S809 VENTED AILERON MODEL, 18 IN CHORD --------- Run Conditions: vel=107.1 ft/s Re=1.011x10^6 AOA=-6.02 Flap deflection=-5.00 Totals: Cl=-0.4942 Cdp=0.0368 Cm(c/4)=0.0277 Cs=0.0152 Ch=-0.0060 Main component: Cl=-0.3962 Cdp=0.0374 Cm=0.0741 Flap component: Cl=-0.0980 Cdp=-0.0006 Cm=0.0774 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.3313 0.5871, 0.07930, -0.2412 0.5501, 0.08690, -0.2661 0.5112, 0.09370, -0.4027 0.4731, 0.09830, -0.4554 0.4349, 0.10070, -0.4365 0.3960, 0.10120, -0.3805 0.3566, 0.10020, -0.3207 0.3172, 0.09790, -0.2507 0.2778, 0.09440, -0.1994 0.2393, 0.08960, -0.1426 0.2056, 0.08360, -0.0704 0.1633, 0.07610, 0.0281 0.1261, 0.06710, 0.1541 0.0900, 0.05640, 0.2805 0.0571, 0.04390, 0.4992 0.0283, 0.02940, 0.7840 0.0142, 0.01970, 0.9626 0.0081, 0.01410, 0.9989 0.0026, 0.00780, 0.7542 0.0000, 0.00000, -0.3342 0.0037, -0.00840, -1.1999 0.0112, -0.01420, -1.3949 0.0191, -0.01930, -0.8766 0.0397, -0.03030, -0.7847 0.0706, -0.04420, -0.7585 0.1037, -0.05710, -0.7636 0.1384, -0.06890, -0.8298 0.1741, -0.07950, -0.8701 0.2102, -0.08660, -0.9380 0.2472, -0.09640, -1.0168 0.2844, -0.10270, -1.0301 0.3225, -0.10690, -1.0207 0.3608, -0.10890, -0.9962 0.3991, -0.10830, -0.8906 0.4373, -0.10510, -0.7083 0.4757, -0.09890, -0.4644 0.5137, -0.09070, -0.2713 0.5514, -0.08120, -0.2134 0.5917, -0.06870, -0.1938 0.5917, -0.02380, -0.2608 0.5917, 0.02120, -0.1756 16 Flap element taps 1.0000, 0.00130, -0.1836 0.9365, 0.01390, -0.0429 0.8333, 0.03280, 0.0641 0.7436, 0.04930, 0.2199 0.7049, 0.05670, 0.5220 0.6667, 0.05450, -0.2537 0.6302, 0.03770, -0.3390 0.6083, 0.01980, -0.2129 0.6000, 0.00000, -0.2823 0.6076, -0.01900, -0.2512 0.6285, -0.03060, -0.2304 0.6667, -0.04090, -0.2231 0.7046, -0.04120, -0.2162 0.7429, -0.03210, -0.2169 0.8333, -0.01400, -0.2158 0.9311, -0.00120, -0.2407 --------- Run Conditions: vel=106.6 ft/s Re=1.006x10^6 AOA=0.00 Flap deflection=-5.00 Totals: Cl=-0.1578 Cdp=0.0126 Cm(c/4)=0.0326 Cs=-0.0126 Ch=-0.0093 Main component: Cl=-0.1056 Cdp=0.0297 Cm=0.0316 Flap component: Cl=-0.0522 Cdp=-0.0171 Cm=0.0404 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1836 0.5871, 0.07930, -0.2298 0.5501, 0.08690, -0.3057 0.5112, 0.09370, -0.4749 0.4731, 0.09830, -0.5730 0.4349, 0.10070, -0.5890 0.3960, 0.10120, -0.5721 0.3566, 0.10020, -0.5384 0.3172, 0.09790, -0.4934 0.2778, 0.09440, -0.4752 0.2393, 0.08960, -0.4518 0.2056, 0.08360, -0.4258 0.1633, 0.07610, -0.3583 0.1261, 0.06710, -0.2788 0.0900, 0.05640, -0.2187 0.0571, 0.04390, -0.0613 0.0283, 0.02940, 0.1980 0.0142, 0.01970, 0.4255 0.0081, 0.01410, 0.5901 0.0026, 0.00780, 0.7860 0.0000, 0.00000, 0.9924 0.0037, -0.00840, 0.4884 0.0112, -0.01420, 0.0776 0.0191, -0.01930, 0.1590 0.0397, -0.03030, -0.0030 0.0706, -0.04420, -0.1521 0.1037, -0.05710, -0.2579 0.1384, -0.06890, -0.3933 0.1741, -0.07950, -0.4963 0.2102, -0.08660, -0.6233 0.2472, -0.09640, -0.7534 0.2844, -0.10270, -0.8290 0.3225, -0.10690, -0.8815 0.3608, -0.10890, -0.9367 0.3991, -0.10830, -0.9149 0.4373, -0.10510, -0.8424 0.4757, -0.09890, -0.6878 0.5137, -0.09070, -0.5154 0.5514, -0.08120, -0.3159 0.5917, -0.06870, -0.1550 0.5917, -0.02380, -0.1819 0.5917, 0.02120, -0.1534 16 Flap element taps 1.0000, 0.00130, 0.1060 0.9365, 0.01390, 0.1031 0.8333, 0.03280, 0.1278 0.7436, 0.04930, 0.1911 0.7049, 0.05670, 0.0694 0.6667, 0.05450, -0.2007 0.6302, 0.03770, -0.1696 0.6083, 0.01980, -0.1508 0.6000, 0.00000, -0.1790 0.6076, -0.01900, -0.1843 0.6285, -0.03060, -0.1655 0.6667, -0.04090, -0.2011 0.7046, -0.04120, -0.2986 0.7429, -0.03210, -0.1069 0.8333, -0.01400, -0.0028 0.9311, -0.00120, 0.0477 Wake drag found for this condition, Cdw=0.0190 --------- Run Conditions: vel=106.6 ft/s Re=1.006x10^6 AOA=3.04 Flap deflection=-5.00 Totals: Cl=0.0968 Cdp=0.0087 Cm(c/4)=0.0286 Cs=-0.0036 Ch=-0.0129 Main component: Cl=0.1210 Cdp=0.0274 Cm=-0.0138 Flap component: Cl=-0.0242 Cdp=-0.0187 Cm=0.0180 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1478 0.5871, 0.07930, -0.2350 0.5501, 0.08690, -0.3387 0.5112, 0.09370, -0.5272 0.4731, 0.09830, -0.6502 0.4349, 0.10070, -0.6884 0.3960, 0.10120, -0.6958 0.3566, 0.10020, -0.6773 0.3172, 0.09790, -0.6508 0.2778, 0.09440, -0.6518 0.2393, 0.08960, -0.6547 0.2056, 0.08360, -0.6598 0.1633, 0.07610, -0.6161 0.1261, 0.06710, -0.5748 0.0900, 0.05640, -0.5690 0.0571, 0.04390, -0.4863 0.0283, 0.02940, -0.3107 0.0142, 0.01970, -0.1535 0.0081, 0.01410, -0.0699 0.0026, 0.00780, 0.2557 0.0000, 0.00000, 0.8498 0.0037, -0.00840, 0.9317 0.0112, -0.01420, 0.6427 0.0191, -0.01930, 0.5908 0.0397, -0.03030, 0.3727 0.0706, -0.04420, 0.1636 0.1037, -0.05710, 0.0263 0.1384, -0.06890, -0.1252 0.1741, -0.07950, -0.2506 0.2102, -0.08660, -0.3995 0.2472, -0.09640, -0.5398 0.2844, -0.10270, -0.6362 0.3225, -0.10690, -0.7075 0.3608, -0.10890, -0.7875 0.3991, -0.10830, -0.7902 0.4373, -0.10510, -0.7501 0.4757, -0.09890, -0.6240 0.5137, -0.09070, -0.4829 0.5514, -0.08120, -0.3004 0.5917, -0.06870, -0.1437 0.5917, -0.02380, -0.1598 0.5917, 0.02120, -0.1544 16 Flap element taps 1.0000, 0.00130, 0.1810 0.9365, 0.01390, 0.1401 0.8333, 0.03280, 0.1196 0.7436, 0.04930, 0.0306 0.7049, 0.05670, -0.0966 0.6667, 0.05450, -0.1595 0.6302, 0.03770, -0.1511 0.6083, 0.01980, -0.1357 0.6000, 0.00000, -0.1516 0.6076, -0.01900, -0.1618 0.6285, -0.03060, -0.1499 0.6667, -0.04090, -0.1652 0.7046, -0.04120, -0.4421 0.7429, -0.03210, -0.1161 0.8333, -0.01400, 0.0856 0.9311, -0.00120, 0.1706 Wake drag found for this condition, Cdw=0.0156 --------- Run Conditions: vel=106.8 ft/s Re=1.007x10^6 AOA=6.03 Flap deflection=-5.00 Totals: Cl=0.3576 Cdp=0.0125 Cm(c/4)=0.0200 Cs=0.0251 Ch=-0.0175 Main component: Cl=0.3469 Cdp=0.0244 Cm=-0.0587 Flap component: Cl=0.0107 Cdp=-0.0119 Cm=-0.0105 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1261 0.5871, 0.07930, -0.2121 0.5501, 0.08690, -0.3333 0.5112, 0.09370, -0.5328 0.4731, 0.09830, -0.6892 0.4349, 0.10070, -0.7580 0.3960, 0.10120, -0.7954 0.3566, 0.10020, -0.7990 0.3172, 0.09790, -0.7963 0.2778, 0.09440, -0.8202 0.2393, 0.08960, -0.8522 0.2056, 0.08360, -0.8907 0.1633, 0.07610, -0.8805 0.1261, 0.06710, -0.8876 0.0900, 0.05640, -0.9504 0.0571, 0.04390, -0.9663 0.0283, 0.02940, -0.9263 0.0142, 0.01970, -0.9252 0.0081, 0.01410, -0.9700 0.0026, 0.00780, -0.5220 0.0000, 0.00000, -0.0618 0.0037, -0.00840, 0.9910 0.0112, -0.01420, 0.9514 0.0191, -0.01930, 0.8741 0.0397, -0.03030, 0.6656 0.0706, -0.04420, 0.4408 0.1037, -0.05710, 0.2822 0.1384, -0.06890, 0.1241 0.1741, -0.07950, -0.0180 0.2102, -0.08660, -0.1813 0.2472, -0.09640, -0.3267 0.2844, -0.10270, -0.4358 0.3225, -0.10690, -0.5215 0.3608, -0.10890, -0.6148 0.3991, -0.10830, -0.6390 0.4373, -0.10510, -0.6239 0.4757, -0.09890, -0.5243 0.5137, -0.09070, -0.4135 0.5514, -0.08120, -0.2470 0.5917, -0.06870, -0.1118 0.5917, -0.02380, -0.1353 0.5917, 0.02120, -0.1320 16 Flap element taps 1.0000, 0.00130, 0.1336 0.9365, 0.01390, 0.0771 0.8333, 0.03280, -0.0060 0.7436, 0.04930, -0.1059 0.7049, 0.05670, -0.1236 0.6667, 0.05450, -0.1234 0.6302, 0.03770, -0.1277 0.6083, 0.01980, -0.1124 0.6000, 0.00000, -0.1254 0.6076, -0.01900, -0.1454 0.6285, -0.03060, -0.0997 0.6667, -0.04090, -0.0806 0.7046, -0.04120, -0.5205 0.7429, -0.03210, -0.0951 0.8333, -0.01400, 0.1230 0.9311, -0.00120, 0.2012 Wake drag found for this condition, Cdw=0.0180 --------- Run Conditions: vel=106.9 ft/s Re=1.007x10^6 AOA=9.04 Flap deflection=-5.00 Totals: Cl=0.4986 Cdp=0.0228 Cm(c/4)=0.0238 Cs=0.0558 Ch=-0.0260 Main component: Cl=0.4684 Cdp=0.0245 Cm=-0.0721 Flap component: Cl=0.0303 Cdp=-0.0017 Cm=-0.0281 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1322 0.5871, 0.07930, -0.1597 0.5501, 0.08690, -0.2161 0.5112, 0.09370, -0.3706 0.4731, 0.09830, -0.5625 0.4349, 0.10070, -0.6861 0.3960, 0.10120, -0.7703 0.3566, 0.10020, -0.8112 0.3172, 0.09790, -0.8409 0.2778, 0.09440, -0.8939 0.2393, 0.08960, -0.9579 0.2056, 0.08360, -1.0291 0.1633, 0.07610, -1.0579 0.1261, 0.06710, -1.1107 0.0900, 0.05640, -1.2410 0.0571, 0.04390, -1.3543 0.0283, 0.02940, -1.4660 0.0142, 0.01970, -1.6501 0.0081, 0.01410, -1.7430 0.0026, 0.00780, -1.4179 0.0000, 0.00000, -1.3380 0.0037, -0.00840, 0.7750 0.0112, -0.01420, 1.0095 0.0191, -0.01930, 0.9876 0.0397, -0.03030, 0.8361 0.0706, -0.04420, 0.6224 0.1037, -0.05710, 0.4578 0.1384, -0.06890, 0.2977 0.1741, -0.07950, 0.1499 0.2102, -0.08660, -0.0202 0.2472, -0.09640, -0.1747 0.2844, -0.10270, -0.3015 0.3225, -0.10690, -0.4034 0.3608, -0.10890, -0.5117 0.3991, -0.10830, -0.5613 0.4373, -0.10510, -0.5661 0.4757, -0.09890, -0.4815 0.5137, -0.09070, -0.3872 0.5514, -0.08120, -0.2286 0.5917, -0.06870, -0.1333 0.5917, -0.02380, -0.1361 0.5917, 0.02120, -0.1309 16 Flap element taps 1.0000, 0.00130, -0.0471 0.9365, 0.01390, -0.1083 0.8333, 0.03280, -0.1202 0.7436, 0.04930, -0.1358 0.7049, 0.05670, -0.1263 0.6667, 0.05450, -0.1241 0.6302, 0.03770, -0.1288 0.6083, 0.01980, -0.1161 0.6000, 0.00000, -0.1328 0.6076, -0.01900, -0.2119 0.6285, -0.03060, 0.0358 0.6667, -0.04090, -0.0865 0.7046, -0.04120, -0.6250 0.7429, -0.03210, -0.1096 0.8333, -0.01400, 0.1024 0.9311, -0.00120, 0.1476 Wake drag found for this condition, Cdw=0.0242 --------- Run Conditions: vel=106.8 ft/s Re=1.005x10^6 AOA=12.04 Flap deflection=-5.00 Totals: Cl=0.6811 Cdp=0.0376 Cm(c/4)=0.0263 Cs=0.1052 Ch=0.0160 Main component: Cl=0.6043 Cdp=0.0812 Cm=-0.0910 Flap component: Cl=0.0768 Cdp=-0.0436 Cm=-0.0512 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.2555 0.5871, 0.07930, -0.2727 0.5501, 0.08690, -0.3006 0.5112, 0.09370, -0.3915 0.4731, 0.09830, -0.5599 0.4349, 0.10070, -0.6975 0.3960, 0.10120, -0.8021 0.3566, 0.10020, -0.8780 0.3172, 0.09790, -0.9340 0.2778, 0.09440, -1.0116 0.2393, 0.08960, -1.1031 0.2056, 0.08360, -1.2053 0.1633, 0.07610, -1.2822 0.1261, 0.06710, -1.3830 0.0900, 0.05640, -1.5921 0.0571, 0.04390, -1.8277 0.0283, 0.02940, -2.1356 0.0142, 0.01970, -2.5710 0.0081, 0.01410, -2.8681 0.0026, 0.00780, -2.6653 0.0000, 0.00000, -3.3184 0.0037, -0.00840, 0.2315 0.0112, -0.01420, 0.8996 0.0191, -0.01930, 0.9998 0.0397, -0.03030, 0.9550 0.0706, -0.04420, 0.7825 0.1037, -0.05710, 0.6264 0.1384, -0.06890, 0.4674 0.1741, -0.07950, 0.3194 0.2102, -0.08660, 0.1509 0.2472, -0.09640, -0.0102 0.2844, -0.10270, -0.1460 0.3225, -0.10690, -0.2670 0.3608, -0.10890, -0.3920 0.3991, -0.10830, -0.4647 0.4373, -0.10510, -0.4988 0.4757, -0.09890, -0.4653 0.5137, -0.09070, -0.4261 0.5514, -0.08120, -0.3705 0.5917, -0.06870, -1.1664 0.5917, -0.02380, -0.6026 0.5917, 0.02120, -0.1537 16 Flap element taps 1.0000, 0.00130, -0.0198 0.9365, 0.01390, -0.0341 0.8333, 0.03280, -0.0532 0.7436, 0.04930, -0.1051 0.7049, 0.05670, -0.1521 0.6667, 0.05450, -0.1580 0.6302, 0.03770, -0.4015 0.6083, 0.01980, -0.4656 0.6000, 0.00000, -1.7075 0.6076, -0.01900, -0.8885 0.6285, -0.03060, 0.9163 0.6667, -0.04090, -0.0380 0.7046, -0.04120, -0.4806 0.7429, -0.03210, 0.0079 0.8333, -0.01400, 0.1547 0.9311, -0.00120, 0.1846 --------- Run Conditions: vel=106.0 ft/s Re=0.999x10^6 AOA=15.04 Flap deflection=-5.00 Totals: Cl=0.8377 Cdp=0.0690 Cm(c/4)=0.0147 Cs=0.1508 Ch=0.0304 Main component: Cl=0.7188 Cdp=0.1042 Cm=-0.1111 Flap component: Cl=0.1189 Cdp=-0.0352 Cm=-0.0809 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.3875 0.5871, 0.07930, -0.4059 0.5501, 0.08690, -0.4046 0.5112, 0.09370, -0.4215 0.4731, 0.09830, -0.4780 0.4349, 0.10070, -0.5747 0.3960, 0.10120, -0.6863 0.3566, 0.10020, -0.8209 0.3172, 0.09790, -0.9150 0.2778, 0.09440, -1.0287 0.2393, 0.08960, -1.1503 0.2056, 0.08360, -1.2771 0.1633, 0.07610, -1.4219 0.1261, 0.06710, -1.5722 0.0900, 0.05640, -1.8583 0.0571, 0.04390, -2.2117 0.0283, 0.02940, -2.7230 0.0142, 0.01970, -3.3999 0.0081, 0.01410, -3.9340 0.0026, 0.00780, -3.8752 0.0000, 0.00000, -5.4371 0.0037, -0.00840, -0.4668 0.0112, -0.01420, 0.6706 0.0191, -0.01930, 0.9292 0.0397, -0.03030, 1.0012 0.0706, -0.04420, 0.8906 0.1037, -0.05710, 0.7562 0.1384, -0.06890, 0.5908 0.1741, -0.07950, 0.4532 0.2102, -0.08660, 0.3009 0.2472, -0.09640, 0.1321 0.2844, -0.10270, -0.0022 0.3225, -0.10690, -0.1433 0.3608, -0.10890, -0.2680 0.3991, -0.10830, -0.3605 0.4373, -0.10510, -0.4034 0.4757, -0.09890, -0.3883 0.5137, -0.09070, -0.3636 0.5514, -0.08120, -0.3178 0.5917, -0.06870, -1.1856 0.5917, -0.02380, -0.6643 0.5917, 0.02120, -0.3406 16 Flap element taps 1.0000, 0.00130, -0.1205 0.9365, 0.01390, -0.1382 0.8333, 0.03280, -0.1503 0.7436, 0.04930, -0.2090 0.7049, 0.05670, -0.2903 0.6667, 0.05450, -0.2740 0.6302, 0.03770, -0.6048 0.6083, 0.01980, -0.6623 0.6000, 0.00000, -1.7755 0.6076, -0.01900, -0.8593 0.6285, -0.03060, 0.9235 0.6667, -0.04090, -0.0151 0.7046, -0.04120, -0.4666 0.7429, -0.03210, 0.0085 0.8333, -0.01400, 0.1366 0.9311, -0.00120, 0.1450 --------- Run Conditions: vel=106.3 ft/s Re=1.001x10^6 AOA=18.00 Flap deflection=-5.00 Totals: Cl=0.6932 Cdp=0.1523 Cm(c/4)=-0.0240 Cs=0.0694 Ch=0.0403 Main component: Cl=0.5207 Cdp=0.1696 Cm=-0.0785 Flap component: Cl=0.1725 Cdp=-0.0174 Cm=-0.1221 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.5778 0.5871, 0.07930, -0.5693 0.5501, 0.08690, -0.5747 0.5112, 0.09370, -0.5792 0.4731, 0.09830, -0.5810 0.4349, 0.10070, -0.5808 0.3960, 0.10120, -0.5614 0.3566, 0.10020, -0.6025 0.3172, 0.09790, -0.6061 0.2778, 0.09440, -0.6224 0.2393, 0.08960, -0.6603 0.2056, 0.08360, -0.7212 0.1633, 0.07610, -0.8698 0.1261, 0.06710, -1.0367 0.0900, 0.05640, -1.3239 0.0571, 0.04390, -1.7154 0.0283, 0.02940, -2.2636 0.0142, 0.01970, -2.9296 0.0081, 0.01410, -3.4491 0.0026, 0.00780, -3.4789 0.0000, 0.00000, -4.9620 0.0037, -0.00840, -0.3866 0.0112, -0.01420, 0.6828 0.0191, -0.01930, 0.9275 0.0397, -0.03030, 0.9986 0.0706, -0.04420, 0.8940 0.1037, -0.05710, 0.7653 0.1384, -0.06890, 0.5861 0.1741, -0.07950, 0.4480 0.2102, -0.08660, 0.3065 0.2472, -0.09640, 0.1244 0.2844, -0.10270, -0.0112 0.3225, -0.10690, -0.1742 0.3608, -0.10890, -0.3025 0.3991, -0.10830, -0.4116 0.4373, -0.10510, -0.4601 0.4757, -0.09890, -0.4531 0.5137, -0.09070, -0.4385 0.5514, -0.08120, -0.3971 0.5917, -0.06870, -1.3894 0.5917, -0.02380, -0.8397 0.5917, 0.02120, -0.5461 16 Flap element taps 1.0000, 0.00130, -0.3723 0.9365, 0.01390, -0.3977 0.8333, 0.03280, -0.4066 0.7436, 0.04930, -0.4648 0.7049, 0.05670, -0.5918 0.6667, 0.05450, -0.4490 0.6302, 0.03770, -0.8627 0.6083, 0.01980, -0.9407 0.6000, 0.00000, -2.0510 0.6076, -0.01900, -1.0016 0.6285, -0.03060, 0.9167 0.6667, -0.04090, -0.0948 0.7046, -0.04120, -0.6036 0.7429, -0.03210, -0.0953 0.8333, -0.01400, 0.0274 0.9311, -0.00120, 0.0079 --------- Run Conditions: vel=106.5 ft/s Re=1.002x10^6 AOA=20.00 Flap deflection=-5.00 Totals: Cl=0.6572 Cdp=0.2268 Cm(c/4)=-0.0501 Cs=0.0117 Ch=0.0445 Main component: Cl=0.4684 Cdp=0.2353 Cm=-0.0897 Flap component: Cl=0.1888 Cdp=-0.0085 Cm=-0.1341 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.6987 0.5871, 0.07930, -0.6561 0.5501, 0.08690, -0.6595 0.5112, 0.09370, -0.6728 0.4731, 0.09830, -0.7073 0.4349, 0.10070, -0.7080 0.3960, 0.10120, -0.6769 0.3566, 0.10020, -0.7349 0.3172, 0.09790, -0.7375 0.2778, 0.09440, -0.7514 0.2393, 0.08960, -0.7692 0.2056, 0.08360, -0.7587 0.1633, 0.07610, -0.8271 0.1261, 0.06710, -0.8318 0.0900, 0.05640, -0.8904 0.0571, 0.04390, -1.0406 0.0283, 0.02940, -1.5106 0.0142, 0.01970, -2.1648 0.0081, 0.01410, -2.6810 0.0026, 0.00780, -2.8649 0.0000, 0.00000, -4.2565 0.0037, -0.00840, -0.2644 0.0112, -0.01420, 0.7075 0.0191, -0.01930, 0.9330 0.0397, -0.03030, 0.9996 0.0706, -0.04420, 0.9067 0.1037, -0.05710, 0.7829 0.1384, -0.06890, 0.5959 0.1741, -0.07950, 0.4637 0.2102, -0.08660, 0.3326 0.2472, -0.09640, 0.1443 0.2844, -0.10270, 0.0124 0.3225, -0.10690, -0.1621 0.3608, -0.10890, -0.2883 0.3991, -0.10830, -0.4098 0.4373, -0.10510, -0.4579 0.4757, -0.09890, -0.4536 0.5137, -0.09070, -0.4479 0.5514, -0.08120, -0.4109 0.5917, -0.06870, -1.4349 0.5917, -0.02380, -0.8761 0.5917, 0.02120, -0.6518 16 Flap element taps 1.0000, 0.00130, -0.4433 0.9365, 0.01390, -0.4857 0.8333, 0.03280, -0.4728 0.7436, 0.04930, -0.5252 0.7049, 0.05670, -0.6470 0.6667, 0.05450, -0.5317 0.6302, 0.03770, -0.9655 0.6083, 0.01980, -1.0539 0.6000, 0.00000, -2.1227 0.6076, -0.01900, -1.0355 0.6285, -0.03060, 0.9159 0.6667, -0.04090, -0.1134 0.7046, -0.04120, -0.6400 0.7429, -0.03210, -0.1232 0.8333, -0.01400, -0.0078 0.9311, -0.00120, -0.0361 --------- Run Conditions: vel=106.5 ft/s Re=1.001x10^6 AOA=24.00 Flap deflection=-5.00 Totals: Cl=0.6117 Cdp=0.3436 Cm(c/4)=-0.0743 Cs=-0.0651 Ch=0.0504 Main component: Cl=0.4068 Cdp=0.3377 Cm=-0.1035 Flap component: Cl=0.2050 Cdp=0.0059 Cm=-0.1455 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.9477 0.5871, 0.07930, -0.8828 0.5501, 0.08690, -0.8336 0.5112, 0.09370, -0.7794 0.4731, 0.09830, -0.7580 0.4349, 0.10070, -0.7371 0.3960, 0.10120, -0.6982 0.3566, 0.10020, -0.7553 0.3172, 0.09790, -0.7344 0.2778, 0.09440, -0.7328 0.2393, 0.08960, -0.7196 0.2056, 0.08360, -0.6944 0.1633, 0.07610, -0.7597 0.1261, 0.06710, -0.7505 0.0900, 0.05640, -0.7662 0.0571, 0.04390, -0.7835 0.0283, 0.02940, -0.9046 0.0142, 0.01970, -1.0587 0.0081, 0.01410, -1.2114 0.0026, 0.00780, -1.3949 0.0000, 0.00000, -2.6821 0.0037, -0.00840, -0.0248 0.0112, -0.01420, 0.7411 0.0191, -0.01930, 0.9336 0.0397, -0.03030, 0.9988 0.0706, -0.04420, 0.9281 0.1037, -0.05710, 0.8220 0.1384, -0.06890, 0.6420 0.1741, -0.07950, 0.5198 0.2102, -0.08660, 0.4041 0.2472, -0.09640, 0.2175 0.2844, -0.10270, 0.0884 0.3225, -0.10690, -0.0924 0.3608, -0.10890, -0.2189 0.3991, -0.10830, -0.3515 0.4373, -0.10510, -0.4066 0.4757, -0.09890, -0.4143 0.5137, -0.09070, -0.4209 0.5514, -0.08120, -0.3927 0.5917, -0.06870, -1.4721 0.5917, -0.02380, -0.9399 0.5917, 0.02120, -0.8189 16 Flap element taps 1.0000, 0.00130, -0.5027 0.9365, 0.01390, -0.5589 0.8333, 0.03280, -0.5530 0.7436, 0.04930, -0.5431 0.7049, 0.05670, -0.6028 0.6667, 0.05450, -0.6415 0.6302, 0.03770, -1.1100 0.6083, 0.01980, -1.2295 0.6000, 0.00000, -2.1998 0.6076, -0.01900, -1.0371 0.6285, -0.03060, 0.9163 0.6667, -0.04090, -0.1150 0.7046, -0.04120, -0.6586 0.7429, -0.03210, -0.1451 0.8333, -0.01400, -0.0393 0.9311, -0.00120, -0.0764 --------- Run Conditions: vel=106.5 ft/s Re=1.001x10^6 AOA=26.96 Flap deflection=-5.00 Totals: Cl=0.6282 Cdp=0.4052 Cm(c/4)=-0.0843 Cs=-0.0764 Ch=0.0567 Main component: Cl=0.4078 Cdp=0.3780 Cm=-0.1103 Flap component: Cl=0.2204 Cdp=0.0273 Cm=-0.1599 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.8886 0.5871, 0.07930, -0.8183 0.5501, 0.08690, -0.8003 0.5112, 0.09370, -0.7672 0.4731, 0.09830, -0.7547 0.4349, 0.10070, -0.7451 0.3960, 0.10120, -0.6858 0.3566, 0.10020, -0.7519 0.3172, 0.09790, -0.7388 0.2778, 0.09440, -0.7580 0.2393, 0.08960, -0.7589 0.2056, 0.08360, -0.7363 0.1633, 0.07610, -0.8031 0.1261, 0.06710, -0.7951 0.0900, 0.05640, -0.8340 0.0571, 0.04390, -0.8314 0.0283, 0.02940, -0.8944 0.0142, 0.01970, -0.9406 0.0081, 0.01410, -0.9445 0.0026, 0.00780, -0.9225 0.0000, 0.00000, -1.9457 0.0037, -0.00840, -0.0156 0.0112, -0.01420, 0.7034 0.0191, -0.01930, 0.9058 0.0397, -0.03030, 0.9979 0.0706, -0.04420, 0.9495 0.1037, -0.05710, 0.8612 0.1384, -0.06890, 0.6877 0.1741, -0.07950, 0.5710 0.2102, -0.08660, 0.4667 0.2472, -0.09640, 0.2789 0.2844, -0.10270, 0.1535 0.3225, -0.10690, -0.0314 0.3608, -0.10890, -0.1600 0.3991, -0.10830, -0.2990 0.4373, -0.10510, -0.3583 0.4757, -0.09890, -0.3748 0.5137, -0.09070, -0.3903 0.5514, -0.08120, -0.3695 0.5917, -0.06870, -1.4556 0.5917, -0.02380, -0.9334 0.5917, 0.02120, -0.8521 16 Flap element taps 1.0000, 0.00130, -0.5836 0.9365, 0.01390, -0.6099 0.8333, 0.03280, -0.5932 0.7436, 0.04930, -0.6521 0.7049, 0.05670, -0.7838 0.6667, 0.05450, -0.6504 0.6302, 0.03770, -1.1385 0.6083, 0.01980, -1.2572 0.6000, 0.00000, -2.1801 0.6076, -0.01900, -1.0210 0.6285, -0.03060, 0.9117 0.6667, -0.04090, -0.1114 0.7046, -0.04120, -0.6625 0.7429, -0.03210, -0.1524 0.8333, -0.01400, -0.0578 0.9311, -0.00120, -0.1055