S809 UNVENTED AILERON, CLEAN, CHORD = 18 INCHES --------- Run Conditions: vel=104.9 ft/s Re=1.000x10^6 AOA=-5.99 Flap deflection=-90.00 Totals: Cl=-1.5517 Cdp=0.5899 Cm(c/4)=0.1638 Cs=-0.4247 Ch=0.5162 Main component: Cl=-1.5503 Cdp=0.0713 Cm=0.4158 Flap component: Cl=-0.0013 Cdp=0.5186 Cm=0.1491 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.9256 0.6175, -0.04610, -0.8686 0.5841, -0.02440, -0.8612 0.5775, 0.01750, -0.8734 0.5777, 0.04660, -0.8748 0.6274, 0.07170, 0.9045 0.5694, 0.08320, 0.8927 0.5112, 0.09370, 0.8820 0.4731, 0.09830, 0.8836 0.4349, 0.10070, 0.8641 0.3960, 0.10120, 0.8137 0.3566, 0.10020, 0.8210 0.3172, 0.09790, 0.8067 0.2778, 0.09440, 0.7934 0.2393, 0.08960, 0.7963 0.2056, 0.08360, 0.8024 0.1633, 0.07610, 0.8444 0.1261, 0.06710, 0.8895 0.0900, 0.05640, 0.9523 0.0571, 0.04390, 1.0013 0.0283, 0.02940, 0.9274 0.0142, 0.01970, 0.6244 0.0081, 0.01410, 0.2027 0.0026, 0.00780, -0.7291 0.0000, 0.00000, -2.9244 0.0037, -0.00840, -2.6752 0.0112, -0.01420, -2.6658 0.0191, -0.01930, -2.6559 0.0397, -0.03030, -2.6811 0.0706, -0.04420, -2.7345 0.1037, -0.05710, -2.6712 0.1384, -0.06890, -2.5268 0.1741, -0.07950, -2.3218 0.2102, -0.08660, -2.0569 0.2472, -0.09640, -1.8160 0.2844, -0.10270, -1.6205 0.3225, -0.10690, -1.4313 0.3608, -0.10890, -1.3053 0.3991, -0.10830, -1.2279 0.4373, -0.10510, -1.1546 0.4757, -0.09890, -1.0886 0.5137, -0.09070, -1.0363 0.5694, -0.07640, -0.9598 15 Flap element taps 1.0000, 0.00130, -0.8259 0.9365, 0.01390, 0.6385 0.8333, 0.03280, 0.9027 0.7436, 0.04930, 0.8990 0.7049, 0.05670, 0.8943 0.6662, 0.06410, 0.9070 0.6522, 0.01390, -0.8866 0.5969, -0.00020, -0.9077 0.6000, -0.03020, -0.9011 0.6324, -0.04540, -0.9007 0.6667, -0.04880, -0.8829 0.7046, -0.04110, -0.8485 0.7429, -0.03210, -0.8407 0.8333, -0.01400, -0.8382 0.9311, -0.00120, -0.8170 --------- Run Conditions: vel=108.4 ft/s Re=1.034x10^6 AOA=-0.02 Flap deflection=-90.00 Totals: Cl=-1.6703 Cdp=0.4044 Cm(c/4)=0.1897 Cs=-0.4039 Ch=0.5017 Main component: Cl=-1.6214 Cdp=-0.0974 Cm=0.4655 Flap component: Cl=-0.0489 Cdp=0.5018 Cm=0.1418 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8563 0.6175, -0.04610, -0.7961 0.5841, -0.02440, -0.7983 0.5775, 0.01750, -0.8049 0.5777, 0.04660, -0.8111 0.6274, 0.07170, 0.8915 0.5694, 0.08320, 0.8944 0.5112, 0.09370, 0.8814 0.4731, 0.09830, 0.8832 0.4349, 0.10070, 0.8587 0.3960, 0.10120, 0.7725 0.3566, 0.10020, 0.7765 0.3172, 0.09790, 0.7619 0.2778, 0.09440, 0.7425 0.2393, 0.08960, 0.7373 0.2056, 0.08360, 0.7258 0.1633, 0.07610, 0.7814 0.1261, 0.06710, 0.8214 0.0900, 0.05640, 0.9045 0.0571, 0.04390, 0.9824 0.0283, 0.02940, 0.9735 0.0142, 0.01970, 0.7170 0.0081, 0.01410, 0.2752 0.0026, 0.00780, -0.8601 0.0000, 0.00000, -5.0175 0.0037, -0.00840, -5.3373 0.0112, -0.01420, -4.0911 0.0191, -0.01930, -2.7399 0.0397, -0.03030, -2.1591 0.0706, -0.04420, -1.8988 0.1037, -0.05710, -1.8343 0.1384, -0.06890, -1.8171 0.1741, -0.07950, -1.8396 0.2102, -0.08660, -1.9310 0.2472, -0.09640, -2.0269 0.2844, -0.10270, -2.0721 0.3225, -0.10690, -2.0727 0.3608, -0.10890, -2.1077 0.3991, -0.10830, -2.0290 0.4373, -0.10510, -1.8664 0.4757, -0.09890, -1.6175 0.5137, -0.09070, -1.3782 0.5694, -0.07640, -1.0139 15 Flap element taps 1.0000, 0.00130, -0.8090 0.9365, 0.01390, 0.6198 0.8333, 0.03280, 0.8935 0.7436, 0.04930, 0.8845 0.7049, 0.05670, 0.8816 0.6662, 0.06410, 0.8915 0.6522, 0.01390, -0.8087 0.5969, -0.00020, -0.8064 0.6000, -0.03020, -0.8094 0.6324, -0.04540, -0.8150 0.6667, -0.04880, -0.8135 0.7046, -0.04110, -0.8030 0.7429, -0.03210, -0.8083 0.8333, -0.01400, -0.8151 0.9311, -0.00120, -0.7946 --------- Run Conditions: vel=105.3 ft/s Re=1.008x10^6 AOA=2.98 Flap deflection=-90.00 Totals: Cl=-1.6991 Cdp=0.4191 Cm(c/4)=0.2183 Cs=-0.5069 Ch=0.5398 Main component: Cl=-1.6175 Cdp=-0.1179 Cm=0.4839 Flap component: Cl=-0.0816 Cdp=0.5371 Cm=0.1531 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.0400 0.6175, -0.04610, -0.9300 0.5841, -0.02440, -0.9363 0.5775, 0.01750, -0.9434 0.5777, 0.04660, -0.9476 0.6274, 0.07170, 0.8827 0.5694, 0.08320, 0.8943 0.5112, 0.09370, 0.8736 0.4731, 0.09830, 0.8730 0.4349, 0.10070, 0.8439 0.3960, 0.10120, 0.7484 0.3566, 0.10020, 0.7429 0.3172, 0.09790, 0.7252 0.2778, 0.09440, 0.7048 0.2393, 0.08960, 0.6920 0.2056, 0.08360, 0.6613 0.1633, 0.07610, 0.7323 0.1261, 0.06710, 0.7610 0.0900, 0.05640, 0.8555 0.0571, 0.04390, 0.9480 0.0283, 0.02940, 0.9977 0.0142, 0.01970, 0.8473 0.0081, 0.01410, 0.5142 0.0026, 0.00780, -0.3966 0.0000, 0.00000, -3.7667 0.0037, -0.00840, -4.2428 0.0112, -0.01420, -3.9180 0.0191, -0.01930, -2.1568 0.0397, -0.03030, -1.8625 0.0706, -0.04420, -1.7022 0.1037, -0.05710, -1.6939 0.1384, -0.06890, -1.6994 0.1741, -0.07950, -1.7598 0.2102, -0.08660, -1.8961 0.2472, -0.09640, -2.0197 0.2844, -0.10270, -2.1039 0.3225, -0.10690, -2.1303 0.3608, -0.10890, -2.2133 0.3991, -0.10830, -2.1705 0.4373, -0.10510, -2.0566 0.4757, -0.09890, -1.8426 0.5137, -0.09070, -1.6441 0.5694, -0.07640, -1.2484 15 Flap element taps 1.0000, 0.00130, -0.9273 0.9365, 0.01390, 0.5951 0.8333, 0.03280, 0.8876 0.7436, 0.04930, 0.8729 0.7049, 0.05670, 0.8690 0.6662, 0.06410, 0.8767 0.6522, 0.01390, -0.9551 0.5969, -0.00020, -0.9475 0.6000, -0.03020, -0.9486 0.6324, -0.04540, -0.9664 0.6667, -0.04880, -0.9691 0.7046, -0.04110, -0.9439 0.7429, -0.03210, -0.9497 0.8333, -0.01400, -0.9561 0.9311, -0.00120, -0.9216 --------- Run Conditions: vel=105.0 ft/s Re=1.008x10^6 AOA=6.00 Flap deflection=-90.00 Totals: Cl=-1.5875 Cdp=0.4417 Cm(c/4)=0.2354 Cs=-0.6052 Ch=0.5620 Main component: Cl=-1.4742 Cdp=-0.1132 Cm=0.4598 Flap component: Cl=-0.1133 Cdp=0.5548 Cm=0.1588 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.1053 0.6175, -0.04610, -1.0059 0.5841, -0.02440, -1.0116 0.5775, 0.01750, -1.0160 0.5777, 0.04660, -1.0212 0.6274, 0.07170, 0.8695 0.5694, 0.08320, 0.8903 0.5112, 0.09370, 0.8611 0.4731, 0.09830, 0.8625 0.4349, 0.10070, 0.8273 0.3960, 0.10120, 0.7220 0.3566, 0.10020, 0.6912 0.3172, 0.09790, 0.6644 0.2778, 0.09440, 0.6478 0.2393, 0.08960, 0.6227 0.2056, 0.08360, 0.5678 0.1633, 0.07610, 0.6463 0.1261, 0.06710, 0.6573 0.0900, 0.05640, 0.7551 0.0571, 0.04390, 0.8592 0.0283, 0.02940, 0.9837 0.0142, 0.01970, 0.9764 0.0081, 0.01410, 0.8059 0.0026, 0.00780, 0.1986 0.0000, 0.00000, -1.8993 0.0037, -0.00840, -2.7259 0.0112, -0.01420, -2.2253 0.0191, -0.01930, -2.0954 0.0397, -0.03030, -1.2825 0.0706, -0.04420, -1.2824 0.1037, -0.05710, -1.3459 0.1384, -0.06890, -1.3869 0.1741, -0.07950, -1.4853 0.2102, -0.08660, -1.6664 0.2472, -0.09640, -1.8098 0.2844, -0.10270, -1.9290 0.3225, -0.10690, -1.9742 0.3608, -0.10890, -2.0964 0.3991, -0.10830, -2.0811 0.4373, -0.10510, -2.0125 0.4757, -0.09890, -1.8313 0.5137, -0.09070, -1.6712 0.5694, -0.07640, -1.2908 15 Flap element taps 1.0000, 0.00130, -1.0101 0.9365, 0.01390, 0.5658 0.8333, 0.03280, 0.8757 0.7436, 0.04930, 0.8577 0.7049, 0.05670, 0.8544 0.6662, 0.06410, 0.8612 0.6522, 0.01390, -1.0344 0.5969, -0.00020, -1.0235 0.6000, -0.03020, -1.0262 0.6324, -0.04540, -1.0474 0.6667, -0.04880, -1.0626 0.7046, -0.04110, -1.0339 0.7429, -0.03210, -1.0403 0.8333, -0.01400, -1.0539 0.9311, -0.00120, -1.0080 --------- Run Conditions: vel=103.5 ft/s Re=0.997x10^6 AOA=8.84 Flap deflection=-90.00 Totals: Cl=-1.4726 Cdp=0.4374 Cm(c/4)=0.2467 Cs=-0.6585 Ch=0.5587 Main component: Cl=-1.3316 Cdp=-0.1063 Cm=0.4350 Flap component: Cl=-0.1410 Cdp=0.5437 Cm=0.1587 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.1038 0.6175, -0.04610, -1.0292 0.5841, -0.02440, -1.0400 0.5775, 0.01750, -1.0465 0.5777, 0.04660, -1.0490 0.6274, 0.07170, 0.8480 0.5694, 0.08320, 0.8722 0.5112, 0.09370, 0.8392 0.4731, 0.09830, 0.8434 0.4349, 0.10070, 0.8073 0.3960, 0.10120, 0.6788 0.3566, 0.10020, 0.7169 0.3172, 0.09790, 0.5936 0.2778, 0.09440, 0.5837 0.2393, 0.08960, 0.5532 0.2056, 0.08360, 0.4726 0.1633, 0.07610, 0.5523 0.1261, 0.06710, 0.5437 0.0900, 0.05640, 0.6366 0.0571, 0.04390, 0.7355 0.0283, 0.02940, 0.8991 0.0142, 0.01970, 0.9900 0.0081, 0.01410, 0.9266 0.0026, 0.00780, 0.6714 0.0000, 0.00000, -0.5205 0.0037, -0.00840, -1.4687 0.0112, -0.01420, -1.2282 0.0191, -0.01930, -1.0533 0.0397, -0.03030, -0.8818 0.0706, -0.04420, -0.9313 0.1037, -0.05710, -1.0397 0.1384, -0.06890, -1.1005 0.1741, -0.07950, -1.2444 0.2102, -0.08660, -1.4618 0.2472, -0.09640, -1.6144 0.2844, -0.10270, -1.7670 0.3225, -0.10690, -1.8331 0.3608, -0.10890, -1.9887 0.3991, -0.10830, -2.0049 0.4373, -0.10510, -1.9548 0.4757, -0.09890, -1.8379 0.5137, -0.09070, -1.7800 0.5694, -0.07640, -1.2270 15 Flap element taps 1.0000, 0.00130, -1.0084 0.9365, 0.01390, 0.5484 0.8333, 0.03280, 0.8584 0.7436, 0.04930, 0.8356 0.7049, 0.05670, 0.8316 0.6662, 0.06410, 0.8406 0.6522, 0.01390, -1.0672 0.5969, -0.00020, -1.0498 0.6000, -0.03020, -1.0432 0.6324, -0.04540, -1.0553 0.6667, -0.04880, -1.0705 0.7046, -0.04110, -1.0341 0.7429, -0.03210, -1.0615 0.8333, -0.01400, -1.0647 0.9311, -0.00120, -1.0064 --------- Run Conditions: vel=103.5 ft/s Re=0.999x10^6 AOA=12.04 Flap deflection=-90.00 Totals: Cl=-1.2992 Cdp=0.4594 Cm(c/4)=0.2574 Cs=-0.7203 Ch=0.5708 Main component: Cl=-1.1253 Cdp=-0.0871 Cm=0.3895 Flap component: Cl=-0.1739 Cdp=0.5465 Cm=0.1615 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.0979 0.6175, -0.04610, -1.0718 0.5841, -0.02440, -1.0807 0.5775, 0.01750, -1.0843 0.5777, 0.04660, -1.0871 0.6274, 0.07170, 0.8164 0.5694, 0.08320, 0.8319 0.5112, 0.09370, 0.8046 0.4731, 0.09830, 0.8091 0.4349, 0.10070, 0.7783 0.3960, 0.10120, 0.6345 0.3566, 0.10020, 0.6723 0.3172, 0.09790, 0.5733 0.2778, 0.09440, 0.4837 0.2393, 0.08960, 0.4601 0.2056, 0.08360, 0.3547 0.1633, 0.07610, 0.4285 0.1261, 0.06710, 0.3879 0.0900, 0.05640, 0.4608 0.0571, 0.04390, 0.5345 0.0283, 0.02940, 0.6979 0.0142, 0.01970, 0.8570 0.0081, 0.01410, 0.8824 0.0026, 0.00780, 0.9300 0.0000, 0.00000, 0.5678 0.0037, -0.00840, -0.2438 0.0112, -0.01420, -0.3221 0.0191, -0.01930, -0.3152 0.0397, -0.03030, -0.3462 0.0706, -0.04420, -0.5084 0.1037, -0.05710, -0.6679 0.1384, -0.06890, -0.7506 0.1741, -0.07950, -0.9216 0.2102, -0.08660, -1.1693 0.2472, -0.09640, -1.3345 0.2844, -0.10270, -1.5115 0.3225, -0.10690, -1.5923 0.3608, -0.10890, -1.7765 0.3991, -0.10830, -1.8166 0.4373, -0.10510, -1.8090 0.4757, -0.09890, -1.7058 0.5137, -0.09070, -1.6693 0.5694, -0.07640, -1.1889 15 Flap element taps 1.0000, 0.00130, -1.0637 0.9365, 0.01390, 0.5251 0.8333, 0.03280, 0.8463 0.7436, 0.04930, 0.8008 0.7049, 0.05670, 0.7929 0.6662, 0.06410, 0.8049 0.6522, 0.01390, -1.1147 0.5969, -0.00020, -1.0950 0.6000, -0.03020, -1.0902 0.6324, -0.04540, -1.1170 0.6667, -0.04880, -1.1372 0.7046, -0.04110, -1.0935 0.7429, -0.03210, -1.1171 0.8333, -0.01400, -1.1292 0.9311, -0.00120, -1.0665 --------- Run Conditions: vel=103.5 ft/s Re=1.003x10^6 AOA=15.00 Flap deflection=-90.00 Totals: Cl=-1.1344 Cdp=0.4562 Cm(c/4)=0.2616 Cs=-0.7343 Ch=0.5616 Main component: Cl=-0.9358 Cdp=-0.0687 Cm=0.3467 Flap component: Cl=-0.1987 Cdp=0.5249 Cm=0.1593 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.0856 0.6175, -0.04610, -1.1037 0.5841, -0.02440, -1.0907 0.5775, 0.01750, -1.1043 0.5777, 0.04660, -1.1048 0.6274, 0.07170, 0.7729 0.5694, 0.08320, 0.7529 0.5112, 0.09370, 0.7594 0.4731, 0.09830, 0.7724 0.4349, 0.10070, 0.7600 0.3960, 0.10120, 0.7004 0.3566, 0.10020, 0.6219 0.3172, 0.09790, 0.5450 0.2778, 0.09440, 0.4194 0.2393, 0.08960, 0.3501 0.2056, 0.08360, 0.3057 0.1633, 0.07610, 0.2789 0.1261, 0.06710, 0.2481 0.0900, 0.05640, 0.2462 0.0571, 0.04390, 0.2865 0.0283, 0.02940, 0.4074 0.0142, 0.01970, 0.5747 0.0081, 0.01410, 0.6873 0.0026, 0.00780, 0.8622 0.0000, 0.00000, 0.9764 0.0037, -0.00840, 0.5365 0.0112, -0.01420, 0.3257 0.0191, -0.01930, 0.2239 0.0397, -0.03030, 0.0759 0.0706, -0.04420, -0.1284 0.1037, -0.05710, -0.3199 0.1384, -0.06890, -0.4990 0.1741, -0.07950, -0.6668 0.2102, -0.08660, -0.8638 0.2472, -0.09640, -1.0771 0.2844, -0.10270, -1.2451 0.3225, -0.10690, -1.4058 0.3608, -0.10890, -1.5566 0.3991, -0.10830, -1.6546 0.4373, -0.10510, -1.6479 0.4757, -0.09890, -1.5627 0.5137, -0.09070, -1.5358 0.5694, -0.07640, -1.1674 15 Flap element taps 1.0000, 0.00130, -1.0805 0.9365, 0.01390, 0.5073 0.8333, 0.03280, 0.8238 0.7436, 0.04930, 0.7545 0.7049, 0.05670, 0.7626 0.6662, 0.06410, 0.7752 0.6522, 0.01390, -1.0987 0.5969, -0.00020, -1.1140 0.6000, -0.03020, -1.1058 0.6324, -0.04540, -1.1095 0.6667, -0.04880, -1.1064 0.7046, -0.04110, -1.0946 0.7429, -0.03210, -1.0981 0.8333, -0.01400, -1.0972 0.9311, -0.00120, -1.0844 --------- Run Conditions: vel=103.8 ft/s Re=1.007x10^6 AOA=17.99 Flap deflection=-90.00 Totals: Cl=-0.9585 Cdp=0.4531 Cm(c/4)=0.2628 Cs=-0.7270 Ch=0.5512 Main component: Cl=-0.7373 Cdp=-0.0479 Cm=0.2992 Flap component: Cl=-0.2212 Cdp=0.5009 Cm=0.1566 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.0478 0.6175, -0.04610, -1.1104 0.5841, -0.02440, -1.0997 0.5775, 0.01750, -1.1134 0.5777, 0.04660, -1.1133 0.6274, 0.07170, 0.7122 0.5694, 0.08320, 0.6856 0.5112, 0.09370, 0.6936 0.4731, 0.09830, 0.7080 0.4349, 0.10070, 0.7040 0.3960, 0.10120, 0.6632 0.3566, 0.10020, 0.6049 0.3172, 0.09790, 0.5015 0.2778, 0.09440, 0.4067 0.2393, 0.08960, 0.3046 0.2056, 0.08360, 0.1600 0.1633, 0.07610, 0.1424 0.1261, 0.06710, 0.0769 0.0900, 0.05640, 0.0355 0.0571, 0.04390, 0.0096 0.0283, 0.02940, 0.0399 0.0142, 0.01970, 0.1415 0.0081, 0.01410, 0.2214 0.0026, 0.00780, 0.4295 0.0000, 0.00000, 0.8661 0.0037, -0.00840, 0.9266 0.0112, -0.01420, 0.7498 0.0191, -0.01930, 0.6218 0.0397, -0.03030, 0.4229 0.0706, -0.04420, 0.1848 0.1037, -0.05710, -0.0211 0.1384, -0.06890, -0.2071 0.1741, -0.07950, -0.3868 0.2102, -0.08660, -0.5986 0.2472, -0.09640, -0.8121 0.2844, -0.10270, -0.9956 0.3225, -0.10690, -1.1619 0.3608, -0.10890, -1.3315 0.3991, -0.10830, -1.4476 0.4373, -0.10510, -1.4737 0.4757, -0.09890, -1.4172 0.5137, -0.09070, -1.4122 0.5694, -0.07640, -1.1044 15 Flap element taps 1.0000, 0.00130, -1.0801 0.9365, 0.01390, 0.5036 0.8333, 0.03280, 0.7782 0.7436, 0.04930, 0.6778 0.7049, 0.05670, 0.6933 0.6662, 0.06410, 0.7117 0.6522, 0.01390, -1.1107 0.5969, -0.00020, -1.1177 0.6000, -0.03020, -1.1105 0.6324, -0.04540, -1.1157 0.6667, -0.04880, -1.1138 0.7046, -0.04110, -1.0976 0.7429, -0.03210, -1.1042 0.8333, -0.01400, -1.0964 0.9311, -0.00120, -1.0821 --------- Run Conditions: vel=103.5 ft/s Re=1.006x10^6 AOA=19.97 Flap deflection=-90.00 Totals: Cl=-0.8278 Cdp=0.4468 Cm(c/4)=0.2593 Cs=-0.7026 Ch=0.5376 Main component: Cl=-0.5969 Cdp=-0.0294 Cm=0.2632 Flap component: Cl=-0.2309 Cdp=0.4762 Cm=0.1525 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.0167 0.6175, -0.04610, -1.1076 0.5841, -0.02440, -1.0986 0.5775, 0.01750, -1.1126 0.5777, 0.04660, -1.1132 0.6274, 0.07170, 0.6433 0.5694, 0.08320, 0.5979 0.5112, 0.09370, 0.6071 0.4731, 0.09830, 0.6248 0.4349, 0.10070, 0.6262 0.3960, 0.10120, 0.5960 0.3566, 0.10020, 0.5920 0.3172, 0.09790, 0.5002 0.2778, 0.09440, 0.3776 0.2393, 0.08960, 0.2627 0.2056, 0.08360, 0.1354 0.1633, 0.07610, 0.0243 0.1261, 0.06710, -0.0578 0.0900, 0.05640, -0.1222 0.0571, 0.04390, -0.2063 0.0283, 0.02940, -0.2607 0.0142, 0.01970, -0.2429 0.0081, 0.01410, -0.2297 0.0026, 0.00780, -0.0296 0.0000, 0.00000, 0.4542 0.0037, -0.00840, 0.9853 0.0112, -0.01420, 0.9218 0.0191, -0.01930, 0.8120 0.0397, -0.03030, 0.6153 0.0706, -0.04420, 0.3708 0.1037, -0.05710, 0.1612 0.1384, -0.06890, -0.0225 0.1741, -0.07950, -0.2057 0.2102, -0.08660, -0.4295 0.2472, -0.09640, -0.6402 0.2844, -0.10270, -0.8320 0.3225, -0.10690, -0.9990 0.3608, -0.10890, -1.1828 0.3991, -0.10830, -1.3060 0.4373, -0.10510, -1.3547 0.4757, -0.09890, -1.3168 0.5137, -0.09070, -1.3283 0.5694, -0.07640, -1.0572 15 Flap element taps 1.0000, 0.00130, -1.0853 0.9365, 0.01390, 0.5089 0.8333, 0.03280, 0.7140 0.7436, 0.04930, 0.5918 0.7049, 0.05670, 0.6100 0.6662, 0.06410, 0.6435 0.6522, 0.01390, -1.1096 0.5969, -0.00020, -1.1175 0.6000, -0.03020, -1.1046 0.6324, -0.04540, -1.1095 0.6667, -0.04880, -1.1053 0.7046, -0.04110, -1.0910 0.7429, -0.03210, -1.0990 0.8333, -0.01400, -1.0935 0.9311, -0.00120, -1.0744 --------- Run Conditions: vel=103.3 ft/s Re=1.005x10^6 AOA=23.99 Flap deflection=-90.00 Totals: Cl=-0.4571 Cdp=0.4172 Cm(c/4)=0.2184 Cs=-0.5670 Ch=0.4472 Main component: Cl=-0.2443 Cdp=0.0464 Cm=0.1553 Flap component: Cl=-0.2128 Cdp=0.3708 Cm=0.1251 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.9450 0.6175, -0.04610, -1.0827 0.5841, -0.02440, -1.0784 0.5775, 0.01750, -1.0921 0.5777, 0.04660, -1.0948 0.6274, 0.07170, 0.3302 0.5694, 0.08320, 0.2220 0.5112, 0.09370, 0.2008 0.4731, 0.09830, 0.2322 0.4349, 0.10070, 0.2445 0.3960, 0.10120, 0.2232 0.3566, 0.10020, 0.2667 0.3172, 0.09790, 0.2730 0.2778, 0.09440, 0.2773 0.2393, 0.08960, 0.2614 0.2056, 0.08360, 0.1326 0.1633, 0.07610, -0.0102 0.1261, 0.06710, -0.2342 0.0900, 0.05640, -0.4327 0.0571, 0.04390, -0.6728 0.0283, 0.02940, -1.0659 0.0142, 0.01970, -1.3391 0.0081, 0.01410, -1.6184 0.0026, 0.00780, -1.4728 0.0000, 0.00000, -1.5180 0.0037, -0.00840, 0.6149 0.0112, -0.01420, 0.9793 0.0191, -0.01930, 1.0000 0.0397, -0.03030, 0.9132 0.0706, -0.04420, 0.7050 0.1037, -0.05710, 0.5154 0.1384, -0.06890, 0.3473 0.1741, -0.07950, 0.1668 0.2102, -0.08660, -0.0623 0.2472, -0.09640, -0.2619 0.2844, -0.10270, -0.4639 0.3225, -0.10690, -0.6331 0.3608, -0.10890, -0.8316 0.3991, -0.10830, -0.9745 0.4373, -0.10510, -1.0601 0.4757, -0.09890, -1.0632 0.5137, -0.09070, -1.1108 0.5694, -0.07640, -0.9126 15 Flap element taps 1.0000, 0.00130, -1.0921 0.9365, 0.01390, 0.4043 0.8333, 0.03280, 0.3124 0.7436, 0.04930, 0.2022 0.7049, 0.05670, 0.2574 0.6662, 0.06410, 0.3290 0.6522, 0.01390, -1.0804 0.5969, -0.00020, -1.0914 0.6000, -0.03020, -1.0757 0.6324, -0.04540, -1.0765 0.6667, -0.04880, -1.0738 0.7046, -0.04110, -1.0588 0.7429, -0.03210, -1.0711 0.8333, -0.01400, -1.0743 0.9311, -0.00120, -1.0638 --------- Run Conditions: vel=106.8 ft/s Re=1.039x10^6 AOA=26.99 Flap deflection=-90.00 Totals: Cl=0.7091 Cdp=0.2728 Cm(c/4)=-0.0416 Cs=0.0787 Ch=-0.1718 Main component: Cl=0.6161 Cdp=0.4185 Cm=-0.1820 Flap component: Cl=0.0930 Cdp=-0.1457 Cm=-0.0485 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4909 0.6175, -0.04610, -0.6083 0.5841, -0.02440, -0.6015 0.5775, 0.01750, -0.6160 0.5777, 0.04660, -0.6186 0.6274, 0.07170, -0.9901 0.5694, 0.08320, -1.0745 0.5112, 0.09370, -1.2538 0.4731, 0.09830, -1.3156 0.4349, 0.10070, -1.2986 0.3960, 0.10120, -1.2666 0.3566, 0.10020, -1.1733 0.3172, 0.09790, -1.1322 0.2778, 0.09440, -1.1146 0.2393, 0.08960, -1.1048 0.2056, 0.08360, -1.1305 0.1633, 0.07610, -1.0726 0.1261, 0.06710, -1.0913 0.0900, 0.05640, -1.0669 0.0571, 0.04390, -1.0671 0.0283, 0.02940, -1.0653 0.0142, 0.01970, -1.0730 0.0081, 0.01410, -1.1045 0.0026, 0.00780, -0.9710 0.0000, 0.00000, -1.1208 0.0037, -0.00840, 0.0928 0.0112, -0.01420, 0.7432 0.0191, -0.01930, 0.9196 0.0397, -0.03030, 1.0069 0.0706, -0.04420, 0.9255 0.1037, -0.05710, 0.8132 0.1384, -0.06890, 0.7031 0.1741, -0.07950, 0.5660 0.2102, -0.08660, 0.3739 0.2472, -0.09640, 0.2195 0.2844, -0.10270, 0.0432 0.3225, -0.10690, -0.0934 0.3608, -0.10890, -0.2711 0.3991, -0.10830, -0.3996 0.4373, -0.10510, -0.4981 0.4757, -0.09890, -0.5237 0.5137, -0.09070, -0.5857 0.5694, -0.07640, -0.4544 15 Flap element taps 1.0000, 0.00130, -0.7310 0.9365, 0.01390, -0.9478 0.8333, 0.03280, -1.2727 0.7436, 0.04930, -1.1300 0.7049, 0.05670, -1.0400 0.6662, 0.06410, -0.9898 0.6522, 0.01390, -0.6150 0.5969, -0.00020, -0.6144 0.6000, -0.03020, -0.5955 0.6324, -0.04540, -0.5802 0.6667, -0.04880, -0.5624 0.7046, -0.04110, -0.5397 0.7429, -0.03210, -0.5501 0.8333, -0.01400, -0.5534 0.9311, -0.00120, -0.5487 --------- Run Conditions: vel=102.2 ft/s Re=1.003x10^6 AOA=29.99 Flap deflection=-90.00 Totals: Cl=0.6685 Cdp=0.3414 Cm(c/4)=-0.0326 Cs=0.0385 Ch=-0.1509 Main component: Cl=0.5813 Cdp=0.4591 Cm=-0.1764 Flap component: Cl=0.0872 Cdp=-0.1177 Cm=-0.0436 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5545 0.6175, -0.04610, -0.7145 0.5841, -0.02440, -0.7109 0.5775, 0.01750, -0.7251 0.5777, 0.04660, -0.7182 0.6274, 0.07170, -1.0324 0.5694, 0.08320, -1.0496 0.5112, 0.09370, -1.1314 0.4731, 0.09830, -1.1605 0.4349, 0.10070, -1.1654 0.3960, 0.10120, -1.1719 0.3566, 0.10020, -1.1404 0.3172, 0.09790, -1.1141 0.2778, 0.09440, -1.1046 0.2393, 0.08960, -1.0853 0.2056, 0.08360, -1.0977 0.1633, 0.07610, -1.0824 0.1261, 0.06710, -1.0815 0.0900, 0.05640, -1.0744 0.0571, 0.04390, -1.0768 0.0283, 0.02940, -1.0807 0.0142, 0.01970, -1.0889 0.0081, 0.01410, -1.0983 0.0026, 0.00780, -0.9718 0.0000, 0.00000, -1.1095 0.0037, -0.00840, -0.0588 0.0112, -0.01420, 0.6502 0.0191, -0.01930, 0.8765 0.0397, -0.03030, 1.0015 0.0706, -0.04420, 0.9596 0.1037, -0.05710, 0.8697 0.1384, -0.06890, 0.7472 0.1741, -0.07950, 0.6120 0.2102, -0.08660, 0.4503 0.2472, -0.09640, 0.2907 0.2844, -0.10270, 0.1139 0.3225, -0.10690, -0.0354 0.3608, -0.10890, -0.2170 0.3991, -0.10830, -0.3651 0.4373, -0.10510, -0.4621 0.4757, -0.09890, -0.5052 0.5137, -0.09070, -0.5785 0.5694, -0.07640, -0.4817 15 Flap element taps 1.0000, 0.00130, -1.3029 0.9365, 0.01390, -1.1340 0.8333, 0.03280, -1.1657 0.7436, 0.04930, -1.0775 0.7049, 0.05670, -1.0547 0.6662, 0.06410, -1.0240 0.6522, 0.01390, -0.7196 0.5969, -0.00020, -0.7205 0.6000, -0.03020, -0.6955 0.6324, -0.04540, -0.6600 0.6667, -0.04880, -0.6439 0.7046, -0.04110, -0.6337 0.7429, -0.03210, -0.6474 0.8333, -0.01400, -0.6494 0.9311, -0.00120, -0.6490 --------- Run Conditions: vel=101.3 ft/s Re=0.994x10^6 AOA=34.97 Flap deflection=-90.00 Totals: Cl=0.5077 Cdp=0.4431 Cm(c/4)=-0.0032 Cs=-0.0722 Ch=-0.0625 Main component: Cl=0.4689 Cdp=0.4950 Cm=-0.1555 Flap component: Cl=0.0388 Cdp=-0.0519 Cm=-0.0152 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6316 0.6175, -0.04610, -0.8613 0.5841, -0.02440, -0.8559 0.5775, 0.01750, -0.8693 0.5777, 0.04660, -0.8619 0.6274, 0.07170, -0.9686 0.5694, 0.08320, -0.9708 0.5112, 0.09370, -0.9819 0.4731, 0.09830, -0.9624 0.4349, 0.10070, -0.9573 0.3960, 0.10120, -0.9773 0.3566, 0.10020, -0.9544 0.3172, 0.09790, -0.9491 0.2778, 0.09440, -0.9540 0.2393, 0.08960, -0.9474 0.2056, 0.08360, -0.9709 0.1633, 0.07610, -0.9544 0.1261, 0.06710, -0.9551 0.0900, 0.05640, -0.9510 0.0571, 0.04390, -0.9513 0.0283, 0.02940, -0.9515 0.0142, 0.01970, -0.9571 0.0081, 0.01410, -0.9694 0.0026, 0.00780, -0.8528 0.0000, 0.00000, -0.9641 0.0037, -0.00840, -0.1661 0.0112, -0.01420, 0.5630 0.0191, -0.01930, 0.8179 0.0397, -0.03030, 0.9892 0.0706, -0.04420, 0.9798 0.1037, -0.05710, 0.9138 0.1384, -0.06890, 0.8141 0.1741, -0.07950, 0.6868 0.2102, -0.08660, 0.5274 0.2472, -0.09640, 0.3769 0.2844, -0.10270, 0.1972 0.3225, -0.10690, 0.0475 0.3608, -0.10890, -0.1461 0.3991, -0.10830, -0.3059 0.4373, -0.10510, -0.4252 0.4757, -0.09890, -0.4904 0.5137, -0.09070, -0.5816 0.5694, -0.07640, -0.5214 15 Flap element taps 1.0000, 0.00130, -0.9869 0.9365, 0.01390, -0.9966 0.8333, 0.03280, -0.9757 0.7436, 0.04930, -0.9751 0.7049, 0.05670, -0.9646 0.6662, 0.06410, -0.9616 0.6522, 0.01390, -0.8719 0.5969, -0.00020, -0.8686 0.6000, -0.03020, -0.8334 0.6324, -0.04540, -0.7954 0.6667, -0.04880, -0.7818 0.7046, -0.04110, -0.7726 0.7429, -0.03210, -0.7866 0.8333, -0.01400, -0.7867 0.9311, -0.00120, -0.7712 --------- Run Conditions: vel=101.6 ft/s Re=0.996x10^6 AOA=39.97 Flap deflection=-90.00 Totals: Cl=0.4842 Cdp=0.5378 Cm(c/4)=-0.0027 Cs=-0.1011 Ch=-0.0385 Main component: Cl=0.4550 Cdp=0.5753 Cm=-0.1741 Flap component: Cl=0.0292 Cdp=-0.0376 Cm=-0.0078 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6556 0.6175, -0.04610, -0.9653 0.5841, -0.02440, -0.9643 0.5775, 0.01750, -0.9803 0.5777, 0.04660, -0.9723 0.6274, 0.07170, -0.9748 0.5694, 0.08320, -0.9707 0.5112, 0.09370, -0.9911 0.4731, 0.09830, -0.9798 0.4349, 0.10070, -0.9737 0.3960, 0.10120, -0.9983 0.3566, 0.10020, -0.9680 0.3172, 0.09790, -0.9591 0.2778, 0.09440, -0.9626 0.2393, 0.08960, -0.9545 0.2056, 0.08360, -0.9800 0.1633, 0.07610, -0.9573 0.1261, 0.06710, -0.9626 0.0900, 0.05640, -0.9535 0.0571, 0.04390, -0.9554 0.0283, 0.02940, -0.9530 0.0142, 0.01970, -0.9589 0.0081, 0.01410, -0.9749 0.0026, 0.00780, -0.8543 0.0000, 0.00000, -0.9568 0.0037, -0.00840, -0.3778 0.0112, -0.01420, 0.4046 0.0191, -0.01930, 0.7087 0.0397, -0.03030, 0.9518 0.0706, -0.04420, 0.9917 0.1037, -0.05710, 0.9603 0.1384, -0.06890, 0.8896 0.1741, -0.07950, 0.7821 0.2102, -0.08660, 0.6348 0.2472, -0.09640, 0.4983 0.2844, -0.10270, 0.3262 0.3225, -0.10690, 0.1827 0.3608, -0.10890, -0.0154 0.3991, -0.10830, -0.1782 0.4373, -0.10510, -0.3146 0.4757, -0.09890, -0.4001 0.5137, -0.09070, -0.5162 0.5694, -0.07640, -0.4942 15 Flap element taps 1.0000, 0.00130, -1.0225 0.9365, 0.01390, -0.9943 0.8333, 0.03280, -0.9816 0.7436, 0.04930, -0.9802 0.7049, 0.05670, -0.9717 0.6662, 0.06410, -0.9727 0.6522, 0.01390, -0.9698 0.5969, -0.00020, -0.9709 0.6000, -0.03020, -0.8943 0.6324, -0.04540, -0.8411 0.6667, -0.04880, -0.8321 0.7046, -0.04110, -0.8282 0.7429, -0.03210, -0.8465 0.8333, -0.01400, -0.8579 0.9311, -0.00120, -0.8593 --------- Run Conditions: vel=101.5 ft/s Re=0.997x10^6 AOA=44.96 Flap deflection=-90.00 Totals: Cl=0.4102 Cdp=0.6399 Cm(c/4)=0.0106 Cs=-0.1629 Ch=-0.0054 Main component: Cl=0.3934 Cdp=0.7004 Cm=-0.1911 Flap component: Cl=0.0169 Cdp=-0.0605 Cm=0.0161 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.9186 0.6175, -0.04610, -1.5640 0.5841, -0.02440, -1.5623 0.5775, 0.01750, -1.5792 0.5777, 0.04660, -1.5683 0.6274, 0.07170, -1.0332 0.5694, 0.08320, -1.0282 0.5112, 0.09370, -1.0449 0.4731, 0.09830, -1.0332 0.4349, 0.10070, -1.0318 0.3960, 0.10120, -1.0649 0.3566, 0.10020, -1.0281 0.3172, 0.09790, -1.0233 0.2778, 0.09440, -1.0250 0.2393, 0.08960, -1.0186 0.2056, 0.08360, -1.0505 0.1633, 0.07610, -1.0195 0.1261, 0.06710, -1.0283 0.0900, 0.05640, -1.0160 0.0571, 0.04390, -1.0189 0.0283, 0.02940, -1.0183 0.0142, 0.01970, -1.0246 0.0081, 0.01410, -1.0467 0.0026, 0.00780, -0.9172 0.0000, 0.00000, -1.0174 0.0037, -0.00840, -0.6207 0.0112, -0.01420, 0.2215 0.0191, -0.01930, 0.5821 0.0397, -0.03030, 0.8996 0.0706, -0.04420, 0.9922 0.1037, -0.05710, 0.9930 0.1384, -0.06890, 0.9546 0.1741, -0.07950, 0.8630 0.2102, -0.08660, 0.7202 0.2472, -0.09640, 0.5979 0.2844, -0.10270, 0.4232 0.3225, -0.10690, 0.2825 0.3608, -0.10890, 0.0687 0.3991, -0.10830, -0.1119 0.4373, -0.10510, -0.2818 0.4757, -0.09890, -0.4040 0.5137, -0.09070, -0.5629 0.5694, -0.07640, -0.6199 15 Flap element taps 1.0000, 0.00130, -1.1137 0.9365, 0.01390, -1.0586 0.8333, 0.03280, -1.0339 0.7436, 0.04930, -1.0373 0.7049, 0.05670, -1.0302 0.6662, 0.06410, -1.0309 0.6522, 0.01390, -1.5780 0.5969, -0.00020, -1.5726 0.6000, -0.03020, -1.0513 0.6324, -0.04540, -0.9655 0.6667, -0.04880, -0.9511 0.7046, -0.04110, -0.9456 0.7429, -0.03210, -0.9747 0.8333, -0.01400, -0.9906 0.9311, -0.00120, -0.9891 --------- Run Conditions: vel=101.6 ft/s Re=0.997x10^6 AOA=59.98 Flap deflection=-90.00 Totals: Cl=0.3035 Cdp=0.9739 Cm(c/4)=-0.0098 Cs=-0.2245 Ch=0.0458 Main component: Cl=0.3317 Cdp=1.0097 Cm=-0.2957 Flap component: Cl=-0.0282 Cdp=-0.0358 Cm=0.0371 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8637 0.6175, -0.04610, -1.9302 0.5841, -0.02440, -1.9087 0.5775, 0.01750, -1.9205 0.5777, 0.04660, -1.9181 0.6274, 0.07170, -1.2781 0.5694, 0.08320, -1.2803 0.5112, 0.09370, -1.2929 0.4731, 0.09830, -1.2837 0.4349, 0.10070, -1.2806 0.3960, 0.10120, -1.2997 0.3566, 0.10020, -1.2825 0.3172, 0.09790, -1.2746 0.2778, 0.09440, -1.2729 0.2393, 0.08960, -1.2620 0.2056, 0.08360, -1.2756 0.1633, 0.07610, -1.2606 0.1261, 0.06710, -1.2680 0.0900, 0.05640, -1.2503 0.0571, 0.04390, -1.2490 0.0283, 0.02940, -1.2429 0.0142, 0.01970, -1.2401 0.0081, 0.01410, -1.2497 0.0026, 0.00780, -1.1393 0.0000, 0.00000, -1.2448 0.0037, -0.00840, -1.3027 0.0112, -0.01420, -0.4787 0.0191, -0.01930, 0.0059 0.0397, -0.03030, 0.5384 0.0706, -0.04420, 0.8155 0.1037, -0.05710, 0.9477 0.1384, -0.06890, 0.9976 0.1741, -0.07950, 0.9971 0.2102, -0.08660, 0.9511 0.2472, -0.09640, 0.8855 0.2844, -0.10270, 0.7781 0.3225, -0.10690, 0.6697 0.3608, -0.10890, 0.4957 0.3991, -0.10830, 0.3275 0.4373, -0.10510, 0.1539 0.4757, -0.09890, -0.0091 0.5137, -0.09070, -0.2181 0.5694, -0.07640, -0.4054 15 Flap element taps 1.0000, 0.00130, -1.6648 0.9365, 0.01390, -1.3557 0.8333, 0.03280, -1.3071 0.7436, 0.04930, -1.2878 0.7049, 0.05670, -1.2807 0.6662, 0.06410, -1.2755 0.6522, 0.01390, -1.9252 0.5969, -0.00020, -1.9342 0.6000, -0.03020, -2.1089 0.6324, -0.04540, -1.3866 0.6667, -0.04880, -1.3510 0.7046, -0.04110, -1.3436 0.7429, -0.03210, -1.3661 0.8333, -0.01400, -1.4012 0.9311, -0.00120, -1.4481 --------- Run Conditions: vel=100.9 ft/s Re=0.988x10^6 AOA=70.01 Flap deflection=-90.00 Totals: Cl=0.1962 Cdp=1.1781 Cm(c/4)=-0.0412 Cs=-0.2183 Ch=0.0637 Main component: Cl=0.2752 Cdp=1.1732 Cm=-0.3640 Flap component: Cl=-0.0790 Cdp=0.0049 Cm=0.0292 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5670 0.6175, -0.04610, -1.6563 0.5841, -0.02440, -1.6206 0.5775, 0.01750, -1.6284 0.5777, 0.04660, -1.6287 0.6274, 0.07170, -1.3904 0.5694, 0.08320, -1.4010 0.5112, 0.09370, -1.4410 0.4731, 0.09830, -1.4338 0.4349, 0.10070, -1.4350 0.3960, 0.10120, -1.4632 0.3566, 0.10020, -1.4465 0.3172, 0.09790, -1.4388 0.2778, 0.09440, -1.4390 0.2393, 0.08960, -1.4318 0.2056, 0.08360, -1.4442 0.1633, 0.07610, -1.4223 0.1261, 0.06710, -1.4274 0.0900, 0.05640, -1.4027 0.0571, 0.04390, -1.3947 0.0283, 0.02940, -1.3858 0.0142, 0.01970, -1.3790 0.0081, 0.01410, -1.3898 0.0026, 0.00780, -1.2667 0.0000, 0.00000, -1.3794 0.0037, -0.00840, -1.5474 0.0112, -0.01420, -0.9241 0.0191, -0.01930, -0.4170 0.0397, -0.03030, 0.2042 0.0706, -0.04420, 0.5776 0.1037, -0.05710, 0.7890 0.1384, -0.06890, 0.9142 0.1741, -0.07950, 0.9773 0.2102, -0.08660, 0.9842 0.2472, -0.09640, 0.9837 0.2844, -0.10270, 0.9310 0.3225, -0.10690, 0.8788 0.3608, -0.10890, 0.7553 0.3991, -0.10830, 0.6292 0.4373, -0.10510, 0.4792 0.4757, -0.09890, 0.3200 0.5137, -0.09070, 0.1220 0.5694, -0.07640, -0.0996 15 Flap element taps 1.0000, 0.00130, -1.9583 0.9365, 0.01390, -1.5659 0.8333, 0.03280, -1.4824 0.7436, 0.04930, -1.4397 0.7049, 0.05670, -1.4149 0.6662, 0.06410, -1.3949 0.6522, 0.01390, -1.6623 0.5969, -0.00020, -1.6697 0.6000, -0.03020, -2.5770 0.6324, -0.04540, -1.6959 0.6667, -0.04880, -1.6216 0.7046, -0.04110, -1.6128 0.7429, -0.03210, -1.6403 0.8333, -0.01400, -1.6874 0.9311, -0.00120, -1.7107 --------- Run Conditions: vel=102.2 ft/s Re=1.001x10^6 AOA=79.98 Flap deflection=-90.00 Totals: Cl=0.0548 Cdp=1.3520 Cm(c/4)=-0.0815 Cs=-0.1813 Ch=0.0661 Main component: Cl=0.1841 Cdp=1.3104 Cm=-0.4230 Flap component: Cl=-0.1293 Cdp=0.0416 Cm=0.0063 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2203 0.6175, -0.04610, -1.2633 0.5841, -0.02440, -1.1906 0.5775, 0.01750, -1.2036 0.5777, 0.04660, -1.1820 0.6274, 0.07170, -1.5164 0.5694, 0.08320, -1.5358 0.5112, 0.09370, -1.5606 0.4731, 0.09830, -1.5781 0.4349, 0.10070, -1.5984 0.3960, 0.10120, -1.6390 0.3566, 0.10020, -1.6277 0.3172, 0.09790, -1.6371 0.2778, 0.09440, -1.6509 0.2393, 0.08960, -1.6383 0.2056, 0.08360, -1.6421 0.1633, 0.07610, -1.6075 0.1261, 0.06710, -1.5955 0.0900, 0.05640, -1.5550 0.0571, 0.04390, -1.5373 0.0283, 0.02940, -1.5164 0.0142, 0.01970, -1.5038 0.0081, 0.01410, -1.5100 0.0026, 0.00780, -1.3750 0.0000, 0.00000, -1.4912 0.0037, -0.00840, -1.6117 0.0112, -0.01420, -1.2909 0.0191, -0.01930, -0.8117 0.0397, -0.03030, -0.1536 0.0706, -0.04420, 0.2832 0.1037, -0.05710, 0.5517 0.1384, -0.06890, 0.7372 0.1741, -0.07950, 0.8566 0.2102, -0.08660, 0.9203 0.2472, -0.09640, 0.9769 0.2844, -0.10270, 0.9796 0.3225, -0.10690, 0.9851 0.3608, -0.10890, 0.9209 0.3991, -0.10830, 0.8471 0.4373, -0.10510, 0.7386 0.4757, -0.09890, 0.6061 0.5137, -0.09070, 0.4356 0.5694, -0.07640, 0.2169 15 Flap element taps 1.0000, 0.00130, -2.2504 0.9365, 0.01390, -1.8142 0.8333, 0.03280, -1.6856 0.7436, 0.04930, -1.5919 0.7049, 0.05670, -1.5613 0.6662, 0.06410, -1.5011 0.6522, 0.01390, -1.3228 0.5969, -0.00020, -1.2899 0.6000, -0.03020, -2.5322 0.6324, -0.04540, -1.9746 0.6667, -0.04880, -1.9026 0.7046, -0.04110, -1.8916 0.7429, -0.03210, -1.9130 0.8333, -0.01400, -1.9614 0.9311, -0.00120, -1.9763 --------- Run Conditions: vel=102.5 ft/s Re=1.003x10^6 AOA=90.04 Flap deflection=-90.00 Totals: Cl=-0.1885 Cdp=1.3686 Cm(c/4)=-0.0948 Cs=-0.1875 Ch=0.1178 Main component: Cl=0.0429 Cdp=1.3209 Cm=-0.4381 Flap component: Cl=-0.2314 Cdp=0.0477 Cm=0.0011 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.1242 0.6175, -0.04610, -0.8414 0.5841, -0.02440, -0.7545 0.5775, 0.01750, -0.7575 0.5777, 0.04660, -0.7400 0.6274, 0.07170, -1.4512 0.5694, 0.08320, -1.4662 0.5112, 0.09370, -1.5352 0.4731, 0.09830, -1.5653 0.4349, 0.10070, -1.5873 0.3960, 0.10120, -1.6334 0.3566, 0.10020, -1.6396 0.3172, 0.09790, -1.6564 0.2778, 0.09440, -1.6697 0.2393, 0.08960, -1.6631 0.2056, 0.08360, -1.6798 0.1633, 0.07610, -1.6479 0.1261, 0.06710, -1.6458 0.0900, 0.05640, -1.6027 0.0571, 0.04390, -1.5711 0.0283, 0.02940, -1.5423 0.0142, 0.01970, -1.5270 0.0081, 0.01410, -1.5362 0.0026, 0.00780, -1.3953 0.0000, 0.00000, -1.5122 0.0037, -0.00840, -1.5407 0.0112, -0.01420, -1.4977 0.0191, -0.01930, -1.0995 0.0397, -0.03030, -0.4707 0.0706, -0.04420, -0.0145 0.1037, -0.05710, 0.2833 0.1384, -0.06890, 0.5064 0.1741, -0.07950, 0.6680 0.2102, -0.08660, 0.7773 0.2472, -0.09640, 0.8795 0.2844, -0.10270, 0.9359 0.3225, -0.10690, 0.9950 0.3608, -0.10890, 0.9880 0.3991, -0.10830, 0.9726 0.4373, -0.10510, 0.9152 0.4757, -0.09890, 0.8235 0.5137, -0.09070, 0.6931 0.5694, -0.07640, 0.5024 15 Flap element taps 1.0000, 0.00130, -2.2310 0.9365, 0.01390, -1.7494 0.8333, 0.03280, -1.6194 0.7436, 0.04930, -1.5284 0.7049, 0.05670, -1.5116 0.6662, 0.06410, -1.4563 0.6522, 0.01390, -0.9061 0.5969, -0.00020, -0.8595 0.6000, -0.03020, -2.3919 0.6324, -0.04540, -2.1561 0.6667, -0.04880, -2.0723 0.7046, -0.04110, -2.0468 0.7429, -0.03210, -2.0735 0.8333, -0.01400, -2.1464 0.9311, -0.00120, -2.0828 --------- Run Conditions: vel=101.3 ft/s Re=0.992x10^6 AOA=120.01 Flap deflection=-90.00 Totals: Cl=-0.2148 Cdp=1.0534 Cm(c/4)=-0.1894 Cs=0.3409 Ch=-0.2754 Main component: Cl=-0.2353 Cdp=0.9896 Cm=-0.3675 Flap component: Cl=0.0206 Cdp=0.0638 Cm=-0.0768 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.9506 0.6175, -0.04610, 0.6337 0.5841, -0.02440, 0.6533 0.5775, 0.01750, 0.6211 0.5777, 0.04660, 0.6165 0.6274, 0.07170, -1.4176 0.5694, 0.08320, -1.4359 0.5112, 0.09370, -1.4714 0.4731, 0.09830, -1.4629 0.4349, 0.10070, -1.4730 0.3960, 0.10120, -1.4948 0.3566, 0.10020, -1.5008 0.3172, 0.09790, -1.5005 0.2778, 0.09440, -1.5022 0.2393, 0.08960, -1.5012 0.2056, 0.08360, -1.5068 0.1633, 0.07610, -1.5090 0.1261, 0.06710, -1.5257 0.0900, 0.05640, -1.5036 0.0571, 0.04390, -1.4963 0.0283, 0.02940, -1.4763 0.0142, 0.01970, -1.4547 0.0081, 0.01410, -1.4568 0.0026, 0.00780, -1.3251 0.0000, 0.00000, -1.4386 0.0037, -0.00840, -1.4317 0.0112, -0.01420, -1.4904 0.0191, -0.01930, -1.5165 0.0397, -0.03030, -1.2412 0.0706, -0.04420, -0.9348 0.1037, -0.05710, -0.6946 0.1384, -0.06890, -0.4775 0.1741, -0.07950, -0.2923 0.2102, -0.08660, -0.1317 0.2472, -0.09640, 0.0255 0.2844, -0.10270, 0.1856 0.3225, -0.10690, 0.3597 0.3608, -0.10890, 0.5014 0.3991, -0.10830, 0.6547 0.4373, -0.10510, 0.7864 0.4757, -0.09890, 0.8832 0.5137, -0.09070, 0.9457 0.5694, -0.07640, 1.0003 15 Flap element taps 1.0000, 0.00130, -1.4865 0.9365, 0.01390, -1.4731 0.8333, 0.03280, -1.4524 0.7436, 0.04930, -1.4127 0.7049, 0.05670, -1.4155 0.6662, 0.06410, -1.4085 0.6522, 0.01390, 0.6523 0.5969, -0.00020, 0.5421 0.6000, -0.03020, -2.8317 0.6324, -0.04540, -1.6866 0.6667, -0.04880, -1.8520 0.7046, -0.04110, -0.9923 0.7429, -0.03210, -0.7062 0.8333, -0.01400, -0.5183 0.9311, -0.00120, -0.5949 --------- Run Conditions: vel=102.4 ft/s Re=1.003x10^6 AOA=150.01 Flap deflection=-90.00 Totals: Cl=0.2758 Cdp=0.8615 Cm(c/4)=-0.2074 Cs=0.8840 Ch=-0.5397 Main component: Cl=0.0807 Cdp=0.3334 Cm=-0.0745 Flap component: Cl=0.1951 Cdp=0.5281 Cm=-0.1809 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2633 0.6175, -0.04610, 0.8105 0.5841, -0.02440, 0.8192 0.5775, 0.01750, 0.7854 0.5777, 0.04660, 0.8104 0.6274, 0.07170, -1.2349 0.5694, 0.08320, -1.2448 0.5112, 0.09370, -1.2757 0.4731, 0.09830, -1.2916 0.4349, 0.10070, -1.3058 0.3960, 0.10120, -1.3218 0.3566, 0.10020, -1.3114 0.3172, 0.09790, -1.3235 0.2778, 0.09440, -1.3236 0.2393, 0.08960, -1.3219 0.2056, 0.08360, -1.3493 0.1633, 0.07610, -1.3308 0.1261, 0.06710, -1.3404 0.0900, 0.05640, -1.3211 0.0571, 0.04390, -1.3303 0.0283, 0.02940, -1.3103 0.0142, 0.01970, -1.2916 0.0081, 0.01410, -1.2968 0.0026, 0.00780, -1.1570 0.0000, 0.00000, -1.2658 0.0037, -0.00840, -1.3496 0.0112, -0.01420, -1.7104 0.0191, -0.01930, -1.8273 0.0397, -0.03030, -1.8069 0.0706, -0.04420, -1.7396 0.1037, -0.05710, -1.6828 0.1384, -0.06890, -1.6017 0.1741, -0.07950, -1.5567 0.2102, -0.08660, -1.5049 0.2472, -0.09640, -1.4723 0.2844, -0.10270, -1.3808 0.3225, -0.10690, -1.2580 0.3608, -0.10890, -1.1558 0.3991, -0.10830, -0.9721 0.4373, -0.10510, -0.7532 0.4757, -0.09890, -0.5007 0.5137, -0.09070, -0.2757 0.5694, -0.07640, 0.0665 15 Flap element taps 1.0000, 0.00130, -1.2674 0.9365, 0.01390, -1.2709 0.8333, 0.03280, -1.2654 0.7436, 0.04930, -1.2289 0.7049, 0.05670, -1.2365 0.6662, 0.06410, -1.2374 0.6522, 0.01390, 0.7940 0.5969, -0.00020, 0.7958 0.6000, -0.03020, 0.9152 0.6324, -0.04540, 0.9819 0.6667, -0.04880, 0.8444 0.7046, -0.04110, 0.7690 0.7429, -0.03210, 0.6973 0.8333, -0.01400, 0.5184 0.9311, -0.00120, 0.2016 --------- Run Conditions: vel=104.4 ft/s Re=1.024x10^6 AOA=180.06 Flap deflection=-90.00 Totals: Cl=0.5859 Cdp=0.3596 Cm(c/4)=0.0313 Cs=0.3590 Ch=-0.4073 Main component: Cl=0.4179 Cdp=-0.1768 Cm=0.1648 Flap component: Cl=0.1680 Cdp=0.5365 Cm=0.0131 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.9931 0.6175, -0.04610, -1.9453 0.5841, -0.02440, -1.9039 0.5775, 0.01750, -1.9610 0.5777, 0.04660, -1.7327 0.6274, 0.07170, -0.6476 0.5694, 0.08320, -0.6517 0.5112, 0.09370, -0.6655 0.4731, 0.09830, -0.6478 0.4349, 0.10070, -0.6609 0.3960, 0.10120, -0.6890 0.3566, 0.10020, -0.6522 0.3172, 0.09790, -0.6547 0.2778, 0.09440, -0.6589 0.2393, 0.08960, -0.6508 0.2056, 0.08360, -0.6953 0.1633, 0.07610, -0.6570 0.1261, 0.06710, -0.6756 0.0900, 0.05640, -0.6489 0.0571, 0.04390, -0.6551 0.0283, 0.02940, -0.6490 0.0142, 0.01970, -0.6520 0.0081, 0.01410, -0.6857 0.0026, 0.00780, -0.5998 0.0000, 0.00000, -0.6702 0.0037, -0.00840, -0.6729 0.0112, -0.01420, -0.6624 0.0191, -0.01930, -0.6564 0.0397, -0.03030, -0.6526 0.0706, -0.04420, -0.6895 0.1037, -0.05710, -0.7298 0.1384, -0.06890, -0.7798 0.1741, -0.07950, -0.9426 0.2102, -0.08660, -1.1470 0.2472, -0.09640, -1.3481 0.2844, -0.10270, -1.5370 0.3225, -0.10690, -1.6655 0.3608, -0.10890, -1.8227 0.3991, -0.10830, -1.8780 0.4373, -0.10510, -1.8721 0.4757, -0.09890, -1.7900 0.5137, -0.09070, -1.7192 0.5694, -0.07640, -1.6025 15 Flap element taps 1.0000, 0.00130, -0.6421 0.9365, 0.01390, -0.6373 0.8333, 0.03280, -0.6409 0.7436, 0.04930, -0.6493 0.7049, 0.05670, -0.6491 0.6662, 0.06410, -0.6492 0.6522, 0.01390, -2.0635 0.5969, -0.00020, -1.9586 0.6000, -0.03020, -1.5915 0.6324, -0.04540, -0.6279 0.6667, -0.04880, 0.2319 0.7046, -0.04110, 0.8192 0.7429, -0.03210, 0.9465 0.8333, -0.01400, 0.9928 0.9311, -0.00120, 0.8619 --------- Run Conditions: vel=103.0 ft/s Re=1.010x10^6 AOA=210.00 Flap deflection=-90.00 Totals: Cl=-0.3204 Cdp=0.4312 Cm(c/4)=-0.0900 Cs=0.5336 Ch=-0.5216 Main component: Cl=-0.1252 Cdp=-0.0428 Cm=-0.0361 Flap component: Cl=-0.1952 Cdp=0.4739 Cm=-0.0693 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7421 0.6175, -0.04610, -0.7747 0.5841, -0.02440, -0.7641 0.5775, 0.01750, -0.7735 0.5777, 0.04660, -0.7845 0.6274, 0.07170, -0.9135 0.5694, 0.08320, -0.9112 0.5112, 0.09370, -0.9327 0.4731, 0.09830, -0.9266 0.4349, 0.10070, -0.9373 0.3960, 0.10120, -0.9759 0.3566, 0.10020, -0.9401 0.3172, 0.09790, -0.9497 0.2778, 0.09440, -0.9630 0.2393, 0.08960, -0.9697 0.2056, 0.08360, -1.0294 0.1633, 0.07610, -0.9933 0.1261, 0.06710, -1.0180 0.0900, 0.05640, -0.9982 0.0571, 0.04390, -1.0246 0.0283, 0.02940, -1.0693 0.0142, 0.01970, -1.1208 0.0081, 0.01410, -1.2010 0.0026, 0.00780, -1.1219 0.0000, 0.00000, -1.2884 0.0037, -0.00840, -0.9688 0.0112, -0.01420, -0.8346 0.0191, -0.01930, -0.7883 0.0397, -0.03030, -0.7475 0.0706, -0.04420, -0.7630 0.1037, -0.05710, -0.7626 0.1384, -0.06890, -0.7277 0.1741, -0.07950, -0.7440 0.2102, -0.08660, -0.7777 0.2472, -0.09640, -0.7617 0.2844, -0.10270, -0.7786 0.3225, -0.10690, -0.7330 0.3608, -0.10890, -0.7624 0.3991, -0.10830, -0.7428 0.4373, -0.10510, -0.7608 0.4757, -0.09890, -0.7643 0.5137, -0.09070, -0.7624 0.5694, -0.07640, -0.7388 15 Flap element taps 1.0000, 0.00130, -0.8865 0.9365, 0.01390, -0.8890 0.8333, 0.03280, -0.9068 0.7436, 0.04930, -0.9192 0.7049, 0.05670, -0.9173 0.6662, 0.06410, -0.9154 0.6522, 0.01390, -0.7773 0.5969, -0.00020, -0.7759 0.6000, -0.03020, -0.7582 0.6324, -0.04540, -0.8850 0.6667, -0.04880, -0.3065 0.7046, -0.04110, 0.4858 0.7429, -0.03210, 0.7280 0.8333, -0.01400, 0.9392 0.9311, -0.00120, 0.9999 --------- Run Conditions: vel=97.2 ft/s Re=0.954x10^6 AOA=239.98 Flap deflection=-90.00 Totals: Cl=0.7897 Cdp=0.7355 Cm(c/4)=0.2307 Cs=-0.3159 Ch=0.2365 Main component: Cl=0.4204 Cdp=0.7823 Cm=0.3371 Flap component: Cl=0.3693 Cdp=-0.0469 Cm=0.1516 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.2587 0.6175, -0.04610, -1.2948 0.5841, -0.02440, -1.2715 0.5775, 0.01750, -1.2728 0.5777, 0.04660, -1.2848 0.6274, 0.07170, 0.8310 0.5694, 0.08320, 0.8411 0.5112, 0.09370, 0.8579 0.4731, 0.09830, 0.8549 0.4349, 0.10070, 0.8018 0.3960, 0.10120, 0.6840 0.3566, 0.10020, 0.6289 0.3172, 0.09790, 0.5119 0.2778, 0.09440, 0.3716 0.2393, 0.08960, 0.2199 0.2056, 0.08360, -0.0151 0.1633, 0.07610, -0.1668 0.1261, 0.06710, -0.4263 0.0900, 0.05640, -0.6915 0.0571, 0.04390, -1.0989 0.0283, 0.02940, -1.4012 0.0142, 0.01970, -1.3643 0.0081, 0.01410, -1.3564 0.0026, 0.00780, -1.1518 0.0000, 0.00000, -1.2402 0.0037, -0.00840, -1.2342 0.0112, -0.01420, -1.2354 0.0191, -0.01930, -1.2349 0.0397, -0.03030, -1.2381 0.0706, -0.04420, -1.2637 0.1037, -0.05710, -1.2583 0.1384, -0.06890, -1.2190 0.1741, -0.07950, -1.2429 0.2102, -0.08660, -1.2831 0.2472, -0.09640, -1.2785 0.2844, -0.10270, -1.3120 0.3225, -0.10690, -1.2905 0.3608, -0.10890, -1.3449 0.3991, -0.10830, -1.3203 0.4373, -0.10510, -1.3327 0.4757, -0.09890, -1.3231 0.5137, -0.09070, -1.3304 0.5694, -0.07640, -1.2743 15 Flap element taps 1.0000, 0.00130, 1.0025 0.9365, 0.01390, 0.7507 0.8333, 0.03280, 0.8032 0.7436, 0.04930, 0.7942 0.7049, 0.05670, 0.8126 0.6662, 0.06410, 0.8373 0.6522, 0.01390, -1.2819 0.5969, -0.00020, -1.2955 0.6000, -0.03020, -1.4529 0.6324, -0.04540, -2.2297 0.6667, -0.04880, -2.2000 0.7046, -0.04110, -0.8123 0.7429, -0.03210, -0.3290 0.8333, -0.01400, 0.1222 0.9311, -0.00120, 0.4865 --------- Run Conditions: vel=100.3 ft/s Re=0.981x10^6 AOA=269.03 Flap deflection=-90.00 Totals: Cl=0.9620 Cdp=1.4880 Cm(c/4)=0.3770 Cs=-0.9367 Ch=0.9066 Main component: Cl=0.0748 Cdp=1.4069 Cm=0.4931 Flap component: Cl=0.8872 Cdp=0.0812 Cm=0.2600 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.8701 0.6175, -0.04610, -1.8934 0.5841, -0.02440, -1.8754 0.5775, 0.01750, -1.8957 0.5777, 0.04660, -1.9003 0.6274, 0.07170, 0.9964 0.5694, 0.08320, 1.0171 0.5112, 0.09370, 0.9897 0.4731, 0.09830, 0.9837 0.4349, 0.10070, 0.9622 0.3960, 0.10120, 0.8957 0.3566, 0.10020, 0.9040 0.3172, 0.09790, 0.8525 0.2778, 0.09440, 0.7851 0.2393, 0.08960, 0.7004 0.2056, 0.08360, 0.5307 0.1633, 0.07610, 0.4238 0.1261, 0.06710, 0.1865 0.0900, 0.05640, -0.0911 0.0571, 0.04390, -0.5912 0.0283, 0.02940, -1.2030 0.0142, 0.01970, -1.6094 0.0081, 0.01410, -1.6434 0.0026, 0.00780, -1.3707 0.0000, 0.00000, -1.4919 0.0037, -0.00840, -1.5219 0.0112, -0.01420, -1.5508 0.0191, -0.01930, -1.5599 0.0397, -0.03030, -1.5742 0.0706, -0.04420, -1.6774 0.1037, -0.05710, -1.7509 0.1384, -0.06890, -1.7684 0.1741, -0.07950, -1.8097 0.2102, -0.08660, -1.8474 0.2472, -0.09640, -1.8287 0.2844, -0.10270, -1.8482 0.3225, -0.10690, -1.8175 0.3608, -0.10890, -1.8687 0.3991, -0.10830, -1.8665 0.4373, -0.10510, -1.9126 0.4757, -0.09890, -1.9329 0.5137, -0.09070, -1.9540 0.5694, -0.07640, -1.9150 15 Flap element taps 1.0000, 0.00130, -1.8012 0.9365, 0.01390, 1.0080 0.8333, 0.03280, 1.0028 0.7436, 0.04930, 0.9895 0.7049, 0.05670, 0.9978 0.6662, 0.06410, 0.9940 0.6522, 0.01390, -1.8888 0.5969, -0.00020, -1.9386 0.6000, -0.03020, -1.9838 0.6324, -0.04540, -1.9273 0.6667, -0.04880, -1.9426 0.7046, -0.04110, -1.8929 0.7429, -0.03210, -1.8894 0.8333, -0.01400, -1.8568 0.9311, -0.00120, -1.7973