S809 VENTED AILERON MODEL, 18 IN CHORD --------- Run Conditions: vel=105.6 ft/s Re=1.002x10^6 AOA=-5.98 Flap deflection=-10.00 Totals: Cl=-0.7084 Cdp=0.0699 Cm(c/4)=0.0872 Cs=0.0043 Ch=-0.0346 Main component: Cl=-0.4991 Cdp=0.1021 Cm=0.1062 Flap component: Cl=-0.2093 Cdp=-0.0323 Cm=0.1589 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.9937 0.5871, 0.07930, -0.2658 0.5501, 0.08690, -0.3611 0.5112, 0.09370, -0.3985 0.4731, 0.09830, -0.4171 0.4349, 0.10070, -0.3927 0.3960, 0.10120, -0.3702 0.3566, 0.10020, -0.2603 0.3172, 0.09790, -0.1978 0.2778, 0.09440, -0.1481 0.2393, 0.08960, -0.0970 0.2056, 0.08360, -0.0415 0.1633, 0.07610, 0.1016 0.1261, 0.06710, 0.2072 0.0900, 0.05640, 0.3792 0.0571, 0.04390, 0.5775 0.0283, 0.02940, 0.8381 0.0142, 0.01970, 0.9937 0.0081, 0.01410, 0.9771 0.0026, 0.00780, 0.6747 0.0000, 0.00000, -0.6422 0.0037, -0.00840, -1.6309 0.0112, -0.01420, -1.3540 0.0191, -0.01930, -1.1562 0.0397, -0.03030, -0.9266 0.0706, -0.04420, -0.8819 0.1037, -0.05710, -0.9244 0.1384, -0.06890, -0.9361 0.1741, -0.07950, -0.9900 0.2102, -0.08660, -1.0848 0.2472, -0.09640, -1.1512 0.2844, -0.10270, -1.1866 0.3225, -0.10690, -1.1618 0.3608, -0.10890, -1.1616 0.3991, -0.10830, -1.0716 0.4373, -0.10510, -0.9871 0.4757, -0.09890, -0.6483 0.5137, -0.09070, -0.4110 0.5514, -0.08120, -0.1520 0.5917, -0.06870, 0.0304 0.5917, -0.02380, -0.6049 0.5917, 0.02120, -0.9740 16 Flap element taps 1.0000, 0.00130, -0.1175 0.9365, 0.01390, 0.0824 0.8333, 0.03280, 0.2388 0.7436, 0.04930, 0.4760 0.7049, 0.05670, 0.8215 0.6667, 0.05450, 0.2688 0.6302, 0.03770, -1.2530 0.6083, 0.01980, -1.0999 0.6000, 0.00000, -1.4581 0.6076, -0.01900, -0.7006 0.6285, -0.03060, -0.5853 0.6667, -0.04090, -0.7567 0.7046, -0.04120, -0.7394 0.7429, -0.03210, -0.3718 0.8333, -0.01400, -0.2338 0.9311, -0.00120, -0.1619 --------- Run Conditions: vel=106.8 ft/s Re=1.009x10^6 AOA=-0.02 Flap deflection=-10.00 Totals: Cl=-0.4016 Cdp=0.0226 Cm(c/4)=0.0913 Cs=-0.0224 Ch=-0.0676 Main component: Cl=-0.2286 Cdp=0.0184 Cm=0.0631 Flap component: Cl=-0.1731 Cdp=0.0042 Cm=0.1286 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.2601 0.5871, 0.07930, -0.0854 0.5501, 0.08690, -0.4250 0.5112, 0.09370, -0.4304 0.4731, 0.09830, -0.4728 0.4349, 0.10070, -0.4960 0.3960, 0.10120, -0.5272 0.3566, 0.10020, -0.4364 0.3172, 0.09790, -0.4053 0.2778, 0.09440, -0.3862 0.2393, 0.08960, -0.3726 0.2056, 0.08360, -0.3673 0.1633, 0.07610, -0.2437 0.1261, 0.06710, -0.1880 0.0900, 0.05640, -0.0558 0.0571, 0.04390, 0.0914 0.0283, 0.02940, 0.3387 0.0142, 0.01970, 0.5977 0.0081, 0.01410, 0.7227 0.0026, 0.00780, 0.9585 0.0000, 0.00000, 0.9145 0.0037, -0.00840, 0.2409 0.0112, -0.01420, 0.0323 0.0191, -0.01930, -0.0300 0.0397, -0.03030, -0.1252 0.0706, -0.04420, -0.2799 0.1037, -0.05710, -0.4249 0.1384, -0.06890, -0.4975 0.1741, -0.07950, -0.6142 0.2102, -0.08660, -0.7774 0.2472, -0.09640, -0.8892 0.2844, -0.10270, -0.9872 0.3225, -0.10690, -1.0154 0.3608, -0.10890, -1.0880 0.3991, -0.10830, -1.0529 0.4373, -0.10510, -0.9850 0.4757, -0.09890, -0.9271 0.5137, -0.09070, -0.6229 0.5514, -0.08120, -0.2818 0.5917, -0.06870, 0.0050 0.5917, -0.02380, -0.0765 0.5917, 0.02120, -0.0844 16 Flap element taps 1.0000, 0.00130, 0.1366 0.9365, 0.01390, 0.1696 0.8333, 0.03280, 0.2573 0.7436, 0.04930, 0.4802 0.7049, 0.05670, 0.5878 0.6667, 0.05450, -0.1833 0.6302, 0.03770, -0.1745 0.6083, 0.01980, -0.0791 0.6000, 0.00000, -0.1372 0.6076, -0.01900, -0.1299 0.6285, -0.03060, -0.3020 0.6667, -0.04090, -0.8151 0.7046, -0.04120, -0.9499 0.7429, -0.03210, -0.3146 0.8333, -0.01400, -0.0204 0.9311, -0.00120, 0.0938 Wake drag found for this condition, Cdw=0.0169 --------- Run Conditions: vel=107.5 ft/s Re=1.012x10^6 AOA=3.03 Flap deflection=-10.00 Totals: Cl=-0.1175 Cdp=0.0154 Cm(c/4)=0.0842 Cs=-0.0216 Ch=-0.0592 Main component: Cl=0.0205 Cdp=0.0157 Cm=0.0117 Flap component: Cl=-0.1380 Cdp=-0.0003 Cm=0.1016 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.0979 0.5871, 0.07930, -0.0893 0.5501, 0.08690, -0.5095 0.5112, 0.09370, -0.5098 0.4731, 0.09830, -0.5513 0.4349, 0.10070, -0.5978 0.3960, 0.10120, -0.6571 0.3566, 0.10020, -0.5816 0.3172, 0.09790, -0.5711 0.2778, 0.09440, -0.5757 0.2393, 0.08960, -0.5840 0.2056, 0.08360, -0.6086 0.1633, 0.07610, -0.5116 0.1261, 0.06710, -0.4914 0.0900, 0.05640, -0.4069 0.0571, 0.04390, -0.3245 0.0283, 0.02940, -0.1603 0.0142, 0.01970, 0.0574 0.0081, 0.01410, 0.1793 0.0026, 0.00780, 0.5120 0.0000, 0.00000, 0.9707 0.0037, -0.00840, 0.8706 0.0112, -0.01420, 0.6245 0.0191, -0.01930, 0.4967 0.0397, -0.03030, 0.3032 0.0706, -0.04420, 0.0830 0.1037, -0.05710, -0.0958 0.1384, -0.06890, -0.1913 0.1741, -0.07950, -0.3292 0.2102, -0.08660, -0.5169 0.2472, -0.09640, -0.6403 0.2844, -0.10270, -0.7622 0.3225, -0.10690, -0.8056 0.3608, -0.10890, -0.9019 0.3991, -0.10830, -0.8947 0.4373, -0.10510, -0.8515 0.4757, -0.09890, -0.7656 0.5137, -0.09070, -0.7340 0.5514, -0.08120, -0.2365 0.5917, -0.06870, -0.0384 0.5917, -0.02380, -0.0545 0.5917, 0.02120, -0.0353 16 Flap element taps 1.0000, 0.00130, 0.1856 0.9365, 0.01390, 0.1822 0.8333, 0.03280, 0.2485 0.7436, 0.04930, 0.3869 0.7049, 0.05670, 0.1589 0.6667, 0.05450, -0.1110 0.6302, 0.03770, -0.0584 0.6083, 0.01980, -0.0398 0.6000, 0.00000, -0.0573 0.6076, -0.01900, -0.0603 0.6285, -0.03060, -0.1039 0.6667, -0.04090, -0.7674 0.7046, -0.04120, -1.0121 0.7429, -0.03210, -0.2981 0.8333, -0.01400, 0.0339 0.9311, -0.00120, 0.1662 Wake drag found for this condition, Cdw=0.0139 --------- Run Conditions: vel=107.8 ft/s Re=1.015x10^6 AOA=6.03 Flap deflection=-10.00 Totals: Cl=0.1894 Cdp=0.0107 Cm(c/4)=0.0728 Cs=0.0093 Ch=-0.0465 Main component: Cl=0.2838 Cdp=0.0153 Cm=-0.0432 Flap component: Cl=-0.0944 Cdp=-0.0047 Cm=0.0686 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.0401 0.5871, 0.07930, -0.1545 0.5501, 0.08690, -0.2417 0.5112, 0.09370, -0.6426 0.4731, 0.09830, -0.6772 0.4349, 0.10070, -0.7227 0.3960, 0.10120, -0.8011 0.3566, 0.10020, -0.7468 0.3172, 0.09790, -0.7545 0.2778, 0.09440, -0.7783 0.2393, 0.08960, -0.8146 0.2056, 0.08360, -0.8709 0.1633, 0.07610, -0.8087 0.1261, 0.06710, -0.8347 0.0900, 0.05640, -0.8128 0.0571, 0.04390, -0.8267 0.0283, 0.02940, -0.8095 0.0142, 0.01970, -0.7291 0.0081, 0.01410, -0.7042 0.0026, 0.00780, -0.3604 0.0000, 0.00000, 0.2314 0.0037, -0.00840, 1.0152 0.0112, -0.01420, 0.9491 0.0191, -0.01930, 0.8440 0.0397, -0.03030, 0.6383 0.0706, -0.04420, 0.3957 0.1037, -0.05710, 0.2047 0.1384, -0.06890, 0.0922 0.1741, -0.07950, -0.0589 0.2102, -0.08660, -0.2592 0.2472, -0.09640, -0.3913 0.2844, -0.10270, -0.5278 0.3225, -0.10690, -0.5864 0.3608, -0.10890, -0.7010 0.3991, -0.10830, -0.7188 0.4373, -0.10510, -0.7041 0.4757, -0.09890, -0.6118 0.5137, -0.09070, -0.5688 0.5514, -0.08120, -0.1981 0.5917, -0.06870, -0.0357 0.5917, -0.02380, -0.0482 0.5917, 0.02120, -0.0482 16 Flap element taps 1.0000, 0.00130, 0.1955 0.9365, 0.01390, 0.1784 0.8333, 0.03280, 0.2195 0.7436, 0.04930, 0.1629 0.7049, 0.05670, -0.0540 0.6667, 0.05450, -0.0492 0.6302, 0.03770, -0.0443 0.6083, 0.01980, -0.0328 0.6000, 0.00000, -0.0417 0.6076, -0.01900, -0.0893 0.6285, -0.03060, 0.1311 0.6667, -0.04090, -0.6936 0.7046, -0.04120, -0.9988 0.7429, -0.03210, -0.2518 0.8333, -0.01400, 0.0765 0.9311, -0.00120, 0.2070 Wake drag found for this condition, Cdw=0.0129 --------- Run Conditions: vel=107.9 ft/s Re=1.014x10^6 AOA=8.99 Flap deflection=-10.00 Totals: Cl=0.3814 Cdp=0.0229 Cm(c/4)=0.0593 Cs=0.0370 Ch=-0.0197 Main component: Cl=0.4011 Cdp=0.0404 Cm=-0.0504 Flap component: Cl=-0.0197 Cdp=-0.0176 Cm=0.0146 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.0354 0.5871, 0.07930, -0.0743 0.5501, 0.08690, -0.2149 0.5112, 0.09370, -0.4449 0.4731, 0.09830, -0.6232 0.4349, 0.10070, -0.7073 0.3960, 0.10120, -0.7968 0.3566, 0.10020, -0.7697 0.3172, 0.09790, -0.8087 0.2778, 0.09440, -0.8806 0.2393, 0.08960, -0.9529 0.2056, 0.08360, -1.0368 0.1633, 0.07610, -1.0164 0.1261, 0.06710, -1.0880 0.0900, 0.05640, -1.1325 0.0571, 0.04390, -1.2455 0.0283, 0.02940, -1.3942 0.0142, 0.01970, -1.4846 0.0081, 0.01410, -1.6077 0.0026, 0.00780, -1.3574 0.0000, 0.00000, -0.9702 0.0037, -0.00840, 0.8399 0.0112, -0.01420, 1.0131 0.0191, -0.01930, 0.9851 0.0397, -0.03030, 0.8267 0.0706, -0.04420, 0.5953 0.1037, -0.05710, 0.4032 0.1384, -0.06890, 0.2826 0.1741, -0.07950, 0.1259 0.2102, -0.08660, -0.0787 0.2472, -0.09640, -0.2214 0.2844, -0.10270, -0.3709 0.3225, -0.10690, -0.4500 0.3608, -0.10890, -0.5806 0.3991, -0.10830, -0.6264 0.4373, -0.10510, -0.6486 0.4757, -0.09890, -0.5753 0.5137, -0.09070, -0.5121 0.5514, -0.08120, -0.5034 0.5917, -0.06870, -0.7473 0.5917, -0.02380, -0.2660 0.5917, 0.02120, -0.0338 16 Flap element taps 1.0000, 0.00130, 0.1203 0.9365, 0.01390, 0.0842 0.8333, 0.03280, 0.0464 0.7436, 0.04930, 0.0168 0.7049, 0.05670, 0.0002 0.6667, 0.05450, -0.0102 0.6302, 0.03770, -0.0694 0.6083, 0.01980, -0.2950 0.6000, 0.00000, -1.2221 0.6076, -0.01900, 0.8896 0.6285, -0.03060, 0.2974 0.6667, -0.04090, -0.6004 0.7046, -0.04120, -0.8319 0.7429, -0.03210, -0.1230 0.8333, -0.01400, 0.0993 0.9311, -0.00120, 0.2061 Wake drag found for this condition, Cdw=0.0204 --------- Run Conditions: vel=108.1 ft/s Re=1.011x10^6 AOA=12.02 Flap deflection=-10.00 Totals: Cl=0.5882 Cdp=0.0386 Cm(c/4)=0.0529 Cs=0.0847 Ch=-0.0147 Main component: Cl=0.5746 Cdp=0.0460 Cm=-0.0810 Flap component: Cl=0.0136 Cdp=-0.0074 Cm=-0.0120 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1520 0.5871, 0.07930, -0.1602 0.5501, 0.08690, -0.1903 0.5112, 0.09370, -0.3064 0.4731, 0.09830, -0.5040 0.4349, 0.10070, -0.6507 0.3960, 0.10120, -0.7836 0.3566, 0.10020, -0.8181 0.3172, 0.09790, -0.8809 0.2778, 0.09440, -0.9619 0.2393, 0.08960, -1.0653 0.2056, 0.08360, -1.1824 0.1633, 0.07610, -1.2212 0.1261, 0.06710, -1.3371 0.0900, 0.05640, -1.4660 0.0571, 0.04390, -1.6808 0.0283, 0.02940, -2.1097 0.0142, 0.01970, -2.4542 0.0081, 0.01410, -2.8495 0.0026, 0.00780, -2.7773 0.0000, 0.00000, -2.8467 0.0037, -0.00840, 0.3354 0.0112, -0.01420, 0.9220 0.0191, -0.01930, 1.0095 0.0397, -0.03030, 0.9555 0.0706, -0.04420, 0.7702 0.1037, -0.05710, 0.5936 0.1384, -0.06890, 0.4647 0.1741, -0.07950, 0.3102 0.2102, -0.08660, 0.1158 0.2472, -0.09640, -0.0329 0.2844, -0.10270, -0.1843 0.3225, -0.10690, -0.2840 0.3608, -0.10890, -0.4164 0.3991, -0.10830, -0.4837 0.4373, -0.10510, -0.5226 0.4757, -0.09890, -0.4666 0.5137, -0.09070, -0.4116 0.5514, -0.08120, -0.3736 0.5917, -0.06870, -0.6476 0.5917, -0.02380, -0.2196 0.5917, 0.02120, -0.1674 16 Flap element taps 1.0000, 0.00130, -0.0147 0.9365, 0.01390, -0.0596 0.8333, 0.03280, -0.0588 0.7436, 0.04930, -0.0758 0.7049, 0.05670, -0.0907 0.6667, 0.05450, -0.1040 0.6302, 0.03770, -0.2070 0.6083, 0.01980, -0.3271 0.6000, 0.00000, -0.9076 0.6076, -0.01900, 0.8918 0.6285, -0.03060, 0.3087 0.6667, -0.04090, -0.5710 0.7046, -0.04120, -0.8277 0.7429, -0.03210, -0.1429 0.8333, -0.01400, 0.0744 0.9311, -0.00120, 0.1541 --------- Run Conditions: vel=107.8 ft/s Re=1.007x10^6 AOA=15.02 Flap deflection=-10.00 Totals: Cl=0.7528 Cdp=0.0584 Cm(c/4)=0.0465 Cs=0.1387 Ch=-0.0035 Main component: Cl=0.7073 Cdp=0.0604 Cm=-0.1033 Flap component: Cl=0.0455 Cdp=-0.0021 Cm=-0.0357 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.2765 0.5871, 0.07930, -0.2893 0.5501, 0.08690, -0.2821 0.5112, 0.09370, -0.2921 0.4731, 0.09830, -0.3639 0.4349, 0.10070, -0.4991 0.3960, 0.10120, -0.6703 0.3566, 0.10020, -0.7687 0.3172, 0.09790, -0.8746 0.2778, 0.09440, -0.9942 0.2393, 0.08960, -1.1300 0.2056, 0.08360, -1.2764 0.1633, 0.07610, -1.3764 0.1261, 0.06710, -1.5458 0.0900, 0.05640, -1.7605 0.0571, 0.04390, -2.1143 0.0283, 0.02940, -2.6737 0.0142, 0.01970, -3.2628 0.0081, 0.01410, -4.3166 0.0026, 0.00780, -4.3700 0.0000, 0.00000, -4.9744 0.0037, -0.00840, -0.3747 0.0112, -0.01420, 0.6941 0.0191, -0.01930, 0.9378 0.0397, -0.03030, 1.0078 0.0706, -0.04420, 0.8867 0.1037, -0.05710, 0.7380 0.1384, -0.06890, 0.6070 0.1741, -0.07950, 0.4604 0.2102, -0.08660, 0.2786 0.2472, -0.09640, 0.1244 0.2844, -0.10270, -0.0271 0.3225, -0.10690, -0.1430 0.3608, -0.10890, -0.2777 0.3991, -0.10830, -0.3623 0.4373, -0.10510, -0.4150 0.4757, -0.09890, -0.3781 0.5137, -0.09070, -0.3393 0.5514, -0.08120, -0.2821 0.5917, -0.06870, -0.6520 0.5917, -0.02380, -0.2682 0.5917, 0.02120, -0.2868 16 Flap element taps 1.0000, 0.00130, -0.1230 0.9365, 0.01390, -0.1568 0.8333, 0.03280, -0.1472 0.7436, 0.04930, -0.1670 0.7049, 0.05670, -0.1945 0.6667, 0.05450, -0.2108 0.6302, 0.03770, -0.3717 0.6083, 0.01980, -0.4150 0.6000, 0.00000, -0.8731 0.6076, -0.01900, 0.9101 0.6285, -0.03060, 0.3262 0.6667, -0.04090, -0.5421 0.7046, -0.04120, -0.8175 0.7429, -0.03210, -0.1512 0.8333, -0.01400, 0.0507 0.9311, -0.00120, 0.1061 --------- Run Conditions: vel=106.9 ft/s Re=0.997x10^6 AOA=17.99 Flap deflection=-10.00 Totals: Cl=0.7774 Cdp=0.1095 Cm(c/4)=0.0242 Cs=0.1360 Ch=0.0134 Main component: Cl=0.6814 Cdp=0.1040 Cm=-0.0961 Flap component: Cl=0.0960 Cdp=0.0055 Cm=-0.0730 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.4500 0.5871, 0.07930, -0.4479 0.5501, 0.08690, -0.4482 0.5112, 0.09370, -0.4412 0.4731, 0.09830, -0.4393 0.4349, 0.10070, -0.4394 0.3960, 0.10120, -0.4670 0.3566, 0.10020, -0.4934 0.3172, 0.09790, -0.5753 0.2778, 0.09440, -0.7099 0.2393, 0.08960, -0.8891 0.2056, 0.08360, -1.0809 0.1633, 0.07610, -1.2500 0.1261, 0.06710, -1.4717 0.0900, 0.05640, -1.7508 0.0571, 0.04390, -2.1874 0.0283, 0.02940, -2.8884 0.0142, 0.01970, -3.5393 0.0081, 0.01410, -5.1375 0.0026, 0.00780, -5.2416 0.0000, 0.00000, -6.1807 0.0037, -0.00840, -0.8509 0.0112, -0.01420, 0.5118 0.0191, -0.01930, 0.8580 0.0397, -0.03030, 1.0139 0.0706, -0.04420, 0.9390 0.1037, -0.05710, 0.8098 0.1384, -0.06890, 0.6764 0.1741, -0.07950, 0.5352 0.2102, -0.08660, 0.3626 0.2472, -0.09640, 0.2008 0.2844, -0.10270, 0.0482 0.3225, -0.10690, -0.0821 0.3608, -0.10890, -0.2214 0.3991, -0.10830, -0.3252 0.4373, -0.10510, -0.3899 0.4757, -0.09890, -0.3679 0.5137, -0.09070, -0.3512 0.5514, -0.08120, -0.2886 0.5917, -0.06870, -0.9062 0.5917, -0.02380, -0.4399 0.5917, 0.02120, -0.4852 16 Flap element taps 1.0000, 0.00130, -0.2934 0.9365, 0.01390, -0.3201 0.8333, 0.03280, -0.3279 0.7436, 0.04930, -0.3789 0.7049, 0.05670, -0.4284 0.6667, 0.05450, -0.3862 0.6302, 0.03770, -0.6303 0.6083, 0.01980, -0.6391 0.6000, 0.00000, -1.1006 0.6076, -0.01900, 0.9056 0.6285, -0.03060, 0.3413 0.6667, -0.04090, -0.5634 0.7046, -0.04120, -0.8831 0.7429, -0.03210, -0.2065 0.8333, -0.01400, -0.0154 0.9311, -0.00120, 0.0176 --------- Run Conditions: vel=107.8 ft/s Re=1.004x10^6 AOA=19.99 Flap deflection=-10.00 Totals: Cl=0.3564 Cdp=0.2475 Cm(c/4)=-0.0157 Cs=-0.1108 Ch=0.0116 Main component: Cl=0.2606 Cdp=0.2378 Cm=-0.0470 Flap component: Cl=0.0958 Cdp=0.0097 Cm=-0.0735 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.6733 0.5871, 0.07930, -0.5908 0.5501, 0.08690, -0.5809 0.5112, 0.09370, -0.5867 0.4731, 0.09830, -0.6095 0.4349, 0.10070, -0.6152 0.3960, 0.10120, -0.6259 0.3566, 0.10020, -0.6170 0.3172, 0.09790, -0.6164 0.2778, 0.09440, -0.6185 0.2393, 0.08960, -0.6221 0.2056, 0.08360, -0.6227 0.1633, 0.07610, -0.6055 0.1261, 0.06710, -0.6152 0.0900, 0.05640, -0.6073 0.0571, 0.04390, -0.6185 0.0283, 0.02940, -0.6482 0.0142, 0.01970, -0.6387 0.0081, 0.01410, -0.6509 0.0026, 0.00780, -0.5981 0.0000, 0.00000, -0.8971 0.0037, -0.00840, 0.6378 0.0112, -0.01420, 0.9691 0.0191, -0.01930, 1.0115 0.0397, -0.03030, 0.9528 0.0706, -0.04420, 0.8000 0.1037, -0.05710, 0.6414 0.1384, -0.06890, 0.4925 0.1741, -0.07950, 0.3410 0.2102, -0.08660, 0.1698 0.2472, -0.09640, -0.0076 0.2844, -0.10270, -0.1640 0.3225, -0.10690, -0.3074 0.3608, -0.10890, -0.4523 0.3991, -0.10830, -0.5630 0.4373, -0.10510, -0.6210 0.4757, -0.09890, -0.5888 0.5137, -0.09070, -0.5629 0.5514, -0.08120, -0.4907 0.5917, -0.06870, -1.1430 0.5917, -0.02380, -0.6013 0.5917, 0.02120, -0.6922 16 Flap element taps 1.0000, 0.00130, -0.4817 0.9365, 0.01390, -0.5162 0.8333, 0.03280, -0.5011 0.7436, 0.04930, -0.5561 0.7049, 0.05670, -0.6287 0.6667, 0.05450, -0.5447 0.6302, 0.03770, -0.8544 0.6083, 0.01980, -0.8525 0.6000, 0.00000, -1.3694 0.6076, -0.01900, 0.8926 0.6285, -0.03060, 0.2300 0.6667, -0.04090, -0.8116 0.7046, -0.04120, -1.1930 0.7429, -0.03210, -0.4122 0.8333, -0.01400, -0.1830 0.9311, -0.00120, -0.1442 --------- Run Conditions: vel=108.4 ft/s Re=1.007x10^6 AOA=23.99 Flap deflection=-10.00 Totals: Cl=0.4745 Cdp=0.3396 Cm(c/4)=-0.0482 Cs=-0.1173 Ch=0.0150 Main component: Cl=0.3333 Cdp=0.3053 Cm=-0.0781 Flap component: Cl=0.1412 Cdp=0.0343 Cm=-0.1130 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.7183 0.5871, 0.07930, -0.6985 0.5501, 0.08690, -0.7002 0.5112, 0.09370, -0.6995 0.4731, 0.09830, -0.7125 0.4349, 0.10070, -0.7079 0.3960, 0.10120, -0.7179 0.3566, 0.10020, -0.7085 0.3172, 0.09790, -0.7070 0.2778, 0.09440, -0.7070 0.2393, 0.08960, -0.7104 0.2056, 0.08360, -0.7091 0.1633, 0.07610, -0.6975 0.1261, 0.06710, -0.7014 0.0900, 0.05640, -0.6957 0.0571, 0.04390, -0.7033 0.0283, 0.02940, -0.7237 0.0142, 0.01970, -0.7228 0.0081, 0.01410, -0.7285 0.0026, 0.00780, -0.6771 0.0000, 0.00000, -0.9621 0.0037, -0.00840, 0.4437 0.0112, -0.01420, 0.8941 0.0191, -0.01930, 0.9936 0.0397, -0.03030, 0.9946 0.0706, -0.04420, 0.8798 0.1037, -0.05710, 0.7427 0.1384, -0.06890, 0.6045 0.1741, -0.07950, 0.4625 0.2102, -0.08660, 0.2946 0.2472, -0.09640, 0.1203 0.2844, -0.10270, -0.0391 0.3225, -0.10690, -0.1870 0.3608, -0.10890, -0.3418 0.3991, -0.10830, -0.4644 0.4373, -0.10510, -0.5383 0.4757, -0.09890, -0.5244 0.5137, -0.09070, -0.5165 0.5514, -0.08120, -0.4521 0.5917, -0.06870, -1.2533 0.5917, -0.02380, -0.6552 0.5917, 0.02120, -0.7627 16 Flap element taps 1.0000, 0.00130, -0.6771 0.9365, 0.01390, -0.7036 0.8333, 0.03280, -0.7290 0.7436, 0.04930, -0.7230 0.7049, 0.05670, -0.7158 0.6667, 0.05450, -0.6311 0.6302, 0.03770, -0.9659 0.6083, 0.01980, -0.9612 0.6000, 0.00000, -1.4485 0.6076, -0.01900, 0.8901 0.6285, -0.03060, 0.2560 0.6667, -0.04090, -0.7933 0.7046, -0.04120, -1.2042 0.7429, -0.03210, -0.4331 0.8333, -0.01400, -0.2239 0.9311, -0.00120, -0.2135 --------- Run Conditions: vel=107.4 ft/s Re=0.994x10^6 AOA=26.88 Flap deflection=-10.00 Totals: Cl=0.5271 Cdp=0.4042 Cm(c/4)=-0.0614 Cs=-0.1222 Ch=0.0199 Main component: Cl=0.3698 Cdp=0.3580 Cm=-0.0977 Flap component: Cl=0.1574 Cdp=0.0462 Cm=-0.1270 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.7575 0.5871, 0.07930, -0.7436 0.5501, 0.08690, -0.7453 0.5112, 0.09370, -0.7414 0.4731, 0.09830, -0.7511 0.4349, 0.10070, -0.7464 0.3960, 0.10120, -0.7602 0.3566, 0.10020, -0.7482 0.3172, 0.09790, -0.7465 0.2778, 0.09440, -0.7480 0.2393, 0.08960, -0.7500 0.2056, 0.08360, -0.7509 0.1633, 0.07610, -0.7353 0.1261, 0.06710, -0.7443 0.0900, 0.05640, -0.7368 0.0571, 0.04390, -0.7438 0.0283, 0.02940, -0.7582 0.0142, 0.01970, -0.7568 0.0081, 0.01410, -0.7660 0.0026, 0.00780, -0.7120 0.0000, 0.00000, -0.8785 0.0037, -0.00840, 0.2866 0.0112, -0.01420, 0.8177 0.0191, -0.01930, 0.9615 0.0397, -0.03030, 1.0097 0.0706, -0.04420, 0.9279 0.1037, -0.05710, 0.8125 0.1384, -0.06890, 0.6881 0.1741, -0.07950, 0.5545 0.2102, -0.08660, 0.3903 0.2472, -0.09640, 0.2230 0.2844, -0.10270, 0.0624 0.3225, -0.10690, -0.0818 0.3608, -0.10890, -0.2421 0.3991, -0.10830, -0.3705 0.4373, -0.10510, -0.4555 0.4757, -0.09890, -0.4547 0.5137, -0.09070, -0.4640 0.5514, -0.08120, -0.4109 0.5917, -0.06870, -1.3272 0.5917, -0.02380, -0.7255 0.5917, 0.02120, -0.8061 16 Flap element taps 1.0000, 0.00130, -0.7472 0.9365, 0.01390, -0.7747 0.8333, 0.03280, -0.7728 0.7436, 0.04930, -0.7554 0.7049, 0.05670, -0.7474 0.6667, 0.05450, -0.6708 0.6302, 0.03770, -1.0195 0.6083, 0.01980, -1.0198 0.6000, 0.00000, -1.5334 0.6076, -0.01900, 0.8823 0.6285, -0.03060, 0.2891 0.6667, -0.04090, -0.7513 0.7046, -0.04120, -1.1750 0.7429, -0.03210, -0.4245 0.8333, -0.01400, -0.2318 0.9311, -0.00120, -0.2366