S809 UNVENTED AILERON, LEGR, CHORD = 18 IN --------- Run Conditions: vel=215.8 ft/s Re=2.010x10^6 AOA=-6.02 Flap deflection=-45.00 Totals: Cl=-1.4629 Cdp=0.3065 Cm(c/4)=0.1871 Cs=-0.1514 Ch=0.3269 Main component: Cl=-1.2167 Cdp=0.0481 Cm=0.3158 Flap component: Cl=-0.2462 Cdp=0.2584 Cm=0.2430 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6452 0.6175, -0.04610, -0.5945 0.5841, -0.02440, -0.5877 0.5775, 0.01750, -0.5881 0.5777, 0.04660, -0.5842 0.6274, 0.07170, 0.7412 0.5694, 0.08320, 0.7209 0.5112, 0.09370, 0.5973 0.4731, 0.09830, 0.5024 0.4349, 0.10070, 0.4512 0.3960, 0.10120, 0.4412 0.3566, 0.10020, 0.4341 0.3172, 0.09790, 0.4493 0.2778, 0.09440, 0.4667 0.2393, 0.08960, 0.4974 0.2056, 0.08360, 0.5481 0.1633, 0.07610, 0.6149 0.1261, 0.06710, 0.7094 0.0900, 0.05640, 0.7964 0.0571, 0.04390, 0.9463 0.0283, 0.02940, 1.0054 0.0142, 0.01970, 0.8282 0.0081, 0.01410, 0.5062 0.0026, 0.00780, -0.5023 0.0000, 0.00000, -0.1863 0.0037, -0.00840, -4.6883 0.0112, -0.01420, -3.3570 0.0191, -0.01930, -2.8548 0.0397, -0.03030, -2.0895 0.0706, -0.04420, -1.8056 0.1037, -0.05710, -1.6203 0.1384, -0.06890, -1.6127 0.1741, -0.07950, -1.5896 0.2102, -0.08660, -1.6128 0.2472, -0.09640, -1.6497 0.2844, -0.10270, -1.6187 0.3225, -0.10690, -1.5645 0.3608, -0.10890, -1.4618 0.3991, -0.10830, -1.2688 0.4373, -0.10510, -0.9963 0.4757, -0.09890, -0.7510 0.5137, -0.09070, -0.6775 0.5694, -0.07640, -0.6501 14 Flap element taps 1.0000, 0.00130, -0.6052 0.9365, 0.01390, 0.1641 0.8333, 0.03280, 0.5172 0.7436, 0.04930, 0.7538 0.7049, 0.05670, 0.8297 0.6662, 0.06410, 0.7545 0.6522, 0.01390, -0.5825 0.5969, -0.00020, -0.6133 0.6000, -0.03020, -0.6129 0.6324, -0.04540, -0.6116 0.6667, -0.04880, -0.6160 0.7046, -0.04110, -0.6181 0.7429, -0.03210, -0.6191 0.9311, -0.00120, -0.6157 --------- Run Conditions: vel=216.5 ft/s Re=2.006x10^6 AOA=0.05 Flap deflection=-45.00 Totals: Cl=-1.3887 Cdp=0.2262 Cm(c/4)=0.2234 Cs=-0.2274 Ch=0.3166 Main component: Cl=-1.1290 Cdp=0.0084 Cm=0.3380 Flap component: Cl=-0.2597 Cdp=0.2178 Cm=0.2325 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6836 0.6175, -0.04610, -0.5822 0.5841, -0.02440, -0.5798 0.5775, 0.01750, -0.5806 0.5777, 0.04660, -0.5785 0.6274, 0.07170, 0.6082 0.5694, 0.08320, 0.6126 0.5112, 0.09370, 0.5861 0.4731, 0.09830, 0.4747 0.4349, 0.10070, 0.3807 0.3960, 0.10120, 0.3443 0.3566, 0.10020, 0.3132 0.3172, 0.09790, 0.3083 0.2778, 0.09440, 0.3053 0.2393, 0.08960, 0.3131 0.2056, 0.08360, 0.3436 0.1633, 0.07610, 0.3906 0.1261, 0.06710, 0.4748 0.0900, 0.05640, 0.5243 0.0571, 0.04390, 0.7385 0.0283, 0.02940, 0.9324 0.0142, 0.01970, 1.0125 0.0081, 0.01410, 0.9684 0.0026, 0.00780, 0.4452 0.0000, 0.00000, -0.1071 0.0037, -0.00840, -2.1381 0.0112, -0.01420, -1.5987 0.0191, -0.01930, -1.4955 0.0397, -0.03030, -1.2033 0.0706, -0.04420, -1.1776 0.1037, -0.05710, -1.1406 0.1384, -0.06890, -1.2667 0.1741, -0.07950, -1.3355 0.2102, -0.08660, -1.4427 0.2472, -0.09640, -1.5839 0.2844, -0.10270, -1.6548 0.3225, -0.10690, -1.7203 0.3608, -0.10890, -1.7576 0.3991, -0.10830, -1.7292 0.4373, -0.10510, -1.6266 0.4757, -0.09890, -1.3866 0.5137, -0.09070, -1.1956 0.5694, -0.07640, -0.8720 14 Flap element taps 1.0000, 0.00130, -0.6130 0.9365, 0.01390, 0.1383 0.8333, 0.03280, 0.5097 0.7436, 0.04930, 0.6916 0.7049, 0.05670, 0.6415 0.6662, 0.06410, 0.6089 0.6522, 0.01390, -0.5781 0.5969, -0.00020, -0.6037 0.6000, -0.03020, -0.6279 0.6324, -0.04540, -0.6087 0.6667, -0.04880, -0.6080 0.7046, -0.04110, -0.6139 0.7429, -0.03210, -0.6140 0.9311, -0.00120, -0.6186 --------- Run Conditions: vel=217.8 ft/s Re=2.011x10^6 AOA=3.06 Flap deflection=-45.00 Totals: Cl=-1.2788 Cdp=0.1925 Cm(c/4)=0.2339 Cs=-0.2605 Ch=0.3184 Main component: Cl=-1.0086 Cdp=-0.0106 Cm=0.3182 Flap component: Cl=-0.2702 Cdp=0.2030 Cm=0.2324 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7211 0.6175, -0.04610, -0.6034 0.5841, -0.02440, -0.6035 0.5775, 0.01750, -0.6028 0.5777, 0.04660, -0.6001 0.6274, 0.07170, 0.5676 0.5694, 0.08320, 0.5691 0.5112, 0.09370, 0.5598 0.4731, 0.09830, 0.4659 0.4349, 0.10070, 0.3567 0.3960, 0.10120, 0.3087 0.3566, 0.10020, 0.2628 0.3172, 0.09790, 0.2481 0.2778, 0.09440, 0.2335 0.2393, 0.08960, 0.2297 0.2056, 0.08360, 0.2499 0.1633, 0.07610, 0.2828 0.1261, 0.06710, 0.3564 0.0900, 0.05640, 0.3751 0.0571, 0.04390, 0.5985 0.0283, 0.02940, 0.8159 0.0142, 0.01970, 0.9763 0.0081, 0.01410, 1.0132 0.0026, 0.00780, 0.7165 0.0000, 0.00000, -0.0435 0.0037, -0.00840, -1.1660 0.0112, -0.01420, -0.9364 0.0191, -0.01930, -0.9387 0.0397, -0.03030, -0.8148 0.0706, -0.04420, -0.8724 0.1037, -0.05710, -0.8850 0.1384, -0.06890, -1.0529 0.1741, -0.07950, -1.1489 0.2102, -0.08660, -1.2750 0.2472, -0.09640, -1.4387 0.2844, -0.10270, -1.5315 0.3225, -0.10690, -1.6231 0.3608, -0.10890, -1.6830 0.3991, -0.10830, -1.6819 0.4373, -0.10510, -1.6099 0.4757, -0.09890, -1.3947 0.5137, -0.09070, -1.2321 0.5694, -0.07640, -0.9173 14 Flap element taps 1.0000, 0.00130, -0.6388 0.9365, 0.01390, 0.1292 0.8333, 0.03280, 0.5057 0.7436, 0.04930, 0.6391 0.7049, 0.05670, 0.5879 0.6662, 0.06410, 0.5689 0.6522, 0.01390, -0.5968 0.5969, -0.00020, -0.6251 0.6000, -0.03020, -0.6529 0.6324, -0.04540, -0.6295 0.6667, -0.04880, -0.6285 0.7046, -0.04110, -0.6335 0.7429, -0.03210, -0.6348 0.9311, -0.00120, -0.6406 --------- Run Conditions: vel=217.2 ft/s Re=1.998x10^6 AOA=6.04 Flap deflection=-45.00 Totals: Cl=-1.0504 Cdp=0.1712 Cm(c/4)=0.2359 Cs=-0.2808 Ch=0.3073 Main component: Cl=-0.7824 Cdp=-0.0086 Cm=0.2699 Flap component: Cl=-0.2681 Cdp=0.1798 Cm=0.2227 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7062 0.6175, -0.04610, -0.5940 0.5841, -0.02440, -0.5912 0.5775, 0.01750, -0.5934 0.5777, 0.04660, -0.5929 0.6274, 0.07170, 0.4971 0.5694, 0.08320, 0.4988 0.5112, 0.09370, 0.5000 0.4731, 0.09830, 0.4371 0.4349, 0.10070, 0.3122 0.3960, 0.10120, 0.2425 0.3566, 0.10020, 0.1732 0.3172, 0.09790, 0.1414 0.2778, 0.09440, 0.1083 0.2393, 0.08960, 0.0861 0.2056, 0.08360, 0.0872 0.1633, 0.07610, 0.0957 0.1261, 0.06710, 0.1484 0.0900, 0.05640, 0.1154 0.0571, 0.04390, 0.3328 0.0283, 0.02940, 0.5499 0.0142, 0.01970, 0.7597 0.0081, 0.01410, 0.9037 0.0026, 0.00780, 0.9781 0.0000, 0.00000, 0.0044 0.0037, -0.00840, -0.0145 0.0112, -0.01420, -0.1150 0.0191, -0.01930, -0.2385 0.0397, -0.03030, -0.2898 0.0706, -0.04420, -0.4376 0.1037, -0.05710, -0.5107 0.1384, -0.06890, -0.7174 0.1741, -0.07950, -0.8431 0.2102, -0.08660, -0.9861 0.2472, -0.09640, -1.1702 0.2844, -0.10270, -1.2835 0.3225, -0.10690, -1.4004 0.3608, -0.10890, -1.4852 0.3991, -0.10830, -1.5122 0.4373, -0.10510, -1.4759 0.4757, -0.09890, -1.2977 0.5137, -0.09070, -1.1619 0.5694, -0.07640, -0.8793 14 Flap element taps 1.0000, 0.00130, -0.6266 0.9365, 0.01390, 0.1139 0.8333, 0.03280, 0.4944 0.7436, 0.04930, 0.5572 0.7049, 0.05670, 0.5036 0.6662, 0.06410, 0.4967 0.6522, 0.01390, -0.5880 0.5969, -0.00020, -0.6162 0.6000, -0.03020, -0.6444 0.6324, -0.04540, -0.6199 0.6667, -0.04880, -0.6205 0.7046, -0.04110, -0.6268 0.7429, -0.03210, -0.6261 0.9311, -0.00120, -0.6333 --------- Run Conditions: vel=217.8 ft/s Re=1.995x10^6 AOA=9.02 Flap deflection=-45.00 Totals: Cl=-0.8032 Cdp=0.1546 Cm(c/4)=0.2334 Cs=-0.2786 Ch=0.2916 Main component: Cl=-0.5438 Cdp=0.0004 Cm=0.2165 Flap component: Cl=-0.2593 Cdp=0.1542 Cm=0.2091 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6763 0.6175, -0.04610, -0.5849 0.5841, -0.02440, -0.5826 0.5775, 0.01750, -0.5817 0.5777, 0.04660, -0.5817 0.6274, 0.07170, 0.4094 0.5694, 0.08320, 0.4083 0.5112, 0.09370, 0.4151 0.4731, 0.09830, 0.3922 0.4349, 0.10070, 0.2810 0.3960, 0.10120, 0.1870 0.3566, 0.10020, 0.0895 0.3172, 0.09790, 0.0356 0.2778, 0.09440, -0.0196 0.2393, 0.08960, -0.0652 0.2056, 0.08360, -0.0873 0.1633, 0.07610, -0.1098 0.1261, 0.06710, -0.0868 0.0900, 0.05640, -0.1843 0.0571, 0.04390, 0.0005 0.0283, 0.02940, 0.1614 0.0142, 0.01970, 0.3496 0.0081, 0.01410, 0.5298 0.0026, 0.00780, 0.6507 0.0000, 0.00000, 0.0441 0.0037, -0.00840, 0.7197 0.0112, -0.01420, 0.4821 0.0191, -0.01930, 0.3236 0.0397, -0.03030, 0.1523 0.0706, -0.04420, -0.0486 0.1037, -0.05710, -0.1688 0.1384, -0.06890, -0.3972 0.1741, -0.07950, -0.5440 0.2102, -0.08660, -0.6986 0.2472, -0.09640, -0.8952 0.2844, -0.10270, -1.0246 0.3225, -0.10690, -1.1629 0.3608, -0.10890, -1.2658 0.3991, -0.10830, -1.3198 0.4373, -0.10510, -1.3125 0.4757, -0.09890, -1.1703 0.5137, -0.09070, -1.0639 0.5694, -0.07640, -0.8198 14 Flap element taps 1.0000, 0.00130, -0.6087 0.9365, 0.01390, 0.1049 0.8333, 0.03280, 0.4665 0.7436, 0.04930, 0.4508 0.7049, 0.05670, 0.4140 0.6662, 0.06410, 0.4117 0.6522, 0.01390, -0.5736 0.5969, -0.00020, -0.6036 0.6000, -0.03020, -0.6255 0.6324, -0.04540, -0.6046 0.6667, -0.04880, -0.6016 0.7046, -0.04110, -0.6104 0.7429, -0.03210, -0.6099 0.9311, -0.00120, -0.6191 --------- Run Conditions: vel=219.1 ft/s Re=2.002x10^6 AOA=12.05 Flap deflection=-45.00 Totals: Cl=-0.5374 Cdp=0.1458 Cm(c/4)=0.2270 Cs=-0.2548 Ch=0.2733 Main component: Cl=-0.2921 Cdp=0.0188 Cm=0.1577 Flap component: Cl=-0.2453 Cdp=0.1270 Cm=0.1931 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6268 0.6175, -0.04610, -0.5654 0.5841, -0.02440, -0.5581 0.5775, 0.01750, -0.5605 0.5777, 0.04660, -0.5602 0.6274, 0.07170, 0.2970 0.5694, 0.08320, 0.2967 0.5112, 0.09370, 0.3068 0.4731, 0.09830, 0.3038 0.4349, 0.10070, 0.2459 0.3960, 0.10120, 0.1453 0.3566, 0.10020, 0.0152 0.3172, 0.09790, -0.0662 0.2778, 0.09440, -0.1491 0.2393, 0.08960, -0.2227 0.2056, 0.08360, -0.2737 0.1633, 0.07610, -0.3345 0.1261, 0.06710, -0.3511 0.0900, 0.05640, -0.5190 0.0571, 0.04390, -0.4061 0.0283, 0.02940, -0.3571 0.0142, 0.01970, -0.2666 0.0081, 0.01410, -0.1786 0.0026, 0.00780, 0.0295 0.0000, 0.00000, 0.0855 0.0037, -0.00840, 1.0011 0.0112, -0.01420, 0.8750 0.0191, -0.01930, 0.7320 0.0397, -0.03030, 0.5211 0.0706, -0.04420, 0.2977 0.1037, -0.05710, 0.1464 0.1384, -0.06890, -0.0902 0.1741, -0.07950, -0.2499 0.2102, -0.08660, -0.4106 0.2472, -0.09640, -0.6146 0.2844, -0.10270, -0.7562 0.3225, -0.10690, -0.9101 0.3608, -0.10890, -1.0275 0.3991, -0.10830, -1.1057 0.4373, -0.10510, -1.1255 0.4757, -0.09890, -1.0195 0.5137, -0.09070, -0.9394 0.5694, -0.07640, -0.7358 14 Flap element taps 1.0000, 0.00130, -0.5806 0.9365, 0.01390, 0.1073 0.8333, 0.03280, 0.4355 0.7436, 0.04930, 0.3398 0.7049, 0.05670, 0.3005 0.6662, 0.06410, 0.2999 0.6522, 0.01390, -0.5533 0.5969, -0.00020, -0.5819 0.6000, -0.03020, -0.6014 0.6324, -0.04540, -0.5792 0.6667, -0.04880, -0.5757 0.7046, -0.04110, -0.5839 0.7429, -0.03210, -0.5841 0.9311, -0.00120, -0.5931 --------- Run Conditions: vel=219.7 ft/s Re=1.996x10^6 AOA=15.02 Flap deflection=-45.00 Totals: Cl=-0.2617 Cdp=0.1435 Cm(c/4)=0.2113 Cs=-0.2064 Ch=0.2424 Main component: Cl=-0.0455 Cdp=0.0469 Cm=0.0979 Flap component: Cl=-0.2162 Cdp=0.0966 Cm=0.1673 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5762 0.6175, -0.04610, -0.5430 0.5841, -0.02440, -0.5436 0.5775, 0.01750, -0.5470 0.5777, 0.04660, -0.5447 0.6274, 0.07170, 0.1581 0.5694, 0.08320, 0.1585 0.5112, 0.09370, 0.1654 0.4731, 0.09830, 0.1698 0.4349, 0.10070, 0.1540 0.3960, 0.10120, 0.1030 0.3566, 0.10020, -0.0130 0.3172, 0.09790, -0.1346 0.2778, 0.09440, -0.2558 0.2393, 0.08960, -0.3656 0.2056, 0.08360, -0.4682 0.1633, 0.07610, -0.5565 0.1261, 0.06710, -0.6331 0.0900, 0.05640, -0.8655 0.0571, 0.04390, -0.8635 0.0283, 0.02940, -0.9800 0.0142, 0.01970, -1.0705 0.0081, 0.01410, -1.1161 0.0026, 0.00780, -0.8547 0.0000, 0.00000, -0.0823 0.0037, -0.00840, 0.9006 0.0112, -0.01420, 1.0107 0.0191, -0.01930, 0.9607 0.0397, -0.03030, 0.7871 0.0706, -0.04420, 0.5700 0.1037, -0.05710, 0.4039 0.1384, -0.06890, 0.1909 0.1741, -0.07950, 0.0231 0.2102, -0.08660, -0.1526 0.2472, -0.09640, -0.3483 0.2844, -0.10270, -0.5029 0.3225, -0.10690, -0.6600 0.3608, -0.10890, -0.7972 0.3991, -0.10830, -0.8894 0.4373, -0.10510, -0.9388 0.4757, -0.09890, -0.8684 0.5137, -0.09070, -0.8149 0.5694, -0.07640, -0.6428 14 Flap element taps 1.0000, 0.00130, -0.5699 0.9365, 0.01390, 0.1113 0.8333, 0.03280, 0.3246 0.7436, 0.04930, 0.1720 0.7049, 0.05670, 0.1472 0.6662, 0.06410, 0.1550 0.6522, 0.01390, -0.5403 0.5969, -0.00020, -0.5584 0.6000, -0.03020, -0.5701 0.6324, -0.04540, -0.5561 0.6667, -0.04880, -0.5542 0.7046, -0.04110, -0.5564 0.7429, -0.03210, -0.5589 0.9311, -0.00120, -0.5656 --------- Run Conditions: vel=220.9 ft/s Re=2.001x10^6 AOA=18.01 Flap deflection=-45.00 Totals: Cl=0.1133 Cdp=0.1442 Cm(c/4)=0.1580 Cs=-0.1021 Ch=0.1589 Main component: Cl=0.2467 Cdp=0.0952 Cm=0.0165 Flap component: Cl=-0.1334 Cdp=0.0491 Cm=0.1034 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4714 0.6175, -0.04610, -0.4804 0.5841, -0.02440, -0.4776 0.5775, 0.01750, -0.4809 0.5777, 0.04660, -0.4790 0.6274, 0.07170, -0.1143 0.5694, 0.08320, -0.1208 0.5112, 0.09370, -0.1151 0.4731, 0.09830, -0.1058 0.4349, 0.10070, -0.1089 0.3960, 0.10120, -0.1140 0.3566, 0.10020, -0.1370 0.3172, 0.09790, -0.1813 0.2778, 0.09440, -0.2643 0.2393, 0.08960, -0.4093 0.2056, 0.08360, -0.5844 0.1633, 0.07610, -0.7557 0.1261, 0.06710, -0.9170 0.0900, 0.05640, -1.2309 0.0571, 0.04390, -1.4126 0.0283, 0.02940, -1.8008 0.0142, 0.01970, -2.1981 0.0081, 0.01410, -2.4855 0.0026, 0.00780, -2.3368 0.0000, 0.00000, -0.0465 0.0037, -0.00840, 0.3325 0.0112, -0.01420, 0.9119 0.0191, -0.01930, 1.0055 0.0397, -0.03030, 0.9616 0.0706, -0.04420, 0.8005 0.1037, -0.05710, 0.6430 0.1384, -0.06890, 0.4529 0.1741, -0.07950, 0.2863 0.2102, -0.08660, 0.1152 0.2472, -0.09640, -0.0729 0.2844, -0.10270, -0.2219 0.3225, -0.10690, -0.3804 0.3608, -0.10890, -0.5228 0.3991, -0.10830, -0.6301 0.4373, -0.10510, -0.6990 0.4757, -0.09890, -0.6617 0.5137, -0.09070, -0.6319 0.5694, -0.07640, -0.5023 14 Flap element taps 1.0000, 0.00130, -0.4965 0.9365, 0.01390, 0.0608 0.8333, 0.03280, 0.0368 0.7436, 0.04930, -0.1224 0.7049, 0.05670, -0.1309 0.6662, 0.06410, -0.1102 0.6522, 0.01390, -0.4764 0.5969, -0.00020, -0.4877 0.6000, -0.03020, -0.4923 0.6324, -0.04540, -0.4761 0.6667, -0.04880, -0.4698 0.7046, -0.04110, -0.4715 0.7429, -0.03210, -0.4760 0.9311, -0.00120, -0.4882 --------- Run Conditions: vel=220.4 ft/s Re=1.992x10^6 AOA=20.01 Flap deflection=-45.00 Totals: Cl=0.4133 Cdp=0.1825 Cm(c/4)=0.0363 Cs=-0.0301 Ch=0.0005 Main component: Cl=0.3948 Cdp=0.2071 Cm=-0.0690 Flap component: Cl=0.0186 Cdp=-0.0246 Cm=-0.0075 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4498 0.6175, -0.04610, -0.5488 0.5841, -0.02440, -0.5461 0.5775, 0.01750, -0.5476 0.5777, 0.04660, -0.5467 0.6274, 0.07170, -0.4935 0.5694, 0.08320, -0.5521 0.5112, 0.09370, -0.5683 0.4731, 0.09830, -0.5662 0.4349, 0.10070, -0.5809 0.3960, 0.10120, -0.5824 0.3566, 0.10020, -0.6072 0.3172, 0.09790, -0.6306 0.2778, 0.09440, -0.6522 0.2393, 0.08960, -0.6707 0.2056, 0.08360, -0.6946 0.1633, 0.07610, -0.7239 0.1261, 0.06710, -0.7534 0.0900, 0.05640, -0.7806 0.0571, 0.04390, -0.9181 0.0283, 0.02940, -1.2965 0.0142, 0.01970, -1.8309 0.0081, 0.01410, -2.2683 0.0026, 0.00780, -2.3832 0.0000, 0.00000, -0.0219 0.0037, -0.00840, 0.0728 0.0112, -0.01420, 0.8119 0.0191, -0.01930, 0.9729 0.0397, -0.03030, 0.9970 0.0706, -0.04420, 0.8808 0.1037, -0.05710, 0.7437 0.1384, -0.06890, 0.5728 0.1741, -0.07950, 0.4173 0.2102, -0.08660, 0.2580 0.2472, -0.09640, 0.0744 0.2844, -0.10270, -0.0787 0.3225, -0.10690, -0.2374 0.3608, -0.10890, -0.3770 0.3991, -0.10830, -0.5037 0.4373, -0.10510, -0.5752 0.4757, -0.09890, -0.5553 0.5137, -0.09070, -0.5407 0.5694, -0.07640, -0.4347 14 Flap element taps 1.0000, 0.00130, -0.4317 0.9365, 0.01390, -0.2770 0.8333, 0.03280, -0.4257 0.7436, 0.04930, -0.5158 0.7049, 0.05670, -0.5191 0.6662, 0.06410, -0.4870 0.6522, 0.01390, -0.5472 0.5969, -0.00020, -0.5535 0.6000, -0.03020, -0.5583 0.6324, -0.04540, -0.3793 0.6667, -0.04880, -0.3437 0.7046, -0.04110, -0.3447 0.7429, -0.03210, -0.3468 0.9311, -0.00120, -0.3721 --------- Run Conditions: vel=221.6 ft/s Re=2.001x10^6 AOA=23.99 Flap deflection=-45.00 Totals: Cl=0.5499 Cdp=0.2838 Cm(c/4)=0.0043 Cs=-0.0357 Ch=-0.0408 Main component: Cl=0.4840 Cdp=0.3377 Cm=-0.1142 Flap component: Cl=0.0659 Cdp=-0.0539 Cm=-0.0359 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6265 0.6175, -0.04610, -0.8778 0.5841, -0.02440, -0.8807 0.5775, 0.01750, -0.8913 0.5777, 0.04660, -0.8890 0.6274, 0.07170, -0.7267 0.5694, 0.08320, -0.8054 0.5112, 0.09370, -0.8379 0.4731, 0.09830, -0.8431 0.4349, 0.10070, -0.8409 0.3960, 0.10120, -0.8313 0.3566, 0.10020, -0.8463 0.3172, 0.09790, -0.8569 0.2778, 0.09440, -0.8748 0.2393, 0.08960, -0.8975 0.2056, 0.08360, -0.9371 0.1633, 0.07610, -0.9850 0.1261, 0.06710, -1.0115 0.0900, 0.05640, -1.0399 0.0571, 0.04390, -1.1197 0.0283, 0.02940, -1.2354 0.0142, 0.01970, -1.4762 0.0081, 0.01410, -1.7289 0.0026, 0.00780, -1.8800 0.0000, 0.00000, -0.0082 0.0037, -0.00840, -0.0619 0.0112, -0.01420, 0.7354 0.0191, -0.01930, 0.9372 0.0397, -0.03030, 1.0109 0.0706, -0.04420, 0.9295 0.1037, -0.05710, 0.8077 0.1384, -0.06890, 0.6476 0.1741, -0.07950, 0.4961 0.2102, -0.08660, 0.3379 0.2472, -0.09640, 0.1511 0.2844, -0.10270, -0.0115 0.3225, -0.10690, -0.1914 0.3608, -0.10890, -0.3526 0.3991, -0.10830, -0.5012 0.4373, -0.10510, -0.5950 0.4757, -0.09890, -0.5993 0.5137, -0.09070, -0.6192 0.5694, -0.07640, -0.5317 14 Flap element taps 1.0000, 0.00130, -0.6556 0.9365, 0.01390, -0.5233 0.8333, 0.03280, -0.6892 0.7436, 0.04930, -0.7651 0.7049, 0.05670, -0.7597 0.6662, 0.06410, -0.7136 0.6522, 0.01390, -0.8793 0.5969, -0.00020, -0.8874 0.6000, -0.03020, -0.8851 0.6324, -0.04540, -0.5561 0.6667, -0.04880, -0.4425 0.7046, -0.04110, -0.4427 0.7429, -0.03210, -0.4410 0.9311, -0.00120, -0.4771 --------- Run Conditions: vel=221.6 ft/s Re=1.996x10^6 AOA=27.02 Flap deflection=-45.00 Totals: Cl=0.4844 Cdp=0.3366 Cm(c/4)=0.0098 Cs=-0.0798 Ch=-0.0322 Main component: Cl=0.4321 Cdp=0.3844 Cm=-0.1112 Flap component: Cl=0.0523 Cdp=-0.0478 Cm=-0.0252 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7097 0.6175, -0.04610, -1.0211 0.5841, -0.02440, -1.0210 0.5775, 0.01750, -1.0210 0.5777, 0.04660, -1.0196 0.6274, 0.07170, -0.7271 0.5694, 0.08320, -0.7865 0.5112, 0.09370, -0.8162 0.4731, 0.09830, -0.8352 0.4349, 0.10070, -0.8429 0.3960, 0.10120, -0.8335 0.3566, 0.10020, -0.8497 0.3172, 0.09790, -0.8602 0.2778, 0.09440, -0.8682 0.2393, 0.08960, -0.8766 0.2056, 0.08360, -0.8986 0.1633, 0.07610, -0.9369 0.1261, 0.06710, -0.9581 0.0900, 0.05640, -0.9733 0.0571, 0.04390, -1.0022 0.0283, 0.02940, -1.0448 0.0142, 0.01970, -1.1749 0.0081, 0.01410, -1.3396 0.0026, 0.00780, -1.3488 0.0000, 0.00000, 0.0093 0.0037, -0.00840, -0.0321 0.0112, -0.01420, 0.7164 0.0191, -0.01930, 0.9192 0.0397, -0.03030, 1.0085 0.0706, -0.04420, 0.9462 0.1037, -0.05710, 0.8352 0.1384, -0.06890, 0.6836 0.1741, -0.07950, 0.5363 0.2102, -0.08660, 0.3814 0.2472, -0.09640, 0.1939 0.2844, -0.10270, 0.0279 0.3225, -0.10690, -0.1602 0.3608, -0.10890, -0.3308 0.3991, -0.10830, -0.4897 0.4373, -0.10510, -0.5962 0.4757, -0.09890, -0.6148 0.5137, -0.09070, -0.6626 0.5694, -0.07640, -0.5931 14 Flap element taps 1.0000, 0.00130, -0.7529 0.9365, 0.01390, -0.6831 0.8333, 0.03280, -0.7441 0.7436, 0.04930, -0.7626 0.7049, 0.05670, -0.7494 0.6662, 0.06410, -0.7239 0.6522, 0.01390, -1.0107 0.5969, -0.00020, -1.0231 0.6000, -0.03020, -1.0211 0.6324, -0.04540, -0.7051 0.6667, -0.04880, -0.5471 0.7046, -0.04110, -0.5449 0.7429, -0.03210, -0.5456 0.9311, -0.00120, -0.5990