S809 UNVENTED AILERON, CLEAN, CHORD = 18 INCHES --------- Run Conditions: vel=102.8 ft/s Re=0.998x10^6 AOA=-5.95 Flap deflection=-60.00 Totals: Cl=-1.7674 Cdp=0.3568 Cm(c/4)=0.1840 Cs=-0.1717 Ch=0.3906 Main component: Cl=-1.5662 Cdp=0.0003 Cm=0.3962 Flap component: Cl=-0.2013 Cdp=0.3566 Cm=0.2366 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7353 0.6175, -0.04610, -0.6807 0.5841, -0.02440, -0.6740 0.5775, 0.01750, -0.6908 0.5777, 0.04660, -0.6874 0.6274, 0.07170, 0.7714 0.5694, 0.08320, 0.7786 0.5112, 0.09370, 0.7139 0.4731, 0.09830, 0.6610 0.4349, 0.10070, 0.6452 0.3960, 0.10120, 0.6035 0.3566, 0.10020, 0.6105 0.3172, 0.09790, 0.6089 0.2778, 0.09440, 0.6183 0.2393, 0.08960, 0.6450 0.2056, 0.08360, 0.6639 0.1633, 0.07610, 0.7522 0.1261, 0.06710, 0.8118 0.0900, 0.05640, 0.9165 0.0571, 0.04390, 0.9895 0.0283, 0.02940, 0.9541 0.0142, 0.01970, 0.6442 0.0081, 0.01410, 0.1719 0.0026, 0.00780, -0.8723 0.0000, 0.00000, -3.7523 0.0037, -0.00840, -3.5873 0.0112, -0.01420, -3.5812 0.0191, -0.01930, -3.5916 0.0397, -0.03030, -3.5851 0.0706, -0.04420, -3.5126 0.1037, -0.05710, -3.1000 0.1384, -0.06890, -2.4211 0.1741, -0.07950, -1.9219 0.2102, -0.08660, -1.7568 0.2472, -0.09640, -1.7195 0.2844, -0.10270, -1.7355 0.3225, -0.10690, -1.6777 0.3608, -0.10890, -1.6344 0.3991, -0.10830, -1.5051 0.4373, -0.10510, -1.3319 0.4757, -0.09890, -1.1410 0.5137, -0.09070, -0.9857 0.5694, -0.07640, -0.8200 15 Flap element taps 1.0000, 0.00130, -0.6631 0.9365, 0.01390, 0.3173 0.8333, 0.03280, 0.6878 0.7436, 0.04930, 0.8350 0.7049, 0.05670, 0.8329 0.6662, 0.06410, 0.7860 0.6522, 0.01390, -0.6792 0.5969, -0.00020, -0.6895 0.6000, -0.03020, -0.6855 0.6324, -0.04540, -0.6811 0.6667, -0.04880, -0.6772 0.7046, -0.04110, -0.6643 0.7429, -0.03210, -0.6791 0.8333, -0.01400, -0.6878 0.9311, -0.00120, -0.6598 --------- Run Conditions: vel=103.4 ft/s Re=1.002x10^6 AOA=-0.04 Flap deflection=-60.00 Totals: Cl=-1.5825 Cdp=0.2896 Cm(c/4)=0.2301 Cs=-0.2885 Ch=0.3828 Main component: Cl=-1.3491 Cdp=-0.0432 Cm=0.3928 Flap component: Cl=-0.2334 Cdp=0.3328 Cm=0.2330 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7584 0.6175, -0.04610, -0.6834 0.5841, -0.02440, -0.6768 0.5775, 0.01750, -0.6960 0.5777, 0.04660, -0.6933 0.6274, 0.07170, 0.7860 0.5694, 0.08320, 0.7956 0.5112, 0.09370, 0.7126 0.4731, 0.09830, 0.5639 0.4349, 0.10070, 0.5206 0.3960, 0.10120, 0.4599 0.3566, 0.10020, 0.4763 0.3172, 0.09790, 0.4653 0.2778, 0.09440, 0.4659 0.2393, 0.08960, 0.4739 0.2056, 0.08360, 0.4646 0.1633, 0.07610, 0.5679 0.1261, 0.06710, 0.6149 0.0900, 0.05640, 0.7443 0.0571, 0.04390, 0.8709 0.0283, 0.02940, 1.0014 0.0142, 0.01970, 0.9451 0.0081, 0.01410, 0.6978 0.0026, 0.00780, -0.0477 0.0000, 0.00000, -2.8716 0.0037, -0.00840, -3.5815 0.0112, -0.01420, -3.1248 0.0191, -0.01930, -1.9038 0.0397, -0.03030, -1.6356 0.0706, -0.04420, -1.5028 0.1037, -0.05710, -1.5144 0.1384, -0.06890, -1.5200 0.1741, -0.07950, -1.5764 0.2102, -0.08660, -1.6995 0.2472, -0.09640, -1.7971 0.2844, -0.10270, -1.8733 0.3225, -0.10690, -1.8832 0.3608, -0.10890, -1.9258 0.3991, -0.10830, -1.8569 0.4373, -0.10510, -1.7291 0.4757, -0.09890, -1.5001 0.5137, -0.09070, -1.2879 0.5694, -0.07640, -0.9450 15 Flap element taps 1.0000, 0.00130, -0.6949 0.9365, 0.01390, 0.2570 0.8333, 0.03280, 0.6399 0.7436, 0.04930, 0.8199 0.7049, 0.05670, 0.8278 0.6662, 0.06410, 0.7844 0.6522, 0.01390, -0.6872 0.5969, -0.00020, -0.6936 0.6000, -0.03020, -0.6973 0.6324, -0.04540, -0.7055 0.6667, -0.04880, -0.7037 0.7046, -0.04110, -0.6823 0.7429, -0.03210, -0.7018 0.8333, -0.01400, -0.7148 0.9311, -0.00120, -0.6809 --------- Run Conditions: vel=103.3 ft/s Re=1.000x10^6 AOA=3.00 Flap deflection=-60.00 Totals: Cl=-1.5576 Cdp=0.2762 Cm(c/4)=0.2530 Cs=-0.3573 Ch=0.4045 Main component: Cl=-1.2934 Cdp=-0.0616 Cm=0.3926 Flap component: Cl=-0.2641 Cdp=0.3378 Cm=0.2456 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8793 0.6175, -0.04610, -0.7737 0.5841, -0.02440, -0.7686 0.5775, 0.01750, -0.7883 0.5777, 0.04660, -0.7882 0.6274, 0.07170, 0.7868 0.5694, 0.08320, 0.7988 0.5112, 0.09370, 0.6896 0.4731, 0.09830, 0.5726 0.4349, 0.10070, 0.4718 0.3960, 0.10120, 0.3976 0.3566, 0.10020, 0.4237 0.3172, 0.09790, 0.4075 0.2778, 0.09440, 0.4057 0.2393, 0.08960, 0.4059 0.2056, 0.08360, 0.3766 0.1633, 0.07610, 0.4884 0.1261, 0.06710, 0.5211 0.0900, 0.05640, 0.6543 0.0571, 0.04390, 0.7838 0.0283, 0.02940, 0.9612 0.0142, 0.01970, 0.9975 0.0081, 0.01410, 0.8466 0.0026, 0.00780, 0.3151 0.0000, 0.00000, -1.7217 0.0037, -0.00840, -2.6518 0.0112, -0.01420, -2.1465 0.0191, -0.01930, -2.0377 0.0397, -0.03030, -1.2727 0.0706, -0.04420, -1.2622 0.1037, -0.05710, -1.3271 0.1384, -0.06890, -1.3589 0.1741, -0.07950, -1.4455 0.2102, -0.08660, -1.6097 0.2472, -0.09640, -1.7276 0.2844, -0.10270, -1.8372 0.3225, -0.10690, -1.8669 0.3608, -0.10890, -1.9474 0.3991, -0.10830, -1.9047 0.4373, -0.10510, -1.8208 0.4757, -0.09890, -1.6148 0.5137, -0.09070, -1.4326 0.5694, -0.07640, -1.0890 15 Flap element taps 1.0000, 0.00130, -0.7929 0.9365, 0.01390, 0.2235 0.8333, 0.03280, 0.6202 0.7436, 0.04930, 0.8083 0.7049, 0.05670, 0.8243 0.6662, 0.06410, 0.7785 0.6522, 0.01390, -0.7755 0.5969, -0.00020, -0.7813 0.6000, -0.03020, -0.7820 0.6324, -0.04540, -0.7901 0.6667, -0.04880, -0.7919 0.7046, -0.04110, -0.7653 0.7429, -0.03210, -0.7897 0.8333, -0.01400, -0.8120 0.9311, -0.00120, -0.7716 --------- Run Conditions: vel=103.7 ft/s Re=1.004x10^6 AOA=6.00 Flap deflection=-60.00 Totals: Cl=-1.3812 Cdp=0.2463 Cm(c/4)=0.2566 Cs=-0.3893 Ch=0.3830 Main component: Cl=-1.1134 Cdp=-0.0598 Cm=0.3602 Flap component: Cl=-0.2677 Cdp=0.3060 Cm=0.2334 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8406 0.6175, -0.04610, -0.7302 0.5841, -0.02440, -0.7209 0.5775, 0.01750, -0.7410 0.5777, 0.04660, -0.7432 0.6274, 0.07170, 0.7500 0.5694, 0.08320, 0.7706 0.5112, 0.09370, 0.6675 0.4731, 0.09830, 0.5781 0.4349, 0.10070, 0.4075 0.3960, 0.10120, 0.3127 0.3566, 0.10020, 0.3480 0.3172, 0.09790, 0.3235 0.2778, 0.09440, 0.3104 0.2393, 0.08960, 0.2943 0.2056, 0.08360, 0.2430 0.1633, 0.07610, 0.3487 0.1261, 0.06710, 0.3607 0.0900, 0.05640, 0.4804 0.0571, 0.04390, 0.6029 0.0283, 0.02940, 0.8181 0.0142, 0.01970, 0.9700 0.0081, 0.01410, 0.9369 0.0026, 0.00780, 0.7500 0.0000, 0.00000, -0.2147 0.0037, -0.00840, -1.2225 0.0112, -0.01420, -1.0784 0.0191, -0.01930, -0.9513 0.0397, -0.03030, -0.8183 0.0706, -0.04420, -0.8615 0.1037, -0.05710, -0.9795 0.1384, -0.06890, -1.0462 0.1741, -0.07950, -1.1779 0.2102, -0.08660, -1.3746 0.2472, -0.09640, -1.5068 0.2844, -0.10270, -1.6473 0.3225, -0.10690, -1.7103 0.3608, -0.10890, -1.8148 0.3991, -0.10830, -1.8070 0.4373, -0.10510, -1.7429 0.4757, -0.09890, -1.6311 0.5137, -0.09070, -1.5488 0.5694, -0.07640, -1.0089 15 Flap element taps 1.0000, 0.00130, -0.7323 0.9365, 0.01390, 0.2128 0.8333, 0.03280, 0.6017 0.7436, 0.04930, 0.7786 0.7049, 0.05670, 0.7895 0.6662, 0.06410, 0.7470 0.6522, 0.01390, -0.7383 0.5969, -0.00020, -0.7474 0.6000, -0.03020, -0.7457 0.6324, -0.04540, -0.7506 0.6667, -0.04880, -0.7494 0.7046, -0.04110, -0.7200 0.7429, -0.03210, -0.7420 0.8333, -0.01400, -0.7635 0.9311, -0.00120, -0.7165 --------- Run Conditions: vel=103.5 ft/s Re=1.003x10^6 AOA=8.99 Flap deflection=-60.00 Totals: Cl=-1.1612 Cdp=0.2433 Cm(c/4)=0.2610 Cs=-0.4218 Ch=0.3766 Main component: Cl=-0.8834 Cdp=-0.0414 Cm=0.3092 Flap component: Cl=-0.2779 Cdp=0.2847 Cm=0.2291 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8296 0.6175, -0.04610, -0.7504 0.5841, -0.02440, -0.7396 0.5775, 0.01750, -0.7609 0.5777, 0.04660, -0.7637 0.6274, 0.07170, 0.6954 0.5694, 0.08320, 0.7262 0.5112, 0.09370, 0.6510 0.4731, 0.09830, 0.5413 0.4349, 0.10070, 0.4442 0.3960, 0.10120, 0.2129 0.3566, 0.10020, 0.2419 0.3172, 0.09790, 0.2202 0.2778, 0.09440, 0.1995 0.2393, 0.08960, 0.1634 0.2056, 0.08360, 0.0884 0.1633, 0.07610, 0.1769 0.1261, 0.06710, 0.1636 0.0900, 0.05640, 0.2581 0.0571, 0.04390, 0.3498 0.0283, 0.02940, 0.5549 0.0142, 0.01970, 0.7681 0.0081, 0.01410, 0.8227 0.0026, 0.00780, 0.9824 0.0000, 0.00000, 0.7330 0.0037, -0.00840, -0.0554 0.0112, -0.01420, -0.2004 0.0191, -0.01930, -0.2358 0.0397, -0.03030, -0.2898 0.0706, -0.04420, -0.4368 0.1037, -0.05710, -0.6042 0.1384, -0.06890, -0.6999 0.1741, -0.07950, -0.8562 0.2102, -0.08660, -1.0796 0.2472, -0.09640, -1.2232 0.2844, -0.10270, -1.3900 0.3225, -0.10690, -1.4677 0.3608, -0.10890, -1.5971 0.3991, -0.10830, -1.6146 0.4373, -0.10510, -1.5900 0.4757, -0.09890, -1.4701 0.5137, -0.09070, -1.4009 0.5694, -0.07640, -0.9426 15 Flap element taps 1.0000, 0.00130, -0.7339 0.9365, 0.01390, 0.1848 0.8333, 0.03280, 0.5845 0.7436, 0.04930, 0.7347 0.7049, 0.05670, 0.7244 0.6662, 0.06410, 0.6888 0.6522, 0.01390, -0.7529 0.5969, -0.00020, -0.7578 0.6000, -0.03020, -0.7567 0.6324, -0.04540, -0.7566 0.6667, -0.04880, -0.7566 0.7046, -0.04110, -0.7253 0.7429, -0.03210, -0.7498 0.8333, -0.01400, -0.7745 0.9311, -0.00120, -0.7213 --------- Run Conditions: vel=103.7 ft/s Re=1.004x10^6 AOA=11.99 Flap deflection=-60.00 Totals: Cl=-0.9293 Cdp=0.2360 Cm(c/4)=0.2625 Cs=-0.4239 Ch=0.3658 Main component: Cl=-0.6471 Cdp=-0.0224 Cm=0.2558 Flap component: Cl=-0.2822 Cdp=0.2584 Cm=0.2216 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7964 0.6175, -0.04610, -0.7502 0.5841, -0.02440, -0.7407 0.5775, 0.01750, -0.7618 0.5777, 0.04660, -0.7663 0.6274, 0.07170, 0.6192 0.5694, 0.08320, 0.6544 0.5112, 0.09370, 0.6158 0.4731, 0.09830, 0.5227 0.4349, 0.10070, 0.3926 0.3960, 0.10120, 0.2212 0.3566, 0.10020, 0.1928 0.3172, 0.09790, 0.0877 0.2778, 0.09440, 0.0757 0.2393, 0.08960, 0.0236 0.2056, 0.08360, -0.0786 0.1633, 0.07610, -0.0125 0.1261, 0.06710, -0.0624 0.0900, 0.05640, -0.0070 0.0571, 0.04390, 0.0264 0.0283, 0.02940, 0.1663 0.0142, 0.01970, 0.3608 0.0081, 0.01410, 0.4352 0.0026, 0.00780, 0.7215 0.0000, 0.00000, 1.0038 0.0037, -0.00840, 0.6983 0.0112, -0.01420, 0.4551 0.0191, -0.01930, 0.3309 0.0397, -0.03030, 0.1615 0.0706, -0.04420, -0.0508 0.1037, -0.05710, -0.2520 0.1384, -0.06890, -0.3702 0.1741, -0.07950, -0.5439 0.2102, -0.08660, -0.7869 0.2472, -0.09640, -0.9398 0.2844, -0.10270, -1.1234 0.3225, -0.10690, -1.2174 0.3608, -0.10890, -1.3654 0.3991, -0.10830, -1.4059 0.4373, -0.10510, -1.4169 0.4757, -0.09890, -1.3105 0.5137, -0.09070, -1.2566 0.5694, -0.07640, -0.8624 15 Flap element taps 1.0000, 0.00130, -0.7237 0.9365, 0.01390, 0.1665 0.8333, 0.03280, 0.5718 0.7436, 0.04930, 0.6750 0.7049, 0.05670, 0.6329 0.6662, 0.06410, 0.6097 0.6522, 0.01390, -0.7504 0.5969, -0.00020, -0.7556 0.6000, -0.03020, -0.7540 0.6324, -0.04540, -0.7469 0.6667, -0.04880, -0.7471 0.7046, -0.04110, -0.7159 0.7429, -0.03210, -0.7410 0.8333, -0.01400, -0.7664 0.9311, -0.00120, -0.7123 --------- Run Conditions: vel=104.0 ft/s Re=1.002x10^6 AOA=14.99 Flap deflection=-60.00 Totals: Cl=-0.7097 Cdp=0.2254 Cm(c/4)=0.2630 Cs=-0.4013 Ch=0.3549 Main component: Cl=-0.4277 Cdp=-0.0053 Cm=0.2070 Flap component: Cl=-0.2820 Cdp=0.2307 Cm=0.2127 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7552 0.6175, -0.04610, -0.7526 0.5841, -0.02440, -0.7385 0.5775, 0.01750, -0.7542 0.5777, 0.04660, -0.7529 0.6274, 0.07170, 0.5525 0.5694, 0.08320, 0.5589 0.5112, 0.09370, 0.5521 0.4731, 0.09830, 0.5186 0.4349, 0.10070, 0.3828 0.3960, 0.10120, 0.2496 0.3566, 0.10020, 0.1450 0.3172, 0.09790, 0.0848 0.2778, 0.09440, -0.0808 0.2393, 0.08960, -0.1256 0.2056, 0.08360, -0.1807 0.1633, 0.07610, -0.2322 0.1261, 0.06710, -0.2695 0.0900, 0.05640, -0.3138 0.0571, 0.04390, -0.3388 0.0283, 0.02940, -0.3244 0.0142, 0.01970, -0.2363 0.0081, 0.01410, -0.1581 0.0026, 0.00780, 0.0561 0.0000, 0.00000, 0.6088 0.0037, -0.00840, 0.9826 0.0112, -0.01420, 0.8537 0.0191, -0.01930, 0.7355 0.0397, -0.03030, 0.5214 0.0706, -0.04420, 0.2819 0.1037, -0.05710, 0.0762 0.1384, -0.06890, -0.1210 0.1741, -0.07950, -0.2959 0.2102, -0.08660, -0.4749 0.2472, -0.09640, -0.6791 0.2844, -0.10270, -0.8415 0.3225, -0.10690, -1.0001 0.3608, -0.10890, -1.1512 0.3991, -0.10830, -1.2375 0.4373, -0.10510, -1.2395 0.4757, -0.09890, -1.1663 0.5137, -0.09070, -1.0883 0.5694, -0.07640, -0.8346 15 Flap element taps 1.0000, 0.00130, -0.7157 0.9365, 0.01390, 0.1678 0.8333, 0.03280, 0.5643 0.7436, 0.04930, 0.5707 0.7049, 0.05670, 0.5511 0.6662, 0.06410, 0.5516 0.6522, 0.01390, -0.7381 0.5969, -0.00020, -0.7589 0.6000, -0.03020, -0.7451 0.6324, -0.04540, -0.7209 0.6667, -0.04880, -0.7107 0.7046, -0.04110, -0.7145 0.7429, -0.03210, -0.7215 0.8333, -0.01400, -0.7292 0.9311, -0.00120, -0.7186 --------- Run Conditions: vel=104.6 ft/s Re=1.008x10^6 AOA=17.96 Flap deflection=-60.00 Totals: Cl=-0.4621 Cdp=0.2142 Cm(c/4)=0.2532 Cs=-0.3463 Ch=0.3337 Main component: Cl=-0.1944 Cdp=0.0215 Cm=0.1503 Flap component: Cl=-0.2677 Cdp=0.1928 Cm=0.1962 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7070 0.6175, -0.04610, -0.7411 0.5841, -0.02440, -0.7292 0.5775, 0.01750, -0.7455 0.5777, 0.04660, -0.7427 0.6274, 0.07170, 0.3594 0.5694, 0.08320, 0.3538 0.5112, 0.09370, 0.3656 0.4731, 0.09830, 0.3814 0.4349, 0.10070, 0.3588 0.3960, 0.10120, 0.2729 0.3566, 0.10020, 0.1364 0.3172, 0.09790, 0.0225 0.2778, 0.09440, -0.1049 0.2393, 0.08960, -0.2140 0.2056, 0.08360, -0.3163 0.1633, 0.07610, -0.4111 0.1261, 0.06710, -0.5301 0.0900, 0.05640, -0.6485 0.0571, 0.04390, -0.7775 0.0283, 0.02940, -0.9375 0.0142, 0.01970, -1.0316 0.0081, 0.01410, -1.1189 0.0026, 0.00780, -0.8678 0.0000, 0.00000, -0.5840 0.0037, -0.00840, 0.8721 0.0112, -0.01420, 0.9924 0.0191, -0.01930, 0.9502 0.0397, -0.03030, 0.7815 0.0706, -0.04420, 0.5545 0.1037, -0.05710, 0.3528 0.1384, -0.06890, 0.1522 0.1741, -0.07950, -0.0258 0.2102, -0.08660, -0.2072 0.2472, -0.09640, -0.4121 0.2844, -0.10270, -0.5824 0.3225, -0.10690, -0.7528 0.3608, -0.10890, -0.9145 0.3991, -0.10830, -1.0186 0.4373, -0.10510, -1.0497 0.4757, -0.09890, -1.0040 0.5137, -0.09070, -0.9588 0.5694, -0.07640, -0.8137 15 Flap element taps 1.0000, 0.00130, -0.6973 0.9365, 0.01390, 0.1853 0.8333, 0.03280, 0.5226 0.7436, 0.04930, 0.3809 0.7049, 0.05670, 0.3521 0.6662, 0.06410, 0.3636 0.6522, 0.01390, -0.7244 0.5969, -0.00020, -0.7461 0.6000, -0.03020, -0.7324 0.6324, -0.04540, -0.6983 0.6667, -0.04880, -0.6889 0.7046, -0.04110, -0.6918 0.7429, -0.03210, -0.7003 0.8333, -0.01400, -0.7075 0.9311, -0.00120, -0.6951 --------- Run Conditions: vel=104.3 ft/s Re=1.004x10^6 AOA=19.98 Flap deflection=-60.00 Totals: Cl=-0.2659 Cdp=0.2005 Cm(c/4)=0.2317 Cs=-0.2793 Ch=0.2962 Main component: Cl=-0.0303 Cdp=0.0485 Cm=0.1060 Flap component: Cl=-0.2357 Cdp=0.1519 Cm=0.1710 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6959 0.6175, -0.04610, -0.7701 0.5841, -0.02440, -0.7561 0.5775, 0.01750, -0.7723 0.5777, 0.04660, -0.7705 0.6274, 0.07170, 0.2031 0.5694, 0.08320, 0.1867 0.5112, 0.09370, 0.1946 0.4731, 0.09830, 0.2144 0.4349, 0.10070, 0.2165 0.3960, 0.10120, 0.2031 0.3566, 0.10020, 0.1499 0.3172, 0.09790, 0.0417 0.2778, 0.09440, -0.1194 0.2393, 0.08960, -0.2675 0.2056, 0.08360, -0.4118 0.1633, 0.07610, -0.5476 0.1261, 0.06710, -0.6758 0.0900, 0.05640, -0.8498 0.0571, 0.04390, -1.0511 0.0283, 0.02940, -1.4289 0.0142, 0.01970, -1.6770 0.0081, 0.01410, -1.9461 0.0026, 0.00780, -1.7801 0.0000, 0.00000, -1.8282 0.0037, -0.00840, 0.5722 0.0112, -0.01420, 0.9669 0.0191, -0.01930, 0.9985 0.0397, -0.03030, 0.9022 0.0706, -0.04420, 0.7037 0.1037, -0.05710, 0.5153 0.1384, -0.06890, 0.3165 0.1741, -0.07950, 0.1409 0.2102, -0.08660, -0.0389 0.2472, -0.09640, -0.2407 0.2844, -0.10270, -0.4154 0.3225, -0.10690, -0.5910 0.3608, -0.10890, -0.7596 0.3991, -0.10830, -0.8789 0.4373, -0.10510, -0.9277 0.4757, -0.09890, -0.8999 0.5137, -0.09070, -0.8776 0.5694, -0.07640, -0.7461 15 Flap element taps 1.0000, 0.00130, -0.6863 0.9365, 0.01390, 0.1945 0.8333, 0.03280, 0.3329 0.7436, 0.04930, 0.1762 0.7049, 0.05670, 0.1756 0.6662, 0.06410, 0.1990 0.6522, 0.01390, -0.7519 0.5969, -0.00020, -0.7743 0.6000, -0.03020, -0.7422 0.6324, -0.04540, -0.6829 0.6667, -0.04880, -0.6692 0.7046, -0.04110, -0.6719 0.7429, -0.03210, -0.6804 0.8333, -0.01400, -0.6897 0.9311, -0.00120, -0.6781 --------- Run Conditions: vel=104.4 ft/s Re=1.006x10^6 AOA=23.98 Flap deflection=-60.00 Totals: Cl=0.4932 Cdp=0.2406 Cm(c/4)=-0.0242 Cs=-0.0194 Ch=-0.1031 Main component: Cl=0.3833 Cdp=0.3548 Cm=-0.1010 Flap component: Cl=0.1099 Cdp=-0.1142 Cm=-0.0603 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7799 0.6175, -0.04610, -1.1122 0.5841, -0.02440, -1.0998 0.5775, 0.01750, -1.1176 0.5777, 0.04660, -1.1155 0.6274, 0.07170, -0.8064 0.5694, 0.08320, -0.9151 0.5112, 0.09370, -0.9749 0.4731, 0.09830, -0.9639 0.4349, 0.10070, -0.9287 0.3960, 0.10120, -0.9062 0.3566, 0.10020, -0.8960 0.3172, 0.09790, -0.8744 0.2778, 0.09440, -0.8732 0.2393, 0.08960, -0.8612 0.2056, 0.08360, -0.8603 0.1633, 0.07610, -0.8551 0.1261, 0.06710, -0.8521 0.0900, 0.05640, -0.8518 0.0571, 0.04390, -0.8478 0.0283, 0.02940, -0.8543 0.0142, 0.01970, -0.8538 0.0081, 0.01410, -0.8598 0.0026, 0.00780, -0.7732 0.0000, 0.00000, -1.1303 0.0037, -0.00840, 0.4000 0.0112, -0.01420, 0.8775 0.0191, -0.01930, 0.9800 0.0397, -0.03030, 0.9805 0.0706, -0.04420, 0.8568 0.1037, -0.05710, 0.7151 0.1384, -0.06890, 0.5466 0.1741, -0.07950, 0.3955 0.2102, -0.08660, 0.2294 0.2472, -0.09640, 0.0429 0.2844, -0.10270, -0.1287 0.3225, -0.10690, -0.3021 0.3608, -0.10890, -0.4782 0.3991, -0.10830, -0.6152 0.4373, -0.10510, -0.6993 0.4757, -0.09890, -0.7106 0.5137, -0.09070, -0.7439 0.5694, -0.07640, -0.6897 15 Flap element taps 1.0000, 0.00130, -0.7836 0.9365, 0.01390, -0.7226 0.8333, 0.03280, -0.9504 0.7436, 0.04930, -0.9572 0.7049, 0.05670, -0.8838 0.6662, 0.06410, -0.8143 0.6522, 0.01390, -1.0968 0.5969, -0.00020, -1.1209 0.6000, -0.03020, -0.8291 0.6324, -0.04540, -0.5477 0.6667, -0.04880, -0.4568 0.7046, -0.04110, -0.4310 0.7429, -0.03210, -0.4378 0.8333, -0.01400, -0.4613 0.9311, -0.00120, -0.4876 --------- Run Conditions: vel=104.0 ft/s Re=1.000x10^6 AOA=26.97 Flap deflection=-60.00 Totals: Cl=0.4720 Cdp=0.2994 Cm(c/4)=-0.0166 Cs=-0.0528 Ch=-0.0996 Main component: Cl=0.3713 Cdp=0.4004 Cm=-0.1032 Flap component: Cl=0.1007 Cdp=-0.1010 Cm=-0.0525 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8617 0.6175, -0.04610, -1.2488 0.5841, -0.02440, -1.2387 0.5775, 0.01750, -1.2577 0.5777, 0.04660, -1.2579 0.6274, 0.07170, -0.8532 0.5694, 0.08320, -0.8947 0.5112, 0.09370, -0.9277 0.4731, 0.09830, -0.9228 0.4349, 0.10070, -0.9147 0.3960, 0.10120, -0.9112 0.3566, 0.10020, -0.9097 0.3172, 0.09790, -0.8938 0.2778, 0.09440, -0.8883 0.2393, 0.08960, -0.8748 0.2056, 0.08360, -0.8752 0.1633, 0.07610, -0.8693 0.1261, 0.06710, -0.8673 0.0900, 0.05640, -0.8671 0.0571, 0.04390, -0.8693 0.0283, 0.02940, -0.8740 0.0142, 0.01970, -0.8715 0.0081, 0.01410, -0.8844 0.0026, 0.00780, -0.7908 0.0000, 0.00000, -1.0364 0.0037, -0.00840, 0.2728 0.0112, -0.01420, 0.8189 0.0191, -0.01930, 0.9581 0.0397, -0.03030, 0.9959 0.0706, -0.04420, 0.9004 0.1037, -0.05710, 0.7711 0.1384, -0.06890, 0.6146 0.1741, -0.07950, 0.4656 0.2102, -0.08660, 0.2968 0.2472, -0.09640, 0.1121 0.2844, -0.10270, -0.0660 0.3225, -0.10690, -0.2453 0.3608, -0.10890, -0.4336 0.3991, -0.10830, -0.5821 0.4373, -0.10510, -0.6856 0.4757, -0.09890, -0.7121 0.5137, -0.09070, -0.7670 0.5694, -0.07640, -0.7354 15 Flap element taps 1.0000, 0.00130, -1.0585 0.9365, 0.01390, -0.9659 0.8333, 0.03280, -0.9716 0.7436, 0.04930, -0.9347 0.7049, 0.05670, -0.9003 0.6662, 0.06410, -0.8683 0.6522, 0.01390, -1.2294 0.5969, -0.00020, -1.2591 0.6000, -0.03020, -1.0093 0.6324, -0.04540, -0.7028 0.6667, -0.04880, -0.5771 0.7046, -0.04110, -0.5592 0.7429, -0.03210, -0.5684 0.8333, -0.01400, -0.5815 0.9311, -0.00120, -0.6028 --------- Run Conditions: vel=103.5 ft/s Re=0.995x10^6 AOA=29.97 Flap deflection=-60.00 Totals: Cl=0.3645 Cdp=0.3462 Cm(c/4)=0.0156 Cs=-0.1178 Ch=-0.0375 Main component: Cl=0.3175 Cdp=0.4171 Cm=-0.0923 Flap component: Cl=0.0470 Cdp=-0.0709 Cm=-0.0143 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.9007 0.6175, -0.04610, -1.3170 0.5841, -0.02440, -1.3087 0.5775, 0.01750, -1.3202 0.5777, 0.04660, -1.3206 0.6274, 0.07170, -0.8081 0.5694, 0.08320, -0.8182 0.5112, 0.09370, -0.8164 0.4731, 0.09830, -0.8107 0.4349, 0.10070, -0.8196 0.3960, 0.10120, -0.8181 0.3566, 0.10020, -0.8266 0.3172, 0.09790, -0.8200 0.2778, 0.09440, -0.8292 0.2393, 0.08960, -0.8125 0.2056, 0.08360, -0.8120 0.1633, 0.07610, -0.8183 0.1261, 0.06710, -0.8138 0.0900, 0.05640, -0.8154 0.0571, 0.04390, -0.8038 0.0283, 0.02940, -0.8187 0.0142, 0.01970, -0.8211 0.0081, 0.01410, -0.8209 0.0026, 0.00780, -0.7384 0.0000, 0.00000, -0.8706 0.0037, -0.00840, 0.2061 0.0112, -0.01420, 0.7747 0.0191, -0.01930, 0.9370 0.0397, -0.03030, 1.0012 0.0706, -0.04420, 0.9277 0.1037, -0.05710, 0.8125 0.1384, -0.06890, 0.6557 0.1741, -0.07950, 0.5120 0.2102, -0.08660, 0.3520 0.2472, -0.09640, 0.1618 0.2844, -0.10270, -0.0174 0.3225, -0.10690, -0.1955 0.3608, -0.10890, -0.3838 0.3991, -0.10830, -0.5615 0.4373, -0.10510, -0.6551 0.4757, -0.09890, -0.7045 0.5137, -0.09070, -0.7741 0.5694, -0.07640, -0.7511 15 Flap element taps 1.0000, 0.00130, -0.9302 0.9365, 0.01390, -0.8953 0.8333, 0.03280, -0.8425 0.7436, 0.04930, -0.8304 0.7049, 0.05670, -0.8235 0.6662, 0.06410, -0.8149 0.6522, 0.01390, -1.3008 0.5969, -0.00020, -1.3177 0.6000, -0.03020, -1.1485 0.6324, -0.04540, -0.8178 0.6667, -0.04880, -0.6825 0.7046, -0.04110, -0.6567 0.7429, -0.03210, -0.6689 0.8333, -0.01400, -0.6822 0.9311, -0.00120, -0.7052 --------- Run Conditions: vel=104.0 ft/s Re=1.000x10^6 AOA=34.97 Flap deflection=-60.00 Totals: Cl=0.3073 Cdp=0.4316 Cm(c/4)=0.0376 Cs=-0.1776 Ch=0.0200 Main component: Cl=0.3063 Cdp=0.4843 Cm=-0.1070 Flap component: Cl=0.0010 Cdp=-0.0526 Cm=0.0199 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.9484 0.6175, -0.04610, -1.4516 0.5841, -0.02440, -1.4406 0.5775, 0.01750, -1.4472 0.5777, 0.04660, -1.4481 0.6274, 0.07170, -0.8186 0.5694, 0.08320, -0.8258 0.5112, 0.09370, -0.8213 0.4731, 0.09830, -0.8141 0.4349, 0.10070, -0.8216 0.3960, 0.10120, -0.8182 0.3566, 0.10020, -0.8273 0.3172, 0.09790, -0.8203 0.2778, 0.09440, -0.8299 0.2393, 0.08960, -0.8138 0.2056, 0.08360, -0.8112 0.1633, 0.07610, -0.8203 0.1261, 0.06710, -0.8181 0.0900, 0.05640, -0.8184 0.0571, 0.04390, -0.8072 0.0283, 0.02940, -0.8186 0.0142, 0.01970, -0.8175 0.0081, 0.01410, -0.8168 0.0026, 0.00780, -0.7369 0.0000, 0.00000, -0.8379 0.0037, -0.00840, -0.0041 0.0112, -0.01420, 0.6469 0.0191, -0.01930, 0.8665 0.0397, -0.03030, 0.9983 0.0706, -0.04420, 0.9732 0.1037, -0.05710, 0.8894 0.1384, -0.06890, 0.7536 0.1741, -0.07950, 0.6233 0.2102, -0.08660, 0.4723 0.2472, -0.09640, 0.2902 0.2844, -0.10270, 0.1104 0.3225, -0.10690, -0.0691 0.3608, -0.10890, -0.2676 0.3991, -0.10830, -0.4610 0.4373, -0.10510, -0.5768 0.4757, -0.09890, -0.6525 0.5137, -0.09070, -0.7350 0.5694, -0.07640, -0.7528 15 Flap element taps 1.0000, 0.00130, -0.8916 0.9365, 0.01390, -0.8348 0.8333, 0.03280, -0.8227 0.7436, 0.04930, -0.8239 0.7049, 0.05670, -0.8225 0.6662, 0.06410, -0.8113 0.6522, 0.01390, -1.4445 0.5969, -0.00020, -1.4726 0.6000, -0.03020, -1.3576 0.6324, -0.04540, -1.0036 0.6667, -0.04880, -0.8086 0.7046, -0.04110, -0.7924 0.7429, -0.03210, -0.8099 0.8333, -0.01400, -0.8285 0.9311, -0.00120, -0.8512 --------- Run Conditions: vel=104.9 ft/s Re=1.009x10^6 AOA=39.97 Flap deflection=-60.00 Totals: Cl=0.3087 Cdp=0.5319 Cm(c/4)=0.0400 Cs=-0.2093 Ch=0.0345 Main component: Cl=0.3254 Cdp=0.5849 Cm=-0.1389 Flap component: Cl=-0.0166 Cdp=-0.0530 Cm=0.0343 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.0245 0.6175, -0.04610, -1.6299 0.5841, -0.02440, -1.6273 0.5775, 0.01750, -1.6415 0.5777, 0.04660, -1.6386 0.6274, 0.07170, -0.8893 0.5694, 0.08320, -0.9001 0.5112, 0.09370, -0.8987 0.4731, 0.09830, -0.9000 0.4349, 0.10070, -0.9084 0.3960, 0.10120, -0.9049 0.3566, 0.10020, -0.9113 0.3172, 0.09790, -0.9023 0.2778, 0.09440, -0.9108 0.2393, 0.08960, -0.8943 0.2056, 0.08360, -0.8925 0.1633, 0.07610, -0.8986 0.1261, 0.06710, -0.8954 0.0900, 0.05640, -0.8953 0.0571, 0.04390, -0.8835 0.0283, 0.02940, -0.8939 0.0142, 0.01970, -0.8927 0.0081, 0.01410, -0.8942 0.0026, 0.00780, -0.8097 0.0000, 0.00000, -0.9062 0.0037, -0.00840, -0.2848 0.0112, -0.01420, 0.4620 0.0191, -0.01930, 0.7488 0.0397, -0.03030, 0.9672 0.0706, -0.04420, 0.9995 0.1037, -0.05710, 0.9548 0.1384, -0.06890, 0.8464 0.1741, -0.07950, 0.7359 0.2102, -0.08660, 0.6008 0.2472, -0.09640, 0.4312 0.2844, -0.10270, 0.2575 0.3225, -0.10690, 0.0798 0.3608, -0.10890, -0.1223 0.3991, -0.10830, -0.3241 0.4373, -0.10510, -0.4598 0.4757, -0.09890, -0.5616 0.5137, -0.09070, -0.6908 0.5694, -0.07640, -0.7547 15 Flap element taps 1.0000, 0.00130, -1.0746 0.9365, 0.01390, -0.9291 0.8333, 0.03280, -0.9105 0.7436, 0.04930, -0.9104 0.7049, 0.05670, -0.9053 0.6662, 0.06410, -0.8956 0.6522, 0.01390, -1.6112 0.5969, -0.00020, -1.6338 0.6000, -0.03020, -1.6305 0.6324, -0.04540, -1.3647 0.6667, -0.04880, -0.9465 0.7046, -0.04110, -0.9193 0.7429, -0.03210, -0.9379 0.8333, -0.01400, -0.9472 0.9311, -0.00120, -0.9869 --------- Run Conditions: vel=103.3 ft/s Re=0.993x10^6 AOA=44.92 Flap deflection=-60.00 Totals: Cl=0.2529 Cdp=0.6346 Cm(c/4)=0.0565 Cs=-0.2707 Ch=0.0799 Main component: Cl=0.3258 Cdp=0.6801 Cm=-0.1688 Flap component: Cl=-0.0728 Cdp=-0.0455 Cm=0.0685 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.0737 0.6175, -0.04610, -1.8056 0.5841, -0.02440, -1.7967 0.5775, 0.01750, -1.8077 0.5777, 0.04660, -1.8054 0.6274, 0.07170, -0.9531 0.5694, 0.08320, -0.9694 0.5112, 0.09370, -0.9758 0.4731, 0.09830, -0.9757 0.4349, 0.10070, -0.9849 0.3960, 0.10120, -0.9837 0.3566, 0.10020, -0.9933 0.3172, 0.09790, -0.9837 0.2778, 0.09440, -0.9916 0.2393, 0.08960, -0.9747 0.2056, 0.08360, -0.9734 0.1633, 0.07610, -0.9795 0.1261, 0.06710, -0.9735 0.0900, 0.05640, -0.9711 0.0571, 0.04390, -0.9578 0.0283, 0.02940, -0.9663 0.0142, 0.01970, -0.9651 0.0081, 0.01410, -0.9652 0.0026, 0.00780, -0.8762 0.0000, 0.00000, -0.9722 0.0037, -0.00840, -0.5446 0.0112, -0.01420, 0.2632 0.0191, -0.01930, 0.6059 0.0397, -0.03030, 0.9029 0.0706, -0.04420, 0.9921 0.1037, -0.05710, 0.9868 0.1384, -0.06890, 0.9061 0.1741, -0.07950, 0.8181 0.2102, -0.08660, 0.7006 0.2472, -0.09640, 0.5475 0.2844, -0.10270, 0.3821 0.3225, -0.10690, 0.2099 0.3608, -0.10890, 0.0076 0.3991, -0.10830, -0.2036 0.4373, -0.10510, -0.3580 0.4757, -0.09890, -0.4825 0.5137, -0.09070, -0.6259 0.5694, -0.07640, -0.7432 15 Flap element taps 1.0000, 0.00130, -1.3199 0.9365, 0.01390, -1.0232 0.8333, 0.03280, -0.9933 0.7436, 0.04930, -0.9843 0.7049, 0.05670, -0.9766 0.6662, 0.06410, -0.9613 0.6522, 0.01390, -1.7924 0.5969, -0.00020, -1.8219 0.6000, -0.03020, -1.9944 0.6324, -0.04540, -1.8850 0.6667, -0.04880, -1.2031 0.7046, -0.04110, -1.1467 0.7429, -0.03210, -1.1603 0.8333, -0.01400, -1.1857 0.9311, -0.00120, -1.2038 --------- Run Conditions: vel=105.3 ft/s Re=1.005x10^6 AOA=60.00 Flap deflection=-60.00 Totals: Cl=0.0677 Cdp=0.8664 Cm(c/4)=0.0709 Cs=-0.3746 Ch=0.1496 Main component: Cl=0.2651 Cdp=0.9331 Cm=-0.2590 Flap component: Cl=-0.1974 Cdp=-0.0667 Cm=0.1338 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.9853 0.6175, -0.04610, -1.9506 0.5841, -0.02440, -1.9381 0.5775, 0.01750, -1.9567 0.5777, 0.04660, -1.9567 0.6274, 0.07170, -1.1077 0.5694, 0.08320, -1.1298 0.5112, 0.09370, -1.1532 0.4731, 0.09830, -1.1500 0.4349, 0.10070, -1.1531 0.3960, 0.10120, -1.1594 0.3566, 0.10020, -1.1598 0.3172, 0.09790, -1.1491 0.2778, 0.09440, -1.1557 0.2393, 0.08960, -1.1407 0.2056, 0.08360, -1.1464 0.1633, 0.07610, -1.1385 0.1261, 0.06710, -1.1338 0.0900, 0.05640, -1.1314 0.0571, 0.04390, -1.1221 0.0283, 0.02940, -1.1154 0.0142, 0.01970, -1.1195 0.0081, 0.01410, -1.1225 0.0026, 0.00780, -1.0175 0.0000, 0.00000, -1.1229 0.0037, -0.00840, -1.1590 0.0112, -0.01420, -0.3571 0.0191, -0.01930, 0.1023 0.0397, -0.03030, 0.6014 0.0706, -0.04420, 0.8481 0.1037, -0.05710, 0.9680 0.1384, -0.06890, 0.9995 0.1741, -0.07950, 0.9906 0.2102, -0.08660, 0.9405 0.2472, -0.09640, 0.8665 0.2844, -0.10270, 0.7530 0.3225, -0.10690, 0.6192 0.3608, -0.10890, 0.4446 0.3991, -0.10830, 0.2538 0.4373, -0.10510, 0.0704 0.4757, -0.09890, -0.0946 0.5137, -0.09070, -0.2856 0.5694, -0.07640, -0.5191 15 Flap element taps 1.0000, 0.00130, -1.4010 0.9365, 0.01390, -1.1821 0.8333, 0.03280, -1.1590 0.7436, 0.04930, -1.1476 0.7049, 0.05670, -1.1288 0.6662, 0.06410, -1.1038 0.6522, 0.01390, -1.9323 0.5969, -0.00020, -1.9667 0.6000, -0.03020, -2.5291 0.6324, -0.04540, -3.1108 0.6667, -0.04880, -2.0465 0.7046, -0.04110, -1.6238 0.7429, -0.03210, -1.6182 0.8333, -0.01400, -1.6302 0.9311, -0.00120, -1.5204 --------- Run Conditions: vel=103.0 ft/s Re=0.982x10^6 AOA=70.04 Flap deflection=-60.00 Totals: Cl=0.0590 Cdp=1.0066 Cm(c/4)=0.0092 Cs=-0.2882 Ch=-0.0126 Main component: Cl=0.2082 Cdp=1.1070 Cm=-0.3309 Flap component: Cl=-0.1493 Cdp=-0.1004 Cm=0.0985 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7635 0.6175, -0.04610, -1.8316 0.5841, -0.02440, -1.8212 0.5775, 0.01750, -1.8356 0.5777, 0.04660, -1.8344 0.6274, 0.07170, -1.2512 0.5694, 0.08320, -1.2802 0.5112, 0.09370, -1.3115 0.4731, 0.09830, -1.3113 0.4349, 0.10070, -1.3153 0.3960, 0.10120, -1.3281 0.3566, 0.10020, -1.3353 0.3172, 0.09790, -1.3320 0.2778, 0.09440, -1.3400 0.2393, 0.08960, -1.3236 0.2056, 0.08360, -1.3325 0.1633, 0.07610, -1.3208 0.1261, 0.06710, -1.3148 0.0900, 0.05640, -1.3095 0.0571, 0.04390, -1.2919 0.0283, 0.02940, -1.2772 0.0142, 0.01970, -1.2760 0.0081, 0.01410, -1.2761 0.0026, 0.00780, -1.1611 0.0000, 0.00000, -1.2722 0.0037, -0.00840, -1.4351 0.0112, -0.01420, -0.8138 0.0191, -0.01930, -0.3246 0.0397, -0.03030, 0.2733 0.0706, -0.04420, 0.6233 0.1037, -0.05710, 0.8256 0.1384, -0.06890, 0.9315 0.1741, -0.07950, 0.9880 0.2102, -0.08660, 0.9940 0.2472, -0.09640, 0.9849 0.2844, -0.10270, 0.9263 0.3225, -0.10690, 0.8444 0.3608, -0.10890, 0.7185 0.3991, -0.10830, 0.5654 0.4373, -0.10510, 0.3999 0.4757, -0.09890, 0.2317 0.5137, -0.09070, 0.0328 0.5694, -0.07640, -0.2476 15 Flap element taps 1.0000, 0.00130, -1.3397 0.9365, 0.01390, -1.3018 0.8333, 0.03280, -1.2974 0.7436, 0.04930, -1.2836 0.7049, 0.05670, -1.2707 0.6662, 0.06410, -1.2417 0.6522, 0.01390, -1.8165 0.5969, -0.00020, -1.8465 0.6000, -0.03020, -2.6624 0.6324, -0.04540, -3.8894 0.6667, -0.04880, -3.5475 0.7046, -0.04110, -2.0079 0.7429, -0.03210, -1.5808 0.8333, -0.01400, -1.1554 0.9311, -0.00120, -0.9354 --------- Run Conditions: vel=104.4 ft/s Re=0.994x10^6 AOA=80.05 Flap deflection=-60.00 Totals: Cl=0.1791 Cdp=1.2126 Cm(c/4)=-0.1115 Cs=-0.0331 Ch=-0.1725 Main component: Cl=0.1664 Cdp=1.2246 Cm=-0.3952 Flap component: Cl=0.0127 Cdp=-0.0120 Cm=-0.0226 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2142 0.6175, -0.04610, -1.1138 0.5841, -0.02440, -1.1141 0.5775, 0.01750, -1.1322 0.5777, 0.04660, -1.1268 0.6274, 0.07170, -1.3738 0.5694, 0.08320, -1.4083 0.5112, 0.09370, -1.4429 0.4731, 0.09830, -1.4405 0.4349, 0.10070, -1.4507 0.3960, 0.10120, -1.4623 0.3566, 0.10020, -1.4709 0.3172, 0.09790, -1.4550 0.2778, 0.09440, -1.4642 0.2393, 0.08960, -1.4528 0.2056, 0.08360, -1.4541 0.1633, 0.07610, -1.4449 0.1261, 0.06710, -1.4292 0.0900, 0.05640, -1.4314 0.0571, 0.04390, -1.4154 0.0283, 0.02940, -1.3969 0.0142, 0.01970, -1.3974 0.0081, 0.01410, -1.3981 0.0026, 0.00780, -1.2726 0.0000, 0.00000, -1.3945 0.0037, -0.00840, -1.5031 0.0112, -0.01420, -1.2298 0.0191, -0.01930, -0.7736 0.0397, -0.03030, -0.1353 0.0706, -0.04420, 0.2895 0.1037, -0.05710, 0.5586 0.1384, -0.06890, 0.7320 0.1741, -0.07950, 0.8547 0.2102, -0.08660, 0.9322 0.2472, -0.09640, 0.9879 0.2844, -0.10270, 0.9987 0.3225, -0.10690, 0.9874 0.3608, -0.10890, 0.9379 0.3991, -0.10830, 0.8543 0.4373, -0.10510, 0.7479 0.4757, -0.09890, 0.6228 0.5137, -0.09070, 0.4649 0.5694, -0.07640, 0.2180 15 Flap element taps 1.0000, 0.00130, -1.4615 0.9365, 0.01390, -1.4443 0.8333, 0.03280, -1.4303 0.7436, 0.04930, -1.4142 0.7049, 0.05670, -1.3982 0.6662, 0.06410, -1.3768 0.6522, 0.01390, -1.1057 0.5969, -0.00020, -1.1329 0.6000, -0.03020, -1.5926 0.6324, -0.04540, -2.9549 0.6667, -0.04880, -2.9545 0.7046, -0.04110, -1.5640 0.7429, -0.03210, -1.0942 0.8333, -0.01400, -0.7502 0.9311, -0.00120, -0.7384 --------- Run Conditions: vel=104.4 ft/s Re=0.993x10^6 AOA=90.07 Flap deflection=-60.00 Totals: Cl=0.2237 Cdp=1.4309 Cm(c/4)=-0.2219 Cs=0.2255 Ch=-0.3059 Main component: Cl=0.0902 Cdp=1.3078 Cm=-0.4423 Flap component: Cl=0.1335 Cdp=0.1231 Cm=-0.1372 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.2810 0.6175, -0.04610, -0.4897 0.5841, -0.02440, -0.3858 0.5775, 0.01750, -0.4073 0.5777, 0.04660, -0.3751 0.6274, 0.07170, -1.5358 0.5694, 0.08320, -1.5537 0.5112, 0.09370, -1.5839 0.4731, 0.09830, -1.5922 0.4349, 0.10070, -1.6023 0.3960, 0.10120, -1.6060 0.3566, 0.10020, -1.6228 0.3172, 0.09790, -1.6085 0.2778, 0.09440, -1.6149 0.2393, 0.08960, -1.6036 0.2056, 0.08360, -1.6065 0.1633, 0.07610, -1.6097 0.1261, 0.06710, -1.5920 0.0900, 0.05640, -1.5879 0.0571, 0.04390, -1.5571 0.0283, 0.02940, -1.5373 0.0142, 0.01970, -1.5340 0.0081, 0.01410, -1.5257 0.0026, 0.00780, -1.3974 0.0000, 0.00000, -1.5271 0.0037, -0.00840, -1.5515 0.0112, -0.01420, -1.5608 0.0191, -0.01930, -1.1916 0.0397, -0.03030, -0.5716 0.0706, -0.04420, -0.1100 0.1037, -0.05710, 0.2010 0.1384, -0.06890, 0.4181 0.1741, -0.07950, 0.5943 0.2102, -0.08660, 0.7349 0.2472, -0.09640, 0.8440 0.2844, -0.10270, 0.9238 0.3225, -0.10690, 0.9759 0.3608, -0.10890, 1.0024 0.3991, -0.10830, 0.9886 0.4373, -0.10510, 0.9565 0.4757, -0.09890, 0.8924 0.5137, -0.09070, 0.7924 0.5694, -0.07640, 0.6084 15 Flap element taps 1.0000, 0.00130, -1.6274 0.9365, 0.01390, -1.6138 0.8333, 0.03280, -1.5859 0.7436, 0.04930, -1.5608 0.7049, 0.05670, -1.5506 0.6662, 0.06410, -1.5228 0.6522, 0.01390, -0.4424 0.5969, -0.00020, -0.4491 0.6000, -0.03020, -0.7438 0.6324, -0.04540, -1.8788 0.6667, -0.04880, -2.0483 0.7046, -0.04110, -0.9651 0.7429, -0.03210, -0.6913 0.8333, -0.01400, -0.5221 0.9311, -0.00120, -0.6365 --------- Run Conditions: vel=103.8 ft/s Re=0.986x10^6 AOA=120.03 Flap deflection=-60.00 Totals: Cl=0.0165 Cdp=1.5544 Cm(c/4)=-0.4046 Cs=0.7921 Ch=-0.5933 Main component: Cl=-0.1583 Cdp=0.9999 Cm=-0.3630 Flap component: Cl=0.1747 Cdp=0.5545 Cm=-0.3760 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.9959 0.6175, -0.04610, 0.9566 0.5841, -0.02440, 0.9727 0.5775, 0.01750, 0.9536 0.5777, 0.04660, 0.9760 0.6274, 0.07170, -1.5980 0.5694, 0.08320, -1.6400 0.5112, 0.09370, -1.6678 0.4731, 0.09830, -1.6569 0.4349, 0.10070, -1.6660 0.3960, 0.10120, -1.6763 0.3566, 0.10020, -1.7045 0.3172, 0.09790, -1.6844 0.2778, 0.09440, -1.6944 0.2393, 0.08960, -1.6774 0.2056, 0.08360, -1.6762 0.1633, 0.07610, -1.6971 0.1261, 0.06710, -1.6919 0.0900, 0.05640, -1.7029 0.0571, 0.04390, -1.6836 0.0283, 0.02940, -1.6570 0.0142, 0.01970, -1.6408 0.0081, 0.01410, -1.6227 0.0026, 0.00780, -1.4920 0.0000, 0.00000, -1.6265 0.0037, -0.00840, -1.6228 0.0112, -0.01420, -1.6493 0.0191, -0.01930, -1.7222 0.0397, -0.03030, -1.5051 0.0706, -0.04420, -1.2155 0.1037, -0.05710, -0.9767 0.1384, -0.06890, -0.7838 0.1741, -0.07950, -0.5952 0.2102, -0.08660, -0.4128 0.2472, -0.09640, -0.2640 0.2844, -0.10270, -0.0882 0.3225, -0.10690, 0.0670 0.3608, -0.10890, 0.2384 0.3991, -0.10830, 0.3977 0.4373, -0.10510, 0.5693 0.4757, -0.09890, 0.7160 0.5137, -0.09070, 0.8286 0.5694, -0.07640, 0.9374 15 Flap element taps 1.0000, 0.00130, -1.6055 0.9365, 0.01390, -1.6178 0.8333, 0.03280, -1.6218 0.7436, 0.04930, -1.5905 0.7049, 0.05670, -1.5877 0.6662, 0.06410, -1.5766 0.6522, 0.01390, 0.9598 0.5969, -0.00020, 0.9581 0.6000, -0.03020, 0.9011 0.6324, -0.04540, 0.6850 0.6667, -0.04880, 0.4561 0.7046, -0.04110, 0.4899 0.7429, -0.03210, 0.4745 0.8333, -0.01400, 0.3257 0.9311, -0.00120, -0.0159 --------- Run Conditions: vel=106.3 ft/s Re=1.003x10^6 AOA=149.93 Flap deflection=-60.00 Totals: Cl=0.0363 Cdp=0.9767 Cm(c/4)=-0.3414 Cs=0.8634 Ch=-0.6608 Main component: Cl=0.0744 Cdp=0.2963 Cm=-0.0732 Flap component: Cl=-0.0381 Cdp=0.6803 Cm=-0.3827 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0555 0.6175, -0.04610, 0.4178 0.5841, -0.02440, 0.4516 0.5775, 0.01750, 0.3852 0.5777, 0.04660, 0.4743 0.6274, 0.07170, -1.2901 0.5694, 0.08320, -1.3108 0.5112, 0.09370, -1.3540 0.4731, 0.09830, -1.3624 0.4349, 0.10070, -1.3689 0.3960, 0.10120, -1.3595 0.3566, 0.10020, -1.3735 0.3172, 0.09790, -1.3619 0.2778, 0.09440, -1.3684 0.2393, 0.08960, -1.3474 0.2056, 0.08360, -1.3413 0.1633, 0.07610, -1.3631 0.1261, 0.06710, -1.3732 0.0900, 0.05640, -1.3853 0.0571, 0.04390, -1.3710 0.0283, 0.02940, -1.3472 0.0142, 0.01970, -1.3288 0.0081, 0.01410, -1.3058 0.0026, 0.00780, -1.1848 0.0000, 0.00000, -1.3037 0.0037, -0.00840, -1.3975 0.0112, -0.01420, -1.7474 0.0191, -0.01930, -1.8605 0.0397, -0.03030, -1.8486 0.0706, -0.04420, -1.7817 0.1037, -0.05710, -1.7292 0.1384, -0.06890, -1.6907 0.1741, -0.07950, -1.6377 0.2102, -0.08660, -1.5666 0.2472, -0.09640, -1.5586 0.2844, -0.10270, -1.4621 0.3225, -0.10690, -1.3814 0.3608, -0.10890, -1.2610 0.3991, -0.10830, -1.1071 0.4373, -0.10510, -0.8799 0.4757, -0.09890, -0.6215 0.5137, -0.09070, -0.3910 0.5694, -0.07640, -0.0875 15 Flap element taps 1.0000, 0.00130, -1.2836 0.9365, 0.01390, -1.3070 0.8333, 0.03280, -1.3174 0.7436, 0.04930, -1.3007 0.7049, 0.05670, -1.2896 0.6662, 0.06410, -1.2886 0.6522, 0.01390, 0.4161 0.5969, -0.00020, 0.2635 0.6000, -0.03020, 0.3145 0.6324, -0.04540, 0.5352 0.6667, -0.04880, 0.8366 0.7046, -0.04110, 0.9910 0.7429, -0.03210, 1.0064 0.8333, -0.01400, 0.9437 0.9311, -0.00120, 0.6805 --------- Run Conditions: vel=105.7 ft/s Re=0.999x10^6 AOA=180.07 Flap deflection=-60.00 Totals: Cl=0.3498 Cdp=0.2695 Cm(c/4)=-0.0426 Cs=0.2691 Ch=-0.3640 Main component: Cl=0.3950 Cdp=-0.0993 Cm=0.1541 Flap component: Cl=-0.0452 Cdp=0.3688 Cm=-0.1091 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.5899 0.6175, -0.04610, -1.4477 0.5841, -0.02440, -1.1560 0.5775, 0.01750, -1.2079 0.5777, 0.04660, -1.1205 0.6274, 0.07170, -0.5503 0.5694, 0.08320, -0.5485 0.5112, 0.09370, -0.5664 0.4731, 0.09830, -0.5634 0.4349, 0.10070, -0.5677 0.3960, 0.10120, -0.5695 0.3566, 0.10020, -0.5746 0.3172, 0.09790, -0.5708 0.2778, 0.09440, -0.5892 0.2393, 0.08960, -0.5843 0.2056, 0.08360, -0.5860 0.1633, 0.07610, -0.5875 0.1261, 0.06710, -0.5827 0.0900, 0.05640, -0.5751 0.0571, 0.04390, -0.5645 0.0283, 0.02940, -0.5671 0.0142, 0.01970, -0.5709 0.0081, 0.01410, -0.5673 0.0026, 0.00780, -0.5151 0.0000, 0.00000, -0.5793 0.0037, -0.00840, -0.5897 0.0112, -0.01420, -0.5698 0.0191, -0.01930, -0.5579 0.0397, -0.03030, -0.5615 0.0706, -0.04420, -0.5943 0.1037, -0.05710, -0.6305 0.1384, -0.06890, -0.7431 0.1741, -0.07950, -0.8922 0.2102, -0.08660, -1.0560 0.2472, -0.09640, -1.2589 0.2844, -0.10270, -1.4132 0.3225, -0.10690, -1.5617 0.3608, -0.10890, -1.6867 0.3991, -0.10830, -1.7494 0.4373, -0.10510, -1.7191 0.4757, -0.09890, -1.6242 0.5137, -0.09070, -1.4652 0.5694, -0.07640, -1.3302 15 Flap element taps 1.0000, 0.00130, -0.5528 0.9365, 0.01390, -0.5499 0.8333, 0.03280, -0.5522 0.7436, 0.04930, -0.5642 0.7049, 0.05670, -0.5637 0.6662, 0.06410, -0.5654 0.6522, 0.01390, -1.3573 0.5969, -0.00020, -1.8776 0.6000, -0.03020, -1.6828 0.6324, -0.04540, -1.8358 0.6667, -0.04880, -1.0260 0.7046, -0.04110, 0.1339 0.7429, -0.03210, 0.5159 0.8333, -0.01400, 0.8622 0.9311, -0.00120, 1.0070 --------- Run Conditions: vel=107.2 ft/s Re=1.011x10^6 AOA=210.04 Flap deflection=-60.00 Totals: Cl=-0.0648 Cdp=0.2489 Cm(c/4)=-0.0586 Cs=0.2479 Ch=-0.2790 Main component: Cl=0.1078 Cdp=0.0832 Cm=0.0602 Flap component: Cl=-0.1726 Cdp=0.1657 Cm=-0.1016 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6518 0.6175, -0.04610, -0.6724 0.5841, -0.02440, -0.6621 0.5775, 0.01750, -0.6733 0.5777, 0.04660, -0.6695 0.6274, 0.07170, -0.4133 0.5694, 0.08320, -0.4422 0.5112, 0.09370, -0.4354 0.4731, 0.09830, -0.3650 0.4349, 0.10070, -0.2477 0.3960, 0.10120, -0.1279 0.3566, 0.10020, -0.0653 0.3172, 0.09790, -0.0500 0.2778, 0.09440, -0.1026 0.2393, 0.08960, -0.2142 0.2056, 0.08360, -0.3704 0.1633, 0.07610, -0.5365 0.1261, 0.06710, -0.7018 0.0900, 0.05640, -0.8821 0.0571, 0.04390, -1.0768 0.0283, 0.02940, -1.1764 0.0142, 0.01970, -1.0792 0.0081, 0.01410, -0.9040 0.0026, 0.00780, -0.6248 0.0000, 0.00000, -0.6718 0.0037, -0.00840, -0.6722 0.0112, -0.01420, -0.6564 0.0191, -0.01930, -0.6474 0.0397, -0.03030, -0.6451 0.0706, -0.04420, -0.6597 0.1037, -0.05710, -0.6506 0.1384, -0.06890, -0.6647 0.1741, -0.07950, -0.6676 0.2102, -0.08660, -0.6633 0.2472, -0.09640, -0.6680 0.2844, -0.10270, -0.6651 0.3225, -0.10690, -0.6569 0.3608, -0.10890, -0.6607 0.3991, -0.10830, -0.6658 0.4373, -0.10510, -0.6645 0.4757, -0.09890, -0.6623 0.5137, -0.09070, -0.6587 0.5694, -0.07640, -0.6555 15 Flap element taps 1.0000, 0.00130, -0.4247 0.9365, 0.01390, -0.3820 0.8333, 0.03280, -0.4038 0.7436, 0.04930, -0.4333 0.7049, 0.05670, -0.4261 0.6662, 0.06410, -0.3942 0.6522, 0.01390, -0.6641 0.5969, -0.00020, -0.6639 0.6000, -0.03020, -0.6917 0.6324, -0.04540, -0.6920 0.6667, -0.04880, -0.8290 0.7046, -0.04110, -0.0806 0.7429, -0.03210, 0.2238 0.8333, -0.01400, 0.5541 0.9311, -0.00120, 0.8332 --------- Run Conditions: vel=104.7 ft/s Re=0.987x10^6 AOA=240.00 Flap deflection=-60.00 Totals: Cl=1.1697 Cdp=0.8986 Cm(c/4)=0.4440 Cs=-0.5637 Ch=0.7401 Main component: Cl=0.4463 Cdp=0.8232 Cm=0.3535 Flap component: Cl=0.7235 Cdp=0.0754 Cm=0.4313 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.4062 0.6175, -0.04610, -1.4143 0.5841, -0.02440, -1.3956 0.5775, 0.01750, -1.3990 0.5777, 0.04660, -1.3913 0.6274, 0.07170, 0.9703 0.5694, 0.08320, 0.9402 0.5112, 0.09370, 0.8352 0.4731, 0.09830, 0.7683 0.4349, 0.10070, 0.6876 0.3960, 0.10120, 0.5972 0.3566, 0.10020, 0.4942 0.3172, 0.09790, 0.3935 0.2778, 0.09440, 0.2486 0.2393, 0.08960, 0.1069 0.2056, 0.08360, -0.0708 0.1633, 0.07610, -0.2673 0.1261, 0.06710, -0.4898 0.0900, 0.05640, -0.7686 0.0571, 0.04390, -1.1221 0.0283, 0.02940, -1.3568 0.0142, 0.01970, -1.2769 0.0081, 0.01410, -1.2613 0.0026, 0.00780, -1.1527 0.0000, 0.00000, -1.2804 0.0037, -0.00840, -1.3024 0.0112, -0.01420, -1.3003 0.0191, -0.01930, -1.3112 0.0397, -0.03030, -1.3446 0.0706, -0.04420, -1.3934 0.1037, -0.05710, -1.4037 0.1384, -0.06890, -1.4079 0.1741, -0.07950, -1.4034 0.2102, -0.08660, -1.3946 0.2472, -0.09640, -1.4052 0.2844, -0.10270, -1.4256 0.3225, -0.10690, -1.4471 0.3608, -0.10890, -1.4594 0.3991, -0.10830, -1.4797 0.4373, -0.10510, -1.4796 0.4757, -0.09890, -1.4667 0.5137, -0.09070, -1.4579 0.5694, -0.07640, -1.4313 15 Flap element taps 1.0000, 0.00130, -1.3467 0.9365, 0.01390, 0.9829 0.8333, 0.03280, 0.9335 0.7436, 0.04930, 0.9288 0.7049, 0.05670, 0.9533 0.6662, 0.06410, 0.9649 0.6522, 0.01390, -1.3920 0.5969, -0.00020, -1.4019 0.6000, -0.03020, -1.4234 0.6324, -0.04540, -1.4508 0.6667, -0.04880, -1.4444 0.7046, -0.04110, -1.4183 0.7429, -0.03210, -1.3981 0.8333, -0.01400, -1.3647 0.9311, -0.00120, -1.3501 --------- Run Conditions: vel=100.5 ft/s Re=0.944x10^6 AOA=269.05 Flap deflection=-60.00 Totals: Cl=0.8084 Cdp=1.9873 Cm(c/4)=0.5592 Cs=-0.7753 Ch=0.9264 Main component: Cl=0.0619 Cdp=1.4550 Cm=0.5129 Flap component: Cl=0.7465 Cdp=0.5323 Cm=0.5464 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -2.0885 0.6175, -0.04610, -2.0800 0.5841, -0.02440, -2.0561 0.5775, 0.01750, -2.0642 0.5777, 0.04660, -2.0377 0.6274, 0.07170, 1.0021 0.5694, 0.08320, 1.0000 0.5112, 0.09370, 0.9729 0.4731, 0.09830, 0.9723 0.4349, 0.10070, 0.9472 0.3960, 0.10120, 0.9056 0.3566, 0.10020, 0.8592 0.3172, 0.09790, 0.7992 0.2778, 0.09440, 0.6984 0.2393, 0.08960, 0.5964 0.2056, 0.08360, 0.4454 0.1633, 0.07610, 0.2636 0.1261, 0.06710, 0.0203 0.0900, 0.05640, -0.3158 0.0571, 0.04390, -0.8392 0.0283, 0.02940, -1.4893 0.0142, 0.01970, -1.8697 0.0081, 0.01410, -1.8019 0.0026, 0.00780, -1.5749 0.0000, 0.00000, -1.7187 0.0037, -0.00840, -1.7448 0.0112, -0.01420, -1.7520 0.0191, -0.01930, -1.7538 0.0397, -0.03030, -1.7838 0.0706, -0.04420, -1.8522 0.1037, -0.05710, -1.9039 0.1384, -0.06890, -1.9642 0.1741, -0.07950, -2.0031 0.2102, -0.08660, -2.0166 0.2472, -0.09640, -2.0505 0.2844, -0.10270, -2.0612 0.3225, -0.10690, -2.0480 0.3608, -0.10890, -2.0516 0.3991, -0.10830, -2.0513 0.4373, -0.10510, -2.0479 0.4757, -0.09890, -2.0430 0.5137, -0.09070, -2.0510 0.5694, -0.07640, -2.0472 15 Flap element taps 1.0000, 0.00130, -1.8622 0.9365, 0.01390, 0.9095 0.8333, 0.03280, 1.0015 0.7436, 0.04930, 0.9840 0.7049, 0.05670, 0.9968 0.6662, 0.06410, 0.9989 0.6522, 0.01390, -2.0703 0.5969, -0.00020, -2.0962 0.6000, -0.03020, -2.1195 0.6324, -0.04540, -2.1224 0.6667, -0.04880, -2.0851 0.7046, -0.04110, -2.0305 0.7429, -0.03210, -2.0123 0.8333, -0.01400, -1.9499 0.9311, -0.00120, -1.8957