S809 UNVENTED AILERON, CLEAN, CHORD = 18 IN --------- Run Conditions: vel=211.5 ft/s Re=1.993x10^6 AOA=-6.02 Flap deflection=5.00 Totals: Cl=-0.2839 Cdp=0.0033 Cm(c/4)=-0.0649 Cs=0.0265 Ch=-0.0724 Main component: Cl=-0.3687 Cdp=0.0240 Cm=0.0744 Flap component: Cl=0.0848 Cdp=-0.0207 Cm=-0.0687 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.0920 0.6175, -0.04610, -0.0178 0.5841, -0.02440, -0.0254 0.5775, 0.01750, -0.0249 0.5777, 0.04660, -0.0226 0.6274, 0.07170, -0.2398 0.5694, 0.08320, -0.3598 0.5112, 0.09370, -0.5493 0.4731, 0.09830, -0.6132 0.4349, 0.10070, -0.5973 0.3960, 0.10120, -0.5106 0.3566, 0.10020, -0.4488 0.3172, 0.09790, -0.3742 0.2778, 0.09440, -0.3209 0.2393, 0.08960, -0.2625 0.2056, 0.08360, -0.1806 0.1633, 0.07610, -0.0833 0.1261, 0.06710, 0.0503 0.0900, 0.05640, 0.1991 0.0571, 0.04390, 0.4147 0.0283, 0.02940, 0.6970 0.0142, 0.01970, 0.9202 0.0081, 0.01410, 1.0024 0.0026, 0.00780, 0.8908 0.0000, 0.00000, 0.0819 0.0037, -0.00840, -0.9281 0.0112, -0.01420, -0.8559 0.0191, -0.01930, -0.7542 0.0397, -0.03030, -0.6472 0.0706, -0.04420, -0.6604 0.1037, -0.05710, -0.7365 0.1384, -0.06890, -0.8081 0.1741, -0.07950, -0.8750 0.2102, -0.08660, -0.9469 0.2472, -0.09640, -1.0437 0.2844, -0.10270, -1.0767 0.3225, -0.10690, -1.1157 0.3608, -0.10890, -1.1138 0.3991, -0.10830, -1.0693 0.4373, -0.10510, -0.9867 0.4757, -0.09890, -0.7708 0.5137, -0.09070, -0.5203 0.5694, -0.07640, -0.2596 15 Flap element taps 1.0000, 0.00130, 0.1963 0.9365, 0.01390, 0.0981 0.8333, 0.03280, -0.0221 0.7436, 0.04930, -0.1321 0.7049, 0.05670, -0.1725 0.6662, 0.06410, -0.3131 0.6522, 0.01390, -0.0251 0.5969, -0.00020, -0.0285 0.6000, -0.03020, -0.0248 0.6324, -0.04540, -0.0194 0.6667, -0.04880, -0.0860 0.7046, -0.04110, 0.2138 0.7429, -0.03210, 0.2035 0.8333, -0.01400, 0.2545 0.9311, -0.00120, 0.2956 Wake drag found for this condition, Cdw=0.0087 --------- Run Conditions: vel=212.5 ft/s Re=1.997x10^6 AOA=0.00 Flap deflection=5.00 Totals: Cl=0.4022 Cdp=-0.0037 Cm(c/4)=-0.0776 Cs=0.0037 Ch=-0.1081 Main component: Cl=0.2649 Cdp=0.0002 Cm=-0.0711 Flap component: Cl=0.1373 Cdp=-0.0039 Cm=-0.1071 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0111 0.6175, -0.04610, 0.0681 0.5841, -0.02440, 0.0486 0.5775, 0.01750, 0.0464 0.5777, 0.04660, 0.0596 0.6274, 0.07170, -0.4135 0.5694, 0.08320, -0.4984 0.5112, 0.09370, -0.8599 0.4731, 0.09830, -0.9387 0.4349, 0.10070, -0.9674 0.3960, 0.10120, -0.9069 0.3566, 0.10020, -0.8764 0.3172, 0.09790, -0.8311 0.2778, 0.09440, -0.8188 0.2393, 0.08960, -0.8057 0.2056, 0.08360, -0.7699 0.1633, 0.07610, -0.7314 0.1261, 0.06710, -0.6567 0.0900, 0.05640, -0.5949 0.0571, 0.04390, -0.4864 0.0283, 0.02940, -0.3221 0.0142, 0.01970, -0.0986 0.0081, 0.01410, 0.0802 0.0026, 0.00780, 0.3550 0.0000, 0.00000, 0.8909 0.0037, -0.00840, 0.9265 0.0112, -0.01420, 0.7058 0.0191, -0.01930, 0.5756 0.0397, -0.03030, 0.3788 0.0706, -0.04420, 0.1863 0.1037, -0.05710, 0.0225 0.1384, -0.06890, -0.1202 0.1741, -0.07950, -0.2379 0.2102, -0.08660, -0.3486 0.2472, -0.09640, -0.4803 0.2844, -0.10270, -0.5534 0.3225, -0.10690, -0.6317 0.3608, -0.10890, -0.6718 0.3991, -0.10830, -0.6758 0.4373, -0.10510, -0.6137 0.4757, -0.09890, -0.5463 0.5137, -0.09070, -0.2742 0.5694, -0.07640, -0.1030 15 Flap element taps 1.0000, 0.00130, 0.1845 0.9365, 0.01390, 0.0687 0.8333, 0.03280, -0.0926 0.7436, 0.04930, -0.2434 0.7049, 0.05670, -0.3030 0.6662, 0.06410, -0.4668 0.6522, 0.01390, 0.0433 0.5969, -0.00020, 0.0361 0.6000, -0.03020, 0.0463 0.6324, -0.04540, 0.0605 0.6667, -0.04880, 0.1897 0.7046, -0.04110, 0.3016 0.7429, -0.03210, 0.2819 0.8333, -0.01400, 0.3097 0.9311, -0.00120, 0.3250 Wake drag found for this condition, Cdw=0.0116 --------- Run Conditions: vel=212.4 ft/s Re=1.992x10^6 AOA=3.03 Flap deflection=5.00 Totals: Cl=0.7441 Cdp=-0.0017 Cm(c/4)=-0.0836 Cs=0.0410 Ch=-0.1220 Main component: Cl=0.5843 Cdp=-0.0088 Cm=-0.1454 Flap component: Cl=0.1598 Cdp=0.0071 Cm=-0.1239 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0711 0.6175, -0.04610, 0.1031 0.5841, -0.02440, 0.0767 0.5775, 0.01750, 0.0733 0.5777, 0.04660, 0.0914 0.6274, 0.07170, -0.4915 0.5694, 0.08320, -0.6289 0.5112, 0.09370, -1.0337 0.4731, 0.09830, -1.0951 0.4349, 0.10070, -1.1436 0.3960, 0.10120, -1.0981 0.3566, 0.10020, -1.0889 0.3172, 0.09790, -1.0642 0.2778, 0.09440, -1.0772 0.2393, 0.08960, -1.0927 0.2056, 0.08360, -1.0882 0.1633, 0.07610, -1.0943 0.1261, 0.06710, -1.0660 0.0900, 0.05640, -1.0783 0.0571, 0.04390, -1.0818 0.0283, 0.02940, -1.0833 0.0142, 0.01970, -1.0287 0.0081, 0.01410, -0.9729 0.0026, 0.00780, -0.7120 0.0000, 0.00000, -0.1380 0.0037, -0.00840, 0.9819 0.0112, -0.01420, 0.9864 0.0191, -0.01930, 0.9019 0.0397, -0.03030, 0.7100 0.0706, -0.04420, 0.5027 0.1037, -0.05710, 0.3282 0.1384, -0.06890, 0.1676 0.1741, -0.07950, 0.0383 0.2102, -0.08660, -0.0800 0.2472, -0.09640, -0.2215 0.2844, -0.10270, -0.3075 0.3225, -0.10690, -0.4025 0.3608, -0.10890, -0.4580 0.3991, -0.10830, -0.4835 0.4373, -0.10510, -0.4446 0.4757, -0.09890, -0.3712 0.5137, -0.09070, -0.1968 0.5694, -0.07640, -0.0197 15 Flap element taps 1.0000, 0.00130, 0.1675 0.9365, 0.01390, 0.0604 0.8333, 0.03280, -0.1130 0.7436, 0.04930, -0.2827 0.7049, 0.05670, -0.3541 0.6662, 0.06410, -0.5299 0.6522, 0.01390, 0.0702 0.5969, -0.00020, 0.0607 0.6000, -0.03020, 0.0741 0.6324, -0.04540, 0.0908 0.6667, -0.04880, 0.3578 0.7046, -0.04110, 0.3449 0.7429, -0.03210, 0.3225 0.8333, -0.01400, 0.3379 0.9311, -0.00120, 0.3378 Wake drag found for this condition, Cdw=0.0145 --------- Run Conditions: vel=212.8 ft/s Re=1.993x10^6 AOA=6.02 Flap deflection=5.00 Totals: Cl=0.9144 Cdp=0.0121 Cm(c/4)=-0.0716 Cs=0.0839 Ch=-0.1245 Main component: Cl=0.7565 Cdp=-0.0070 Cm=-0.1757 Flap component: Cl=0.1579 Cdp=0.0190 Cm=-0.1235 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0863 0.6175, -0.04610, 0.1080 0.5841, -0.02440, 0.0801 0.5775, 0.01750, 0.0777 0.5777, 0.04660, 0.0969 0.6274, 0.07170, -0.5066 0.5694, 0.08320, -0.6719 0.5112, 0.09370, -0.9468 0.4731, 0.09830, -1.1066 0.4349, 0.10070, -1.1717 0.3960, 0.10120, -1.1436 0.3566, 0.10020, -1.1578 0.3172, 0.09790, -1.1515 0.2778, 0.09440, -1.1830 0.2393, 0.08960, -1.2365 0.2056, 0.08360, -1.2637 0.1633, 0.07610, -1.3067 0.1261, 0.06710, -1.3295 0.0900, 0.05640, -1.4407 0.0571, 0.04390, -1.5512 0.0283, 0.02940, -1.7256 0.0142, 0.01970, -1.8672 0.0081, 0.01410, -1.9876 0.0026, 0.00780, -1.9081 0.0000, 0.00000, -1.5507 0.0037, -0.00840, 0.7196 0.0112, -0.01420, 1.0030 0.0191, -0.01930, 1.0013 0.0397, -0.03030, 0.8720 0.0706, -0.04420, 0.6827 0.1037, -0.05710, 0.5118 0.1384, -0.06890, 0.3431 0.1741, -0.07950, 0.2082 0.2102, -0.08660, 0.0871 0.2472, -0.09640, -0.0631 0.2844, -0.10270, -0.1589 0.3225, -0.10690, -0.2684 0.3608, -0.10890, -0.3358 0.3991, -0.10830, -0.3793 0.4373, -0.10510, -0.3578 0.4757, -0.09890, -0.2851 0.5137, -0.09070, -0.2175 0.5694, -0.07640, 0.0087 15 Flap element taps 1.0000, 0.00130, 0.0297 0.9365, 0.01390, -0.0187 0.8333, 0.03280, -0.1169 0.7436, 0.04930, -0.2610 0.7049, 0.05670, -0.3428 0.6662, 0.06410, -0.4922 0.6522, 0.01390, 0.0755 0.5969, -0.00020, 0.0647 0.6000, -0.03020, 0.0790 0.6324, -0.04540, 0.0964 0.6667, -0.04880, 0.3820 0.7046, -0.04110, 0.3476 0.7429, -0.03210, 0.3210 0.8333, -0.01400, 0.3223 0.9311, -0.00120, 0.2926 Wake drag found for this condition, Cdw=0.0251 --------- Run Conditions: vel=211.5 ft/s Re=1.977x10^6 AOA=9.01 Flap deflection=5.00 Totals: Cl=1.0767 Cdp=0.0344 Cm(c/4)=-0.0683 Cs=0.1346 Ch=-0.1589 Main component: Cl=0.9074 Cdp=-0.0087 Cm=-0.1974 Flap component: Cl=0.1693 Cdp=0.0431 Cm=-0.1380 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.1013 0.6175, -0.04610, 0.1149 0.5841, -0.02440, 0.0916 0.5775, 0.01750, 0.0879 0.5777, 0.04660, 0.1070 0.6274, 0.07170, -0.3826 0.5694, 0.08320, -0.5502 0.5112, 0.09370, -0.8433 0.4731, 0.09830, -1.0394 0.4349, 0.10070, -1.1467 0.3960, 0.10120, -1.1547 0.3566, 0.10020, -1.2064 0.3172, 0.09790, -1.2313 0.2778, 0.09440, -1.2953 0.2393, 0.08960, -1.3794 0.2056, 0.08360, -1.4413 0.1633, 0.07610, -1.5391 0.1261, 0.06710, -1.6035 0.0900, 0.05640, -1.7708 0.0571, 0.04390, -1.9966 0.0283, 0.02940, -2.3491 0.0142, 0.01970, -2.7684 0.0081, 0.01410, -3.1466 0.0026, 0.00780, -3.3005 0.0000, 0.00000, -3.4193 0.0037, -0.00840, 0.2084 0.0112, -0.01420, 0.8903 0.0191, -0.01930, 1.0025 0.0397, -0.03030, 0.9696 0.0706, -0.04420, 0.8203 0.1037, -0.05710, 0.6636 0.1384, -0.06890, 0.4939 0.1741, -0.07950, 0.3595 0.2102, -0.08660, 0.2390 0.2472, -0.09640, 0.0830 0.2844, -0.10270, -0.0203 0.3225, -0.10690, -0.1420 0.3608, -0.10890, -0.2195 0.3991, -0.10830, -0.2795 0.4373, -0.10510, -0.2751 0.4757, -0.09890, -0.2107 0.5137, -0.09070, -0.1561 0.5694, -0.07640, 0.0426 15 Flap element taps 1.0000, 0.00130, -0.1476 0.9365, 0.01390, -0.2307 0.8333, 0.03280, -0.2577 0.7436, 0.04930, -0.2702 0.7049, 0.05670, -0.2821 0.6662, 0.06410, -0.3215 0.6522, 0.01390, 0.0874 0.5969, -0.00020, 0.0744 0.6000, -0.03020, 0.0886 0.6324, -0.04540, 0.1066 0.6667, -0.04880, 0.3694 0.7046, -0.04110, 0.3462 0.7429, -0.03210, 0.3138 0.8333, -0.01400, 0.2984 0.9311, -0.00120, 0.2316 --------- Run Conditions: vel=215.0 ft/s Re=2.005x10^6 AOA=12.02 Flap deflection=5.00 Totals: Cl=1.1539 Cdp=0.0622 Cm(c/4)=-0.0655 Cs=0.1795 Ch=-0.1903 Main component: Cl=0.9602 Cdp=-0.0049 Cm=-0.1891 Flap component: Cl=0.1937 Cdp=0.0671 Cm=-0.1618 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0990 0.6175, -0.04610, 0.0989 0.5841, -0.02440, 0.0711 0.5775, 0.01750, 0.0657 0.5777, 0.04660, 0.0866 0.6274, 0.07170, -0.3924 0.5694, 0.08320, -0.4219 0.5112, 0.09370, -0.5545 0.4731, 0.09830, -0.7449 0.4349, 0.10070, -0.9115 0.3960, 0.10120, -0.9839 0.3566, 0.10020, -1.0909 0.3172, 0.09790, -1.1616 0.2778, 0.09440, -1.2650 0.2393, 0.08960, -1.3852 0.2056, 0.08360, -1.4864 0.1633, 0.07610, -1.6358 0.1261, 0.06710, -1.7571 0.0900, 0.05640, -2.0020 0.0571, 0.04390, -2.3458 0.0283, 0.02940, -2.9070 0.0142, 0.01970, -3.4811 0.0081, 0.01410, -4.2419 0.0026, 0.00780, -4.5652 0.0000, 0.00000, -5.3014 0.0037, -0.00840, -0.4036 0.0112, -0.01420, 0.6883 0.0191, -0.01930, 0.9353 0.0397, -0.03030, 1.0079 0.0706, -0.04420, 0.9105 0.1037, -0.05710, 0.7742 0.1384, -0.06890, 0.6098 0.1741, -0.07950, 0.4770 0.2102, -0.08660, 0.3582 0.2472, -0.09640, 0.1990 0.2844, -0.10270, 0.0903 0.3225, -0.10690, -0.0421 0.3608, -0.10890, -0.1297 0.3991, -0.10830, -0.2046 0.4373, -0.10510, -0.2149 0.4757, -0.09890, -0.1629 0.5137, -0.09070, -0.1155 0.5694, -0.07640, 0.0612 15 Flap element taps 1.0000, 0.00130, -0.3170 0.9365, 0.01390, -0.4006 0.8333, 0.03280, -0.3862 0.7436, 0.04930, -0.3858 0.7049, 0.05670, -0.3798 0.6662, 0.06410, -0.3800 0.6522, 0.01390, 0.0661 0.5969, -0.00020, 0.0524 0.6000, -0.03020, 0.0683 0.6324, -0.04540, 0.0872 0.6667, -0.04880, 0.4056 0.7046, -0.04110, 0.3358 0.7429, -0.03210, 0.2980 0.8333, -0.01400, 0.2639 0.9311, -0.00120, 0.1639 --------- Run Conditions: vel=215.8 ft/s Re=2.007x10^6 AOA=14.99 Flap deflection=5.00 Totals: Cl=1.1884 Cdp=0.0933 Cm(c/4)=-0.0637 Cs=0.2172 Ch=-0.2089 Main component: Cl=0.9795 Cdp=0.0057 Cm=-0.1786 Flap component: Cl=0.2089 Cdp=0.0877 Cm=-0.1782 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.1011 0.6175, -0.04610, 0.0820 0.5841, -0.02440, 0.0513 0.5775, 0.01750, 0.0500 0.5777, 0.04660, 0.0738 0.6274, 0.07170, -0.4516 0.5694, 0.08320, -0.4593 0.5112, 0.09370, -0.4574 0.4731, 0.09830, -0.4901 0.4349, 0.10070, -0.5822 0.3960, 0.10120, -0.6909 0.3566, 0.10020, -0.8645 0.3172, 0.09790, -0.9963 0.2778, 0.09440, -1.1494 0.2393, 0.08960, -1.3106 0.2056, 0.08360, -1.4549 0.1633, 0.07610, -1.6562 0.1261, 0.06710, -1.8335 0.0900, 0.05640, -2.1488 0.0571, 0.04390, -2.6003 0.0283, 0.02940, -3.3481 0.0142, 0.01970, -4.1532 0.0081, 0.01410, -5.0196 0.0026, 0.00780, -5.7274 0.0000, 0.00000, -7.1513 0.0037, -0.00840, -1.0443 0.0112, -0.01420, 0.4432 0.0191, -0.01930, 0.8256 0.0397, -0.03030, 1.0090 0.0706, -0.04420, 0.9640 0.1037, -0.05710, 0.8520 0.1384, -0.06890, 0.6951 0.1741, -0.07950, 0.5680 0.2102, -0.08660, 0.4545 0.2472, -0.09640, 0.2939 0.2844, -0.10270, 0.1816 0.3225, -0.10690, 0.0414 0.3608, -0.10890, -0.0527 0.3991, -0.10830, -0.1393 0.4373, -0.10510, -0.1615 0.4757, -0.09890, -0.1220 0.5137, -0.09070, -0.0841 0.5694, -0.07640, 0.0638 15 Flap element taps 1.0000, 0.00130, -0.4403 0.9365, 0.01390, -0.4912 0.8333, 0.03280, -0.4829 0.7436, 0.04930, -0.4744 0.7049, 0.05670, -0.4646 0.6662, 0.06410, -0.4583 0.6522, 0.01390, 0.0498 0.5969, -0.00020, 0.0343 0.6000, -0.03020, 0.0520 0.6324, -0.04540, 0.0716 0.6667, -0.04880, 0.4430 0.7046, -0.04110, 0.3290 0.7429, -0.03210, 0.2872 0.8333, -0.01400, 0.2386 0.9311, -0.00120, 0.1115 --------- Run Conditions: vel=215.0 ft/s Re=1.994x10^6 AOA=18.01 Flap deflection=5.00 Totals: Cl=1.0062 Cdp=0.1739 Cm(c/4)=-0.0875 Cs=0.1457 Ch=-0.2282 Main component: Cl=0.7807 Cdp=0.0646 Cm=-0.1436 Flap component: Cl=0.2255 Cdp=0.1094 Cm=-0.1966 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0473 0.6175, -0.04610, 0.0156 0.5841, -0.02440, -0.0188 0.5775, 0.01750, -0.0217 0.5777, 0.04660, 0.0045 0.6274, 0.07170, -0.6058 0.5694, 0.08320, -0.6036 0.5112, 0.09370, -0.5963 0.4731, 0.09830, -0.5927 0.4349, 0.10070, -0.5869 0.3960, 0.10120, -0.5579 0.3566, 0.10020, -0.5899 0.3172, 0.09790, -0.5943 0.2778, 0.09440, -0.6150 0.2393, 0.08960, -0.6728 0.2056, 0.08360, -0.7825 0.1633, 0.07610, -1.0279 0.1261, 0.06710, -1.2873 0.0900, 0.05640, -1.6643 0.0571, 0.04390, -2.1587 0.0283, 0.02940, -2.9324 0.0142, 0.01970, -3.7424 0.0081, 0.01410, -4.5522 0.0026, 0.00780, -5.3327 0.0000, 0.00000, -6.7696 0.0037, -0.00840, -0.9950 0.0112, -0.01420, 0.4476 0.0191, -0.01930, 0.8237 0.0397, -0.03030, 1.0076 0.0706, -0.04420, 0.9678 0.1037, -0.05710, 0.8593 0.1384, -0.06890, 0.7002 0.1741, -0.07950, 0.5720 0.2102, -0.08660, 0.4586 0.2472, -0.09640, 0.2911 0.2844, -0.10270, 0.1744 0.3225, -0.10690, 0.0244 0.3608, -0.10890, -0.0772 0.3991, -0.10830, -0.1740 0.4373, -0.10510, -0.2021 0.4757, -0.09890, -0.1667 0.5137, -0.09070, -0.1311 0.5694, -0.07640, -0.0008 15 Flap element taps 1.0000, 0.00130, -0.5903 0.9365, 0.01390, -0.6147 0.8333, 0.03280, -0.6203 0.7436, 0.04930, -0.6154 0.7049, 0.05670, -0.6078 0.6662, 0.06410, -0.6063 0.6522, 0.01390, -0.0226 0.5969, -0.00020, -0.0395 0.6000, -0.03020, -0.0196 0.6324, -0.04540, 0.0013 0.6667, -0.04880, 0.4310 0.7046, -0.04110, 0.2841 0.7429, -0.03210, 0.2361 0.8333, -0.01400, 0.1760 0.9311, -0.00120, 0.0263 --------- Run Conditions: vel=212.7 ft/s Re=1.969x10^6 AOA=19.98 Flap deflection=5.00 Totals: Cl=0.6935 Cdp=0.3294 Cm(c/4)=-0.1313 Cs=-0.0726 Ch=-0.2350 Main component: Cl=0.4627 Cdp=0.2096 Cm=-0.1184 Flap component: Cl=0.2307 Cdp=0.1198 Cm=-0.2039 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.0516 0.6175, -0.04610, -0.0773 0.5841, -0.02440, -0.1182 0.5775, 0.01750, -0.1198 0.5777, 0.04660, -0.0919 0.6274, 0.07170, -0.7155 0.5694, 0.08320, -0.7208 0.5112, 0.09370, -0.7130 0.4731, 0.09830, -0.7067 0.4349, 0.10070, -0.7012 0.3960, 0.10120, -0.6641 0.3566, 0.10020, -0.6945 0.3172, 0.09790, -0.6893 0.2778, 0.09440, -0.6912 0.2393, 0.08960, -0.6871 0.2056, 0.08360, -0.6593 0.1633, 0.07610, -0.6937 0.1261, 0.06710, -0.6730 0.0900, 0.05640, -0.6895 0.0571, 0.04390, -0.6811 0.0283, 0.02940, -0.6885 0.0142, 0.01970, -0.6968 0.0081, 0.01410, -0.6854 0.0026, 0.00780, -0.7134 0.0000, 0.00000, -1.0924 0.0037, -0.00840, 0.4367 0.0112, -0.01420, 0.9009 0.0191, -0.01930, 0.9964 0.0397, -0.03030, 0.9871 0.0706, -0.04420, 0.8778 0.1037, -0.05710, 0.7459 0.1384, -0.06890, 0.5751 0.1741, -0.07950, 0.4417 0.2102, -0.08660, 0.3258 0.2472, -0.09640, 0.1511 0.2844, -0.10270, 0.0332 0.3225, -0.10690, -0.1223 0.3608, -0.10890, -0.2252 0.3991, -0.10830, -0.3233 0.4373, -0.10510, -0.3453 0.4757, -0.09890, -0.2996 0.5137, -0.09070, -0.2547 0.5694, -0.07640, -0.0868 15 Flap element taps 1.0000, 0.00130, -0.6735 0.9365, 0.01390, -0.7082 0.8333, 0.03280, -0.7268 0.7436, 0.04930, -0.7310 0.7049, 0.05670, -0.7218 0.6662, 0.06410, -0.7321 0.6522, 0.01390, -0.1232 0.5969, -0.00020, -0.1391 0.6000, -0.03020, -0.1188 0.6324, -0.04540, -0.0955 0.6667, -0.04880, 0.3511 0.7046, -0.04110, 0.2109 0.7429, -0.03210, 0.1603 0.8333, -0.01400, 0.0978 0.9311, -0.00120, -0.0547 --------- Run Conditions: vel=213.8 ft/s Re=1.973x10^6 AOA=23.98 Flap deflection=5.00 Totals: Cl=0.9072 Cdp=0.4891 Cm(c/4)=-0.1770 Cs=-0.0782 Ch=-0.2912 Main component: Cl=0.6302 Cdp=0.3174 Cm=-0.1791 Flap component: Cl=0.2770 Cdp=0.1717 Cm=-0.2548 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.0324 0.6175, -0.04610, -0.1096 0.5841, -0.02440, -0.1598 0.5775, 0.01750, -0.1632 0.5777, 0.04660, -0.1227 0.6274, 0.07170, -0.9518 0.5694, 0.08320, -0.9640 0.5112, 0.09370, -0.9563 0.4731, 0.09830, -0.9500 0.4349, 0.10070, -0.9463 0.3960, 0.10120, -0.9114 0.3566, 0.10020, -0.9424 0.3172, 0.09790, -0.9367 0.2778, 0.09440, -0.9397 0.2393, 0.08960, -0.9345 0.2056, 0.08360, -0.9051 0.1633, 0.07610, -0.9416 0.1261, 0.06710, -0.9197 0.0900, 0.05640, -0.9354 0.0571, 0.04390, -0.9264 0.0283, 0.02940, -0.9344 0.0142, 0.01970, -0.9451 0.0081, 0.01410, -0.9329 0.0026, 0.00780, -0.9404 0.0000, 0.00000, -1.0126 0.0037, -0.00840, 0.2213 0.0112, -0.01420, 0.8007 0.0191, -0.01930, 0.9569 0.0397, -0.03030, 1.0125 0.0706, -0.04420, 0.9487 0.1037, -0.05710, 0.8436 0.1384, -0.06890, 0.6875 0.1741, -0.07950, 0.5645 0.2102, -0.08660, 0.4567 0.2472, -0.09640, 0.2861 0.2844, -0.10270, 0.1663 0.3225, -0.10690, 0.0069 0.3608, -0.10890, -0.1039 0.3991, -0.10830, -0.2141 0.4373, -0.10510, -0.2526 0.4757, -0.09890, -0.2258 0.5137, -0.09070, -0.1942 0.5694, -0.07640, -0.0997 15 Flap element taps 1.0000, 0.00130, -0.8962 0.9365, 0.01390, -0.9224 0.8333, 0.03280, -0.9411 0.7436, 0.04930, -0.9499 0.7049, 0.05670, -0.9478 0.6662, 0.06410, -0.9566 0.6522, 0.01390, -0.1710 0.5969, -0.00020, -0.1883 0.6000, -0.03020, -0.1614 0.6324, -0.04540, -0.1370 0.6667, -0.04880, 0.5079 0.7046, -0.04110, 0.2167 0.7429, -0.03210, 0.1597 0.8333, -0.01400, 0.0749 0.9311, -0.00120, -0.1189 --------- Run Conditions: vel=217.8 ft/s Re=2.004x10^6 AOA=26.95 Flap deflection=5.00 Totals: Cl=0.9736 Cdp=0.5818 Cm(c/4)=-0.1953 Cs=-0.0773 Ch=-0.3108 Main component: Cl=0.6884 Cdp=0.3821 Cm=-0.2063 Flap component: Cl=0.2852 Cdp=0.1996 Cm=-0.2719 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0008 0.6175, -0.04610, -0.0976 0.5841, -0.02440, -0.1531 0.5775, 0.01750, -0.1578 0.5777, 0.04660, -0.1138 0.6274, 0.07170, -1.0131 0.5694, 0.08320, -1.0340 0.5112, 0.09370, -1.0299 0.4731, 0.09830, -1.0223 0.4349, 0.10070, -1.0185 0.3960, 0.10120, -0.9819 0.3566, 0.10020, -1.0149 0.3172, 0.09790, -1.0092 0.2778, 0.09440, -1.0118 0.2393, 0.08960, -1.0064 0.2056, 0.08360, -0.9745 0.1633, 0.07610, -1.0113 0.1261, 0.06710, -0.9886 0.0900, 0.05640, -1.0055 0.0571, 0.04390, -0.9967 0.0283, 0.02940, -1.0024 0.0142, 0.01970, -1.0094 0.0081, 0.01410, -0.9905 0.0026, 0.00780, -0.9919 0.0000, 0.00000, -1.0365 0.0037, -0.00840, 0.0174 0.0112, -0.01420, 0.6872 0.0191, -0.01930, 0.8936 0.0397, -0.03030, 1.0064 0.0706, -0.04420, 0.9813 0.1037, -0.05710, 0.8997 0.1384, -0.06890, 0.7590 0.1741, -0.07950, 0.6464 0.2102, -0.08660, 0.5474 0.2472, -0.09640, 0.3843 0.2844, -0.10270, 0.2677 0.3225, -0.10690, 0.1084 0.3608, -0.10890, -0.0035 0.3991, -0.10830, -0.1189 0.4373, -0.10510, -0.1660 0.4757, -0.09890, -0.1528 0.5137, -0.09070, -0.1313 0.5694, -0.07640, -0.0561 15 Flap element taps 1.0000, 0.00130, -0.9803 0.9365, 0.01390, -0.9944 0.8333, 0.03280, -0.9958 0.7436, 0.04930, -1.0086 0.7049, 0.05670, -1.0078 0.6662, 0.06410, -1.0157 0.6522, 0.01390, -0.1666 0.5969, -0.00020, -0.1863 0.6000, -0.03020, -0.1562 0.6324, -0.04540, -0.1329 0.6667, -0.04880, 0.5778 0.7046, -0.04110, 0.2345 0.7429, -0.03210, 0.1740 0.8333, -0.01400, 0.0794 0.9311, -0.00120, -0.1325