S809 VENTED AILERON MODEL, 18 IN CHORD --------- Run Conditions: vel=108.2 ft/s Re=1.001x10^6 AOA=-6.03 Flap deflection=-60.00 Totals: Cl=-0.5883 Cdp=0.4150 Cm(c/4)=0.1492 Cs=-0.3509 Ch=-0.0062 Main component: Cl=-0.3105 Cdp=-0.0553 Cm=0.0407 Flap component: Cl=-0.2777 Cdp=0.4703 Cm=0.2657 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.3080 0.5871, 0.07930, 0.3089 0.5501, 0.08690, -0.0043 0.5112, 0.09370, 0.0040 0.4731, 0.09830, -0.0230 0.4349, 0.10070, -0.0679 0.3960, 0.10120, -0.0835 0.3566, 0.10020, -0.0497 0.3172, 0.09790, -0.0234 0.2778, 0.09440, 0.0037 0.2393, 0.08960, 0.0397 0.2056, 0.08360, 0.0863 0.1633, 0.07610, 0.1759 0.1261, 0.06710, 0.2667 0.0900, 0.05640, 0.4025 0.0571, 0.04390, 0.5828 0.0283, 0.02940, 0.8265 0.0142, 0.01970, 0.9762 0.0081, 0.01410, 0.9887 0.0026, 0.00780, 0.7631 0.0000, 0.00000, -0.2990 0.0037, -0.00840, -1.1842 0.0112, -0.01420, -0.9798 0.0191, -0.01930, -0.8208 0.0397, -0.03030, -0.6363 0.0706, -0.04420, -0.5973 0.1037, -0.05710, -0.6159 0.1384, -0.06890, -0.6292 0.1741, -0.07950, -0.6459 0.2102, -0.08660, -0.6731 0.2472, -0.09640, -0.6866 0.2844, -0.10270, -0.6547 0.3225, -0.10690, -0.5842 0.3608, -0.10890, -0.5213 0.3991, -0.10830, -0.2638 0.4373, -0.10510, -0.0312 0.4757, -0.09890, 0.2161 0.5137, -0.09070, 0.3221 0.5514, -0.08120, 0.3216 0.5917, -0.06870, 0.3633 0.5917, -0.02380, 0.3048 0.5917, 0.02120, 0.3177 16 Flap element taps 1.0000, 0.00130, -0.9228 0.9365, 0.01390, 0.5695 0.8333, 0.03280, 1.0051 0.7436, 0.04930, 0.5040 0.7049, 0.05670, 0.1418 0.6667, 0.05450, 0.0991 0.6302, 0.03770, 0.1880 0.6083, 0.01980, -0.6094 0.6000, 0.00000, -1.8157 0.6076, -0.01900, -1.1635 0.6285, -0.03060, -1.0173 0.6667, -0.04090, -1.0148 0.7046, -0.04120, -1.0232 0.7429, -0.03210, -0.9952 0.8333, -0.01400, -0.9701 0.9311, -0.00120, -0.9467 --------- Run Conditions: vel=108.1 ft/s Re=0.999x10^6 AOA=0.01 Flap deflection=-60.00 Totals: Cl=-0.3764 Cdp=0.3968 Cm(c/4)=0.1719 Cs=-0.3969 Ch=-0.0355 Main component: Cl=-0.0428 Cdp=-0.0734 Cm=-0.0016 Flap component: Cl=-0.3336 Cdp=0.4702 Cm=0.2677 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.4482 0.5871, 0.07930, 0.3510 0.5501, 0.08690, 0.2428 0.5112, 0.09370, -0.1184 0.4731, 0.09830, -0.1190 0.4349, 0.10070, -0.1631 0.3960, 0.10120, -0.2223 0.3566, 0.10020, -0.2081 0.3172, 0.09790, -0.2127 0.2778, 0.09440, -0.2145 0.2393, 0.08960, -0.2143 0.2056, 0.08360, -0.2118 0.1633, 0.07610, -0.1471 0.1261, 0.06710, -0.1003 0.0900, 0.05640, -0.0062 0.0571, 0.04390, 0.1230 0.0283, 0.02940, 0.3474 0.0142, 0.01970, 0.5712 0.0081, 0.01410, 0.7073 0.0026, 0.00780, 0.9265 0.0000, 0.00000, 0.9657 0.0037, -0.00840, 0.4246 0.0112, -0.01420, 0.2268 0.0191, -0.01930, 0.1571 0.0397, -0.03030, 0.0648 0.0706, -0.04420, -0.0691 0.1037, -0.05710, -0.1809 0.1384, -0.06890, -0.2502 0.1741, -0.07950, -0.3231 0.2102, -0.08660, -0.4119 0.2472, -0.09640, -0.4699 0.2844, -0.10270, -0.4879 0.3225, -0.10690, -0.4463 0.3608, -0.10890, -0.3997 0.3991, -0.10830, -0.3478 0.4373, -0.10510, -0.2849 0.4757, -0.09890, 0.1907 0.5137, -0.09070, 0.3925 0.5514, -0.08120, 0.4774 0.5917, -0.06870, 0.5047 0.5917, -0.02380, 0.4640 0.5917, 0.02120, 0.4652 16 Flap element taps 1.0000, 0.00130, -1.0081 0.9365, 0.01390, 0.5502 0.8333, 0.03280, 0.7945 0.7436, 0.04930, 0.4611 0.7049, 0.05670, 0.4263 0.6667, 0.05450, 0.4524 0.6302, 0.03770, 0.3494 0.6083, 0.01980, -0.4107 0.6000, 0.00000, -2.1577 0.6076, -0.01900, -1.2303 0.6285, -0.03060, -1.0575 0.6667, -0.04090, -1.0538 0.7046, -0.04120, -1.0773 0.7429, -0.03210, -1.0695 0.8333, -0.01400, -1.0455 0.9311, -0.00120, -1.0264 --------- Run Conditions: vel=108.1 ft/s Re=0.998x10^6 AOA=3.05 Flap deflection=-60.00 Totals: Cl=-0.2477 Cdp=0.3755 Cm(c/4)=0.1565 Cs=-0.3882 Ch=-0.0793 Main component: Cl=0.0644 Cdp=-0.0804 Cm=-0.0102 Flap component: Cl=-0.3121 Cdp=0.4559 Cm=0.2236 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.5384 0.5871, 0.07930, 0.4382 0.5501, 0.08690, 0.2926 0.5112, 0.09370, 0.1048 0.4731, 0.09830, -0.1527 0.4349, 0.10070, -0.1855 0.3960, 0.10120, -0.2672 0.3566, 0.10020, -0.2474 0.3172, 0.09790, -0.2735 0.2778, 0.09440, -0.2953 0.2393, 0.08960, -0.3175 0.2056, 0.08360, -0.3556 0.1633, 0.07610, -0.2970 0.1261, 0.06710, -0.2915 0.0900, 0.05640, -0.2279 0.0571, 0.04390, -0.1562 0.0283, 0.02940, 0.0032 0.0142, 0.01970, 0.1939 0.0081, 0.01410, 0.3117 0.0026, 0.00780, 0.6059 0.0000, 0.00000, 0.9924 0.0037, -0.00840, 0.8505 0.0112, -0.01420, 0.6313 0.0191, -0.01930, 0.5152 0.0397, -0.03030, 0.3534 0.0706, -0.04420, 0.1627 0.1037, -0.05710, 0.0201 0.1384, -0.06890, -0.0595 0.1741, -0.07950, -0.1605 0.2102, -0.08660, -0.2886 0.2472, -0.09640, -0.3614 0.2844, -0.10270, -0.4149 0.3225, -0.10690, -0.3957 0.3608, -0.10890, -0.3896 0.3991, -0.10830, -0.3020 0.4373, -0.10510, -0.3082 0.4757, -0.09890, 0.0916 0.5137, -0.09070, 0.2847 0.5514, -0.08120, 0.4511 0.5917, -0.06870, 0.5556 0.5917, -0.02380, 0.5292 0.5917, 0.02120, 0.5369 16 Flap element taps 1.0000, 0.00130, -0.9389 0.9365, 0.01390, 0.3695 0.8333, 0.03280, 0.6186 0.7436, 0.04930, 0.5456 0.7049, 0.05670, 0.4614 0.6667, 0.05450, 0.6682 0.6302, 0.03770, 0.8989 0.6083, 0.01980, 0.0805 0.6000, 0.00000, -1.3634 0.6076, -0.01900, -1.0719 0.6285, -0.03060, -0.9969 0.6667, -0.04090, -1.0001 0.7046, -0.04120, -1.0027 0.7429, -0.03210, -0.9918 0.8333, -0.01400, -0.9610 0.9311, -0.00120, -0.9531 --------- Run Conditions: vel=108.7 ft/s Re=1.001x10^6 AOA=6.05 Flap deflection=-60.00 Totals: Cl=-0.1733 Cdp=0.3949 Cm(c/4)=0.1719 Cs=-0.4109 Ch=-0.0889 Main component: Cl=0.1638 Cdp=-0.0714 Cm=-0.0166 Flap component: Cl=-0.3370 Cdp=0.4663 Cm=0.2212 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.4994 0.5871, 0.07930, 0.4598 0.5501, 0.08690, 0.3452 0.5112, 0.09370, 0.1376 0.4731, 0.09830, -0.0249 0.4349, 0.10070, -0.1847 0.3960, 0.10120, -0.3340 0.3566, 0.10020, -0.3008 0.3172, 0.09790, -0.3426 0.2778, 0.09440, -0.3790 0.2393, 0.08960, -0.4233 0.2056, 0.08360, -0.5000 0.1633, 0.07610, -0.4491 0.1261, 0.06710, -0.4854 0.0900, 0.05640, -0.4582 0.0571, 0.04390, -0.4499 0.0283, 0.02940, -0.3806 0.0142, 0.01970, -0.2669 0.0081, 0.01410, -0.2098 0.0026, 0.00780, 0.0640 0.0000, 0.00000, 0.6547 0.0037, -0.00840, 1.0128 0.0112, -0.01420, 0.8775 0.0191, -0.01930, 0.7656 0.0397, -0.03030, 0.5792 0.0706, -0.04420, 0.3594 0.1037, -0.05710, 0.1974 0.1384, -0.06890, 0.1143 0.1741, -0.07950, -0.0061 0.2102, -0.08660, -0.1654 0.2472, -0.09640, -0.2493 0.2844, -0.10270, -0.3309 0.3225, -0.10690, -0.3248 0.3608, -0.10890, -0.3594 0.3991, -0.10830, -0.2743 0.4373, -0.10510, -0.2613 0.4757, -0.09890, -0.2322 0.5137, -0.09070, 0.2250 0.5514, -0.08120, 0.3770 0.5917, -0.06870, 0.5257 0.5917, -0.02380, 0.4954 0.5917, 0.02120, 0.5018 16 Flap element taps 1.0000, 0.00130, -1.0541 0.9365, 0.01390, 0.2870 0.8333, 0.03280, 0.5640 0.7436, 0.04930, 0.5016 0.7049, 0.05670, 0.4226 0.6667, 0.05450, 0.8283 0.6302, 0.03770, 0.9325 0.6083, 0.01980, 0.1511 0.6000, 0.00000, -1.1400 0.6076, -0.01900, -1.0622 0.6285, -0.03060, -1.0383 0.6667, -0.04090, -1.0664 0.7046, -0.04120, -1.0713 0.7429, -0.03210, -1.0782 0.8333, -0.01400, -1.0691 0.9311, -0.00120, -1.0611 --------- Run Conditions: vel=109.1 ft/s Re=1.003x10^6 AOA=9.05 Flap deflection=-60.00 Totals: Cl=-0.0786 Cdp=0.3871 Cm(c/4)=0.1751 Cs=-0.3946 Ch=-0.0903 Main component: Cl=0.2584 Cdp=-0.0428 Cm=-0.0246 Flap component: Cl=-0.3369 Cdp=0.4299 Cm=0.2039 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.3003 0.5871, 0.07930, 0.2864 0.5501, 0.08690, 0.2910 0.5112, 0.09370, 0.2262 0.4731, 0.09830, 0.0711 0.4349, 0.10070, -0.0883 0.3960, 0.10120, -0.2574 0.3566, 0.10020, -0.2574 0.3172, 0.09790, -0.3584 0.2778, 0.09440, -0.4517 0.2393, 0.08960, -0.5135 0.2056, 0.08360, -0.6224 0.1633, 0.07610, -0.5963 0.1261, 0.06710, -0.6756 0.0900, 0.05640, -0.6969 0.0571, 0.04390, -0.7707 0.0283, 0.02940, -0.8214 0.0142, 0.01970, -0.8334 0.0081, 0.01410, -0.8879 0.0026, 0.00780, -0.5929 0.0000, 0.00000, -0.0995 0.0037, -0.00840, 0.9797 0.0112, -0.01420, 1.0023 0.0191, -0.01930, 0.9298 0.0397, -0.03030, 0.7619 0.0706, -0.04420, 0.5340 0.1037, -0.05710, 0.3592 0.1384, -0.06890, 0.2737 0.1741, -0.07950, 0.1391 0.2102, -0.08660, -0.0441 0.2472, -0.09640, -0.1384 0.2844, -0.10270, -0.2439 0.3225, -0.10690, -0.2563 0.3608, -0.10890, -0.3221 0.3991, -0.10830, -0.2659 0.4373, -0.10510, -0.2296 0.4757, -0.09890, -0.2140 0.5137, -0.09070, 0.1653 0.5514, -0.08120, 0.2797 0.5917, -0.06870, 0.3717 0.5917, -0.02380, 0.3336 0.5917, 0.02120, 0.3366 16 Flap element taps 1.0000, 0.00130, -1.0964 0.9365, 0.01390, 0.1885 0.8333, 0.03280, 0.4414 0.7436, 0.04930, 0.3546 0.7049, 0.05670, 0.2706 0.6667, 0.05450, 0.7599 0.6302, 0.03770, 0.9634 0.6083, 0.01980, 0.2703 0.6000, 0.00000, -1.2183 0.6076, -0.01900, -1.0704 0.6285, -0.03060, -1.0413 0.6667, -0.04090, -1.0769 0.7046, -0.04120, -1.0830 0.7429, -0.03210, -1.0958 0.8333, -0.01400, -1.0813 0.9311, -0.00120, -1.0920 --------- Run Conditions: vel=109.9 ft/s Re=1.009x10^6 AOA=12.08 Flap deflection=-60.00 Totals: Cl=0.0465 Cdp=0.3638 Cm(c/4)=0.1711 Cs=-0.3460 Ch=-0.0874 Main component: Cl=0.3665 Cdp=-0.0158 Cm=-0.0377 Flap component: Cl=-0.3200 Cdp=0.3796 Cm=0.1784 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.1703 0.5871, 0.07930, 0.1681 0.5501, 0.08690, 0.1698 0.5112, 0.09370, 0.1615 0.4731, 0.09830, 0.1229 0.4349, 0.10070, -0.0199 0.3960, 0.10120, -0.2318 0.3566, 0.10020, -0.2840 0.3172, 0.09790, -0.3834 0.2778, 0.09440, -0.4771 0.2393, 0.08960, -0.5834 0.2056, 0.08360, -0.7275 0.1633, 0.07610, -0.7314 0.1261, 0.06710, -0.8647 0.0900, 0.05640, -0.9743 0.0571, 0.04390, -1.1396 0.0283, 0.02940, -1.3487 0.0142, 0.01970, -1.5297 0.0081, 0.01410, -1.7408 0.0026, 0.00780, -1.5676 0.0000, 0.00000, -1.3306 0.0037, -0.00840, 0.7242 0.0112, -0.01420, 1.0047 0.0191, -0.01930, 1.0074 0.0397, -0.03030, 0.9016 0.0706, -0.04420, 0.6895 0.1037, -0.05710, 0.5174 0.1384, -0.06890, 0.4261 0.1741, -0.07950, 0.2866 0.2102, -0.08660, 0.0913 0.2472, -0.09640, -0.0139 0.2844, -0.10270, -0.1359 0.3225, -0.10690, -0.1687 0.3608, -0.10890, -0.2563 0.3991, -0.10830, -0.2319 0.4373, -0.10510, -0.2031 0.4757, -0.09890, -0.1602 0.5137, -0.09070, -0.0841 0.5514, -0.08120, 0.2265 0.5917, -0.06870, 0.2174 0.5917, -0.02380, 0.1804 0.5917, 0.02120, 0.1858 16 Flap element taps 1.0000, 0.00130, -1.0752 0.9365, 0.01390, 0.1170 0.8333, 0.03280, 0.2845 0.7436, 0.04930, 0.2024 0.7049, 0.05670, 0.0762 0.6667, 0.05450, 0.6473 0.6302, 0.03770, 0.9853 0.6083, 0.01980, 0.3987 0.6000, 0.00000, -1.2078 0.6076, -0.01900, -1.0436 0.6285, -0.03060, -1.0125 0.6667, -0.04090, -1.0468 0.7046, -0.04120, -1.0565 0.7429, -0.03210, -1.0610 0.8333, -0.01400, -1.0524 0.9311, -0.00120, -1.0729 --------- Run Conditions: vel=110.4 ft/s Re=1.012x10^6 AOA=15.04 Flap deflection=-60.00 Totals: Cl=0.2043 Cdp=0.3587 Cm(c/4)=0.1606 Cs=-0.2934 Ch=-0.0786 Main component: Cl=0.5021 Cdp=0.0240 Cm=-0.0651 Flap component: Cl=-0.2977 Cdp=0.3347 Cm=0.1531 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.0247 0.5871, 0.07930, -0.0183 0.5501, 0.08690, -0.0142 0.5112, 0.09370, -0.0060 0.4731, 0.09830, -0.0088 0.4349, 0.10070, -0.0425 0.3960, 0.10120, -0.1922 0.3566, 0.10020, -0.2694 0.3172, 0.09790, -0.4058 0.2778, 0.09440, -0.5327 0.2393, 0.08960, -0.6710 0.2056, 0.08360, -0.8488 0.1633, 0.07610, -0.9054 0.1261, 0.06710, -1.0742 0.0900, 0.05640, -1.2316 0.0571, 0.04390, -1.4950 0.0283, 0.02940, -1.8708 0.0142, 0.01970, -2.4160 0.0081, 0.01410, -2.8554 0.0026, 0.00780, -2.8037 0.0000, 0.00000, -2.9970 0.0037, -0.00840, 0.2404 0.0112, -0.01420, 0.8918 0.0191, -0.01930, 1.0065 0.0397, -0.03030, 0.9894 0.0706, -0.04420, 0.8210 0.1037, -0.05710, 0.6615 0.1384, -0.06890, 0.5664 0.1741, -0.07950, 0.4241 0.2102, -0.08660, 0.2291 0.2472, -0.09640, 0.1157 0.2844, -0.10270, -0.0180 0.3225, -0.10690, -0.0688 0.3608, -0.10890, -0.1748 0.3991, -0.10830, -0.1787 0.4373, -0.10510, -0.1768 0.4757, -0.09890, -0.1110 0.5137, -0.09070, -0.0776 0.5514, -0.08120, 0.1914 0.5917, -0.06870, 0.0205 0.5917, -0.02380, -0.0132 0.5917, 0.02120, -0.0092 16 Flap element taps 1.0000, 0.00130, -1.1129 0.9365, 0.01390, 0.0304 0.8333, 0.03280, 0.1749 0.7436, 0.04930, 0.0391 0.7049, 0.05670, -0.1570 0.6667, 0.05450, 0.5083 0.6302, 0.03770, 0.9980 0.6083, 0.01980, 0.5213 0.6000, 0.00000, -1.1413 0.6076, -0.01900, -0.9923 0.6285, -0.03060, -0.9600 0.6667, -0.04090, -0.9943 0.7046, -0.04120, -1.0063 0.7429, -0.03210, -1.0326 0.8333, -0.01400, -1.0438 0.9311, -0.00120, -1.0717 --------- Run Conditions: vel=111.2 ft/s Re=1.017x10^6 AOA=18.04 Flap deflection=-60.00 Totals: Cl=0.3777 Cdp=0.3487 Cm(c/4)=0.1386 Cs=-0.2146 Ch=-0.0688 Main component: Cl=0.6302 Cdp=0.0735 Cm=-0.0953 Flap component: Cl=-0.2525 Cdp=0.2752 Cm=0.1171 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.2283 0.5871, 0.07930, -0.2557 0.5501, 0.08690, -0.2445 0.5112, 0.09370, -0.2342 0.4731, 0.09830, -0.2278 0.4349, 0.10070, -0.2341 0.3960, 0.10120, -0.3062 0.3566, 0.10020, -0.2789 0.3172, 0.09790, -0.3705 0.2778, 0.09440, -0.5019 0.2393, 0.08960, -0.6821 0.2056, 0.08360, -0.9072 0.1633, 0.07610, -1.0155 0.1261, 0.06710, -1.2429 0.0900, 0.05640, -1.4734 0.0571, 0.04390, -1.8631 0.0283, 0.02940, -2.4410 0.0142, 0.01970, -3.0403 0.0081, 0.01410, -4.2843 0.0026, 0.00780, -4.2944 0.0000, 0.00000, -5.0015 0.0037, -0.00840, -0.4593 0.0112, -0.01420, 0.6502 0.0191, -0.01930, 0.9183 0.0397, -0.03030, 1.0242 0.0706, -0.04420, 0.9121 0.1037, -0.05710, 0.7780 0.1384, -0.06890, 0.6922 0.1741, -0.07950, 0.5516 0.2102, -0.08660, 0.3568 0.2472, -0.09640, 0.2401 0.2844, -0.10270, 0.0968 0.3225, -0.10690, 0.0347 0.3608, -0.10890, -0.0893 0.3991, -0.10830, -0.1165 0.4373, -0.10510, -0.1458 0.4757, -0.09890, -0.0905 0.5137, -0.09070, -0.0368 0.5514, -0.08120, -0.0031 0.5917, -0.06870, -0.1772 0.5917, -0.02380, -0.2129 0.5917, 0.02120, -0.2157 16 Flap element taps 1.0000, 0.00130, -1.0775 0.9365, 0.01390, -0.0384 0.8333, 0.03280, -0.0274 0.7436, 0.04930, -0.1752 0.7049, 0.05670, -0.4609 0.6667, 0.05450, 0.3271 0.6302, 0.03770, 0.9941 0.6083, 0.01980, 0.6386 0.6000, 0.00000, -1.0424 0.6076, -0.01900, -0.9384 0.6285, -0.03060, -0.9089 0.6667, -0.04090, -0.9426 0.7046, -0.04120, -0.9553 0.7429, -0.03210, -0.9699 0.8333, -0.01400, -0.9805 0.9311, -0.00120, -1.0310 --------- Run Conditions: vel=108.8 ft/s Re=0.995x10^6 AOA=20.03 Flap deflection=-60.00 Totals: Cl=0.6257 Cdp=0.3974 Cm(c/4)=-0.0395 Cs=-0.1591 Ch=-0.0598 Main component: Cl=0.5766 Cdp=0.3495 Cm=-0.1608 Flap component: Cl=0.0491 Cdp=0.0479 Cm=-0.0597 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.9185 0.5871, 0.07930, -0.8897 0.5501, 0.08690, -0.9262 0.5112, 0.09370, -0.9512 0.4731, 0.09830, -0.9516 0.4349, 0.10070, -0.9522 0.3960, 0.10120, -1.0169 0.3566, 0.10020, -0.9297 0.3172, 0.09790, -0.9220 0.2778, 0.09440, -0.9017 0.2393, 0.08960, -0.9047 0.2056, 0.08360, -0.9645 0.1633, 0.07610, -0.8793 0.1261, 0.06710, -0.9204 0.0900, 0.05640, -0.8776 0.0571, 0.04390, -0.9025 0.0283, 0.02940, -0.9165 0.0142, 0.01970, -0.9313 0.0081, 0.01410, -0.9879 0.0026, 0.00780, -0.8705 0.0000, 0.00000, -1.1858 0.0037, -0.00840, 0.4114 0.0112, -0.01420, 0.8930 0.0191, -0.01930, 0.9998 0.0397, -0.03030, 1.0148 0.0706, -0.04420, 0.8783 0.1037, -0.05710, 0.7461 0.1384, -0.06890, 0.6788 0.1741, -0.07950, 0.5427 0.2102, -0.08660, 0.3350 0.2472, -0.09640, 0.2258 0.2844, -0.10270, 0.0756 0.3225, -0.10690, 0.0181 0.3608, -0.10890, -0.1252 0.3991, -0.10830, -0.1632 0.4373, -0.10510, -0.2230 0.4757, -0.09890, -0.1936 0.5137, -0.09070, -0.1744 0.5514, -0.08120, -0.1471 0.5917, -0.06870, -0.8322 0.5917, -0.02380, -0.8793 0.5917, 0.02120, -0.8910 16 Flap element taps 1.0000, 0.00130, -0.6033 0.9365, 0.01390, -0.6818 0.8333, 0.03280, -0.8410 0.7436, 0.04930, -0.8790 0.7049, 0.05670, -1.4264 0.6667, 0.05450, -0.2524 0.6302, 0.03770, 0.9201 0.6083, 0.01980, 0.8625 0.6000, 0.00000, -0.5884 0.6076, -0.01900, -0.5979 0.6285, -0.03060, -0.5666 0.6667, -0.04090, -0.5846 0.7046, -0.04120, -0.5779 0.7429, -0.03210, -0.5862 0.8333, -0.01400, -0.5736 0.9311, -0.00120, -0.5913 --------- Run Conditions: vel=108.2 ft/s Re=0.988x10^6 AOA=23.99 Flap deflection=-60.00 Totals: Cl=0.6444 Cdp=0.4545 Cm(c/4)=-0.0500 Cs=-0.1532 Ch=-0.0669 Main component: Cl=0.5787 Cdp=0.4121 Cm=-0.1706 Flap component: Cl=0.0657 Cdp=0.0424 Cm=-0.0728 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.9546 0.5871, 0.07930, -0.9042 0.5501, 0.08690, -0.9182 0.5112, 0.09370, -0.9283 0.4731, 0.09830, -0.9296 0.4349, 0.10070, -0.9400 0.3960, 0.10120, -1.0360 0.3566, 0.10020, -0.9252 0.3172, 0.09790, -0.9223 0.2778, 0.09440, -0.8990 0.2393, 0.08960, -0.9044 0.2056, 0.08360, -0.9830 0.1633, 0.07610, -0.8682 0.1261, 0.06710, -0.9266 0.0900, 0.05640, -0.8805 0.0571, 0.04390, -0.9029 0.0283, 0.02940, -0.9035 0.0142, 0.01970, -0.9173 0.0081, 0.01410, -0.9924 0.0026, 0.00780, -0.8530 0.0000, 0.00000, -1.0419 0.0037, -0.00840, 0.2374 0.0112, -0.01420, 0.8058 0.0191, -0.01930, 0.9629 0.0397, -0.03030, 1.0362 0.0706, -0.04420, 0.9307 0.1037, -0.05710, 0.8175 0.1384, -0.06890, 0.7856 0.1741, -0.07950, 0.6528 0.2102, -0.08660, 0.4281 0.2472, -0.09640, 0.3328 0.2844, -0.10270, 0.1708 0.3225, -0.10690, 0.1254 0.3608, -0.10890, -0.0372 0.3991, -0.10830, -0.0778 0.4373, -0.10510, -0.1661 0.4757, -0.09890, -0.1529 0.5137, -0.09070, -0.1450 0.5514, -0.08120, -0.1313 0.5917, -0.06870, -0.8707 0.5917, -0.02380, -0.9200 0.5917, 0.02120, -0.9285 16 Flap element taps 1.0000, 0.00130, -0.5936 0.9365, 0.01390, -0.8561 0.8333, 0.03280, -0.8966 0.7436, 0.04930, -0.9314 0.7049, 0.05670, -1.5184 0.6667, 0.05450, -0.3107 0.6302, 0.03770, 0.9085 0.6083, 0.01980, 0.8888 0.6000, 0.00000, -0.5757 0.6076, -0.01900, -0.6245 0.6285, -0.03060, -0.5849 0.6667, -0.04090, -0.6075 0.7046, -0.04120, -0.5959 0.7429, -0.03210, -0.6086 0.8333, -0.01400, -0.5920 0.9311, -0.00120, -0.6142 --------- Run Conditions: vel=110.3 ft/s Re=1.006x10^6 AOA=26.99 Flap deflection=-60.00 Totals: Cl=0.6496 Cdp=0.5121 Cm(c/4)=-0.0518 Cs=-0.1615 Ch=-0.0667 Main component: Cl=0.5884 Cdp=0.4636 Cm=-0.1824 Flap component: Cl=0.0612 Cdp=0.0486 Cm=-0.0722 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.9757 0.5871, 0.07930, -0.9339 0.5501, 0.08690, -0.9334 0.5112, 0.09370, -0.9420 0.4731, 0.09830, -0.9411 0.4349, 0.10070, -0.9542 0.3960, 0.10120, -1.0676 0.3566, 0.10020, -0.9430 0.3172, 0.09790, -0.9414 0.2778, 0.09440, -0.9182 0.2393, 0.08960, -0.9248 0.2056, 0.08360, -1.0138 0.1633, 0.07610, -0.8865 0.1261, 0.06710, -0.9531 0.0900, 0.05640, -0.8963 0.0571, 0.04390, -0.9237 0.0283, 0.02940, -0.9195 0.0142, 0.01970, -0.9340 0.0081, 0.01410, -1.0189 0.0026, 0.00780, -0.8696 0.0000, 0.00000, -0.9328 0.0037, -0.00840, 0.0814 0.0112, -0.01420, 0.7154 0.0191, -0.01930, 0.9165 0.0397, -0.03030, 1.0372 0.0706, -0.04420, 0.9614 0.1037, -0.05710, 0.8655 0.1384, -0.06890, 0.8577 0.1741, -0.07950, 0.7302 0.2102, -0.08660, 0.4969 0.2472, -0.09640, 0.4137 0.2844, -0.10270, 0.2443 0.3225, -0.10690, 0.2078 0.3608, -0.10890, 0.0315 0.3991, -0.10830, -0.0107 0.4373, -0.10510, -0.1173 0.4757, -0.09890, -0.1151 0.5137, -0.09070, -0.1191 0.5514, -0.08120, -0.1171 0.5917, -0.06870, -0.8995 0.5917, -0.02380, -0.9481 0.5917, 0.02120, -0.9554 16 Flap element taps 1.0000, 0.00130, -0.6278 0.9365, 0.01390, -0.8799 0.8333, 0.03280, -0.9098 0.7436, 0.04930, -0.9584 0.7049, 0.05670, -1.5736 0.6667, 0.05450, -0.3481 0.6302, 0.03770, 0.8976 0.6083, 0.01980, 0.8985 0.6000, 0.00000, -0.5771 0.6076, -0.01900, -0.6595 0.6285, -0.03060, -0.6179 0.6667, -0.04090, -0.6402 0.7046, -0.04120, -0.6266 0.7429, -0.03210, -0.6398 0.8333, -0.01400, -0.6252 0.9311, -0.00120, -0.6485 --------- Run Conditions: vel=110.4 ft/s Re=1.001x10^6 AOA=30.01 Flap deflection=-60.00 Totals: Cl=0.6334 Cdp=0.5520 Cm(c/4)=-0.0543 Cs=-0.1612 Ch=-0.0688 Main component: Cl=0.5727 Cdp=0.4998 Cm=-0.1862 Flap component: Cl=0.0607 Cdp=0.0523 Cm=-0.0743 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.9835 0.5871, 0.07930, -0.9369 0.5501, 0.08690, -0.9331 0.5112, 0.09370, -0.9304 0.4731, 0.09830, -0.9489 0.4349, 0.10070, -0.9500 0.3960, 0.10120, -0.9512 0.3566, 0.10020, -0.9478 0.3172, 0.09790, -0.9456 0.2778, 0.09440, -0.9420 0.2393, 0.08960, -0.9397 0.2056, 0.08360, -0.9317 0.1633, 0.07610, -0.9394 0.1261, 0.06710, -0.9329 0.0900, 0.05640, -0.9351 0.0571, 0.04390, -0.9276 0.0283, 0.02940, -0.9318 0.0142, 0.01970, -0.9332 0.0081, 0.01410, -0.9434 0.0026, 0.00780, -0.8917 0.0000, 0.00000, -0.9549 0.0037, -0.00840, -0.0862 0.0112, -0.01420, 0.6078 0.0191, -0.01930, 0.8418 0.0397, -0.03030, 0.9987 0.0706, -0.04420, 0.9904 0.1037, -0.05710, 0.9284 0.1384, -0.06890, 0.8250 0.1741, -0.07950, 0.7210 0.2102, -0.08660, 0.6011 0.2472, -0.09640, 0.4635 0.2844, -0.10270, 0.3460 0.3225, -0.10690, 0.2189 0.3608, -0.10890, 0.0960 0.3991, -0.10830, -0.0057 0.4373, -0.10510, -0.0679 0.4757, -0.09890, -0.0686 0.5137, -0.09070, -0.0979 0.5514, -0.08120, -0.1001 0.5917, -0.06870, -0.9361 0.5917, -0.02380, -0.9503 0.5917, 0.02120, -0.9665 16 Flap element taps 1.0000, 0.00130, -0.6571 0.9365, 0.01390, -0.9140 0.8333, 0.03280, -0.9348 0.7436, 0.04930, -0.9614 0.7049, 0.05670, -1.5791 0.6667, 0.05450, -0.3657 0.6302, 0.03770, 0.8965 0.6083, 0.01980, 0.8961 0.6000, 0.00000, -0.5699 0.6076, -0.01900, -0.6509 0.6285, -0.03060, -0.6465 0.6667, -0.04090, -0.6447 0.7046, -0.04120, -0.6417 0.7429, -0.03210, -0.6455 0.8333, -0.01400, -0.6503 0.9311, -0.00120, -0.6551 --------- Run Conditions: vel=109.9 ft/s Re=0.994x10^6 AOA=35.01 Flap deflection=-60.00 Totals: Cl=0.6415 Cdp=0.6574 Cm(c/4)=-0.0605 Cs=-0.1704 Ch=-0.0686 Main component: Cl=0.5873 Cdp=0.5947 Cm=-0.2107 Flap component: Cl=0.0541 Cdp=0.0627 Cm=-0.0754 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.0462 0.5871, 0.07930, -1.0024 0.5501, 0.08690, -0.9996 0.5112, 0.09370, -0.9953 0.4731, 0.09830, -1.0126 0.4349, 0.10070, -1.0166 0.3960, 0.10120, -1.0180 0.3566, 0.10020, -1.0173 0.3172, 0.09790, -1.0187 0.2778, 0.09440, -1.0170 0.2393, 0.08960, -1.0144 0.2056, 0.08360, -1.0039 0.1633, 0.07610, -1.0108 0.1261, 0.06710, -1.0049 0.0900, 0.05640, -1.0053 0.0571, 0.04390, -0.9996 0.0283, 0.02940, -1.0011 0.0142, 0.01970, -1.0029 0.0081, 0.01410, -1.0121 0.0026, 0.00780, -0.9589 0.0000, 0.00000, -1.0127 0.0037, -0.00840, -0.3743 0.0112, -0.01420, 0.4131 0.0191, -0.01930, 0.7138 0.0397, -0.03030, 0.9567 0.0706, -0.04420, 1.0061 0.1037, -0.05710, 0.9829 0.1384, -0.06890, 0.9038 0.1741, -0.07950, 0.8170 0.2102, -0.08660, 0.7100 0.2472, -0.09640, 0.5823 0.2844, -0.10270, 0.4684 0.3225, -0.10690, 0.3396 0.3608, -0.10890, 0.2118 0.3991, -0.10830, 0.0992 0.4373, -0.10510, 0.0185 0.4757, -0.09890, -0.0040 0.5137, -0.09070, -0.0551 0.5514, -0.08120, -0.0827 0.5917, -0.06870, -1.0035 0.5917, -0.02380, -1.0187 0.5917, 0.02120, -1.0367 16 Flap element taps 1.0000, 0.00130, -0.7365 0.9365, 0.01390, -0.9707 0.8333, 0.03280, -0.9935 0.7436, 0.04930, -1.0352 0.7049, 0.05670, -1.7039 0.6667, 0.05450, -0.4527 0.6302, 0.03770, 0.8743 0.6083, 0.01980, 0.9207 0.6000, 0.00000, -0.5599 0.6076, -0.01900, -0.7214 0.6285, -0.03060, -0.7179 0.6667, -0.04090, -0.7165 0.7046, -0.04120, -0.7146 0.7429, -0.03210, -0.7196 0.8333, -0.01400, -0.7275 0.9311, -0.00120, -0.7328 --------- Run Conditions: vel=110.7 ft/s Re=1.000x10^6 AOA=39.99 Flap deflection=-60.00 Totals: Cl=0.6473 Cdp=0.7681 Cm(c/4)=-0.0711 Cs=-0.1725 Ch=-0.0688 Main component: Cl=0.5903 Cdp=0.6988 Cm=-0.2365 Flap component: Cl=0.0571 Cdp=0.0693 Cm=-0.0819 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.1596 0.5871, 0.07930, -1.0969 0.5501, 0.08690, -1.0947 0.5112, 0.09370, -1.0917 0.4731, 0.09830, -1.1083 0.4349, 0.10070, -1.1083 0.3960, 0.10120, -1.1077 0.3566, 0.10020, -1.1071 0.3172, 0.09790, -1.1098 0.2778, 0.09440, -1.1098 0.2393, 0.08960, -1.1082 0.2056, 0.08360, -1.1004 0.1633, 0.07610, -1.1084 0.1261, 0.06710, -1.0980 0.0900, 0.05640, -1.1003 0.0571, 0.04390, -1.0943 0.0283, 0.02940, -1.0938 0.0142, 0.01970, -1.0946 0.0081, 0.01410, -1.1031 0.0026, 0.00780, -1.0511 0.0000, 0.00000, -1.1017 0.0037, -0.00840, -0.6606 0.0112, -0.01420, 0.1962 0.0191, -0.01930, 0.5572 0.0397, -0.03030, 0.8857 0.0706, -0.04420, 0.9936 0.1037, -0.05710, 1.0064 0.1384, -0.06890, 0.9557 0.1741, -0.07950, 0.8870 0.2102, -0.08660, 0.7970 0.2472, -0.09640, 0.6803 0.2844, -0.10270, 0.5728 0.3225, -0.10690, 0.4460 0.3608, -0.10890, 0.3139 0.3991, -0.10830, 0.1918 0.4373, -0.10510, 0.0947 0.4757, -0.09890, 0.0518 0.5137, -0.09070, -0.0225 0.5514, -0.08120, -0.0772 0.5917, -0.06870, -1.1057 0.5917, -0.02380, -1.1200 0.5917, 0.02120, -1.1512 16 Flap element taps 1.0000, 0.00130, -0.8068 0.9365, 0.01390, -1.0595 0.8333, 0.03280, -1.0925 0.7436, 0.04930, -1.1439 0.7049, 0.05670, -1.8859 0.6667, 0.05450, -0.5757 0.6302, 0.03770, 0.8373 0.6083, 0.01980, 0.9419 0.6000, 0.00000, -0.5394 0.6076, -0.01900, -0.8063 0.6285, -0.03060, -0.8026 0.6667, -0.04090, -0.7995 0.7046, -0.04120, -0.7957 0.7429, -0.03210, -0.7994 0.8333, -0.01400, -0.8040 0.9311, -0.00120, -0.8103 --------- Run Conditions: vel=110.1 ft/s Re=0.995x10^6 AOA=45.03 Flap deflection=-60.00 Totals: Cl=0.2976 Cdp=0.7967 Cm(c/4)=-0.0054 Cs=-0.3525 Ch=-0.0969 Main component: Cl=0.4657 Cdp=0.6706 Cm=-0.2093 Flap component: Cl=-0.1681 Cdp=0.1261 Cm=0.0104 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.9780 0.5871, 0.07930, -0.9206 0.5501, 0.08690, -0.9145 0.5112, 0.09370, -0.9096 0.4731, 0.09830, -0.9168 0.4349, 0.10070, -0.9152 0.3960, 0.10120, -0.9147 0.3566, 0.10020, -0.9178 0.3172, 0.09790, -0.9202 0.2778, 0.09440, -0.9221 0.2393, 0.08960, -0.9195 0.2056, 0.08360, -0.9094 0.1633, 0.07610, -0.9179 0.1261, 0.06710, -0.9087 0.0900, 0.05640, -0.9128 0.0571, 0.04390, -0.9046 0.0283, 0.02940, -0.9036 0.0142, 0.01970, -0.9047 0.0081, 0.01410, -0.9125 0.0026, 0.00780, -0.8675 0.0000, 0.00000, -0.9116 0.0037, -0.00840, -0.6270 0.0112, -0.01420, 0.1634 0.0191, -0.01930, 0.5155 0.0397, -0.03030, 0.8517 0.0706, -0.04420, 0.9793 0.1037, -0.05710, 1.0062 0.1384, -0.06890, 0.9646 0.1741, -0.07950, 0.9090 0.2102, -0.08660, 0.8250 0.2472, -0.09640, 0.7152 0.2844, -0.10270, 0.6076 0.3225, -0.10690, 0.4789 0.3608, -0.10890, 0.3465 0.3991, -0.10830, 0.2199 0.4373, -0.10510, 0.1184 0.4757, -0.09890, 0.0720 0.5137, -0.09070, -0.0048 0.5514, -0.08120, -0.0456 0.5917, -0.06870, -0.9363 0.5917, -0.02380, -0.9502 0.5917, 0.02120, -0.9729 16 Flap element taps 1.0000, 0.00130, -1.2502 0.9365, 0.01390, -0.9833 0.8333, 0.03280, -0.9153 0.7436, 0.04930, -0.9494 0.7049, 0.05670, -1.5772 0.6667, 0.05450, -0.3768 0.6302, 0.03770, 0.8888 0.6083, 0.01980, 0.8676 0.6000, 0.00000, -0.9626 0.6076, -0.01900, -1.2635 0.6285, -0.03060, -1.2631 0.6667, -0.04090, -1.2601 0.7046, -0.04120, -1.2614 0.7429, -0.03210, -1.2612 0.8333, -0.01400, -1.2757 0.9311, -0.00120, -1.2750 --------- Run Conditions: vel=111.6 ft/s Re=1.004x10^6 AOA=60.04 Flap deflection=-60.00 Totals: Cl=0.0761 Cdp=0.9978 Cm(c/4)=-0.0128 Cs=-0.4324 Ch=-0.1059 Main component: Cl=0.3529 Cdp=0.9009 Cm=-0.2681 Flap component: Cl=-0.2768 Cdp=0.0969 Cm=0.0297 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.1693 0.5871, 0.07930, -1.0995 0.5501, 0.08690, -1.1022 0.5112, 0.09370, -1.1019 0.4731, 0.09830, -1.1003 0.4349, 0.10070, -1.0891 0.3960, 0.10120, -1.0734 0.3566, 0.10020, -1.0834 0.3172, 0.09790, -1.0809 0.2778, 0.09440, -1.0814 0.2393, 0.08960, -1.0783 0.2056, 0.08360, -1.0656 0.1633, 0.07610, -1.0729 0.1261, 0.06710, -1.0689 0.0900, 0.05640, -1.0707 0.0571, 0.04390, -1.0606 0.0283, 0.02940, -1.0620 0.0142, 0.01970, -1.0583 0.0081, 0.01410, -1.0536 0.0026, 0.00780, -1.0139 0.0000, 0.00000, -1.0601 0.0037, -0.00840, -1.1284 0.0112, -0.01420, -0.4085 0.0191, -0.01930, 0.0360 0.0397, -0.03030, 0.5413 0.0706, -0.04420, 0.8059 0.1037, -0.05710, 0.9482 0.1384, -0.06890, 0.9853 0.1741, -0.07950, 1.0032 0.2102, -0.08660, 0.9849 0.2472, -0.09640, 0.9282 0.2844, -0.10270, 0.8554 0.3225, -0.10690, 0.7631 0.3608, -0.10890, 0.6442 0.3991, -0.10830, 0.5119 0.4373, -0.10510, 0.3884 0.4757, -0.09890, 0.2852 0.5137, -0.09070, 0.1613 0.5514, -0.08120, 0.0400 0.5917, -0.06870, -1.1226 0.5917, -0.02380, -1.1344 0.5917, 0.02120, -1.1587 16 Flap element taps 1.0000, 0.00130, -1.6173 0.9365, 0.01390, -1.2239 0.8333, 0.03280, -1.1129 0.7436, 0.04930, -1.1594 0.7049, 0.05670, -1.9535 0.6667, 0.05450, -0.6629 0.6302, 0.03770, 0.7943 0.6083, 0.01980, 0.9573 0.6000, 0.00000, -0.8086 0.6076, -0.01900, -1.6880 0.6285, -0.03060, -1.6899 0.6667, -0.04090, -1.6769 0.7046, -0.04120, -1.6777 0.7429, -0.03210, -1.6804 0.8333, -0.01400, -1.7241 0.9311, -0.00120, -1.7588 --------- Run Conditions: vel=111.3 ft/s Re=0.999x10^6 AOA=70.05 Flap deflection=-60.00 Totals: Cl=0.0168 Cdp=1.0620 Cm(c/4)=-0.0312 Cs=-0.3466 Ch=-0.3500 Main component: Cl=0.2448 Cdp=1.1121 Cm=-0.3288 Flap component: Cl=-0.2280 Cdp=-0.0501 Cm=0.0465 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.5004 0.5871, 0.07930, -1.3953 0.5501, 0.08690, -1.3918 0.5112, 0.09370, -1.4056 0.4731, 0.09830, -1.4101 0.4349, 0.10070, -1.4039 0.3960, 0.10120, -1.3867 0.3566, 0.10020, -1.4132 0.3172, 0.09790, -1.4107 0.2778, 0.09440, -1.4016 0.2393, 0.08960, -1.4001 0.2056, 0.08360, -1.3843 0.1633, 0.07610, -1.3868 0.1261, 0.06710, -1.3699 0.0900, 0.05640, -1.3582 0.0571, 0.04390, -1.3319 0.0283, 0.02940, -1.3284 0.0142, 0.01970, -1.3163 0.0081, 0.01410, -1.3032 0.0026, 0.00780, -1.2556 0.0000, 0.00000, -1.3040 0.0037, -0.00840, -1.4579 0.0112, -0.01420, -0.8573 0.0191, -0.01930, -0.3684 0.0397, -0.03030, 0.2363 0.0706, -0.04420, 0.5982 0.1037, -0.05710, 0.8121 0.1384, -0.06890, 0.9100 0.1741, -0.07950, 0.9780 0.2102, -0.08660, 1.0057 0.2472, -0.09640, 0.9900 0.2844, -0.10270, 0.9495 0.3225, -0.10690, 0.8828 0.3608, -0.10890, 0.7809 0.3991, -0.10830, 0.6506 0.4373, -0.10510, 0.5113 0.4757, -0.09890, 0.3755 0.5137, -0.09070, 0.2075 0.5514, -0.08120, 0.0274 0.5917, -0.06870, -1.3935 0.5917, -0.02380, -1.4146 0.5917, 0.02120, -1.4693 16 Flap element taps 1.0000, 0.00130, -0.9345 0.9365, 0.01390, -1.3096 0.8333, 0.03280, -1.3625 0.7436, 0.04930, -1.4535 0.7049, 0.05670, -2.4204 0.6667, 0.05450, -0.9659 0.6302, 0.03770, 0.7152 0.6083, 0.01980, 0.9657 0.6000, 0.00000, -1.4069 0.6076, -0.01900, -5.2492 0.6285, -0.03060, -3.1889 0.6667, -0.04090, -3.3679 0.7046, -0.04120, -3.2812 0.7429, -0.03210, -1.5229 0.8333, -0.01400, -0.8954 0.9311, -0.00120, -0.6518 --------- Run Conditions: vel=110.3 ft/s Re=0.989x10^6 AOA=80.02 Flap deflection=-60.00 Totals: Cl=0.1454 Cdp=1.3147 Cm(c/4)=-0.1536 Cs=-0.0847 Ch=-0.1875 Main component: Cl=0.0820 Cdp=1.2279 Cm=-0.3754 Flap component: Cl=0.0634 Cdp=0.0868 Cm=-0.1082 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.6453 0.5871, 0.07930, -1.5489 0.5501, 0.08690, -1.5640 0.5112, 0.09370, -1.5533 0.4731, 0.09830, -1.5690 0.4349, 0.10070, -1.5635 0.3960, 0.10120, -1.5392 0.3566, 0.10020, -1.5527 0.3172, 0.09790, -1.5577 0.2778, 0.09440, -1.5671 0.2393, 0.08960, -1.5647 0.2056, 0.08360, -1.5448 0.1633, 0.07610, -1.5387 0.1261, 0.06710, -1.5147 0.0900, 0.05640, -1.4964 0.0571, 0.04390, -1.4636 0.0283, 0.02940, -1.4511 0.0142, 0.01970, -1.4389 0.0081, 0.01410, -1.4233 0.0026, 0.00780, -1.3716 0.0000, 0.00000, -1.4222 0.0037, -0.00840, -1.5166 0.0112, -0.01420, -1.2539 0.0191, -0.01930, -0.7963 0.0397, -0.03030, -0.1532 0.0706, -0.04420, 0.2782 0.1037, -0.05710, 0.5592 0.1384, -0.06890, 0.7220 0.1741, -0.07950, 0.8536 0.2102, -0.08660, 0.9444 0.2472, -0.09640, 0.9870 0.2844, -0.10270, 1.0081 0.3225, -0.10690, 1.0009 0.3608, -0.10890, 0.9610 0.3991, -0.10830, 0.8801 0.4373, -0.10510, 0.7743 0.4757, -0.09890, 0.6457 0.5137, -0.09070, 0.4646 0.5514, -0.08120, 0.2283 0.5917, -0.06870, -1.5465 0.5917, -0.02380, -1.5705 0.5917, 0.02120, -1.6091 16 Flap element taps 1.0000, 0.00130, -0.9549 0.9365, 0.01390, -1.3852 0.8333, 0.03280, -1.4957 0.7436, 0.04930, -1.6400 0.7049, 0.05670, -2.8409 0.6667, 0.05450, -1.4168 0.6302, 0.03770, 0.3732 0.6083, 0.01980, 0.9834 0.6000, 0.00000, 0.1738 0.6076, -0.01900, -2.4510 0.6285, -0.03060, -2.0439 0.6667, -0.04090, -2.1953 0.7046, -0.04120, -2.0814 0.7429, -0.03210, -0.9404 0.8333, -0.01400, -0.5422 0.9311, -0.00120, -0.4778 --------- Run Conditions: vel=110.1 ft/s Re=0.986x10^6 AOA=90.03 Flap deflection=-60.00 Totals: Cl=0.1829 Cdp=1.5133 Cm(c/4)=-0.2449 Cs=0.1837 Ch=-0.0131 Main component: Cl=-0.1042 Cdp=1.2361 Cm=-0.3951 Flap component: Cl=0.2871 Cdp=0.2772 Cm=-0.2281 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.7682 0.5871, 0.07930, -1.6145 0.5501, 0.08690, -1.6320 0.5112, 0.09370, -1.6535 0.4731, 0.09830, -1.6516 0.4349, 0.10070, -1.6410 0.3960, 0.10120, -1.6305 0.3566, 0.10020, -1.6616 0.3172, 0.09790, -1.6633 0.2778, 0.09440, -1.6679 0.2393, 0.08960, -1.6651 0.2056, 0.08360, -1.6509 0.1633, 0.07610, -1.6530 0.1261, 0.06710, -1.6349 0.0900, 0.05640, -1.6179 0.0571, 0.04390, -1.5834 0.0283, 0.02940, -1.5631 0.0142, 0.01970, -1.5487 0.0081, 0.01410, -1.5308 0.0026, 0.00780, -1.4715 0.0000, 0.00000, -1.5222 0.0037, -0.00840, -1.5359 0.0112, -0.01420, -1.5455 0.0191, -0.01930, -1.1774 0.0397, -0.03030, -0.5612 0.0706, -0.04420, -0.1003 0.1037, -0.05710, 0.2156 0.1384, -0.06890, 0.4221 0.1741, -0.07950, 0.6037 0.2102, -0.08660, 0.7472 0.2472, -0.09640, 0.8432 0.2844, -0.10270, 0.9263 0.3225, -0.10690, 0.9791 0.3608, -0.10890, 1.0025 0.3991, -0.10830, 0.9800 0.4373, -0.10510, 0.9309 0.4757, -0.09890, 0.8374 0.5137, -0.09070, 0.6747 0.5514, -0.08120, 0.4172 0.5917, -0.06870, -1.6418 0.5917, -0.02380, -1.6685 0.5917, 0.02120, -1.7124 16 Flap element taps 1.0000, 0.00130, -0.8934 0.9365, 0.01390, -1.3653 0.8333, 0.03280, -1.5647 0.7436, 0.04930, -1.7852 0.7049, 0.05670, -3.2200 0.6667, 0.05450, -1.8950 0.6302, 0.03770, -0.1277 0.6083, 0.01980, 0.6045 0.6000, 0.00000, 0.9452 0.6076, -0.01900, -0.2610 0.6285, -0.03060, -0.5690 0.6667, -0.04090, -1.0194 0.7046, -0.04120, -1.1707 0.7429, -0.03210, -0.3885 0.8333, -0.01400, -0.2575 0.9311, -0.00120, -0.3041 --------- Run Conditions: vel=110.1 ft/s Re=0.986x10^6 AOA=120.01 Flap deflection=-60.00 Totals: Cl=0.0863 Cdp=1.5773 Cm(c/4)=-0.2699 Cs=0.8637 Ch=0.3101 Main component: Cl=-0.4895 Cdp=0.8254 Cm=-0.3489 Flap component: Cl=0.5759 Cdp=0.7519 Cm=-0.2516 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.7591 0.5871, 0.07930, -1.6403 0.5501, 0.08690, -1.6730 0.5112, 0.09370, -1.7031 0.4731, 0.09830, -1.7075 0.4349, 0.10070, -1.7057 0.3960, 0.10120, -1.6741 0.3566, 0.10020, -1.6941 0.3172, 0.09790, -1.6863 0.2778, 0.09440, -1.6768 0.2393, 0.08960, -1.6702 0.2056, 0.08360, -1.6447 0.1633, 0.07610, -1.6735 0.1261, 0.06710, -1.6700 0.0900, 0.05640, -1.6705 0.0571, 0.04390, -1.6224 0.0283, 0.02940, -1.5895 0.0142, 0.01970, -1.5678 0.0081, 0.01410, -1.5459 0.0026, 0.00780, -1.4962 0.0000, 0.00000, -1.5431 0.0037, -0.00840, -1.5302 0.0112, -0.01420, -1.5790 0.0191, -0.01930, -1.6285 0.0397, -0.03030, -1.3876 0.0706, -0.04420, -1.0894 0.1037, -0.05710, -0.8298 0.1384, -0.06890, -0.6376 0.1741, -0.07950, -0.4319 0.2102, -0.08660, -0.2280 0.2472, -0.09640, -0.0720 0.2844, -0.10270, 0.1239 0.3225, -0.10690, 0.3056 0.3608, -0.10890, 0.4966 0.3991, -0.10830, 0.6700 0.4373, -0.10510, 0.8371 0.4757, -0.09890, 0.9595 0.5137, -0.09070, 0.9931 0.5514, -0.08120, 0.8640 0.5917, -0.06870, -1.6616 0.5917, -0.02380, -1.6839 0.5917, 0.02120, -1.6944 16 Flap element taps 1.0000, 0.00130, -0.5433 0.9365, 0.01390, -0.8813 0.8333, 0.03280, -1.4495 0.7436, 0.04930, -1.9964 0.7049, 0.05670, -3.7629 0.6667, 0.05450, -3.1502 0.6302, 0.03770, -1.9535 0.6083, 0.01980, -3.1734 0.6000, 0.00000, -2.8809 0.6076, -0.01900, -0.5113 0.6285, -0.03060, 0.8424 0.6667, -0.04090, 0.9899 0.7046, -0.04120, 0.8659 0.7429, -0.03210, 0.7886 0.8333, -0.01400, 0.6367 0.9311, -0.00120, 0.3826 --------- Run Conditions: vel=113.1 ft/s Re=1.007x10^6 AOA=150.05 Flap deflection=-60.00 Totals: Cl=-0.0602 Cdp=0.7316 Cm(c/4)=-0.1898 Cs=0.6038 Ch=0.0163 Main component: Cl=-0.1158 Cdp=0.1060 Cm=-0.0782 Flap component: Cl=0.0556 Cdp=0.6256 Cm=-0.2159 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.1554 0.5871, 0.07930, -1.1070 0.5501, 0.08690, -1.1119 0.5112, 0.09370, -1.1066 0.4731, 0.09830, -1.1195 0.4349, 0.10070, -1.1198 0.3960, 0.10120, -1.1038 0.3566, 0.10020, -1.1063 0.3172, 0.09790, -1.1059 0.2778, 0.09440, -1.1096 0.2393, 0.08960, -1.1021 0.2056, 0.08360, -1.0984 0.1633, 0.07610, -1.1115 0.1261, 0.06710, -1.1060 0.0900, 0.05640, -1.1161 0.0571, 0.04390, -1.1221 0.0283, 0.02940, -1.1165 0.0142, 0.01970, -1.1059 0.0081, 0.01410, -1.0999 0.0026, 0.00780, -1.0420 0.0000, 0.00000, -1.0826 0.0037, -0.00840, -1.1920 0.0112, -0.01420, -1.5517 0.0191, -0.01930, -1.6339 0.0397, -0.03030, -1.5666 0.0706, -0.04420, -1.4704 0.1037, -0.05710, -1.3761 0.1384, -0.06890, -1.3030 0.1741, -0.07950, -1.2012 0.2102, -0.08660, -1.0915 0.2472, -0.09640, -0.9967 0.2844, -0.10270, -0.8204 0.3225, -0.10690, -0.5961 0.3608, -0.10890, -0.3340 0.3991, -0.10830, -0.0283 0.4373, -0.10510, 0.1267 0.4757, -0.09890, -0.1440 0.5137, -0.09070, -0.7366 0.5514, -0.08120, -1.0340 0.5917, -0.06870, -1.1201 0.5917, -0.02380, -1.1268 0.5917, 0.02120, -1.1346 16 Flap element taps 1.0000, 0.00130, -0.9999 0.9365, 0.01390, -1.0524 0.8333, 0.03280, -1.0834 0.7436, 0.04930, -1.0755 0.7049, 0.05670, -1.0215 0.6667, 0.05450, -0.8544 0.6302, 0.03770, -1.0532 0.6083, 0.01980, -0.9880 0.6000, 0.00000, -0.9389 0.6076, -0.01900, -0.9872 0.6285, -0.03060, -0.1471 0.6667, -0.04090, 0.5278 0.7046, -0.04120, 0.7943 0.7429, -0.03210, 0.9902 0.8333, -0.01400, 0.9768 0.9311, -0.00120, 0.7462 --------- Run Conditions: vel=114.1 ft/s Re=1.016x10^6 AOA=180.07 Flap deflection=-60.00 Totals: Cl=-0.1616 Cdp=0.4620 Cm(c/4)=-0.1231 Cs=0.4622 Ch=-0.0686 Main component: Cl=0.0383 Cdp=-0.0284 Cm=0.0131 Flap component: Cl=-0.1998 Cdp=0.4904 Cm=-0.1764 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.2790 0.5871, 0.07930, -1.1303 0.5501, 0.08690, -1.1286 0.5112, 0.09370, -1.1357 0.4731, 0.09830, -1.1619 0.4349, 0.10070, -1.1703 0.3960, 0.10120, -1.1606 0.3566, 0.10020, -1.1595 0.3172, 0.09790, -1.1299 0.2778, 0.09440, -1.1057 0.2393, 0.08960, -1.0643 0.2056, 0.08360, -1.0205 0.1633, 0.07610, -0.9690 0.1261, 0.06710, -0.9250 0.0900, 0.05640, -0.9068 0.0571, 0.04390, -0.9468 0.0283, 0.02940, -1.0621 0.0142, 0.01970, -1.1839 0.0081, 0.01410, -1.2788 0.0026, 0.00780, -1.3356 0.0000, 0.00000, -1.5228 0.0037, -0.00840, -1.2064 0.0112, -0.01420, -1.0785 0.0191, -0.01930, -1.0270 0.0397, -0.03030, -0.9624 0.0706, -0.04420, -0.9730 0.1037, -0.05710, -0.9849 0.1384, -0.06890, -1.0565 0.1741, -0.07950, -1.1013 0.2102, -0.08660, -1.1366 0.2472, -0.09640, -1.1787 0.2844, -0.10270, -1.2093 0.3225, -0.10690, -1.2189 0.3608, -0.10890, -1.2360 0.3991, -0.10830, -1.2173 0.4373, -0.10510, -1.1965 0.4757, -0.09890, -1.1695 0.5137, -0.09070, -1.1919 0.5514, -0.08120, -1.2095 0.5917, -0.06870, -1.2387 0.5917, -0.02380, -1.2042 0.5917, 0.02120, -1.2282 16 Flap element taps 1.0000, 0.00130, -0.9737 0.9365, 0.01390, -0.9994 0.8333, 0.03280, -1.0266 0.7436, 0.04930, -1.0913 0.7049, 0.05670, -1.1815 0.6667, 0.05450, -1.1636 0.6302, 0.03770, -1.0874 0.6083, 0.01980, -1.0733 0.6000, 0.00000, -1.0603 0.6076, -0.01900, -1.0487 0.6285, -0.03060, -1.0164 0.6667, -0.04090, -0.5150 0.7046, -0.04120, -0.2461 0.7429, -0.03210, 0.6229 0.8333, -0.01400, 0.9367 0.9311, -0.00120, 0.9988 --------- Run Conditions: vel=113.7 ft/s Re=1.012x10^6 AOA=210.03 Flap deflection=-60.00 Totals: Cl=0.0165 Cdp=0.3624 Cm(c/4)=-0.0556 Cs=0.3055 Ch=-0.1315 Main component: Cl=0.3793 Cdp=0.1458 Cm=0.1838 Flap component: Cl=-0.3628 Cdp=0.2166 Cm=-0.1904 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.5307 0.5871, 0.07930, 1.0066 0.5501, 0.08690, 0.8489 0.5112, 0.09370, 0.6306 0.4731, 0.09830, 0.3880 0.4349, 0.10070, 0.1969 0.3960, 0.10120, 0.0572 0.3566, 0.10020, -0.0914 0.3172, 0.09790, -0.2111 0.2778, 0.09440, -0.3543 0.2393, 0.08960, -0.4753 0.2056, 0.08360, -0.6008 0.1633, 0.07610, -0.7167 0.1261, 0.06710, -0.7919 0.0900, 0.05640, -0.8406 0.0571, 0.04390, -0.7636 0.0283, 0.02940, -0.7391 0.0142, 0.01970, -0.7517 0.0081, 0.01410, -0.7586 0.0026, 0.00780, -0.7278 0.0000, 0.00000, -0.7619 0.0037, -0.00840, -0.7345 0.0112, -0.01420, -0.7326 0.0191, -0.01930, -0.7374 0.0397, -0.03030, -0.7415 0.0706, -0.04420, -0.7730 0.1037, -0.05710, -0.7757 0.1384, -0.06890, -0.8086 0.1741, -0.07950, -0.8093 0.2102, -0.08660, -0.8105 0.2472, -0.09640, -0.8174 0.2844, -0.10270, -0.8149 0.3225, -0.10690, -0.8040 0.3608, -0.10890, -0.8038 0.3991, -0.10830, -0.7963 0.4373, -0.10510, -0.7913 0.4757, -0.09890, -0.7813 0.5137, -0.09070, -0.7901 0.5514, -0.08120, -0.8276 0.5917, -0.06870, -0.8567 0.5917, -0.02380, -1.6429 0.5917, 0.02120, -1.5569 16 Flap element taps 1.0000, 0.00130, -1.1882 0.9365, 0.01390, -1.2225 0.8333, 0.03280, -1.3472 0.7436, 0.04930, -0.7558 0.7049, 0.05670, -0.6140 0.6667, 0.05450, -0.9981 0.6302, 0.03770, -0.5791 0.6083, 0.01980, -0.4951 0.6000, 0.00000, -0.4521 0.6076, -0.01900, -0.4805 0.6285, -0.03060, -0.5362 0.6667, -0.04090, -0.6831 0.7046, -0.04120, -0.8581 0.7429, -0.03210, 0.1782 0.8333, -0.01400, 0.5940 0.9311, -0.00120, 0.8873 --------- Run Conditions: vel=111.9 ft/s Re=0.995x10^6 AOA=240.03 Flap deflection=-60.00 Totals: Cl=0.7110 Cdp=0.7362 Cm(c/4)=0.2636 Cs=-0.2482 Ch=0.2973 Main component: Cl=0.4861 Cdp=0.6514 Cm=0.3131 Flap component: Cl=0.2249 Cdp=0.0847 Cm=0.1987 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.7491 0.5871, 0.07930, 0.8958 0.5501, 0.08690, 1.0038 0.5112, 0.09370, 1.0117 0.4731, 0.09830, 0.9558 0.4349, 0.10070, 0.8862 0.3960, 0.10120, 0.8213 0.3566, 0.10020, 0.7034 0.3172, 0.09790, 0.5955 0.2778, 0.09440, 0.4587 0.2393, 0.08960, 0.3190 0.2056, 0.08360, 0.1593 0.1633, 0.07610, -0.0500 0.1261, 0.06710, -0.2527 0.0900, 0.05640, -0.5244 0.0571, 0.04390, -0.8373 0.0283, 0.02940, -1.0498 0.0142, 0.01970, -0.9531 0.0081, 0.01410, -0.9376 0.0026, 0.00780, -0.9091 0.0000, 0.00000, -0.9535 0.0037, -0.00840, -0.9493 0.0112, -0.01420, -0.9534 0.0191, -0.01930, -0.9583 0.0397, -0.03030, -0.9547 0.0706, -0.04420, -0.9648 0.1037, -0.05710, -0.9506 0.1384, -0.06890, -0.9845 0.1741, -0.07950, -0.9809 0.2102, -0.08660, -0.9747 0.2472, -0.09640, -0.9933 0.2844, -0.10270, -0.9975 0.3225, -0.10690, -1.0027 0.3608, -0.10890, -1.0050 0.3991, -0.10830, -1.0074 0.4373, -0.10510, -1.0002 0.4757, -0.09890, -0.9853 0.5137, -0.09070, -0.9822 0.5514, -0.08120, -0.9840 0.5917, -0.06870, -1.0370 0.5917, -0.02380, -1.8371 0.5917, 0.02120, -1.7716 16 Flap element taps 1.0000, 0.00130, -1.3700 0.9365, 0.01390, 0.8210 0.8333, 0.03280, 0.3772 0.7436, 0.04930, -0.6821 0.7049, 0.05670, -2.5338 0.6667, 0.05450, -3.5579 0.6302, 0.03770, -2.6710 0.6083, 0.01980, -1.1648 0.6000, 0.00000, -0.8362 0.6076, -0.01900, -0.8782 0.6285, -0.03060, -1.0219 0.6667, -0.04090, -1.1678 0.7046, -0.04120, -1.3513 0.7429, -0.03210, -1.4532 0.8333, -0.01400, -1.4671 0.9311, -0.00120, -1.3941 --------- Run Conditions: vel=109.9 ft/s Re=0.974x10^6 AOA=269.10 Flap deflection=-60.00 Totals: Cl=0.4398 Cdp=1.4237 Cm(c/4)=0.3608 Cs=-0.4174 Ch=0.2689 Main component: Cl=0.0950 Cdp=1.0507 Cm=0.3672 Flap component: Cl=0.3448 Cdp=0.3730 Cm=0.3512 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.3186 0.5871, 0.07930, 0.6445 0.5501, 0.08690, 0.8357 0.5112, 0.09370, 0.9263 0.4731, 0.09830, 0.9683 0.4349, 0.10070, 0.9983 0.3960, 0.10120, 1.0232 0.3566, 0.10020, 0.9894 0.3172, 0.09790, 0.9543 0.2778, 0.09440, 0.8908 0.2393, 0.08960, 0.8162 0.2056, 0.08360, 0.7195 0.1633, 0.07610, 0.5491 0.1261, 0.06710, 0.3650 0.0900, 0.05640, 0.0771 0.0571, 0.04390, -0.3351 0.0283, 0.02940, -0.8875 0.0142, 0.01970, -1.2317 0.0081, 0.01410, -1.2024 0.0026, 0.00780, -1.0740 0.0000, 0.00000, -1.1146 0.0037, -0.00840, -1.1098 0.0112, -0.01420, -1.1105 0.0191, -0.01930, -1.1146 0.0397, -0.03030, -1.1111 0.0706, -0.04420, -1.1226 0.1037, -0.05710, -1.1024 0.1384, -0.06890, -1.1374 0.1741, -0.07950, -1.1300 0.2102, -0.08660, -1.1189 0.2472, -0.09640, -1.1342 0.2844, -0.10270, -1.1327 0.3225, -0.10690, -1.1405 0.3608, -0.10890, -1.1440 0.3991, -0.10830, -1.1499 0.4373, -0.10510, -1.1453 0.4757, -0.09890, -1.1362 0.5137, -0.09070, -1.1492 0.5514, -0.08120, -1.1622 0.5917, -0.06870, -1.4513 0.5917, -0.02380, -1.3686 0.5917, 0.02120, -1.3327 16 Flap element taps 1.0000, 0.00130, -1.7816 0.9365, 0.01390, 0.9920 0.8333, 0.03280, 0.7655 0.7436, 0.04930, -0.1937 0.7049, 0.05670, -1.9471 0.6667, 0.05450, -3.2948 0.6302, 0.03770, -2.9870 0.6083, 0.01980, -2.4978 0.6000, 0.00000, -1.8551 0.6076, -0.01900, -1.8651 0.6285, -0.03060, -1.8355 0.6667, -0.04090, -1.8131 0.7046, -0.04120, -1.8342 0.7429, -0.03210, -1.8245 0.8333, -0.01400, -1.8120 0.9311, -0.00120, -1.7962