S809 UNVENTED AILERON, LEGR, CHORD = 18 INCHES --------- Run Conditions: vel=221.5 ft/s Re=1.997x10^6 AOA=-6.01 Flap deflection=-60.00 Totals: Cl=-1.6396 Cdp=0.3729 Cm(c/4)=0.2007 Cs=-0.1992 Ch=0.4085 Main component: Cl=-1.4292 Cdp=-0.0056 Cm=0.3699 Flap component: Cl=-0.2104 Cdp=0.3785 Cm=0.2482 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7670 0.6175, -0.04610, -0.7446 0.5841, -0.02440, -0.7403 0.5775, 0.01750, -0.7410 0.5777, 0.04660, -0.7404 0.6274, 0.07170, 0.8471 0.5694, 0.08320, 0.8437 0.5112, 0.09370, 0.7612 0.4731, 0.09830, 0.6621 0.4349, 0.10070, 0.6223 0.3960, 0.10120, 0.5980 0.3566, 0.10020, 0.5870 0.3172, 0.09790, 0.5954 0.2778, 0.09440, 0.6075 0.2393, 0.08960, 0.6334 0.2056, 0.08360, 0.6761 0.1633, 0.07610, 0.7383 0.1261, 0.06710, 0.8168 0.0900, 0.05640, 0.9074 0.0571, 0.04390, 0.9952 0.0283, 0.02940, 0.9617 0.0142, 0.01970, 0.6496 0.0081, 0.01410, 0.1790 0.0026, 0.00780, -1.0995 0.0000, 0.00000, -5.8992 0.0037, -0.00840, -6.4215 0.0112, -0.01420, -4.4106 0.0191, -0.01930, -3.4703 0.0397, -0.03030, -2.5937 0.0706, -0.04420, -2.1475 0.1037, -0.05710, -1.8937 0.1384, -0.06890, -1.8707 0.1741, -0.07950, -1.8174 0.2102, -0.08660, -1.8154 0.2472, -0.09640, -1.8362 0.2844, -0.10270, -1.7872 0.3225, -0.10690, -1.7122 0.3608, -0.10890, -1.5917 0.3991, -0.10830, -1.3706 0.4373, -0.10510, -1.0857 0.4757, -0.09890, -0.8725 0.5137, -0.09070, -0.8065 0.5694, -0.07640, -0.7876 15 Flap element taps 1.0000, 0.00130, -0.7432 0.9365, 0.01390, 0.2883 0.8333, 0.03280, 0.6648 0.7436, 0.04930, 0.8521 0.7049, 0.05670, 0.8938 0.6662, 0.06410, 0.8526 0.6522, 0.01390, -0.7410 0.5969, -0.00020, -0.7502 0.6000, -0.03020, -0.7499 0.6324, -0.04540, -0.7532 0.6667, -0.04880, -0.7545 0.7046, -0.04110, -0.7484 0.7429, -0.03210, -0.7488 0.8333, -0.01400, -0.7495 0.9311, -0.00120, -0.7410 --------- Run Conditions: vel=222.4 ft/s Re=1.998x10^6 AOA=-0.03 Flap deflection=-60.00 Totals: Cl=-1.5171 Cdp=0.2913 Cm(c/4)=0.2222 Cs=-0.2905 Ch=0.3781 Main component: Cl=-1.2900 Cdp=-0.0295 Cm=0.3742 Flap component: Cl=-0.2270 Cdp=0.3208 Cm=0.2273 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7382 0.6175, -0.04610, -0.6915 0.5841, -0.02440, -0.6870 0.5775, 0.01750, -0.6902 0.5777, 0.04660, -0.6894 0.6274, 0.07170, 0.7135 0.5694, 0.08320, 0.7217 0.5112, 0.09370, 0.7251 0.4731, 0.09830, 0.6899 0.4349, 0.10070, 0.5963 0.3960, 0.10120, 0.5312 0.3566, 0.10020, 0.4920 0.3172, 0.09790, 0.4798 0.2778, 0.09440, 0.4712 0.2393, 0.08960, 0.4725 0.2056, 0.08360, 0.4987 0.1633, 0.07610, 0.5485 0.1261, 0.06710, 0.6222 0.0900, 0.05640, 0.7085 0.0571, 0.04390, 0.8518 0.0283, 0.02940, 0.9983 0.0142, 0.01970, 0.9823 0.0081, 0.01410, 0.8369 0.0026, 0.00780, 0.0938 0.0000, 0.00000, -2.2882 0.0037, -0.00840, -3.4568 0.0112, -0.01420, -2.5577 0.0191, -0.01930, -1.9080 0.0397, -0.03030, -1.5545 0.0706, -0.04420, -1.4540 0.1037, -0.05710, -1.3279 0.1384, -0.06890, -1.4573 0.1741, -0.07950, -1.5060 0.2102, -0.08660, -1.5919 0.2472, -0.09640, -1.7143 0.2844, -0.10270, -1.7653 0.3225, -0.10690, -1.8057 0.3608, -0.10890, -1.8253 0.3991, -0.10830, -1.7592 0.4373, -0.10510, -1.6102 0.4757, -0.09890, -1.3474 0.5137, -0.09070, -1.1052 0.5694, -0.07640, -0.8400 15 Flap element taps 1.0000, 0.00130, -0.6901 0.9365, 0.01390, 0.2701 0.8333, 0.03280, 0.6530 0.7436, 0.04930, 0.7295 0.7049, 0.05670, 0.7138 0.6662, 0.06410, 0.7104 0.6522, 0.01390, -0.6893 0.5969, -0.00020, -0.6936 0.6000, -0.03020, -0.6908 0.6324, -0.04540, -0.6888 0.6667, -0.04880, -0.6880 0.7046, -0.04110, -0.6842 0.7429, -0.03210, -0.6887 0.8333, -0.01400, -0.6914 0.9311, -0.00120, -0.6869 --------- Run Conditions: vel=223.2 ft/s Re=1.998x10^6 AOA=3.01 Flap deflection=-60.00 Totals: Cl=-1.5039 Cdp=0.2831 Cm(c/4)=0.2495 Cs=-0.3616 Ch=0.3971 Main component: Cl=-1.2492 Cdp=-0.0385 Cm=0.3834 Flap component: Cl=-0.2547 Cdp=0.3215 Cm=0.2379 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8658 0.6175, -0.04610, -0.7744 0.5841, -0.02440, -0.7702 0.5775, 0.01750, -0.7707 0.5777, 0.04660, -0.7706 0.6274, 0.07170, 0.6748 0.5694, 0.08320, 0.6802 0.5112, 0.09370, 0.6880 0.4731, 0.09830, 0.6684 0.4349, 0.10070, 0.5792 0.3960, 0.10120, 0.5018 0.3566, 0.10020, 0.4497 0.3172, 0.09790, 0.4285 0.2778, 0.09440, 0.4124 0.2393, 0.08960, 0.4056 0.2056, 0.08360, 0.4210 0.1633, 0.07610, 0.4600 0.1261, 0.06710, 0.5258 0.0900, 0.05640, 0.6002 0.0571, 0.04390, 0.7504 0.0283, 0.02940, 0.9443 0.0142, 0.01970, 1.0126 0.0081, 0.01410, 0.9631 0.0026, 0.00780, 0.4517 0.0000, 0.00000, -1.1579 0.0037, -0.00840, -2.4067 0.0112, -0.01420, -1.8588 0.0191, -0.01930, -1.3908 0.0397, -0.03030, -1.1949 0.0706, -0.04420, -1.2005 0.1037, -0.05710, -1.1240 0.1384, -0.06890, -1.3038 0.1741, -0.07950, -1.3878 0.2102, -0.08660, -1.5073 0.2472, -0.09640, -1.6670 0.2844, -0.10270, -1.7518 0.3225, -0.10690, -1.8337 0.3608, -0.10890, -1.8965 0.3991, -0.10830, -1.8784 0.4373, -0.10510, -1.7820 0.4757, -0.09890, -1.5663 0.5137, -0.09070, -1.3572 0.5694, -0.07640, -1.0588 15 Flap element taps 1.0000, 0.00130, -0.7678 0.9365, 0.01390, 0.2483 0.8333, 0.03280, 0.6436 0.7436, 0.04930, 0.6902 0.7049, 0.05670, 0.6736 0.6662, 0.06410, 0.6741 0.6522, 0.01390, -0.7700 0.5969, -0.00020, -0.7741 0.6000, -0.03020, -0.7712 0.6324, -0.04540, -0.7671 0.6667, -0.04880, -0.7650 0.7046, -0.04110, -0.7640 0.7429, -0.03210, -0.7707 0.8333, -0.01400, -0.7756 0.9311, -0.00120, -0.7643 --------- Run Conditions: vel=222.5 ft/s Re=1.988x10^6 AOA=6.02 Flap deflection=-60.00 Totals: Cl=-1.3089 Cdp=0.2649 Cm(c/4)=0.2538 Cs=-0.4007 Ch=0.3855 Main component: Cl=-1.0471 Cdp=-0.0307 Cm=0.3424 Flap component: Cl=-0.2617 Cdp=0.2957 Cm=0.2299 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8626 0.6175, -0.04610, -0.7660 0.5841, -0.02440, -0.7653 0.5775, 0.01750, -0.7670 0.5777, 0.04660, -0.7662 0.6274, 0.07170, 0.6165 0.5694, 0.08320, 0.6219 0.5112, 0.09370, 0.6321 0.4731, 0.09830, 0.6265 0.4349, 0.10070, 0.5574 0.3960, 0.10120, 0.4595 0.3566, 0.10020, 0.3857 0.3172, 0.09790, 0.3477 0.2778, 0.09440, 0.3159 0.2393, 0.08960, 0.2922 0.2056, 0.08360, 0.2908 0.1633, 0.07610, 0.3125 0.1261, 0.06710, 0.3615 0.0900, 0.05640, 0.4197 0.0571, 0.04390, 0.5486 0.0283, 0.02940, 0.7762 0.0142, 0.01970, 0.9357 0.0081, 0.01410, 1.0032 0.0026, 0.00780, 0.7734 0.0000, 0.00000, 0.1546 0.0037, -0.00840, -0.9879 0.0112, -0.01420, -0.8621 0.0191, -0.01930, -0.6409 0.0397, -0.03030, -0.6406 0.0706, -0.04420, -0.7584 0.1037, -0.05710, -0.7494 0.1384, -0.06890, -0.9699 0.1741, -0.07950, -1.0864 0.2102, -0.08660, -1.2298 0.2472, -0.09640, -1.4111 0.2844, -0.10270, -1.5202 0.3225, -0.10690, -1.6296 0.3608, -0.10890, -1.7189 0.3991, -0.10830, -1.7330 0.4373, -0.10510, -1.6737 0.4757, -0.09890, -1.4963 0.5137, -0.09070, -1.3211 0.5694, -0.07640, -1.0379 15 Flap element taps 1.0000, 0.00130, -0.7542 0.9365, 0.01390, 0.2340 0.8333, 0.03280, 0.6277 0.7436, 0.04930, 0.6212 0.7049, 0.05670, 0.6069 0.6662, 0.06410, 0.6149 0.6522, 0.01390, -0.7616 0.5969, -0.00020, -0.7684 0.6000, -0.03020, -0.7632 0.6324, -0.04540, -0.7534 0.6667, -0.04880, -0.7515 0.7046, -0.04110, -0.7501 0.7429, -0.03210, -0.7558 0.8333, -0.01400, -0.7642 0.9311, -0.00120, -0.7548 --------- Run Conditions: vel=223.5 ft/s Re=1.994x10^6 AOA=9.03 Flap deflection=-60.00 Totals: Cl=-1.0972 Cdp=0.2554 Cm(c/4)=0.2566 Cs=-0.4244 Ch=0.3763 Main component: Cl=-0.8288 Cdp=-0.0165 Cm=0.2941 Flap component: Cl=-0.2684 Cdp=0.2718 Cm=0.2234 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8450 0.6175, -0.04610, -0.7706 0.5841, -0.02440, -0.7662 0.5775, 0.01750, -0.7705 0.5777, 0.04660, -0.7708 0.6274, 0.07170, 0.5494 0.5694, 0.08320, 0.5500 0.5112, 0.09370, 0.5594 0.4731, 0.09830, 0.5620 0.4349, 0.10070, 0.5271 0.3960, 0.10120, 0.4238 0.3566, 0.10020, 0.3230 0.3172, 0.09790, 0.2643 0.2778, 0.09440, 0.2135 0.2393, 0.08960, 0.1684 0.2056, 0.08360, 0.1464 0.1633, 0.07610, 0.1440 0.1261, 0.06710, 0.1691 0.0900, 0.05640, 0.2167 0.0571, 0.04390, 0.2811 0.0283, 0.02940, 0.4935 0.0142, 0.01970, 0.6666 0.0081, 0.01410, 0.8313 0.0026, 0.00780, 0.9020 0.0000, 0.00000, 0.8806 0.0037, -0.00840, 0.0953 0.0112, -0.01420, -0.0502 0.0191, -0.01930, -0.0193 0.0397, -0.03030, -0.1495 0.0706, -0.04420, -0.3446 0.1037, -0.05710, -0.3938 0.1384, -0.06890, -0.6407 0.1741, -0.07950, -0.7809 0.2102, -0.08660, -0.9411 0.2472, -0.09640, -1.1378 0.2844, -0.10270, -1.2665 0.3225, -0.10690, -1.3993 0.3608, -0.10890, -1.5105 0.3991, -0.10830, -1.5534 0.4373, -0.10510, -1.5268 0.4757, -0.09890, -1.3840 0.5137, -0.09070, -1.2455 0.5694, -0.07640, -0.9918 15 Flap element taps 1.0000, 0.00130, -0.7578 0.9365, 0.01390, 0.2215 0.8333, 0.03280, 0.5944 0.7436, 0.04930, 0.5480 0.7049, 0.05670, 0.5364 0.6662, 0.06410, 0.5462 0.6522, 0.01390, -0.7657 0.5969, -0.00020, -0.7718 0.6000, -0.03020, -0.7672 0.6324, -0.04540, -0.7557 0.6667, -0.04880, -0.7532 0.7046, -0.04110, -0.7521 0.7429, -0.03210, -0.7576 0.8333, -0.01400, -0.7652 0.9311, -0.00120, -0.7592 --------- Run Conditions: vel=224.4 ft/s Re=1.996x10^6 AOA=12.02 Flap deflection=-60.00 Totals: Cl=-0.8693 Cdp=0.2460 Cm(c/4)=0.2563 Cs=-0.4217 Ch=0.3640 Main component: Cl=-0.5989 Cdp=0.0004 Cm=0.2413 Flap component: Cl=-0.2705 Cdp=0.2456 Cm=0.2147 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8128 0.6175, -0.04610, -0.7666 0.5841, -0.02440, -0.7614 0.5775, 0.01750, -0.7637 0.5777, 0.04660, -0.7641 0.6274, 0.07170, 0.4610 0.5694, 0.08320, 0.4601 0.5112, 0.09370, 0.4723 0.4731, 0.09830, 0.4783 0.4349, 0.10070, 0.4673 0.3960, 0.10120, 0.3913 0.3566, 0.10020, 0.2683 0.3172, 0.09790, 0.1841 0.2778, 0.09440, 0.1079 0.2393, 0.08960, 0.0385 0.2056, 0.08360, -0.0097 0.1633, 0.07610, -0.0431 0.1261, 0.06710, -0.0508 0.0900, 0.05640, -0.0395 0.0571, 0.04390, -0.0534 0.0283, 0.02940, 0.0874 0.0142, 0.01970, 0.1790 0.0081, 0.01410, 0.3934 0.0026, 0.00780, 0.5841 0.0000, 0.00000, 0.9923 0.0037, -0.00840, 0.7881 0.0112, -0.01420, 0.5162 0.0191, -0.01930, 0.4611 0.0397, -0.03030, 0.2679 0.0706, -0.04420, 0.0315 0.1037, -0.05710, -0.0671 0.1384, -0.06890, -0.3244 0.1741, -0.07950, -0.4838 0.2102, -0.08660, -0.6565 0.2472, -0.09640, -0.8623 0.2844, -0.10270, -1.0073 0.3225, -0.10690, -1.1577 0.3608, -0.10890, -1.2869 0.3991, -0.10830, -1.3555 0.4373, -0.10510, -1.3585 0.4757, -0.09890, -1.2492 0.5137, -0.09070, -1.1550 0.5694, -0.07640, -0.9278 15 Flap element taps 1.0000, 0.00130, -0.7559 0.9365, 0.01390, 0.2123 0.8333, 0.03280, 0.5553 0.7436, 0.04930, 0.4605 0.7049, 0.05670, 0.4508 0.6662, 0.06410, 0.4605 0.6522, 0.01390, -0.7619 0.5969, -0.00020, -0.7693 0.6000, -0.03020, -0.7655 0.6324, -0.04540, -0.7520 0.6667, -0.04880, -0.7492 0.7046, -0.04110, -0.7499 0.7429, -0.03210, -0.7547 0.8333, -0.01400, -0.7632 0.9311, -0.00120, -0.7546 --------- Run Conditions: vel=225.4 ft/s Re=1.996x10^6 AOA=15.00 Flap deflection=-60.00 Totals: Cl=-0.6169 Cdp=0.2312 Cm(c/4)=0.2468 Cs=-0.3830 Ch=0.3375 Main component: Cl=-0.3583 Cdp=0.0210 Cm=0.1836 Flap component: Cl=-0.2586 Cdp=0.2102 Cm=0.1972 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7626 0.6175, -0.04610, -0.7531 0.5841, -0.02440, -0.7458 0.5775, 0.01750, -0.7427 0.5777, 0.04660, -0.7432 0.6274, 0.07170, 0.3529 0.5694, 0.08320, 0.3424 0.5112, 0.09370, 0.3563 0.4731, 0.09830, 0.3667 0.4349, 0.10070, 0.3659 0.3960, 0.10120, 0.3422 0.3566, 0.10020, 0.2477 0.3172, 0.09790, 0.1294 0.2778, 0.09440, 0.0143 0.2393, 0.08960, -0.0861 0.2056, 0.08360, -0.1692 0.1633, 0.07610, -0.2433 0.1261, 0.06710, -0.2936 0.0900, 0.05640, -0.3347 0.0571, 0.04390, -0.4464 0.0283, 0.02940, -0.4346 0.0142, 0.01970, -0.5164 0.0081, 0.01410, -0.3359 0.0026, 0.00780, -0.0965 0.0000, 0.00000, 0.4390 0.0037, -0.00840, 1.0088 0.0112, -0.01420, 0.9174 0.0191, -0.01930, 0.8038 0.0397, -0.03030, 0.6046 0.0706, -0.04420, 0.3572 0.1037, -0.05710, 0.2178 0.1384, -0.06890, -0.0255 0.1741, -0.07950, -0.1975 0.2102, -0.08660, -0.3761 0.2472, -0.09640, -0.5849 0.2844, -0.10270, -0.7417 0.3225, -0.10690, -0.9058 0.3608, -0.10890, -1.0513 0.3991, -0.10830, -1.1409 0.4373, -0.10510, -1.1684 0.4757, -0.09890, -1.0893 0.5137, -0.09070, -1.0373 0.5694, -0.07640, -0.8453 15 Flap element taps 1.0000, 0.00130, -0.7326 0.9365, 0.01390, 0.2119 0.8333, 0.03280, 0.4607 0.7436, 0.04930, 0.3325 0.7049, 0.05670, 0.3308 0.6662, 0.06410, 0.3487 0.6522, 0.01390, -0.7386 0.5969, -0.00020, -0.7474 0.6000, -0.03020, -0.7450 0.6324, -0.04540, -0.7337 0.6667, -0.04880, -0.7274 0.7046, -0.04110, -0.7282 0.7429, -0.03210, -0.7347 0.8333, -0.01400, -0.7366 0.9311, -0.00120, -0.7304 --------- Run Conditions: vel=226.8 ft/s Re=2.004x10^6 AOA=17.99 Flap deflection=-60.00 Totals: Cl=-0.3330 Cdp=0.2153 Cm(c/4)=0.2257 Cs=-0.3076 Ch=0.3011 Main component: Cl=-0.1003 Cdp=0.0482 Cm=0.1159 Flap component: Cl=-0.2327 Cdp=0.1671 Cm=0.1724 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6907 0.6175, -0.04610, -0.7073 0.5841, -0.02440, -0.7025 0.5775, 0.01750, -0.7100 0.5777, 0.04660, -0.7091 0.6274, 0.07170, 0.1684 0.5694, 0.08320, 0.1475 0.5112, 0.09370, 0.1677 0.4731, 0.09830, 0.1808 0.4349, 0.10070, 0.1850 0.3960, 0.10120, 0.1847 0.3566, 0.10020, 0.1612 0.3172, 0.09790, 0.0898 0.2778, 0.09440, -0.0398 0.2393, 0.08960, -0.1786 0.2056, 0.08360, -0.3080 0.1633, 0.07610, -0.4345 0.1261, 0.06710, -0.5418 0.0900, 0.05640, -0.6630 0.0571, 0.04390, -0.8897 0.0283, 0.02940, -1.0613 0.0142, 0.01970, -1.4099 0.0081, 0.01410, -1.3257 0.0026, 0.00780, -1.0909 0.0000, 0.00000, -0.9881 0.0037, -0.00840, 0.8021 0.0112, -0.01420, 1.0101 0.0191, -0.01930, 0.9851 0.0397, -0.03030, 0.8407 0.0706, -0.04420, 0.6222 0.1037, -0.05710, 0.4548 0.1384, -0.06890, 0.2416 0.1741, -0.07950, 0.0668 0.2102, -0.08660, -0.1097 0.2472, -0.09640, -0.3152 0.2844, -0.10270, -0.4777 0.3225, -0.10690, -0.6495 0.3608, -0.10890, -0.8038 0.3991, -0.10830, -0.9119 0.4373, -0.10510, -0.9611 0.4757, -0.09890, -0.9112 0.5137, -0.09070, -0.8943 0.5694, -0.07640, -0.7318 15 Flap element taps 1.0000, 0.00130, -0.6976 0.9365, 0.01390, 0.2197 0.8333, 0.03280, 0.3441 0.7436, 0.04930, 0.1551 0.7049, 0.05670, 0.1426 0.6662, 0.06410, 0.1743 0.6522, 0.01390, -0.7031 0.5969, -0.00020, -0.7122 0.6000, -0.03020, -0.7087 0.6324, -0.04540, -0.6920 0.6667, -0.04880, -0.6865 0.7046, -0.04110, -0.6878 0.7429, -0.03210, -0.6911 0.8333, -0.01400, -0.6965 0.9311, -0.00120, -0.6904 --------- Run Conditions: vel=227.6 ft/s Re=2.006x10^6 AOA=19.99 Flap deflection=-60.00 Totals: Cl=-0.0860 Cdp=0.2009 Cm(c/4)=0.1900 Cs=-0.2182 Ch=0.2468 Main component: Cl=0.1000 Cdp=0.0799 Cm=0.0562 Flap component: Cl=-0.1860 Cdp=0.1210 Cm=0.1369 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6232 0.6175, -0.04610, -0.6635 0.5841, -0.02440, -0.6621 0.5775, 0.01750, -0.6668 0.5777, 0.04660, -0.6659 0.6274, 0.07170, -0.0357 0.5694, 0.08320, -0.0798 0.5112, 0.09370, -0.0455 0.4731, 0.09830, -0.0387 0.4349, 0.10070, -0.0315 0.3960, 0.10120, -0.0266 0.3566, 0.10020, -0.0366 0.3172, 0.09790, -0.0463 0.2778, 0.09440, -0.0820 0.2393, 0.08960, -0.1775 0.2056, 0.08360, -0.3315 0.1633, 0.07610, -0.5125 0.1261, 0.06710, -0.6822 0.0900, 0.05640, -0.8841 0.0571, 0.04390, -1.2031 0.0283, 0.02940, -1.5462 0.0142, 0.01970, -2.1259 0.0081, 0.01410, -2.1813 0.0026, 0.00780, -1.9499 0.0000, 0.00000, -2.5007 0.0037, -0.00840, 0.3950 0.0112, -0.01420, 0.9515 0.0191, -0.01930, 1.0091 0.0397, -0.03030, 0.9474 0.0706, -0.04420, 0.7705 0.1037, -0.05710, 0.6122 0.1384, -0.06890, 0.4118 0.1741, -0.07950, 0.2396 0.2102, -0.08660, 0.0653 0.2472, -0.09640, -0.1359 0.2844, -0.10270, -0.2929 0.3225, -0.10690, -0.4639 0.3608, -0.10890, -0.6234 0.3991, -0.10830, -0.7396 0.4373, -0.10510, -0.8001 0.4757, -0.09890, -0.7696 0.5137, -0.09070, -0.7820 0.5694, -0.07640, -0.6412 15 Flap element taps 1.0000, 0.00130, -0.6496 0.9365, 0.01390, 0.2085 0.8333, 0.03280, 0.1421 0.7436, 0.04930, -0.0653 0.7049, 0.05670, -0.0776 0.6662, 0.06410, -0.0295 0.6522, 0.01390, -0.6608 0.5969, -0.00020, -0.6683 0.6000, -0.03020, -0.6629 0.6324, -0.04540, -0.6415 0.6667, -0.04880, -0.6342 0.7046, -0.04110, -0.6373 0.7429, -0.03210, -0.6395 0.8333, -0.01400, -0.6449 0.9311, -0.00120, -0.6424 --------- Run Conditions: vel=226.6 ft/s Re=1.997x10^6 AOA=24.02 Flap deflection=-60.00 Totals: Cl=0.5564 Cdp=0.2314 Cm(c/4)=0.0060 Cs=0.0151 Ch=-0.0378 Main component: Cl=0.5009 Cdp=0.2879 Cm=-0.1163 Flap component: Cl=0.0556 Cdp=-0.0565 Cm=-0.0284 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5606 0.6175, -0.04610, -0.7505 0.5841, -0.02440, -0.7478 0.5775, 0.01750, -0.7563 0.5777, 0.04660, -0.7548 0.6274, 0.07170, -0.6858 0.5694, 0.08320, -0.8309 0.5112, 0.09370, -0.8553 0.4731, 0.09830, -0.8507 0.4349, 0.10070, -0.8363 0.3960, 0.10120, -0.8318 0.3566, 0.10020, -0.8443 0.3172, 0.09790, -0.8552 0.2778, 0.09440, -0.8583 0.2393, 0.08960, -0.8587 0.2056, 0.08360, -0.8649 0.1633, 0.07610, -0.8923 0.1261, 0.06710, -0.9147 0.0900, 0.05640, -0.9471 0.0571, 0.04390, -1.0241 0.0283, 0.02940, -1.2271 0.0142, 0.01970, -1.7507 0.0081, 0.01410, -2.1285 0.0026, 0.00780, -2.1699 0.0000, 0.00000, -3.9726 0.0037, -0.00840, -0.2957 0.0112, -0.01420, 0.7317 0.0191, -0.01930, 0.9235 0.0397, -0.03030, 1.0114 0.0706, -0.04420, 0.9314 0.1037, -0.05710, 0.8147 0.1384, -0.06890, 0.6496 0.1741, -0.07950, 0.5008 0.2102, -0.08660, 0.3441 0.2472, -0.09640, 0.1591 0.2844, -0.10270, -0.0011 0.3225, -0.10690, -0.1793 0.3608, -0.10890, -0.3398 0.3991, -0.10830, -0.4791 0.4373, -0.10510, -0.5535 0.4757, -0.09890, -0.5549 0.5137, -0.09070, -0.5899 0.5694, -0.07640, -0.4991 15 Flap element taps 1.0000, 0.00130, -0.5787 0.9365, 0.01390, -0.4378 0.8333, 0.03280, -0.6804 0.7436, 0.04930, -0.7745 0.7049, 0.05670, -0.7518 0.6662, 0.06410, -0.6740 0.6522, 0.01390, -0.7441 0.5969, -0.00020, -0.7549 0.6000, -0.03020, -0.5676 0.6324, -0.04540, -0.4426 0.6667, -0.04880, -0.4296 0.7046, -0.04110, -0.4339 0.7429, -0.03210, -0.4344 0.8333, -0.01400, -0.4410 0.9311, -0.00120, -0.4576 --------- Run Conditions: vel=227.9 ft/s Re=2.005x10^6 AOA=27.01 Flap deflection=-60.00 Totals: Cl=0.5722 Cdp=0.2931 Cm(c/4)=-0.0203 Cs=-0.0012 Ch=-0.0869 Main component: Cl=0.4765 Cdp=0.3726 Cm=-0.1285 Flap component: Cl=0.0957 Cdp=-0.0795 Cm=-0.0525 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6665 0.6175, -0.04610, -0.9774 0.5841, -0.02440, -0.9679 0.5775, 0.01750, -0.9716 0.5777, 0.04660, -0.9705 0.6274, 0.07170, -0.7881 0.5694, 0.08320, -0.8910 0.5112, 0.09370, -0.9241 0.4731, 0.09830, -0.9418 0.4349, 0.10070, -0.9289 0.3960, 0.10120, -0.9094 0.3566, 0.10020, -0.9114 0.3172, 0.09790, -0.9039 0.2778, 0.09440, -0.9004 0.2393, 0.08960, -0.8951 0.2056, 0.08360, -0.8886 0.1633, 0.07610, -0.9019 0.1261, 0.06710, -0.9095 0.0900, 0.05640, -0.9359 0.0571, 0.04390, -0.9693 0.0283, 0.02940, -1.0309 0.0142, 0.01970, -1.1834 0.0081, 0.01410, -1.4095 0.0026, 0.00780, -1.4430 0.0000, 0.00000, -3.2241 0.0037, -0.00840, -0.2280 0.0112, -0.01420, 0.7202 0.0191, -0.01930, 0.9079 0.0397, -0.03030, 1.0106 0.0706, -0.04420, 0.9510 0.1037, -0.05710, 0.8471 0.1384, -0.06890, 0.6930 0.1741, -0.07950, 0.5503 0.2102, -0.08660, 0.3979 0.2472, -0.09640, 0.2141 0.2844, -0.10270, 0.0510 0.3225, -0.10690, -0.1323 0.3608, -0.10890, -0.3025 0.3991, -0.10830, -0.4548 0.4373, -0.10510, -0.5468 0.4757, -0.09890, -0.5697 0.5137, -0.09070, -0.6234 0.5694, -0.07640, -0.5607 15 Flap element taps 1.0000, 0.00130, -0.8360 0.9365, 0.01390, -0.7932 0.8333, 0.03280, -0.9014 0.7436, 0.04930, -0.8923 0.7049, 0.05670, -0.8518 0.6662, 0.06410, -0.8051 0.6522, 0.01390, -0.9693 0.5969, -0.00020, -0.9820 0.6000, -0.03020, -0.7153 0.6324, -0.04540, -0.5322 0.6667, -0.04880, -0.5055 0.7046, -0.04110, -0.5127 0.7429, -0.03210, -0.5140 0.8333, -0.01400, -0.5317 0.9311, -0.00120, -0.5588