S809 UNVENTED AILERON, CLEAN, CHORD = 18 INCHES --------- Run Conditions: vel=218.7 ft/s Re=1.994x10^6 AOA=-6.06 Flap deflection=-60.00 Totals: Cl=-1.5194 Cdp=0.3422 Cm(c/4)=0.1727 Cs=-0.1799 Ch=0.3748 Main component: Cl=-1.3258 Cdp=-0.0082 Cm=0.3308 Flap component: Cl=-0.1936 Cdp=0.3504 Cm=0.2287 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6315 0.6175, -0.04610, -0.6190 0.5841, -0.02440, -0.6180 0.5775, 0.01750, -0.6215 0.5777, 0.04660, -0.6153 0.6274, 0.07170, 0.8582 0.5694, 0.08320, 0.8520 0.5112, 0.09370, 0.7673 0.4731, 0.09830, 0.6515 0.4349, 0.10070, 0.6198 0.3960, 0.10120, 0.6000 0.3566, 0.10020, 0.5826 0.3172, 0.09790, 0.5899 0.2778, 0.09440, 0.5982 0.2393, 0.08960, 0.6241 0.2056, 0.08360, 0.6707 0.1633, 0.07610, 0.7251 0.1261, 0.06710, 0.8057 0.0900, 0.05640, 0.8972 0.0571, 0.04390, 0.9920 0.0283, 0.02940, 0.9838 0.0142, 0.01970, 0.7170 0.0081, 0.01410, 0.2962 0.0026, 0.00780, -0.8132 0.0000, 0.00000, -4.4053 0.0037, -0.00840, -4.1111 0.0112, -0.01420, -3.9565 0.0191, -0.01930, -3.9226 0.0397, -0.03030, -3.1212 0.0706, -0.04420, -2.1415 0.1037, -0.05710, -1.8702 0.1384, -0.06890, -1.7528 0.1741, -0.07950, -1.6821 0.2102, -0.08660, -1.6502 0.2472, -0.09640, -1.6526 0.2844, -0.10270, -1.5746 0.3225, -0.10690, -1.4623 0.3608, -0.10890, -1.2758 0.3991, -0.10830, -0.9979 0.4373, -0.10510, -0.7429 0.4757, -0.09890, -0.6558 0.5137, -0.09070, -0.6231 0.5694, -0.07640, -0.6258 15 Flap element taps 1.0000, 0.00130, -0.6314 0.9365, 0.01390, 0.3089 0.8333, 0.03280, 0.6709 0.7436, 0.04930, 0.8562 0.7049, 0.05670, 0.8963 0.6662, 0.06410, 0.8618 0.6522, 0.01390, -0.6168 0.5969, -0.00020, -0.6304 0.6000, -0.03020, -0.6327 0.6324, -0.04540, -0.6488 0.6667, -0.04880, -0.6496 0.7046, -0.04110, -0.6329 0.7429, -0.03210, -0.6283 0.8333, -0.01400, -0.6262 0.9311, -0.00120, -0.6280 --------- Run Conditions: vel=219.7 ft/s Re=2.000x10^6 AOA=0.02 Flap deflection=-60.00 Totals: Cl=-1.5408 Cdp=0.2904 Cm(c/4)=0.2262 Cs=-0.2909 Ch=0.3770 Main component: Cl=-1.3109 Cdp=-0.0375 Cm=0.3820 Flap component: Cl=-0.2300 Cdp=0.3279 Cm=0.2293 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7383 0.6175, -0.04610, -0.6750 0.5841, -0.02440, -0.6712 0.5775, 0.01750, -0.6763 0.5777, 0.04660, -0.6737 0.6274, 0.07170, 0.8089 0.5694, 0.08320, 0.8077 0.5112, 0.09370, 0.7362 0.4731, 0.09830, 0.6370 0.4349, 0.10070, 0.5282 0.3960, 0.10120, 0.5091 0.3566, 0.10020, 0.4757 0.3172, 0.09790, 0.4682 0.2778, 0.09440, 0.4595 0.2393, 0.08960, 0.4701 0.2056, 0.08360, 0.5056 0.1633, 0.07610, 0.5452 0.1261, 0.06710, 0.6251 0.0900, 0.05640, 0.7219 0.0571, 0.04390, 0.8644 0.0283, 0.02940, 1.0005 0.0142, 0.01970, 0.9765 0.0081, 0.01410, 0.8150 0.0026, 0.00780, 0.0491 0.0000, 0.00000, -2.5040 0.0037, -0.00840, -3.4326 0.0112, -0.01420, -2.8580 0.0191, -0.01930, -1.8646 0.0397, -0.03030, -1.5359 0.0706, -0.04420, -1.4048 0.1037, -0.05710, -1.4308 0.1384, -0.06890, -1.4830 0.1741, -0.07950, -1.5291 0.2102, -0.08660, -1.6080 0.2472, -0.09640, -1.7405 0.2844, -0.10270, -1.7930 0.3225, -0.10690, -1.8443 0.3608, -0.10890, -1.8606 0.3991, -0.10830, -1.8081 0.4373, -0.10510, -1.6609 0.4757, -0.09890, -1.3980 0.5137, -0.09070, -1.1692 0.5694, -0.07640, -0.8739 15 Flap element taps 1.0000, 0.00130, -0.6745 0.9365, 0.01390, 0.2582 0.8333, 0.03280, 0.6372 0.7436, 0.04930, 0.8227 0.7049, 0.05670, 0.8469 0.6662, 0.06410, 0.8129 0.6522, 0.01390, -0.6672 0.5969, -0.00020, -0.6774 0.6000, -0.03020, -0.6772 0.6324, -0.04540, -0.6732 0.6667, -0.04880, -0.6722 0.7046, -0.04110, -0.6730 0.7429, -0.03210, -0.6750 0.8333, -0.01400, -0.6759 0.9311, -0.00120, -0.6790 --------- Run Conditions: vel=219.9 ft/s Re=1.994x10^6 AOA=3.00 Flap deflection=-60.00 Totals: Cl=-1.5406 Cdp=0.2876 Cm(c/4)=0.2553 Cs=-0.3679 Ch=0.4037 Main component: Cl=-1.2778 Cdp=-0.0485 Cm=0.3916 Flap component: Cl=-0.2628 Cdp=0.3361 Cm=0.2446 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8841 0.6175, -0.04610, -0.7757 0.5841, -0.02440, -0.7703 0.5775, 0.01750, -0.7730 0.5777, 0.04660, -0.7707 0.6274, 0.07170, 0.7837 0.5694, 0.08320, 0.7837 0.5112, 0.09370, 0.7222 0.4731, 0.09830, 0.6171 0.4349, 0.10070, 0.5061 0.3960, 0.10120, 0.4706 0.3566, 0.10020, 0.4314 0.3172, 0.09790, 0.4171 0.2778, 0.09440, 0.4004 0.2393, 0.08960, 0.4032 0.2056, 0.08360, 0.4321 0.1633, 0.07610, 0.4608 0.1261, 0.06710, 0.5354 0.0900, 0.05640, 0.6262 0.0571, 0.04390, 0.7753 0.0283, 0.02940, 0.9523 0.0142, 0.01970, 1.0125 0.0081, 0.01410, 0.9546 0.0026, 0.00780, 0.4568 0.0000, 0.00000, -1.3891 0.0037, -0.00840, -2.4240 0.0112, -0.01420, -1.9758 0.0191, -0.01930, -1.6723 0.0397, -0.03030, -1.2009 0.0706, -0.04420, -1.1756 0.1037, -0.05710, -1.2532 0.1384, -0.06890, -1.3481 0.1741, -0.07950, -1.4269 0.2102, -0.08660, -1.5357 0.2472, -0.09640, -1.7023 0.2844, -0.10270, -1.7869 0.3225, -0.10690, -1.8775 0.3608, -0.10890, -1.9327 0.3991, -0.10830, -1.9230 0.4373, -0.10510, -1.8199 0.4757, -0.09890, -1.5956 0.5137, -0.09070, -1.3912 0.5694, -0.07640, -1.0812 15 Flap element taps 1.0000, 0.00130, -0.7797 0.9365, 0.01390, 0.2265 0.8333, 0.03280, 0.6235 0.7436, 0.04930, 0.8009 0.7049, 0.05670, 0.8168 0.6662, 0.06410, 0.7926 0.6522, 0.01390, -0.7692 0.5969, -0.00020, -0.7801 0.6000, -0.03020, -0.7824 0.6324, -0.04540, -0.7758 0.6667, -0.04880, -0.7744 0.7046, -0.04110, -0.7777 0.7429, -0.03210, -0.7802 0.8333, -0.01400, -0.7855 0.9311, -0.00120, -0.7860 --------- Run Conditions: vel=220.7 ft/s Re=1.995x10^6 AOA=6.06 Flap deflection=-60.00 Totals: Cl=-1.3711 Cdp=0.2604 Cm(c/4)=0.2606 Cs=-0.4037 Ch=0.3898 Main component: Cl=-1.1005 Cdp=-0.0485 Cm=0.3584 Flap component: Cl=-0.2707 Cdp=0.3089 Cm=0.2362 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8741 0.6175, -0.04610, -0.7630 0.5841, -0.02440, -0.7599 0.5775, 0.01750, -0.7630 0.5777, 0.04660, -0.7612 0.6274, 0.07170, 0.7436 0.5694, 0.08320, 0.7459 0.5112, 0.09370, 0.7098 0.4731, 0.09830, 0.5895 0.4349, 0.10070, 0.4990 0.3960, 0.10120, 0.4019 0.3566, 0.10020, 0.3557 0.3172, 0.09790, 0.3315 0.2778, 0.09440, 0.3015 0.2393, 0.08960, 0.2888 0.2056, 0.08360, 0.3048 0.1633, 0.07610, 0.3138 0.1261, 0.06710, 0.3741 0.0900, 0.05640, 0.4457 0.0571, 0.04390, 0.5877 0.0283, 0.02940, 0.7928 0.0142, 0.01970, 0.9589 0.0081, 0.01410, 1.0172 0.0026, 0.00780, 0.8282 0.0000, 0.00000, -0.0067 0.0037, -0.00840, -1.0010 0.0112, -0.01420, -0.9133 0.0191, -0.01930, -0.8126 0.0397, -0.03030, -0.7242 0.0706, -0.04420, -0.7790 0.1037, -0.05710, -0.9077 0.1384, -0.06890, -1.0457 0.1741, -0.07950, -1.1782 0.2102, -0.08660, -1.3060 0.2472, -0.09640, -1.4934 0.2844, -0.10270, -1.6057 0.3225, -0.10690, -1.7395 0.3608, -0.10890, -1.8214 0.3991, -0.10830, -1.8598 0.4373, -0.10510, -1.7717 0.4757, -0.09890, -1.6410 0.5137, -0.09070, -1.2996 0.5694, -0.07640, -1.0375 15 Flap element taps 1.0000, 0.00130, -0.7525 0.9365, 0.01390, 0.2095 0.8333, 0.03280, 0.6086 0.7436, 0.04930, 0.7714 0.7049, 0.05670, 0.7694 0.6662, 0.06410, 0.7494 0.6522, 0.01390, -0.7535 0.5969, -0.00020, -0.7663 0.6000, -0.03020, -0.7646 0.6324, -0.04540, -0.7514 0.6667, -0.04880, -0.7493 0.7046, -0.04110, -0.7530 0.7429, -0.03210, -0.7550 0.8333, -0.01400, -0.7592 0.9311, -0.00120, -0.7625 --------- Run Conditions: vel=221.2 ft/s Re=1.996x10^6 AOA=9.06 Flap deflection=-60.00 Totals: Cl=-1.1425 Cdp=0.2542 Cm(c/4)=0.2651 Cs=-0.4310 Ch=0.3812 Main component: Cl=-0.8631 Cdp=-0.0319 Cm=0.3065 Flap component: Cl=-0.2794 Cdp=0.2861 Cm=0.2306 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8391 0.6175, -0.04610, -0.7609 0.5841, -0.02440, -0.7540 0.5775, 0.01750, -0.7585 0.5777, 0.04660, -0.7556 0.6274, 0.07170, 0.6821 0.5694, 0.08320, 0.6842 0.5112, 0.09370, 0.6750 0.4731, 0.09830, 0.5676 0.4349, 0.10070, 0.4480 0.3960, 0.10120, 0.3858 0.3566, 0.10020, 0.2643 0.3172, 0.09790, 0.2250 0.2778, 0.09440, 0.1830 0.2393, 0.08960, 0.1522 0.2056, 0.08360, 0.1488 0.1633, 0.07610, 0.1309 0.1261, 0.06710, 0.1670 0.0900, 0.05640, 0.2058 0.0571, 0.04390, 0.3147 0.0283, 0.02940, 0.4992 0.0142, 0.01970, 0.7129 0.0081, 0.01410, 0.8601 0.0026, 0.00780, 0.9737 0.0000, 0.00000, 0.8447 0.0037, -0.00840, 0.1497 0.0112, -0.01420, -0.0320 0.0191, -0.01930, -0.0908 0.0397, -0.03030, -0.1873 0.0706, -0.04420, -0.3416 0.1037, -0.05710, -0.5158 0.1384, -0.06890, -0.6905 0.1741, -0.07950, -0.8458 0.2102, -0.08660, -0.9921 0.2472, -0.09640, -1.1968 0.2844, -0.10270, -1.3283 0.3225, -0.10690, -1.4841 0.3608, -0.10890, -1.5875 0.3991, -0.10830, -1.6539 0.4373, -0.10510, -1.5963 0.4757, -0.09890, -1.4697 0.5137, -0.09070, -1.2450 0.5694, -0.07640, -0.9746 15 Flap element taps 1.0000, 0.00130, -0.7503 0.9365, 0.01390, 0.1860 0.8333, 0.03280, 0.5966 0.7436, 0.04930, 0.7284 0.7049, 0.05670, 0.7025 0.6662, 0.06410, 0.6891 0.6522, 0.01390, -0.7525 0.5969, -0.00020, -0.7632 0.6000, -0.03020, -0.7635 0.6324, -0.04540, -0.7516 0.6667, -0.04880, -0.7466 0.7046, -0.04110, -0.7509 0.7429, -0.03210, -0.7520 0.8333, -0.01400, -0.7565 0.9311, -0.00120, -0.7596 --------- Run Conditions: vel=221.8 ft/s Re=1.996x10^6 AOA=12.08 Flap deflection=-60.00 Totals: Cl=-0.9003 Cdp=0.2433 Cm(c/4)=0.2656 Cs=-0.4263 Ch=0.3680 Main component: Cl=-0.6186 Cdp=-0.0151 Cm=0.2516 Flap component: Cl=-0.2816 Cdp=0.2583 Cm=0.2214 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7956 0.6175, -0.04610, -0.7433 0.5841, -0.02440, -0.7398 0.5775, 0.01750, -0.7450 0.5777, 0.04660, -0.7422 0.6274, 0.07170, 0.6082 0.5694, 0.08320, 0.6063 0.5112, 0.09370, 0.6168 0.4731, 0.09830, 0.5568 0.4349, 0.10070, 0.4160 0.3960, 0.10120, 0.3239 0.3566, 0.10020, 0.2220 0.3172, 0.09790, 0.1576 0.2778, 0.09440, 0.0486 0.2393, 0.08960, 0.0057 0.2056, 0.08360, -0.0190 0.1633, 0.07610, -0.0696 0.1261, 0.06710, -0.0668 0.0900, 0.05640, -0.0757 0.0571, 0.04390, -0.0300 0.0283, 0.02940, 0.0767 0.0142, 0.01970, 0.2522 0.0081, 0.01410, 0.4105 0.0026, 0.00780, 0.6024 0.0000, 0.00000, 0.9849 0.0037, -0.00840, 0.8238 0.0112, -0.01420, 0.5873 0.0191, -0.01930, 0.4583 0.0397, -0.03030, 0.2607 0.0706, -0.04420, 0.0490 0.1037, -0.05710, -0.1523 0.1384, -0.06890, -0.3523 0.1741, -0.07950, -0.5233 0.2102, -0.08660, -0.6815 0.2472, -0.09640, -0.8964 0.2844, -0.10270, -1.0422 0.3225, -0.10690, -1.2156 0.3608, -0.10890, -1.3366 0.3991, -0.10830, -1.4278 0.4373, -0.10510, -1.3998 0.4757, -0.09890, -1.2935 0.5137, -0.09070, -1.1571 0.5694, -0.07640, -0.8964 15 Flap element taps 1.0000, 0.00130, -0.7363 0.9365, 0.01390, 0.1700 0.8333, 0.03280, 0.5868 0.7436, 0.04930, 0.6549 0.7049, 0.05670, 0.6186 0.6662, 0.06410, 0.6126 0.6522, 0.01390, -0.7357 0.5969, -0.00020, -0.7488 0.6000, -0.03020, -0.7465 0.6324, -0.04540, -0.7327 0.6667, -0.04880, -0.7268 0.7046, -0.04110, -0.7325 0.7429, -0.03210, -0.7336 0.8333, -0.01400, -0.7376 0.9311, -0.00120, -0.7462 --------- Run Conditions: vel=222.6 ft/s Re=1.992x10^6 AOA=15.08 Flap deflection=-60.00 Totals: Cl=-0.6550 Cdp=0.2333 Cm(c/4)=0.2629 Cs=-0.3957 Ch=0.3533 Main component: Cl=-0.3761 Cdp=0.0054 Cm=0.1952 Flap component: Cl=-0.2789 Cdp=0.2279 Cm=0.2106 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7518 0.6175, -0.04610, -0.7443 0.5841, -0.02440, -0.7413 0.5775, 0.01750, -0.7342 0.5777, 0.04660, -0.7339 0.6274, 0.07170, 0.4938 0.5694, 0.08320, 0.4968 0.5112, 0.09370, 0.5160 0.4731, 0.09830, 0.5034 0.4349, 0.10070, 0.4104 0.3960, 0.10120, 0.2749 0.3566, 0.10020, 0.1540 0.3172, 0.09790, 0.0657 0.2778, 0.09440, -0.0204 0.2393, 0.08960, -0.1288 0.2056, 0.08360, -0.2189 0.1633, 0.07610, -0.2797 0.1261, 0.06710, -0.3271 0.0900, 0.05640, -0.3868 0.0571, 0.04390, -0.4350 0.0283, 0.02940, -0.4557 0.0142, 0.01970, -0.4053 0.0081, 0.01410, -0.3434 0.0026, 0.00780, -0.1031 0.0000, 0.00000, 0.4160 0.0037, -0.00840, 1.0081 0.0112, -0.01420, 0.9253 0.0191, -0.01930, 0.8143 0.0397, -0.03030, 0.6002 0.0706, -0.04420, 0.3681 0.1037, -0.05710, 0.1563 0.1384, -0.06890, -0.0392 0.1741, -0.07950, -0.2177 0.2102, -0.08660, -0.4001 0.2472, -0.09640, -0.6109 0.2844, -0.10270, -0.7721 0.3225, -0.10690, -0.9465 0.3608, -0.10890, -1.0931 0.3991, -0.10830, -1.1974 0.4373, -0.10510, -1.2066 0.4757, -0.09890, -1.1295 0.5137, -0.09070, -1.0625 0.5694, -0.07640, -0.8257 15 Flap element taps 1.0000, 0.00130, -0.7232 0.9365, 0.01390, 0.1636 0.8333, 0.03280, 0.5713 0.7436, 0.04930, 0.5422 0.7049, 0.05670, 0.4912 0.6662, 0.06410, 0.4914 0.6522, 0.01390, -0.7258 0.5969, -0.00020, -0.7376 0.6000, -0.03020, -0.7323 0.6324, -0.04540, -0.7190 0.6667, -0.04880, -0.7130 0.7046, -0.04110, -0.7154 0.7429, -0.03210, -0.7194 0.8333, -0.01400, -0.7284 0.9311, -0.00120, -0.7268 --------- Run Conditions: vel=223.2 ft/s Re=1.997x10^6 AOA=18.03 Flap deflection=-60.00 Totals: Cl=-0.3785 Cdp=0.2124 Cm(c/4)=0.2420 Cs=-0.3191 Ch=0.3159 Main component: Cl=-0.1283 Cdp=0.0311 Cm=0.1319 Flap component: Cl=-0.2501 Cdp=0.1813 Cm=0.1837 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6902 0.6175, -0.04610, -0.7134 0.5841, -0.02440, -0.7146 0.5775, 0.01750, -0.7071 0.5777, 0.04660, -0.7067 0.6274, 0.07170, 0.2993 0.5694, 0.08320, 0.2839 0.5112, 0.09370, 0.3030 0.4731, 0.09830, 0.3022 0.4349, 0.10070, 0.3008 0.3960, 0.10120, 0.2844 0.3566, 0.10020, 0.1876 0.3172, 0.09790, 0.0478 0.2778, 0.09440, -0.0988 0.2393, 0.08960, -0.2325 0.2056, 0.08360, -0.3484 0.1633, 0.07610, -0.4647 0.1261, 0.06710, -0.5625 0.0900, 0.05640, -0.6982 0.0571, 0.04390, -0.8931 0.0283, 0.02940, -1.1030 0.0142, 0.01970, -1.2591 0.0081, 0.01410, -1.3566 0.0026, 0.00780, -1.2098 0.0000, 0.00000, -0.9869 0.0037, -0.00840, 0.8145 0.0112, -0.01420, 1.0113 0.0191, -0.01930, 0.9907 0.0397, -0.03030, 0.8400 0.0706, -0.04420, 0.6286 0.1037, -0.05710, 0.4261 0.1384, -0.06890, 0.2302 0.1741, -0.07950, 0.0514 0.2102, -0.08660, -0.1297 0.2472, -0.09640, -0.3399 0.2844, -0.10270, -0.5075 0.3225, -0.10690, -0.6903 0.3608, -0.10890, -0.8472 0.3991, -0.10830, -0.9691 0.4373, -0.10510, -1.0024 0.4757, -0.09890, -0.9541 0.5137, -0.09070, -0.9193 0.5694, -0.07640, -0.7290 15 Flap element taps 1.0000, 0.00130, -0.7010 0.9365, 0.01390, 0.1886 0.8333, 0.03280, 0.4388 0.7436, 0.04930, 0.2814 0.7049, 0.05670, 0.2707 0.6662, 0.06410, 0.2891 0.6522, 0.01390, -0.6984 0.5969, -0.00020, -0.7089 0.6000, -0.03020, -0.7048 0.6324, -0.04540, -0.6891 0.6667, -0.04880, -0.6818 0.7046, -0.04110, -0.6850 0.7429, -0.03210, -0.6876 0.8333, -0.01400, -0.6935 0.9311, -0.00120, -0.6972 --------- Run Conditions: vel=223.8 ft/s Re=1.997x10^6 AOA=20.02 Flap deflection=-60.00 Totals: Cl=-0.1644 Cdp=0.1992 Cm(c/4)=0.2157 Cs=-0.2434 Ch=0.2736 Main component: Cl=0.0513 Cdp=0.0560 Cm=0.0811 Flap component: Cl=-0.2157 Cdp=0.1431 Cm=0.1562 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6334 0.6175, -0.04610, -0.6857 0.5841, -0.02440, -0.6793 0.5775, 0.01750, -0.6814 0.5777, 0.04660, -0.6795 0.6274, 0.07170, 0.1159 0.5694, 0.08320, 0.0848 0.5112, 0.09370, 0.1036 0.4731, 0.09830, 0.1200 0.4349, 0.10070, 0.1220 0.3960, 0.10120, 0.1307 0.3566, 0.10020, 0.1134 0.3172, 0.09790, 0.0695 0.2778, 0.09440, -0.0672 0.2393, 0.08960, -0.2447 0.2056, 0.08360, -0.4107 0.1633, 0.07610, -0.5774 0.1261, 0.06710, -0.7280 0.0900, 0.05640, -0.9372 0.0571, 0.04390, -1.1895 0.0283, 0.02940, -1.5429 0.0142, 0.01970, -1.9403 0.0081, 0.01410, -2.2469 0.0026, 0.00780, -2.1693 0.0000, 0.00000, -2.4080 0.0037, -0.00840, 0.4416 0.0112, -0.01420, 0.9473 0.0191, -0.01930, 1.0121 0.0397, -0.03030, 0.9434 0.0706, -0.04420, 0.7691 0.1037, -0.05710, 0.5844 0.1384, -0.06890, 0.3940 0.1741, -0.07950, 0.2204 0.2102, -0.08660, 0.0450 0.2472, -0.09640, -0.1616 0.2844, -0.10270, -0.3297 0.3225, -0.10690, -0.5153 0.3608, -0.10890, -0.6763 0.3991, -0.10830, -0.8072 0.4373, -0.10510, -0.8546 0.4757, -0.09890, -0.8243 0.5137, -0.09070, -0.8174 0.5694, -0.07640, -0.6496 15 Flap element taps 1.0000, 0.00130, -0.6711 0.9365, 0.01390, 0.1818 0.8333, 0.03280, 0.2548 0.7436, 0.04930, 0.0915 0.7049, 0.05670, 0.0893 0.6662, 0.06410, 0.1198 0.6522, 0.01390, -0.6805 0.5969, -0.00020, -0.6901 0.6000, -0.03020, -0.6863 0.6324, -0.04540, -0.6674 0.6667, -0.04880, -0.6594 0.7046, -0.04110, -0.6633 0.7429, -0.03210, -0.6648 0.8333, -0.01400, -0.6687 0.9311, -0.00120, -0.6669 --------- Run Conditions: vel=224.1 ft/s Re=1.995x10^6 AOA=24.05 Flap deflection=-60.00 Totals: Cl=0.4768 Cdp=0.3200 Cm(c/4)=0.0346 Cs=-0.0979 Ch=0.0442 Main component: Cl=0.4853 Cdp=0.3414 Cm=-0.1239 Flap component: Cl=-0.0086 Cdp=-0.0214 Cm=0.0170 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6194 0.6175, -0.04610, -0.8066 0.5841, -0.02440, -0.8062 0.5775, 0.01750, -0.8093 0.5777, 0.04660, -0.8067 0.6274, 0.07170, -0.6504 0.5694, 0.08320, -0.8148 0.5112, 0.09370, -0.8586 0.4731, 0.09830, -0.9066 0.4349, 0.10070, -0.9761 0.3960, 0.10120, -1.0295 0.3566, 0.10020, -1.0937 0.3172, 0.09790, -1.1169 0.2778, 0.09440, -1.1153 0.2393, 0.08960, -1.0917 0.2056, 0.08360, -1.0561 0.1633, 0.07610, -1.0339 0.1261, 0.06710, -0.9797 0.0900, 0.05640, -0.9424 0.0571, 0.04390, -0.9082 0.0283, 0.02940, -0.8783 0.0142, 0.01970, -0.8811 0.0081, 0.01410, -0.8862 0.0026, 0.00780, -0.8384 0.0000, 0.00000, -1.3214 0.0037, -0.00840, 0.2529 0.0112, -0.01420, 0.8343 0.0191, -0.01930, 0.9747 0.0397, -0.03030, 1.0019 0.0706, -0.04420, 0.9024 0.1037, -0.05710, 0.7633 0.1384, -0.06890, 0.6013 0.1741, -0.07950, 0.4493 0.2102, -0.08660, 0.2918 0.2472, -0.09640, 0.1003 0.2844, -0.10270, -0.0614 0.3225, -0.10690, -0.2442 0.3608, -0.10890, -0.4075 0.3991, -0.10830, -0.5509 0.4373, -0.10510, -0.6220 0.4757, -0.09890, -0.6245 0.5137, -0.09070, -0.6884 0.5694, -0.07640, -0.5558 15 Flap element taps 1.0000, 0.00130, -0.5815 0.9365, 0.01390, -0.2433 0.8333, 0.03280, -0.4532 0.7436, 0.04930, -0.6571 0.7049, 0.05670, -0.6909 0.6662, 0.06410, -0.6071 0.6522, 0.01390, -0.7994 0.5969, -0.00020, -0.8070 0.6000, -0.03020, -0.6377 0.6324, -0.04540, -0.5131 0.6667, -0.04880, -0.4997 0.7046, -0.04110, -0.5072 0.7429, -0.03210, -0.5052 0.8333, -0.01400, -0.5130 0.9311, -0.00120, -0.5268 --------- Run Conditions: vel=224.6 ft/s Re=1.994x10^6 AOA=27.05 Flap deflection=-60.00 Totals: Cl=0.4839 Cdp=0.3098 Cm(c/4)=-0.0160 Cs=-0.0558 Ch=-0.0865 Main component: Cl=0.3936 Cdp=0.3872 Cm=-0.1092 Flap component: Cl=0.0903 Cdp=-0.0774 Cm=-0.0497 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7354 0.6175, -0.04610, -1.0619 0.5841, -0.02440, -1.0603 0.5775, 0.01750, -1.0600 0.5777, 0.04660, -1.0573 0.6274, 0.07170, -0.8290 0.5694, 0.08320, -0.8723 0.5112, 0.09370, -0.8776 0.4731, 0.09830, -0.8824 0.4349, 0.10070, -0.8779 0.3960, 0.10120, -0.8637 0.3566, 0.10020, -0.8687 0.3172, 0.09790, -0.8628 0.2778, 0.09440, -0.8632 0.2393, 0.08960, -0.8553 0.2056, 0.08360, -0.8428 0.1633, 0.07610, -0.8527 0.1261, 0.06710, -0.8443 0.0900, 0.05640, -0.8474 0.0571, 0.04390, -0.8445 0.0283, 0.02940, -0.8479 0.0142, 0.01970, -0.8596 0.0081, 0.01410, -0.8630 0.0026, 0.00780, -0.8016 0.0000, 0.00000, -0.9554 0.0037, -0.00840, 0.2825 0.0112, -0.01420, 0.8277 0.0191, -0.01930, 0.9686 0.0397, -0.03030, 1.0082 0.0706, -0.04420, 0.9257 0.1037, -0.05710, 0.8004 0.1384, -0.06890, 0.6455 0.1741, -0.07950, 0.4994 0.2102, -0.08660, 0.3468 0.2472, -0.09640, 0.1564 0.2844, -0.10270, -0.0080 0.3225, -0.10690, -0.1975 0.3608, -0.10890, -0.3698 0.3991, -0.10830, -0.5278 0.4373, -0.10510, -0.6161 0.4757, -0.09890, -0.6434 0.5137, -0.09070, -0.6915 0.5694, -0.07640, -0.6153 15 Flap element taps 1.0000, 0.00130, -0.9893 0.9365, 0.01390, -0.9440 0.8333, 0.03280, -0.9237 0.7436, 0.04930, -0.8881 0.7049, 0.05670, -0.8603 0.6662, 0.06410, -0.8427 0.6522, 0.01390, -1.0595 0.5969, -0.00020, -1.0683 0.6000, -0.03020, -0.8084 0.6324, -0.04540, -0.6065 0.6667, -0.04880, -0.5706 0.7046, -0.04110, -0.5768 0.7429, -0.03210, -0.5859 0.8333, -0.01400, -0.5934 0.9311, -0.00120, -0.6430