S809 VENTED AILERON MODEL, 18 IN CHORD --------- Run Conditions: vel=107.7 ft/s Re=1.011x10^6 AOA=-6.00 Flap deflection=0.00 Totals: Cl=-0.4246 Cdp=0.0293 Cm(c/4)=0.0024 Cs=0.0152 Ch=0.0029 Main component: Cl=-0.3787 Cdp=0.0324 Cm=0.0719 Flap component: Cl=-0.0458 Cdp=-0.0031 Cm=0.0368 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1878 0.5871, 0.07930, -0.2179 0.5501, 0.08690, -0.2679 0.5112, 0.09370, -0.4181 0.4731, 0.09830, -0.4891 0.4349, 0.10070, -0.4672 0.3960, 0.10120, -0.4133 0.3566, 0.10020, -0.3446 0.3172, 0.09790, -0.2796 0.2778, 0.09440, -0.2271 0.2393, 0.08960, -0.1760 0.2056, 0.08360, -0.1002 0.1633, 0.07610, -0.0008 0.1261, 0.06710, 0.1257 0.0900, 0.05640, 0.2547 0.0571, 0.04390, 0.4725 0.0283, 0.02940, 0.7566 0.0142, 0.01970, 0.9473 0.0081, 0.01410, 1.0015 0.0026, 0.00780, 0.7771 0.0000, 0.00000, -0.1847 0.0037, -0.00840, -1.0591 0.0112, -0.01420, -1.2966 0.0191, -0.01930, -0.8057 0.0397, -0.03030, -0.7254 0.0706, -0.04420, -0.7167 0.1037, -0.05710, -0.7273 0.1384, -0.06890, -0.7975 0.1741, -0.07950, -0.8428 0.2102, -0.08660, -0.9232 0.2472, -0.09640, -1.0044 0.2844, -0.10270, -1.0212 0.3225, -0.10690, -1.0196 0.3608, -0.10890, -1.0055 0.3991, -0.10830, -0.9068 0.4373, -0.10510, -0.7492 0.4757, -0.09890, -0.5113 0.5137, -0.09070, -0.3094 0.5514, -0.08120, -0.2151 0.5917, -0.06870, -0.1767 0.5917, -0.02380, -0.1851 0.5917, 0.02120, -0.1806 16 Flap element taps 1.0000, 0.00130, -0.0442 0.9365, 0.01390, -0.0156 0.8333, 0.03280, -0.0234 0.7436, 0.04930, -0.0470 0.7049, 0.05670, -0.0379 0.6667, 0.05450, -0.1259 0.6302, 0.03770, -0.1838 0.6083, 0.01980, -0.1689 0.6000, 0.00000, -0.1838 0.6076, -0.01900, -0.1921 0.6285, -0.03060, -0.1843 0.6667, -0.04090, -0.1867 0.7046, -0.04120, -0.1824 0.7429, -0.03210, -0.1893 0.8333, -0.01400, -0.1910 0.9311, -0.00120, -0.1617 --------- Run Conditions: vel=107.7 ft/s Re=1.010x10^6 AOA=0.00 Flap deflection=0.00 Totals: Cl=0.0221 Cdp=0.0091 Cm(c/4)=-0.0179 Cs=-0.0091 Ch=-0.0020 Main component: Cl=-0.0196 Cdp=0.0338 Cm=0.0107 Flap component: Cl=0.0416 Cdp=-0.0247 Cm=-0.0341 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1859 0.5871, 0.07930, -0.2660 0.5501, 0.08690, -0.3523 0.5112, 0.09370, -0.5323 0.4731, 0.09830, -0.6472 0.4349, 0.10070, -0.6621 0.3960, 0.10120, -0.6541 0.3566, 0.10020, -0.6026 0.3172, 0.09790, -0.5649 0.2778, 0.09440, -0.5469 0.2393, 0.08960, -0.5346 0.2056, 0.08360, -0.5091 0.1633, 0.07610, -0.4395 0.1261, 0.06710, -0.3677 0.0900, 0.05640, -0.3119 0.0571, 0.04390, -0.1698 0.0283, 0.02940, 0.0703 0.0142, 0.01970, 0.2896 0.0081, 0.01410, 0.4374 0.0026, 0.00780, 0.6897 0.0000, 0.00000, 1.0168 0.0037, -0.00840, 0.6462 0.0112, -0.01420, 0.2579 0.0191, -0.01930, 0.2892 0.0397, -0.03030, 0.1144 0.0706, -0.04420, -0.0554 0.1037, -0.05710, -0.1697 0.1384, -0.06890, -0.3009 0.1741, -0.07950, -0.4083 0.2102, -0.08660, -0.5488 0.2472, -0.09640, -0.6754 0.2844, -0.10270, -0.7552 0.3225, -0.10690, -0.8040 0.3608, -0.10890, -0.8706 0.3991, -0.10830, -0.8475 0.4373, -0.10510, -0.7913 0.4757, -0.09890, -0.6488 0.5137, -0.09070, -0.5013 0.5514, -0.08120, -0.3161 0.5917, -0.06870, -0.1757 0.5917, -0.02380, -0.1856 0.5917, 0.02120, -0.1901 16 Flap element taps 1.0000, 0.00130, 0.1749 0.9365, 0.01390, 0.1014 0.8333, 0.03280, 0.0127 0.7436, 0.04930, -0.0763 0.7049, 0.05670, -0.1134 0.6667, 0.05450, -0.1899 0.6302, 0.03770, -0.1856 0.6083, 0.01980, -0.1796 0.6000, 0.00000, -0.1841 0.6076, -0.01900, -0.1974 0.6285, -0.03060, -0.2005 0.6667, -0.04090, -0.0926 0.7046, -0.04120, 0.0111 0.7429, -0.03210, 0.0553 0.8333, -0.01400, 0.1642 0.9311, -0.00120, 0.2293 Wake drag found for this condition, Cdw=0.0149 --------- Run Conditions: vel=107.7 ft/s Re=1.010x10^6 AOA=3.04 Flap deflection=0.00 Totals: Cl=0.2978 Cdp=0.0116 Cm(c/4)=-0.0226 Cs=0.0042 Ch=0.0029 Main component: Cl=0.2266 Cdp=0.0302 Cm=-0.0408 Flap component: Cl=0.0712 Cdp=-0.0186 Cm=-0.0563 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1880 0.5871, 0.07930, -0.2814 0.5501, 0.08690, -0.3932 0.5112, 0.09370, -0.5878 0.4731, 0.09830, -0.7323 0.4349, 0.10070, -0.7713 0.3960, 0.10120, -0.7932 0.3566, 0.10020, -0.7513 0.3172, 0.09790, -0.7357 0.2778, 0.09440, -0.7380 0.2393, 0.08960, -0.7529 0.2056, 0.08360, -0.7642 0.1633, 0.07610, -0.7140 0.1261, 0.06710, -0.6879 0.0900, 0.05640, -0.6896 0.0571, 0.04390, -0.6328 0.0283, 0.02940, -0.4905 0.0142, 0.01970, -0.3685 0.0081, 0.01410, -0.3258 0.0026, 0.00780, 0.0731 0.0000, 0.00000, 0.6726 0.0037, -0.00840, 0.9874 0.0112, -0.01420, 0.7631 0.0191, -0.01930, 0.6949 0.0397, -0.03030, 0.4819 0.0706, -0.04420, 0.2605 0.1037, -0.05710, 0.1159 0.1384, -0.06890, -0.0231 0.1741, -0.07950, -0.1527 0.2102, -0.08660, -0.3189 0.2472, -0.09640, -0.4459 0.2844, -0.10270, -0.5477 0.3225, -0.10690, -0.6056 0.3608, -0.10890, -0.6961 0.3991, -0.10830, -0.6964 0.4373, -0.10510, -0.6706 0.4757, -0.09890, -0.5548 0.5137, -0.09070, -0.4367 0.5514, -0.08120, -0.2740 0.5917, -0.06870, -0.1563 0.5917, -0.02380, -0.1539 0.5917, 0.02120, -0.1867 16 Flap element taps 1.0000, 0.00130, 0.1049 0.9365, 0.01390, 0.0540 0.8333, 0.03280, -0.0275 0.7436, 0.04930, -0.1273 0.7049, 0.05670, -0.1743 0.6667, 0.05450, -0.1789 0.6302, 0.03770, -0.1810 0.6083, 0.01980, -0.1752 0.6000, 0.00000, -0.1884 0.6076, -0.01900, -0.1980 0.6285, -0.03060, -0.2010 0.6667, -0.04090, 0.0863 0.7046, -0.04120, 0.0552 0.7429, -0.03210, 0.1006 0.8333, -0.01400, 0.2018 0.9311, -0.00120, 0.2407 Wake drag found for this condition, Cdw=0.0171 --------- Run Conditions: vel=107.7 ft/s Re=1.008x10^6 AOA=6.04 Flap deflection=0.00 Totals: Cl=0.5203 Cdp=0.0198 Cm(c/4)=-0.0210 Cs=0.0351 Ch=-0.0006 Main component: Cl=0.4312 Cdp=0.0252 Cm=-0.0797 Flap component: Cl=0.0890 Cdp=-0.0054 Cm=-0.0711 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1617 0.5871, 0.07930, -0.2448 0.5501, 0.08690, -0.3670 0.5112, 0.09370, -0.5713 0.4731, 0.09830, -0.7474 0.4349, 0.10070, -0.8183 0.3960, 0.10120, -0.8757 0.3566, 0.10020, -0.8540 0.3172, 0.09790, -0.8643 0.2778, 0.09440, -0.8910 0.2393, 0.08960, -0.9369 0.2056, 0.08360, -0.9862 0.1633, 0.07610, -0.9648 0.1261, 0.06710, -0.9887 0.0900, 0.05640, -1.0578 0.0571, 0.04390, -1.1003 0.0283, 0.02940, -1.1035 0.0142, 0.01970, -1.1538 0.0081, 0.01410, -1.1961 0.0026, 0.00780, -0.7728 0.0000, 0.00000, -0.3917 0.0037, -0.00840, 0.9574 0.0112, -0.01420, 0.9926 0.0191, -0.01930, 0.9245 0.0397, -0.03030, 0.7382 0.0706, -0.04420, 0.5066 0.1037, -0.05710, 0.3457 0.1384, -0.06890, 0.2065 0.1741, -0.07950, 0.0606 0.2102, -0.08660, -0.1198 0.2472, -0.09640, -0.2548 0.2844, -0.10270, -0.3719 0.3225, -0.10690, -0.4400 0.3608, -0.10890, -0.5501 0.3991, -0.10830, -0.5645 0.4373, -0.10510, -0.5600 0.4757, -0.09890, -0.4657 0.5137, -0.09070, -0.3726 0.5514, -0.08120, -0.2239 0.5917, -0.06870, -0.1306 0.5917, -0.02380, -0.1169 0.5917, 0.02120, -0.1609 16 Flap element taps 1.0000, 0.00130, -0.0264 0.9365, 0.01390, -0.0746 0.8333, 0.03280, -0.0969 0.7436, 0.04930, -0.1419 0.7049, 0.05670, -0.1512 0.6667, 0.05450, -0.1511 0.6302, 0.03770, -0.1556 0.6083, 0.01980, -0.1521 0.6000, 0.00000, -0.1688 0.6076, -0.01900, -0.1800 0.6285, -0.03060, -0.1871 0.6667, -0.04090, 0.2523 0.7046, -0.04120, 0.0227 0.7429, -0.03210, 0.1056 0.8333, -0.01400, 0.1980 0.9311, -0.00120, 0.2066 Wake drag found for this condition, Cdw=0.0226 --------- Run Conditions: vel=107.5 ft/s Re=1.005x10^6 AOA=9.01 Flap deflection=0.00 Totals: Cl=0.6977 Cdp=0.0293 Cm(c/4)=-0.0180 Cs=0.0804 Ch=0.0035 Main component: Cl=0.5865 Cdp=0.0253 Cm=-0.1030 Flap component: Cl=0.1111 Cdp=0.0039 Cm=-0.0885 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.2010 0.5871, 0.07930, -0.2349 0.5501, 0.08690, -0.3013 0.5112, 0.09370, -0.4634 0.4731, 0.09830, -0.6686 0.4349, 0.10070, -0.7858 0.3960, 0.10120, -0.8873 0.3566, 0.10020, -0.8971 0.3172, 0.09790, -0.9396 0.2778, 0.09440, -0.9942 0.2393, 0.08960, -1.0708 0.2056, 0.08360, -1.1591 0.1633, 0.07610, -1.1756 0.1261, 0.06710, -1.2506 0.0900, 0.05640, -1.3921 0.0571, 0.04390, -1.5468 0.0283, 0.02940, -1.7250 0.0142, 0.01970, -1.9932 0.0081, 0.01410, -2.1646 0.0026, 0.00780, -1.8506 0.0000, 0.00000, -1.9934 0.0037, -0.00840, 0.6157 0.0112, -0.01420, 0.9932 0.0191, -0.01930, 1.0090 0.0397, -0.03030, 0.9006 0.0706, -0.04420, 0.6905 0.1037, -0.05710, 0.5281 0.1384, -0.06890, 0.3944 0.1741, -0.07950, 0.2444 0.2102, -0.08660, 0.0558 0.2472, -0.09640, -0.0839 0.2844, -0.10270, -0.2159 0.3225, -0.10690, -0.2980 0.3608, -0.10890, -0.4209 0.3991, -0.10830, -0.4549 0.4373, -0.10510, -0.4773 0.4757, -0.09890, -0.4120 0.5137, -0.09070, -0.3414 0.5514, -0.08120, -0.2030 0.5917, -0.06870, -0.1482 0.5917, -0.02380, -0.0576 0.5917, 0.02120, -0.1979 16 Flap element taps 1.0000, 0.00130, -0.1370 0.9365, 0.01390, -0.1705 0.8333, 0.03280, -0.1592 0.7436, 0.04930, -0.1719 0.7049, 0.05670, -0.1721 0.6667, 0.05450, -0.1768 0.6302, 0.03770, -0.1828 0.6083, 0.01980, -0.1946 0.6000, 0.00000, -0.2521 0.6076, -0.01900, -0.2513 0.6285, -0.03060, -0.2646 0.6667, -0.04090, 0.5955 0.7046, -0.04120, -0.0753 0.7429, -0.03210, 0.1143 0.8333, -0.01400, 0.1935 0.9311, -0.00120, 0.1752 Wake drag found for this condition, Cdw=0.0318 --------- Run Conditions: vel=107.1 ft/s Re=0.999x10^6 AOA=12.03 Flap deflection=0.00 Totals: Cl=0.9464 Cdp=0.0367 Cm(c/4)=-0.0190 Cs=0.1614 Ch=0.0307 Main component: Cl=0.7991 Cdp=0.0559 Cm=-0.1439 Flap component: Cl=0.1473 Cdp=-0.0192 Cm=-0.1084 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.3596 0.5871, 0.07930, -0.3931 0.5501, 0.08690, -0.4257 0.5112, 0.09370, -0.5168 0.4731, 0.09830, -0.7030 0.4349, 0.10070, -0.8411 0.3960, 0.10120, -0.9739 0.3566, 0.10020, -1.0123 0.3172, 0.09790, -1.0821 0.2778, 0.09440, -1.1673 0.2393, 0.08960, -1.2769 0.2056, 0.08360, -1.4019 0.1633, 0.07610, -1.4654 0.1261, 0.06710, -1.6026 0.0900, 0.05640, -1.8298 0.0571, 0.04390, -2.1299 0.0283, 0.02940, -2.5468 0.0142, 0.01970, -3.1212 0.0081, 0.01410, -3.5476 0.0026, 0.00780, -3.3867 0.0000, 0.00000, -4.5215 0.0037, -0.00840, -0.1391 0.0112, -0.01420, 0.7912 0.0191, -0.01930, 0.9783 0.0397, -0.03030, 1.0050 0.0706, -0.04420, 0.8496 0.1037, -0.05710, 0.7043 0.1384, -0.06890, 0.5816 0.1741, -0.07950, 0.4380 0.2102, -0.08660, 0.2470 0.2472, -0.09640, 0.1077 0.2844, -0.10270, -0.0337 0.3225, -0.10690, -0.1240 0.3608, -0.10890, -0.2617 0.3991, -0.10830, -0.3131 0.4373, -0.10510, -0.3617 0.4757, -0.09890, -0.3289 0.5137, -0.09070, -0.2958 0.5514, -0.08120, -0.2417 0.5917, -0.06870, -0.5422 0.5917, -0.02380, -0.1137 0.5917, 0.02120, -0.3840 16 Flap element taps 1.0000, 0.00130, -0.0824 0.9365, 0.01390, -0.0932 0.8333, 0.03280, -0.1132 0.7436, 0.04930, -0.1932 0.7049, 0.05670, -0.2956 0.6667, 0.05450, -0.2951 0.6302, 0.03770, -0.2712 0.6083, 0.01980, -0.4339 0.6000, 0.00000, -1.2342 0.6076, -0.01900, -1.2848 0.6285, -0.03060, 0.6826 0.6667, -0.04090, 0.5163 0.7046, -0.04120, -0.0638 0.7429, -0.03210, 0.1704 0.8333, -0.01400, 0.2475 0.9311, -0.00120, 0.2233 --------- Run Conditions: vel=106.8 ft/s Re=0.997x10^6 AOA=15.01 Flap deflection=0.00 Totals: Cl=0.9926 Cdp=0.0904 Cm(c/4)=-0.0405 Cs=0.1697 Ch=0.0436 Main component: Cl=0.7886 Cdp=0.0912 Cm=-0.1339 Flap component: Cl=0.2040 Cdp=-0.0008 Cm=-0.1521 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.5357 0.5871, 0.07930, -0.5422 0.5501, 0.08690, -0.5381 0.5112, 0.09370, -0.5373 0.4731, 0.09830, -0.5662 0.4349, 0.10070, -0.6092 0.3960, 0.10120, -0.7090 0.3566, 0.10020, -0.7735 0.3172, 0.09790, -0.8797 0.2778, 0.09440, -0.9997 0.2393, 0.08960, -1.1464 0.2056, 0.08360, -1.3117 0.1633, 0.07610, -1.4267 0.1261, 0.06710, -1.6102 0.0900, 0.05640, -1.8870 0.0571, 0.04390, -2.2734 0.0283, 0.02940, -2.8313 0.0142, 0.01970, -3.5655 0.0081, 0.01410, -4.1797 0.0026, 0.00780, -4.1081 0.0000, 0.00000, -5.8628 0.0037, -0.00840, -0.6208 0.0112, -0.01420, 0.6139 0.0191, -0.01930, 0.9107 0.0397, -0.03030, 1.0207 0.0706, -0.04420, 0.9060 0.1037, -0.05710, 0.7746 0.1384, -0.06890, 0.6575 0.1741, -0.07950, 0.5150 0.2102, -0.08660, 0.3281 0.2472, -0.09640, 0.1846 0.2844, -0.10270, 0.0383 0.3225, -0.10690, -0.0613 0.3608, -0.10890, -0.2054 0.3991, -0.10830, -0.2727 0.4373, -0.10510, -0.3354 0.4757, -0.09890, -0.3146 0.5137, -0.09070, -0.2956 0.5514, -0.08120, -0.2467 0.5917, -0.06870, -0.6262 0.5917, -0.02380, -0.1925 0.5917, 0.02120, -0.5808 16 Flap element taps 1.0000, 0.00130, -0.2689 0.9365, 0.01390, -0.2928 0.8333, 0.03280, -0.3139 0.7436, 0.04930, -0.3849 0.7049, 0.05670, -0.5133 0.6667, 0.05450, -0.5393 0.6302, 0.03770, -0.4392 0.6083, 0.01980, -0.6753 0.6000, 0.00000, -1.5092 0.6076, -0.01900, -1.4533 0.6285, -0.03060, 0.7328 0.6667, -0.04090, 0.5009 0.7046, -0.04120, -0.1005 0.7429, -0.03210, 0.1329 0.8333, -0.01400, 0.1945 0.9311, -0.00120, 0.1409 --------- Run Conditions: vel=107.2 ft/s Re=1.001x10^6 AOA=18.00 Flap deflection=0.00 Totals: Cl=0.8041 Cdp=0.1787 Cm(c/4)=-0.0714 Cs=0.0785 Ch=0.0452 Main component: Cl=0.5752 Cdp=0.1602 Cm=-0.1032 Flap component: Cl=0.2288 Cdp=0.0185 Cm=-0.1732 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.6424 0.5871, 0.07930, -0.6290 0.5501, 0.08690, -0.6308 0.5112, 0.09370, -0.6372 0.4731, 0.09830, -0.6564 0.4349, 0.10070, -0.6567 0.3960, 0.10120, -0.6951 0.3566, 0.10020, -0.6709 0.3172, 0.09790, -0.6825 0.2778, 0.09440, -0.6917 0.2393, 0.08960, -0.7174 0.2056, 0.08360, -0.7719 0.1633, 0.07610, -0.8057 0.1261, 0.06710, -0.9470 0.0900, 0.05640, -1.1541 0.0571, 0.04390, -1.5411 0.0283, 0.02940, -2.1236 0.0142, 0.01970, -2.8082 0.0081, 0.01410, -3.3802 0.0026, 0.00780, -3.4008 0.0000, 0.00000, -4.9155 0.0037, -0.00840, -0.3986 0.0112, -0.01420, 0.6738 0.0191, -0.01930, 0.9280 0.0397, -0.03030, 1.0185 0.0706, -0.04420, 0.9034 0.1037, -0.05710, 0.7733 0.1384, -0.06890, 0.6526 0.1741, -0.07950, 0.5132 0.2102, -0.08660, 0.3211 0.2472, -0.09640, 0.1729 0.2844, -0.10270, 0.0218 0.3225, -0.10690, -0.0887 0.3608, -0.10890, -0.2414 0.3991, -0.10830, -0.3186 0.4373, -0.10510, -0.3879 0.4757, -0.09890, -0.3750 0.5137, -0.09070, -0.3625 0.5514, -0.08120, -0.3135 0.5917, -0.06870, -0.7453 0.5917, -0.02380, -0.2498 0.5917, 0.02120, -0.7057 16 Flap element taps 1.0000, 0.00130, -0.4518 0.9365, 0.01390, -0.4784 0.8333, 0.03280, -0.4756 0.7436, 0.04930, -0.5217 0.7049, 0.05670, -0.6564 0.6667, 0.05450, -0.6735 0.6302, 0.03770, -0.5460 0.6083, 0.01980, -0.8004 0.6000, 0.00000, -1.6946 0.6076, -0.01900, -1.6264 0.6285, -0.03060, 0.7205 0.6667, -0.04090, 0.4634 0.7046, -0.04120, -0.1877 0.7429, -0.03210, 0.0599 0.8333, -0.01400, 0.1141 0.9311, -0.00120, 0.0377 --------- Run Conditions: vel=107.1 ft/s Re=0.999x10^6 AOA=20.01 Flap deflection=0.00 Totals: Cl=0.8145 Cdp=0.2648 Cm(c/4)=-0.0975 Cs=0.0299 Ch=0.0497 Main component: Cl=0.5670 Cdp=0.2357 Cm=-0.1234 Flap component: Cl=0.2475 Cdp=0.0291 Cm=-0.1880 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.7908 0.5871, 0.07930, -0.7260 0.5501, 0.08690, -0.7235 0.5112, 0.09370, -0.7488 0.4731, 0.09830, -0.7828 0.4349, 0.10070, -0.7964 0.3960, 0.10120, -0.8435 0.3566, 0.10020, -0.8215 0.3172, 0.09790, -0.8273 0.2778, 0.09440, -0.8382 0.2393, 0.08960, -0.8705 0.2056, 0.08360, -0.9192 0.1633, 0.07610, -0.9205 0.1261, 0.06710, -0.9562 0.0900, 0.05640, -0.9530 0.0571, 0.04390, -1.0472 0.0283, 0.02940, -1.3954 0.0142, 0.01970, -1.9757 0.0081, 0.01410, -2.5259 0.0026, 0.00780, -2.7209 0.0000, 0.00000, -4.2165 0.0037, -0.00840, -0.3054 0.0112, -0.01420, 0.6854 0.0191, -0.01930, 0.9281 0.0397, -0.03030, 1.0229 0.0706, -0.04420, 0.9166 0.1037, -0.05710, 0.7955 0.1384, -0.06890, 0.6805 0.1741, -0.07950, 0.5433 0.2102, -0.08660, 0.3532 0.2472, -0.09640, 0.2059 0.2844, -0.10270, 0.0543 0.3225, -0.10690, -0.0576 0.3608, -0.10890, -0.2144 0.3991, -0.10830, -0.2953 0.4373, -0.10510, -0.3726 0.4757, -0.09890, -0.3646 0.5137, -0.09070, -0.3578 0.5514, -0.08120, -0.3115 0.5917, -0.06870, -0.7777 0.5917, -0.02380, -0.2713 0.5917, 0.02120, -0.8339 16 Flap element taps 1.0000, 0.00130, -0.5028 0.9365, 0.01390, -0.5528 0.8333, 0.03280, -0.5422 0.7436, 0.04930, -0.5740 0.7049, 0.05670, -0.6787 0.6667, 0.05450, -0.7513 0.6302, 0.03770, -0.6486 0.6083, 0.01980, -0.9321 0.6000, 0.00000, -1.8263 0.6076, -0.01900, -1.6876 0.6285, -0.03060, 0.7381 0.6667, -0.04090, 0.4614 0.7046, -0.04120, -0.1995 0.7429, -0.03210, 0.0484 0.8333, -0.01400, 0.0966 0.9311, -0.00120, 0.0117 Wake drag found for this condition, Cdw=0.3033 --------- Run Conditions: vel=106.5 ft/s Re=0.993x10^6 AOA=24.01 Flap deflection=0.00 Totals: Cl=0.8189 Cdp=0.3828 Cm(c/4)=-0.1171 Cs=-0.0165 Ch=0.0570 Main component: Cl=0.5561 Cdp=0.3345 Cm=-0.1423 Flap component: Cl=0.2629 Cdp=0.0482 Cm=-0.2007 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.9376 0.5871, 0.07930, -0.9019 0.5501, 0.08690, -0.8716 0.5112, 0.09370, -0.8506 0.4731, 0.09830, -0.8447 0.4349, 0.10070, -0.8304 0.3960, 0.10120, -0.8599 0.3566, 0.10020, -0.8380 0.3172, 0.09790, -0.8492 0.2778, 0.09440, -0.8578 0.2393, 0.08960, -0.8885 0.2056, 0.08360, -0.9303 0.1633, 0.07610, -0.9226 0.1261, 0.06710, -0.9760 0.0900, 0.05640, -1.0100 0.0571, 0.04390, -1.0436 0.0283, 0.02940, -1.1271 0.0142, 0.01970, -1.2505 0.0081, 0.01410, -1.3889 0.0026, 0.00780, -1.3801 0.0000, 0.00000, -2.8673 0.0037, -0.00840, -0.1744 0.0112, -0.01420, 0.6731 0.0191, -0.01930, 0.9064 0.0397, -0.03030, 1.0219 0.0706, -0.04420, 0.9430 0.1037, -0.05710, 0.8397 0.1384, -0.06890, 0.7415 0.1741, -0.07950, 0.6125 0.2102, -0.08660, 0.4261 0.2472, -0.09640, 0.2870 0.2844, -0.10270, 0.1348 0.3225, -0.10690, 0.0238 0.3608, -0.10890, -0.1388 0.3991, -0.10830, -0.2250 0.4373, -0.10510, -0.3133 0.4757, -0.09890, -0.3189 0.5137, -0.09070, -0.3255 0.5514, -0.08120, -0.2907 0.5917, -0.06870, -0.7980 0.5917, -0.02380, -0.2622 0.5917, 0.02120, -0.9533 16 Flap element taps 1.0000, 0.00130, -0.5663 0.9365, 0.01390, -0.6081 0.8333, 0.03280, -0.6046 0.7436, 0.04930, -0.6106 0.7049, 0.05670, -0.6691 0.6667, 0.05450, -0.8155 0.6302, 0.03770, -0.7905 0.6083, 0.01980, -1.1160 0.6000, 0.00000, -1.9344 0.6076, -0.01900, -1.7292 0.6285, -0.03060, 0.7596 0.6667, -0.04090, 0.4623 0.7046, -0.04120, -0.2010 0.7429, -0.03210, 0.0409 0.8333, -0.01400, 0.0798 0.9311, -0.00120, -0.0193 --------- Run Conditions: vel=106.8 ft/s Re=0.997x10^6 AOA=26.94 Flap deflection=0.00 Totals: Cl=0.7112 Cdp=0.4339 Cm(c/4)=-0.1274 Cs=-0.0646 Ch=0.0571 Main component: Cl=0.4431 Cdp=0.3558 Cm=-0.1227 Flap component: Cl=0.2681 Cdp=0.0781 Cm=-0.2124 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.8374 0.5871, 0.07930, -0.7812 0.5501, 0.08690, -0.7569 0.5112, 0.09370, -0.7471 0.4731, 0.09830, -0.7458 0.4349, 0.10070, -0.7296 0.3960, 0.10120, -0.7587 0.3566, 0.10020, -0.7197 0.3172, 0.09790, -0.7197 0.2778, 0.09440, -0.7160 0.2393, 0.08960, -0.7262 0.2056, 0.08360, -0.7506 0.1633, 0.07610, -0.7206 0.1261, 0.06710, -0.7516 0.0900, 0.05640, -0.7359 0.0571, 0.04390, -0.7459 0.0283, 0.02940, -0.7736 0.0142, 0.01970, -0.8025 0.0081, 0.01410, -0.8465 0.0026, 0.00780, -0.7167 0.0000, 0.00000, -1.4047 0.0037, -0.00840, 0.1032 0.0112, -0.01420, 0.7396 0.0191, -0.01930, 0.9244 0.0397, -0.03030, 1.0208 0.0706, -0.04420, 0.9490 0.1037, -0.05710, 0.8554 0.1384, -0.06890, 0.7642 0.1741, -0.07950, 0.6411 0.2102, -0.08660, 0.4604 0.2472, -0.09640, 0.3230 0.2844, -0.10270, 0.1703 0.3225, -0.10690, 0.0592 0.3608, -0.10890, -0.1048 0.3991, -0.10830, -0.1952 0.4373, -0.10510, -0.2897 0.4757, -0.09890, -0.3011 0.5137, -0.09070, -0.3119 0.5514, -0.08120, -0.2796 0.5917, -0.06870, -0.7777 0.5917, -0.02380, -0.3007 0.5917, 0.02120, -0.8776 16 Flap element taps 1.0000, 0.00130, -0.6303 0.9365, 0.01390, -0.6513 0.8333, 0.03280, -0.6683 0.7436, 0.04930, -0.7394 0.7049, 0.05670, -0.8686 0.6667, 0.05450, -0.8205 0.6302, 0.03770, -0.6842 0.6083, 0.01980, -1.0006 0.6000, 0.00000, -1.8551 0.6076, -0.01900, -1.6952 0.6285, -0.03060, 0.7497 0.6667, -0.04090, 0.4550 0.7046, -0.04120, -0.2169 0.7429, -0.03210, 0.0261 0.8333, -0.01400, 0.0593 0.9311, -0.00120, -0.0503