S809 UNVENTED AILERON, CLEAN, CHORD = 18 IN --------- Run Conditions: vel=103.0 ft/s Re=1.005x10^6 AOA=-6.00 Flap deflection=-10.00 Totals: Cl=-0.7985 Cdp=0.0554 Cm(c/4)=0.0525 Cs=0.0284 Ch=0.1014 Main component: Cl=-0.6873 Cdp=0.0308 Cm=0.1617 Flap component: Cl=-0.1113 Cdp=0.0246 Cm=0.0908 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3162 0.6175, -0.04610, -0.2802 0.5841, -0.02440, -0.2362 0.5775, 0.01750, -0.2300 0.5777, 0.04660, -0.2359 0.6274, 0.07170, 0.3142 0.5694, 0.08320, -0.0742 0.5112, 0.09370, -0.1323 0.4731, 0.09830, -0.1922 0.4349, 0.10070, -0.2180 0.3960, 0.10120, -0.1814 0.3566, 0.10020, -0.1214 0.3172, 0.09790, -0.0721 0.2778, 0.09440, -0.0220 0.2393, 0.08960, 0.0306 0.2056, 0.08360, 0.0879 0.1633, 0.07610, 0.1955 0.1261, 0.06710, 0.3113 0.0900, 0.05640, 0.4760 0.0571, 0.04390, 0.6686 0.0283, 0.02940, 0.9125 0.0142, 0.01970, 1.0166 0.0081, 0.01410, 0.9579 0.0026, 0.00780, 0.5459 0.0000, 0.00000, -1.2083 0.0037, -0.00840, -2.1994 0.0112, -0.01420, -1.7647 0.0191, -0.01930, -1.5950 0.0397, -0.03030, -1.0228 0.0706, -0.04420, -1.0397 0.1037, -0.05710, -1.0681 0.1384, -0.06890, -1.0955 0.1741, -0.07950, -1.1255 0.2102, -0.08660, -1.2167 0.2472, -0.09640, -1.2971 0.2844, -0.10270, -1.3132 0.3225, -0.10690, -1.3046 0.3608, -0.10890, -1.2867 0.3991, -0.10830, -1.1863 0.4373, -0.10510, -1.0467 0.4757, -0.09890, -0.7763 0.5137, -0.09070, -0.5643 0.5694, -0.07640, -0.3581 15 Flap element taps 1.0000, 0.00130, -0.2572 0.9365, 0.01390, -0.0536 0.8333, 0.03280, 0.0487 0.7436, 0.04930, 0.1370 0.7049, 0.05670, 0.2143 0.6662, 0.06410, 0.1279 0.6522, 0.01390, -0.2263 0.5969, -0.00020, -0.2545 0.6000, -0.03020, -0.2927 0.6324, -0.04540, -0.2839 0.6667, -0.04880, -0.2747 0.7046, -0.04110, -0.2753 0.7429, -0.03210, -0.2848 0.8333, -0.01400, -0.2969 0.9311, -0.00120, -0.3060 --------- Run Conditions: vel=102.4 ft/s Re=1.001x10^6 AOA=0.01 Flap deflection=-10.00 Totals: Cl=-0.5284 Cdp=0.0249 Cm(c/4)=0.0724 Cs=-0.0250 Ch=0.0681 Main component: Cl=-0.4435 Cdp=0.0296 Cm=0.1385 Flap component: Cl=-0.0849 Cdp=-0.0046 Cm=0.0660 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3755 0.6175, -0.04610, -0.2787 0.5841, -0.02440, -0.2217 0.5775, 0.01750, -0.2202 0.5777, 0.04660, -0.2247 0.6274, 0.07170, 0.2757 0.5694, 0.08320, 0.0730 0.5112, 0.09370, -0.2665 0.4731, 0.09830, -0.2918 0.4349, 0.10070, -0.3534 0.3960, 0.10120, -0.3748 0.3566, 0.10020, -0.3114 0.3172, 0.09790, -0.2917 0.2778, 0.09440, -0.2668 0.2393, 0.08960, -0.2490 0.2056, 0.08360, -0.2470 0.1633, 0.07610, -0.1420 0.1261, 0.06710, -0.0766 0.0900, 0.05640, 0.0634 0.0571, 0.04390, 0.2179 0.0283, 0.02940, 0.4824 0.0142, 0.01970, 0.7351 0.0081, 0.01410, 0.8404 0.0026, 0.00780, 1.0057 0.0000, 0.00000, 0.7429 0.0037, -0.00840, -0.0767 0.0112, -0.01420, -0.2298 0.0191, -0.01930, -0.2533 0.0397, -0.03030, -0.2975 0.0706, -0.04420, -0.4298 0.1037, -0.05710, -0.5579 0.1384, -0.06890, -0.6340 0.1741, -0.07950, -0.7445 0.2102, -0.08660, -0.9178 0.2472, -0.09640, -1.0385 0.2844, -0.10270, -1.1318 0.3225, -0.10690, -1.1735 0.3608, -0.10890, -1.2425 0.3991, -0.10830, -1.2140 0.4373, -0.10510, -1.1670 0.4757, -0.09890, -1.0876 0.5137, -0.09070, -1.0218 0.5694, -0.07640, -0.5247 15 Flap element taps 1.0000, 0.00130, 0.0200 0.9365, 0.01390, 0.0833 0.8333, 0.03280, 0.1003 0.7436, 0.04930, 0.1477 0.7049, 0.05670, 0.2048 0.6662, 0.06410, 0.1176 0.6522, 0.01390, -0.2203 0.5969, -0.00020, -0.2401 0.6000, -0.03020, -0.3031 0.6324, -0.04540, -0.2959 0.6667, -0.04880, -0.3200 0.7046, -0.04110, -0.1946 0.7429, -0.03210, -0.1563 0.8333, -0.01400, -0.1225 0.9311, -0.00120, -0.0460 Wake drag found for this condition, Cdw=0.0239 --------- Run Conditions: vel=102.7 ft/s Re=1.005x10^6 AOA=3.04 Flap deflection=-10.00 Totals: Cl=-0.2370 Cdp=0.0174 Cm(c/4)=0.0705 Cs=-0.0299 Ch=0.0491 Main component: Cl=-0.1677 Cdp=0.0352 Cm=0.0767 Flap component: Cl=-0.0692 Cdp=-0.0179 Cm=0.0527 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3728 0.6175, -0.04610, -0.3125 0.5841, -0.02440, -0.2589 0.5775, 0.01750, -0.2552 0.5777, 0.04660, -0.2644 0.6274, 0.07170, 0.2430 0.5694, 0.08320, 0.0540 0.5112, 0.09370, -0.3947 0.4731, 0.09830, -0.4117 0.4349, 0.10070, -0.4752 0.3960, 0.10120, -0.5389 0.3566, 0.10020, -0.4684 0.3172, 0.09790, -0.4637 0.2778, 0.09440, -0.4576 0.2393, 0.08960, -0.4633 0.2056, 0.08360, -0.5074 0.1633, 0.07610, -0.4033 0.1261, 0.06710, -0.3846 0.0900, 0.05640, -0.2765 0.0571, 0.04390, -0.1842 0.0283, 0.02940, 0.0162 0.0142, 0.01970, 0.2502 0.0081, 0.01410, 0.3693 0.0026, 0.00780, 0.7155 0.0000, 0.00000, 1.0279 0.0037, -0.00840, 0.7361 0.0112, -0.01420, 0.4728 0.0191, -0.01930, 0.3518 0.0397, -0.03030, 0.1806 0.0706, -0.04420, -0.0345 0.1037, -0.05710, -0.2066 0.1384, -0.06890, -0.2953 0.1741, -0.07950, -0.4319 0.2102, -0.08660, -0.6434 0.2472, -0.09640, -0.7680 0.2844, -0.10270, -0.8937 0.3225, -0.10690, -0.9380 0.3608, -0.10890, -1.0424 0.3991, -0.10830, -1.0334 0.4373, -0.10510, -1.0273 0.4757, -0.09890, -0.9273 0.5137, -0.09070, -0.9114 0.5694, -0.07640, -0.4634 15 Flap element taps 1.0000, 0.00130, 0.1101 0.9365, 0.01390, 0.1131 0.8333, 0.03280, 0.0924 0.7436, 0.04930, 0.1237 0.7049, 0.05670, 0.1741 0.6662, 0.06410, 0.0651 0.6522, 0.01390, -0.2630 0.5969, -0.00020, -0.2734 0.6000, -0.03020, -0.3437 0.6324, -0.04540, -0.3367 0.6667, -0.04880, -0.3856 0.7046, -0.04110, -0.2141 0.7429, -0.03210, -0.1384 0.8333, -0.01400, -0.0564 0.9311, -0.00120, 0.0629 Wake drag found for this condition, Cdw=0.0195 --------- Run Conditions: vel=102.4 ft/s Re=1.005x10^6 AOA=6.02 Flap deflection=-10.00 Totals: Cl=0.0830 Cdp=0.0130 Cm(c/4)=0.0610 Cs=-0.0042 Ch=0.0235 Main component: Cl=0.1279 Cdp=0.0403 Cm=0.0066 Flap component: Cl=-0.0449 Cdp=-0.0273 Cm=0.0335 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3337 0.6175, -0.04610, -0.3104 0.5841, -0.02440, -0.2671 0.5775, 0.01750, -0.2650 0.5777, 0.04660, -0.2723 0.6274, 0.07170, 0.1949 0.5694, 0.08320, -0.0270 0.5112, 0.09370, -0.5399 0.4731, 0.09830, -0.5630 0.4349, 0.10070, -0.6232 0.3960, 0.10120, -0.7161 0.3566, 0.10020, -0.6370 0.3172, 0.09790, -0.6518 0.2778, 0.09440, -0.6636 0.2393, 0.08960, -0.6967 0.2056, 0.08360, -0.7889 0.1633, 0.07610, -0.6939 0.1261, 0.06710, -0.7288 0.0900, 0.05640, -0.6698 0.0571, 0.04390, -0.6701 0.0283, 0.02940, -0.6002 0.0142, 0.01970, -0.4777 0.0081, 0.01410, -0.4425 0.0026, 0.00780, -0.0782 0.0000, 0.00000, 0.5475 0.0037, -0.00840, 1.0235 0.0112, -0.01420, 0.8881 0.0191, -0.01930, 0.7657 0.0397, -0.03030, 0.5583 0.0706, -0.04420, 0.3016 0.1037, -0.05710, 0.1092 0.1384, -0.06890, 0.0254 0.1741, -0.07950, -0.1312 0.2102, -0.08660, -0.3770 0.2472, -0.09640, -0.5003 0.2844, -0.10270, -0.6495 0.3225, -0.10690, -0.6951 0.3608, -0.10890, -0.8289 0.3991, -0.10830, -0.8328 0.4373, -0.10510, -0.8705 0.4757, -0.09890, -0.7687 0.5137, -0.09070, -0.7323 0.5694, -0.07640, -0.3704 15 Flap element taps 1.0000, 0.00130, 0.1764 0.9365, 0.01390, 0.1305 0.8333, 0.03280, 0.0790 0.7436, 0.04930, 0.0946 0.7049, 0.05670, 0.1369 0.6662, 0.06410, 0.0032 0.6522, 0.01390, -0.2776 0.5969, -0.00020, -0.2748 0.6000, -0.03020, -0.3424 0.6324, -0.04540, -0.3420 0.6667, -0.04880, -0.4063 0.7046, -0.04110, -0.2176 0.7429, -0.03210, -0.1065 0.8333, -0.01400, 0.0272 0.9311, -0.00120, 0.1738 Wake drag found for this condition, Cdw=0.0135 --------- Run Conditions: vel=102.5 ft/s Re=1.008x10^6 AOA=8.97 Flap deflection=-10.00 Totals: Cl=0.3854 Cdp=0.0134 Cm(c/4)=0.0572 Cs=0.0469 Ch=0.0003 Main component: Cl=0.4029 Cdp=0.0434 Cm=-0.0513 Flap component: Cl=-0.0174 Cdp=-0.0300 Cm=0.0128 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2642 0.6175, -0.04610, -0.2783 0.5841, -0.02440, -0.2535 0.5775, 0.01750, -0.2520 0.5777, 0.04660, -0.2638 0.6274, 0.07170, 0.0475 0.5694, 0.08320, -0.1239 0.5112, 0.09370, -0.4646 0.4731, 0.09830, -0.6446 0.4349, 0.10070, -0.7483 0.3960, 0.10120, -0.8573 0.3566, 0.10020, -0.7776 0.3172, 0.09790, -0.8232 0.2778, 0.09440, -0.8750 0.2393, 0.08960, -0.9422 0.2056, 0.08360, -1.0820 0.1633, 0.07610, -1.0079 0.1261, 0.06710, -1.1064 0.0900, 0.05640, -1.1122 0.0571, 0.04390, -1.2381 0.0283, 0.02940, -1.3661 0.0142, 0.01970, -1.4482 0.0081, 0.01410, -1.6147 0.0026, 0.00780, -1.3602 0.0000, 0.00000, -0.8846 0.0037, -0.00840, 0.8662 0.0112, -0.01420, 1.0189 0.0191, -0.01930, 0.9837 0.0397, -0.03030, 0.8313 0.0706, -0.04420, 0.5794 0.1037, -0.05710, 0.3850 0.1384, -0.06890, 0.3107 0.1741, -0.07950, 0.1471 0.2102, -0.08660, -0.1220 0.2472, -0.09640, -0.2380 0.2844, -0.10270, -0.4061 0.3225, -0.10690, -0.4483 0.3608, -0.10890, -0.6048 0.3991, -0.10830, -0.6222 0.4373, -0.10510, -0.6950 0.4757, -0.09890, -0.6114 0.5137, -0.09070, -0.5753 0.5694, -0.07640, -0.4350 15 Flap element taps 1.0000, 0.00130, 0.1964 0.9365, 0.01390, 0.1355 0.8333, 0.03280, 0.0592 0.7436, 0.04930, 0.0553 0.7049, 0.05670, 0.0644 0.6662, 0.06410, -0.0007 0.6522, 0.01390, -0.2721 0.5969, -0.00020, -0.2557 0.6000, -0.03020, -0.3046 0.6324, -0.04540, -0.3176 0.6667, -0.04880, -0.3621 0.7046, -0.04110, -0.1761 0.7429, -0.03210, -0.0574 0.8333, -0.01400, 0.0964 0.9311, -0.00120, 0.2389 Wake drag found for this condition, Cdw=0.0111 --------- Run Conditions: vel=102.4 ft/s Re=1.009x10^6 AOA=12.01 Flap deflection=-10.00 Totals: Cl=0.6855 Cdp=0.0169 Cm(c/4)=0.0429 Cs=0.1261 Ch=-0.0301 Main component: Cl=0.6557 Cdp=0.0478 Cm=-0.1039 Flap component: Cl=0.0298 Cdp=-0.0309 Cm=-0.0217 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2078 0.6175, -0.04610, -0.2645 0.5841, -0.02440, -0.2667 0.5775, 0.01750, -0.2659 0.5777, 0.04660, -0.2787 0.6274, 0.07170, -0.1805 0.5694, 0.08320, -0.1802 0.5112, 0.09370, -0.4108 0.4731, 0.09830, -0.6217 0.4349, 0.10070, -0.7815 0.3960, 0.10120, -0.9629 0.3566, 0.10020, -0.9038 0.3172, 0.09790, -0.9660 0.2778, 0.09440, -1.0265 0.2393, 0.08960, -1.1352 0.2056, 0.08360, -1.3333 0.1633, 0.07610, -1.2894 0.1261, 0.06710, -1.4557 0.0900, 0.05640, -1.5461 0.0571, 0.04390, -1.8043 0.0283, 0.02940, -2.2063 0.0142, 0.01970, -2.6578 0.0081, 0.01410, -3.1166 0.0026, 0.00780, -3.2284 0.0000, 0.00000, -3.1623 0.0037, -0.00840, 0.2556 0.0112, -0.01420, 0.9071 0.0191, -0.01930, 1.0142 0.0397, -0.03030, 0.9867 0.0706, -0.04420, 0.7820 0.1037, -0.05710, 0.6049 0.1384, -0.06890, 0.5533 0.1741, -0.07950, 0.3873 0.2102, -0.08660, 0.1037 0.2472, -0.09640, -0.0024 0.2844, -0.10270, -0.1835 0.3225, -0.10690, -0.2209 0.3608, -0.10890, -0.3950 0.3991, -0.10830, -0.4200 0.4373, -0.10510, -0.5288 0.4757, -0.09890, -0.4698 0.5137, -0.09070, -0.4578 0.5694, -0.07640, -0.3226 15 Flap element taps 1.0000, 0.00130, 0.1582 0.9365, 0.01390, 0.1139 0.8333, 0.03280, 0.0067 0.7436, 0.04930, -0.0790 0.7049, 0.05670, -0.1348 0.6662, 0.06410, -0.1749 0.6522, 0.01390, -0.2906 0.5969, -0.00020, -0.2603 0.6000, -0.03020, -0.2826 0.6324, -0.04540, -0.3100 0.6667, -0.04880, -0.2632 0.7046, -0.04110, -0.1180 0.7429, -0.03210, -0.0033 0.8333, -0.01400, 0.1413 0.9311, -0.00120, 0.2744 Wake drag found for this condition, Cdw=0.0156 --------- Run Conditions: vel=102.1 ft/s Re=1.007x10^6 AOA=15.00 Flap deflection=-10.00 Totals: Cl=0.8510 Cdp=0.0455 Cm(c/4)=0.0128 Cs=0.1763 Ch=-0.1029 Main component: Cl=0.7482 Cdp=0.0616 Cm=-0.1147 Flap component: Cl=0.1028 Cdp=-0.0161 Cm=-0.0810 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2470 0.6175, -0.04610, -0.3179 0.5841, -0.02440, -0.3335 0.5775, 0.01750, -0.3351 0.5777, 0.04660, -0.3485 0.6274, 0.07170, -0.3452 0.5694, 0.08320, -0.2926 0.5112, 0.09370, -0.3483 0.4731, 0.09830, -0.4081 0.4349, 0.10070, -0.5462 0.3960, 0.10120, -0.8029 0.3566, 0.10020, -0.7856 0.3172, 0.09790, -0.8993 0.2778, 0.09440, -0.9944 0.2393, 0.08960, -1.1446 0.2056, 0.08360, -1.4010 0.1633, 0.07610, -1.3835 0.1261, 0.06710, -1.6185 0.0900, 0.05640, -1.7772 0.0571, 0.04390, -2.1684 0.0283, 0.02940, -2.7272 0.0142, 0.01970, -3.3478 0.0081, 0.01410, -4.4630 0.0026, 0.00780, -4.7847 0.0000, 0.00000, -5.1353 0.0037, -0.00840, -0.4135 0.0112, -0.01420, 0.6870 0.0191, -0.01930, 0.9431 0.0397, -0.03030, 1.0363 0.0706, -0.04420, 0.8837 0.1037, -0.05710, 0.7269 0.1384, -0.06890, 0.7019 0.1741, -0.07950, 0.5405 0.2102, -0.08660, 0.2384 0.2472, -0.09640, 0.1427 0.2844, -0.10270, -0.0529 0.3225, -0.10690, -0.0847 0.3608, -0.10890, -0.2779 0.3991, -0.10830, -0.3105 0.4373, -0.10510, -0.4462 0.4757, -0.09890, -0.4061 0.5137, -0.09070, -0.4249 0.5694, -0.07640, -0.2720 15 Flap element taps 1.0000, 0.00130, -0.0427 0.9365, 0.01390, -0.1613 0.8333, 0.03280, -0.2807 0.7436, 0.04930, -0.3241 0.7049, 0.05670, -0.3566 0.6662, 0.06410, -0.3632 0.6522, 0.01390, -0.3636 0.5969, -0.00020, -0.3246 0.6000, -0.03020, -0.3368 0.6324, -0.04540, -0.3719 0.6667, -0.04880, -0.2609 0.7046, -0.04110, -0.1097 0.7429, -0.03210, -0.0113 0.8333, -0.01400, 0.1081 0.9311, -0.00120, 0.2151 --------- Run Conditions: vel=101.5 ft/s Re=1.002x10^6 AOA=17.98 Flap deflection=-10.00 Totals: Cl=0.8044 Cdp=0.1016 Cm(c/4)=-0.0134 Cs=0.1517 Ch=-0.1505 Main component: Cl=0.6600 Cdp=0.0993 Cm=-0.0959 Flap component: Cl=0.1444 Cdp=0.0023 Cm=-0.1166 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3172 0.6175, -0.04610, -0.4207 0.5841, -0.02440, -0.4417 0.5775, 0.01750, -0.4429 0.5777, 0.04660, -0.4563 0.6274, 0.07170, -0.5153 0.5694, 0.08320, -0.4491 0.5112, 0.09370, -0.4930 0.4731, 0.09830, -0.4814 0.4349, 0.10070, -0.4848 0.3960, 0.10120, -0.6257 0.3566, 0.10020, -0.4658 0.3172, 0.09790, -0.5007 0.2778, 0.09440, -0.5547 0.2393, 0.08960, -0.7352 0.2056, 0.08360, -1.0769 0.1633, 0.07610, -1.1088 0.1261, 0.06710, -1.4211 0.0900, 0.05640, -1.6258 0.0571, 0.04390, -2.0898 0.0283, 0.02940, -2.7460 0.0142, 0.01970, -3.4233 0.0081, 0.01410, -4.7680 0.0026, 0.00780, -5.2357 0.0000, 0.00000, -5.7825 0.0037, -0.00840, -0.6903 0.0112, -0.01420, 0.5766 0.0191, -0.01930, 0.8928 0.0397, -0.03030, 1.0424 0.0706, -0.04420, 0.9125 0.1037, -0.05710, 0.7651 0.1384, -0.06890, 0.7616 0.1741, -0.07950, 0.6002 0.2102, -0.08660, 0.2759 0.2472, -0.09640, 0.1866 0.2844, -0.10270, -0.0242 0.3225, -0.10690, -0.0496 0.3608, -0.10890, -0.2638 0.3991, -0.10830, -0.3007 0.4373, -0.10510, -0.4619 0.4757, -0.09890, -0.4356 0.5137, -0.09070, -0.4743 0.5694, -0.07640, -0.3191 15 Flap element taps 1.0000, 0.00130, -0.3661 0.9365, 0.01390, -0.4727 0.8333, 0.03280, -0.5375 0.7436, 0.04930, -0.5323 0.7049, 0.05670, -0.5466 0.6662, 0.06410, -0.5449 0.6522, 0.01390, -0.4770 0.5969, -0.00020, -0.4322 0.6000, -0.03020, -0.4413 0.6324, -0.04540, -0.4811 0.6667, -0.04880, -0.3660 0.7046, -0.04110, -0.1854 0.7429, -0.03210, -0.0978 0.8333, -0.01400, -0.0001 0.9311, -0.00120, 0.0724 --------- Run Conditions: vel=100.8 ft/s Re=0.997x10^6 AOA=19.99 Flap deflection=-10.00 Totals: Cl=0.3824 Cdp=0.2212 Cm(c/4)=-0.0305 Cs=-0.0771 Ch=-0.1253 Main component: Cl=0.2711 Cdp=0.2222 Cm=-0.0489 Flap component: Cl=0.1113 Cdp=-0.0010 Cm=-0.0903 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5084 0.6175, -0.04610, -0.5998 0.5841, -0.02440, -0.6175 0.5775, 0.01750, -0.6164 0.5777, 0.04660, -0.6327 0.6274, 0.07170, -0.5814 0.5694, 0.08320, -0.5260 0.5112, 0.09370, -0.5910 0.4731, 0.09830, -0.5957 0.4349, 0.10070, -0.6116 0.3960, 0.10120, -0.7747 0.3566, 0.10020, -0.5883 0.3172, 0.09790, -0.5992 0.2778, 0.09440, -0.5672 0.2393, 0.08960, -0.5919 0.2056, 0.08360, -0.7520 0.1633, 0.07610, -0.5489 0.1261, 0.06710, -0.6548 0.0900, 0.05640, -0.5532 0.0571, 0.04390, -0.6083 0.0283, 0.02940, -0.6226 0.0142, 0.01970, -0.6215 0.0081, 0.01410, -0.7782 0.0026, 0.00780, -0.5919 0.0000, 0.00000, -0.8260 0.0037, -0.00840, 0.6741 0.0112, -0.01420, 0.9823 0.0191, -0.01930, 1.0223 0.0397, -0.03030, 0.9826 0.0706, -0.04420, 0.7746 0.1037, -0.05710, 0.6004 0.1384, -0.06890, 0.6071 0.1741, -0.07950, 0.4311 0.2102, -0.08660, 0.0817 0.2472, -0.09640, -0.0086 0.2844, -0.10270, -0.2346 0.3225, -0.10690, -0.2540 0.3608, -0.10890, -0.4856 0.3991, -0.10830, -0.5213 0.4373, -0.10510, -0.6961 0.4757, -0.09890, -0.6575 0.5137, -0.09070, -0.6969 0.5694, -0.07640, -0.5200 15 Flap element taps 1.0000, 0.00130, -0.5019 0.9365, 0.01390, -0.5718 0.8333, 0.03280, -0.6236 0.7436, 0.04930, -0.6024 0.7049, 0.05670, -0.6115 0.6662, 0.06410, -0.6009 0.6522, 0.01390, -0.6554 0.5969, -0.00020, -0.6057 0.6000, -0.03020, -0.6263 0.6324, -0.04540, -0.6680 0.6667, -0.04880, -0.6822 0.7046, -0.04110, -0.3863 0.7429, -0.03210, -0.2821 0.8333, -0.01400, -0.1704 0.9311, -0.00120, -0.0817 --------- Run Conditions: vel=101.1 ft/s Re=1.003x10^6 AOA=23.98 Flap deflection=-10.00 Totals: Cl=0.4602 Cdp=0.2933 Cm(c/4)=-0.0467 Cs=-0.0809 Ch=-0.1388 Main component: Cl=0.3307 Cdp=0.2812 Cm=-0.0765 Flap component: Cl=0.1295 Cdp=0.0121 Cm=-0.1050 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4979 0.6175, -0.04610, -0.6245 0.5841, -0.02440, -0.6491 0.5775, 0.01750, -0.6499 0.5777, 0.04660, -0.6669 0.6274, 0.07170, -0.6610 0.5694, 0.08320, -0.6004 0.5112, 0.09370, -0.6689 0.4731, 0.09830, -0.6747 0.4349, 0.10070, -0.6852 0.3960, 0.10120, -0.8634 0.3566, 0.10020, -0.6530 0.3172, 0.09790, -0.6585 0.2778, 0.09440, -0.6196 0.2393, 0.08960, -0.6421 0.2056, 0.08360, -0.8134 0.1633, 0.07610, -0.5901 0.1261, 0.06710, -0.7066 0.0900, 0.05640, -0.5954 0.0571, 0.04390, -0.6520 0.0283, 0.02940, -0.6527 0.0142, 0.01970, -0.6572 0.0081, 0.01410, -0.8255 0.0026, 0.00780, -0.6222 0.0000, 0.00000, -0.8529 0.0037, -0.00840, 0.5132 0.0112, -0.01420, 0.9193 0.0191, -0.01930, 1.0071 0.0397, -0.03030, 1.0211 0.0706, -0.04420, 0.8451 0.1037, -0.05710, 0.6903 0.1384, -0.06890, 0.7248 0.1741, -0.07950, 0.5526 0.2102, -0.08660, 0.1900 0.2472, -0.09640, 0.1160 0.2844, -0.10270, -0.1210 0.3225, -0.10690, -0.1318 0.3608, -0.10890, -0.3793 0.3991, -0.10830, -0.4157 0.4373, -0.10510, -0.6144 0.4757, -0.09890, -0.5934 0.5137, -0.09070, -0.6534 0.5694, -0.07640, -0.4837 15 Flap element taps 1.0000, 0.00130, -0.5904 0.9365, 0.01390, -0.6434 0.8333, 0.03280, -0.6952 0.7436, 0.04930, -0.6813 0.7049, 0.05670, -0.6923 0.6662, 0.06410, -0.6856 0.6522, 0.01390, -0.6931 0.5969, -0.00020, -0.6375 0.6000, -0.03020, -0.6536 0.6324, -0.04540, -0.6988 0.6667, -0.04880, -0.6163 0.7046, -0.04110, -0.3869 0.7429, -0.03210, -0.2966 0.8333, -0.01400, -0.1996 0.9311, -0.00120, -0.1201 --------- Run Conditions: vel=101.5 ft/s Re=1.008x10^6 AOA=27.01 Flap deflection=-10.00 Totals: Cl=0.5827 Cdp=0.3824 Cm(c/4)=-0.0754 Cs=-0.0761 Ch=-0.1658 Main component: Cl=0.4156 Cdp=0.3518 Cm=-0.1131 Flap component: Cl=0.1671 Cdp=0.0306 Cm=-0.1356 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4734 0.6175, -0.04610, -0.6609 0.5841, -0.02440, -0.6896 0.5775, 0.01750, -0.6873 0.5777, 0.04660, -0.7050 0.6274, 0.07170, -0.7698 0.5694, 0.08320, -0.7035 0.5112, 0.09370, -0.7768 0.4731, 0.09830, -0.7825 0.4349, 0.10070, -0.7925 0.3960, 0.10120, -0.9818 0.3566, 0.10020, -0.7586 0.3172, 0.09790, -0.7640 0.2778, 0.09440, -0.7191 0.2393, 0.08960, -0.7435 0.2056, 0.08360, -0.9267 0.1633, 0.07610, -0.6847 0.1261, 0.06710, -0.8087 0.0900, 0.05640, -0.6892 0.0571, 0.04390, -0.7469 0.0283, 0.02940, -0.7413 0.0142, 0.01970, -0.7431 0.0081, 0.01410, -0.9240 0.0026, 0.00780, -0.7147 0.0000, 0.00000, -0.7653 0.0037, -0.00840, 0.3158 0.0112, -0.01420, 0.8273 0.0191, -0.01930, 0.9699 0.0397, -0.03030, 1.0441 0.0706, -0.04420, 0.9050 0.1037, -0.05710, 0.7694 0.1384, -0.06890, 0.8309 0.1741, -0.07950, 0.6693 0.2102, -0.08660, 0.2993 0.2472, -0.09640, 0.2377 0.2844, -0.10270, -0.0046 0.3225, -0.10690, -0.0042 0.3608, -0.10890, -0.2606 0.3991, -0.10830, -0.2985 0.4373, -0.10510, -0.5158 0.4757, -0.09890, -0.5110 0.5137, -0.09070, -0.5911 0.5694, -0.07640, -0.4365 15 Flap element taps 1.0000, 0.00130, -0.6841 0.9365, 0.01390, -0.7399 0.8333, 0.03280, -0.7968 0.7436, 0.04930, -0.7866 0.7049, 0.05670, -0.8018 0.6662, 0.06410, -0.7970 0.6522, 0.01390, -0.7357 0.5969, -0.00020, -0.6741 0.6000, -0.03020, -0.6887 0.6324, -0.04540, -0.7389 0.6667, -0.04880, -0.3173 0.7046, -0.04110, -0.3775 0.7429, -0.03210, -0.2914 0.8333, -0.01400, -0.2121 0.9311, -0.00120, -0.1455