S809 SPOILER FLAP, CLEAN, CHORD = 18 INCHES --------- Run Conditions: vel=101.1 ft/s Re=1.005x10^6 AOA=-5.96 Flap deflection=45.00 Totals: Cl=-0.4269 Cdp=0.3302 Cm(c/4)=-0.0733 Cs=-0.2841 Ch=0.0012 Main component: Cl=-0.5817 Cdp=0.0461 Cm=0.1378 Flap component: Cl=0.1548 Cdp=0.2842 Cm=-0.0964 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1963 0.5905, -0.01667, -0.2814 0.5709, 0.03110, -0.2554 0.5889, 0.07933, -0.3168 0.5500, 0.08689, 0.5126 0.5110, 0.09367, 0.3431 0.4731, 0.09830, 0.2126 0.4349, 0.10070, 0.1985 0.3960, 0.10120, 0.1351 0.3566, 0.10020, 0.1284 0.3172, 0.09790, 0.1269 0.2778, 0.09440, 0.1303 0.2393, 0.08960, 0.1576 0.2056, 0.08360, 0.1839 0.1633, 0.07610, 0.2657 0.1261, 0.06710, 0.3548 0.0900, 0.05640, 0.4922 0.0571, 0.04390, 0.6613 0.0283, 0.02940, 0.8830 0.0142, 0.01970, 0.9997 0.0081, 0.01410, 0.9530 0.0026, 0.00780, 0.6265 0.0000, 0.00000, -0.8589 0.0037, -0.00840, -1.7824 0.0112, -0.01420, -1.4193 0.0191, -0.01930, -1.2297 0.0397, -0.03030, -0.8485 0.0706, -0.04420, -0.8004 0.1037, -0.05710, -0.8232 0.1384, -0.06890, -0.8406 0.1741, -0.07950, -0.8598 0.2102, -0.08660, -0.9093 0.2472, -0.09640, -0.9442 0.2844, -0.10270, -0.9360 0.3225, -0.10690, -0.8876 0.3608, -0.10890, -0.8245 0.3991, -0.10830, -0.6673 0.4373, -0.10510, -0.4317 0.4757, -0.09890, -0.2346 0.5137, -0.09067, -0.1595 0.5611, -0.07859, -0.1608 16 Flap element taps 1.0000, 0.00130, -1.0214 0.9365, 0.01390, -0.9897 0.8333, 0.03280, -0.9788 0.7436, 0.04930, -0.9683 0.7049, 0.05667, -0.9584 0.6662, 0.06411, -0.9598 0.6274, 0.07172, -0.9493 0.6009, 0.07523, -0.9580 0.6069, 0.02889, 0.5609 0.6079, -0.01747, 0.8621 0.6167, -0.06381, -0.3244 0.6558, -0.05300, -0.3528 0.7045, -0.04117, -0.3496 0.7429, -0.03210, -0.2472 0.8333, -0.01400, -0.0575 0.9311, -0.00120, 0.0174 --------- Run Conditions: vel=100.3 ft/s Re=0.996x10^6 AOA=-0.01 Flap deflection=45.00 Totals: Cl=0.0554 Cdp=0.3695 Cm(c/4)=-0.1228 Cs=-0.3695 Ch=0.0517 Main component: Cl=-0.2272 Cdp=-0.0524 Cm=0.0769 Flap component: Cl=0.2826 Cdp=0.4219 Cm=-0.2136 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.3723 0.5905, -0.01667, 0.3363 0.5709, 0.03110, 0.3650 0.5889, 0.07933, 0.3416 0.5500, 0.08689, 0.5127 0.5110, 0.09367, 0.3641 0.4731, 0.09830, 0.2461 0.4349, 0.10070, 0.0013 0.3960, 0.10120, -0.0521 0.3566, 0.10020, -0.0624 0.3172, 0.09790, -0.1028 0.2778, 0.09440, -0.1367 0.2393, 0.08960, -0.1494 0.2056, 0.08360, -0.1749 0.1633, 0.07610, -0.1251 0.1261, 0.06710, -0.0899 0.0900, 0.05640, -0.0042 0.0571, 0.04390, 0.1092 0.0283, 0.02940, 0.3181 0.0142, 0.01970, 0.5603 0.0081, 0.01410, 0.6818 0.0026, 0.00780, 0.9011 0.0000, 0.00000, 0.9565 0.0037, -0.00840, 0.4220 0.0112, -0.01420, 0.2199 0.0191, -0.01930, 0.1536 0.0397, -0.03030, 0.0459 0.0706, -0.04420, -0.0901 0.1037, -0.05710, -0.2094 0.1384, -0.06890, -0.2897 0.1741, -0.07950, -0.3815 0.2102, -0.08660, -0.4913 0.2472, -0.09640, -0.5686 0.2844, -0.10270, -0.6206 0.3225, -0.10690, -0.6331 0.3608, -0.10890, -0.6429 0.3991, -0.10830, -0.5749 0.4373, -0.10510, -0.5290 0.4757, -0.09890, -0.5215 0.5137, -0.09067, 0.0015 0.5611, -0.07859, 0.1957 16 Flap element taps 1.0000, 0.00130, -1.0501 0.9365, 0.01390, -1.0340 0.8333, 0.03280, -1.0392 0.7436, 0.04930, -1.0300 0.7049, 0.05667, -1.0209 0.6662, 0.06411, -1.0278 0.6274, 0.07172, -1.0177 0.6009, 0.07523, -1.0419 0.6069, 0.02889, 0.4819 0.6079, -0.01747, 0.7893 0.6167, -0.06381, 0.3441 0.6558, -0.05300, 0.3211 0.7045, -0.04117, 0.3004 0.7429, -0.03210, 0.3101 0.8333, -0.01400, 0.4578 0.9311, -0.00120, 0.2543 --------- Run Conditions: vel=100.6 ft/s Re=0.997x10^6 AOA=2.99 Flap deflection=45.00 Totals: Cl=0.2633 Cdp=0.3864 Cm(c/4)=-0.1214 Cs=-0.3722 Ch=0.0552 Main component: Cl=-0.0118 Cdp=-0.0632 Cm=0.0333 Flap component: Cl=0.2751 Cdp=0.4497 Cm=-0.2254 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.4102 0.5905, -0.01667, 0.3784 0.5709, 0.03110, 0.4039 0.5889, 0.07933, 0.3847 0.5500, 0.08689, 0.4725 0.5110, 0.09367, 0.3252 0.4731, 0.09830, 0.1702 0.4349, 0.10070, 0.0470 0.3960, 0.10120, -0.1848 0.3566, 0.10020, -0.1918 0.3172, 0.09790, -0.2377 0.2778, 0.09440, -0.2843 0.2393, 0.08960, -0.3194 0.2056, 0.08360, -0.3765 0.1633, 0.07610, -0.3490 0.1261, 0.06710, -0.3525 0.0900, 0.05640, -0.3075 0.0571, 0.04390, -0.2588 0.0283, 0.02940, -0.1341 0.0142, 0.01970, 0.0567 0.0081, 0.01410, 0.1609 0.0026, 0.00780, 0.4392 0.0000, 0.00000, 0.9061 0.0037, -0.00840, 0.8965 0.0112, -0.01420, 0.6951 0.0191, -0.01930, 0.5815 0.0397, -0.03030, 0.3990 0.0706, -0.04420, 0.2115 0.1037, -0.05710, 0.0639 0.1384, -0.06890, -0.0343 0.1741, -0.07950, -0.1453 0.2102, -0.08660, -0.2767 0.2472, -0.09640, -0.3634 0.2844, -0.10270, -0.4374 0.3225, -0.10690, -0.4608 0.3608, -0.10890, -0.4940 0.3991, -0.10830, -0.4415 0.4373, -0.10510, -0.3868 0.4757, -0.09890, -0.3810 0.5137, -0.09067, 0.0702 0.5611, -0.07859, 0.2402 16 Flap element taps 1.0000, 0.00130, -1.0645 0.9365, 0.01390, -1.0481 0.8333, 0.03280, -1.0707 0.7436, 0.04930, -1.0576 0.7049, 0.05667, -1.0454 0.6662, 0.06411, -1.0591 0.6274, 0.07172, -1.0410 0.6009, 0.07523, -1.0626 0.6069, 0.02889, 0.4537 0.6079, -0.01747, 0.7719 0.6167, -0.06381, 0.3812 0.6558, -0.05300, 0.3609 0.7045, -0.04117, 0.3521 0.7429, -0.03210, 0.3320 0.8333, -0.01400, 0.4825 0.9311, -0.00120, 0.2849 --------- Run Conditions: vel=100.5 ft/s Re=0.996x10^6 AOA=6.00 Flap deflection=45.00 Totals: Cl=0.4450 Cdp=0.4001 Cm(c/4)=-0.1144 Cs=-0.3513 Ch=0.0506 Main component: Cl=0.1911 Cdp=-0.0667 Cm=-0.0069 Flap component: Cl=0.2539 Cdp=0.4667 Cm=-0.2286 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.4516 0.5905, -0.01667, 0.3849 0.5709, 0.03110, 0.3974 0.5889, 0.07933, 0.3705 0.5500, 0.08689, 0.3920 0.5110, 0.09367, 0.3121 0.4731, 0.09830, 0.1640 0.4349, 0.10070, -0.0081 0.3960, 0.10120, -0.1726 0.3566, 0.10020, -0.2199 0.3172, 0.09790, -0.3792 0.2778, 0.09440, -0.4318 0.2393, 0.08960, -0.4818 0.2056, 0.08360, -0.5741 0.1633, 0.07610, -0.5702 0.1261, 0.06710, -0.6204 0.0900, 0.05640, -0.6276 0.0571, 0.04390, -0.6672 0.0283, 0.02940, -0.6713 0.0142, 0.01970, -0.6054 0.0081, 0.01410, -0.5963 0.0026, 0.00780, -0.3033 0.0000, 0.00000, 0.2342 0.0037, -0.00840, 0.9878 0.0112, -0.01420, 0.9490 0.0191, -0.01930, 0.8603 0.0397, -0.03030, 0.6718 0.0706, -0.04420, 0.4625 0.1037, -0.05710, 0.3014 0.1384, -0.06890, 0.1977 0.1741, -0.07950, 0.0739 0.2102, -0.08660, -0.0799 0.2472, -0.09640, -0.1711 0.2844, -0.10270, -0.2622 0.3225, -0.10690, -0.2929 0.3608, -0.10890, -0.3484 0.3991, -0.10830, -0.3114 0.4373, -0.10510, -0.2556 0.4757, -0.09890, -0.2419 0.5137, -0.09067, 0.1228 0.5611, -0.07859, 0.2967 16 Flap element taps 1.0000, 0.00130, -1.0740 0.9365, 0.01390, -1.0611 0.8333, 0.03280, -1.0779 0.7436, 0.04930, -1.0582 0.7049, 0.05667, -1.0384 0.6662, 0.06411, -1.0600 0.6274, 0.07172, -1.0417 0.6009, 0.07523, -1.0651 0.6069, 0.02889, 0.4434 0.6079, -0.01747, 0.7768 0.6167, -0.06381, 0.3760 0.6558, -0.05300, 0.3471 0.7045, -0.04117, 0.3366 0.7429, -0.03210, 0.3524 0.8333, -0.01400, 0.4699 0.9311, -0.00120, 0.3323 --------- Run Conditions: vel=101.1 ft/s Re=0.999x10^6 AOA=9.01 Flap deflection=45.00 Totals: Cl=0.5669 Cdp=0.4197 Cm(c/4)=-0.1395 Cs=-0.3258 Ch=0.0248 Main component: Cl=0.2692 Cdp=-0.0554 Cm=-0.0094 Flap component: Cl=0.2977 Cdp=0.4751 Cm=-0.2866 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.3360 0.5905, -0.01667, 0.2899 0.5709, 0.03110, 0.4052 0.5889, 0.07933, 0.2262 0.5500, 0.08689, 0.2802 0.5110, 0.09367, 0.2575 0.4731, 0.09830, 0.2555 0.4349, 0.10070, 0.1616 0.3960, 0.10120, -0.0432 0.3566, 0.10020, -0.1485 0.3172, 0.09790, -0.2753 0.2778, 0.09440, -0.3869 0.2393, 0.08960, -0.4957 0.2056, 0.08360, -0.6518 0.1633, 0.07610, -0.6955 0.1261, 0.06710, -0.7962 0.0900, 0.05640, -0.8614 0.0571, 0.04390, -0.9910 0.0283, 0.02940, -1.1412 0.0142, 0.01970, -1.2244 0.0081, 0.01410, -1.3489 0.0026, 0.00780, -1.1231 0.0000, 0.00000, -0.7870 0.0037, -0.00840, 0.8325 0.0112, -0.01420, 0.9959 0.0191, -0.01930, 0.9727 0.0397, -0.03030, 0.8273 0.0706, -0.04420, 0.6246 0.1037, -0.05710, 0.4620 0.1384, -0.06890, 0.3567 0.1741, -0.07950, 0.2266 0.2102, -0.08660, 0.0519 0.2472, -0.09640, -0.0461 0.2844, -0.10270, -0.1570 0.3225, -0.10690, -0.2040 0.3608, -0.10890, -0.2846 0.3991, -0.10830, -0.2774 0.4373, -0.10510, -0.2381 0.4757, -0.09890, -0.1948 0.5137, -0.09067, -0.1760 0.5611, -0.07859, 0.2203 16 Flap element taps 1.0000, 0.00130, -1.0200 0.9365, 0.01390, -1.0174 0.8333, 0.03280, -1.0505 0.7436, 0.04930, -1.0291 0.7049, 0.05667, -1.0078 0.6662, 0.06411, -1.0316 0.6274, 0.07172, -1.0088 0.6009, 0.07523, -1.0462 0.6069, 0.02889, 0.1102 0.6079, -0.01747, 0.1501 0.6167, -0.06381, 0.1998 0.6558, -0.05300, 0.3085 0.7045, -0.04117, 0.3450 0.7429, -0.03210, 0.3766 0.8333, -0.01400, 0.9230 0.9311, -0.00120, 0.5008 --------- Run Conditions: vel=101.5 ft/s Re=1.003x10^6 AOA=12.02 Flap deflection=45.00 Totals: Cl=0.8163 Cdp=0.4189 Cm(c/4)=-0.1648 Cs=-0.2397 Ch=0.0131 Main component: Cl=0.4877 Cdp=-0.0229 Cm=-0.0612 Flap component: Cl=0.3286 Cdp=0.4418 Cm=-0.3250 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.1828 0.5905, -0.01667, 0.1163 0.5709, 0.03110, 0.1991 0.5889, 0.07933, -0.0250 0.5500, 0.08689, 0.0082 0.5110, 0.09367, -0.0153 0.4731, 0.09830, -0.0055 0.4349, 0.10070, -0.0118 0.3960, 0.10120, -0.0926 0.3566, 0.10020, -0.1552 0.3172, 0.09790, -0.3189 0.2778, 0.09440, -0.4828 0.2393, 0.08960, -0.6383 0.2056, 0.08360, -0.8264 0.1633, 0.07610, -0.9086 0.1261, 0.06710, -1.0700 0.0900, 0.05640, -1.2236 0.0571, 0.04390, -1.4651 0.0283, 0.02940, -1.8589 0.0142, 0.01970, -2.2743 0.0081, 0.01410, -2.6902 0.0026, 0.00780, -2.6325 0.0000, 0.00000, -2.7771 0.0037, -0.00840, 0.2870 0.0112, -0.01420, 0.8892 0.0191, -0.01930, 0.9874 0.0397, -0.03030, 0.9519 0.0706, -0.04420, 0.7925 0.1037, -0.05710, 0.6429 0.1384, -0.06890, 0.5406 0.1741, -0.07950, 0.4072 0.2102, -0.08660, 0.2326 0.2472, -0.09640, 0.1308 0.2844, -0.10270, 0.0074 0.3225, -0.10690, -0.0549 0.3608, -0.10890, -0.1510 0.3991, -0.10830, -0.1679 0.4373, -0.10510, -0.1616 0.4757, -0.09890, -0.1027 0.5137, -0.09067, -0.0645 0.5611, -0.07859, 0.2217 16 Flap element taps 1.0000, 0.00130, -0.9826 0.9365, 0.01390, -0.9868 0.8333, 0.03280, -1.0139 0.7436, 0.04930, -0.9990 0.7049, 0.05667, -0.9756 0.6662, 0.06411, -0.9967 0.6274, 0.07172, -0.9765 0.6009, 0.07523, -1.0178 0.6069, 0.02889, -0.3068 0.6079, -0.01747, -0.7230 0.6167, -0.06381, -0.2586 0.6558, -0.05300, 0.1328 0.7045, -0.04117, 0.3875 0.7429, -0.03210, 0.8028 0.8333, -0.01400, 0.8882 0.9311, -0.00120, 0.5045 --------- Run Conditions: vel=101.6 ft/s Re=1.004x10^6 AOA=15.00 Flap deflection=45.00 Totals: Cl=1.0684 Cdp=0.4166 Cm(c/4)=-0.1811 Cs=-0.1259 Ch=0.0047 Main component: Cl=0.7293 Cdp=0.0075 Cm=-0.1231 Flap component: Cl=0.3391 Cdp=0.4091 Cm=-0.3430 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.1309 0.5905, -0.01667, 0.0538 0.5709, 0.03110, 0.1104 0.5889, 0.07933, -0.3441 0.5500, 0.08689, -0.2964 0.5110, 0.09367, -0.3084 0.4731, 0.09830, -0.3180 0.4349, 0.10070, -0.3094 0.3960, 0.10120, -0.3581 0.3566, 0.10020, -0.3463 0.3172, 0.09790, -0.4015 0.2778, 0.09440, -0.5256 0.2393, 0.08960, -0.7171 0.2056, 0.08360, -0.9581 0.1633, 0.07610, -1.1189 0.1261, 0.06710, -1.3496 0.0900, 0.05640, -1.6029 0.0571, 0.04390, -2.0042 0.0283, 0.02940, -2.6279 0.0142, 0.01970, -3.2402 0.0081, 0.01410, -4.3760 0.0026, 0.00780, -4.6008 0.0000, 0.00000, -5.4438 0.0037, -0.00840, -0.6287 0.0112, -0.01420, 0.5748 0.0191, -0.01930, 0.8725 0.0397, -0.03030, 0.9928 0.0706, -0.04420, 0.9128 0.1037, -0.05710, 0.7955 0.1384, -0.06890, 0.6961 0.1741, -0.07950, 0.5716 0.2102, -0.08660, 0.4094 0.2472, -0.09640, 0.3049 0.2844, -0.10270, 0.1821 0.3225, -0.10690, 0.1040 0.3608, -0.10890, 0.0062 0.3991, -0.10830, -0.0302 0.4373, -0.10510, -0.0453 0.4757, -0.09890, -0.0003 0.5137, -0.09067, 0.0528 0.5611, -0.07859, 0.2170 16 Flap element taps 1.0000, 0.00130, -0.9085 0.9365, 0.01390, -0.9022 0.8333, 0.03280, -0.9278 0.7436, 0.04930, -0.9198 0.7049, 0.05667, -0.8999 0.6662, 0.06411, -0.9155 0.6274, 0.07172, -0.9045 0.6009, 0.07523, -0.9511 0.6069, 0.02889, -0.8125 0.6079, -0.01747, -1.1364 0.6167, -0.06381, -0.4987 0.6558, -0.05300, 0.0909 0.7045, -0.04117, 0.5306 0.7429, -0.03210, 0.9048 0.8333, -0.01400, 0.8897 0.9311, -0.00120, 0.5307 --------- Run Conditions: vel=100.9 ft/s Re=0.996x10^6 AOA=17.97 Flap deflection=45.00 Totals: Cl=0.9923 Cdp=0.6140 Cm(c/4)=-0.2399 Cs=-0.2779 Ch=0.0019 Main component: Cl=0.6671 Cdp=0.2241 Cm=-0.1826 Flap component: Cl=0.3251 Cdp=0.3899 Cm=-0.3406 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0710 0.5905, -0.01667, -0.0210 0.5709, 0.03110, 0.0437 0.5889, 0.07933, -0.9220 0.5500, 0.08689, -0.8978 0.5110, 0.09367, -0.9496 0.4731, 0.09830, -0.9721 0.4349, 0.10070, -0.9005 0.3960, 0.10120, -0.8910 0.3566, 0.10020, -0.8962 0.3172, 0.09790, -0.9156 0.2778, 0.09440, -0.9088 0.2393, 0.08960, -0.8929 0.2056, 0.08360, -0.9125 0.1633, 0.07610, -0.8856 0.1261, 0.06710, -0.8943 0.0900, 0.05640, -0.8719 0.0571, 0.04390, -0.8874 0.0283, 0.02940, -0.9022 0.0142, 0.01970, -0.8949 0.0081, 0.01410, -0.9253 0.0026, 0.00780, -0.8391 0.0000, 0.00000, -1.1773 0.0037, -0.00840, 0.3949 0.0112, -0.01420, 0.8678 0.0191, -0.01930, 0.9682 0.0397, -0.03030, 0.9708 0.0706, -0.04420, 0.8666 0.1037, -0.05710, 0.7490 0.1384, -0.06890, 0.6410 0.1741, -0.07950, 0.5261 0.2102, -0.08660, 0.3798 0.2472, -0.09640, 0.2733 0.2844, -0.10270, 0.1579 0.3225, -0.10690, 0.0725 0.3608, -0.10890, -0.0162 0.3991, -0.10830, -0.0561 0.4373, -0.10510, -0.0657 0.4757, -0.09890, -0.0188 0.5137, -0.09067, 0.0314 0.5611, -0.07859, 0.1829 16 Flap element taps 1.0000, 0.00130, -0.7977 0.9365, 0.01390, -0.8001 0.8333, 0.03280, -0.8317 0.7436, 0.04930, -0.8392 0.7049, 0.05667, -0.8319 0.6662, 0.06411, -0.8596 0.6274, 0.07172, -0.8783 0.6009, 0.07523, -1.1251 0.6069, 0.02889, -1.1303 0.6079, -0.01747, -1.0685 0.6167, -0.06381, -0.5945 0.6558, -0.05300, 0.0510 0.7045, -0.04117, 0.5598 0.7429, -0.03210, 0.9193 0.8333, -0.01400, 0.8884 0.9311, -0.00120, 0.5363 --------- Run Conditions: vel=101.2 ft/s Re=0.997x10^6 AOA=19.96 Flap deflection=45.00 Totals: Cl=0.9641 Cdp=0.6681 Cm(c/4)=-0.2428 Cs=-0.2988 Ch=0.0030 Main component: Cl=0.6541 Cdp=0.2537 Cm=-0.1835 Flap component: Cl=0.3099 Cdp=0.4143 Cm=-0.3429 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0743 0.5905, -0.01667, -0.0195 0.5709, 0.03110, 0.0429 0.5889, 0.07933, -0.9442 0.5500, 0.08689, -0.8939 0.5110, 0.09367, -0.9475 0.4731, 0.09830, -0.9745 0.4349, 0.10070, -0.9077 0.3960, 0.10120, -0.8685 0.3566, 0.10020, -0.8655 0.3172, 0.09790, -0.8708 0.2778, 0.09440, -0.8699 0.2393, 0.08960, -0.8533 0.2056, 0.08360, -0.8593 0.1633, 0.07610, -0.8397 0.1261, 0.06710, -0.8438 0.0900, 0.05640, -0.8270 0.0571, 0.04390, -0.8384 0.0283, 0.02940, -0.8466 0.0142, 0.01970, -0.8308 0.0081, 0.01410, -0.8574 0.0026, 0.00780, -0.7845 0.0000, 0.00000, -1.0886 0.0037, -0.00840, 0.3385 0.0112, -0.01420, 0.8397 0.0191, -0.01930, 0.9559 0.0397, -0.03030, 0.9798 0.0706, -0.04420, 0.8939 0.1037, -0.05710, 0.7859 0.1384, -0.06890, 0.6733 0.1741, -0.07950, 0.5634 0.2102, -0.08660, 0.4274 0.2472, -0.09640, 0.3160 0.2844, -0.10270, 0.2041 0.3225, -0.10690, 0.1076 0.3608, -0.10890, 0.0238 0.3991, -0.10830, -0.0280 0.4373, -0.10510, -0.0374 0.4757, -0.09890, 0.0042 0.5137, -0.09067, 0.0561 0.5611, -0.07859, 0.1652 16 Flap element taps 1.0000, 0.00130, -0.8414 0.9365, 0.01390, -0.8352 0.8333, 0.03280, -0.8632 0.7436, 0.04930, -0.8729 0.7049, 0.05667, -0.8620 0.6662, 0.06411, -0.8828 0.6274, 0.07172, -0.9005 0.6009, 0.07523, -1.0707 0.6069, 0.02889, -1.1028 0.6079, -0.01747, -1.0216 0.6167, -0.06381, -0.5823 0.6558, -0.05300, 0.0601 0.7045, -0.04117, 0.5636 0.7429, -0.03210, 0.9258 0.8333, -0.01400, 0.8905 0.9311, -0.00120, 0.5301 --------- Run Conditions: vel=103.3 ft/s Re=1.008x10^6 AOA=23.97 Flap deflection=45.00 Totals: Cl=1.0217 Cdp=0.8240 Cm(c/4)=-0.2685 Cs=-0.3379 Ch=0.0063 Main component: Cl=0.7205 Cdp=0.3353 Cm=-0.2109 Flap component: Cl=0.3012 Cdp=0.4887 Cm=-0.3748 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0576 0.5905, -0.01667, -0.0216 0.5709, 0.03110, 0.0538 0.5889, 0.07933, -1.0438 0.5500, 0.08689, -0.9855 0.5110, 0.09367, -1.0181 0.4731, 0.09830, -1.0533 0.4349, 0.10070, -1.0412 0.3960, 0.10120, -0.9750 0.3566, 0.10020, -0.9326 0.3172, 0.09790, -0.9280 0.2778, 0.09440, -0.9587 0.2393, 0.08960, -0.9559 0.2056, 0.08360, -0.9504 0.1633, 0.07610, -0.9559 0.1261, 0.06710, -0.9416 0.0900, 0.05640, -0.9437 0.0571, 0.04390, -0.9324 0.0283, 0.02940, -0.9362 0.0142, 0.01970, -0.9394 0.0081, 0.01410, -0.9463 0.0026, 0.00780, -0.8830 0.0000, 0.00000, -0.9856 0.0037, -0.00840, 0.0975 0.0112, -0.01420, 0.7239 0.0191, -0.01930, 0.9076 0.0397, -0.03030, 0.9997 0.0706, -0.04420, 0.9564 0.1037, -0.05710, 0.8755 0.1384, -0.06890, 0.7607 0.1741, -0.07950, 0.6551 0.2102, -0.08660, 0.5477 0.2472, -0.09640, 0.4222 0.2844, -0.10270, 0.3186 0.3225, -0.10690, 0.2146 0.3608, -0.10890, 0.1174 0.3991, -0.10830, 0.0447 0.4373, -0.10510, 0.0339 0.4757, -0.09890, 0.0537 0.5137, -0.09067, 0.1170 0.5611, -0.07859, 0.1604 16 Flap element taps 1.0000, 0.00130, -0.9832 0.9365, 0.01390, -0.9990 0.8333, 0.03280, -1.0141 0.7436, 0.04930, -1.0287 0.7049, 0.05667, -1.0190 0.6662, 0.06411, -1.0358 0.6274, 0.07172, -1.0616 0.6009, 0.07523, -1.1566 0.6069, 0.02889, -1.1659 0.6079, -0.01747, -1.1239 0.6167, -0.06381, -0.6621 0.6558, -0.05300, 0.0550 0.7045, -0.04117, 0.5979 0.7429, -0.03210, 0.9434 0.8333, -0.01400, 0.8973 0.9311, -0.00120, 0.5457 --------- Run Conditions: vel=101.5 ft/s Re=0.990x10^6 AOA=26.98 Flap deflection=45.00 Totals: Cl=1.1599 Cdp=1.0089 Cm(c/4)=-0.3112 Cs=-0.3729 Ch=0.0100 Main component: Cl=0.8484 Cdp=0.4391 Cm=-0.2604 Flap component: Cl=0.3115 Cdp=0.5698 Cm=-0.4236 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0302 0.5905, -0.01667, -0.0730 0.5709, 0.03110, -0.0096 0.5889, 0.07933, -1.2807 0.5500, 0.08689, -1.1994 0.5110, 0.09367, -1.2390 0.4731, 0.09830, -1.2703 0.4349, 0.10070, -1.2835 0.3960, 0.10120, -1.2413 0.3566, 0.10020, -1.1887 0.3172, 0.09790, -1.1577 0.2778, 0.09440, -1.1747 0.2393, 0.08960, -1.1683 0.2056, 0.08360, -1.1686 0.1633, 0.07610, -1.1813 0.1261, 0.06710, -1.1684 0.0900, 0.05640, -1.1689 0.0571, 0.04390, -1.1551 0.0283, 0.02940, -1.1528 0.0142, 0.01970, -1.1558 0.0081, 0.01410, -1.1617 0.0026, 0.00780, -1.0918 0.0000, 0.00000, -1.1853 0.0037, -0.00840, -0.2194 0.0112, -0.01420, 0.5508 0.0191, -0.01930, 0.8091 0.0397, -0.03030, 0.9803 0.0706, -0.04420, 0.9830 0.1037, -0.05710, 0.9308 0.1384, -0.06890, 0.8287 0.1741, -0.07950, 0.7316 0.2102, -0.08660, 0.6336 0.2472, -0.09640, 0.5120 0.2844, -0.10270, 0.4071 0.3225, -0.10690, 0.3002 0.3608, -0.10890, 0.1974 0.3991, -0.10830, 0.1127 0.4373, -0.10510, 0.0899 0.4757, -0.09890, 0.0923 0.5137, -0.09067, 0.1532 0.5611, -0.07859, 0.1971 16 Flap element taps 1.0000, 0.00130, -1.2025 0.9365, 0.01390, -1.2326 0.8333, 0.03280, -1.2379 0.7436, 0.04930, -1.2508 0.7049, 0.05667, -1.2349 0.6662, 0.06411, -1.2570 0.6274, 0.07172, -1.2949 0.6009, 0.07523, -1.4145 0.6069, 0.02889, -1.4133 0.6079, -0.01747, -1.3686 0.6167, -0.06381, -0.8127 0.6558, -0.05300, 0.0278 0.7045, -0.04117, 0.6139 0.7429, -0.03210, 0.9458 0.8333, -0.01400, 0.8934 0.9311, -0.00120, 0.5269 --------- Run Conditions: vel=102.5 ft/s Re=0.999x10^6 AOA=29.98 Flap deflection=45.00 Totals: Cl=1.2210 Cdp=1.1549 Cm(c/4)=-0.3392 Cs=-0.3902 Ch=0.0165 Main component: Cl=0.9185 Cdp=0.5305 Cm=-0.2952 Flap component: Cl=0.3026 Cdp=0.6243 Cm=-0.4527 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0336 0.5905, -0.01667, -0.0807 0.5709, 0.03110, -0.0255 0.5889, 0.07933, -1.4128 0.5500, 0.08689, -1.3503 0.5110, 0.09367, -1.3735 0.4731, 0.09830, -1.4014 0.4349, 0.10070, -1.4223 0.3960, 0.10120, -1.4054 0.3566, 0.10020, -1.3665 0.3172, 0.09790, -1.3054 0.2778, 0.09440, -1.2962 0.2393, 0.08960, -1.2738 0.2056, 0.08360, -1.2736 0.1633, 0.07610, -1.2915 0.1261, 0.06710, -1.2811 0.0900, 0.05640, -1.2808 0.0571, 0.04390, -1.2658 0.0283, 0.02940, -1.2610 0.0142, 0.01970, -1.2632 0.0081, 0.01410, -1.2685 0.0026, 0.00780, -1.1955 0.0000, 0.00000, -1.2828 0.0037, -0.00840, -0.4690 0.0112, -0.01420, 0.3978 0.0191, -0.01930, 0.7140 0.0397, -0.03030, 0.9544 0.0706, -0.04420, 0.9999 0.1037, -0.05710, 0.9729 0.1384, -0.06890, 0.8874 0.1741, -0.07950, 0.8029 0.2102, -0.08660, 0.7137 0.2472, -0.09640, 0.5985 0.2844, -0.10270, 0.4969 0.3225, -0.10690, 0.3895 0.3608, -0.10890, 0.2848 0.3991, -0.10830, 0.1956 0.4373, -0.10510, 0.1618 0.4757, -0.09890, 0.1503 0.5137, -0.09067, 0.2049 0.5611, -0.07859, 0.2361 16 Flap element taps 1.0000, 0.00130, -1.2868 0.9365, 0.01390, -1.3237 0.8333, 0.03280, -1.3451 0.7436, 0.04930, -1.3746 0.7049, 0.05667, -1.3681 0.6662, 0.06411, -1.3885 0.6274, 0.07172, -1.4310 0.6009, 0.07523, -1.5690 0.6069, 0.02889, -1.5622 0.6079, -0.01747, -1.5045 0.6167, -0.06381, -0.8859 0.6558, -0.05300, 0.0398 0.7045, -0.04117, 0.6461 0.7429, -0.03210, 0.9585 0.8333, -0.01400, 0.9020 0.9311, -0.00120, 0.5350 --------- Run Conditions: vel=101.5 ft/s Re=0.988x10^6 AOA=34.95 Flap deflection=45.00 Totals: Cl=1.2524 Cdp=1.3684 Cm(c/4)=-0.3748 Cs=-0.4041 Ch=0.0195 Main component: Cl=0.9852 Cdp=0.6735 Cm=-0.3411 Flap component: Cl=0.2672 Cdp=0.6948 Cm=-0.4863 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0474 0.5905, -0.01667, -0.0640 0.5709, 0.03110, -0.0110 0.5889, 0.07933, -1.6265 0.5500, 0.08689, -1.5462 0.5110, 0.09367, -1.5728 0.4731, 0.09830, -1.5859 0.4349, 0.10070, -1.5891 0.3960, 0.10120, -1.5658 0.3566, 0.10020, -1.5439 0.3172, 0.09790, -1.4895 0.2778, 0.09440, -1.4678 0.2393, 0.08960, -1.4291 0.2056, 0.08360, -1.4160 0.1633, 0.07610, -1.4346 0.1261, 0.06710, -1.4205 0.0900, 0.05640, -1.4210 0.0571, 0.04390, -1.4041 0.0283, 0.02940, -1.3934 0.0142, 0.01970, -1.3948 0.0081, 0.01410, -1.3996 0.0026, 0.00780, -1.3251 0.0000, 0.00000, -1.4075 0.0037, -0.00840, -0.8553 0.0112, -0.01420, 0.1174 0.0191, -0.01930, 0.5167 0.0397, -0.03030, 0.8648 0.0706, -0.04420, 0.9840 0.1037, -0.05710, 1.0008 0.1384, -0.06890, 0.9460 0.1741, -0.07950, 0.8836 0.2102, -0.08660, 0.8152 0.2472, -0.09640, 0.7160 0.2844, -0.10270, 0.6243 0.3225, -0.10690, 0.5200 0.3608, -0.10890, 0.4157 0.3991, -0.10830, 0.3228 0.4373, -0.10510, 0.2776 0.4757, -0.09890, 0.2483 0.5137, -0.09067, 0.2898 0.5611, -0.07859, 0.2958 16 Flap element taps 1.0000, 0.00130, -1.3882 0.9365, 0.01390, -1.4538 0.8333, 0.03280, -1.4921 0.7436, 0.04930, -1.5012 0.7049, 0.05667, -1.4978 0.6662, 0.06411, -1.5088 0.6274, 0.07172, -1.5499 0.6009, 0.07523, -1.7660 0.6069, 0.02889, -1.7228 0.6079, -0.01747, -1.6608 0.6167, -0.06381, -0.9518 0.6558, -0.05300, 0.0688 0.7045, -0.04117, 0.6751 0.7429, -0.03210, 0.9603 0.8333, -0.01400, 0.9042 0.9311, -0.00120, 0.5463 --------- Run Conditions: vel=101.6 ft/s Re=0.989x10^6 AOA=39.96 Flap deflection=45.00 Totals: Cl=1.2464 Cdp=1.5778 Cm(c/4)=-0.4094 Cs=-0.4089 Ch=0.0272 Main component: Cl=1.0197 Cdp=0.8237 Cm=-0.3837 Flap component: Cl=0.2267 Cdp=0.7542 Cm=-0.5178 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0622 0.5905, -0.01667, -0.0563 0.5709, 0.03110, -0.0254 0.5889, 0.07933, -1.8437 0.5500, 0.08689, -1.7294 0.5110, 0.09367, -1.7756 0.4731, 0.09830, -1.7562 0.4349, 0.10070, -1.7596 0.3960, 0.10120, -1.7286 0.3566, 0.10020, -1.7072 0.3172, 0.09790, -1.6476 0.2778, 0.09440, -1.6179 0.2393, 0.08960, -1.5810 0.2056, 0.08360, -1.5526 0.1633, 0.07610, -1.5614 0.1261, 0.06710, -1.5386 0.0900, 0.05640, -1.5401 0.0571, 0.04390, -1.5224 0.0283, 0.02940, -1.5050 0.0142, 0.01970, -1.5024 0.0081, 0.01410, -1.5025 0.0026, 0.00780, -1.4300 0.0000, 0.00000, -1.5131 0.0037, -0.00840, -1.1974 0.0112, -0.01420, -0.1685 0.0191, -0.01930, 0.3004 0.0397, -0.03030, 0.7437 0.0706, -0.04420, 0.9372 0.1037, -0.05710, 0.9982 0.1384, -0.06890, 0.9732 0.1741, -0.07950, 0.9389 0.2102, -0.08660, 0.8954 0.2472, -0.09640, 0.8111 0.2844, -0.10270, 0.7327 0.3225, -0.10690, 0.6337 0.3608, -0.10890, 0.5388 0.3991, -0.10830, 0.4401 0.4373, -0.10510, 0.3905 0.4757, -0.09890, 0.3481 0.5137, -0.09067, 0.3733 0.5611, -0.07859, 0.3579 16 Flap element taps 1.0000, 0.00130, -1.4617 0.9365, 0.01390, -1.5290 0.8333, 0.03280, -1.5831 0.7436, 0.04930, -1.6201 0.7049, 0.05667, -1.6035 0.6662, 0.06411, -1.6301 0.6274, 0.07172, -1.7039 0.6009, 0.07523, -2.0183 0.6069, 0.02889, -1.9298 0.6079, -0.01747, -1.8306 0.6167, -0.06381, -1.0233 0.6558, -0.05300, 0.1013 0.7045, -0.04117, 0.7010 0.7429, -0.03210, 0.9641 0.8333, -0.01400, 0.9112 0.9311, -0.00120, 0.5620 --------- Run Conditions: vel=101.1 ft/s Re=0.982x10^6 AOA=44.96 Flap deflection=45.00 Totals: Cl=1.1663 Cdp=1.7472 Cm(c/4)=-0.4339 Cs=-0.4122 Ch=0.0316 Main component: Cl=0.9993 Cdp=0.9450 Cm=-0.4104 Flap component: Cl=0.1670 Cdp=0.8022 Cm=-0.5385 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0967 0.5905, -0.01667, -0.0097 0.5709, 0.03110, 0.0025 0.5889, 0.07933, -1.9528 0.5500, 0.08689, -1.8570 0.5110, 0.09367, -1.8732 0.4731, 0.09830, -1.8558 0.4349, 0.10070, -1.8431 0.3960, 0.10120, -1.7989 0.3566, 0.10020, -1.7889 0.3172, 0.09790, -1.7354 0.2778, 0.09440, -1.7120 0.2393, 0.08960, -1.6606 0.2056, 0.08360, -1.6173 0.1633, 0.07610, -1.6244 0.1261, 0.06710, -1.5883 0.0900, 0.05640, -1.5863 0.0571, 0.04390, -1.5653 0.0283, 0.02940, -1.5525 0.0142, 0.01970, -1.5441 0.0081, 0.01410, -1.5420 0.0026, 0.00780, -1.4719 0.0000, 0.00000, -1.5556 0.0037, -0.00840, -1.4398 0.0112, -0.01420, -0.4184 0.0191, -0.01930, 0.0926 0.0397, -0.03030, 0.6103 0.0706, -0.04420, 0.8653 0.1037, -0.05710, 0.9709 0.1384, -0.06890, 0.9714 0.1741, -0.07950, 0.9632 0.2102, -0.08660, 0.9469 0.2472, -0.09640, 0.8795 0.2844, -0.10270, 0.8169 0.3225, -0.10690, 0.7244 0.3608, -0.10890, 0.6406 0.3991, -0.10830, 0.5428 0.4373, -0.10510, 0.4903 0.4757, -0.09890, 0.4390 0.5137, -0.09067, 0.4517 0.5611, -0.07859, 0.4176 16 Flap element taps 1.0000, 0.00130, -1.5214 0.9365, 0.01390, -1.6016 0.8333, 0.03280, -1.6633 0.7436, 0.04930, -1.6923 0.7049, 0.05667, -1.6854 0.6662, 0.06411, -1.7111 0.6274, 0.07172, -1.7908 0.6009, 0.07523, -2.1099 0.6069, 0.02889, -2.0193 0.6079, -0.01747, -1.9426 0.6167, -0.06381, -1.0428 0.6558, -0.05300, 0.1473 0.7045, -0.04117, 0.7238 0.7429, -0.03210, 0.9628 0.8333, -0.01400, 0.9113 0.9311, -0.00120, 0.5761 --------- Run Conditions: vel=104.3 ft/s Re=1.009x10^6 AOA=59.97 Flap deflection=45.00 Totals: Cl=0.7603 Cdp=2.1187 Cm(c/4)=-0.4853 Cs=-0.4021 Ch=0.0441 Main component: Cl=0.8188 Cdp=1.2361 Cm=-0.4631 Flap component: Cl=-0.0585 Cdp=0.8825 Cm=-0.5759 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.2611 0.5905, -0.01667, 0.1387 0.5709, 0.03110, 0.1435 0.5889, 0.07933, -2.0889 0.5500, 0.08689, -2.0411 0.5110, 0.09367, -2.0392 0.4731, 0.09830, -2.0363 0.4349, 0.10070, -1.9892 0.3960, 0.10120, -1.9512 0.3566, 0.10020, -1.9111 0.3172, 0.09790, -1.8640 0.2778, 0.09440, -1.8403 0.2393, 0.08960, -1.8038 0.2056, 0.08360, -1.7687 0.1633, 0.07610, -1.7256 0.1261, 0.06710, -1.6992 0.0900, 0.05640, -1.6686 0.0571, 0.04390, -1.6506 0.0283, 0.02940, -1.6436 0.0142, 0.01970, -1.6279 0.0081, 0.01410, -1.6302 0.0026, 0.00780, -1.5471 0.0000, 0.00000, -1.6253 0.0037, -0.00840, -1.8023 0.0112, -0.01420, -1.0573 0.0191, -0.01930, -0.5040 0.0397, -0.03030, 0.1583 0.0706, -0.04420, 0.5490 0.1037, -0.05710, 0.7607 0.1384, -0.06890, 0.8731 0.1741, -0.07950, 0.9432 0.2102, -0.08660, 0.9773 0.2472, -0.09640, 0.9818 0.2844, -0.10270, 0.9657 0.3225, -0.10690, 0.9384 0.3608, -0.10890, 0.8816 0.3991, -0.10830, 0.8199 0.4373, -0.10510, 0.7618 0.4757, -0.09890, 0.6983 0.5137, -0.09067, 0.6764 0.5611, -0.07859, 0.6148 16 Flap element taps 1.0000, 0.00130, -1.6575 0.9365, 0.01390, -1.7141 0.8333, 0.03280, -1.7812 0.7436, 0.04930, -1.8272 0.7049, 0.05667, -1.8344 0.6662, 0.06411, -1.8693 0.6274, 0.07172, -1.9251 0.6009, 0.07523, -2.2332 0.6069, 0.02889, -2.1089 0.6079, -0.01747, -2.0587 0.6167, -0.06381, -0.9831 0.6558, -0.05300, 0.3042 0.7045, -0.04117, 0.7952 0.7429, -0.03210, 0.9614 0.8333, -0.01400, 0.9340 0.9311, -0.00120, 0.6507 --------- Run Conditions: vel=102.4 ft/s Re=0.989x10^6 AOA=70.00 Flap deflection=45.00 Totals: Cl=0.4063 Cdp=2.2919 Cm(c/4)=-0.5303 Cs=-0.4021 Ch=0.0566 Main component: Cl=0.6388 Cdp=1.3577 Cm=-0.4792 Flap component: Cl=-0.2325 Cdp=0.9341 Cm=-0.6243 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.3912 0.5905, -0.01667, 0.2603 0.5709, 0.03110, 0.2595 0.5889, 0.07933, -2.0993 0.5500, 0.08689, -2.0818 0.5110, 0.09367, -2.0631 0.4731, 0.09830, -2.0506 0.4349, 0.10070, -2.0118 0.3960, 0.10120, -1.9705 0.3566, 0.10020, -1.9363 0.3172, 0.09790, -1.8968 0.2778, 0.09440, -1.8780 0.2393, 0.08960, -1.8439 0.2056, 0.08360, -1.8247 0.1633, 0.07610, -1.7943 0.1261, 0.06710, -1.7744 0.0900, 0.05640, -1.7420 0.0571, 0.04390, -1.7240 0.0283, 0.02940, -1.7158 0.0142, 0.01970, -1.7030 0.0081, 0.01410, -1.7035 0.0026, 0.00780, -1.6141 0.0000, 0.00000, -1.6913 0.0037, -0.00840, -1.8601 0.0112, -0.01420, -1.4160 0.0191, -0.01930, -0.8858 0.0397, -0.03030, -0.1815 0.0706, -0.04420, 0.2763 0.1037, -0.05710, 0.5448 0.1384, -0.06890, 0.7156 0.1741, -0.07950, 0.8360 0.2102, -0.08660, 0.9151 0.2472, -0.09640, 0.9650 0.2844, -0.10270, 0.9890 0.3225, -0.10690, 1.0017 0.3608, -0.10890, 0.9777 0.3991, -0.10830, 0.9430 0.4373, -0.10510, 0.9024 0.4757, -0.09890, 0.8462 0.5137, -0.09067, 0.8179 0.5611, -0.07859, 0.7480 16 Flap element taps 1.0000, 0.00130, -1.7874 0.9365, 0.01390, -1.8518 0.8333, 0.03280, -1.9342 0.7436, 0.04930, -2.0206 0.7049, 0.05667, -2.0340 0.6662, 0.06411, -2.0698 0.6274, 0.07172, -2.1268 0.6009, 0.07523, -2.4551 0.6069, 0.02889, -2.3010 0.6079, -0.01747, -2.2471 0.6167, -0.06381, -0.9683 0.6558, -0.05300, 0.4130 0.7045, -0.04117, 0.8358 0.7429, -0.03210, 0.9726 0.8333, -0.01400, 0.9609 0.9311, -0.00120, 0.7224 --------- Run Conditions: vel=104.9 ft/s Re=1.011x10^6 AOA=79.95 Flap deflection=45.00 Totals: Cl=0.0176 Cdp=2.2690 Cm(c/4)=-0.5355 Cs=-0.3787 Ch=0.0612 Main component: Cl=0.4206 Cdp=1.3953 Cm=-0.4781 Flap component: Cl=-0.4030 Cdp=0.8737 Cm=-0.6167 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.5441 0.5905, -0.01667, 0.4095 0.5709, 0.03110, 0.4126 0.5889, 0.07933, -2.1298 0.5500, 0.08689, -2.1128 0.5110, 0.09367, -2.1559 0.4731, 0.09830, -1.9887 0.4349, 0.10070, -1.9662 0.3960, 0.10120, -1.9471 0.3566, 0.10020, -1.9251 0.3172, 0.09790, -1.8960 0.2778, 0.09440, -1.8751 0.2393, 0.08960, -1.8362 0.2056, 0.08360, -1.8157 0.1633, 0.07610, -1.7731 0.1261, 0.06710, -1.7410 0.0900, 0.05640, -1.6949 0.0571, 0.04390, -1.6641 0.0283, 0.02940, -1.6496 0.0142, 0.01970, -1.6341 0.0081, 0.01410, -1.6372 0.0026, 0.00780, -1.5428 0.0000, 0.00000, -1.6218 0.0037, -0.00840, -1.6585 0.0112, -0.01420, -1.5638 0.0191, -0.01930, -1.1265 0.0397, -0.03030, -0.4664 0.0706, -0.04420, -0.0002 0.1037, -0.05710, 0.2929 0.1384, -0.06890, 0.5052 0.1741, -0.07950, 0.6595 0.2102, -0.08660, 0.7696 0.2472, -0.09640, 0.8592 0.2844, -0.10270, 0.9199 0.3225, -0.10690, 0.9761 0.3608, -0.10890, 0.9856 0.3991, -0.10830, 0.9898 0.4373, -0.10510, 0.9740 0.4757, -0.09890, 0.9385 0.5137, -0.09067, 0.9182 0.5611, -0.07859, 0.8571 16 Flap element taps 1.0000, 0.00130, -1.7580 0.9365, 0.01390, -1.8095 0.8333, 0.03280, -1.8919 0.7436, 0.04930, -1.9610 0.7049, 0.05667, -1.9685 0.6662, 0.06411, -2.0300 0.6274, 0.07172, -2.1050 0.6009, 0.07523, -2.4113 0.6069, 0.02889, -2.1311 0.6079, -0.01747, -2.0919 0.6167, -0.06381, -0.7780 0.6558, -0.05300, 0.5286 0.7045, -0.04117, 0.8626 0.7429, -0.03210, 0.9669 0.8333, -0.01400, 0.9698 0.9311, -0.00120, 0.7958 --------- Run Conditions: vel=103.4 ft/s Re=0.997x10^6 AOA=89.99 Flap deflection=45.00 Totals: Cl=-0.3237 Cdp=2.1284 Cm(c/4)=-0.5352 Cs=-0.3241 Ch=0.0562 Main component: Cl=0.2218 Cdp=1.3433 Cm=-0.4536 Flap component: Cl=-0.5455 Cdp=0.7851 Cm=-0.6136 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.7158 0.5905, -0.01667, 0.5774 0.5709, 0.03110, 0.5992 0.5889, 0.07933, -1.9819 0.5500, 0.08689, -1.9302 0.5110, 0.09367, -1.9907 0.4731, 0.09830, -1.8930 0.4349, 0.10070, -1.8402 0.3960, 0.10120, -1.8469 0.3566, 0.10020, -1.8154 0.3172, 0.09790, -1.7774 0.2778, 0.09440, -1.7789 0.2393, 0.08960, -1.7666 0.2056, 0.08360, -1.7780 0.1633, 0.07610, -1.7392 0.1261, 0.06710, -1.7337 0.0900, 0.05640, -1.6906 0.0571, 0.04390, -1.6546 0.0283, 0.02940, -1.6301 0.0142, 0.01970, -1.6200 0.0081, 0.01410, -1.6302 0.0026, 0.00780, -1.5304 0.0000, 0.00000, -1.6044 0.0037, -0.00840, -1.6182 0.0112, -0.01420, -1.6875 0.0191, -0.01930, -1.3547 0.0397, -0.03030, -0.7524 0.0706, -0.04420, -0.2928 0.1037, -0.05710, 0.0148 0.1384, -0.06890, 0.2595 0.1741, -0.07950, 0.4408 0.2102, -0.08660, 0.5771 0.2472, -0.09640, 0.7002 0.2844, -0.10270, 0.7982 0.3225, -0.10690, 0.9016 0.3608, -0.10890, 0.9445 0.3991, -0.10830, 0.9913 0.4373, -0.10510, 1.0078 0.4757, -0.09890, 1.0010 0.5137, -0.09067, 0.9991 0.5611, -0.07859, 0.9618 16 Flap element taps 1.0000, 0.00130, -1.7378 0.9365, 0.01390, -1.7650 0.8333, 0.03280, -1.8240 0.7436, 0.04930, -1.8815 0.7049, 0.05667, -1.8974 0.6662, 0.06411, -1.9326 0.6274, 0.07172, -1.9710 0.6009, 0.07523, -2.2104 0.6069, 0.02889, -2.1048 0.6079, -0.01747, -2.0717 0.6167, -0.06381, -0.6341 0.6558, -0.05300, 0.6414 0.7045, -0.04117, 0.9078 0.7429, -0.03210, 0.9819 0.8333, -0.01400, 1.0005 0.9311, -0.00120, 0.8888 --------- Run Conditions: vel=107.4 ft/s Re=1.034x10^6 AOA=119.98 Flap deflection=45.00 Totals: Cl=-0.9654 Cdp=1.2721 Cm(c/4)=-0.4866 Cs=-0.2006 Ch=0.0471 Main component: Cl=-0.1596 Cdp=0.8969 Cm=-0.3132 Flap component: Cl=-0.8058 Cdp=0.3752 Cm=-0.5695 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 1.0068 0.5905, -0.01667, 0.9253 0.5709, 0.03110, 0.9206 0.5889, 0.07933, -1.3937 0.5500, 0.08689, -1.4091 0.5110, 0.09367, -1.4473 0.4731, 0.09830, -1.4644 0.4349, 0.10070, -1.4786 0.3960, 0.10120, -1.5067 0.3566, 0.10020, -1.4582 0.3172, 0.09790, -1.4502 0.2778, 0.09440, -1.4534 0.2393, 0.08960, -1.4539 0.2056, 0.08360, -1.4934 0.1633, 0.07610, -1.4508 0.1261, 0.06710, -1.4643 0.0900, 0.05640, -1.4251 0.0571, 0.04390, -1.4109 0.0283, 0.02940, -1.4010 0.0142, 0.01970, -1.3856 0.0081, 0.01410, -1.4046 0.0026, 0.00780, -1.2922 0.0000, 0.00000, -1.3541 0.0037, -0.00840, -1.3507 0.0112, -0.01420, -1.3889 0.0191, -0.01930, -1.4381 0.0397, -0.03030, -1.2102 0.0706, -0.04420, -0.9434 0.1037, -0.05710, -0.7280 0.1384, -0.06890, -0.5037 0.1741, -0.07950, -0.3390 0.2102, -0.08660, -0.2036 0.2472, -0.09640, -0.0587 0.2844, -0.10270, 0.0858 0.3225, -0.10690, 0.2650 0.3608, -0.10890, 0.3802 0.3991, -0.10830, 0.5342 0.4373, -0.10510, 0.6604 0.4757, -0.09890, 0.7699 0.5137, -0.09067, 0.8860 0.5611, -0.07859, 0.9592 16 Flap element taps 1.0000, 0.00130, -1.5633 0.9365, 0.01390, -1.5743 0.8333, 0.03280, -1.5955 0.7436, 0.04930, -1.6085 0.7049, 0.05667, -1.5989 0.6662, 0.06411, -1.6273 0.6274, 0.07172, -1.6541 0.6009, 0.07523, -1.8519 0.6069, 0.02889, -1.8790 0.6079, -0.01747, -1.8483 0.6167, -0.06381, -0.2102 0.6558, -0.05300, 0.8186 0.7045, -0.04117, 0.9352 0.7429, -0.03210, 0.9486 0.8333, -0.01400, 0.9710 0.9311, -0.00120, 1.0198 --------- Run Conditions: vel=104.6 ft/s Re=1.006x10^6 AOA=149.99 Flap deflection=45.00 Totals: Cl=-0.2659 Cdp=0.4024 Cm(c/4)=-0.1969 Cs=0.2155 Ch=0.0788 Main component: Cl=0.0185 Cdp=0.3120 Cm=-0.0848 Flap component: Cl=-0.2844 Cdp=0.0904 Cm=-0.2200 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.3296 0.5905, -0.01667, 0.9016 0.5709, 0.03110, 0.8965 0.5889, 0.07933, -0.9045 0.5500, 0.08689, -0.8958 0.5110, 0.09367, -0.9173 0.4731, 0.09830, -0.9178 0.4349, 0.10070, -0.9280 0.3960, 0.10120, -0.9425 0.3566, 0.10020, -0.9430 0.3172, 0.09790, -0.9432 0.2778, 0.09440, -0.9549 0.2393, 0.08960, -0.9404 0.2056, 0.08360, -0.9488 0.1633, 0.07610, -0.9390 0.1261, 0.06710, -0.9318 0.0900, 0.05640, -0.9236 0.0571, 0.04390, -0.9232 0.0283, 0.02940, -0.9118 0.0142, 0.01970, -0.9043 0.0081, 0.01410, -0.9097 0.0026, 0.00780, -0.8550 0.0000, 0.00000, -0.9009 0.0037, -0.00840, -0.9951 0.0112, -0.01420, -1.3410 0.0191, -0.01930, -1.4291 0.0397, -0.03030, -1.3740 0.0706, -0.04420, -1.2846 0.1037, -0.05710, -1.2190 0.1384, -0.06890, -1.1433 0.1741, -0.07950, -1.0772 0.2102, -0.08660, -1.0082 0.2472, -0.09640, -0.9585 0.2844, -0.10270, -0.8622 0.3225, -0.10690, -0.7482 0.3608, -0.10890, -0.6267 0.3991, -0.10830, -0.4584 0.4373, -0.10510, -0.2445 0.4757, -0.09890, -0.0240 0.5137, -0.09067, 0.2569 0.5611, -0.07859, 0.4772 16 Flap element taps 1.0000, 0.00130, 0.9955 0.9365, 0.01390, 0.2982 0.8333, 0.03280, 0.0553 0.7436, 0.04930, -0.1418 0.7049, 0.05667, -0.1653 0.6662, 0.06411, -0.3399 0.6274, 0.07172, -0.5457 0.6009, 0.07523, -0.9616 0.6069, 0.02889, -1.0281 0.6079, -0.01747, -1.0335 0.6167, -0.06381, 0.1211 0.6558, -0.05300, 0.7598 0.7045, -0.04117, 0.7861 0.7429, -0.03210, 0.7741 0.8333, -0.01400, 0.6949 0.9311, -0.00120, 0.5445 --------- Run Conditions: vel=103.3 ft/s Re=0.993x10^6 AOA=180.02 Flap deflection=45.00 Totals: Cl=0.3738 Cdp=0.4630 Cm(c/4)=0.1820 Cs=0.4629 Ch=0.0178 Main component: Cl=0.0454 Cdp=0.0035 Cm=0.0143 Flap component: Cl=0.3285 Cdp=0.4596 Cm=0.2612 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.9164 0.5905, -0.01667, -0.9089 0.5709, 0.03110, -0.9281 0.5889, 0.07933, -0.9361 0.5500, 0.08689, -0.8298 0.5110, 0.09367, -0.8457 0.4731, 0.09830, -0.8334 0.4349, 0.10070, -0.8403 0.3960, 0.10120, -0.8630 0.3566, 0.10020, -0.8453 0.3172, 0.09790, -0.8465 0.2778, 0.09440, -0.8605 0.2393, 0.08960, -0.8498 0.2056, 0.08360, -0.8801 0.1633, 0.07610, -0.8696 0.1261, 0.06710, -0.8845 0.0900, 0.05640, -0.8799 0.0571, 0.04390, -0.8913 0.0283, 0.02940, -0.9004 0.0142, 0.01970, -0.9212 0.0081, 0.01410, -0.9651 0.0026, 0.00780, -0.9340 0.0000, 0.00000, -1.0859 0.0037, -0.00840, -1.0506 0.0112, -0.01420, -1.0035 0.0191, -0.01930, -0.9809 0.0397, -0.03030, -0.9527 0.0706, -0.04420, -0.9439 0.1037, -0.05710, -0.9373 0.1384, -0.06890, -0.9271 0.1741, -0.07950, -0.9333 0.2102, -0.08660, -0.9543 0.2472, -0.09640, -0.9440 0.2844, -0.10270, -0.9576 0.3225, -0.10690, -0.9344 0.3608, -0.10890, -0.9478 0.3991, -0.10830, -0.9409 0.4373, -0.10510, -0.9376 0.4757, -0.09890, -0.9403 0.5137, -0.09067, -0.9188 0.5611, -0.07859, -0.9182 16 Flap element taps 1.0000, 0.00130, -0.8901 0.9365, 0.01390, 1.0024 0.8333, 0.03280, 0.8368 0.7436, 0.04930, 0.5993 0.7049, 0.05667, 0.5013 0.6662, 0.06411, 0.2885 0.6274, 0.07172, -0.0099 0.6009, 0.07523, -0.8101 0.6069, 0.02889, -0.8164 0.6079, -0.01747, -0.8161 0.6167, -0.06381, -0.9222 0.6558, -0.05300, -0.9272 0.7045, -0.04117, -0.9250 0.7429, -0.03210, -0.9291 0.8333, -0.01400, -0.9147 0.9311, -0.00120, -0.8920 --------- Run Conditions: vel=103.7 ft/s Re=0.995x10^6 AOA=209.98 Flap deflection=45.00 Totals: Cl=0.0913 Cdp=0.7616 Cm(c/4)=0.2081 Cs=0.6141 Ch=-0.0379 Main component: Cl=0.0439 Cdp=0.0491 Cm=0.0172 Flap component: Cl=0.0474 Cdp=0.7126 Cm=0.3057 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -1.1854 0.5905, -0.01667, -1.1861 0.5709, 0.03110, -1.1777 0.5889, 0.07933, -1.2669 0.5500, 0.08689, -1.2222 0.5110, 0.09367, -1.2455 0.4731, 0.09830, -1.2481 0.4349, 0.10070, -1.2662 0.3960, 0.10120, -1.2798 0.3566, 0.10020, -1.1394 0.3172, 0.09790, -0.9553 0.2778, 0.09440, -0.8098 0.2393, 0.08960, -0.7296 0.2056, 0.08360, -0.8251 0.1633, 0.07610, -0.9305 0.1261, 0.06710, -1.1159 0.0900, 0.05640, -1.3207 0.0571, 0.04390, -1.5772 0.0283, 0.02940, -1.7372 0.0142, 0.01970, -1.7036 0.0081, 0.01410, -1.5866 0.0026, 0.00780, -1.2432 0.0000, 0.00000, -1.2657 0.0037, -0.00840, -1.2744 0.0112, -0.01420, -1.2863 0.0191, -0.01930, -1.3094 0.0397, -0.03030, -1.3824 0.0706, -0.04420, -1.4211 0.1037, -0.05710, -1.3728 0.1384, -0.06890, -1.2813 0.1741, -0.07950, -1.2496 0.2102, -0.08660, -1.2556 0.2472, -0.09640, -1.2322 0.2844, -0.10270, -1.2560 0.3225, -0.10690, -1.2239 0.3608, -0.10890, -1.2482 0.3991, -0.10830, -1.2300 0.4373, -0.10510, -1.2356 0.4757, -0.09890, -1.2262 0.5137, -0.09067, -1.1992 0.5611, -0.07859, -1.1858 16 Flap element taps 1.0000, 0.00130, -1.1117 0.9365, 0.01390, 0.8302 0.8333, 0.03280, 0.9922 0.7436, 0.04930, 0.9154 0.7049, 0.05667, 0.8471 0.6662, 0.06411, 0.6649 0.6274, 0.07172, 0.3299 0.6009, 0.07523, -1.1993 0.6069, 0.02889, -1.2129 0.6079, -0.01747, -1.2182 0.6167, -0.06381, -1.2156 0.6558, -0.05300, -1.1837 0.7045, -0.04117, -1.1653 0.7429, -0.03210, -1.1521 0.8333, -0.01400, -1.1354 0.9311, -0.00120, -1.1246 --------- Run Conditions: vel=101.1 ft/s Re=0.968x10^6 AOA=239.97 Flap deflection=45.00 Totals: Cl=0.3256 Cdp=1.6062 Cm(c/4)=0.4436 Cs=0.5219 Ch=-0.1280 Main component: Cl=0.4712 Cdp=0.7663 Cm=0.3344 Flap component: Cl=-0.1456 Cdp=0.8399 Cm=0.4976 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -1.5698 0.5905, -0.01667, -1.4472 0.5709, 0.03110, -2.0425 0.5889, 0.07933, -1.7002 0.5500, 0.08689, 1.0028 0.5110, 0.09367, 0.9362 0.4731, 0.09830, 0.8159 0.4349, 0.10070, 0.6768 0.3960, 0.10120, 0.4985 0.3566, 0.10020, 0.3978 0.3172, 0.09790, 0.2542 0.2778, 0.09440, 0.0793 0.2393, 0.08960, -0.0960 0.2056, 0.08360, -0.3507 0.1633, 0.07610, -0.5333 0.1261, 0.06710, -0.8083 0.0900, 0.05640, -1.1016 0.0571, 0.04390, -1.4951 0.0283, 0.02940, -1.6794 0.0142, 0.01970, -1.5630 0.0081, 0.01410, -1.5969 0.0026, 0.00780, -1.4909 0.0000, 0.00000, -1.5690 0.0037, -0.00840, -1.5947 0.0112, -0.01420, -1.6021 0.0191, -0.01930, -1.6050 0.0397, -0.03030, -1.6182 0.0706, -0.04420, -1.6562 0.1037, -0.05710, -1.6580 0.1384, -0.06890, -1.6349 0.1741, -0.07950, -1.6452 0.2102, -0.08660, -1.6826 0.2472, -0.09640, -1.6651 0.2844, -0.10270, -1.6834 0.3225, -0.10690, -1.6408 0.3608, -0.10890, -1.6719 0.3991, -0.10830, -1.6519 0.4373, -0.10510, -1.6635 0.4757, -0.09890, -1.6649 0.5137, -0.09067, -1.6201 0.5611, -0.07859, -1.5956 16 Flap element taps 1.0000, 0.00130, -1.5345 0.9365, 0.01390, 0.0969 0.8333, 0.03280, 0.5956 0.7436, 0.04930, 0.8319 0.7049, 0.05667, 0.9308 0.6662, 0.06411, 0.9783 0.6274, 0.07172, 1.0029 0.6009, 0.07523, 0.2727 0.6069, 0.02889, 0.2514 0.6079, -0.01747, 0.3483 0.6167, -0.06381, -1.6506 0.6558, -0.05300, -1.6723 0.7045, -0.04117, -1.6932 0.7429, -0.03210, -1.7287 0.8333, -0.01400, -1.8577 0.9311, -0.00120, -1.7543 --------- Run Conditions: vel=103.1 ft/s Re=0.986x10^6 AOA=268.99 Flap deflection=45.00 Totals: Cl=-0.0031 Cdp=1.6402 Cm(c/4)=0.3373 Cs=0.0320 Ch=0.0112 Main component: Cl=0.1340 Cdp=1.2154 Cm=0.4091 Flap component: Cl=-0.1371 Cdp=0.4248 Cm=0.3382 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -1.6662 0.5905, -0.01667, -1.7388 0.5709, 0.03110, -2.0592 0.5889, 0.07933, -1.8822 0.5500, 0.08689, 0.8963 0.5110, 0.09367, 0.9563 0.4731, 0.09830, 0.9940 0.4349, 0.10070, 0.9983 0.3960, 0.10120, 0.9362 0.3566, 0.10020, 0.9531 0.3172, 0.09790, 0.9013 0.2778, 0.09440, 0.8226 0.2393, 0.08960, 0.7339 0.2056, 0.08360, 0.5539 0.1633, 0.07610, 0.4298 0.1261, 0.06710, 0.1770 0.0900, 0.05640, -0.1246 0.0571, 0.04390, -0.6469 0.0283, 0.02940, -1.2854 0.0142, 0.01970, -1.6950 0.0081, 0.01410, -1.7086 0.0026, 0.00780, -1.4832 0.0000, 0.00000, -1.5541 0.0037, -0.00840, -1.5703 0.0112, -0.01420, -1.5719 0.0191, -0.01930, -1.5760 0.0397, -0.03030, -1.5761 0.0706, -0.04420, -1.6053 0.1037, -0.05710, -1.6220 0.1384, -0.06890, -1.6094 0.1741, -0.07950, -1.6325 0.2102, -0.08660, -1.6856 0.2472, -0.09640, -1.6710 0.2844, -0.10270, -1.6957 0.3225, -0.10690, -1.6511 0.3608, -0.10890, -1.6882 0.3991, -0.10830, -1.6752 0.4373, -0.10510, -1.7069 0.4757, -0.09890, -1.7251 0.5137, -0.09067, -1.7186 0.5611, -0.07859, -1.7038 16 Flap element taps 1.0000, 0.00130, -1.6067 0.9365, 0.01390, -0.6669 0.8333, 0.03280, -0.2174 0.7436, 0.04930, -0.6200 0.7049, 0.05667, -0.8246 0.6662, 0.06411, -0.8251 0.6274, 0.07172, -0.7886 0.6009, 0.07523, -0.7733 0.6069, 0.02889, 0.9749 0.6079, -0.01747, 0.9594 0.6167, -0.06381, -1.6708 0.6558, -0.05300, -1.6948 0.7045, -0.04117, -1.7181 0.7429, -0.03210, -1.7423 0.8333, -0.01400, -1.8314 0.9311, -0.00120, -1.7372