S809 UNVENTED AILERON, LEGR, CHORD = 18 IN --------- Run Conditions: vel=103.8 ft/s Re=1.003x10^6 AOA=-6.00 Flap deflection=-5.00 Totals: Cl=-0.6197 Cdp=0.0494 Cm(c/4)=0.0295 Cs=0.0156 Ch=0.0781 Main component: Cl=-0.5347 Cdp=0.0366 Cm=0.1161 Flap component: Cl=-0.0850 Cdp=0.0128 Cm=0.0687 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2758 0.6175, -0.04610, -0.2469 0.5841, -0.02440, -0.2261 0.5775, 0.01750, -0.2243 0.5777, 0.04660, -0.2245 0.6274, 0.07170, 0.0586 0.5694, 0.08320, -0.0802 0.5112, 0.09370, -0.2986 0.4731, 0.09830, -0.3493 0.4349, 0.10070, -0.3439 0.3960, 0.10120, -0.3106 0.3566, 0.10020, -0.2231 0.3172, 0.09790, -0.1654 0.2778, 0.09440, -0.1118 0.2393, 0.08960, -0.0528 0.2056, 0.08360, -0.0117 0.1633, 0.07610, 0.1263 0.1261, 0.06710, 0.2272 0.0900, 0.05640, 0.3423 0.0571, 0.04390, 0.6072 0.0283, 0.02940, 0.8696 0.0142, 0.01970, 1.0060 0.0081, 0.01410, 0.9725 0.0026, 0.00780, 0.5976 0.0000, 0.00000, -0.0357 0.0037, -0.00840, -1.8786 0.0112, -0.01420, -1.3387 0.0191, -0.01930, -1.2017 0.0397, -0.03030, -0.9495 0.0706, -0.04420, -0.9412 0.1037, -0.05710, -0.8960 0.1384, -0.06890, -0.9497 0.1741, -0.07950, -0.9935 0.2102, -0.08660, -1.0847 0.2472, -0.09640, -1.1341 0.2844, -0.10270, -1.1571 0.3225, -0.10690, -1.1256 0.3608, -0.10890, -1.1192 0.3991, -0.10830, -1.0112 0.4373, -0.10510, -0.8525 0.4757, -0.09890, -0.6024 0.5137, -0.09070, -0.4059 0.5694, -0.07640, -0.2852 14 Flap element taps 1.0000, 0.00130, -0.1972 0.9365, 0.01390, -0.0627 0.8333, 0.03280, -0.0095 0.7436, 0.04930, 0.0137 0.7049, 0.05670, 0.0493 0.6662, 0.06410, 0.1029 0.6522, 0.01390, -0.2260 0.5969, -0.00020, -0.2310 0.6000, -0.03020, -0.2646 0.6324, -0.04540, -0.2661 0.6667, -0.04880, -0.2661 0.7046, -0.04110, -0.2588 0.7429, -0.03210, -0.2732 0.9311, -0.00120, -0.2788 --------- Run Conditions: vel=103.1 ft/s Re=1.000x10^6 AOA=0.01 Flap deflection=-5.00 Totals: Cl=-0.2289 Cdp=0.0051 Cm(c/4)=0.0234 Cs=-0.0051 Ch=0.0225 Main component: Cl=-0.2043 Cdp=0.0099 Cm=0.0612 Flap component: Cl=-0.0247 Cdp=-0.0048 Cm=0.0194 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1777 0.6175, -0.04610, -0.0868 0.5841, -0.02440, -0.0875 0.5775, 0.01750, -0.0883 0.5777, 0.04660, -0.0875 0.6274, 0.07170, -0.0052 0.5694, 0.08320, -0.1453 0.5112, 0.09370, -0.4116 0.4731, 0.09830, -0.4959 0.4349, 0.10070, -0.5318 0.3960, 0.10120, -0.5591 0.3566, 0.10020, -0.4506 0.3172, 0.09790, -0.4197 0.2778, 0.09440, -0.3960 0.2393, 0.08960, -0.3746 0.2056, 0.08360, -0.4031 0.1633, 0.07610, -0.2560 0.1261, 0.06710, -0.2163 0.0900, 0.05640, -0.1776 0.0571, 0.04390, 0.0782 0.0283, 0.02940, 0.3471 0.0142, 0.01970, 0.5912 0.0081, 0.01410, 0.7057 0.0026, 0.00780, 0.9135 0.0000, 0.00000, -0.1537 0.0037, -0.00840, 0.2870 0.0112, -0.01420, 0.1004 0.0191, -0.01930, -0.0305 0.0397, -0.03030, -0.0889 0.0706, -0.04420, -0.2683 0.1037, -0.05710, -0.3426 0.1384, -0.06890, -0.4391 0.1741, -0.07950, -0.5553 0.2102, -0.08660, -0.7390 0.2472, -0.09640, -0.8225 0.2844, -0.10270, -0.9202 0.3225, -0.10690, -0.9215 0.3608, -0.10890, -1.0074 0.3991, -0.10830, -0.9647 0.4373, -0.10510, -0.9221 0.4757, -0.09890, -0.7555 0.5137, -0.09070, -0.6100 0.5694, -0.07640, -0.3307 14 Flap element taps 1.0000, 0.00130, 0.0434 0.9365, 0.01390, 0.0505 0.8333, 0.03280, 0.0202 0.7436, 0.04930, 0.0036 0.7049, 0.05670, 0.0125 0.6662, 0.06410, 0.0361 0.6522, 0.01390, -0.1033 0.5969, -0.00020, -0.0851 0.6000, -0.03020, -0.1010 0.6324, -0.04540, -0.1205 0.6667, -0.04880, -0.1238 0.7046, -0.04110, -0.0741 0.7429, -0.03210, -0.0755 0.9311, -0.00120, -0.0048 Wake drag found for this condition, Cdw=0.0201 --------- Run Conditions: vel=103.3 ft/s Re=1.002x10^6 AOA=3.03 Flap deflection=-5.00 Totals: Cl=0.0212 Cdp=0.0006 Cm(c/4)=0.0242 Cs=0.0005 Ch=0.0048 Main component: Cl=0.0280 Cdp=0.0174 Cm=0.0141 Flap component: Cl=-0.0068 Cdp=-0.0168 Cm=0.0048 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2113 0.6175, -0.04610, -0.1292 0.5841, -0.02440, -0.1331 0.5775, 0.01750, -0.1342 0.5777, 0.04660, -0.1350 0.6274, 0.07170, -0.0489 0.5694, 0.08320, -0.1860 0.5112, 0.09370, -0.4793 0.4731, 0.09830, -0.5872 0.4349, 0.10070, -0.6428 0.3960, 0.10120, -0.7149 0.3566, 0.10020, -0.5946 0.3172, 0.09790, -0.5830 0.2778, 0.09440, -0.5756 0.2393, 0.08960, -0.5785 0.2056, 0.08360, -0.6589 0.1633, 0.07610, -0.5056 0.1261, 0.06710, -0.5169 0.0900, 0.05640, -0.5321 0.0571, 0.04390, -0.3205 0.0283, 0.02940, -0.1205 0.0142, 0.01970, 0.0843 0.0081, 0.01410, 0.1642 0.0026, 0.00780, 0.4278 0.0000, 0.00000, -0.2662 0.0037, -0.00840, 0.8623 0.0112, -0.01420, 0.6346 0.0191, -0.01930, 0.4724 0.0397, -0.03030, 0.3083 0.0706, -0.04420, 0.0714 0.1037, -0.05710, -0.0577 0.1384, -0.06890, -0.1448 0.1741, -0.07950, -0.2887 0.2102, -0.08660, -0.5175 0.2472, -0.09640, -0.6008 0.2844, -0.10270, -0.7339 0.3225, -0.10690, -0.7367 0.3608, -0.10890, -0.8610 0.3991, -0.10830, -0.8338 0.4373, -0.10510, -0.8383 0.4757, -0.09890, -0.7044 0.5137, -0.09070, -0.5966 0.5694, -0.07640, -0.3375 14 Flap element taps 1.0000, 0.00130, 0.1618 0.9365, 0.01390, 0.1099 0.8333, 0.03280, 0.0353 0.7436, 0.04930, -0.0053 0.7049, 0.05670, -0.0142 0.6662, 0.06410, -0.0092 0.6522, 0.01390, -0.1570 0.5969, -0.00020, -0.1302 0.6000, -0.03020, -0.1488 0.6324, -0.04540, -0.1721 0.6667, -0.04880, -0.1762 0.7046, -0.04110, -0.0734 0.7429, -0.03210, -0.0434 0.9311, -0.00120, 0.1433 Wake drag found for this condition, Cdw=0.0153 --------- Run Conditions: vel=103.5 ft/s Re=1.005x10^6 AOA=6.03 Flap deflection=-5.00 Totals: Cl=0.3153 Cdp=0.0085 Cm(c/4)=0.0173 Cs=0.0247 Ch=-0.0200 Main component: Cl=0.2943 Cdp=0.0308 Cm=-0.0446 Flap component: Cl=0.0210 Cdp=-0.0223 Cm=-0.0167 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1907 0.6175, -0.04610, -0.1420 0.5841, -0.02440, -0.1537 0.5775, 0.01750, -0.1554 0.5777, 0.04660, -0.1569 0.6274, 0.07170, -0.1140 0.5694, 0.08320, -0.2373 0.5112, 0.09370, -0.5541 0.4731, 0.09830, -0.6876 0.4349, 0.10070, -0.7656 0.3960, 0.10120, -0.8807 0.3566, 0.10020, -0.7568 0.3172, 0.09790, -0.7638 0.2778, 0.09440, -0.7756 0.2393, 0.08960, -0.8086 0.2056, 0.08360, -0.9395 0.1633, 0.07610, -0.7951 0.1261, 0.06710, -0.8627 0.0900, 0.05640, -0.9441 0.0571, 0.04390, -0.8175 0.0283, 0.02940, -0.7575 0.0142, 0.01970, -0.6310 0.0081, 0.01410, -0.8049 0.0026, 0.00780, -0.2128 0.0000, 0.00000, -0.3861 0.0037, -0.00840, 1.0161 0.0112, -0.01420, 0.9516 0.0191, -0.01930, 0.8338 0.0397, -0.03030, 0.6465 0.0706, -0.04420, 0.3802 0.1037, -0.05710, 0.2159 0.1384, -0.06890, 0.1465 0.1741, -0.07950, -0.0166 0.2102, -0.08660, -0.2796 0.2472, -0.09640, -0.3614 0.2844, -0.10270, -0.5131 0.3225, -0.10690, -0.5129 0.3608, -0.10890, -0.6681 0.3991, -0.10830, -0.6572 0.4373, -0.10510, -0.6968 0.4757, -0.09890, -0.5932 0.5137, -0.09070, -0.5188 0.5694, -0.07640, -0.2821 14 Flap element taps 1.0000, 0.00130, 0.1830 0.9365, 0.01390, 0.1217 0.8333, 0.03280, 0.0237 0.7436, 0.04930, -0.0370 0.7049, 0.05670, -0.0630 0.6662, 0.06410, -0.0794 0.6522, 0.01390, -0.1834 0.5969, -0.00020, -0.1484 0.6000, -0.03020, -0.1629 0.6324, -0.04540, -0.1929 0.6667, -0.04880, -0.1760 0.7046, -0.04110, -0.0481 0.7429, -0.03210, 0.0084 0.9311, -0.00120, 0.2486 Wake drag found for this condition, Cdw=0.0133 --------- Run Conditions: vel=103.4 ft/s Re=1.006x10^6 AOA=9.01 Flap deflection=-5.00 Totals: Cl=0.5984 Cdp=0.0289 Cm(c/4)=0.0096 Cs=0.0652 Ch=-0.0442 Main component: Cl=0.5457 Cdp=0.0508 Cm=-0.0988 Flap component: Cl=0.0527 Cdp=-0.0218 Cm=-0.0405 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1475 0.6175, -0.04610, -0.1459 0.5841, -0.02440, -0.1647 0.5775, 0.01750, -0.1677 0.5777, 0.04660, -0.1690 0.6274, 0.07170, -0.1892 0.5694, 0.08320, -0.2725 0.5112, 0.09370, -0.5903 0.4731, 0.09830, -0.7495 0.4349, 0.10070, -0.8603 0.3960, 0.10120, -1.0194 0.3566, 0.10020, -0.9016 0.3172, 0.09790, -0.9318 0.2778, 0.09440, -0.9667 0.2393, 0.08960, -1.0339 0.2056, 0.08360, -1.2146 0.1633, 0.07610, -1.0908 0.1261, 0.06710, -1.2189 0.0900, 0.05640, -1.3713 0.0571, 0.04390, -1.3670 0.0283, 0.02940, -1.4858 0.0142, 0.01970, -1.5948 0.0081, 0.01410, -1.8637 0.0026, 0.00780, -1.2939 0.0000, 0.00000, -0.4952 0.0037, -0.00840, 0.7940 0.0112, -0.01420, 1.0249 0.0191, -0.01930, 1.0120 0.0397, -0.03030, 0.8818 0.0706, -0.04420, 0.6256 0.1037, -0.05710, 0.4497 0.1384, -0.06890, 0.4039 0.1741, -0.07950, 0.2273 0.2102, -0.08660, -0.0605 0.2472, -0.09640, -0.1375 0.2844, -0.10270, -0.3144 0.3225, -0.10690, -0.3139 0.3608, -0.10890, -0.4894 0.3991, -0.10830, -0.4951 0.4373, -0.10510, -0.5616 0.4757, -0.09890, -0.4866 0.5137, -0.09070, -0.4324 0.5694, -0.07640, -0.2035 14 Flap element taps 1.0000, 0.00130, 0.1356 0.9365, 0.01390, 0.0920 0.8333, 0.03280, -0.0074 0.7436, 0.04930, -0.0837 0.7049, 0.05670, -0.1276 0.6662, 0.06410, -0.1649 0.6522, 0.01390, -0.1995 0.5969, -0.00020, -0.1580 0.6000, -0.03020, -0.1668 0.6324, -0.04540, -0.2008 0.6667, -0.04880, -0.0952 0.7046, -0.04110, 0.0093 0.7429, -0.03210, 0.0654 0.9311, -0.00120, 0.2897 --------- Run Conditions: vel=103.4 ft/s Re=1.009x10^6 AOA=12.02 Flap deflection=-5.00 Totals: Cl=0.7510 Cdp=0.0642 Cm(c/4)=-0.0043 Cs=0.0936 Ch=-0.1005 Main component: Cl=0.6433 Cdp=0.0701 Cm=-0.1057 Flap component: Cl=0.1077 Cdp=-0.0059 Cm=-0.0856 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1369 0.6175, -0.04610, -0.1909 0.5841, -0.02440, -0.2123 0.5775, 0.01750, -0.2148 0.5777, 0.04660, -0.2192 0.6274, 0.07170, -0.2693 0.5694, 0.08320, -0.2257 0.5112, 0.09370, -0.3553 0.4731, 0.09830, -0.5026 0.4349, 0.10070, -0.6683 0.3960, 0.10120, -0.9135 0.3566, 0.10020, -0.8367 0.3172, 0.09790, -0.9138 0.2778, 0.09440, -0.9840 0.2393, 0.08960, -1.0922 0.2056, 0.08360, -1.3283 0.1633, 0.07610, -1.2346 0.1261, 0.06710, -1.4267 0.0900, 0.05640, -1.6279 0.0571, 0.04390, -1.7601 0.0283, 0.02940, -2.0738 0.0142, 0.01970, -2.4075 0.0081, 0.01410, -2.8534 0.0026, 0.00780, -2.3719 0.0000, 0.00000, -0.6452 0.0037, -0.00840, 0.3509 0.0112, -0.01420, 0.9346 0.0191, -0.01930, 1.0263 0.0397, -0.03030, 0.9925 0.0706, -0.04420, 0.7715 0.1037, -0.05710, 0.6001 0.1384, -0.06890, 0.5758 0.1741, -0.07950, 0.3969 0.2102, -0.08660, 0.0942 0.2472, -0.09640, 0.0220 0.2844, -0.10270, -0.1701 0.3225, -0.10690, -0.1723 0.3608, -0.10890, -0.3686 0.3991, -0.10830, -0.3793 0.4373, -0.10510, -0.4762 0.4757, -0.09890, -0.4246 0.5137, -0.09070, -0.3982 0.5694, -0.07640, -0.1862 14 Flap element taps 1.0000, 0.00130, -0.0780 0.9365, 0.01390, -0.1590 0.8333, 0.03280, -0.2189 0.7436, 0.04930, -0.2471 0.7049, 0.05670, -0.2695 0.6662, 0.06410, -0.2856 0.6522, 0.01390, -0.2520 0.5969, -0.00020, -0.2058 0.6000, -0.03020, -0.2137 0.6324, -0.04540, -0.2515 0.6667, -0.04880, 0.0030 0.7046, -0.04110, 0.0149 0.7429, -0.03210, 0.0575 0.9311, -0.00120, 0.2258 --------- Run Conditions: vel=102.8 ft/s Re=1.006x10^6 AOA=15.01 Flap deflection=-5.00 Totals: Cl=0.7656 Cdp=0.1038 Cm(c/4)=-0.0058 Cs=0.0980 Ch=-0.1246 Main component: Cl=0.6347 Cdp=0.0940 Cm=-0.0919 Flap component: Cl=0.1309 Cdp=0.0098 Cm=-0.1055 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1797 0.6175, -0.04610, -0.2854 0.5841, -0.02440, -0.2752 0.5775, 0.01750, -0.2877 0.5777, 0.04660, -0.2919 0.6274, 0.07170, -0.3368 0.5694, 0.08320, -0.3390 0.5112, 0.09370, -0.3317 0.4731, 0.09830, -0.3324 0.4349, 0.10070, -0.3729 0.3960, 0.10120, -0.4521 0.3566, 0.10020, -0.5694 0.3172, 0.09790, -0.6897 0.2778, 0.09440, -0.8312 0.2393, 0.08960, -0.9863 0.2056, 0.08360, -1.1403 0.1633, 0.07610, -1.2834 0.1261, 0.06710, -1.4361 0.0900, 0.05640, -1.7645 0.0571, 0.04390, -1.9896 0.0283, 0.02940, -2.4936 0.0142, 0.01970, -3.0170 0.0081, 0.01410, -3.4791 0.0026, 0.00780, -3.2959 0.0000, 0.00000, -0.3977 0.0037, -0.00840, -0.1479 0.0112, -0.01420, 0.7665 0.0191, -0.01930, 0.9708 0.0397, -0.03030, 1.0044 0.0706, -0.04420, 0.8744 0.1037, -0.05710, 0.7292 0.1384, -0.06890, 0.5673 0.1741, -0.07950, 0.4235 0.2102, -0.08660, 0.2595 0.2472, -0.09640, 0.1016 0.2844, -0.10270, -0.0405 0.3225, -0.10690, -0.1649 0.3608, -0.10890, -0.2969 0.3991, -0.10830, -0.3872 0.4373, -0.10510, -0.4260 0.4757, -0.09890, -0.3858 0.5137, -0.09070, -0.3497 0.5694, -0.07640, -0.2457 14 Flap element taps 1.0000, 0.00130, -0.2775 0.9365, 0.01390, -0.3568 0.8333, 0.03280, -0.3631 0.7436, 0.04930, -0.3595 0.7049, 0.05670, -0.3514 0.6662, 0.06410, -0.3519 0.6522, 0.01390, -0.2811 0.5969, -0.00020, -0.2800 0.6000, -0.03020, -0.2872 0.6324, -0.04540, -0.2835 0.6667, -0.04880, 0.0871 0.7046, -0.04110, -0.0290 0.7429, -0.03210, 0.0365 0.9311, -0.00120, 0.0934 --------- Run Conditions: vel=101.9 ft/s Re=1.001x10^6 AOA=18.02 Flap deflection=-5.00 Totals: Cl=0.5642 Cdp=0.1947 Cm(c/4)=-0.0562 Cs=-0.0106 Ch=-0.1530 Main component: Cl=0.3985 Cdp=0.1704 Cm=-0.0715 Flap component: Cl=0.1657 Cdp=0.0243 Cm=-0.1338 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2878 0.6175, -0.04610, -0.4123 0.5841, -0.02440, -0.4065 0.5775, 0.01750, -0.4196 0.5777, 0.04660, -0.4245 0.6274, 0.07170, -0.5350 0.5694, 0.08320, -0.5497 0.5112, 0.09370, -0.5547 0.4731, 0.09830, -0.5401 0.4349, 0.10070, -0.5445 0.3960, 0.10120, -0.5523 0.3566, 0.10020, -0.5451 0.3172, 0.09790, -0.5418 0.2778, 0.09440, -0.5365 0.2393, 0.08960, -0.5485 0.2056, 0.08360, -0.5783 0.1633, 0.07610, -0.5848 0.1261, 0.06710, -0.6168 0.0900, 0.05640, -0.6739 0.0571, 0.04390, -0.8806 0.0283, 0.02940, -1.3942 0.0142, 0.01970, -1.9251 0.0081, 0.01410, -2.4486 0.0026, 0.00780, -2.3321 0.0000, 0.00000, -0.4937 0.0037, -0.00840, 0.1215 0.0112, -0.01420, 0.8344 0.0191, -0.01930, 0.9894 0.0397, -0.03030, 0.9968 0.0706, -0.04420, 0.8599 0.1037, -0.05710, 0.7168 0.1384, -0.06890, 0.5664 0.1741, -0.07950, 0.4224 0.2102, -0.08660, 0.2431 0.2472, -0.09640, 0.0874 0.2844, -0.10270, -0.0657 0.3225, -0.10690, -0.1918 0.3608, -0.10890, -0.3386 0.3991, -0.10830, -0.4341 0.4373, -0.10510, -0.4892 0.4757, -0.09890, -0.4552 0.5137, -0.09070, -0.4308 0.5694, -0.07640, -0.3168 14 Flap element taps 1.0000, 0.00130, -0.4222 0.9365, 0.01390, -0.5158 0.8333, 0.03280, -0.5726 0.7436, 0.04930, -0.5652 0.7049, 0.05670, -0.5493 0.6662, 0.06410, -0.5622 0.6522, 0.01390, -0.4121 0.5969, -0.00020, -0.4109 0.6000, -0.03020, -0.4177 0.6324, -0.04540, -0.4172 0.6667, -0.04880, 0.1140 0.7046, -0.04110, -0.1046 0.7429, -0.03210, -0.0464 0.9311, -0.00120, -0.0087 --------- Run Conditions: vel=101.5 ft/s Re=0.997x10^6 AOA=19.99 Flap deflection=-5.00 Totals: Cl=0.6250 Cdp=0.2353 Cm(c/4)=-0.0641 Cs=-0.0075 Ch=-0.1652 Main component: Cl=0.4481 Cdp=0.2008 Cm=-0.0868 Flap component: Cl=0.1769 Cdp=0.0346 Cm=-0.1442 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3024 0.6175, -0.04610, -0.4347 0.5841, -0.02440, -0.4282 0.5775, 0.01750, -0.4408 0.5777, 0.04660, -0.4443 0.6274, 0.07170, -0.5825 0.5694, 0.08320, -0.5840 0.5112, 0.09370, -0.5980 0.4731, 0.09830, -0.5947 0.4349, 0.10070, -0.5966 0.3960, 0.10120, -0.6216 0.3566, 0.10020, -0.6106 0.3172, 0.09790, -0.6181 0.2778, 0.09440, -0.6283 0.2393, 0.08960, -0.6543 0.2056, 0.08360, -0.7040 0.1633, 0.07610, -0.7005 0.1261, 0.06710, -0.7605 0.0900, 0.05640, -0.7916 0.0571, 0.04390, -0.9714 0.0283, 0.02940, -1.4089 0.0142, 0.01970, -1.9488 0.0081, 0.01410, -2.4806 0.0026, 0.00780, -2.4609 0.0000, 0.00000, -0.5838 0.0037, -0.00840, -0.0077 0.0112, -0.01420, 0.7863 0.0191, -0.01930, 0.9717 0.0397, -0.03030, 1.0101 0.0706, -0.04420, 0.8879 0.1037, -0.05710, 0.7490 0.1384, -0.06890, 0.6150 0.1741, -0.07950, 0.4673 0.2102, -0.08660, 0.2770 0.2472, -0.09640, 0.1260 0.2844, -0.10270, -0.0348 0.3225, -0.10690, -0.1559 0.3608, -0.10890, -0.3142 0.3991, -0.10830, -0.4100 0.4373, -0.10510, -0.4789 0.4757, -0.09890, -0.4517 0.5137, -0.09070, -0.4377 0.5694, -0.07640, -0.3254 14 Flap element taps 1.0000, 0.00130, -0.4961 0.9365, 0.01390, -0.5835 0.8333, 0.03280, -0.6316 0.7436, 0.04930, -0.6274 0.7049, 0.05670, -0.6149 0.6662, 0.06410, -0.6317 0.6522, 0.01390, -0.4392 0.5969, -0.00020, -0.4326 0.6000, -0.03020, -0.4404 0.6324, -0.04540, -0.4434 0.6667, -0.04880, 0.1127 0.7046, -0.04110, -0.1218 0.7429, -0.03210, -0.0676 0.9311, -0.00120, -0.0372 --------- Run Conditions: vel=101.2 ft/s Re=0.995x10^6 AOA=24.00 Flap deflection=-5.00 Totals: Cl=0.8349 Cdp=0.3694 Cm(c/4)=-0.0930 Cs=0.0021 Ch=-0.1948 Main component: Cl=0.6282 Cdp=0.3065 Cm=-0.1487 Flap component: Cl=0.2067 Cdp=0.0630 Cm=-0.1726 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2724 0.6175, -0.04610, -0.4304 0.5841, -0.02440, -0.4251 0.5775, 0.01750, -0.4413 0.5777, 0.04660, -0.4434 0.6274, 0.07170, -0.7376 0.5694, 0.08320, -0.7227 0.5112, 0.09370, -0.7856 0.4731, 0.09830, -0.8017 0.4349, 0.10070, -0.8068 0.3960, 0.10120, -0.8648 0.3566, 0.10020, -0.8650 0.3172, 0.09790, -0.8850 0.2778, 0.09440, -0.9110 0.2393, 0.08960, -0.9756 0.2056, 0.08360, -1.0671 0.1633, 0.07610, -1.0981 0.1261, 0.06710, -1.1789 0.0900, 0.05640, -1.2481 0.0571, 0.04390, -1.3904 0.0283, 0.02940, -1.4892 0.0142, 0.01970, -1.7219 0.0081, 0.01410, -2.0703 0.0026, 0.00780, -2.0162 0.0000, 0.00000, -0.6751 0.0037, -0.00840, -0.2246 0.0112, -0.01420, 0.6612 0.0191, -0.01930, 0.9066 0.0397, -0.03030, 1.0225 0.0706, -0.04420, 0.9483 0.1037, -0.05710, 0.8321 0.1384, -0.06890, 0.7295 0.1741, -0.07950, 0.5953 0.2102, -0.08660, 0.4002 0.2472, -0.09640, 0.2611 0.2844, -0.10270, 0.0953 0.3225, -0.10690, -0.0189 0.3608, -0.10890, -0.1859 0.3991, -0.10830, -0.2864 0.4373, -0.10510, -0.3763 0.4757, -0.09890, -0.3655 0.5137, -0.09070, -0.3717 0.5694, -0.07640, -0.2750 14 Flap element taps 1.0000, 0.00130, -0.6429 0.9365, 0.01390, -0.6971 0.8333, 0.03280, -0.7346 0.7436, 0.04930, -0.7380 0.7049, 0.05670, -0.7377 0.6662, 0.06410, -0.7477 0.6522, 0.01390, -0.4388 0.5969, -0.00020, -0.4312 0.6000, -0.03020, -0.4388 0.6324, -0.04540, -0.4442 0.6667, -0.04880, 0.2732 0.7046, -0.04110, -0.1082 0.7429, -0.03210, -0.0619 0.9311, -0.00120, -0.0742 --------- Run Conditions: vel=101.5 ft/s Re=0.998x10^6 AOA=26.99 Flap deflection=-5.00 Totals: Cl=0.8755 Cdp=0.4467 Cm(c/4)=-0.1001 Cs=-0.0007 Ch=-0.2057 Main component: Cl=0.6655 Cdp=0.3657 Cm=-0.1655 Flap component: Cl=0.2101 Cdp=0.0810 Cm=-0.1804 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2716 0.6175, -0.04610, -0.4375 0.5841, -0.02440, -0.4356 0.5775, 0.01750, -0.4473 0.5777, 0.04660, -0.4513 0.6274, 0.07170, -0.7534 0.5694, 0.08320, -0.7597 0.5112, 0.09370, -0.8246 0.4731, 0.09830, -0.8104 0.4349, 0.10070, -0.8109 0.3960, 0.10120, -0.8841 0.3566, 0.10020, -0.8844 0.3172, 0.09790, -0.9364 0.2778, 0.09440, -0.9763 0.2393, 0.08960, -1.0578 0.2056, 0.08360, -1.1916 0.1633, 0.07610, -1.2571 0.1261, 0.06710, -1.4010 0.0900, 0.05640, -1.4293 0.0571, 0.04390, -1.4697 0.0283, 0.02940, -1.4901 0.0142, 0.01970, -1.5990 0.0081, 0.01410, -1.8177 0.0026, 0.00780, -1.6070 0.0000, 0.00000, -0.7731 0.0037, -0.00840, -0.2689 0.0112, -0.01420, 0.5976 0.0191, -0.01930, 0.8635 0.0397, -0.03030, 1.0138 0.0706, -0.04420, 0.9679 0.1037, -0.05710, 0.8674 0.1384, -0.06890, 0.7858 0.1741, -0.07950, 0.6585 0.2102, -0.08660, 0.4581 0.2472, -0.09640, 0.3278 0.2844, -0.10270, 0.1575 0.3225, -0.10690, 0.0485 0.3608, -0.10890, -0.1263 0.3991, -0.10830, -0.2280 0.4373, -0.10510, -0.3327 0.4757, -0.09890, -0.3301 0.5137, -0.09070, -0.3522 0.5694, -0.07640, -0.2647 14 Flap element taps 1.0000, 0.00130, -0.7744 0.9365, 0.01390, -0.7898 0.8333, 0.03280, -0.7922 0.7436, 0.04930, -0.7843 0.7049, 0.05670, -0.7800 0.6662, 0.06410, -0.7738 0.6522, 0.01390, -0.4510 0.5969, -0.00020, -0.4412 0.6000, -0.03020, -0.4485 0.6324, -0.04540, -0.4533 0.6667, -0.04880, 0.2785 0.7046, -0.04110, -0.1215 0.7429, -0.03210, -0.0816 0.9311, -0.00120, -0.1259