S809 VENTED AILERON MODEL, 18 IN CHORD --------- Run Conditions: vel=115.0 ft/s Re=1.021x10^6 AOA=-6.01 Flap deflection=-5.00 Totals: Cl=-0.6316 Cdp=0.0545 Cm(c/4)=0.0440 Cs=0.0119 Ch=-0.0366 Main component: Cl=-0.5039 Cdp=0.0886 Cm=0.1093 Flap component: Cl=-0.1277 Cdp=-0.0340 Cm=0.0931 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.7852 0.5871, 0.07930, -0.2289 0.5501, 0.08690, -0.3912 0.5112, 0.09370, -0.4116 0.4731, 0.09830, -0.4366 0.4349, 0.10070, -0.4185 0.3960, 0.10120, -0.3660 0.3566, 0.10020, -0.2894 0.3172, 0.09790, -0.2304 0.2778, 0.09440, -0.1806 0.2393, 0.08960, -0.1221 0.2056, 0.08360, -0.0485 0.1633, 0.07610, 0.0611 0.1261, 0.06710, 0.1801 0.0900, 0.05640, 0.3400 0.0571, 0.04390, 0.5470 0.0283, 0.02940, 0.8204 0.0142, 0.01970, 0.9811 0.0081, 0.01410, 0.9964 0.0026, 0.00780, 0.7097 0.0000, 0.00000, -0.5246 0.0037, -0.00840, -1.5244 0.0112, -0.01420, -1.2819 0.0191, -0.01930, -1.0902 0.0397, -0.03030, -0.8916 0.0706, -0.04420, -0.8572 0.1037, -0.05710, -0.9110 0.1384, -0.06890, -0.9542 0.1741, -0.07950, -1.0111 0.2102, -0.08660, -1.0888 0.2472, -0.09640, -1.1706 0.2844, -0.10270, -1.2021 0.3225, -0.10690, -1.2184 0.3608, -0.10890, -1.2223 0.3991, -0.10830, -1.1413 0.4373, -0.10510, -1.0784 0.4757, -0.09890, -0.8197 0.5137, -0.09070, -0.4845 0.5514, -0.08120, -0.2092 0.5917, -0.06870, 0.0615 0.5917, -0.02380, -0.7036 0.5917, 0.02120, -0.6253 16 Flap element taps 1.0000, 0.00130, 0.0400 0.9365, 0.01390, 0.0868 0.8333, 0.03280, 0.1465 0.7436, 0.04930, 0.2688 0.7049, 0.05670, 0.4518 0.6667, 0.05450, 0.8297 0.6302, 0.03770, -0.9437 0.6083, 0.01980, -0.7398 0.6000, 0.00000, -0.9971 0.6076, -0.01900, -0.4882 0.6285, -0.03060, -0.3726 0.6667, -0.04090, -0.3827 0.7046, -0.04120, -0.4407 0.7429, -0.03210, -0.2225 0.8333, -0.01400, -0.0824 0.9311, -0.00120, 0.0040 --------- Run Conditions: vel=114.0 ft/s Re=1.011x10^6 AOA=-0.01 Flap deflection=-5.00 Totals: Cl=-0.1818 Cdp=0.0144 Cm(c/4)=0.0368 Cs=-0.0144 Ch=-0.0328 Main component: Cl=-0.1201 Cdp=0.0327 Cm=0.0380 Flap component: Cl=-0.0617 Cdp=-0.0183 Cm=0.0443 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.2440 0.5871, 0.07930, -0.1378 0.5501, 0.08690, -0.5184 0.5112, 0.09370, -0.5180 0.4731, 0.09830, -0.5666 0.4349, 0.10070, -0.5957 0.3960, 0.10120, -0.5893 0.3566, 0.10020, -0.5361 0.3172, 0.09790, -0.5103 0.2778, 0.09440, -0.4953 0.2393, 0.08960, -0.4762 0.2056, 0.08360, -0.4499 0.1633, 0.07610, -0.3744 0.1261, 0.06710, -0.3041 0.0900, 0.05640, -0.2012 0.0571, 0.04390, -0.0556 0.0283, 0.02940, 0.1870 0.0142, 0.01970, 0.4347 0.0081, 0.01410, 0.6000 0.0026, 0.00780, 0.8561 0.0000, 0.00000, 0.9922 0.0037, -0.00840, 0.4980 0.0112, -0.01420, 0.2577 0.0191, -0.01930, 0.1706 0.0397, -0.03030, 0.0289 0.0706, -0.04420, -0.1410 0.1037, -0.05710, -0.2944 0.1384, -0.06890, -0.4058 0.1741, -0.07950, -0.5210 0.2102, -0.08660, -0.6565 0.2472, -0.09640, -0.7796 0.2844, -0.10270, -0.8641 0.3225, -0.10690, -0.9284 0.3608, -0.10890, -0.9947 0.3991, -0.10830, -0.9730 0.4373, -0.10510, -0.9034 0.4757, -0.09890, -0.8363 0.5137, -0.09070, -0.7682 0.5514, -0.08120, -0.3016 0.5917, -0.06870, -0.1316 0.5917, -0.02380, -0.1650 0.5917, 0.02120, -0.1159 16 Flap element taps 1.0000, 0.00130, 0.1820 0.9365, 0.01390, 0.1380 0.8333, 0.03280, 0.1346 0.7436, 0.04930, 0.2230 0.7049, 0.05670, 0.3713 0.6667, 0.05450, -0.1759 0.6302, 0.03770, -0.1862 0.6083, 0.01980, -0.1371 0.6000, 0.00000, -0.1628 0.6076, -0.01900, -0.1550 0.6285, -0.03060, -0.1437 0.6667, -0.04090, -0.2177 0.7046, -0.04120, -0.5609 0.7429, -0.03210, -0.1543 0.8333, -0.01400, 0.0857 0.9311, -0.00120, 0.1982 Wake drag found for this condition, Cdw=0.0127 --------- Run Conditions: vel=114.3 ft/s Re=1.012x10^6 AOA=3.03 Flap deflection=-5.00 Totals: Cl=0.1225 Cdp=0.0092 Cm(c/4)=0.0277 Cs=-0.0027 Ch=-0.0242 Main component: Cl=0.1498 Cdp=0.0289 Cm=-0.0218 Flap component: Cl=-0.0274 Cdp=-0.0197 Cm=0.0188 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1404 0.5871, 0.07930, -0.1527 0.5501, 0.08690, -0.6233 0.5112, 0.09370, -0.6169 0.4731, 0.09830, -0.6626 0.4349, 0.10070, -0.7121 0.3960, 0.10120, -0.7340 0.3566, 0.10020, -0.6959 0.3172, 0.09790, -0.6915 0.2778, 0.09440, -0.6984 0.2393, 0.08960, -0.7032 0.2056, 0.08360, -0.7067 0.1633, 0.07610, -0.6613 0.1261, 0.06710, -0.6305 0.0900, 0.05640, -0.5775 0.0571, 0.04390, -0.5089 0.0283, 0.02940, -0.3700 0.0142, 0.01970, -0.1944 0.0081, 0.01410, -0.0608 0.0026, 0.00780, 0.2029 0.0000, 0.00000, 0.8036 0.0037, -0.00840, 0.9629 0.0112, -0.01420, 0.7637 0.0191, -0.01930, 0.6403 0.0397, -0.03030, 0.4279 0.0706, -0.04420, 0.2071 0.1037, -0.05710, 0.0258 0.1384, -0.06890, -0.1073 0.1741, -0.07950, -0.2406 0.2102, -0.08660, -0.3937 0.2472, -0.09640, -0.5303 0.2844, -0.10270, -0.6345 0.3225, -0.10690, -0.7134 0.3608, -0.10890, -0.8012 0.3991, -0.10830, -0.8043 0.4373, -0.10510, -0.7607 0.4757, -0.09890, -0.6755 0.5137, -0.09070, -0.6375 0.5514, -0.08120, -0.2182 0.5917, -0.06870, -0.1310 0.5917, -0.02380, -0.1484 0.5917, 0.02120, -0.1422 16 Flap element taps 1.0000, 0.00130, 0.1845 0.9365, 0.01390, 0.1318 0.8333, 0.03280, 0.1080 0.7436, 0.04930, 0.1493 0.7049, 0.05670, 0.1286 0.6667, 0.05450, -0.1911 0.6302, 0.03770, -0.1419 0.6083, 0.01980, -0.1312 0.6000, 0.00000, -0.1394 0.6076, -0.01900, -0.1533 0.6285, -0.03060, -0.0848 0.6667, -0.04090, -0.0956 0.7046, -0.04120, -0.5740 0.7429, -0.03210, -0.1041 0.8333, -0.01400, 0.1324 0.9311, -0.00120, 0.2384 Wake drag found for this condition, Cdw=0.0131 --------- Run Conditions: vel=114.3 ft/s Re=1.011x10^6 AOA=6.02 Flap deflection=-5.00 Totals: Cl=0.4281 Cdp=0.0101 Cm(c/4)=0.0178 Cs=0.0348 Ch=-0.0125 Main component: Cl=0.4135 Cdp=0.0248 Cm=-0.0763 Flap component: Cl=0.0146 Cdp=-0.0147 Cm=-0.0126 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1305 0.5871, 0.07930, -0.2305 0.5501, 0.08690, -0.3393 0.5112, 0.09370, -0.7546 0.4731, 0.09830, -0.7989 0.4349, 0.10070, -0.8471 0.3960, 0.10120, -0.8836 0.3566, 0.10020, -0.8633 0.3172, 0.09790, -0.8792 0.2778, 0.09440, -0.9091 0.2393, 0.08960, -0.9425 0.2056, 0.08360, -0.9798 0.1633, 0.07610, -0.9709 0.1261, 0.06710, -0.9905 0.0900, 0.05640, -1.0061 0.0571, 0.04390, -1.0438 0.0283, 0.02940, -1.0726 0.0142, 0.01970, -1.0657 0.0081, 0.01410, -1.0700 0.0026, 0.00780, -0.7717 0.0000, 0.00000, -0.2487 0.0037, -0.00840, 0.9649 0.0112, -0.01420, 0.9958 0.0191, -0.01930, 0.9256 0.0397, -0.03030, 0.7293 0.0706, -0.04420, 0.4983 0.1037, -0.05710, 0.3108 0.1384, -0.06890, 0.1660 0.1741, -0.07950, 0.0212 0.2102, -0.08660, -0.1436 0.2472, -0.09640, -0.2856 0.2844, -0.10270, -0.4036 0.3225, -0.10690, -0.4968 0.3608, -0.10890, -0.6019 0.3991, -0.10830, -0.6287 0.4373, -0.10510, -0.6138 0.4757, -0.09890, -0.5314 0.5137, -0.09070, -0.4768 0.5514, -0.08120, -0.2313 0.5917, -0.06870, -0.1428 0.5917, -0.02380, -0.1059 0.5917, 0.02120, -0.1160 16 Flap element taps 1.0000, 0.00130, 0.1707 0.9365, 0.01390, 0.1171 0.8333, 0.03280, 0.0576 0.7436, 0.04930, -0.0172 0.7049, 0.05670, -0.0937 0.6667, 0.05450, -0.1106 0.6302, 0.03770, -0.1156 0.6083, 0.01980, -0.1152 0.6000, 0.00000, -0.1364 0.6076, -0.01900, -0.2857 0.6285, -0.03060, 0.2435 0.6667, -0.04090, -0.0342 0.7046, -0.04120, -0.5639 0.7429, -0.03210, -0.0490 0.8333, -0.01400, 0.1710 0.9311, -0.00120, 0.2626 Wake drag found for this condition, Cdw=0.0127 --------- Run Conditions: vel=114.4 ft/s Re=1.011x10^6 AOA=9.06 Flap deflection=-5.00 Totals: Cl=0.6108 Cdp=0.0187 Cm(c/4)=0.0191 Cs=0.0777 Ch=-0.0177 Main component: Cl=0.5724 Cdp=0.0211 Cm=-0.0993 Flap component: Cl=0.0384 Cdp=-0.0023 Cm=-0.0332 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.0943 0.5871, 0.07930, -0.1811 0.5501, 0.08690, -0.3265 0.5112, 0.09370, -0.5459 0.4731, 0.09830, -0.7419 0.4349, 0.10070, -0.8364 0.3960, 0.10120, -0.8970 0.3566, 0.10020, -0.9091 0.3172, 0.09790, -0.9431 0.2778, 0.09440, -0.9977 0.2393, 0.08960, -1.0663 0.2056, 0.08360, -1.1329 0.1633, 0.07610, -1.1741 0.1261, 0.06710, -1.2635 0.0900, 0.05640, -1.3558 0.0571, 0.04390, -1.5038 0.0283, 0.02940, -1.7201 0.0142, 0.01970, -1.9174 0.0081, 0.01410, -2.1336 0.0026, 0.00780, -1.9550 0.0000, 0.00000, -1.7417 0.0037, -0.00840, 0.6526 0.0112, -0.01420, 0.9955 0.0191, -0.01930, 1.0153 0.0397, -0.03030, 0.8937 0.0706, -0.04420, 0.6856 0.1037, -0.05710, 0.5052 0.1384, -0.06890, 0.3559 0.1741, -0.07950, 0.2067 0.2102, -0.08660, 0.0389 0.2472, -0.09640, -0.1084 0.2844, -0.10270, -0.2347 0.3225, -0.10690, -0.3400 0.3608, -0.10890, -0.4586 0.3991, -0.10830, -0.5037 0.4373, -0.10510, -0.5130 0.4757, -0.09890, -0.4422 0.5137, -0.09070, -0.3780 0.5514, -0.08120, -0.3531 0.5917, -0.06870, -0.1477 0.5917, -0.02380, -0.0773 0.5917, 0.02120, -0.0902 16 Flap element taps 1.0000, 0.00130, 0.0151 0.9365, 0.01390, -0.0385 0.8333, 0.03280, -0.0713 0.7436, 0.04930, -0.0771 0.7049, 0.05670, -0.0806 0.6667, 0.05450, -0.0822 0.6302, 0.03770, -0.0915 0.6083, 0.01980, -0.0929 0.6000, 0.00000, -0.1206 0.6076, -0.01900, -0.3019 0.6285, -0.03060, 0.3746 0.6667, -0.04090, -0.0287 0.7046, -0.04120, -0.5643 0.7429, -0.03210, -0.0474 0.8333, -0.01400, 0.1502 0.9311, -0.00120, 0.2102 Wake drag found for this condition, Cdw=0.0187 --------- Run Conditions: vel=114.3 ft/s Re=1.009x10^6 AOA=12.04 Flap deflection=-5.00 Totals: Cl=0.7812 Cdp=0.0279 Cm(c/4)=0.0227 Cs=0.1357 Ch=0.0148 Main component: Cl=0.7004 Cdp=0.0698 Cm=-0.1150 Flap component: Cl=0.0808 Cdp=-0.0419 Cm=-0.0548 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.2316 0.5871, 0.07930, -0.2614 0.5501, 0.08690, -0.3284 0.5112, 0.09370, -0.4693 0.4731, 0.09830, -0.6737 0.4349, 0.10070, -0.8110 0.3960, 0.10120, -0.9062 0.3566, 0.10020, -0.9579 0.3172, 0.09790, -1.0265 0.2778, 0.09440, -1.1105 0.2393, 0.08960, -1.2098 0.2056, 0.08360, -1.3134 0.1633, 0.07610, -1.3981 0.1261, 0.06710, -1.5155 0.0900, 0.05640, -1.6839 0.0571, 0.04390, -1.9494 0.0283, 0.02940, -2.3451 0.0142, 0.01970, -2.9570 0.0081, 0.01410, -3.4406 0.0026, 0.00780, -3.4891 0.0000, 0.00000, -3.7317 0.0037, -0.00840, 0.0596 0.0112, -0.01420, 0.8451 0.0191, -0.01930, 0.9980 0.0397, -0.03030, 0.9847 0.0706, -0.04420, 0.8265 0.1037, -0.05710, 0.6597 0.1384, -0.06890, 0.5111 0.1741, -0.07950, 0.3653 0.2102, -0.08660, 0.1996 0.2472, -0.09640, 0.0442 0.2844, -0.10270, -0.0899 0.3225, -0.10690, -0.2139 0.3608, -0.10890, -0.3452 0.3991, -0.10830, -0.4169 0.4373, -0.10510, -0.4536 0.4757, -0.09890, -0.4204 0.5137, -0.09070, -0.3836 0.5514, -0.08120, -0.3277 0.5917, -0.06870, -1.0696 0.5917, -0.02380, -0.5183 0.5917, 0.02120, -0.1420 16 Flap element taps 1.0000, 0.00130, -0.0022 0.9365, 0.01390, -0.0164 0.8333, 0.03280, -0.0441 0.7436, 0.04930, -0.0865 0.7049, 0.05670, -0.1485 0.6667, 0.05450, -0.1216 0.6302, 0.03770, -0.3654 0.6083, 0.01980, -0.4306 0.6000, 0.00000, -1.5716 0.6076, -0.01900, -0.9976 0.6285, -0.03060, 0.9455 0.6667, -0.04090, 0.0248 0.7046, -0.04120, -0.4225 0.7429, -0.03210, 0.0388 0.8333, -0.01400, 0.1771 0.9311, -0.00120, 0.2176 --------- Run Conditions: vel=113.7 ft/s Re=1.004x10^6 AOA=15.03 Flap deflection=-5.00 Totals: Cl=0.9520 Cdp=0.0514 Cm(c/4)=0.0141 Cs=0.1972 Ch=0.0282 Main component: Cl=0.8312 Cdp=0.0847 Cm=-0.1359 Flap component: Cl=0.1208 Cdp=-0.0333 Cm=-0.0831 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.3699 0.5871, 0.07930, -0.3948 0.5501, 0.08690, -0.4045 0.5112, 0.09370, -0.4225 0.4731, 0.09830, -0.5266 0.4349, 0.10070, -0.6764 0.3960, 0.10120, -0.8058 0.3566, 0.10020, -0.9245 0.3172, 0.09790, -1.0335 0.2778, 0.09440, -1.1554 0.2393, 0.08960, -1.2865 0.2056, 0.08360, -1.4158 0.1633, 0.07610, -1.5670 0.1261, 0.06710, -1.7344 0.0900, 0.05640, -1.9905 0.0571, 0.04390, -2.3839 0.0283, 0.02940, -3.0174 0.0142, 0.01970, -3.6875 0.0081, 0.01410, -4.9603 0.0026, 0.00780, -5.2694 0.0000, 0.00000, -6.0304 0.0037, -0.00840, -0.7530 0.0112, -0.01420, 0.5554 0.0191, -0.01930, 0.8843 0.0397, -0.03030, 1.0090 0.0706, -0.04420, 0.9234 0.1037, -0.05710, 0.7894 0.1384, -0.06890, 0.6384 0.1741, -0.07950, 0.5008 0.2102, -0.08660, 0.3527 0.2472, -0.09640, 0.1931 0.2844, -0.10270, 0.0631 0.3225, -0.10690, -0.0793 0.3608, -0.10890, -0.2084 0.3991, -0.10830, -0.2991 0.4373, -0.10510, -0.3455 0.4757, -0.09890, -0.3294 0.5137, -0.09070, -0.3096 0.5514, -0.08120, -0.2640 0.5917, -0.06870, -1.0619 0.5917, -0.02380, -0.5245 0.5917, 0.02120, -0.3343 16 Flap element taps 1.0000, 0.00130, -0.1072 0.9365, 0.01390, -0.1202 0.8333, 0.03280, -0.1336 0.7436, 0.04930, -0.1696 0.7049, 0.05670, -0.2538 0.6667, 0.05450, -0.2327 0.6302, 0.03770, -0.5540 0.6083, 0.01980, -0.6272 0.6000, 0.00000, -1.6182 0.6076, -0.01900, -0.9435 0.6285, -0.03060, 0.9475 0.6667, -0.04090, 0.0541 0.7046, -0.04120, -0.3984 0.7429, -0.03210, 0.0471 0.8333, -0.01400, 0.1638 0.9311, -0.00120, 0.1815 --------- Run Conditions: vel=113.7 ft/s Re=1.004x10^6 AOA=18.00 Flap deflection=-5.00 Totals: Cl=0.8893 Cdp=0.1139 Cm(c/4)=-0.0171 Cs=0.1665 Ch=0.0414 Main component: Cl=0.7055 Cdp=0.1260 Cm=-0.1055 Flap component: Cl=0.1839 Cdp=-0.0121 Cm=-0.1319 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.5392 0.5871, 0.07930, -0.5309 0.5501, 0.08690, -0.5349 0.5112, 0.09370, -0.5273 0.4731, 0.09830, -0.5289 0.4349, 0.10070, -0.5281 0.3960, 0.10120, -0.5117 0.3566, 0.10020, -0.5433 0.3172, 0.09790, -0.5898 0.2778, 0.09440, -0.6825 0.2393, 0.08960, -0.8383 0.2056, 0.08360, -1.0197 0.1633, 0.07610, -1.2579 0.1261, 0.06710, -1.4878 0.0900, 0.05640, -1.8113 0.0571, 0.04390, -2.2678 0.0283, 0.02940, -3.0011 0.0142, 0.01970, -3.7644 0.0081, 0.01410, -5.1038 0.0026, 0.00780, -5.7252 0.0000, 0.00000, -6.6699 0.0037, -0.00840, -1.0406 0.0112, -0.01420, 0.4358 0.0191, -0.01930, 0.8269 0.0397, -0.03030, 1.0058 0.0706, -0.04420, 0.9534 0.1037, -0.05710, 0.8346 0.1384, -0.06890, 0.6728 0.1741, -0.07950, 0.5396 0.2102, -0.08660, 0.4039 0.2472, -0.09640, 0.2340 0.2844, -0.10270, 0.1031 0.3225, -0.10690, -0.0575 0.3608, -0.10890, -0.1912 0.3991, -0.10830, -0.3008 0.4373, -0.10510, -0.3524 0.4757, -0.09890, -0.3489 0.5137, -0.09070, -0.3419 0.5514, -0.08120, -0.3008 0.5917, -0.06870, -1.1901 0.5917, -0.02380, -0.6675 0.5917, 0.02120, -0.5426 16 Flap element taps 1.0000, 0.00130, -0.3445 0.9365, 0.01390, -0.3673 0.8333, 0.03280, -0.3886 0.7436, 0.04930, -0.4343 0.7049, 0.05670, -0.5685 0.6667, 0.05450, -0.4253 0.6302, 0.03770, -0.8026 0.6083, 0.01980, -0.9019 0.6000, 0.00000, -1.8300 0.6076, -0.01900, -1.0375 0.6285, -0.03060, 0.9468 0.6667, -0.04090, 0.0078 0.7046, -0.04120, -0.4890 0.7429, -0.03210, -0.0276 0.8333, -0.01400, 0.0785 0.9311, -0.00120, 0.0655 --------- Run Conditions: vel=113.8 ft/s Re=1.005x10^6 AOA=20.01 Flap deflection=-5.00 Totals: Cl=0.4740 Cdp=0.2603 Cm(c/4)=-0.0575 Cs=-0.0824 Ch=0.0400 Main component: Cl=0.2850 Cdp=0.2703 Cm=-0.0565 Flap component: Cl=0.1890 Cdp=-0.0100 Cm=-0.1346 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.6952 0.5871, 0.07930, -0.6318 0.5501, 0.08690, -0.6390 0.5112, 0.09370, -0.6474 0.4731, 0.09830, -0.6714 0.4349, 0.10070, -0.6768 0.3960, 0.10120, -0.6471 0.3566, 0.10020, -0.6740 0.3172, 0.09790, -0.6801 0.2778, 0.09440, -0.6844 0.2393, 0.08960, -0.6754 0.2056, 0.08360, -0.6408 0.1633, 0.07610, -0.6725 0.1261, 0.06710, -0.6603 0.0900, 0.05640, -0.6687 0.0571, 0.04390, -0.6646 0.0283, 0.02940, -0.6815 0.0142, 0.01970, -0.6910 0.0081, 0.01410, -0.6652 0.0026, 0.00780, -0.6593 0.0000, 0.00000, -0.9695 0.0037, -0.00840, 0.5851 0.0112, -0.01420, 0.9530 0.0191, -0.01930, 1.0135 0.0397, -0.03030, 0.9609 0.0706, -0.04420, 0.8208 0.1037, -0.05710, 0.6705 0.1384, -0.06890, 0.4874 0.1741, -0.07950, 0.3471 0.2102, -0.08660, 0.2118 0.2472, -0.09640, 0.0245 0.2844, -0.10270, -0.1089 0.3225, -0.10690, -0.2841 0.3608, -0.10890, -0.4239 0.3991, -0.10830, -0.5408 0.4373, -0.10510, -0.5838 0.4757, -0.09890, -0.5707 0.5137, -0.09070, -0.5593 0.5514, -0.08120, -0.5087 0.5917, -0.06870, -1.5353 0.5917, -0.02380, -0.9093 0.5917, 0.02120, -0.6680 16 Flap element taps 1.0000, 0.00130, -0.5099 0.9365, 0.01390, -0.5343 0.8333, 0.03280, -0.5430 0.7436, 0.04930, -0.6107 0.7049, 0.05670, -0.7404 0.6667, 0.05450, -0.5603 0.6302, 0.03770, -0.9535 0.6083, 0.01980, -1.0722 0.6000, 0.00000, -2.2520 0.6076, -0.01900, -1.3557 0.6285, -0.03060, 0.9368 0.6667, -0.04090, -0.1452 0.7046, -0.04120, -0.7233 0.7429, -0.03210, -0.1894 0.8333, -0.01400, -0.0636 0.9311, -0.00120, -0.0737 --------- Run Conditions: vel=113.7 ft/s Re=1.004x10^6 AOA=25.52 Flap deflection=-5.00 Totals: Cl=0.5148 Cdp=0.3473 Cm(c/4)=-0.0780 Cs=-0.0917 Ch=0.0348 Main component: Cl=0.3020 Cdp=0.3199 Cm=-0.0722 Flap component: Cl=0.2128 Cdp=0.0275 Cm=-0.1593 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.6873 0.5871, 0.07930, -0.6579 0.5501, 0.08690, -0.6710 0.5112, 0.09370, -0.6662 0.4731, 0.09830, -0.6799 0.4349, 0.10070, -0.6781 0.3960, 0.10120, -0.6388 0.3566, 0.10020, -0.6710 0.3172, 0.09790, -0.6802 0.2778, 0.09440, -0.6860 0.2393, 0.08960, -0.6821 0.2056, 0.08360, -0.6455 0.1633, 0.07610, -0.6841 0.1261, 0.06710, -0.6694 0.0900, 0.05640, -0.6818 0.0571, 0.04390, -0.6731 0.0283, 0.02940, -0.6811 0.0142, 0.01970, -0.6922 0.0081, 0.01410, -0.6624 0.0026, 0.00780, -0.6620 0.0000, 0.00000, -0.9372 0.0037, -0.00840, 0.4251 0.0112, -0.01420, 0.8826 0.0191, -0.01930, 0.9917 0.0397, -0.03030, 0.9901 0.0706, -0.04420, 0.8875 0.1037, -0.05710, 0.7604 0.1384, -0.06890, 0.5822 0.1741, -0.07950, 0.4507 0.2102, -0.08660, 0.3276 0.2472, -0.09640, 0.1392 0.2844, -0.10270, 0.0074 0.3225, -0.10690, -0.1763 0.3608, -0.10890, -0.3200 0.3991, -0.10830, -0.4490 0.4373, -0.10510, -0.5042 0.4757, -0.09890, -0.5064 0.5137, -0.09070, -0.5073 0.5514, -0.08120, -0.4698 0.5917, -0.06870, -1.4981 0.5917, -0.02380, -0.8773 0.5917, 0.02120, -0.6856 16 Flap element taps 1.0000, 0.00130, -0.6824 0.9365, 0.01390, -0.7092 0.8333, 0.03280, -0.7109 0.7436, 0.04930, -0.6928 0.7049, 0.05670, -0.7952 0.6667, 0.05450, -0.5751 0.6302, 0.03770, -0.9603 0.6083, 0.01980, -1.0967 0.6000, 0.00000, -2.2209 0.6076, -0.01900, -1.3260 0.6285, -0.03060, 0.9321 0.6667, -0.04090, -0.1440 0.7046, -0.04120, -0.7354 0.7429, -0.03210, -0.2081 0.8333, -0.01400, -0.0987 0.9311, -0.00120, -0.1351 --------- Run Conditions: vel=113.8 ft/s Re=1.005x10^6 AOA=26.90 Flap deflection=-5.00 Totals: Cl=0.6089 Cdp=0.4145 Cm(c/4)=-0.0977 Cs=-0.0941 Ch=0.0416 Main component: Cl=0.3721 Cdp=0.3698 Cm=-0.0999 Flap component: Cl=0.2369 Cdp=0.0447 Cm=-0.1804 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.7631 0.5871, 0.07930, -0.7394 0.5501, 0.08690, -0.7508 0.5112, 0.09370, -0.7437 0.4731, 0.09830, -0.7576 0.4349, 0.10070, -0.7550 0.3960, 0.10120, -0.7129 0.3566, 0.10020, -0.7461 0.3172, 0.09790, -0.7545 0.2778, 0.09440, -0.7633 0.2393, 0.08960, -0.7580 0.2056, 0.08360, -0.7200 0.1633, 0.07610, -0.7654 0.1261, 0.06710, -0.7476 0.0900, 0.05640, -0.7635 0.0571, 0.04390, -0.7544 0.0283, 0.02940, -0.7563 0.0142, 0.01970, -0.7702 0.0081, 0.01410, -0.7385 0.0026, 0.00780, -0.7386 0.0000, 0.00000, -0.8555 0.0037, -0.00840, 0.2416 0.0112, -0.01420, 0.7927 0.0191, -0.01930, 0.9518 0.0397, -0.03030, 1.0015 0.0706, -0.04420, 0.9360 0.1037, -0.05710, 0.8315 0.1384, -0.06890, 0.6648 0.1741, -0.07950, 0.5408 0.2102, -0.08660, 0.4290 0.2472, -0.09640, 0.2450 0.2844, -0.10270, 0.1154 0.3225, -0.10690, -0.0698 0.3608, -0.10890, -0.2146 0.3991, -0.10830, -0.3519 0.4373, -0.10510, -0.4136 0.4757, -0.09890, -0.4284 0.5137, -0.09070, -0.4422 0.5514, -0.08120, -0.4152 0.5917, -0.06870, -1.4632 0.5917, -0.02380, -0.8778 0.5917, 0.02120, -0.7902 16 Flap element taps 1.0000, 0.00130, -0.7609 0.9365, 0.01390, -0.7877 0.8333, 0.03280, -0.7846 0.7436, 0.04930, -0.7594 0.7049, 0.05670, -0.8667 0.6667, 0.05450, -0.6308 0.6302, 0.03770, -1.0480 0.6083, 0.01980, -1.1907 0.6000, 0.00000, -2.1913 0.6076, -0.01900, -1.2655 0.6285, -0.03060, 0.9328 0.6667, -0.04090, -0.1186 0.7046, -0.04120, -0.7092 0.7429, -0.03210, -0.1988 0.8333, -0.01400, -0.1055 0.9311, -0.00120, -0.1572