S809 VENTED AILERON MODEL, 18 IN CHORD --------- Run Conditions: vel=111.9 ft/s Re=1.003x10^6 AOA=-6.03 Flap deflection=5.00 Totals: Cl=-0.2878 Cdp=0.0168 Cm(c/4)=-0.0641 Cs=0.0135 Ch=0.0016 Main component: Cl=-0.3740 Cdp=0.0323 Cm=0.0781 Flap component: Cl=0.0862 Cdp=-0.0155 Cm=-0.0701 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1168 0.5871, 0.07930, -0.1542 0.5501, 0.08690, -0.4825 0.5112, 0.09370, -0.4893 0.4731, 0.09830, -0.5291 0.4349, 0.10070, -0.5311 0.3960, 0.10120, -0.4860 0.3566, 0.10020, -0.4067 0.3172, 0.09790, -0.3498 0.2778, 0.09440, -0.3044 0.2393, 0.08960, -0.2513 0.2056, 0.08360, -0.1819 0.1633, 0.07610, -0.0666 0.1261, 0.06710, 0.0445 0.0900, 0.05640, 0.2050 0.0571, 0.04390, 0.4126 0.0283, 0.02940, 0.7013 0.0142, 0.01970, 0.9112 0.0081, 0.01410, 0.9804 0.0026, 0.00780, 0.8854 0.0000, 0.00000, 0.0898 0.0037, -0.00840, -0.8851 0.0112, -0.01420, -0.8142 0.0191, -0.01930, -0.7190 0.0397, -0.03030, -0.6239 0.0706, -0.04420, -0.6479 0.1037, -0.05710, -0.7292 0.1384, -0.06890, -0.7812 0.1741, -0.07950, -0.8487 0.2102, -0.08660, -0.9443 0.2472, -0.09640, -1.0256 0.2844, -0.10270, -1.0723 0.3225, -0.10690, -1.0945 0.3608, -0.10890, -1.1093 0.3991, -0.10830, -1.0415 0.4373, -0.10510, -0.9674 0.4757, -0.09890, -0.9551 0.5137, -0.09070, -0.4480 0.5514, -0.08120, -0.2887 0.5917, -0.06870, -0.0979 0.5917, -0.02380, -0.1044 0.5917, 0.02120, -0.1060 16 Flap element taps 1.0000, 0.00130, 0.1853 0.9365, 0.01390, 0.0780 0.8333, 0.03280, -0.0441 0.7436, 0.04930, -0.2237 0.7049, 0.05670, -0.6764 0.6667, 0.05450, 0.1195 0.6302, 0.03770, -0.1239 0.6083, 0.01980, -0.0965 0.6000, 0.00000, -0.1086 0.6076, -0.01900, -0.1047 0.6285, -0.03060, -0.1043 0.6667, -0.04090, -0.1371 0.7046, -0.04120, 0.0472 0.7429, -0.03210, 0.1577 0.8333, -0.01400, 0.2403 0.9311, -0.00120, 0.2687 Wake drag found for this condition, Cdw=0.0122 --------- Run Conditions: vel=112.8 ft/s Re=1.010x10^6 AOA=0.03 Flap deflection=5.00 Totals: Cl=0.3576 Cdp=0.0116 Cm(c/4)=-0.0838 Cs=-0.0115 Ch=0.0263 Main component: Cl=0.1947 Cdp=0.0175 Cm=-0.0462 Flap component: Cl=0.1629 Cdp=-0.0059 Cm=-0.1270 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1451 0.5871, 0.07930, -0.2266 0.5501, 0.08690, -0.7180 0.5112, 0.09370, -0.7264 0.4731, 0.09830, -0.7794 0.4349, 0.10070, -0.8304 0.3960, 0.10120, -0.8346 0.3566, 0.10020, -0.7793 0.3172, 0.09790, -0.7569 0.2778, 0.09440, -0.7522 0.2393, 0.08960, -0.7436 0.2056, 0.08360, -0.7318 0.1633, 0.07610, -0.6587 0.1261, 0.06710, -0.6159 0.0900, 0.05640, -0.5324 0.0571, 0.04390, -0.4341 0.0283, 0.02940, -0.2572 0.0142, 0.01970, -0.0508 0.0081, 0.01410, 0.0953 0.0026, 0.00780, 0.3917 0.0000, 0.00000, 0.9163 0.0037, -0.00840, 0.9062 0.0112, -0.01420, 0.6861 0.0191, -0.01930, 0.5574 0.0397, -0.03030, 0.3617 0.0706, -0.04420, 0.1563 0.1037, -0.05710, -0.0140 0.1384, -0.06890, -0.1236 0.1741, -0.07950, -0.2439 0.2102, -0.08660, -0.3922 0.2472, -0.09640, -0.5024 0.2844, -0.10270, -0.5969 0.3225, -0.10690, -0.6507 0.3608, -0.10890, -0.7202 0.3991, -0.10830, -0.7070 0.4373, -0.10510, -0.6441 0.4757, -0.09890, -0.5856 0.5137, -0.09070, -0.5572 0.5514, -0.08120, -0.1416 0.5917, -0.06870, -0.0587 0.5917, -0.02380, -0.0497 0.5917, 0.02120, -0.1367 16 Flap element taps 1.0000, 0.00130, 0.1521 0.9365, 0.01390, 0.0525 0.8333, 0.03280, -0.1097 0.7436, 0.04930, -0.3453 0.7049, 0.05670, -0.7840 0.6667, 0.05450, -0.2452 0.6302, 0.03770, -0.1090 0.6083, 0.01980, -0.1127 0.6000, 0.00000, -0.1545 0.6076, -0.01900, -0.1106 0.6285, -0.03060, -0.1513 0.6667, -0.04090, 0.0248 0.7046, -0.04120, 0.4092 0.7429, -0.03210, 0.3275 0.8333, -0.01400, 0.3264 0.9311, -0.00120, 0.3169 Wake drag found for this condition, Cdw=0.0135 --------- Run Conditions: vel=112.9 ft/s Re=1.010x10^6 AOA=3.03 Flap deflection=5.00 Totals: Cl=0.6696 Cdp=0.0181 Cm(c/4)=-0.0894 Cs=0.0173 Ch=0.0342 Main component: Cl=0.4804 Cdp=0.0116 Cm=-0.1098 Flap component: Cl=0.1891 Cdp=0.0065 Cm=-0.1470 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1763 0.5871, 0.07930, -0.3100 0.5501, 0.08690, -0.7153 0.5112, 0.09370, -0.8598 0.4731, 0.09830, -0.9077 0.4349, 0.10070, -0.9757 0.3960, 0.10120, -1.0079 0.3566, 0.10020, -0.9636 0.3172, 0.09790, -0.9626 0.2778, 0.09440, -0.9803 0.2393, 0.08960, -1.0011 0.2056, 0.08360, -1.0280 0.1633, 0.07610, -0.9860 0.1261, 0.06710, -0.9933 0.0900, 0.05640, -0.9739 0.0571, 0.04390, -0.9789 0.0283, 0.02940, -0.9582 0.0142, 0.01970, -0.9048 0.0081, 0.01410, -0.8780 0.0026, 0.00780, -0.4713 0.0000, 0.00000, 0.0240 0.0037, -0.00840, 0.9946 0.0112, -0.01420, 0.9783 0.0191, -0.01930, 0.8867 0.0397, -0.03030, 0.6874 0.0706, -0.04420, 0.4611 0.1037, -0.05710, 0.2772 0.1384, -0.06890, 0.1566 0.1741, -0.07950, 0.0243 0.2102, -0.08660, -0.1416 0.2472, -0.09640, -0.2596 0.2844, -0.10270, -0.3712 0.3225, -0.10690, -0.4337 0.3608, -0.10890, -0.5255 0.3991, -0.10830, -0.5310 0.4373, -0.10510, -0.5005 0.4757, -0.09890, -0.4302 0.5137, -0.09070, -0.3923 0.5514, -0.08120, -0.0678 0.5917, -0.06870, -0.0543 0.5917, -0.02380, -0.0259 0.5917, 0.02120, -0.1655 16 Flap element taps 1.0000, 0.00130, 0.0679 0.9365, 0.01390, -0.0161 0.8333, 0.03280, -0.1300 0.7436, 0.04930, -0.3502 0.7049, 0.05670, -0.8150 0.6667, 0.05450, -0.3351 0.6302, 0.03770, -0.1146 0.6083, 0.01980, -0.1235 0.6000, 0.00000, -0.1978 0.6076, -0.01900, -0.1152 0.6285, -0.03060, -0.1494 0.6667, -0.04090, 0.2188 0.7046, -0.04120, 0.4799 0.7429, -0.03210, 0.3545 0.8333, -0.01400, 0.3478 0.9311, -0.00120, 0.3170 Wake drag found for this condition, Cdw=0.0127 --------- Run Conditions: vel=112.9 ft/s Re=1.009x10^6 AOA=6.04 Flap deflection=5.00 Totals: Cl=0.8351 Cdp=0.0256 Cm(c/4)=-0.0734 Cs=0.0624 Ch=0.0279 Main component: Cl=0.6494 Cdp=0.0075 Cm=-0.1358 Flap component: Cl=0.1857 Cdp=0.0180 Cm=-0.1458 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1844 0.5871, 0.07930, -0.3340 0.5501, 0.08690, -0.4979 0.5112, 0.09370, -0.7618 0.4731, 0.09830, -0.9360 0.4349, 0.10070, -1.0149 0.3960, 0.10120, -1.0554 0.3566, 0.10020, -1.0317 0.3172, 0.09790, -1.0653 0.2778, 0.09440, -1.1187 0.2393, 0.08960, -1.1728 0.2056, 0.08360, -1.2333 0.1633, 0.07610, -1.2233 0.1261, 0.06710, -1.2827 0.0900, 0.05640, -1.3276 0.0571, 0.04390, -1.4389 0.0283, 0.02940, -1.5929 0.0142, 0.01970, -1.7270 0.0081, 0.01410, -1.8799 0.0026, 0.00780, -1.6353 0.0000, 0.00000, -1.3192 0.0037, -0.00840, 0.7579 0.0112, -0.01420, 1.0142 0.0191, -0.01930, 1.0036 0.0397, -0.03030, 0.8645 0.0706, -0.04420, 0.6511 0.1037, -0.05710, 0.4686 0.1384, -0.06890, 0.3464 0.1741, -0.07950, 0.2053 0.2102, -0.08660, 0.0284 0.2472, -0.09640, -0.0919 0.2844, -0.10270, -0.2166 0.3225, -0.10690, -0.2910 0.3608, -0.10890, -0.3973 0.3991, -0.10830, -0.4190 0.4373, -0.10510, -0.4133 0.4757, -0.09890, -0.3502 0.5137, -0.09070, -0.2960 0.5514, -0.08120, -0.2083 0.5917, -0.06870, -0.0343 0.5917, -0.02380, 0.0173 0.5917, 0.02120, -0.1768 16 Flap element taps 1.0000, 0.00130, -0.0629 0.9365, 0.01390, -0.1115 0.8333, 0.03280, -0.1724 0.7436, 0.04930, -0.2643 0.7049, 0.05670, -0.6130 0.6667, 0.05450, -0.3286 0.6302, 0.03770, -0.1198 0.6083, 0.01980, -0.1270 0.6000, 0.00000, -0.2268 0.6076, -0.01900, -0.1053 0.6285, -0.03060, -0.1503 0.6667, -0.04090, 0.3055 0.7046, -0.04120, 0.5007 0.7429, -0.03210, 0.3534 0.8333, -0.01400, 0.3333 0.9311, -0.00120, 0.2734 --------- Run Conditions: vel=112.8 ft/s Re=1.007x10^6 AOA=9.04 Flap deflection=5.00 Totals: Cl=0.9656 Cdp=0.0361 Cm(c/4)=-0.0556 Cs=0.1161 Ch=0.0220 Main component: Cl=0.7893 Cdp=0.0113 Cm=-0.1556 Flap component: Cl=0.1762 Cdp=0.0247 Cm=-0.1398 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.2561 0.5871, 0.07930, -0.3196 0.5501, 0.08690, -0.4289 0.5112, 0.09370, -0.6496 0.4731, 0.09830, -0.8577 0.4349, 0.10070, -0.9785 0.3960, 0.10120, -1.0663 0.3566, 0.10020, -1.0742 0.3172, 0.09790, -1.1204 0.2778, 0.09440, -1.1900 0.2393, 0.08960, -1.2781 0.2056, 0.08360, -1.3765 0.1633, 0.07610, -1.4084 0.1261, 0.06710, -1.5159 0.0900, 0.05640, -1.6341 0.0571, 0.04390, -1.8426 0.0283, 0.02940, -2.2491 0.0142, 0.01970, -2.6404 0.0081, 0.01410, -3.0490 0.0026, 0.00780, -2.9893 0.0000, 0.00000, -3.0889 0.0037, -0.00840, 0.2675 0.0112, -0.01420, 0.9128 0.0191, -0.01930, 1.0138 0.0397, -0.03030, 0.9714 0.0706, -0.04420, 0.7950 0.1037, -0.05710, 0.6226 0.1384, -0.06890, 0.5041 0.1741, -0.07950, 0.3627 0.2102, -0.08660, 0.1801 0.2472, -0.09640, 0.0550 0.2844, -0.10270, -0.0792 0.3225, -0.10690, -0.1644 0.3608, -0.10890, -0.2838 0.3991, -0.10830, -0.3217 0.4373, -0.10510, -0.3371 0.4757, -0.09890, -0.2901 0.5137, -0.09070, -0.2314 0.5514, -0.08120, -0.2054 0.5917, -0.06870, -0.0217 0.5917, -0.02380, 0.0291 0.5917, 0.02120, -0.2353 16 Flap element taps 1.0000, 0.00130, -0.1734 0.9365, 0.01390, -0.1964 0.8333, 0.03280, -0.1804 0.7436, 0.04930, -0.2067 0.7049, 0.05670, -0.3311 0.6667, 0.05450, -0.2785 0.6302, 0.03770, -0.1617 0.6083, 0.01980, -0.1699 0.6000, 0.00000, -0.3182 0.6076, -0.01900, -0.1283 0.6285, -0.03060, -0.1838 0.6667, -0.04090, 0.4736 0.7046, -0.04120, 0.4832 0.7429, -0.03210, 0.3453 0.8333, -0.01400, 0.3136 0.9311, -0.00120, 0.2276 --------- Run Conditions: vel=112.5 ft/s Re=1.004x10^6 AOA=12.06 Flap deflection=5.00 Totals: Cl=1.1600 Cdp=0.0579 Cm(c/4)=-0.0555 Cs=0.1858 Ch=0.0302 Main component: Cl=0.9613 Cdp=0.0227 Cm=-0.1845 Flap component: Cl=0.1987 Cdp=0.0352 Cm=-0.1576 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.4035 0.5871, 0.07930, -0.4253 0.5501, 0.08690, -0.4600 0.5112, 0.09370, -0.5603 0.4731, 0.09830, -0.7558 0.4349, 0.10070, -0.9267 0.3960, 0.10120, -1.0613 0.3566, 0.10020, -1.1130 0.3172, 0.09790, -1.1965 0.2778, 0.09440, -1.2992 0.2393, 0.08960, -1.4220 0.2056, 0.08360, -1.5597 0.1633, 0.07610, -1.6435 0.1261, 0.06710, -1.8128 0.0900, 0.05640, -2.0170 0.0571, 0.04390, -2.3807 0.0283, 0.02940, -2.9468 0.0142, 0.01970, -3.5839 0.0081, 0.01410, -4.7344 0.0026, 0.00780, -4.8604 0.0000, 0.00000, -5.5322 0.0037, -0.00840, -0.5528 0.0112, -0.01420, 0.6405 0.0191, -0.01930, 0.9211 0.0397, -0.03030, 1.0209 0.0706, -0.04420, 0.9094 0.1037, -0.05710, 0.7651 0.1384, -0.06890, 0.6552 0.1741, -0.07950, 0.5192 0.2102, -0.08660, 0.3396 0.2472, -0.09640, 0.2154 0.2844, -0.10270, 0.0766 0.3225, -0.10690, -0.0150 0.3608, -0.10890, -0.1453 0.3991, -0.10830, -0.1980 0.4373, -0.10510, -0.2338 0.4757, -0.09890, -0.2056 0.5137, -0.09070, -0.1576 0.5514, -0.08120, -0.1211 0.5917, -0.06870, -0.0664 0.5917, -0.02380, 0.0368 0.5917, 0.02120, -0.3792 16 Flap element taps 1.0000, 0.00130, -0.2134 0.9365, 0.01390, -0.2448 0.8333, 0.03280, -0.2218 0.7436, 0.04930, -0.2391 0.7049, 0.05670, -0.3047 0.6667, 0.05450, -0.3407 0.6302, 0.03770, -0.2369 0.6083, 0.01980, -0.2498 0.6000, 0.00000, -0.5236 0.6076, -0.01900, -0.2347 0.6285, -0.03060, -0.2697 0.6667, -0.04090, 0.8401 0.7046, -0.04120, 0.4170 0.7429, -0.03210, 0.3560 0.8333, -0.01400, 0.3216 0.9311, -0.00120, 0.2238 --------- Run Conditions: vel=112.1 ft/s Re=0.998x10^6 AOA=15.04 Flap deflection=5.00 Totals: Cl=1.2078 Cdp=0.1101 Cm(c/4)=-0.0703 Cs=0.2071 Ch=0.0400 Main component: Cl=0.9668 Cdp=0.0495 Cm=-0.1753 Flap component: Cl=0.2410 Cdp=0.0607 Cm=-0.1938 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.5327 0.5871, 0.07930, -0.5311 0.5501, 0.08690, -0.5288 0.5112, 0.09370, -0.5386 0.4731, 0.09830, -0.5697 0.4349, 0.10070, -0.6539 0.3960, 0.10120, -0.7912 0.3566, 0.10020, -0.8811 0.3172, 0.09790, -1.0089 0.2778, 0.09440, -1.1509 0.2393, 0.08960, -1.3105 0.2056, 0.08360, -1.4876 0.1633, 0.07610, -1.6178 0.1261, 0.06710, -1.8397 0.0900, 0.05640, -2.1080 0.0571, 0.04390, -2.5724 0.0283, 0.02940, -3.3181 0.0142, 0.01970, -4.1460 0.0081, 0.01410, -5.3891 0.0026, 0.00780, -6.1459 0.0000, 0.00000, -7.1929 0.0037, -0.00840, -1.1925 0.0112, -0.01420, 0.3910 0.0191, -0.01930, 0.8062 0.0397, -0.03030, 1.0178 0.0706, -0.04420, 0.9604 0.1037, -0.05710, 0.8407 0.1384, -0.06890, 0.7401 0.1741, -0.07950, 0.6090 0.2102, -0.08660, 0.4321 0.2472, -0.09640, 0.3068 0.2844, -0.10270, 0.1627 0.3225, -0.10690, 0.0637 0.3608, -0.10890, -0.0745 0.3991, -0.10830, -0.1404 0.4373, -0.10510, -0.1895 0.4757, -0.09890, -0.1780 0.5137, -0.09070, -0.1463 0.5514, -0.08120, -0.0920 0.5917, -0.06870, -0.1272 0.5917, -0.02380, -0.0181 0.5917, 0.02120, -0.5030 16 Flap element taps 1.0000, 0.00130, -0.3528 0.9365, 0.01390, -0.3756 0.8333, 0.03280, -0.3773 0.7436, 0.04930, -0.4174 0.7049, 0.05670, -0.5008 0.6667, 0.05450, -0.5592 0.6302, 0.03770, -0.3102 0.6083, 0.01980, -0.3232 0.6000, 0.00000, -0.7286 0.6076, -0.01900, -0.3660 0.6285, -0.03060, -0.3340 0.6667, -0.04090, 0.9617 0.7046, -0.04120, 0.3663 0.7429, -0.03210, 0.3371 0.8333, -0.01400, 0.2928 0.9311, -0.00120, 0.1747 --------- Run Conditions: vel=110.1 ft/s Re=0.981x10^6 AOA=18.03 Flap deflection=5.00 Totals: Cl=0.6839 Cdp=0.3105 Cm(c/4)=-0.1268 Cs=-0.0836 Ch=0.0427 Main component: Cl=0.4198 Cdp=0.2330 Cm=-0.0985 Flap component: Cl=0.2641 Cdp=0.0775 Cm=-0.2149 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.8202 0.5871, 0.07930, -0.7449 0.5501, 0.08690, -0.6934 0.5112, 0.09370, -0.6845 0.4731, 0.09830, -0.7031 0.4349, 0.10070, -0.7207 0.3960, 0.10120, -0.7527 0.3566, 0.10020, -0.7146 0.3172, 0.09790, -0.7245 0.2778, 0.09440, -0.7291 0.2393, 0.08960, -0.7353 0.2056, 0.08360, -0.7522 0.1633, 0.07610, -0.7160 0.1261, 0.06710, -0.7378 0.0900, 0.05640, -0.7109 0.0571, 0.04390, -0.7272 0.0283, 0.02940, -0.7399 0.0142, 0.01970, -0.7536 0.0081, 0.01410, -0.7773 0.0026, 0.00780, -0.7053 0.0000, 0.00000, -1.0196 0.0037, -0.00840, 0.5773 0.0112, -0.01420, 0.9560 0.0191, -0.01930, 1.0156 0.0397, -0.03030, 0.9746 0.0706, -0.04420, 0.8222 0.1037, -0.05710, 0.6689 0.1384, -0.06890, 0.5519 0.1741, -0.07950, 0.4125 0.2102, -0.08660, 0.2260 0.2472, -0.09640, 0.0889 0.2844, -0.10270, -0.0608 0.3225, -0.10690, -0.1702 0.3608, -0.10890, -0.3168 0.3991, -0.10830, -0.3841 0.4373, -0.10510, -0.4301 0.4757, -0.09890, -0.4076 0.5137, -0.09070, -0.3637 0.5514, -0.08120, -0.3064 0.5917, -0.06870, -0.3453 0.5917, -0.02380, -0.2210 0.5917, 0.02120, -0.7706 16 Flap element taps 1.0000, 0.00130, -0.5692 0.9365, 0.01390, -0.6065 0.8333, 0.03280, -0.5974 0.7436, 0.04930, -0.5895 0.7049, 0.05670, -0.6165 0.6667, 0.05450, -0.8106 0.6302, 0.03770, -0.5554 0.6083, 0.01980, -0.5666 0.6000, 0.00000, -1.0238 0.6076, -0.01900, -0.6024 0.6285, -0.03060, -0.5736 0.6667, -0.04090, 0.9280 0.7046, -0.04120, 0.2554 0.7429, -0.03210, 0.2152 0.8333, -0.01400, 0.1581 0.9311, -0.00120, 0.0189 --------- Run Conditions: vel=111.2 ft/s Re=0.990x10^6 AOA=20.05 Flap deflection=5.00 Totals: Cl=0.7189 Cdp=0.3577 Cm(c/4)=-0.1383 Cs=-0.0895 Ch=0.0467 Main component: Cl=0.4433 Cdp=0.2610 Cm=-0.1100 Flap component: Cl=0.2756 Cdp=0.0966 Cm=-0.2278 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.8330 0.5871, 0.07930, -0.7749 0.5501, 0.08690, -0.7427 0.5112, 0.09370, -0.7275 0.4731, 0.09830, -0.7328 0.4349, 0.10070, -0.7484 0.3960, 0.10120, -0.7856 0.3566, 0.10020, -0.7441 0.3172, 0.09790, -0.7493 0.2778, 0.09440, -0.7474 0.2393, 0.08960, -0.7478 0.2056, 0.08360, -0.7694 0.1633, 0.07610, -0.7227 0.1261, 0.06710, -0.7457 0.0900, 0.05640, -0.7196 0.0571, 0.04390, -0.7329 0.0283, 0.02940, -0.7420 0.0142, 0.01970, -0.7601 0.0081, 0.01410, -0.7853 0.0026, 0.00780, -0.7128 0.0000, 0.00000, -1.0121 0.0037, -0.00840, 0.4976 0.0112, -0.01420, 0.9262 0.0191, -0.01930, 1.0100 0.0397, -0.03030, 0.9968 0.0706, -0.04420, 0.8602 0.1037, -0.05710, 0.7139 0.1384, -0.06890, 0.6067 0.1741, -0.07950, 0.4679 0.2102, -0.08660, 0.2799 0.2472, -0.09640, 0.1439 0.2844, -0.10270, -0.0099 0.3225, -0.10690, -0.1189 0.3608, -0.10890, -0.2718 0.3991, -0.10830, -0.3431 0.4373, -0.10510, -0.3988 0.4757, -0.09890, -0.3851 0.5137, -0.09070, -0.3472 0.5514, -0.08120, -0.2850 0.5917, -0.06870, -0.3410 0.5917, -0.02380, -0.1952 0.5917, 0.02120, -0.7707 16 Flap element taps 1.0000, 0.00130, -0.6279 0.9365, 0.01390, -0.6565 0.8333, 0.03280, -0.6391 0.7436, 0.04930, -0.6567 0.7049, 0.05670, -0.7600 0.6667, 0.05450, -0.8822 0.6302, 0.03770, -0.5446 0.6083, 0.01980, -0.5555 0.6000, 0.00000, -1.0372 0.6076, -0.01900, -0.6166 0.6285, -0.03060, -0.5751 0.6667, -0.04090, 0.9432 0.7046, -0.04120, 0.2457 0.7429, -0.03210, 0.2097 0.8333, -0.01400, 0.1497 0.9311, -0.00120, -0.0011 --------- Run Conditions: vel=112.8 ft/s Re=1.003x10^6 AOA=24.04 Flap deflection=5.00 Totals: Cl=0.7778 Cdp=0.4574 Cm(c/4)=-0.1596 Cs=-0.1009 Ch=0.0467 Main component: Cl=0.4853 Cdp=0.3191 Cm=-0.1307 Flap component: Cl=0.2926 Cdp=0.1383 Cm=-0.2530 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.7997 0.5871, 0.07930, -0.7728 0.5501, 0.08690, -0.7631 0.5112, 0.09370, -0.7653 0.4731, 0.09830, -0.7700 0.4349, 0.10070, -0.7775 0.3960, 0.10120, -0.8073 0.3566, 0.10020, -0.7654 0.3172, 0.09790, -0.7734 0.2778, 0.09440, -0.7741 0.2393, 0.08960, -0.7801 0.2056, 0.08360, -0.8021 0.1633, 0.07610, -0.7591 0.1261, 0.06710, -0.7847 0.0900, 0.05640, -0.7586 0.0571, 0.04390, -0.7670 0.0283, 0.02940, -0.7689 0.0142, 0.01970, -0.7833 0.0081, 0.01410, -0.8092 0.0026, 0.00780, -0.7367 0.0000, 0.00000, -0.9559 0.0037, -0.00840, 0.3052 0.0112, -0.01420, 0.8360 0.0191, -0.01930, 0.9746 0.0397, -0.03030, 1.0192 0.0706, -0.04420, 0.9275 0.1037, -0.05710, 0.8044 0.1384, -0.06890, 0.7109 0.1741, -0.07950, 0.5809 0.2102, -0.08660, 0.4004 0.2472, -0.09640, 0.2714 0.2844, -0.10270, 0.1165 0.3225, -0.10690, 0.0049 0.3608, -0.10890, -0.1525 0.3991, -0.10830, -0.2353 0.4373, -0.10510, -0.3024 0.4757, -0.09890, -0.3056 0.5137, -0.09070, -0.2839 0.5514, -0.08120, -0.2247 0.5917, -0.06870, -0.3316 0.5917, -0.02380, -0.2127 0.5917, 0.02120, -0.7699 16 Flap element taps 1.0000, 0.00130, -0.7407 0.9365, 0.01390, -0.7447 0.8333, 0.03280, -0.7622 0.7436, 0.04930, -0.8145 0.7049, 0.05670, -0.9075 0.6667, 0.05450, -0.8806 0.6302, 0.03770, -0.5093 0.6083, 0.01980, -0.5172 0.6000, 0.00000, -1.0505 0.6076, -0.01900, -0.6343 0.6285, -0.03060, -0.5515 0.6667, -0.04090, 0.9644 0.7046, -0.04120, 0.2400 0.7429, -0.03210, 0.2162 0.8333, -0.01400, 0.1459 0.9311, -0.00120, -0.0235 --------- Run Conditions: vel=112.9 ft/s Re=1.003x10^6 AOA=26.89 Flap deflection=5.00 Totals: Cl=0.8862 Cdp=0.5739 Cm(c/4)=-0.1887 Cs=-0.1110 Ch=0.0450 Main component: Cl=0.5661 Cdp=0.4014 Cm=-0.1657 Flap component: Cl=0.3201 Cdp=0.1725 Cm=-0.2855 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.9226 0.5871, 0.07930, -0.8978 0.5501, 0.08690, -0.8963 0.5112, 0.09370, -0.8999 0.4731, 0.09830, -0.9063 0.4349, 0.10070, -0.9141 0.3960, 0.10120, -0.9416 0.3566, 0.10020, -0.9010 0.3172, 0.09790, -0.9075 0.2778, 0.09440, -0.9069 0.2393, 0.08960, -0.9112 0.2056, 0.08360, -0.9309 0.1633, 0.07610, -0.8896 0.1261, 0.06710, -0.9166 0.0900, 0.05640, -0.8920 0.0571, 0.04390, -0.8995 0.0283, 0.02940, -0.8976 0.0142, 0.01970, -0.9123 0.0081, 0.01410, -0.9376 0.0026, 0.00780, -0.8638 0.0000, 0.00000, -0.9340 0.0037, -0.00840, 0.0699 0.0112, -0.01420, 0.7122 0.0191, -0.01930, 0.9094 0.0397, -0.03030, 1.0177 0.0706, -0.04420, 0.9642 0.1037, -0.05710, 0.8658 0.1384, -0.06890, 0.7873 0.1741, -0.07950, 0.6688 0.2102, -0.08660, 0.4974 0.2472, -0.09640, 0.3717 0.2844, -0.10270, 0.2192 0.3225, -0.10690, 0.1064 0.3608, -0.10890, -0.0540 0.3991, -0.10830, -0.1451 0.4373, -0.10510, -0.2261 0.4757, -0.09890, -0.2432 0.5137, -0.09070, -0.2403 0.5514, -0.08120, -0.1946 0.5917, -0.06870, -0.3983 0.5917, -0.02380, -0.3287 0.5917, 0.02120, -0.8911 16 Flap element taps 1.0000, 0.00130, -0.8846 0.9365, 0.01390, -0.9049 0.8333, 0.03280, -0.9173 0.7436, 0.04930, -0.9373 0.7049, 0.05670, -1.0556 0.6667, 0.05450, -1.0336 0.6302, 0.03770, -0.5262 0.6083, 0.01980, -0.5471 0.6000, 0.00000, -1.3008 0.6076, -0.01900, -0.8372 0.6285, -0.03060, -0.5378 0.6667, -0.04090, 0.9377 0.7046, -0.04120, 0.2200 0.7429, -0.03210, 0.2156 0.8333, -0.01400, 0.1349 0.9311, -0.00120, -0.0587