S809 SPOILER FLAP, CLEAN, CHORD = 18 INCHES --------- Run Conditions: vel=106.0 ft/s Re=1.004x10^6 AOA=-6.00 Flap deflection=20.00 Totals: Cl=-0.8263 Cdp=0.1040 Cm(c/4)=0.0300 Cs=-0.0170 Ch=-0.0142 Main component: Cl=-0.7615 Cdp=0.0242 Cm=0.1815 Flap component: Cl=-0.0648 Cdp=0.0798 Cm=0.0567 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3068 0.5905, -0.01667, -0.4379 0.5709, 0.03110, -0.0457 0.5889, 0.07933, -0.0420 0.5500, 0.08689, 0.4998 0.5110, 0.09367, 0.1670 0.4731, 0.09830, 0.1796 0.4349, 0.10070, 0.1535 0.3960, 0.10120, 0.1035 0.3566, 0.10020, 0.0972 0.3172, 0.09790, 0.1203 0.2778, 0.09440, 0.1295 0.2393, 0.08960, 0.1710 0.2056, 0.08360, 0.2175 0.1633, 0.07610, 0.3018 0.1261, 0.06710, 0.4078 0.0900, 0.05640, 0.5517 0.0571, 0.04390, 0.7381 0.0283, 0.02940, 0.9462 0.0142, 0.01970, 1.0029 0.0081, 0.01410, 0.9114 0.0026, 0.00780, 0.3558 0.0000, 0.00000, -1.6337 0.0037, -0.00840, -2.5327 0.0112, -0.01420, -2.0392 0.0191, -0.01930, -1.9601 0.0397, -0.03030, -1.1452 0.0706, -0.04420, -1.0934 0.1037, -0.05710, -1.1011 0.1384, -0.06890, -1.1225 0.1741, -0.07950, -1.1449 0.2102, -0.08660, -1.1884 0.2472, -0.09640, -1.2405 0.2844, -0.10270, -1.2505 0.3225, -0.10690, -1.2186 0.3608, -0.10890, -1.1589 0.3991, -0.10830, -1.0230 0.4373, -0.10510, -0.7787 0.4757, -0.09890, -0.5006 0.5137, -0.09067, -0.3492 0.5611, -0.07859, -0.3340 16 Flap element taps 1.0000, 0.00130, -0.5246 0.9365, 0.01390, -0.4839 0.8333, 0.03280, -0.4912 0.7436, 0.04930, -0.4832 0.7049, 0.05667, -0.4819 0.6662, 0.06411, -0.4830 0.6274, 0.07172, -0.4773 0.6009, 0.07523, -0.4806 0.6069, 0.02889, 0.9870 0.6079, -0.01747, -0.1092 0.6167, -0.06381, -0.6820 0.6558, -0.05300, -0.7057 0.7045, -0.04117, -0.7153 0.7429, -0.03210, -0.7282 0.8333, -0.01400, -0.6962 0.9311, -0.00120, -0.3691 --------- Run Conditions: vel=106.0 ft/s Re=1.004x10^6 AOA=-0.02 Flap deflection=20.00 Totals: Cl=-0.1234 Cdp=0.1291 Cm(c/4)=-0.0671 Cs=-0.1291 Ch=0.0055 Main component: Cl=-0.2839 Cdp=-0.0306 Cm=0.0896 Flap component: Cl=0.1605 Cdp=0.1597 Cm=-0.1259 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.3229 0.5905, -0.01667, -0.0657 0.5709, 0.03110, 0.2593 0.5889, 0.07933, 0.2221 0.5500, 0.08689, 0.4594 0.5110, 0.09367, 0.2740 0.4731, 0.09830, -0.0580 0.4349, 0.10070, -0.0937 0.3960, 0.10120, -0.1338 0.3566, 0.10020, -0.1736 0.3172, 0.09790, -0.1890 0.2778, 0.09440, -0.2204 0.2393, 0.08960, -0.2194 0.2056, 0.08360, -0.2122 0.1633, 0.07610, -0.1762 0.1261, 0.06710, -0.1108 0.0900, 0.05640, -0.0204 0.0571, 0.04390, 0.1236 0.0283, 0.02940, 0.3544 0.0142, 0.01970, 0.5998 0.0081, 0.01410, 0.7477 0.0026, 0.00780, 0.9383 0.0000, 0.00000, 0.9084 0.0037, -0.00840, 0.2746 0.0112, -0.01420, 0.0840 0.0191, -0.01930, 0.0203 0.0397, -0.03030, -0.0669 0.0706, -0.04420, -0.2069 0.1037, -0.05710, -0.3343 0.1384, -0.06890, -0.4447 0.1741, -0.07950, -0.5470 0.2102, -0.08660, -0.6458 0.2472, -0.09640, -0.7495 0.2844, -0.10270, -0.8215 0.3225, -0.10690, -0.8615 0.3608, -0.10890, -0.8748 0.3991, -0.10830, -0.8333 0.4373, -0.10510, -0.7527 0.4757, -0.09890, -0.7379 0.5137, -0.09067, -0.1734 0.5611, -0.07859, 0.0435 16 Flap element taps 1.0000, 0.00130, -0.7044 0.9365, 0.01390, -0.6866 0.8333, 0.03280, -0.6895 0.7436, 0.04930, -0.6770 0.7049, 0.05667, -0.6738 0.6662, 0.06411, -0.6750 0.6274, 0.07172, -0.6686 0.6009, 0.07523, -0.6756 0.6069, 0.02889, 0.9820 0.6079, -0.01747, 0.1890 0.6167, -0.06381, -0.2293 0.6558, -0.05300, -0.2507 0.7045, -0.04117, -0.2635 0.7429, -0.03210, -0.2575 0.8333, -0.01400, -0.0207 0.9311, -0.00120, 0.0147 --------- Run Conditions: vel=106.0 ft/s Re=1.003x10^6 AOA=2.98 Flap deflection=20.00 Totals: Cl=0.1266 Cdp=0.1408 Cm(c/4)=-0.0702 Cs=-0.1340 Ch=0.0105 Main component: Cl=-0.0510 Cdp=-0.0395 Cm=0.0424 Flap component: Cl=0.1776 Cdp=0.1803 Cm=-0.1460 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.3585 0.5905, -0.01667, -0.0216 0.5709, 0.03110, 0.2898 0.5889, 0.07933, 0.2718 0.5500, 0.08689, 0.4264 0.5110, 0.09367, 0.2249 0.4731, 0.09830, 0.0527 0.4349, 0.10070, -0.2255 0.3960, 0.10120, -0.2396 0.3566, 0.10020, -0.2996 0.3172, 0.09790, -0.3296 0.2778, 0.09440, -0.3831 0.2393, 0.08960, -0.4041 0.2056, 0.08360, -0.4102 0.1633, 0.07610, -0.4210 0.1261, 0.06710, -0.3823 0.0900, 0.05640, -0.3459 0.0571, 0.04390, -0.2620 0.0283, 0.02940, -0.1136 0.0142, 0.01970, 0.0908 0.0081, 0.01410, 0.2496 0.0026, 0.00780, 0.5052 0.0000, 0.00000, 0.9393 0.0037, -0.00840, 0.8527 0.0112, -0.01420, 0.6341 0.0191, -0.01930, 0.5103 0.0397, -0.03030, 0.3301 0.0706, -0.04420, 0.1375 0.1037, -0.05710, -0.0174 0.1384, -0.06890, -0.1688 0.1741, -0.07950, -0.2891 0.2102, -0.08660, -0.3907 0.2472, -0.09640, -0.5152 0.2844, -0.10270, -0.5968 0.3225, -0.10690, -0.6692 0.3608, -0.10890, -0.6929 0.3991, -0.10830, -0.6842 0.4373, -0.10510, -0.5909 0.4757, -0.09890, -0.5652 0.5137, -0.09067, -0.1083 0.5611, -0.07859, 0.0944 16 Flap element taps 1.0000, 0.00130, -0.7292 0.9365, 0.01390, -0.7162 0.8333, 0.03280, -0.7173 0.7436, 0.04930, -0.7084 0.7049, 0.05667, -0.7078 0.6662, 0.06411, -0.7043 0.6274, 0.07172, -0.7021 0.6009, 0.07523, -0.7070 0.6069, 0.02889, 0.9858 0.6079, -0.01747, 0.2297 0.6167, -0.06381, -0.1742 0.6558, -0.05300, -0.1946 0.7045, -0.04117, -0.2107 0.7429, -0.03210, -0.2007 0.8333, -0.01400, 0.0410 0.9311, -0.00120, 0.0362 --------- Run Conditions: vel=106.0 ft/s Re=1.003x10^6 AOA=6.00 Flap deflection=20.00 Totals: Cl=0.3902 Cdp=0.1558 Cm(c/4)=-0.0778 Cs=-0.1142 Ch=0.0146 Main component: Cl=0.1833 Cdp=-0.0510 Cm=-0.0012 Flap component: Cl=0.2069 Cdp=0.2068 Cm=-0.1777 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.3634 0.5905, -0.01667, 0.0369 0.5709, 0.03110, 0.3687 0.5889, 0.07933, 0.3611 0.5500, 0.08689, 0.3493 0.5110, 0.09367, 0.1928 0.4731, 0.09830, -0.0263 0.4349, 0.10070, -0.1927 0.3960, 0.10120, -0.2886 0.3566, 0.10020, -0.4649 0.3172, 0.09790, -0.5048 0.2778, 0.09440, -0.5704 0.2393, 0.08960, -0.6123 0.2056, 0.08360, -0.6394 0.1633, 0.07610, -0.7024 0.1261, 0.06710, -0.7015 0.0900, 0.05640, -0.7370 0.0571, 0.04390, -0.7459 0.0283, 0.02940, -0.7453 0.0142, 0.01970, -0.6798 0.0081, 0.01410, -0.6045 0.0026, 0.00780, -0.4034 0.0000, 0.00000, 0.1898 0.0037, -0.00840, 0.9774 0.0112, -0.01420, 0.9409 0.0191, -0.01930, 0.8413 0.0397, -0.03030, 0.6495 0.0706, -0.04420, 0.4404 0.1037, -0.05710, 0.2720 0.1384, -0.06890, 0.0895 0.1741, -0.07950, -0.0389 0.2102, -0.08660, -0.1386 0.2472, -0.09640, -0.2804 0.2844, -0.10270, -0.3719 0.3225, -0.10690, -0.4713 0.3608, -0.10890, -0.5067 0.3991, -0.10830, -0.5298 0.4373, -0.10510, -0.4405 0.4757, -0.09890, -0.3978 0.5137, -0.09067, -0.3054 0.5611, -0.07859, 0.1357 16 Flap element taps 1.0000, 0.00130, -0.7559 0.9365, 0.01390, -0.7480 0.8333, 0.03280, -0.7511 0.7436, 0.04930, -0.7426 0.7049, 0.05667, -0.7430 0.6662, 0.06411, -0.7336 0.6274, 0.07172, -0.7338 0.6009, 0.07523, -0.7434 0.6069, 0.02889, 0.9284 0.6079, -0.01747, 0.3042 0.6167, -0.06381, -0.0962 0.6558, -0.05300, -0.1198 0.7045, -0.04117, -0.1365 0.7429, -0.03210, -0.0995 0.8333, -0.01400, 0.1713 0.9311, -0.00120, 0.0774 --------- Run Conditions: vel=106.5 ft/s Re=1.006x10^6 AOA=9.01 Flap deflection=20.00 Totals: Cl=0.6516 Cdp=0.1546 Cm(c/4)=-0.1049 Cs=-0.0506 Ch=0.0244 Main component: Cl=0.3746 Cdp=-0.0398 Cm=-0.0340 Flap component: Cl=0.2771 Cdp=0.1943 Cm=-0.2379 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.1587 0.5905, -0.01667, 0.1870 0.5709, 0.03110, 0.1664 0.5889, 0.07933, 0.1022 0.5500, 0.08689, 0.1217 0.5110, 0.09367, 0.1045 0.4731, 0.09830, 0.0434 0.4349, 0.10070, -0.1455 0.3960, 0.10120, -0.2901 0.3566, 0.10020, -0.4760 0.3172, 0.09790, -0.5611 0.2778, 0.09440, -0.6755 0.2393, 0.08960, -0.7632 0.2056, 0.08360, -0.8171 0.1633, 0.07610, -0.9512 0.1261, 0.06710, -1.0122 0.0900, 0.05640, -1.1237 0.0571, 0.04390, -1.2459 0.0283, 0.02940, -1.4369 0.0142, 0.01970, -1.5706 0.0081, 0.01410, -1.7248 0.0026, 0.00780, -1.6578 0.0000, 0.00000, -1.2925 0.0037, -0.00840, 0.7258 0.0112, -0.01420, 0.9875 0.0191, -0.01930, 0.9786 0.0397, -0.03030, 0.8489 0.0706, -0.04420, 0.6588 0.1037, -0.05710, 0.4957 0.1384, -0.06890, 0.2988 0.1741, -0.07950, 0.1675 0.2102, -0.08660, 0.0660 0.2472, -0.09640, -0.0889 0.2844, -0.10270, -0.1900 0.3225, -0.10690, -0.3140 0.3608, -0.10890, -0.3666 0.3991, -0.10830, -0.4252 0.4373, -0.10510, -0.3697 0.4757, -0.09890, -0.2995 0.5137, -0.09067, -0.2670 0.5611, -0.07859, 0.0924 16 Flap element taps 1.0000, 0.00130, -0.6522 0.9365, 0.01390, -0.6828 0.8333, 0.03280, -0.6832 0.7436, 0.04930, -0.6728 0.7049, 0.05667, -0.6771 0.6662, 0.06411, -0.6660 0.6274, 0.07172, -0.6657 0.6009, 0.07523, -0.7018 0.6069, 0.02889, 0.1339 0.6079, -0.01747, 0.1452 0.6167, -0.06381, 0.1712 0.6558, -0.05300, 0.1665 0.7045, -0.04117, 0.1482 0.7429, -0.03210, 0.2241 0.8333, -0.01400, 0.4538 0.9311, -0.00120, 0.1822 --------- Run Conditions: vel=106.2 ft/s Re=1.003x10^6 AOA=11.97 Flap deflection=20.00 Totals: Cl=0.8910 Cdp=0.1739 Cm(c/4)=-0.1183 Cs=0.0146 Ch=0.0194 Main component: Cl=0.5907 Cdp=-0.0236 Cm=-0.0818 Flap component: Cl=0.3003 Cdp=0.1975 Cm=-0.2633 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.1442 0.5905, -0.01667, 0.1921 0.5709, 0.03110, -0.0066 0.5889, 0.07933, -0.1090 0.5500, 0.08689, -0.1025 0.5110, 0.09367, -0.1167 0.4731, 0.09830, -0.1236 0.4349, 0.10070, -0.1766 0.3960, 0.10120, -0.2729 0.3566, 0.10020, -0.4977 0.3172, 0.09790, -0.6278 0.2778, 0.09440, -0.7854 0.2393, 0.08960, -0.9087 0.2056, 0.08360, -1.0036 0.1633, 0.07610, -1.1827 0.1261, 0.06710, -1.2817 0.0900, 0.05640, -1.4893 0.0571, 0.04390, -1.7228 0.0283, 0.02940, -2.1301 0.0142, 0.01970, -2.6872 0.0081, 0.01410, -3.0708 0.0026, 0.00780, -3.2958 0.0000, 0.00000, -3.4106 0.0037, -0.00840, 0.1204 0.0112, -0.01420, 0.8519 0.0191, -0.01930, 0.9810 0.0397, -0.03030, 0.9652 0.0706, -0.04420, 0.8255 0.1037, -0.05710, 0.6820 0.1384, -0.06890, 0.4834 0.1741, -0.07950, 0.3536 0.2102, -0.08660, 0.2579 0.2472, -0.09640, 0.0977 0.2844, -0.10270, -0.0093 0.3225, -0.10690, -0.1465 0.3608, -0.10890, -0.2105 0.3991, -0.10830, -0.2906 0.4373, -0.10510, -0.2565 0.4757, -0.09890, -0.1946 0.5137, -0.09067, -0.1445 0.5611, -0.07859, 0.1337 16 Flap element taps 1.0000, 0.00130, -0.6396 0.9365, 0.01390, -0.6695 0.8333, 0.03280, -0.6654 0.7436, 0.04930, -0.6589 0.7049, 0.05667, -0.6619 0.6662, 0.06411, -0.6470 0.6274, 0.07172, -0.6525 0.6009, 0.07523, -0.6973 0.6069, 0.02889, -0.0796 0.6079, -0.01747, -0.0329 0.6167, -0.06381, 0.0661 0.6558, -0.05300, 0.0938 0.7045, -0.04117, 0.1700 0.7429, -0.03210, 0.5881 0.8333, -0.01400, 0.5402 0.9311, -0.00120, 0.2188 --------- Run Conditions: vel=106.6 ft/s Re=1.009x10^6 AOA=15.00 Flap deflection=20.00 Totals: Cl=1.0811 Cdp=0.1915 Cm(c/4)=-0.1210 Cs=0.0948 Ch=0.0203 Main component: Cl=0.7777 Cdp=-0.0003 Cm=-0.1245 Flap component: Cl=0.3034 Cdp=0.1919 Cm=-0.2699 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.1590 0.5905, -0.01667, 0.2355 0.5709, 0.03110, -0.1393 0.5889, 0.07933, -0.3336 0.5500, 0.08689, -0.3233 0.5110, 0.09367, -0.3317 0.4731, 0.09830, -0.3221 0.4349, 0.10070, -0.3356 0.3960, 0.10120, -0.3678 0.3566, 0.10020, -0.4630 0.3172, 0.09790, -0.6102 0.2778, 0.09440, -0.7982 0.2393, 0.08960, -0.9779 0.2056, 0.08360, -1.1461 0.1633, 0.07610, -1.3271 0.1261, 0.06710, -1.5189 0.0900, 0.05640, -1.7885 0.0571, 0.04390, -2.1756 0.0283, 0.02940, -2.8219 0.0142, 0.01970, -3.4712 0.0081, 0.01410, -4.6304 0.0026, 0.00780, -5.1404 0.0000, 0.00000, -5.8148 0.0037, -0.00840, -0.7148 0.0112, -0.01420, 0.5564 0.0191, -0.01930, 0.8767 0.0397, -0.03030, 1.0084 0.0706, -0.04420, 0.9244 0.1037, -0.05710, 0.8083 0.1384, -0.06890, 0.6635 0.1741, -0.07950, 0.5328 0.2102, -0.08660, 0.4049 0.2472, -0.09640, 0.2651 0.2844, -0.10270, 0.1471 0.3225, -0.10690, 0.0347 0.3608, -0.10890, -0.0690 0.3991, -0.10830, -0.1398 0.4373, -0.10510, -0.1424 0.4757, -0.09890, -0.1018 0.5137, -0.09067, -0.0421 0.5611, -0.07859, 0.0948 16 Flap element taps 1.0000, 0.00130, -0.5785 0.9365, 0.01390, -0.6003 0.8333, 0.03280, -0.5999 0.7436, 0.04930, -0.5931 0.7049, 0.05667, -0.5934 0.6662, 0.06411, -0.5951 0.6274, 0.07172, -0.5869 0.6009, 0.07523, -0.6155 0.6069, 0.02889, -0.2798 0.6079, -0.01747, -0.1774 0.6167, -0.06381, -0.0017 0.6558, -0.05300, 0.0552 0.7045, -0.04117, 0.3580 0.7429, -0.03210, 0.8396 0.8333, -0.01400, 0.5439 0.9311, -0.00120, 0.2560 --------- Run Conditions: vel=105.6 ft/s Re=0.997x10^6 AOA=17.96 Flap deflection=20.00 Totals: Cl=0.8430 Cdp=0.3998 Cm(c/4)=-0.1934 Cs=-0.1203 Ch=0.0192 Main component: Cl=0.5140 Cdp=0.2139 Cm=-0.1323 Flap component: Cl=0.3290 Cdp=0.1859 Cm=-0.2924 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0246 0.5905, -0.01667, 0.1150 0.5709, 0.03110, -0.5334 0.5889, 0.07933, -0.8782 0.5500, 0.08689, -0.9111 0.5110, 0.09367, -0.8734 0.4731, 0.09830, -0.7405 0.4349, 0.10070, -0.7148 0.3960, 0.10120, -0.7514 0.3566, 0.10020, -0.7678 0.3172, 0.09790, -0.7612 0.2778, 0.09440, -0.7634 0.2393, 0.08960, -0.7533 0.2056, 0.08360, -0.7481 0.1633, 0.07610, -0.7433 0.1261, 0.06710, -0.7441 0.0900, 0.05640, -0.7310 0.0571, 0.04390, -0.7405 0.0283, 0.02940, -0.7590 0.0142, 0.01970, -0.7662 0.0081, 0.01410, -0.7747 0.0026, 0.00780, -0.7613 0.0000, 0.00000, -1.0486 0.0037, -0.00840, 0.5317 0.0112, -0.01420, 0.9286 0.0191, -0.01930, 1.0016 0.0397, -0.03030, 0.9739 0.0706, -0.04420, 0.8348 0.1037, -0.05710, 0.7069 0.1384, -0.06890, 0.5647 0.1741, -0.07950, 0.4336 0.2102, -0.08660, 0.2989 0.2472, -0.09640, 0.1602 0.2844, -0.10270, 0.0383 0.3225, -0.10690, -0.0694 0.3608, -0.10890, -0.1787 0.3991, -0.10830, -0.2484 0.4373, -0.10510, -0.2521 0.4757, -0.09890, -0.2088 0.5137, -0.09067, -0.1445 0.5611, -0.07859, 0.0063 16 Flap element taps 1.0000, 0.00130, -0.6396 0.9365, 0.01390, -0.6642 0.8333, 0.03280, -0.6772 0.7436, 0.04930, -0.6771 0.7049, 0.05667, -0.6757 0.6662, 0.06411, -0.6774 0.6274, 0.07172, -0.6644 0.6009, 0.07523, -0.6743 0.6069, 0.02889, -0.7239 0.6079, -0.01747, -0.5775 0.6167, -0.06381, -0.2367 0.6558, -0.05300, -0.1231 0.7045, -0.04117, 0.5820 0.7429, -0.03210, 0.8727 0.8333, -0.01400, 0.5041 0.9311, -0.00120, 0.2129 --------- Run Conditions: vel=105.3 ft/s Re=0.995x10^6 AOA=19.96 Flap deflection=20.00 Totals: Cl=0.8652 Cdp=0.4543 Cm(c/4)=-0.2043 Cs=-0.1317 Ch=0.0227 Main component: Cl=0.5294 Cdp=0.2469 Cm=-0.1416 Flap component: Cl=0.3358 Cdp=0.2074 Cm=-0.3048 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0128 0.5905, -0.01667, 0.1196 0.5709, 0.03110, -0.5538 0.5889, 0.07933, -0.9037 0.5500, 0.08689, -0.9239 0.5110, 0.09367, -0.9402 0.4731, 0.09830, -0.8434 0.4349, 0.10070, -0.7561 0.3960, 0.10120, -0.7501 0.3566, 0.10020, -0.7429 0.3172, 0.09790, -0.7509 0.2778, 0.09440, -0.7609 0.2393, 0.08960, -0.7536 0.2056, 0.08360, -0.7594 0.1633, 0.07610, -0.7359 0.1261, 0.06710, -0.7415 0.0900, 0.05640, -0.7224 0.0571, 0.04390, -0.7268 0.0283, 0.02940, -0.7432 0.0142, 0.01970, -0.7546 0.0081, 0.01410, -0.7706 0.0026, 0.00780, -0.7416 0.0000, 0.00000, -1.0097 0.0037, -0.00840, 0.4613 0.0112, -0.01420, 0.8985 0.0191, -0.01930, 0.9958 0.0397, -0.03030, 0.9954 0.0706, -0.04420, 0.8676 0.1037, -0.05710, 0.7481 0.1384, -0.06890, 0.6269 0.1741, -0.07950, 0.4950 0.2102, -0.08660, 0.3487 0.2472, -0.09640, 0.2170 0.2844, -0.10270, 0.0888 0.3225, -0.10690, -0.0094 0.3608, -0.10890, -0.1332 0.3991, -0.10830, -0.2012 0.4373, -0.10510, -0.2183 0.4757, -0.09890, -0.1828 0.5137, -0.09067, -0.1177 0.5611, -0.07859, -0.0087 16 Flap element taps 1.0000, 0.00130, -0.6865 0.9365, 0.01390, -0.7057 0.8333, 0.03280, -0.7208 0.7436, 0.04930, -0.7198 0.7049, 0.05667, -0.7218 0.6662, 0.06411, -0.7267 0.6274, 0.07172, -0.7107 0.6009, 0.07523, -0.7206 0.6069, 0.02889, -0.7491 0.6079, -0.01747, -0.6028 0.6167, -0.06381, -0.2581 0.6558, -0.05300, -0.1304 0.7045, -0.04117, 0.6370 0.7429, -0.03210, 0.8795 0.8333, -0.01400, 0.5011 0.9311, -0.00120, 0.2064 --------- Run Conditions: vel=104.6 ft/s Re=0.986x10^6 AOA=24.01 Flap deflection=20.00 Totals: Cl=1.0092 Cdp=0.6070 Cm(c/4)=-0.2413 Cs=-0.1438 Ch=0.0342 Main component: Cl=0.6418 Cdp=0.3331 Cm=-0.1824 Flap component: Cl=0.3673 Cdp=0.2739 Cm=-0.3511 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0277 0.5905, -0.01667, 0.1933 0.5709, 0.03110, -0.6017 0.5889, 0.07933, -1.0220 0.5500, 0.08689, -1.0000 0.5110, 0.09367, -1.0319 0.4731, 0.09830, -1.0171 0.4349, 0.10070, -0.9839 0.3960, 0.10120, -0.9585 0.3566, 0.10020, -0.8930 0.3172, 0.09790, -0.8921 0.2778, 0.09440, -0.9082 0.2393, 0.08960, -0.9094 0.2056, 0.08360, -0.9298 0.1633, 0.07610, -0.8950 0.1261, 0.06710, -0.9115 0.0900, 0.05640, -0.8873 0.0571, 0.04390, -0.8908 0.0283, 0.02940, -0.8959 0.0142, 0.01970, -0.9038 0.0081, 0.01410, -0.9343 0.0026, 0.00780, -0.8972 0.0000, 0.00000, -0.9506 0.0037, -0.00840, 0.1758 0.0112, -0.01420, 0.7658 0.0191, -0.01930, 0.9411 0.0397, -0.03030, 1.0180 0.0706, -0.04420, 0.9371 0.1037, -0.05710, 0.8451 0.1384, -0.06890, 0.7517 0.1741, -0.07950, 0.6273 0.2102, -0.08660, 0.4777 0.2472, -0.09640, 0.3544 0.2844, -0.10270, 0.2212 0.3225, -0.10690, 0.1277 0.3608, -0.10890, -0.0117 0.3991, -0.10830, -0.0858 0.4373, -0.10510, -0.1266 0.4757, -0.09890, -0.1151 0.5137, -0.09067, -0.0518 0.5611, -0.07859, 0.0116 16 Flap element taps 1.0000, 0.00130, -0.8652 0.9365, 0.01390, -0.8843 0.8333, 0.03280, -0.9001 0.7436, 0.04930, -0.8967 0.7049, 0.05667, -0.8970 0.6662, 0.06411, -0.9020 0.6274, 0.07172, -0.8831 0.6009, 0.07523, -0.8936 0.6069, 0.02889, -0.8601 0.6079, -0.01747, -0.6922 0.6167, -0.06381, -0.2932 0.6558, -0.05300, -0.1496 0.7045, -0.04117, 0.8189 0.7429, -0.03210, 0.8573 0.8333, -0.01400, 0.4879 0.9311, -0.00120, 0.1712 --------- Run Conditions: vel=104.6 ft/s Re=0.987x10^6 AOA=27.00 Flap deflection=20.00 Totals: Cl=1.1614 Cdp=0.7670 Cm(c/4)=-0.2837 Cs=-0.1562 Ch=0.0445 Main component: Cl=0.7586 Cdp=0.4301 Cm=-0.2283 Flap component: Cl=0.4028 Cdp=0.3370 Cm=-0.4012 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0154 0.5905, -0.01667, 0.1922 0.5709, 0.03110, -0.7457 0.5889, 0.07933, -1.2017 0.5500, 0.08689, -1.1755 0.5110, 0.09367, -1.2076 0.4731, 0.09830, -1.2042 0.4349, 0.10070, -1.1953 0.3960, 0.10120, -1.1927 0.3566, 0.10020, -1.1017 0.3172, 0.09790, -1.0852 0.2778, 0.09440, -1.0940 0.2393, 0.08960, -1.0939 0.2056, 0.08360, -1.1256 0.1633, 0.07610, -1.0828 0.1261, 0.06710, -1.1062 0.0900, 0.05640, -1.0767 0.0571, 0.04390, -1.0802 0.0283, 0.02940, -1.0835 0.0142, 0.01970, -1.0881 0.0081, 0.01410, -1.1264 0.0026, 0.00780, -1.0784 0.0000, 0.00000, -1.1001 0.0037, -0.00840, -0.1161 0.0112, -0.01420, 0.6106 0.0191, -0.01930, 0.8570 0.0397, -0.03030, 1.0120 0.0706, -0.04420, 0.9718 0.1037, -0.05710, 0.9048 0.1384, -0.06890, 0.8379 0.1741, -0.07950, 0.7213 0.2102, -0.08660, 0.5696 0.2472, -0.09640, 0.4590 0.2844, -0.10270, 0.3207 0.3225, -0.10690, 0.2355 0.3608, -0.10890, 0.0861 0.3991, -0.10830, 0.0082 0.4373, -0.10510, -0.0523 0.4757, -0.09890, -0.0583 0.5137, -0.09067, 0.0012 0.5611, -0.07859, 0.0659 16 Flap element taps 1.0000, 0.00130, -1.0581 0.9365, 0.01390, -1.0709 0.8333, 0.03280, -1.0904 0.7436, 0.04930, -1.0901 0.7049, 0.05667, -1.0933 0.6662, 0.06411, -1.1029 0.6274, 0.07172, -1.0819 0.6009, 0.07523, -1.0898 0.6069, 0.02889, -1.0252 0.6079, -0.01747, -0.8472 0.6167, -0.06381, -0.3609 0.6558, -0.05300, -0.1828 0.7045, -0.04117, 0.9514 0.7429, -0.03210, 0.8450 0.8333, -0.01400, 0.4784 0.9311, -0.00120, 0.1389