S809 VENTED AILERON MODEL, 18 IN CHORD --------- Run Conditions: vel=108.8 ft/s Re=1.002x10^6 AOA=-5.99 Flap deflection=-20.00 Totals: Cl=-0.8120 Cdp=0.0948 Cm(c/4)=0.1382 Cs=-0.0096 Ch=-0.0314 Main component: Cl=-0.5094 Cdp=0.0865 Cm=0.1048 Flap component: Cl=-0.3026 Cdp=0.0083 Cm=0.2378 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.8142 0.5871, 0.07930, -0.1841 0.5501, 0.08690, -0.2861 0.5112, 0.09370, -0.3205 0.4731, 0.09830, -0.3454 0.4349, 0.10070, -0.3226 0.3960, 0.10120, -0.2681 0.3566, 0.10020, -0.2041 0.3172, 0.09790, -0.1394 0.2778, 0.09440, -0.0977 0.2393, 0.08960, -0.0384 0.2056, 0.08360, 0.0433 0.1633, 0.07610, 0.1375 0.1261, 0.06710, 0.2635 0.0900, 0.05640, 0.4137 0.0571, 0.04390, 0.6147 0.0283, 0.02940, 0.8696 0.0142, 0.01970, 1.0017 0.0081, 0.01410, 0.9929 0.0026, 0.00780, 0.6427 0.0000, 0.00000, -0.8805 0.0037, -0.00840, -1.8363 0.0112, -0.01420, -1.4925 0.0191, -0.01930, -1.2760 0.0397, -0.03030, -1.0031 0.0706, -0.04420, -0.8986 0.1037, -0.05710, -0.9263 0.1384, -0.06890, -0.9646 0.1741, -0.07950, -0.9978 0.2102, -0.08660, -1.0528 0.2472, -0.09640, -1.1222 0.2844, -0.10270, -1.1290 0.3225, -0.10690, -1.1064 0.3608, -0.10890, -1.0628 0.3991, -0.10830, -0.9379 0.4373, -0.10510, -0.7163 0.4757, -0.09890, -0.4257 0.5137, -0.09070, -0.2405 0.5514, -0.08120, -0.1997 0.5917, -0.06870, -0.2109 0.5917, -0.02380, -0.5331 0.5917, 0.02120, -0.8257 16 Flap element taps 1.0000, 0.00130, -0.3417 0.9365, 0.01390, 0.1087 0.8333, 0.03280, 0.4415 0.7436, 0.04930, 0.8437 0.7049, 0.05670, 0.9524 0.6667, 0.05450, -0.8055 0.6302, 0.03770, -1.1465 0.6083, 0.01980, -1.0596 0.6000, 0.00000, -1.4291 0.6076, -0.01900, -1.8596 0.6285, -0.03060, -1.2754 0.6667, -0.04090, -0.8957 0.7046, -0.04120, -0.5184 0.7429, -0.03210, -0.4168 0.8333, -0.01400, -0.3837 0.9311, -0.00120, -0.3767 --------- Run Conditions: vel=109.9 ft/s Re=1.011x10^6 AOA=0.04 Flap deflection=-20.00 Totals: Cl=-0.6755 Cdp=0.0389 Cm(c/4)=0.1465 Cs=-0.0394 Ch=-0.0990 Main component: Cl=-0.3932 Cdp=-0.0457 Cm=0.1031 Flap component: Cl=-0.2822 Cdp=0.0846 Cm=0.2123 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.2280 0.5871, 0.07930, 0.1708 0.5501, 0.08690, -0.2198 0.5112, 0.09370, -0.2155 0.4731, 0.09830, -0.2580 0.4349, 0.10070, -0.2996 0.3960, 0.10120, -0.2956 0.3566, 0.10020, -0.2723 0.3172, 0.09790, -0.2432 0.2778, 0.09440, -0.2352 0.2393, 0.08960, -0.2084 0.2056, 0.08360, -0.1623 0.1633, 0.07610, -0.1015 0.1261, 0.06710, -0.0122 0.0900, 0.05640, 0.1037 0.0571, 0.04390, 0.2700 0.0283, 0.02940, 0.5357 0.0142, 0.01970, 0.7762 0.0081, 0.01410, 0.9101 0.0026, 0.00780, 0.9868 0.0000, 0.00000, 0.6263 0.0037, -0.00840, -0.2187 0.0112, -0.01420, -0.3342 0.0191, -0.01930, -0.3325 0.0397, -0.03030, -0.3617 0.0706, -0.04420, -0.4665 0.1037, -0.05710, -0.5826 0.1384, -0.06890, -0.6909 0.1741, -0.07950, -0.7946 0.2102, -0.08660, -0.9051 0.2472, -0.09640, -1.0302 0.2844, -0.10270, -1.1007 0.3225, -0.10690, -1.1547 0.3608, -0.10890, -1.1816 0.3991, -0.10830, -1.1350 0.4373, -0.10510, -1.0441 0.4757, -0.09890, -1.0218 0.5137, -0.09070, -0.4121 0.5514, -0.08120, -0.1420 0.5917, -0.06870, 0.2039 0.5917, -0.02380, 0.2152 0.5917, 0.02120, 0.2150 16 Flap element taps 1.0000, 0.00130, -0.2003 0.9365, 0.01390, 0.1500 0.8333, 0.03280, 0.3953 0.7436, 0.04930, 0.2185 0.7049, 0.05670, 0.2157 0.6667, 0.05450, 0.2178 0.6302, 0.03770, 0.2130 0.6083, 0.01980, 0.1998 0.6000, 0.00000, 0.4307 0.6076, -0.01900, -1.1086 0.6285, -0.03060, -1.3825 0.6667, -0.04090, -1.1960 0.7046, -0.04120, -0.5467 0.7429, -0.03210, -0.3393 0.8333, -0.01400, -0.3427 0.9311, -0.00120, -0.3128 --------- Run Conditions: vel=110.3 ft/s Re=1.011x10^6 AOA=3.03 Flap deflection=-20.00 Totals: Cl=-0.5095 Cdp=0.0325 Cm(c/4)=0.1612 Cs=-0.0594 Ch=-0.1140 Main component: Cl=-0.2109 Cdp=-0.0419 Cm=0.0683 Flap component: Cl=-0.2986 Cdp=0.0744 Cm=0.2197 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.2384 0.5871, 0.07930, 0.1559 0.5501, 0.08690, -0.2842 0.5112, 0.09370, -0.2756 0.4731, 0.09830, -0.3066 0.4349, 0.10070, -0.3548 0.3960, 0.10120, -0.3529 0.3566, 0.10020, -0.3649 0.3172, 0.09790, -0.3519 0.2778, 0.09440, -0.3630 0.2393, 0.08960, -0.3539 0.2056, 0.08360, -0.3153 0.1633, 0.07610, -0.2962 0.1261, 0.06710, -0.2233 0.0900, 0.05640, -0.1522 0.0571, 0.04390, -0.0229 0.0283, 0.02940, 0.1998 0.0142, 0.01970, 0.4440 0.0081, 0.01410, 0.6258 0.0026, 0.00780, 0.8545 0.0000, 0.00000, 0.9880 0.0037, -0.00840, 0.5092 0.0112, -0.01420, 0.2641 0.0191, -0.01930, 0.1691 0.0397, -0.03030, 0.0202 0.0706, -0.04420, -0.1519 0.1037, -0.05710, -0.3046 0.1384, -0.06890, -0.4576 0.1741, -0.07950, -0.5818 0.2102, -0.08660, -0.6980 0.2472, -0.09640, -0.8517 0.2844, -0.10270, -0.9381 0.3225, -0.10690, -1.0286 0.3608, -0.10890, -1.0744 0.3991, -0.10830, -1.0668 0.4373, -0.10510, -0.9619 0.4757, -0.09890, -0.9159 0.5137, -0.09070, -0.4384 0.5514, -0.08120, -0.1455 0.5917, -0.06870, 0.1991 0.5917, -0.02380, 0.2100 0.5917, 0.02120, 0.2092 16 Flap element taps 1.0000, 0.00130, -0.1121 0.9365, 0.01390, 0.1780 0.8333, 0.03280, 0.3512 0.7436, 0.04930, 0.2215 0.7049, 0.05670, 0.2326 0.6667, 0.05450, 0.2208 0.6302, 0.03770, 0.2044 0.6083, 0.01980, 0.1792 0.6000, 0.00000, 0.5453 0.6076, -0.01900, -1.1270 0.6285, -0.03060, -1.4485 0.6667, -0.04090, -1.3371 0.7046, -0.04120, -0.7419 0.7429, -0.03210, -0.3781 0.8333, -0.01400, -0.3724 0.9311, -0.00120, -0.2478 --------- Run Conditions: vel=110.9 ft/s Re=1.014x10^6 AOA=6.03 Flap deflection=-20.00 Totals: Cl=-0.4044 Cdp=0.0170 Cm(c/4)=0.1901 Cs=-0.0594 Ch=-0.1889 Main component: Cl=-0.0598 Cdp=-0.0393 Cm=0.0482 Flap component: Cl=-0.3446 Cdp=0.0563 Cm=0.2420 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.2381 0.5871, 0.07930, 0.1260 0.5501, 0.08690, 0.0220 0.5112, 0.09370, -0.3452 0.4731, 0.09830, -0.3759 0.4349, 0.10070, -0.4183 0.3960, 0.10120, -0.4119 0.3566, 0.10020, -0.4571 0.3172, 0.09790, -0.4589 0.2778, 0.09440, -0.4897 0.2393, 0.08960, -0.5000 0.2056, 0.08360, -0.4696 0.1633, 0.07610, -0.4979 0.1261, 0.06710, -0.4483 0.0900, 0.05640, -0.4286 0.0571, 0.04390, -0.3572 0.0283, 0.02940, -0.2170 0.0142, 0.01970, -0.0265 0.0081, 0.01410, 0.1494 0.0026, 0.00780, 0.3745 0.0000, 0.00000, 0.8894 0.0037, -0.00840, 0.9063 0.0112, -0.01420, 0.6798 0.0191, -0.01930, 0.5490 0.0397, -0.03030, 0.3356 0.0706, -0.04420, 0.1239 0.1037, -0.05710, -0.0522 0.1384, -0.06890, -0.2440 0.1741, -0.07950, -0.3840 0.2102, -0.08660, -0.5044 0.2472, -0.09640, -0.6831 0.2844, -0.10270, -0.7863 0.3225, -0.10690, -0.9097 0.3608, -0.10890, -0.9725 0.3991, -0.10830, -1.0054 0.4373, -0.10510, -0.9093 0.4757, -0.09890, -0.8349 0.5137, -0.09070, -0.8200 0.5514, -0.08120, -0.1533 0.5917, -0.06870, 0.1982 0.5917, -0.02380, 0.2160 0.5917, 0.02120, 0.2178 16 Flap element taps 1.0000, 0.00130, 0.1379 0.9365, 0.01390, 0.2676 0.8333, 0.03280, 0.3766 0.7436, 0.04930, 0.2151 0.7049, 0.05670, 0.2353 0.6667, 0.05450, 0.2244 0.6302, 0.03770, 0.2144 0.6083, 0.01980, 0.1897 0.6000, 0.00000, 0.5316 0.6076, -0.01900, -1.3471 0.6285, -0.03060, -1.7423 0.6667, -0.04090, -1.8736 0.7046, -0.04120, -1.7559 0.7429, -0.03210, -0.5537 0.8333, -0.01400, -0.1119 0.9311, -0.00120, 0.0697 Wake drag found for this condition, Cdw=0.0179 --------- Run Conditions: vel=111.0 ft/s Re=1.014x10^6 AOA=9.02 Flap deflection=-20.00 Totals: Cl=-0.1423 Cdp=0.0119 Cm(c/4)=0.1843 Cs=-0.0340 Ch=-0.1909 Main component: Cl=0.1777 Cdp=-0.0266 Cm=-0.0010 Flap component: Cl=-0.3200 Cdp=0.0385 Cm=0.2200 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.2362 0.5871, 0.07930, 0.1022 0.5501, 0.08690, -0.0386 0.5112, 0.09370, -0.2746 0.4731, 0.09830, -0.4621 0.4349, 0.10070, -0.5319 0.3960, 0.10120, -0.5149 0.3566, 0.10020, -0.5862 0.3172, 0.09790, -0.6081 0.2778, 0.09440, -0.6604 0.2393, 0.08960, -0.6924 0.2056, 0.08360, -0.6810 0.1633, 0.07610, -0.7599 0.1261, 0.06710, -0.7436 0.0900, 0.05640, -0.7931 0.0571, 0.04390, -0.8116 0.0283, 0.02940, -0.8169 0.0142, 0.01970, -0.7661 0.0081, 0.01410, -0.6825 0.0026, 0.00780, -0.4507 0.0000, 0.00000, 0.1064 0.0037, -0.00840, 0.9944 0.0112, -0.01420, 0.9549 0.0191, -0.01930, 0.8577 0.0397, -0.03030, 0.6381 0.0706, -0.04420, 0.4151 0.1037, -0.05710, 0.2301 0.1384, -0.06890, 0.0107 0.1741, -0.07950, -0.1390 0.2102, -0.08660, -0.2569 0.2472, -0.09640, -0.4515 0.2844, -0.10270, -0.5630 0.3225, -0.10690, -0.7140 0.3608, -0.10890, -0.7912 0.3991, -0.10830, -0.8560 0.4373, -0.10510, -0.7822 0.4757, -0.09890, -0.6893 0.5137, -0.09070, -0.6633 0.5514, -0.08120, -0.1161 0.5917, -0.06870, 0.1735 0.5917, -0.02380, 0.1810 0.5917, 0.02120, 0.1740 16 Flap element taps 1.0000, 0.00130, 0.1995 0.9365, 0.01390, 0.2649 0.8333, 0.03280, 0.2843 0.7436, 0.04930, 0.2246 0.7049, 0.05670, 0.2302 0.6667, 0.05450, 0.1846 0.6302, 0.03770, 0.1712 0.6083, 0.01980, 0.1161 0.6000, 0.00000, 0.7387 0.6076, -0.01900, -1.1961 0.6285, -0.03060, -1.6399 0.6667, -0.04090, -1.8530 0.7046, -0.04120, -1.8408 0.7429, -0.03210, -0.5838 0.8333, -0.01400, -0.0581 0.9311, -0.00120, 0.1664 Wake drag found for this condition, Cdw=0.0156 --------- Run Conditions: vel=111.2 ft/s Re=1.013x10^6 AOA=12.04 Flap deflection=-20.00 Totals: Cl=0.1309 Cdp=0.0163 Cm(c/4)=0.1596 Cs=0.0150 Ch=-0.1570 Main component: Cl=0.3657 Cdp=0.0095 Cm=-0.0312 Flap component: Cl=-0.2348 Cdp=0.0068 Cm=0.1580 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.0549 0.5871, 0.07930, 0.0325 0.5501, 0.08690, -0.0127 0.5112, 0.09370, -0.1577 0.4731, 0.09830, -0.3546 0.4349, 0.10070, -0.4791 0.3960, 0.10120, -0.5000 0.3566, 0.10020, -0.6265 0.3172, 0.09790, -0.6727 0.2778, 0.09440, -0.7611 0.2393, 0.08960, -0.8297 0.2056, 0.08360, -0.8455 0.1633, 0.07610, -0.9917 0.1261, 0.06710, -1.0446 0.0900, 0.05640, -1.1798 0.0571, 0.04390, -1.3127 0.0283, 0.02940, -1.5192 0.0142, 0.01970, -1.6841 0.0081, 0.01410, -1.7961 0.0026, 0.00780, -1.6937 0.0000, 0.00000, -1.4372 0.0037, -0.00840, 0.7231 0.0112, -0.01420, 1.0012 0.0191, -0.01930, 1.0010 0.0397, -0.03030, 0.8525 0.0706, -0.04420, 0.6519 0.1037, -0.05710, 0.4728 0.1384, -0.06890, 0.2438 0.1741, -0.07950, 0.0917 0.2102, -0.08660, -0.0211 0.2472, -0.09640, -0.2255 0.2844, -0.10270, -0.3435 0.3225, -0.10690, -0.5146 0.3608, -0.10890, -0.6047 0.3991, -0.10830, -0.6995 0.4373, -0.10510, -0.6526 0.4757, -0.09890, -0.5633 0.5137, -0.09070, -0.5168 0.5514, -0.08120, -0.1732 0.5917, -0.06870, 0.0144 0.5917, -0.02380, 0.0235 0.5917, 0.02120, 0.0228 16 Flap element taps 1.0000, 0.00130, 0.1517 0.9365, 0.01390, 0.1435 0.8333, 0.03280, 0.1326 0.7436, 0.04930, 0.1327 0.7049, 0.05670, 0.0558 0.6667, 0.05450, -0.0495 0.6302, 0.03770, -0.0402 0.6083, 0.01980, -0.1680 0.6000, 0.00000, 0.9678 0.6076, -0.01900, -0.9605 0.6285, -0.03060, -1.4410 0.6667, -0.04090, -1.7096 0.7046, -0.04120, -1.5974 0.7429, -0.03210, -0.5090 0.8333, -0.01400, -0.0415 0.9311, -0.00120, 0.1747 --------- Run Conditions: vel=110.4 ft/s Re=1.005x10^6 AOA=15.02 Flap deflection=-20.00 Totals: Cl=0.8145 Cdp=0.0710 Cm(c/4)=0.0650 Cs=0.1425 Ch=0.0405 Main component: Cl=0.8123 Cdp=0.0689 Cm=-0.1407 Flap component: Cl=0.0021 Cdp=0.0021 Cm=0.0044 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.3073 0.5871, 0.07930, -0.3335 0.5501, 0.08690, -0.3388 0.5112, 0.09370, -0.3596 0.4731, 0.09830, -0.4804 0.4349, 0.10070, -0.6377 0.3960, 0.10120, -0.7152 0.3566, 0.10020, -0.8801 0.3172, 0.09790, -0.9725 0.2778, 0.09440, -1.1044 0.2393, 0.08960, -1.2163 0.2056, 0.08360, -1.2900 0.1633, 0.07610, -1.4885 0.1261, 0.06710, -1.6064 0.0900, 0.05640, -1.8661 0.0571, 0.04390, -2.2138 0.0283, 0.02940, -2.7792 0.0142, 0.01970, -3.3923 0.0081, 0.01410, -4.4721 0.0026, 0.00780, -4.6122 0.0000, 0.00000, -5.2973 0.0037, -0.00840, -0.4884 0.0112, -0.01420, 0.6544 0.0191, -0.01930, 0.9251 0.0397, -0.03030, 1.0009 0.0706, -0.04420, 0.9060 0.1037, -0.05710, 0.7781 0.1384, -0.06890, 0.5793 0.1741, -0.07950, 0.4476 0.2102, -0.08660, 0.3516 0.2472, -0.09640, 0.1699 0.2844, -0.10270, 0.0630 0.3225, -0.10690, -0.0900 0.3608, -0.10890, -0.1776 0.3991, -0.10830, -0.2686 0.4373, -0.10510, -0.2447 0.4757, -0.09890, -0.1825 0.5137, -0.09070, -0.1336 0.5514, -0.08120, -0.0965 0.5917, -0.06870, -0.3454 0.5917, -0.02380, -0.3418 0.5917, 0.02120, -0.3367 16 Flap element taps 1.0000, 0.00130, -0.2970 0.9365, 0.01390, -0.1015 0.8333, 0.03280, -0.0771 0.7436, 0.04930, -0.1810 0.7049, 0.05670, -0.4997 0.6667, 0.05450, -0.5590 0.6302, 0.03770, -0.5549 0.6083, 0.01980, -0.7495 0.6000, 0.00000, 0.9379 0.6076, -0.01900, -0.0177 0.6285, -0.03060, -0.3889 0.6667, -0.04090, -0.2524 0.7046, -0.04120, -0.2636 0.7429, -0.03210, -0.2429 0.8333, -0.01400, -0.2539 0.9311, -0.00120, -0.2534 --------- Run Conditions: vel=110.3 ft/s Re=1.001x10^6 AOA=18.04 Flap deflection=-20.00 Totals: Cl=0.8831 Cdp=0.1111 Cm(c/4)=0.0541 Cs=0.1678 Ch=0.0552 Main component: Cl=0.8462 Cdp=0.1106 Cm=-0.1448 Flap component: Cl=0.0369 Cdp=0.0005 Cm=-0.0197 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.4636 0.5871, 0.07930, -0.4676 0.5501, 0.08690, -0.4689 0.5112, 0.09370, -0.4646 0.4731, 0.09830, -0.4935 0.4349, 0.10070, -0.5438 0.3960, 0.10120, -0.5807 0.3566, 0.10020, -0.7229 0.3172, 0.09790, -0.8412 0.2778, 0.09440, -0.9995 0.2393, 0.08960, -1.1420 0.2056, 0.08360, -1.2622 0.1633, 0.07610, -1.4856 0.1261, 0.06710, -1.6591 0.0900, 0.05640, -1.9711 0.0571, 0.04390, -2.4118 0.0283, 0.02940, -3.1463 0.0142, 0.01970, -3.9267 0.0081, 0.01410, -5.1954 0.0026, 0.00780, -5.8154 0.0000, 0.00000, -6.8749 0.0037, -0.00840, -1.0864 0.0112, -0.01420, 0.4232 0.0191, -0.01930, 0.8259 0.0397, -0.03030, 1.0067 0.0706, -0.04420, 0.9566 0.1037, -0.05710, 0.8497 0.1384, -0.06890, 0.6727 0.1741, -0.07950, 0.5410 0.2102, -0.08660, 0.4352 0.2472, -0.09640, 0.2568 0.2844, -0.10270, 0.1387 0.3225, -0.10690, -0.0127 0.3608, -0.10890, -0.1180 0.3991, -0.10830, -0.2188 0.4373, -0.10510, -0.2165 0.4757, -0.09890, -0.1703 0.5137, -0.09070, -0.1172 0.5514, -0.08120, -0.1163 0.5917, -0.06870, -0.4883 0.5917, -0.02380, -0.4881 0.5917, 0.02120, -0.4871 16 Flap element taps 1.0000, 0.00130, -0.3303 0.9365, 0.01390, -0.1721 0.8333, 0.03280, -0.2167 0.7436, 0.04930, -0.3655 0.7049, 0.05670, -0.7071 0.6667, 0.05450, -0.7480 0.6302, 0.03770, -0.7401 0.6083, 0.01980, -0.9490 0.6000, 0.00000, 0.9221 0.6076, -0.01900, -0.0043 0.6285, -0.03060, -0.4261 0.6667, -0.04090, -0.3107 0.7046, -0.04120, -0.3147 0.7429, -0.03210, -0.3090 0.8333, -0.01400, -0.3181 0.9311, -0.00120, -0.3049 --------- Run Conditions: vel=110.1 ft/s Re=0.998x10^6 AOA=19.99 Flap deflection=-20.00 Totals: Cl=0.5240 Cdp=0.1181 Cm(c/4)=0.1062 Cs=0.0682 Ch=-0.0213 Main component: Cl=0.6067 Cdp=0.1104 Cm=-0.0844 Flap component: Cl=-0.0827 Cdp=0.0077 Cm=0.0574 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.4455 0.5871, 0.07930, -0.4310 0.5501, 0.08690, -0.4446 0.5112, 0.09370, -0.4412 0.4731, 0.09830, -0.4384 0.4349, 0.10070, -0.4305 0.3960, 0.10120, -0.3940 0.3566, 0.10020, -0.4202 0.3172, 0.09790, -0.4454 0.2778, 0.09440, -0.5225 0.2393, 0.08960, -0.6353 0.2056, 0.08360, -0.7860 0.1633, 0.07610, -1.0418 0.1261, 0.06710, -1.2581 0.0900, 0.05640, -1.5772 0.0571, 0.04390, -2.0076 0.0283, 0.02940, -2.6784 0.0142, 0.01970, -3.3207 0.0081, 0.01410, -4.8574 0.0026, 0.00780, -4.9412 0.0000, 0.00000, -5.8450 0.0037, -0.00840, -0.7492 0.0112, -0.01420, 0.5488 0.0191, -0.01930, 0.8834 0.0397, -0.03030, 1.0141 0.0706, -0.04420, 0.9340 0.1037, -0.05710, 0.8118 0.1384, -0.06890, 0.6328 0.1741, -0.07950, 0.4904 0.2102, -0.08660, 0.3619 0.2472, -0.09640, 0.1710 0.2844, -0.10270, 0.0330 0.3225, -0.10690, -0.1284 0.3608, -0.10890, -0.2595 0.3991, -0.10830, -0.3753 0.4373, -0.10510, -0.3924 0.4757, -0.09890, -0.3474 0.5137, -0.09070, -0.2864 0.5514, -0.08120, -0.2812 0.5917, -0.06870, -0.4467 0.5917, -0.02380, -0.4466 0.5917, 0.02120, -0.4524 16 Flap element taps 1.0000, 0.00130, -0.2090 0.9365, 0.01390, -0.2114 0.8333, 0.03280, -0.3136 0.7436, 0.04930, -0.4502 0.7049, 0.05670, -0.6939 0.6667, 0.05450, -0.6876 0.6302, 0.03770, -0.6720 0.6083, 0.01980, -0.8630 0.6000, 0.00000, 0.9682 0.6076, -0.01900, -0.4215 0.6285, -0.03060, -0.9511 0.6667, -0.04090, -1.0028 0.7046, -0.04120, -0.9068 0.7429, -0.03210, -0.9098 0.8333, -0.01400, -0.6355 0.9311, -0.00120, -0.2213 --------- Run Conditions: vel=110.4 ft/s Re=1.000x10^6 AOA=23.98 Flap deflection=-20.00 Totals: Cl=0.1039 Cdp=0.2235 Cm(c/4)=0.0764 Cs=-0.1620 Ch=-0.1222 Main component: Cl=0.2263 Cdp=0.2245 Cm=-0.0414 Flap component: Cl=-0.1224 Cdp=-0.0010 Cm=0.0713 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.5437 0.5871, 0.07930, -0.5147 0.5501, 0.08690, -0.5330 0.5112, 0.09370, -0.5372 0.4731, 0.09830, -0.5457 0.4349, 0.10070, -0.5469 0.3960, 0.10120, -0.5201 0.3566, 0.10020, -0.5360 0.3172, 0.09790, -0.5374 0.2778, 0.09440, -0.5525 0.2393, 0.08960, -0.5387 0.2056, 0.08360, -0.5084 0.1633, 0.07610, -0.5395 0.1261, 0.06710, -0.5237 0.0900, 0.05640, -0.5372 0.0571, 0.04390, -0.5364 0.0283, 0.02940, -0.5470 0.0142, 0.01970, -0.5584 0.0081, 0.01410, -0.5300 0.0026, 0.00780, -0.5234 0.0000, 0.00000, -0.8063 0.0037, -0.00840, 0.5974 0.0112, -0.01420, 0.9537 0.0191, -0.01930, 1.0210 0.0397, -0.03030, 0.9742 0.0706, -0.04420, 0.8297 0.1037, -0.05710, 0.6874 0.1384, -0.06890, 0.5068 0.1741, -0.07950, 0.3558 0.2102, -0.08660, 0.2095 0.2472, -0.09640, 0.0080 0.2844, -0.10270, -0.1458 0.3225, -0.10690, -0.3206 0.3608, -0.10890, -0.4742 0.3991, -0.10830, -0.6039 0.4373, -0.10510, -0.6346 0.4757, -0.09890, -0.5877 0.5137, -0.09070, -0.5216 0.5514, -0.08120, -0.4979 0.5917, -0.06870, -0.5419 0.5917, -0.02380, -0.5420 0.5917, 0.02120, -0.5478 16 Flap element taps 1.0000, 0.00130, -0.5554 0.9365, 0.01390, -0.5867 0.8333, 0.03280, -0.5793 0.7436, 0.04930, -0.5669 0.7049, 0.05670, -0.7567 0.6667, 0.05450, -0.7675 0.6302, 0.03770, -0.7592 0.6083, 0.01980, -0.9642 0.6000, 0.00000, 0.9850 0.6076, -0.01900, -0.8924 0.6285, -0.03060, -1.5706 0.6667, -0.04090, -1.9726 0.7046, -0.04120, -1.7224 0.7429, -0.03210, -1.4430 0.8333, -0.01400, -0.4263 0.9311, -0.00120, -0.2782 --------- Run Conditions: vel=111.0 ft/s Re=1.005x10^6 AOA=26.89 Flap deflection=-20.00 Totals: Cl=0.2832 Cdp=0.3184 Cm(c/4)=0.0348 Cs=-0.1559 Ch=-0.1009 Main component: Cl=0.3339 Cdp=0.3159 Cm=-0.0839 Flap component: Cl=-0.0506 Cdp=0.0025 Cm=0.0196 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.7287 0.5871, 0.07930, -0.6868 0.5501, 0.08690, -0.6997 0.5112, 0.09370, -0.7053 0.4731, 0.09830, -0.7137 0.4349, 0.10070, -0.7140 0.3960, 0.10120, -0.6915 0.3566, 0.10020, -0.6972 0.3172, 0.09790, -0.6993 0.2778, 0.09440, -0.7156 0.2393, 0.08960, -0.7058 0.2056, 0.08360, -0.6836 0.1633, 0.07610, -0.7078 0.1261, 0.06710, -0.6936 0.0900, 0.05640, -0.7038 0.0571, 0.04390, -0.7028 0.0283, 0.02940, -0.7100 0.0142, 0.01970, -0.7213 0.0081, 0.01410, -0.6984 0.0026, 0.00780, -0.6755 0.0000, 0.00000, -0.9364 0.0037, -0.00840, 0.3880 0.0112, -0.01420, 0.8705 0.0191, -0.01930, 0.9957 0.0397, -0.03030, 1.0064 0.0706, -0.04420, 0.8984 0.1037, -0.05710, 0.7758 0.1384, -0.06890, 0.6141 0.1741, -0.07950, 0.4694 0.2102, -0.08660, 0.3240 0.2472, -0.09640, 0.1296 0.2844, -0.10270, -0.0273 0.3225, -0.10690, -0.1994 0.3608, -0.10890, -0.3627 0.3991, -0.10830, -0.5002 0.4373, -0.10510, -0.5502 0.4757, -0.09890, -0.5249 0.5137, -0.09070, -0.4708 0.5514, -0.08120, -0.4325 0.5917, -0.06870, -0.7220 0.5917, -0.02380, -0.7206 0.5917, 0.02120, -0.7279 16 Flap element taps 1.0000, 0.00130, -0.7059 0.9365, 0.01390, -0.7558 0.8333, 0.03280, -0.7652 0.7436, 0.04930, -0.7372 0.7049, 0.05670, -0.9864 0.6667, 0.05450, -0.9953 0.6302, 0.03770, -0.9926 0.6083, 0.01980, -1.2147 0.6000, 0.00000, 0.9676 0.6076, -0.01900, -0.7744 0.6285, -0.03060, -1.4943 0.6667, -0.04090, -1.9594 0.7046, -0.04120, -1.7571 0.7429, -0.03210, -1.3749 0.8333, -0.01400, -0.4401 0.9311, -0.00120, -0.3323