000, 0.00130, -0.0727 0.9365, 0.01390, 0.0045 0.8333, 0.03280, 0.0285 0.7436, 0.04930, 0.0688 0.7049, 0.05670, 0.1133 0.6662, 0.06410, 0.0520 0.6522, 0.01390, -0.1376 0.5969, -0.00020, -0.1427 0.6000, -0.03020, -0.1683 0.6324, -0.04540, -0.1650 0.6667, -0.04880, -0.1622 0.7046, -0.04110, -0.1230 0.7429, -0.03210, -0.1177 0.9311, -0.00120, -0.1181 Wake drag found for this condition, Cdw=0.0280 --------- Run Conditions: vel=103.4 ft/s Re=1.001x10^6 AOA=6.02 Flap deflection=-10.00 Totals: Cl=0.0730 Cdp=0.0110 Cm(c/4)=0.0577 Cs=-0.0033 Ch=0.0379 Main component: Cl=0.1131 Cdp=0.0216 Cm=0.0068 Flap component: Cl=-0.0401 Cdp=-0.0106 Cm=0.0325 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2444 0.6175, -0.04610, -0.1735 0.5841, -0.02440, -0.1496 0.5775, 0.01750, -0.1686 0.5777, 0.04660, -0.1671 0.6274, 0.07170, 0.0268 0.5694, 0.08320, -0.1079 0.5112, 0.09370, -0.3885 0.4731, 0.09830, -0.5227 0.4349, 0.10070, -0.5937 0.3960, 0.10120, -0.6380 0.3566, 0.10020, -0.6147 0.3172, 0.09790, -0.6174 0.2778, 0.09440, -0.6342 0.2393, 0.08960, -0.6585 0.2056, 0.08360, -0.7042 0.1633, 0.07610, -0.6521 0.1261, 0.06710, -0.6547 0.0900, 0.05640, -0.7521 0.0571, 0.04390, -0.5849 0.0283, 0.02940, -0.4806 0.0142, 0.01970, -0.3099 0.0081, 0.01410, -0.3215 0.0026, 0.00780, 0.0679 0.0000, 0.00000, -0.3771 0.0037, -0.00840, 0.9911 0.0112, -0.01420, 0.8459 0.0191, -0.01930, 0.6992 0.0397, -0.03030, 0.5034 0.0706, -0.04420, 0.2705 0.1037, -0.05710, 0.1199 0.1384, -0.06890, -0.0361 0.1741, -0.07950, -0.1798 0.2102, -0.08660, -0.3653 0.2472, -0.09640, -0.4933 0.2844, -0.10270, -0.6087 0.3225, -0.10690, -0.6863 0.3608, -0.10890, -0.7899 0.3991, -0.10830, -0.8053 0.4373, -0.10510, -0.8008 0.4757, -0.09890, -0.6837 0.5137, -0.09070, -0.5945 0.5694, -0.07640, -0.3724 14 Flap element taps 1.0000, 0.00130, 0.0091 0.9365, 0.01390, 0.0380 0.8333, 0.03280, 0.0292 0.7436, 0.04930, 0.0487 0.7049, 0.05670, 0.0699 0.6662, 0.06410, -0.0092 0.6522, 0.01390, -0.1631 0.5969, -0.00020, -0.1648 0.6000, -0.03020, -0.1895 0.6324, -0.04540, -0.1869 0.6667, -0.04880, -0.1785 0.7046, -0.04110, -0.1039 0.7429, -0.03210, -0.0904 0.9311, -0.00120, -0.0579 Wake drag found for this condition, Cdw=0.0227 --------- Run Conditions: vel=103.7 ft/s Re=1.005x10^6 AOA=8.83 Flap deflection=-10.00 Totals: Cl=0.2711 Cdp=0.0200 Cm(c/4)=0.0622 Cs=0.0218 Ch=0.0277 Main component: Cl=0.2992 Cdp=0.0489 Cm=-0.0296 Flap component: Cl=-0.0281 Cdp=-0.0289 Cm=0.0241 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2998 0.6175, -0.04610, -0.2840 0.5841, -0.02440, -0.2581 0.5775, 0.01750, -0.2780 0.5777, 0.04660, -0.2748 0.6274, 0.07170, -0.0395 0.5694, 0.08320, -0.1304 0.5112, 0.09370, -0.3963 0.4731, 0.09830, -0.5537 0.4349, 0.10070, -0.6502 0.3960, 0.10120, -0.7262 0.3566, 0.10020, -0.7179 0.3172, 0.09790, -0.7376 0.2778, 0.09440, -0.7793 0.2393, 0.08960, -0.8266 0.2056, 0.08360, -0.9111 0.1633, 0.07610, -0.8815 0.1261, 0.06710, -0.9334 0.0900, 0.05640, -1.0926 0.0571, 0.04390, -1.0117 0.0283, 0.02940, -1.0441 0.0142, 0.01970, -0.9939 0.0081, 0.01410, -1.1948 0.0026, 0.00780, -0.6524 0.0000, 0.00000, -0.4057 0.0037, -0.00840, 0.9536 0.0112, -0.01420, 0.9961 0.0191, -0.01930, 0.9179 0.0397, -0.03030, 0.7371 0.0706, -0.04420, 0.4985 0.1037, -0.05710, 0.3287 0.1384, -0.06890, 0.1822 0.1741, -0.07950, 0.0231 0.2102, -0.08660, -0.1832 0.2472, -0.09640, -0.3184 0.2844, -0.10270, -0.4521 0.3225, -0.10690, -0.5334 0.3608, -0.10890, -0.6597 0.3991, -0.10830, -0.7005 0.4373, -0.10510, -0.7200 0.4757, -0.09890, -0.6307 0.5137, -0.09070, -0.5715 0.5694, -0.07640, -0.3787 14 Flap element taps 1.0000, 0.00130, 0.1454 0.9365, 0.01390, 0.1166 0.8333, 0.03280, 0.0602 0.7436, 0.04930, 0.0381 0.7049, 0.05670, 0.0257 0.6662, 0.06410, -0.1046 0.6522, 0.01390, -0.2739 0.5969, -0.00020, -0.2726 0.6000, -0.03020, -0.3019 0.6324, -0.04540, -0.3004 0.6667, -0.04880, -0.2940 0.7046, -0.04110, -0.1520 0.7429, -0.03210, -0.0818 0.9311, -0.00120, 0.0993 --------- Run Conditions: vel=103.4 ft/s Re=1.002x10^6 AOA=12.01 Flap deflection=-10.00 Totals: Cl=0.5469 Cdp=0.0451 Cm(c/4)=0.0458 Cs=0.0697 Ch=-0.0187 Main component: Cl=0.5225 Cdp=0.0789 Cm=-0.0741 Flap component: Cl=0.0244 Cdp=-0.0338 Cm=-0.0162 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2818 0.6175, -0.04610, -0.3292 0.5841, -0.02440, -0.3132 0.5775, 0.01750, -0.3331 0.5777, 0.04660, -0.3327 0.6274, 0.07170, -0.1871 0.5694, 0.08320, -0.1922 0.5112, 0.09370, -0.3443 0.4731, 0.09830, -0.5093 0.4349, 0.10070, -0.6524 0.3960, 0.10120, -0.7866 0.3566, 0.10020, -0.8063 0.3172, 0.09790, -0.8618 0.2778, 0.09440, -0.9325 0.2393, 0.08960, -1.0195 0.2056, 0.08360, -1.1504 0.1633, 0.07610, -1.1604 0.1261, 0.06710, -1.2757 0.0900, 0.05640, -1.5083 0.0571, 0.04390, -1.5712 0.0283, 0.02940, -1.8176 0.0142, 0.01970, -2.0483 0.0081, 0.01410, -2.3674 0.0026, 0.00780, -1.9145 0.0000, 0.00000, -0.4463 0.0037, -0.00840, 0.5400 0.0112, -0.01420, 0.9714 0.0191, -0.01930, 1.0152 0.0397, -0.03030, 0.9298 0.0706, -0.04420, 0.7225 0.1037, -0.05710, 0.5515 0.1384, -0.06890, 0.4235 0.1741, -0.07950, 0.2583 0.2102, -0.08660, 0.0426 0.2472, -0.09640, -0.0910 0.2844, -0.10270, -0.2430 0.3225, -0.10690, -0.3381 0.3608, -0.10890, -0.4832 0.3991, -0.10830, -0.5417 0.4373, -0.10510, -0.5898 0.4757, -0.09890, -0.5334 0.5137, -0.09070, -0.4976 0.5694, -0.07640, -0.3191 14 Flap element taps 1.0000, 0.00130, 0.1284 0.9365, 0.01390, 0.0872 0.8333, 0.03280, -0.0213 0.7436, 0.04930, -0.1108 0.7049, 0.05670, -0.1468 0.6662, 0.06410, -0.2409 0.6522, 0.01390, -0.3321 0.5969, -0.00020, -0.3254 0.6000, -0.03020, -0.3474 0.6324, -0.04540, -0.3514 0.6667, -0.04880, -0.3067 0.7046, -0.04110, -0.1660 0.7429, -0.03210, -0.0357 0.9311, -0.00120, 0.2197 --------- Run Conditions: vel=103.4 ft/s Re=1.004x10^6 AOA=15.03 Flap deflection=-10.00 Totals: Cl=0.6616 Cdp=0.0855 Cm(c/4)=0.0267 Cs=0.0890 Ch=-0.0809 Main component: Cl=0.5818 Cdp=0.1026 Cm=-0.0761 Flap component: Cl=0.0798 Cdp=-0.0171 Cm=-0.0625 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3094 0.6175, -0.04610, -0.3861 0.5841, -0.02440, -0.3727 0.5775, 0.01750, -0.3853 0.5777, 0.04660, -0.3869 0.6274, 0.07170, -0.2926 0.5694, 0.08320, -0.2950 0.5112, 0.09370, -0.2893 0.4731, 0.09830, -0.3062 0.4349, 0.10070, -0.3782 0.3960, 0.10120, -0.4864 0.3566, 0.10020, -0.6174 0.3172, 0.09790, -0.7333 0.2778, 0.09440, -0.8670 0.2393, 0.08960, -0.9971 0.2056, 0.08360, -1.1306 0.1633, 0.07610, -1.2708 0.1261, 0.06710, -1.4000 0.0900, 0.05640, -1.7214 0.0571, 0.04390, -1.9028 0.0283, 0.02940, -2.3556 0.0142, 0.01970, -2.8263 0.0081, 0.01410, -3.2480 0.0026, 0.00780, -3.0078 0.0000, 0.00000, -0.3430 0.0037, -0.00840, 0.0107 0.0112, -0.01420, 0.8212 0.0191, -0.01930, 0.9926 0.0397, -0.03030, 0.9937 0.0706, -0.04420, 0.8483 0.1037, -0.05710, 0.6972 0.1384, -0.06890, 0.5246 0.1741, -0.07950, 0.3701 0.2102, -0.08660, 0.2046 0.2472, -0.09640, 0.0426 0.2844, -0.10270, -0.1044 0.3225, -0.10690, -0.2356 0.3608, -0.10890, -0.3723 0.3991, -0.10830, -0.4652 0.4373, -0.10510, -0.5090 0.4757, -0.09890, -0.4703 0.5137, -0.09070, -0.4462 0.5694, -0.07640, -0.3375 14 Flap element taps 1.0000, 0.00130, -0.1051 0.9365, 0.01390, -0.2030 0.8333, 0.03280, -0.2722 0.7436, 0.04930, -0.3003 0.7049, 0.05670, -0.2974 0.6662, 0.06410, -0.3290 0.6522, 0.01390, -0.3754 0.5969, -0.00020, -0.3745 0.6000, -0.03020, -0.3899 0.6324, -0.04540, -0.3895 0.6667, -0.04880, -0.2927 0.7046, -0.04110, -0.1949 0.7429, -0.03210, -0.0582 0.9311, -0.00120, 0.1352 --------- Run Conditions: vel=102.2 ft/s Re=0.994x10^6 AOA=18.02 Flap deflection=-10.00 Totals: Cl=0.5439 Cdp=0.1571 Cm(c/4)=-0.0117 Cs=0.0189 Ch=-0.1151 Main component: Cl=0.4269 Cdp=0.1635 Cm=-0.0610 Flap component: Cl=0.1171 Cdp=-0.0064 Cm=-0.0922 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4086 0.6175, -0.04610, -0.5255 0.5841, -0.02440, -0.5155 0.5775, 0.01750, -0.5293 0.5777, 0.04660, -0.5318 0.6274, 0.07170, -0.4829 0.5694, 0.08320, -0.4837 0.5112, 0.09370, -0.4873 0.4731, 0.09830, -0.4799 0.4349, 0.10070, -0.4832 0.3960, 0.10120, -0.4959 0.3566, 0.10020, -0.5083 0.3172, 0.09790, -0.5358 0.2778, 0.09440, -0.5724 0.2393, 0.08960, -0.6123 0.2056, 0.08360, -0.6729 0.1633, 0.07610, -0.7514 0.1261, 0.06710, -0.8410 0.0900, 0.05640, -1.0404 0.0571, 0.04390, -1.3131 0.0283, 0.02940, -1.8617 0.0142, 0.01970, -2.3811 0.0081, 0.01410, -2.8614 0.0026, 0.00780, -2.7038 0.0000, 0.00000, -0.3887 0.0037, -0.00840, 0.0190 0.0112, -0.01420, 0.8095 0.0191, -0.01930, 0.9833 0.0397, -0.03030, 0.9968 0.0706, -0.04420, 0.8610 0.1037, -0.05710, 0.7133 0.1384, -0.06890, 0.5503 0.1741, -0.07950, 0.3944 0.2102, -0.08660, 0.2207 0.2472, -0.09640, 0.0572 0.2844, -0.10270, -0.0992 0.3225, -0.10690, -0.2366 0.3608, -0.10890, -0.3890 0.3991, -0.10830, -0.4904 0.4373, -0.10510, -0.5505 0.4757, -0.09890, -0.5229 0.5137, -0.09070, -0.5146 0.5694, -0.07640, -0.4064 14 Flap element taps 1.0000, 0.00130, -0.3085 0.9365, 0.01390, -0.4158 0.8333, 0.03280, -0.4946 0.7436, 0.04930, -0.5151 0.7049, 0.05670, -0.5057 0.6662, 0.06410, -0.5063 0.6522, 0.01390, -0.5215 0.5969, -0.00020, -0.5185 0.6000, -0.03020, -0.5278 0.6324, -0.04540, -0.5280 0.6667, -0.04880, -0.3401 0.7046, -0.04110, -0.2804 0.7429, -0.03210, -0.1460 0.9311, -0.00120, 0.0184 --------- Run Conditions: vel=102.8 ft/s Re=1.001x10^6 AOA=19.99 Flap deflection=-10.00 Totals: Cl=0.5351 Cdp=0.1969 Cm(c/4)=-0.0200 Cs=-0.0021 Ch=-0.1231 Main component: Cl=0.4146 Cdp=0.1958 Cm=-0.0663 Flap component: Cl=0.1205 Cdp=0.0011 Cm=-0.0962 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4537 0.6175, -0.04610, -0.5759 0.5841, -0.02440, -0.5698 0.5775, 0.01750, -0.5810 0.5777, 0.04660, -0.5828 0.6274, 0.07170, -0.5572 0.5694, 0.08320, -0.5520 0.5112, 0.09370, -0.5700 0.4731, 0.09830, -0.5567 0.4349, 0.10070, -0.5597 0.3960, 0.10120, -0.5797 0.3566, 0.10020, -0.5736 0.3172, 0.09790, -0.5774 0.2778, 0.09440, -0.5816 0.2393, 0.08960, -0.5930 0.2056, 0.08360, -0.6299 0.1633, 0.07610, -0.6736 0.1261, 0.06710, -0.7625 0.0900, 0.05640, -0.9347 0.0571, 0.04390, -1.2066 0.0283, 0.02940, -1.7085 0.0142, 0.01970, -2.2639 0.0081, 0.01410, -2.7820 0.0026, 0.00780, -2.7147 0.0000, 0.00000, -0.4098 0.0037, -0.00840, -0.0457 0.0112, -0.01420, 0.7802 0.0191, -0.01930, 0.9734 0.0397, -0.03030, 1.0045 0.0706, -0.04420, 0.8778 0.1037, -0.05710, 0.7340 0.1384, -0.06890, 0.5774 0.1741, -0.07950, 0.4199 0.2102, -0.08660, 0.2368 0.2472, -0.09640, 0.0745 0.2844, -0.10270, -0.0923 0.3225, -0.10690, -0.2291 0.3608, -0.10890, -0.3921 0.3991, -0.10830, -0.4989 0.4373, -0.10510, -0.5716 0.4757, -0.09890, -0.5497 0.5137, -0.09070, -0.5500 0.5694, -0.07640, -0.4453 14 Flap element taps 1.0000, 0.00130, -0.4426 0.9365, 0.01390, -0.5393 0.8333, 0.03280, -0.5754 0.7436, 0.04930, -0.5756 0.7049, 0.05670, -0.5716 0.6662, 0.06410, -0.5697 0.6522, 0.01390, -0.5754 0.5969, -0.00020, -0.5708 0.6000, -0.03020, -0.5810 0.6324, -0.04540, -0.5849 0.6667, -0.04880, -0.4200 0.7046, -0.04110, -0.3405 0.7429, -0.03210, -0.2077 0.9311, -0.00120, -0.0608 --------- Run Conditions: vel=101.6 ft/s Re=0.990x10^6 AOA=24.00 Flap deflection=-10.00 Totals: Cl=0.6881 Cdp=0.3219 Cm(c/4)=-0.0517 Cs=-0.0142 Ch=-0.1438 Main component: Cl=0.5395 Cdp=0.3043 Cm=-0.1228 Flap component: Cl=0.1486 Cdp=0.0176 Cm=-0.1188 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4409 0.6175, -0.04610, -0.6105 0.5841, -0.02440, -0.6056 0.5775, 0.01750, -0.6177 0.5777, 0.04660, -0.6228 0.6274, 0.07170, -0.7173 0.5694, 0.08320, -0.7337 0.5112, 0.09370, -0.7658 0.4731, 0.09830, -0.7608 0.4349, 0.10070, -0.7795 0.3960, 0.10120, -0.8085 0.3566, 0.10020, -0.8062 0.3172, 0.09790, -0.8069 0.2778, 0.09440, -0.8372 0.2393, 0.08960, -0.8732 0.2056, 0.08360, -0.9433 0.1633, 0.07610, -1.0073 0.1261, 0.06710, -1.0816 0.0900, 0.05640, -1.1446 0.0571, 0.04390, -1.2487 0.0283, 0.02940, -1.4286 0.0142, 0.01970, -1.7148 0.0081, 0.01410, -2.0358 0.0026, 0.00780, -1.9797 0.0000, 0.00000, -0.4753 0.0037, -0.00840, -0.1483 0.0112, -0.01420, 0.6940 0.0191, -0.01930, 0.9253 0.0397, -0.03030, 1.0147 0.0706, -0.04420, 0.9302 0.1037, -0.05710, 0.8085 0.1384, -0.06890, 0.6786 0.1741, -0.07950, 0.5341 0.2102, -0.08660, 0.3504 0.2472, -0.09640, 0.1982 0.2844, -0.10270, 0.0300 0.3225, -0.10690, -0.1034 0.3608, -0.10890, -0.2740 0.3991, -0.10830, -0.3887 0.4373, -0.10510, -0.4782 0.4757, -0.09890, -0.4735 0.5137, -0.09070, -0.4934 0.5694, -0.07640, -0.4049 14 Flap element taps 1.0000, 0.00130, -0.5308 0.9365, 0.01390, -0.5982 0.8333, 0.03280, -0.6706 0.7436, 0.04930, -0.6876 0.7049, 0.05670, -0.6908 0.6662, 0.06410, -0.6430 0.6522, 0.01390, -0.6134 0.5969, -0.00020, -0.6054 0.6000, -0.03020, -0.6135 0.6324, -0.04540, -0.6206 0.6667, -0.04880, -0.2953 0.7046, -0.04110, -0.3278 0.7429, -0.03210, -0.2042 0.9311, -0.00120, -0.0910 --------- Run Conditions: vel=103.3 ft/s Re=1.007x10^6 AOA=27.00 Flap deflection=-10.00 Totals: Cl=0.7596 Cdp=0.4044 Cm(c/4)=-0.0632 Cs=-0.0155 Ch=-0.1628 Main component: Cl=0.5986 Cdp=0.3686 Cm=-0.1457 Flap component: Cl=0.1610 Cdp=0.0358 Cm=-0.1326 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4421 0.6175, -0.04610, -0.6275 0.5841, -0.02440, -0.6226 0.5775, 0.01750, -0.6332 0.5777, 0.04660, -0.6371 0.6274, 0.07170, -0.7360 0.5694, 0.08320, -0.7682 0.5112, 0.09370, -0.8066 0.4731, 0.09830, -0.8007 0.4349, 0.10070, -0.8003 0.3960, 0.10120, -0.8599 0.3566, 0.10020, -0.8854 0.3172, 0.09790, -0.9201 0.2778, 0.09440, -0.9614 0.2393, 0.08960, -1.0323 0.2056, 0.08360, -1.1196 0.1633, 0.07610, -1.2033 0.1261, 0.06710, -1.2967 0.0900, 0.05640, -1.3504 0.0571, 0.04390, -1.3999 0.0283, 0.02940, -1.4502 0.0142, 0.01970, -1.6046 0.0081, 0.01410, -1.8189 0.0026, 0.00780, -1.6329 0.0000, 0.00000, -0.4851 0.0037, -0.00840, -0.2163 0.0112, -0.01420, 0.6322 0.0191, -0.01930, 0.8879 0.0397, -0.03030, 1.0157 0.0706, -0.04420, 0.9613 0.1037, -0.05710, 0.8568 0.1384, -0.06890, 0.7428 0.1741, -0.07950, 0.6036 0.2102, -0.08660, 0.4201 0.2472, -0.09640, 0.2724 0.2844, -0.10270, 0.1027 0.3225, -0.10690, -0.0326 0.3608, -0.10890, -0.2096 0.3991, -0.10830, -0.3287 0.4373, -0.10510, -0.4323 0.4757, -0.09890, -0.4391 0.5137, -0.09070, -0.4688 0.5694, -0.07640, -0.3951 14 Flap element taps 1.0000, 0.00130, -0.7038 0.9365, 0.01390, -0.7358 0.8333, 0.03280, -0.7589 0.7436, 0.04930, -0.7673 0.7049, 0.05670, -0.7701 0.6662, 0.06410, -0.6870 0.6522, 0.01390, -0.6316 0.5969, -0.00020, -0.6223 0.6000, -0.03020, -0.6308 0.6324, -0.04540, -0.6370 0.6667, -0.04880, -0.3018 0.7046, -0.04110, -0.3533 0.7429, -0.03210, -0.2335 0.9311, -0.00120, -0.1576