S809 UNVENTED AILERON, LEGR, CHORD = 18 INCHES --------- Run Conditions: vel=111.2 ft/s Re=1.004x10^6 AOA=-5.98 Flap deflection=-60.00 Totals: Cl=-1.6310 Cdp=0.3753 Cm(c/4)=0.2023 Cs=-0.2033 Ch=0.4129 Main component: Cl=-1.4190 Cdp=-0.0039 Cm=0.3676 Flap component: Cl=-0.2120 Cdp=0.3792 Cm=0.2500 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7807 0.6175, -0.04610, -0.7427 0.5841, -0.02440, -0.7464 0.5775, 0.01750, -0.7514 0.5777, 0.04660, -0.7478 0.6274, 0.07170, 0.7838 0.5694, 0.08320, 0.7929 0.5112, 0.09370, 0.7186 0.4731, 0.09830, 0.6612 0.4349, 0.10070, 0.6245 0.3960, 0.10120, 0.5492 0.3566, 0.10020, 0.6104 0.3172, 0.09790, 0.5995 0.2778, 0.09440, 0.6053 0.2393, 0.08960, 0.6313 0.2056, 0.08360, 0.6056 0.1633, 0.07610, 0.7465 0.1261, 0.06710, 0.7898 0.0900, 0.05640, 0.9239 0.0571, 0.04390, 0.9944 0.0283, 0.02940, 0.9606 0.0142, 0.01970, 0.6077 0.0081, 0.01410, 0.0683 0.0026, 0.00780, -1.1477 0.0000, 0.00000, -5.8961 0.0037, -0.00840, -6.4300 0.0112, -0.01420, -4.3004 0.0191, -0.01930, -3.4339 0.0397, -0.03030, -2.5672 0.0706, -0.04420, -2.1519 0.1037, -0.05710, -1.9201 0.1384, -0.06890, -1.8175 0.1741, -0.07950, -1.7803 0.2102, -0.08660, -1.8396 0.2472, -0.09640, -1.8195 0.2844, -0.10270, -1.8069 0.3225, -0.10690, -1.6824 0.3608, -0.10890, -1.6024 0.3991, -0.10830, -1.3667 0.4373, -0.10510, -1.1230 0.4757, -0.09890, -0.9103 0.5137, -0.09070, -0.8379 0.5694, -0.07640, -0.7818 15 Flap element taps 1.0000, 0.00130, -0.7526 0.9365, 0.01390, 0.2917 0.8333, 0.03280, 0.6695 0.7436, 0.04930, 0.8191 0.7049, 0.05670, 0.8237 0.6662, 0.06410, 0.7813 0.6522, 0.01390, -0.7567 0.5969, -0.00020, -0.7619 0.6000, -0.03020, -0.7656 0.6324, -0.04540, -0.7845 0.6667, -0.04880, -0.7795 0.7046, -0.04110, -0.7637 0.7429, -0.03210, -0.7774 0.8333, -0.01400, -0.7758 0.9311, -0.00120, -0.7528 --------- Run Conditions: vel=110.3 ft/s Re=0.996x10^6 AOA=-0.02 Flap deflection=-60.00 Totals: Cl=-1.5591 Cdp=0.2980 Cm(c/4)=0.2314 Cs=-0.2975 Ch=0.3841 Main component: Cl=-1.3240 Cdp=-0.0373 Cm=0.3869 Flap component: Cl=-0.2351 Cdp=0.3353 Cm=0.2344 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7473 0.6175, -0.04610, -0.6728 0.5841, -0.02440, -0.6815 0.5775, 0.01750, -0.6841 0.5777, 0.04660, -0.6815 0.6274, 0.07170, 0.8001 0.5694, 0.08320, 0.8248 0.5112, 0.09370, 0.7116 0.4731, 0.09830, 0.6341 0.4349, 0.10070, 0.5146 0.3960, 0.10120, 0.3867 0.3566, 0.10020, 0.4914 0.3172, 0.09790, 0.4699 0.2778, 0.09440, 0.4633 0.2393, 0.08960, 0.4705 0.2056, 0.08360, 0.3948 0.1633, 0.07610, 0.5747 0.1261, 0.06710, 0.5915 0.0900, 0.05640, 0.7491 0.0571, 0.04390, 0.8643 0.0283, 0.02940, 1.0114 0.0142, 0.01970, 0.9564 0.0081, 0.01410, 0.7080 0.0026, 0.00780, 0.0630 0.0000, 0.00000, -2.4417 0.0037, -0.00840, -3.6333 0.0112, -0.01420, -2.5912 0.0191, -0.01930, -2.0201 0.0397, -0.03030, -1.6097 0.0706, -0.04420, -1.5221 0.1037, -0.05710, -1.4250 0.1384, -0.06890, -1.4306 0.1741, -0.07950, -1.4966 0.2102, -0.08660, -1.6868 0.2472, -0.09640, -1.7482 0.2844, -0.10270, -1.8516 0.3225, -0.10690, -1.8134 0.3608, -0.10890, -1.9017 0.3991, -0.10830, -1.8061 0.4373, -0.10510, -1.7149 0.4757, -0.09890, -1.4838 0.5137, -0.09070, -1.2691 0.5694, -0.07640, -0.9116 15 Flap element taps 1.0000, 0.00130, -0.6876 0.9365, 0.01390, 0.2597 0.8333, 0.03280, 0.6323 0.7436, 0.04930, 0.8200 0.7049, 0.05670, 0.8483 0.6662, 0.06410, 0.7844 0.6522, 0.01390, -0.6993 0.5969, -0.00020, -0.6934 0.6000, -0.03020, -0.6954 0.6324, -0.04540, -0.7185 0.6667, -0.04880, -0.7179 0.7046, -0.04110, -0.6963 0.7429, -0.03210, -0.7189 0.8333, -0.01400, -0.7212 0.9311, -0.00120, -0.6808 --------- Run Conditions: vel=110.7 ft/s Re=1.001x10^6 AOA=2.97 Flap deflection=-60.00 Totals: Cl=-1.5146 Cdp=0.2858 Cm(c/4)=0.2535 Cs=-0.3639 Ch=0.4034 Main component: Cl=-1.2514 Cdp=-0.0485 Cm=0.3830 Flap component: Cl=-0.2632 Cdp=0.3343 Cm=0.2449 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8456 0.6175, -0.04610, -0.7409 0.5841, -0.02440, -0.7531 0.5775, 0.01750, -0.7517 0.5777, 0.04660, -0.7507 0.6274, 0.07170, 0.7230 0.5694, 0.08320, 0.7682 0.5112, 0.09370, 0.6992 0.4731, 0.09830, 0.6352 0.4349, 0.10070, 0.5217 0.3960, 0.10120, 0.3244 0.3566, 0.10020, 0.4545 0.3172, 0.09790, 0.4225 0.2778, 0.09440, 0.4093 0.2393, 0.08960, 0.4040 0.2056, 0.08360, 0.2921 0.1633, 0.07610, 0.5011 0.1261, 0.06710, 0.4921 0.0900, 0.05640, 0.6568 0.0571, 0.04390, 0.7706 0.0283, 0.02940, 0.9687 0.0142, 0.01970, 0.9971 0.0081, 0.01410, 0.8262 0.0026, 0.00780, 0.4074 0.0000, 0.00000, -1.3035 0.0037, -0.00840, -2.5813 0.0112, -0.01420, -1.9180 0.0191, -0.01930, -1.4902 0.0397, -0.03030, -1.2373 0.0706, -0.04420, -1.2651 0.1037, -0.05710, -1.2189 0.1384, -0.06890, -1.2386 0.1741, -0.07950, -1.3417 0.2102, -0.08660, -1.5894 0.2472, -0.09640, -1.6638 0.2844, -0.10270, -1.8087 0.3225, -0.10690, -1.7777 0.3608, -0.10890, -1.9144 0.3991, -0.10830, -1.8367 0.4373, -0.10510, -1.7981 0.4757, -0.09890, -1.5937 0.5137, -0.09070, -1.4087 0.5694, -0.07640, -1.0324 15 Flap element taps 1.0000, 0.00130, -0.7505 0.9365, 0.01390, 0.2464 0.8333, 0.03280, 0.6289 0.7436, 0.04930, 0.7997 0.7049, 0.05670, 0.7669 0.6662, 0.06410, 0.7138 0.6522, 0.01390, -0.7847 0.5969, -0.00020, -0.7583 0.6000, -0.03020, -0.7669 0.6324, -0.04540, -0.7970 0.6667, -0.04880, -0.7981 0.7046, -0.04110, -0.7706 0.7429, -0.03210, -0.7982 0.8333, -0.01400, -0.8033 0.9311, -0.00120, -0.7480 --------- Run Conditions: vel=110.6 ft/s Re=1.000x10^6 AOA=7.61 Flap deflection=-60.00 Totals: Cl=-1.3186 Cdp=0.2239 Cm(c/4)=0.2538 Cs=-0.3965 Ch=0.3852 Main component: Cl=-1.0463 Cdp=-0.0682 Cm=0.3417 Flap component: Cl=-0.2724 Cdp=0.2921 Cm=0.2314 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8388 0.6175, -0.04610, -0.7368 0.5841, -0.02440, -0.7510 0.5775, 0.01750, -0.7491 0.5777, 0.04660, -0.7507 0.6274, 0.07170, 0.6404 0.5694, 0.08320, 0.6948 0.5112, 0.09370, 0.6420 0.4731, 0.09830, 0.6457 0.4349, 0.10070, 0.5307 0.3960, 0.10120, 0.2737 0.3566, 0.10020, 0.4029 0.3172, 0.09790, 0.3509 0.2778, 0.09440, 0.3238 0.2393, 0.08960, 0.2919 0.2056, 0.08360, 0.1394 0.1633, 0.07610, 0.3608 0.1261, 0.06710, 0.3209 0.0900, 0.05640, 0.4747 0.0571, 0.04390, 0.5736 0.0283, 0.02940, 0.8147 0.0142, 0.01970, 0.9421 0.0081, 0.01410, 0.8675 0.0026, 0.00780, 0.7732 0.0000, 0.00000, 0.0788 0.0037, -0.00840, -1.1203 0.0112, -0.01420, -0.9303 0.0191, -0.01930, -0.7204 0.0397, -0.03030, -0.6691 0.0706, -0.04420, -0.8223 0.1037, -0.05710, -0.8534 0.1384, -0.06890, -0.8828 0.1741, -0.07950, -1.0243 0.2102, -0.08660, -1.3200 0.2472, -0.09640, -1.4013 0.2844, -0.10270, -1.5807 0.3225, -0.10690, -1.5582 0.3608, -0.10890, -1.7326 0.3991, -0.10830, -1.6774 0.4373, -0.10510, -1.6848 0.4757, -0.09890, -1.5151 0.5137, -0.09070, -1.3640 0.5694, -0.07640, -1.0063 15 Flap element taps 1.0000, 0.00130, -0.7469 0.9365, 0.01390, 0.2353 0.8333, 0.03280, 0.6008 0.7436, 0.04930, 0.6258 0.7049, 0.05670, 0.6187 0.6662, 0.06410, 0.6097 0.6522, 0.01390, -0.7888 0.5969, -0.00020, -0.7556 0.6000, -0.03020, -0.7612 0.6324, -0.04540, -0.7920 0.6667, -0.04880, -0.7957 0.7046, -0.04110, -0.7608 0.7429, -0.03210, -0.7930 0.8333, -0.01400, -0.8008 0.9311, -0.00120, -0.7304 --------- Run Conditions: vel=111.2 ft/s Re=1.006x10^6 AOA=9.01 Flap deflection=-60.00 Totals: Cl=-1.0893 Cdp=0.2504 Cm(c/4)=0.2554 Cs=-0.4179 Ch=0.3744 Main component: Cl=-0.8202 Cdp=-0.0225 Cm=0.2911 Flap component: Cl=-0.2690 Cdp=0.2729 Cm=0.2235 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8128 0.6175, -0.04610, -0.7267 0.5841, -0.02440, -0.7434 0.5775, 0.01750, -0.7422 0.5777, 0.04660, -0.7454 0.6274, 0.07170, 0.5631 0.5694, 0.08320, 0.6199 0.5112, 0.09370, 0.5671 0.4731, 0.09830, 0.5808 0.4349, 0.10070, 0.4965 0.3960, 0.10120, 0.2117 0.3566, 0.10020, 0.3373 0.3172, 0.09790, 0.2644 0.2778, 0.09440, 0.2220 0.2393, 0.08960, 0.1696 0.2056, 0.08360, -0.0211 0.1633, 0.07610, 0.1982 0.1261, 0.06710, 0.1221 0.0900, 0.05640, 0.2433 0.0571, 0.04390, 0.3051 0.0283, 0.02940, 0.5352 0.0142, 0.01970, 0.6894 0.0081, 0.01410, 0.6988 0.0026, 0.00780, 0.9160 0.0000, 0.00000, 0.8883 0.0037, -0.00840, 0.0261 0.0112, -0.01420, -0.1285 0.0191, -0.01930, -0.0504 0.0397, -0.03030, -0.1517 0.0706, -0.04420, -0.3978 0.1037, -0.05710, -0.4999 0.1384, -0.06890, -0.5323 0.1741, -0.07950, -0.7013 0.2102, -0.08660, -1.0341 0.2472, -0.09640, -1.1222 0.2844, -0.10270, -1.3297 0.3225, -0.10690, -1.3144 0.3608, -0.10890, -1.5188 0.3991, -0.10830, -1.4829 0.4373, -0.10510, -1.5318 0.4757, -0.09890, -1.3941 0.5137, -0.09070, -1.2809 0.5694, -0.07640, -0.9512 15 Flap element taps 1.0000, 0.00130, -0.7409 0.9365, 0.01390, 0.2293 0.8333, 0.03280, 0.5856 0.7436, 0.04930, 0.5472 0.7049, 0.05670, 0.5340 0.6662, 0.06410, 0.5289 0.6522, 0.01390, -0.7842 0.5969, -0.00020, -0.7482 0.6000, -0.03020, -0.7511 0.6324, -0.04540, -0.7809 0.6667, -0.04880, -0.7837 0.7046, -0.04110, -0.7433 0.7429, -0.03210, -0.7811 0.8333, -0.01400, -0.7911 0.9311, -0.00120, -0.7205 --------- Run Conditions: vel=111.6 ft/s Re=1.011x10^6 AOA=11.99 Flap deflection=-60.00 Totals: Cl=-0.8729 Cdp=0.2437 Cm(c/4)=0.2559 Cs=-0.4197 Ch=0.3636 Main component: Cl=-0.6003 Cdp=-0.0042 Cm=0.2408 Flap component: Cl=-0.2726 Cdp=0.2478 Cm=0.2159 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7918 0.6175, -0.04610, -0.7343 0.5841, -0.02440, -0.7519 0.5775, 0.01750, -0.7521 0.5777, 0.04660, -0.7534 0.6274, 0.07170, 0.4745 0.5694, 0.08320, 0.5331 0.5112, 0.09370, 0.4801 0.4731, 0.09830, 0.5007 0.4349, 0.10070, 0.4473 0.3960, 0.10120, 0.1635 0.3566, 0.10020, 0.2793 0.3172, 0.09790, 0.1830 0.2778, 0.09440, 0.1208 0.2393, 0.08960, 0.0430 0.2056, 0.08360, -0.1853 0.1633, 0.07610, 0.0227 0.1261, 0.06710, -0.0937 0.0900, 0.05640, -0.0041 0.0571, 0.04390, -0.0124 0.0283, 0.02940, 0.1522 0.0142, 0.01970, 0.2492 0.0081, 0.01410, 0.2782 0.0026, 0.00780, 0.6539 0.0000, 0.00000, 1.0455 0.0037, -0.00840, 0.7456 0.0112, -0.01420, 0.4566 0.0191, -0.01930, 0.4161 0.0397, -0.03030, 0.2606 0.0706, -0.04420, -0.0392 0.1037, -0.05710, -0.1992 0.1384, -0.06890, -0.2202 0.1741, -0.07950, -0.4118 0.2102, -0.08660, -0.7696 0.2472, -0.09640, -0.8606 0.2844, -0.10270, -1.0913 0.3225, -0.10690, -1.0823 0.3608, -0.10890, -1.3134 0.3991, -0.10830, -1.2956 0.4373, -0.10510, -1.3796 0.4757, -0.09890, -1.2732 0.5137, -0.09070, -1.1965 0.5694, -0.07640, -0.8942 15 Flap element taps 1.0000, 0.00130, -0.7376 0.9365, 0.01390, 0.2160 0.8333, 0.03280, 0.5397 0.7436, 0.04930, 0.4519 0.7049, 0.05670, 0.4422 0.6662, 0.06410, 0.4396 0.6522, 0.01390, -0.7956 0.5969, -0.00020, -0.7549 0.6000, -0.03020, -0.7605 0.6324, -0.04540, -0.7924 0.6667, -0.04880, -0.7972 0.7046, -0.04110, -0.7512 0.7429, -0.03210, -0.7922 0.8333, -0.01400, -0.8034 0.9311, -0.00120, -0.7217 --------- Run Conditions: vel=110.1 ft/s Re=1.001x10^6 AOA=14.97 Flap deflection=-60.00 Totals: Cl=-0.6485 Cdp=0.2279 Cm(c/4)=0.2487 Cs=-0.3877 Ch=0.3437 Main component: Cl=-0.3853 Cdp=0.0137 Cm=0.1898 Flap component: Cl=-0.2632 Cdp=0.2142 Cm=0.2008 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7725 0.6175, -0.04610, -0.7518 0.5841, -0.02440, -0.7497 0.5775, 0.01750, -0.7562 0.5777, 0.04660, -0.7558 0.6274, 0.07170, 0.3652 0.5694, 0.08320, 0.3609 0.5112, 0.09370, 0.3676 0.4731, 0.09830, 0.3821 0.4349, 0.10070, 0.3706 0.3960, 0.10120, 0.3224 0.3566, 0.10020, 0.2261 0.3172, 0.09790, 0.1146 0.2778, 0.09440, 0.0044 0.2393, 0.08960, -0.0817 0.2056, 0.08360, -0.1708 0.1633, 0.07610, -0.2295 0.1261, 0.06710, -0.2878 0.0900, 0.05640, -0.3304 0.0571, 0.04390, -0.4044 0.0283, 0.02940, -0.3753 0.0142, 0.01970, -0.3983 0.0081, 0.01410, -0.2647 0.0026, 0.00780, -0.0030 0.0000, 0.00000, 0.5367 0.0037, -0.00840, 0.9874 0.0112, -0.01420, 0.8800 0.0191, -0.01930, 0.7590 0.0397, -0.03030, 0.5508 0.0706, -0.04420, 0.3104 0.1037, -0.05710, 0.1362 0.1384, -0.06890, -0.0741 0.1741, -0.07950, -0.2512 0.2102, -0.08660, -0.4411 0.2472, -0.09640, -0.6316 0.2844, -0.10270, -0.7944 0.3225, -0.10690, -0.9354 0.3608, -0.10890, -1.0819 0.3991, -0.10830, -1.1767 0.4373, -0.10510, -1.1911 0.4757, -0.09890, -1.1148 0.5137, -0.09070, -1.0352 0.5694, -0.07640, -0.8526 15 Flap element taps 1.0000, 0.00130, -0.7455 0.9365, 0.01390, 0.2105 0.8333, 0.03280, 0.4756 0.7436, 0.04930, 0.3445 0.7049, 0.05670, 0.3421 0.6662, 0.06410, 0.3566 0.6522, 0.01390, -0.7484 0.5969, -0.00020, -0.7628 0.6000, -0.03020, -0.7512 0.6324, -0.04540, -0.7431 0.6667, -0.04880, -0.7374 0.7046, -0.04110, -0.7386 0.7429, -0.03210, -0.7390 0.8333, -0.01400, -0.7512 0.9311, -0.00120, -0.7445 --------- Run Conditions: vel=110.9 ft/s Re=1.009x10^6 AOA=17.99 Flap deflection=-60.00 Totals: Cl=-0.3798 Cdp=0.2142 Cm(c/4)=0.2316 Cs=-0.3210 Ch=0.3120 Main component: Cl=-0.1382 Cdp=0.0414 Cm=0.1264 Flap component: Cl=-0.2416 Cdp=0.1728 Cm=0.1789 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7014 0.6175, -0.04610, -0.7244 0.5841, -0.02440, -0.7239 0.5775, 0.01750, -0.7318 0.5777, 0.04660, -0.7300 0.6274, 0.07170, 0.1996 0.5694, 0.08320, 0.1882 0.5112, 0.09370, 0.1927 0.4731, 0.09830, 0.2137 0.4349, 0.10070, 0.2079 0.3960, 0.10120, 0.1836 0.3566, 0.10020, 0.1630 0.3172, 0.09790, 0.0741 0.2778, 0.09440, -0.0586 0.2393, 0.08960, -0.1833 0.2056, 0.08360, -0.3208 0.1633, 0.07610, -0.4188 0.1261, 0.06710, -0.5358 0.0900, 0.05640, -0.6431 0.0571, 0.04390, -0.8412 0.0283, 0.02940, -0.9783 0.0142, 0.01970, -1.2374 0.0081, 0.01410, -1.2094 0.0026, 0.00780, -0.8914 0.0000, 0.00000, -0.7423 0.0037, -0.00840, 0.8365 0.0112, -0.01420, 1.0046 0.0191, -0.01930, 0.9620 0.0397, -0.03030, 0.8001 0.0706, -0.04420, 0.5782 0.1037, -0.05710, 0.4012 0.1384, -0.06890, 0.2007 0.1741, -0.07950, 0.0195 0.2102, -0.08660, -0.1796 0.2472, -0.09640, -0.3693 0.2844, -0.10270, -0.5491 0.3225, -0.10690, -0.7003 0.3608, -0.10890, -0.8616 0.3991, -0.10830, -0.9788 0.4373, -0.10510, -1.0141 0.4757, -0.09890, -0.9586 0.5137, -0.09070, -0.9060 0.5694, -0.07640, -0.7416 15 Flap element taps 1.0000, 0.00130, -0.7017 0.9365, 0.01390, 0.2286 0.8333, 0.03280, 0.3763 0.7436, 0.04930, 0.1839 0.7049, 0.05670, 0.1710 0.6662, 0.06410, 0.1954 0.6522, 0.01390, -0.7237 0.5969, -0.00020, -0.7327 0.6000, -0.03020, -0.7196 0.6324, -0.04540, -0.7019 0.6667, -0.04880, -0.6979 0.7046, -0.04110, -0.6963 0.7429, -0.03210, -0.6992 0.8333, -0.01400, -0.7141 0.9311, -0.00120, -0.7007 --------- Run Conditions: vel=110.3 ft/s Re=1.005x10^6 AOA=19.97 Flap deflection=-60.00 Totals: Cl=-0.1488 Cdp=0.2023 Cm(c/4)=0.2010 Cs=-0.2410 Ch=0.2659 Main component: Cl=0.0513 Cdp=0.0742 Cm=0.0710 Flap component: Cl=-0.2001 Cdp=0.1282 Cm=0.1477 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6396 0.6175, -0.04610, -0.7012 0.5841, -0.02440, -0.7023 0.5775, 0.01750, -0.7106 0.5777, 0.04660, -0.7087 0.6274, 0.07170, 0.0000 0.5694, 0.08320, -0.0298 0.5112, 0.09370, -0.0152 0.4731, 0.09830, 0.0133 0.4349, 0.10070, 0.0122 0.3960, 0.10120, -0.0099 0.3566, 0.10020, 0.0076 0.3172, 0.09790, -0.0127 0.2778, 0.09440, -0.0777 0.2393, 0.08960, -0.1964 0.2056, 0.08360, -0.3762 0.1633, 0.07610, -0.5125 0.1261, 0.06710, -0.6889 0.0900, 0.05640, -0.8493 0.0571, 0.04390, -1.1492 0.0283, 0.02940, -1.4423 0.0142, 0.01970, -1.9097 0.0081, 0.01410, -2.0084 0.0026, 0.00780, -1.7320 0.0000, 0.00000, -2.1050 0.0037, -0.00840, 0.4739 0.0112, -0.01420, 0.9633 0.0191, -0.01930, 0.9996 0.0397, -0.03030, 0.9166 0.0706, -0.04420, 0.7302 0.1037, -0.05710, 0.5621 0.1384, -0.06890, 0.3755 0.1741, -0.07950, 0.2022 0.2102, -0.08660, -0.0033 0.2472, -0.09640, -0.1852 0.2844, -0.10270, -0.3698 0.3225, -0.10690, -0.5188 0.3608, -0.10890, -0.6886 0.3991, -0.10830, -0.8136 0.4373, -0.10510, -0.8699 0.4757, -0.09890, -0.8398 0.5137, -0.09070, -0.8468 0.5694, -0.07640, -0.6509 15 Flap element taps 1.0000, 0.00130, -0.6557 0.9365, 0.01390, 0.2429 0.8333, 0.03280, 0.2074 0.7436, 0.04930, -0.0347 0.7049, 0.05670, -0.0463 0.6662, 0.06410, 0.0053 0.6522, 0.01390, -0.7014 0.5969, -0.00020, -0.7082 0.6000, -0.03020, -0.6844 0.6324, -0.04540, -0.6514 0.6667, -0.04880, -0.6450 0.7046, -0.04110, -0.6409 0.7429, -0.03210, -0.6485 0.8333, -0.01400, -0.6672 0.9311, -0.00120, -0.6503 --------- Run Conditions: vel=110.3 ft/s Re=1.004x10^6 AOA=23.98 Flap deflection=-60.00 Totals: Cl=0.5119 Cdp=0.2180 Cm(c/4)=0.0123 Cs=0.0089 Ch=-0.0333 Main component: Cl=0.4578 Cdp=0.2852 Cm=-0.1022 Flap component: Cl=0.0541 Cdp=-0.0673 Cm=-0.0245 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6175 0.6175, -0.04610, -0.8540 0.5841, -0.02440, -0.8531 0.5775, 0.01750, -0.8621 0.5777, 0.04660, -0.8604 0.6274, 0.07170, -0.6470 0.5694, 0.08320, -0.7584 0.5112, 0.09370, -0.7977 0.4731, 0.09830, -0.8057 0.4349, 0.10070, -0.8119 0.3960, 0.10120, -0.8404 0.3566, 0.10020, -0.8059 0.3172, 0.09790, -0.8052 0.2778, 0.09440, -0.8237 0.2393, 0.08960, -0.8291 0.2056, 0.08360, -0.8789 0.1633, 0.07610, -0.8632 0.1261, 0.06710, -0.9023 0.0900, 0.05640, -0.8753 0.0571, 0.04390, -0.9514 0.0283, 0.02940, -1.1705 0.0142, 0.01970, -1.7247 0.0081, 0.01410, -2.1689 0.0026, 0.00780, -2.2523 0.0000, 0.00000, -3.7222 0.0037, -0.00840, -0.2635 0.0112, -0.01420, 0.7374 0.0191, -0.01930, 0.9200 0.0397, -0.03030, 0.9975 0.0706, -0.04420, 0.9098 0.1037, -0.05710, 0.7833 0.1384, -0.06890, 0.6424 0.1741, -0.07950, 0.4901 0.2102, -0.08660, 0.2912 0.2472, -0.09640, 0.1320 0.2844, -0.10270, -0.0516 0.3225, -0.10690, -0.1902 0.3608, -0.10890, -0.3703 0.3991, -0.10830, -0.5053 0.4373, -0.10510, -0.5966 0.4757, -0.09890, -0.6050 0.5137, -0.09070, -0.6565 0.5694, -0.07640, -0.5429 15 Flap element taps 1.0000, 0.00130, -0.5477 0.9365, 0.01390, -0.4086 0.8333, 0.03280, -0.6385 0.7436, 0.04930, -0.7383 0.7049, 0.05670, -0.7153 0.6662, 0.06410, -0.6475 0.6522, 0.01390, -0.8564 0.5969, -0.00020, -0.8599 0.6000, -0.03020, -0.5983 0.6324, -0.04540, -0.4340 0.6667, -0.04880, -0.4055 0.7046, -0.04110, -0.3942 0.7429, -0.03210, -0.4034 0.8333, -0.01400, -0.4220 0.9311, -0.00120, -0.4158 --------- Run Conditions: vel=109.4 ft/s Re=0.998x10^6 AOA=27.00 Flap deflection=-60.00 Totals: Cl=0.5294 Cdp=0.2758 Cm(c/4)=-0.0061 Cs=-0.0054 Ch=-0.0749 Main component: Cl=0.4430 Cdp=0.3624 Cm=-0.1121 Flap component: Cl=0.0864 Cdp=-0.0866 Cm=-0.0432 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7144 0.6175, -0.04610, -1.0369 0.5841, -0.02440, -1.0420 0.5775, 0.01750, -1.0519 0.5777, 0.04660, -1.0495 0.6274, 0.07170, -0.7311 0.5694, 0.08320, -0.7845 0.5112, 0.09370, -0.8334 0.4731, 0.09830, -0.8321 0.4349, 0.10070, -0.8461 0.3960, 0.10120, -0.8912 0.3566, 0.10020, -0.8582 0.3172, 0.09790, -0.8591 0.2778, 0.09440, -0.8622 0.2393, 0.08960, -0.8704 0.2056, 0.08360, -0.9299 0.1633, 0.07610, -0.9091 0.1261, 0.06710, -0.9676 0.0900, 0.05640, -0.9334 0.0571, 0.04390, -0.9881 0.0283, 0.02940, -1.0517 0.0142, 0.01970, -1.2041 0.0081, 0.01410, -1.4843 0.0026, 0.00780, -1.5420 0.0000, 0.00000, -2.9519 0.0037, -0.00840, -0.1994 0.0112, -0.01420, 0.7280 0.0191, -0.01930, 0.9080 0.0397, -0.03030, 1.0030 0.0706, -0.04420, 0.9346 0.1037, -0.05710, 0.8184 0.1384, -0.06890, 0.7005 0.1741, -0.07950, 0.5513 0.2102, -0.08660, 0.3434 0.2472, -0.09640, 0.1918 0.2844, -0.10270, 0.0001 0.3225, -0.10690, -0.1354 0.3608, -0.10890, -0.3298 0.3991, -0.10830, -0.4717 0.4373, -0.10510, -0.5847 0.4757, -0.09890, -0.6106 0.5137, -0.09070, -0.6832 0.5694, -0.07640, -0.5940 15 Flap element taps 1.0000, 0.00130, -0.7708 0.9365, 0.01390, -0.7075 0.8333, 0.03280, -0.7934 0.7436, 0.04930, -0.8044 0.7049, 0.05670, -0.7806 0.6662, 0.06410, -0.7472 0.6522, 0.01390, -1.0451 0.5969, -0.00020, -1.0490 0.6000, -0.03020, -0.7335 0.6324, -0.04540, -0.5161 0.6667, -0.04880, -0.4703 0.7046, -0.04110, -0.4514 0.7429, -0.03210, -0.4614 0.8333, -0.01400, -0.4838 0.9311, -0.00120, -0.4717