S809 UNVENTED AILERON, LEGR, CHORD = 18 IN --------- Run Conditions: vel=206.8 ft/s Re=2.013x10^6 AOA=-6.00 Flap deflection=-20.00 Totals: Cl=-0.9810 Cdp=0.1187 Cm(c/4)=0.0958 Cs=-0.0155 Ch=0.1678 Main component: Cl=-0.8025 Cdp=0.0421 Cm=0.1916 Flap component: Cl=-0.1786 Cdp=0.0766 Cm=0.1512 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4308 0.6175, -0.04610, -0.4097 0.5841, -0.02440, -0.3999 0.5775, 0.01750, -0.4014 0.5777, 0.04660, -0.3977 0.6274, 0.07170, 0.4521 0.5694, 0.08320, 0.3015 0.5112, 0.09370, 0.0897 0.4731, 0.09830, 0.0075 0.4349, 0.10070, -0.0101 0.3960, 0.10120, 0.0227 0.3566, 0.10020, 0.0509 0.3172, 0.09790, 0.0975 0.2778, 0.09440, 0.1367 0.2393, 0.08960, 0.1823 0.2056, 0.08360, 0.2516 0.1633, 0.07610, 0.3377 0.1261, 0.06710, 0.4587 0.0900, 0.05640, 0.5419 0.0571, 0.04390, 0.7804 0.0283, 0.02940, 0.9717 0.0142, 0.01970, 1.0015 0.0081, 0.01410, 0.8878 0.0026, 0.00780, 0.1659 0.0000, 0.00000, -0.0928 0.0037, -0.00840, -2.8579 0.0112, -0.01420, -2.1269 0.0191, -0.01930, -1.8829 0.0397, -0.03030, -1.4142 0.0706, -0.04420, -1.2961 0.1037, -0.05710, -1.1895 0.1384, -0.06890, -1.2396 0.1741, -0.07950, -1.2413 0.2102, -0.08660, -1.2830 0.2472, -0.09640, -1.3351 0.2844, -0.10270, -1.3195 0.3225, -0.10690, -1.2812 0.3608, -0.10890, -1.1944 0.3991, -0.10830, -1.0192 0.4373, -0.10510, -0.7503 0.4757, -0.09890, -0.5036 0.5137, -0.09070, -0.4407 0.5694, -0.07640, -0.4336 14 Flap element taps 1.0000, 0.00130, -0.4239 0.9365, 0.01390, -0.0709 0.8333, 0.03280, 0.1442 0.7436, 0.04930, 0.3185 0.7049, 0.05670, 0.4273 0.6662, 0.06410, 0.4863 0.6522, 0.01390, -0.3978 0.5969, -0.00020, -0.4088 0.6000, -0.03020, -0.4252 0.6324, -0.04540, -0.4141 0.6667, -0.04880, -0.4234 0.7046, -0.04110, -0.4289 0.7429, -0.03210, -0.4343 0.9311, -0.00120, -0.4468 --------- Run Conditions: vel=208.7 ft/s Re=2.023x10^6 AOA=0.02 Flap deflection=-20.00 Totals: Cl=-0.8043 Cdp=0.0595 Cm(c/4)=0.1187 Cs=-0.0597 Ch=0.1420 Main component: Cl=-0.6473 Cdp=0.0126 Cm=0.1920 Flap component: Cl=-0.1570 Cdp=0.0469 Cm=0.1278 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4115 0.6175, -0.04610, -0.3201 0.5841, -0.02440, -0.3038 0.5775, 0.01750, -0.3049 0.5777, 0.04660, -0.3000 0.6274, 0.07170, 0.3688 0.5694, 0.08320, 0.2542 0.5112, 0.09370, 0.0227 0.4731, 0.09830, -0.0913 0.4349, 0.10070, -0.1355 0.3960, 0.10120, -0.1229 0.3566, 0.10020, -0.1197 0.3172, 0.09790, -0.0942 0.2778, 0.09440, -0.0793 0.2393, 0.08960, -0.0595 0.2056, 0.08360, -0.0141 0.1633, 0.07610, 0.0449 0.1261, 0.06710, 0.1435 0.0900, 0.05640, 0.1598 0.0571, 0.04390, 0.4333 0.0283, 0.02940, 0.6939 0.0142, 0.01970, 0.9073 0.0081, 0.01410, 0.9968 0.0026, 0.00780, 0.8278 0.0000, 0.00000, -0.0140 0.0037, -0.00840, -0.7075 0.0112, -0.01420, -0.6492 0.0191, -0.01930, -0.6969 0.0397, -0.03030, -0.6112 0.0706, -0.04420, -0.6947 0.1037, -0.05710, -0.7138 0.1384, -0.06890, -0.8707 0.1741, -0.07950, -0.9533 0.2102, -0.08660, -1.0627 0.2472, -0.09640, -1.1999 0.2844, -0.10270, -1.2711 0.3225, -0.10690, -1.3374 0.3608, -0.10890, -1.3735 0.3991, -0.10830, -1.3498 0.4373, -0.10510, -1.2589 0.4757, -0.09890, -1.0482 0.5137, -0.09070, -0.8756 0.5694, -0.07640, -0.5867 14 Flap element taps 1.0000, 0.00130, -0.3243 0.9365, 0.01390, -0.0291 0.8333, 0.03280, 0.1526 0.7436, 0.04930, 0.3088 0.7049, 0.05670, 0.3925 0.6662, 0.06410, 0.3985 0.6522, 0.01390, -0.2993 0.5969, -0.00020, -0.3165 0.6000, -0.03020, -0.3479 0.6324, -0.04540, -0.3320 0.6667, -0.04880, -0.3239 0.7046, -0.04110, -0.3246 0.7429, -0.03210, -0.3286 0.9311, -0.00120, -0.3500 --------- Run Conditions: vel=207.7 ft/s Re=2.007x10^6 AOA=3.04 Flap deflection=-20.00 Totals: Cl=-0.5741 Cdp=0.0447 Cm(c/4)=0.1220 Cs=-0.0751 Ch=0.1316 Main component: Cl=-0.4275 Cdp=0.0105 Cm=0.1470 Flap component: Cl=-0.1466 Cdp=0.0342 Cm=0.1178 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4051 0.6175, -0.04610, -0.2985 0.5841, -0.02440, -0.2842 0.5775, 0.01750, -0.2869 0.5777, 0.04660, -0.2831 0.6274, 0.07170, 0.2971 0.5694, 0.08320, 0.2089 0.5112, 0.09370, -0.0282 0.4731, 0.09830, -0.1616 0.4349, 0.10070, -0.2250 0.3960, 0.10120, -0.2237 0.3566, 0.10020, -0.2396 0.3172, 0.09790, -0.2282 0.2778, 0.09440, -0.2308 0.2393, 0.08960, -0.2295 0.2056, 0.08360, -0.2016 0.1633, 0.07610, -0.1675 0.1261, 0.06710, -0.0911 0.0900, 0.05640, -0.1322 0.0571, 0.04390, 0.1323 0.0283, 0.02940, 0.3758 0.0142, 0.01970, 0.6123 0.0081, 0.01410, 0.7936 0.0026, 0.00780, 0.9126 0.0000, 0.00000, 0.0411 0.0037, -0.00840, 0.2638 0.0112, -0.01420, 0.0674 0.0191, -0.01930, -0.0637 0.0397, -0.03030, -0.1410 0.0706, -0.04420, -0.3021 0.1037, -0.05710, -0.3760 0.1384, -0.06890, -0.5690 0.1741, -0.07950, -0.6802 0.2102, -0.08660, -0.8071 0.2472, -0.09640, -0.9653 0.2844, -0.10270, -1.0570 0.3225, -0.10690, -1.1505 0.3608, -0.10890, -1.2084 0.3991, -0.10830, -1.2158 0.4373, -0.10510, -1.1592 0.4757, -0.09890, -0.9822 0.5137, -0.09070, -0.8421 0.5694, -0.07640, -0.5778 14 Flap element taps 1.0000, 0.00130, -0.2953 0.9365, 0.01390, -0.0275 0.8333, 0.03280, 0.1418 0.7436, 0.04930, 0.2877 0.7049, 0.05670, 0.3480 0.6662, 0.06410, 0.3225 0.6522, 0.01390, -0.2789 0.5969, -0.00020, -0.2944 0.6000, -0.03020, -0.3261 0.6324, -0.04540, -0.3114 0.6667, -0.04880, -0.3028 0.7046, -0.04110, -0.3016 0.7429, -0.03210, -0.3035 0.9311, -0.00120, -0.3265 --------- Run Conditions: vel=207.8 ft/s Re=2.002x10^6 AOA=6.04 Flap deflection=-20.00 Totals: Cl=-0.3150 Cdp=0.0385 Cm(c/4)=0.1236 Cs=-0.0715 Ch=0.1221 Main component: Cl=-0.1809 Cdp=0.0164 Cm=0.0938 Flap component: Cl=-0.1341 Cdp=0.0221 Cm=0.1071 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3837 0.6175, -0.04610, -0.2868 0.5841, -0.02440, -0.2729 0.5775, 0.01750, -0.2761 0.5777, 0.04660, -0.2737 0.6274, 0.07170, 0.1958 0.5694, 0.08320, 0.1451 0.5112, 0.09370, -0.0736 0.4731, 0.09830, -0.2311 0.4349, 0.10070, -0.3192 0.3960, 0.10120, -0.3350 0.3566, 0.10020, -0.3721 0.3172, 0.09790, -0.3783 0.2778, 0.09440, -0.4017 0.2393, 0.08960, -0.4227 0.2056, 0.08360, -0.4177 0.1633, 0.07610, -0.4158 0.1261, 0.06710, -0.3704 0.0900, 0.05640, -0.4833 0.0571, 0.04390, -0.2575 0.0283, 0.02940, -0.0865 0.0142, 0.01970, 0.1164 0.0081, 0.01410, 0.2849 0.0026, 0.00780, 0.4094 0.0000, 0.00000, 0.0821 0.0037, -0.00840, 0.8505 0.0112, -0.01420, 0.6177 0.0191, -0.01930, 0.4541 0.0397, -0.03030, 0.2712 0.0706, -0.04420, 0.0650 0.1037, -0.05710, -0.0556 0.1384, -0.06890, -0.2702 0.1741, -0.07950, -0.4031 0.2102, -0.08660, -0.5414 0.2472, -0.09640, -0.7139 0.2844, -0.10270, -0.8225 0.3225, -0.10690, -0.9377 0.3608, -0.10890, -1.0157 0.3991, -0.10830, -1.0486 0.4373, -0.10510, -1.0206 0.4757, -0.09890, -0.8772 0.5137, -0.09070, -0.7641 0.5694, -0.07640, -0.5341 14 Flap element taps 1.0000, 0.00130, -0.2713 0.9365, 0.01390, -0.0286 0.8333, 0.03280, 0.1282 0.7436, 0.04930, 0.2517 0.7049, 0.05670, 0.2694 0.6662, 0.06410, 0.2147 0.6522, 0.01390, -0.2684 0.5969, -0.00020, -0.2813 0.6000, -0.03020, -0.3119 0.6324, -0.04540, -0.2973 0.6667, -0.04880, -0.2872 0.7046, -0.04110, -0.2847 0.7429, -0.03210, -0.2844 0.9311, -0.00120, -0.3135 --------- Run Conditions: vel=208.9 ft/s Re=2.005x10^6 AOA=9.04 Flap deflection=-20.00 Totals: Cl=-0.0452 Cdp=0.0429 Cm(c/4)=0.1216 Cs=-0.0494 Ch=0.1108 Main component: Cl=0.0706 Cdp=0.0330 Cm=0.0381 Flap component: Cl=-0.1158 Cdp=0.0099 Cm=0.0930 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3525 0.6175, -0.04610, -0.2756 0.5841, -0.02440, -0.2651 0.5775, 0.01750, -0.2685 0.5777, 0.04660, -0.2666 0.6274, 0.07170, 0.0801 0.5694, 0.08320, 0.0513 0.5112, 0.09370, -0.1007 0.4731, 0.09830, -0.2793 0.4349, 0.10070, -0.3986 0.3960, 0.10120, -0.4380 0.3566, 0.10020, -0.5010 0.3172, 0.09790, -0.5293 0.2778, 0.09440, -0.5770 0.2393, 0.08960, -0.6243 0.2056, 0.08360, -0.6475 0.1633, 0.07610, -0.6847 0.1261, 0.06710, -0.6805 0.0900, 0.05640, -0.8690 0.0571, 0.04390, -0.7215 0.0283, 0.02940, -0.6740 0.0142, 0.01970, -0.5928 0.0081, 0.01410, -0.5148 0.0026, 0.00780, -0.2163 0.0000, 0.00000, 0.1245 0.0037, -0.00840, 1.0046 0.0112, -0.01420, 0.9318 0.0191, -0.01930, 0.8088 0.0397, -0.03030, 0.6007 0.0706, -0.04420, 0.3786 0.1037, -0.05710, 0.2311 0.1384, -0.06890, 0.0094 0.1741, -0.07950, -0.1374 0.2102, -0.08660, -0.2822 0.2472, -0.09640, -0.4629 0.2844, -0.10270, -0.5835 0.3225, -0.10690, -0.7167 0.3608, -0.10890, -0.8096 0.3991, -0.10830, -0.8661 0.4373, -0.10510, -0.8637 0.4757, -0.09890, -0.7533 0.5137, -0.09070, -0.6675 0.5694, -0.07640, -0.4706 14 Flap element taps 1.0000, 0.00130, -0.2385 0.9365, 0.01390, -0.0198 0.8333, 0.03280, 0.1216 0.7436, 0.04930, 0.1816 0.7049, 0.05670, 0.1547 0.6662, 0.06410, 0.0905 0.6522, 0.01390, -0.2593 0.5969, -0.00020, -0.2730 0.6000, -0.03020, -0.2964 0.6324, -0.04540, -0.2815 0.6667, -0.04880, -0.2637 0.7046, -0.04110, -0.2572 0.7429, -0.03210, -0.2566 0.9311, -0.00120, -0.2951 --------- Run Conditions: vel=209.2 ft/s Re=2.003x10^6 AOA=12.04 Flap deflection=-20.00 Totals: Cl=0.2273 Cdp=0.0557 Cm(c/4)=0.1139 Cs=-0.0071 Ch=0.0928 Main component: Cl=0.3136 Cdp=0.0588 Cm=-0.0158 Flap component: Cl=-0.0863 Cdp=-0.0031 Cm=0.0712 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3177 0.6175, -0.04610, -0.2794 0.5841, -0.02440, -0.2700 0.5775, 0.01750, -0.2722 0.5777, 0.04660, -0.2717 0.6274, 0.07170, -0.0547 0.5694, 0.08320, -0.0750 0.5112, 0.09370, -0.1322 0.4731, 0.09830, -0.2847 0.4349, 0.10070, -0.4368 0.3960, 0.10120, -0.5101 0.3566, 0.10020, -0.6063 0.3172, 0.09790, -0.6621 0.2778, 0.09440, -0.7382 0.2393, 0.08960, -0.8170 0.2056, 0.08360, -0.8729 0.1633, 0.07610, -0.9583 0.1261, 0.06710, -1.0025 0.0900, 0.05640, -1.2690 0.0571, 0.04390, -1.2386 0.0283, 0.02940, -1.3762 0.0142, 0.01970, -1.5038 0.0081, 0.01410, -1.5632 0.0026, 0.00780, -1.2829 0.0000, 0.00000, 0.1661 0.0037, -0.00840, 0.8026 0.0112, -0.01420, 1.0082 0.0191, -0.01930, 0.9853 0.0397, -0.03030, 0.8328 0.0706, -0.04420, 0.6293 0.1037, -0.05710, 0.4710 0.1384, -0.06890, 0.2546 0.1741, -0.07950, 0.1023 0.2102, -0.08660, -0.0413 0.2472, -0.09640, -0.2246 0.2844, -0.10270, -0.3534 0.3225, -0.10690, -0.5008 0.3608, -0.10890, -0.6052 0.3991, -0.10830, -0.6824 0.4373, -0.10510, -0.7022 0.4757, -0.09890, -0.6234 0.5137, -0.09070, -0.5615 0.5694, -0.07640, -0.4004 14 Flap element taps 1.0000, 0.00130, -0.1956 0.9365, 0.01390, 0.0046 0.8333, 0.03280, 0.1026 0.7436, 0.04930, 0.0521 0.7049, 0.05670, -0.0025 0.6662, 0.06410, -0.0506 0.6522, 0.01390, -0.2646 0.5969, -0.00020, -0.2775 0.6000, -0.03020, -0.2914 0.6324, -0.04540, -0.2774 0.6667, -0.04880, -0.2314 0.7046, -0.04110, -0.2143 0.7429, -0.03210, -0.2131 0.9311, -0.00120, -0.2615 --------- Run Conditions: vel=209.3 ft/s Re=1.997x10^6 AOA=15.06 Flap deflection=-20.00 Totals: Cl=0.4940 Cdp=0.0761 Cm(c/4)=0.0943 Cs=0.0548 Ch=0.0537 Main component: Cl=0.5291 Cdp=0.0938 Cm=-0.0632 Flap component: Cl=-0.0351 Cdp=-0.0176 Cm=0.0333 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3058 0.6175, -0.04610, -0.3282 0.5841, -0.02440, -0.3236 0.5775, 0.01750, -0.3253 0.5777, 0.04660, -0.3253 0.6274, 0.07170, -0.2053 0.5694, 0.08320, -0.2103 0.5112, 0.09370, -0.2178 0.4731, 0.09830, -0.2730 0.4349, 0.10070, -0.4076 0.3960, 0.10120, -0.5355 0.3566, 0.10020, -0.6545 0.3172, 0.09790, -0.7485 0.2778, 0.09440, -0.8613 0.2393, 0.08960, -0.9767 0.2056, 0.08360, -1.0919 0.1633, 0.07610, -1.2027 0.1261, 0.06710, -1.3152 0.0900, 0.05640, -1.6438 0.0571, 0.04390, -1.7671 0.0283, 0.02940, -2.1432 0.0142, 0.01970, -2.5491 0.0081, 0.01410, -2.8630 0.0026, 0.00780, -2.6699 0.0000, 0.00000, -0.1499 0.0037, -0.00840, 0.2583 0.0112, -0.01420, 0.8924 0.0191, -0.01930, 1.0037 0.0397, -0.03030, 0.9673 0.0706, -0.04420, 0.8074 0.1037, -0.05710, 0.6534 0.1384, -0.06890, 0.4714 0.1741, -0.07950, 0.3134 0.2102, -0.08660, 0.1521 0.2472, -0.09640, -0.0211 0.2844, -0.10270, -0.1564 0.3225, -0.10690, -0.2928 0.3608, -0.10890, -0.4184 0.3991, -0.10830, -0.5079 0.4373, -0.10510, -0.5531 0.4757, -0.09890, -0.5076 0.5137, -0.09070, -0.4704 0.5694, -0.07640, -0.3410 14 Flap element taps 1.0000, 0.00130, -0.1339 0.9365, 0.01390, 0.0271 0.8333, 0.03280, -0.0123 0.7436, 0.04930, -0.1448 0.7049, 0.05670, -0.1819 0.6662, 0.06410, -0.2079 0.6522, 0.01390, -0.3227 0.5969, -0.00020, -0.3248 0.6000, -0.03020, -0.3351 0.6324, -0.04540, -0.3303 0.6667, -0.04880, -0.2203 0.7046, -0.04110, -0.1609 0.7429, -0.03210, -0.1603 0.9311, -0.00120, -0.1885 --------- Run Conditions: vel=209.3 ft/s Re=1.993x10^6 AOA=18.03 Flap deflection=-20.00 Totals: Cl=0.4517 Cdp=0.1159 Cm(c/4)=0.1004 Cs=0.0296 Ch=0.0529 Main component: Cl=0.4896 Cdp=0.1470 Cm=-0.0532 Flap component: Cl=-0.0379 Cdp=-0.0311 Cm=0.0373 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4785 0.6175, -0.04610, -0.5761 0.5841, -0.02440, -0.5674 0.5775, 0.01750, -0.5684 0.5777, 0.04660, -0.5679 0.6274, 0.07170, -0.3374 0.5694, 0.08320, -0.3442 0.5112, 0.09370, -0.3427 0.4731, 0.09830, -0.3470 0.4349, 0.10070, -0.3740 0.3960, 0.10120, -0.4153 0.3566, 0.10020, -0.4894 0.3172, 0.09790, -0.5760 0.2778, 0.09440, -0.6975 0.2393, 0.08960, -0.8316 0.2056, 0.08360, -0.9708 0.1633, 0.07610, -1.1144 0.1261, 0.06710, -1.2623 0.0900, 0.05640, -1.6037 0.0571, 0.04390, -1.8126 0.0283, 0.02940, -2.2889 0.0142, 0.01970, -2.8041 0.0081, 0.01410, -3.2170 0.0026, 0.00780, -3.1460 0.0000, 0.00000, -0.1201 0.0037, -0.00840, 0.0108 0.0112, -0.01420, 0.8105 0.0191, -0.01930, 0.9802 0.0397, -0.03030, 0.9913 0.0706, -0.04420, 0.8542 0.1037, -0.05710, 0.7045 0.1384, -0.06890, 0.5230 0.1741, -0.07950, 0.3611 0.2102, -0.08660, 0.1952 0.2472, -0.09640, 0.0102 0.2844, -0.10270, -0.1420 0.3225, -0.10690, -0.2922 0.3608, -0.10890, -0.4349 0.3991, -0.10830, -0.5525 0.4373, -0.10510, -0.6129 0.4757, -0.09890, -0.5859 0.5137, -0.09070, -0.5695 0.5694, -0.07640, -0.4644 14 Flap element taps 1.0000, 0.00130, -0.0638 0.9365, 0.01390, -0.0419 0.8333, 0.03280, -0.1718 0.7436, 0.04930, -0.2727 0.7049, 0.05670, -0.3079 0.6662, 0.06410, -0.3356 0.6522, 0.01390, -0.5657 0.5969, -0.00020, -0.5732 0.6000, -0.03020, -0.5889 0.6324, -0.04540, -0.5830 0.6667, -0.04880, -0.5089 0.7046, -0.04110, -0.3556 0.7429, -0.03210, -0.3472 0.9311, -0.00120, -0.2209 --------- Run Conditions: vel=210.6 ft/s Re=2.002x10^6 AOA=20.02 Flap deflection=-20.00 Totals: Cl=0.3037 Cdp=0.1492 Cm(c/4)=0.0879 Cs=-0.0362 Ch=0.0342 Main component: Cl=0.3377 Cdp=0.1876 Cm=-0.0298 Flap component: Cl=-0.0341 Cdp=-0.0385 Cm=0.0336 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6413 0.6175, -0.04610, -0.7916 0.5841, -0.02440, -0.7813 0.5775, 0.01750, -0.7818 0.5777, 0.04660, -0.7814 0.6274, 0.07170, -0.4086 0.5694, 0.08320, -0.4366 0.5112, 0.09370, -0.4424 0.4731, 0.09830, -0.4296 0.4349, 0.10070, -0.4248 0.3960, 0.10120, -0.4193 0.3566, 0.10020, -0.4386 0.3172, 0.09790, -0.4522 0.2778, 0.09440, -0.4923 0.2393, 0.08960, -0.5500 0.2056, 0.08360, -0.6261 0.1633, 0.07610, -0.7310 0.1261, 0.06710, -0.8482 0.0900, 0.05640, -1.0889 0.0571, 0.04390, -1.3543 0.0283, 0.02940, -1.8712 0.0142, 0.01970, -2.3949 0.0081, 0.01410, -2.7983 0.0026, 0.00780, -2.7842 0.0000, 0.00000, -0.0793 0.0037, -0.00840, 0.0925 0.0112, -0.01420, 0.8307 0.0191, -0.01930, 0.9861 0.0397, -0.03030, 0.9904 0.0706, -0.04420, 0.8535 0.1037, -0.05710, 0.7037 0.1384, -0.06890, 0.5182 0.1741, -0.07950, 0.3532 0.2102, -0.08660, 0.1836 0.2472, -0.09640, -0.0111 0.2844, -0.10270, -0.1710 0.3225, -0.10690, -0.3357 0.3608, -0.10890, -0.4915 0.3991, -0.10830, -0.6239 0.4373, -0.10510, -0.6985 0.4757, -0.09890, -0.6828 0.5137, -0.09070, -0.6808 0.5694, -0.07640, -0.5933 14 Flap element taps 1.0000, 0.00130, -0.1780 0.9365, 0.01390, -0.2104 0.8333, 0.03280, -0.3233 0.7436, 0.04930, -0.3922 0.7049, 0.05670, -0.4089 0.6662, 0.06410, -0.4194 0.6522, 0.01390, -0.7800 0.5969, -0.00020, -0.7887 0.6000, -0.03020, -0.8161 0.6324, -0.04540, -0.8100 0.6667, -0.04880, -0.8268 0.7046, -0.04110, -0.5748 0.7429, -0.03210, -0.5273 0.9311, -0.00120, -0.2257 --------- Run Conditions: vel=211.5 ft/s Re=2.010x10^6 AOA=23.98 Flap deflection=-20.00 Totals: Cl=0.2489 Cdp=0.2329 Cm(c/4)=0.0475 Cs=-0.1116 Ch=-0.0151 Main component: Cl=0.2506 Cdp=0.2735 Cm=-0.0403 Flap component: Cl=-0.0017 Cdp=-0.0406 Cm=0.0072 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7740 0.6175, -0.04610, -0.9939 0.5841, -0.02440, -0.9797 0.5775, 0.01750, -0.9825 0.5777, 0.04660, -0.9819 0.6274, 0.07170, -0.5318 0.5694, 0.08320, -0.5637 0.5112, 0.09370, -0.5724 0.4731, 0.09830, -0.5761 0.4349, 0.10070, -0.5737 0.3960, 0.10120, -0.5611 0.3566, 0.10020, -0.5690 0.3172, 0.09790, -0.5708 0.2778, 0.09440, -0.5867 0.2393, 0.08960, -0.5936 0.2056, 0.08360, -0.6051 0.1633, 0.07610, -0.6278 0.1261, 0.06710, -0.6387 0.0900, 0.05640, -0.6587 0.0571, 0.04390, -0.7289 0.0283, 0.02940, -0.9183 0.0142, 0.01970, -1.2338 0.0081, 0.01410, -1.5207 0.0026, 0.00780, -1.6941 0.0000, 0.00000, -0.0520 0.0037, -0.00840, 0.2118 0.0112, -0.01420, 0.8394 0.0191, -0.01930, 0.9829 0.0397, -0.03030, 0.9963 0.0706, -0.04420, 0.8789 0.1037, -0.05710, 0.7408 0.1384, -0.06890, 0.5634 0.1741, -0.07950, 0.4026 0.2102, -0.08660, 0.2355 0.2472, -0.09640, 0.0371 0.2844, -0.10270, -0.1314 0.3225, -0.10690, -0.3090 0.3608, -0.10890, -0.4760 0.3991, -0.10830, -0.6329 0.4373, -0.10510, -0.7241 0.4757, -0.09890, -0.7270 0.5137, -0.09070, -0.7430 0.5694, -0.07640, -0.6771 14 Flap element taps 1.0000, 0.00130, -0.4296 0.9365, 0.01390, -0.4743 0.8333, 0.03280, -0.5522 0.7436, 0.04930, -0.5680 0.7049, 0.05670, -0.5554 0.6662, 0.06410, -0.5402 0.6522, 0.01390, -0.9793 0.5969, -0.00020, -0.9905 0.6000, -0.03020, -1.0272 0.6324, -0.04540, -1.0237 0.6667, -0.04880, -1.1691 0.7046, -0.04110, -0.7838 0.7429, -0.03210, -0.6343 0.9311, -0.00120, -0.2480 --------- Run Conditions: vel=212.8 ft/s Re=2.017x10^6 AOA=26.99 Flap deflection=-20.00 Totals: Cl=0.3858 Cdp=0.3130 Cm(c/4)=0.0237 Cs=-0.1038 Ch=-0.0487 Main component: Cl=0.3561 Cdp=0.3503 Cm=-0.0810 Flap component: Cl=0.0296 Cdp=-0.0373 Cm=-0.0167 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7721 0.6175, -0.04610, -1.0413 0.5841, -0.02440, -1.0246 0.5775, 0.01750, -1.0246 0.5777, 0.04660, -1.0239 0.6274, 0.07170, -0.6476 0.5694, 0.08320, -0.6787 0.5112, 0.09370, -0.6964 0.4731, 0.09830, -0.7141 0.4349, 0.10070, -0.7245 0.3960, 0.10120, -0.7190 0.3566, 0.10020, -0.7409 0.3172, 0.09790, -0.7499 0.2778, 0.09440, -0.7804 0.2393, 0.08960, -0.8079 0.2056, 0.08360, -0.8309 0.1633, 0.07610, -0.8701 0.1261, 0.06710, -0.8923 0.0900, 0.05640, -0.9043 0.0571, 0.04390, -0.9533 0.0283, 0.02940, -1.0090 0.0142, 0.01970, -1.1414 0.0081, 0.01410, -1.2622 0.0026, 0.00780, -1.2988 0.0000, 0.00000, -0.0155 0.0037, -0.00840, 0.0848 0.0112, -0.01420, 0.7686 0.0191, -0.01930, 0.9507 0.0397, -0.03030, 1.0121 0.0706, -0.04420, 0.9299 0.1037, -0.05710, 0.8090 0.1384, -0.06890, 0.6449 0.1741, -0.07950, 0.4922 0.2102, -0.08660, 0.3321 0.2472, -0.09640, 0.1364 0.2844, -0.10270, -0.0337 0.3225, -0.10690, -0.2243 0.3608, -0.10890, -0.3976 0.3991, -0.10830, -0.5632 0.4373, -0.10510, -0.6659 0.4757, -0.09890, -0.6840 0.5137, -0.09070, -0.7185 0.5694, -0.07640, -0.6559 14 Flap element taps 1.0000, 0.00130, -0.5181 0.9365, 0.01390, -0.5871 0.8333, 0.03280, -0.6413 0.7436, 0.04930, -0.6640 0.7049, 0.05670, -0.6533 0.6662, 0.06410, -0.6471 0.6522, 0.01390, -1.0234 0.5969, -0.00020, -1.0362 0.6000, -0.03020, -1.0707 0.6324, -0.04540, -1.0647 0.6667, -0.04880, -1.2682 0.7046, -0.04110, -0.8329 0.7429, -0.03210, -0.6013 0.9311, -0.00120, -0.2476