S809 VENTED AILERON MODEL, 18 IN CHORD --------- Run Conditions: vel=116.2 ft/s Re=1.003x10^6 AOA=-6.02 Flap deflection=-45.00 Totals: Cl=-0.6420 Cdp=0.2419 Cm(c/4)=0.1475 Cs=-0.1732 Ch=-0.0167 Main component: Cl=-0.3391 Cdp=-0.0322 Cm=0.0480 Flap component: Cl=-0.3028 Cdp=0.2741 Cm=0.2655 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.1414 0.5871, 0.07930, 0.2232 0.5501, 0.08690, -0.0737 0.5112, 0.09370, -0.0752 0.4731, 0.09830, -0.1212 0.4349, 0.10070, -0.1483 0.3960, 0.10120, -0.0879 0.3566, 0.10020, -0.0931 0.3172, 0.09790, -0.0625 0.2778, 0.09440, -0.0375 0.2393, 0.08960, 0.0069 0.2056, 0.08360, 0.1016 0.1633, 0.07610, 0.1414 0.1261, 0.06710, 0.2684 0.0900, 0.05640, 0.3892 0.0571, 0.04390, 0.5867 0.0283, 0.02940, 0.8335 0.0142, 0.01970, 0.9846 0.0081, 0.01410, 1.0306 0.0026, 0.00780, 0.7395 0.0000, 0.00000, -0.4200 0.0037, -0.00840, -1.3239 0.0112, -0.01420, -1.0818 0.0191, -0.01930, -0.9149 0.0397, -0.03030, -0.7213 0.0706, -0.04420, -0.6614 0.1037, -0.05710, -0.6719 0.1384, -0.06890, -0.7268 0.1741, -0.07950, -0.7429 0.2102, -0.08660, -0.7286 0.2472, -0.09640, -0.7691 0.2844, -0.10270, -0.7258 0.3225, -0.10690, -0.6937 0.3608, -0.10890, -0.6045 0.3991, -0.10830, -0.4042 0.4373, -0.10510, -0.1326 0.4757, -0.09890, 0.1326 0.5137, -0.09070, 0.2670 0.5514, -0.08120, 0.2650 0.5917, -0.06870, 0.2053 0.5917, -0.02380, 0.1214 0.5917, 0.02120, 0.1401 16 Flap element taps 1.0000, 0.00130, -0.5952 0.9365, 0.01390, 0.3638 0.8333, 0.03280, 0.8738 0.7436, 0.04930, 0.7189 0.7049, 0.05670, -0.0006 0.6667, 0.05450, -0.1437 0.6302, 0.03770, 0.1446 0.6083, 0.01980, -0.1048 0.6000, 0.00000, -1.5460 0.6076, -0.01900, -1.3312 0.6285, -0.03060, -0.8112 0.6667, -0.04090, -0.6734 0.7046, -0.04120, -0.6610 0.7429, -0.03210, -0.6341 0.8333, -0.01400, -0.6303 0.9311, -0.00120, -0.6073 --------- Run Conditions: vel=115.9 ft/s Re=1.001x10^6 AOA=0.01 Flap deflection=-45.00 Totals: Cl=-0.5047 Cdp=0.2621 Cm(c/4)=0.1603 Cs=-0.2622 Ch=-0.0858 Main component: Cl=-0.1880 Cdp=-0.0768 Cm=0.0418 Flap component: Cl=-0.3168 Cdp=0.3389 Cm=0.2448 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.4593 0.5871, 0.07930, 0.3507 0.5501, 0.08690, 0.1886 0.5112, 0.09370, -0.1008 0.4731, 0.09830, -0.1212 0.4349, 0.10070, -0.1634 0.3960, 0.10120, -0.1414 0.3566, 0.10020, -0.1943 0.3172, 0.09790, -0.2001 0.2778, 0.09440, -0.2126 0.2393, 0.08960, -0.1984 0.2056, 0.08360, -0.1311 0.1633, 0.07610, -0.1388 0.1261, 0.06710, -0.0439 0.0900, 0.05640, 0.0291 0.0571, 0.04390, 0.1881 0.0283, 0.02940, 0.4264 0.0142, 0.01970, 0.6621 0.0081, 0.01410, 0.8464 0.0026, 0.00780, 0.9638 0.0000, 0.00000, 0.8448 0.0037, -0.00840, 0.1799 0.0112, -0.01420, 0.0186 0.0191, -0.01930, -0.0317 0.0397, -0.03030, -0.1098 0.0706, -0.04420, -0.2171 0.1037, -0.05710, -0.3192 0.1384, -0.06890, -0.4578 0.1741, -0.07950, -0.5365 0.2102, -0.08660, -0.5739 0.2472, -0.09640, -0.6821 0.2844, -0.10270, -0.6951 0.3225, -0.10690, -0.7336 0.3608, -0.10890, -0.6717 0.3991, -0.10830, -0.6241 0.4373, -0.10510, -0.5839 0.4757, -0.09890, -0.0826 0.5137, -0.09070, 0.0973 0.5514, -0.08120, 0.3068 0.5917, -0.06870, 0.4396 0.5917, -0.02380, 0.4443 0.5917, 0.02120, 0.4457 16 Flap element taps 1.0000, 0.00130, -0.8305 0.9365, 0.01390, 0.1219 0.8333, 0.03280, 0.4857 0.7436, 0.04930, 0.5041 0.7049, 0.05670, 0.2549 0.6667, 0.05450, 0.3582 0.6302, 0.03770, 0.8914 0.6083, 0.01980, 0.8504 0.6000, 0.00000, -0.8360 0.6076, -0.01900, -0.8758 0.6285, -0.03060, -0.8661 0.6667, -0.04090, -0.8465 0.7046, -0.04120, -0.8706 0.7429, -0.03210, -0.8608 0.8333, -0.01400, -0.8698 0.9311, -0.00120, -0.8345 --------- Run Conditions: vel=116.5 ft/s Re=1.004x10^6 AOA=3.05 Flap deflection=-45.00 Totals: Cl=-0.3315 Cdp=0.2614 Cm(c/4)=0.1736 Cs=-0.2787 Ch=-0.0877 Main component: Cl=0.0060 Cdp=-0.0684 Cm=0.0061 Flap component: Cl=-0.3375 Cdp=0.3299 Cm=0.2467 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.4539 0.5871, 0.07930, 0.3269 0.5501, 0.08690, 0.2039 0.5112, 0.09370, -0.2095 0.4731, 0.09830, -0.2250 0.4349, 0.10070, -0.2603 0.3960, 0.10120, -0.2363 0.3566, 0.10020, -0.3058 0.3172, 0.09790, -0.3284 0.2778, 0.09440, -0.3604 0.2393, 0.08960, -0.3660 0.2056, 0.08360, -0.3157 0.1633, 0.07610, -0.3560 0.1261, 0.06710, -0.2874 0.0900, 0.05640, -0.2584 0.0571, 0.04390, -0.1502 0.0283, 0.02940, 0.0243 0.0142, 0.01970, 0.2320 0.0081, 0.01410, 0.4334 0.0026, 0.00780, 0.6479 0.0000, 0.00000, 0.9775 0.0037, -0.00840, 0.7790 0.0112, -0.01420, 0.5562 0.0191, -0.01930, 0.4372 0.0397, -0.03030, 0.2623 0.0706, -0.04420, 0.0933 0.1037, -0.05710, -0.0415 0.1384, -0.06890, -0.2136 0.1741, -0.07950, -0.3145 0.2102, -0.08660, -0.3661 0.2472, -0.09640, -0.4976 0.2844, -0.10270, -0.5311 0.3225, -0.10690, -0.5992 0.3608, -0.10890, -0.5661 0.3991, -0.10830, -0.5247 0.4373, -0.10510, -0.4618 0.4757, -0.09890, -0.2436 0.5137, -0.09070, 0.1102 0.5514, -0.08120, 0.2957 0.5917, -0.06870, 0.4305 0.5917, -0.02380, 0.4365 0.5917, 0.02120, 0.4375 16 Flap element taps 1.0000, 0.00130, -0.9017 0.9365, 0.01390, 0.0779 0.8333, 0.03280, 0.4708 0.7436, 0.04930, 0.5074 0.7049, 0.05670, 0.2277 0.6667, 0.05450, 0.3537 0.6302, 0.03770, 0.9375 0.6083, 0.01980, 0.8458 0.6000, 0.00000, -0.8104 0.6076, -0.01900, -0.8660 0.6285, -0.03060, -0.8873 0.6667, -0.04090, -0.8738 0.7046, -0.04120, -0.8924 0.7429, -0.03210, -0.8961 0.8333, -0.01400, -0.9040 0.9311, -0.00120, -0.8903 --------- Run Conditions: vel=116.7 ft/s Re=1.007x10^6 AOA=6.03 Flap deflection=-45.00 Totals: Cl=-0.1391 Cdp=0.2410 Cm(c/4)=0.1782 Cs=-0.2543 Ch=-0.0861 Main component: Cl=0.1985 Cdp=-0.0600 Cm=-0.0281 Flap component: Cl=-0.3376 Cdp=0.3010 Cm=0.2345 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.4305 0.5871, 0.07930, 0.3095 0.5501, 0.08690, 0.1518 0.5112, 0.09370, -0.0626 0.4731, 0.09830, -0.3018 0.4349, 0.10070, -0.3729 0.3960, 0.10120, -0.3420 0.3566, 0.10020, -0.4247 0.3172, 0.09790, -0.4645 0.2778, 0.09440, -0.5168 0.2393, 0.08960, -0.5439 0.2056, 0.08360, -0.5138 0.1633, 0.07610, -0.5906 0.1261, 0.06710, -0.5553 0.0900, 0.05640, -0.5814 0.0571, 0.04390, -0.5479 0.0283, 0.02940, -0.4851 0.0142, 0.01970, -0.3723 0.0081, 0.01410, -0.2261 0.0026, 0.00780, -0.0280 0.0000, 0.00000, 0.5409 0.0037, -0.00840, 0.9930 0.0112, -0.01420, 0.8833 0.0191, -0.01930, 0.7666 0.0397, -0.03030, 0.5584 0.0706, -0.04420, 0.3615 0.1037, -0.05710, 0.2099 0.1384, -0.06890, 0.0125 0.1741, -0.07950, -0.1032 0.2102, -0.08660, -0.1630 0.2472, -0.09640, -0.3137 0.2844, -0.10270, -0.3626 0.3225, -0.10690, -0.4545 0.3608, -0.10890, -0.4456 0.3991, -0.10830, -0.4293 0.4373, -0.10510, -0.3403 0.4757, -0.09890, -0.3332 0.5137, -0.09070, 0.1284 0.5514, -0.08120, 0.2989 0.5917, -0.06870, 0.4084 0.5917, -0.02380, 0.4153 0.5917, 0.02120, 0.4169 16 Flap element taps 1.0000, 0.00130, -0.8730 0.9365, 0.01390, 0.0661 0.8333, 0.03280, 0.4560 0.7436, 0.04930, 0.4926 0.7049, 0.05670, 0.1961 0.6667, 0.05450, 0.3451 0.6302, 0.03770, 0.9410 0.6083, 0.01980, 0.8666 0.6000, 0.00000, -0.7305 0.6076, -0.01900, -0.8247 0.6285, -0.03060, -0.8471 0.6667, -0.04090, -0.8324 0.7046, -0.04120, -0.8507 0.7429, -0.03210, -0.8508 0.8333, -0.01400, -0.8620 0.9311, -0.00120, -0.8497 --------- Run Conditions: vel=115.9 ft/s Re=1.001x10^6 AOA=9.02 Flap deflection=-45.00 Totals: Cl=0.0245 Cdp=0.2251 Cm(c/4)=0.1676 Cs=-0.2185 Ch=-0.0753 Main component: Cl=0.3181 Cdp=-0.0262 Cm=-0.0399 Flap component: Cl=-0.2935 Cdp=0.2514 Cm=0.1927 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.1701 0.5871, 0.07930, 0.1491 0.5501, 0.08690, 0.1540 0.5112, 0.09370, 0.0477 0.4731, 0.09830, -0.1331 0.4349, 0.10070, -0.2726 0.3960, 0.10120, -0.2821 0.3566, 0.10020, -0.4090 0.3172, 0.09790, -0.5070 0.2778, 0.09440, -0.6174 0.2393, 0.08960, -0.6683 0.2056, 0.08360, -0.6612 0.1633, 0.07610, -0.7833 0.1261, 0.06710, -0.7895 0.0900, 0.05640, -0.8799 0.0571, 0.04390, -0.9341 0.0283, 0.02940, -1.0155 0.0142, 0.01970, -1.0499 0.0081, 0.01410, -1.0311 0.0026, 0.00780, -0.8553 0.0000, 0.00000, -0.4167 0.0037, -0.00840, 0.9179 0.0112, -0.01420, 1.0038 0.0191, -0.01930, 0.9417 0.0397, -0.03030, 0.7598 0.0706, -0.04420, 0.5624 0.1037, -0.05710, 0.4050 0.1384, -0.06890, 0.1901 0.1741, -0.07950, 0.0626 0.2102, -0.08660, -0.0037 0.2472, -0.09640, -0.1726 0.2844, -0.10270, -0.2378 0.3225, -0.10690, -0.3567 0.3608, -0.10890, -0.3730 0.3991, -0.10830, -0.3937 0.4373, -0.10510, -0.2847 0.4757, -0.09890, -0.2568 0.5137, -0.09070, 0.0884 0.5514, -0.08120, 0.2249 0.5917, -0.06870, 0.2060 0.5917, -0.02380, 0.2044 0.5917, 0.02120, 0.1957 16 Flap element taps 1.0000, 0.00130, -0.8714 0.9365, 0.01390, -0.0092 0.8333, 0.03280, 0.2754 0.7436, 0.04930, 0.1510 0.7049, 0.05670, -0.0245 0.6667, 0.05450, 0.1224 0.6302, 0.03770, 0.8807 0.6083, 0.01980, 0.9260 0.6000, 0.00000, -0.6043 0.6076, -0.01900, -0.8168 0.6285, -0.03060, -0.8409 0.6667, -0.04090, -0.8262 0.7046, -0.04120, -0.8432 0.7429, -0.03210, -0.8433 0.8333, -0.01400, -0.8510 0.9311, -0.00120, -0.8383 --------- Run Conditions: vel=116.3 ft/s Re=1.006x10^6 AOA=12.03 Flap deflection=-45.00 Totals: Cl=0.2060 Cdp=0.2065 Cm(c/4)=0.1602 Cs=-0.1590 Ch=-0.0576 Main component: Cl=0.4619 Cdp=-0.0006 Cm=-0.0611 Flap component: Cl=-0.2560 Cdp=0.2071 Cm=0.1602 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.0638 0.5871, 0.07930, 0.0566 0.5501, 0.08690, 0.0471 0.5112, 0.09370, 0.0318 0.4731, 0.09830, -0.0821 0.4349, 0.10070, -0.2554 0.3960, 0.10120, -0.3110 0.3566, 0.10020, -0.4842 0.3172, 0.09790, -0.5837 0.2778, 0.09440, -0.6998 0.2393, 0.08960, -0.7860 0.2056, 0.08360, -0.8114 0.1633, 0.07610, -0.9776 0.1261, 0.06710, -1.0172 0.0900, 0.05640, -1.1867 0.0571, 0.04390, -1.3795 0.0283, 0.02940, -1.6497 0.0142, 0.01970, -1.8889 0.0081, 0.01410, -2.0680 0.0026, 0.00780, -2.0414 0.0000, 0.00000, -1.9414 0.0037, -0.00840, 0.5653 0.0112, -0.01420, 0.9787 0.0191, -0.01930, 1.0083 0.0397, -0.03030, 0.9055 0.0706, -0.04420, 0.7328 0.1037, -0.05710, 0.5829 0.1384, -0.06890, 0.3602 0.1741, -0.07950, 0.2295 0.2102, -0.08660, 0.1597 0.2472, -0.09640, -0.0199 0.2844, -0.10270, -0.0976 0.3225, -0.10690, -0.2371 0.3608, -0.10890, -0.2744 0.3991, -0.10830, -0.3264 0.4373, -0.10510, -0.2317 0.4757, -0.09890, -0.1753 0.5137, -0.09070, -0.1509 0.5514, -0.08120, 0.1961 0.5917, -0.06870, 0.0418 0.5917, -0.02380, 0.0515 0.5917, 0.02120, 0.0501 16 Flap element taps 1.0000, 0.00130, -0.8293 0.9365, 0.01390, -0.0298 0.8333, 0.03280, 0.1761 0.7436, 0.04930, 0.0928 0.7049, 0.05670, -0.4128 0.6667, 0.05450, -0.1032 0.6302, 0.03770, 0.8103 0.6083, 0.01980, 0.9654 0.6000, 0.00000, -0.4483 0.6076, -0.01900, -0.7662 0.6285, -0.03060, -0.7895 0.6667, -0.04090, -0.7749 0.7046, -0.04120, -0.7950 0.7429, -0.03210, -0.7929 0.8333, -0.01400, -0.8045 0.9311, -0.00120, -0.7873 --------- Run Conditions: vel=116.3 ft/s Re=1.006x10^6 AOA=15.05 Flap deflection=-45.00 Totals: Cl=0.4228 Cdp=0.1992 Cm(c/4)=0.1425 Cs=-0.0825 Ch=-0.0421 Main component: Cl=0.6311 Cdp=0.0356 Cm=-0.0957 Flap component: Cl=-0.2083 Cdp=0.1635 Cm=0.1232 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1216 0.5871, 0.07930, -0.1306 0.5501, 0.08690, -0.1316 0.5112, 0.09370, -0.1312 0.4731, 0.09830, -0.1558 0.4349, 0.10070, -0.2388 0.3960, 0.10120, -0.2964 0.3566, 0.10020, -0.5050 0.3172, 0.09790, -0.6440 0.2778, 0.09440, -0.7941 0.2393, 0.08960, -0.9151 0.2056, 0.08360, -0.9771 0.1633, 0.07610, -1.1874 0.1261, 0.06710, -1.2911 0.0900, 0.05640, -1.5304 0.0571, 0.04390, -1.8103 0.0283, 0.02940, -2.2653 0.0142, 0.01970, -2.8590 0.0081, 0.01410, -3.4966 0.0026, 0.00780, -3.6000 0.0000, 0.00000, -4.0217 0.0037, -0.00840, -0.0893 0.0112, -0.01420, 0.7900 0.0191, -0.01930, 0.9673 0.0397, -0.03030, 0.9805 0.0706, -0.04420, 0.8629 0.1037, -0.05710, 0.7305 0.1384, -0.06890, 0.5181 0.1741, -0.07950, 0.3904 0.2102, -0.08660, 0.3194 0.2472, -0.09640, 0.1338 0.2844, -0.10270, 0.0482 0.3225, -0.10690, -0.1045 0.3608, -0.10890, -0.1587 0.3991, -0.10830, -0.2371 0.4373, -0.10510, -0.1721 0.4757, -0.09890, -0.1010 0.5137, -0.09070, -0.0817 0.5514, -0.08120, 0.1813 0.5917, -0.06870, -0.1396 0.5917, -0.02380, -0.1280 0.5917, 0.02120, -0.1298 16 Flap element taps 1.0000, 0.00130, -0.7731 0.9365, 0.01390, -0.0864 0.8333, 0.03280, 0.1182 0.7436, 0.04930, -0.0819 0.7049, 0.05670, -0.6139 0.6667, 0.05450, -0.3249 0.6302, 0.03770, 0.7214 0.6083, 0.01980, 0.9873 0.6000, 0.00000, -0.2819 0.6076, -0.01900, -0.6981 0.6285, -0.03060, -0.7233 0.6667, -0.04090, -0.7047 0.7046, -0.04120, -0.7199 0.7429, -0.03210, -0.7190 0.8333, -0.01400, -0.7307 0.9311, -0.00120, -0.7243 --------- Run Conditions: vel=116.6 ft/s Re=1.008x10^6 AOA=18.00 Flap deflection=-45.00 Totals: Cl=0.6863 Cdp=0.2128 Cm(c/4)=0.1042 Cs=0.0097 Ch=-0.0129 Main component: Cl=0.8088 Cdp=0.1039 Cm=-0.1415 Flap component: Cl=-0.1225 Cdp=0.1089 Cm=0.0661 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.4135 0.5871, 0.07930, -0.4566 0.5501, 0.08690, -0.4594 0.5112, 0.09370, -0.4579 0.4731, 0.09830, -0.4612 0.4349, 0.10070, -0.4740 0.3960, 0.10120, -0.4361 0.3566, 0.10020, -0.5602 0.3172, 0.09790, -0.6879 0.2778, 0.09440, -0.8490 0.2393, 0.08960, -0.9972 0.2056, 0.08360, -1.1062 0.1633, 0.07610, -1.3560 0.1261, 0.06710, -1.5254 0.0900, 0.05640, -1.8436 0.0571, 0.04390, -2.2635 0.0283, 0.02940, -2.9705 0.0142, 0.01970, -3.7173 0.0081, 0.01410, -4.9951 0.0026, 0.00780, -5.5255 0.0000, 0.00000, -6.5317 0.0037, -0.00840, -0.9958 0.0112, -0.01420, 0.4576 0.0191, -0.01930, 0.8320 0.0397, -0.03030, 1.0022 0.0706, -0.04420, 0.9522 0.1037, -0.05710, 0.8531 0.1384, -0.06890, 0.6639 0.1741, -0.07950, 0.5373 0.2102, -0.08660, 0.4610 0.2472, -0.09640, 0.2803 0.2844, -0.10270, 0.1826 0.3225, -0.10690, 0.0289 0.3608, -0.10890, -0.0485 0.3991, -0.10830, -0.1438 0.4373, -0.10510, -0.1150 0.4757, -0.09890, -0.0617 0.5137, -0.09070, -0.0242 0.5514, -0.08120, 0.0010 0.5917, -0.06870, -0.4022 0.5917, -0.02380, -0.4049 0.5917, 0.02120, -0.4218 16 Flap element taps 1.0000, 0.00130, -0.6536 0.9365, 0.01390, -0.0931 0.8333, 0.03280, -0.0187 0.7436, 0.04930, -0.3753 0.7049, 0.05670, -1.0288 0.6667, 0.05450, -0.6819 0.6302, 0.03770, 0.5812 0.6083, 0.01980, 1.0032 0.6000, 0.00000, -0.0677 0.6076, -0.01900, -0.5988 0.6285, -0.03060, -0.6243 0.6667, -0.04090, -0.6085 0.7046, -0.04120, -0.6247 0.7429, -0.03210, -0.6215 0.8333, -0.01400, -0.6267 0.9311, -0.00120, -0.6060 --------- Run Conditions: vel=114.3 ft/s Re=0.985x10^6 AOA=19.99 Flap deflection=-45.00 Totals: Cl=0.7334 Cdp=0.3404 Cm(c/4)=-0.0845 Cs=-0.0691 Ch=-0.0047 Main component: Cl=0.5638 Cdp=0.3424 Cm=-0.1567 Flap component: Cl=0.1696 Cdp=-0.0020 Cm=-0.1292 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.8954 0.5871, 0.07930, -0.8786 0.5501, 0.08690, -0.9029 0.5112, 0.09370, -0.9176 0.4731, 0.09830, -0.9297 0.4349, 0.10070, -0.9293 0.3960, 0.10120, -0.8667 0.3566, 0.10020, -0.8947 0.3172, 0.09790, -0.9080 0.2778, 0.09440, -0.9271 0.2393, 0.08960, -0.9152 0.2056, 0.08360, -0.8624 0.1633, 0.07610, -0.9179 0.1261, 0.06710, -0.8889 0.0900, 0.05640, -0.9079 0.0571, 0.04390, -0.8955 0.0283, 0.02940, -0.9096 0.0142, 0.01970, -0.9278 0.0081, 0.01410, -0.8794 0.0026, 0.00780, -0.8749 0.0000, 0.00000, -1.2103 0.0037, -0.00840, 0.3817 0.0112, -0.01420, 0.8848 0.0191, -0.01930, 0.9950 0.0397, -0.03030, 0.9941 0.0706, -0.04420, 0.8858 0.1037, -0.05710, 0.7751 0.1384, -0.06890, 0.5985 0.1741, -0.07950, 0.4743 0.2102, -0.08660, 0.3875 0.2472, -0.09640, 0.2126 0.2844, -0.10270, 0.1112 0.3225, -0.10690, -0.0333 0.3608, -0.10890, -0.1226 0.3991, -0.10830, -0.2164 0.4373, -0.10510, -0.2019 0.4757, -0.09890, -0.1594 0.5137, -0.09070, -0.1279 0.5514, -0.08120, -0.0811 0.5917, -0.06870, -0.8656 0.5917, -0.02380, -0.8761 0.5917, 0.02120, -0.8975 16 Flap element taps 1.0000, 0.00130, -0.4987 0.9365, 0.01390, -0.8577 0.8333, 0.03280, -0.9493 0.7436, 0.04930, -0.9660 0.7049, 0.05670, -2.0512 0.6667, 0.05450, -1.3880 0.6302, 0.03770, 0.3246 0.6083, 0.01980, 0.9974 0.6000, 0.00000, 0.1462 0.6076, -0.01900, -0.4715 0.6285, -0.03060, -0.4933 0.6667, -0.04090, -0.4788 0.7046, -0.04120, -0.4882 0.7429, -0.03210, -0.4879 0.8333, -0.01400, -0.4906 0.9311, -0.00120, -0.4747 --------- Run Conditions: vel=117.2 ft/s Re=1.005x10^6 AOA=23.99 Flap deflection=-45.00 Totals: Cl=0.7121 Cdp=0.4213 Cm(c/4)=-0.0763 Cs=-0.0954 Ch=-0.0066 Main component: Cl=0.5679 Cdp=0.4016 Cm=-0.1678 Flap component: Cl=0.1442 Cdp=0.0198 Cm=-0.1140 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.9219 0.5871, 0.07930, -0.8884 0.5501, 0.08690, -0.9041 0.5112, 0.09370, -0.9060 0.4731, 0.09830, -0.9225 0.4349, 0.10070, -0.9233 0.3960, 0.10120, -0.9249 0.3566, 0.10020, -0.9119 0.3172, 0.09790, -0.9034 0.2778, 0.09440, -0.8977 0.2393, 0.08960, -0.9025 0.2056, 0.08360, -0.9025 0.1633, 0.07610, -0.8884 0.1261, 0.06710, -0.8953 0.0900, 0.05640, -0.8864 0.0571, 0.04390, -0.8921 0.0283, 0.02940, -0.9002 0.0142, 0.01970, -0.9014 0.0081, 0.01410, -0.9129 0.0026, 0.00780, -0.8575 0.0000, 0.00000, -1.0482 0.0037, -0.00840, 0.2215 0.0112, -0.01420, 0.7929 0.0191, -0.01930, 0.9515 0.0397, -0.03030, 1.0097 0.0706, -0.04420, 0.9389 0.1037, -0.05710, 0.8269 0.1384, -0.06890, 0.7162 0.1741, -0.07950, 0.5931 0.2102, -0.08660, 0.4510 0.2472, -0.09640, 0.3168 0.2844, -0.10270, 0.1829 0.3225, -0.10690, 0.0739 0.3608, -0.10890, -0.0425 0.3991, -0.10830, -0.1209 0.4373, -0.10510, -0.1561 0.4757, -0.09890, -0.1281 0.5137, -0.09070, -0.0911 0.5514, -0.08120, -0.0489 0.5917, -0.06870, -0.8703 0.5917, -0.02380, -0.8983 0.5917, 0.02120, -0.9050 16 Flap element taps 1.0000, 0.00130, -0.5438 0.9365, 0.01390, -0.8853 0.8333, 0.03280, -0.9119 0.7436, 0.04930, -0.9536 0.7049, 0.05670, -2.0528 0.6667, 0.05450, -1.4051 0.6302, 0.03770, 0.3159 0.6083, 0.01980, 1.0028 0.6000, 0.00000, 0.1438 0.6076, -0.01900, -0.5572 0.6285, -0.03060, -0.5460 0.6667, -0.04090, -0.5545 0.7046, -0.04120, -0.5454 0.7429, -0.03210, -0.5520 0.8333, -0.01400, -0.5591 0.9311, -0.00120, -0.5630 --------- Run Conditions: vel=117.0 ft/s Re=1.003x10^6 AOA=26.97 Flap deflection=-45.00 Totals: Cl=0.6828 Cdp=0.4924 Cm(c/4)=-0.0645 Cs=-0.1291 Ch=-0.0131 Main component: Cl=0.5748 Cdp=0.4513 Cm=-0.1777 Flap component: Cl=0.1080 Cdp=0.0411 Cm=-0.0948 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.9580 0.5871, 0.07930, -0.9159 0.5501, 0.08690, -0.9319 0.5112, 0.09370, -0.9398 0.4731, 0.09830, -0.9555 0.4349, 0.10070, -0.9597 0.3960, 0.10120, -0.9623 0.3566, 0.10020, -0.9476 0.3172, 0.09790, -0.9397 0.2778, 0.09440, -0.9312 0.2393, 0.08960, -0.9366 0.2056, 0.08360, -0.9395 0.1633, 0.07610, -0.9206 0.1261, 0.06710, -0.9285 0.0900, 0.05640, -0.9188 0.0571, 0.04390, -0.9235 0.0283, 0.02940, -0.9288 0.0142, 0.01970, -0.9272 0.0081, 0.01410, -0.9423 0.0026, 0.00780, -0.8841 0.0000, 0.00000, -0.9645 0.0037, -0.00840, 0.0862 0.0112, -0.01420, 0.7172 0.0191, -0.01930, 0.9128 0.0397, -0.03030, 1.0124 0.0706, -0.04420, 0.9676 0.1037, -0.05710, 0.8701 0.1384, -0.06890, 0.7697 0.1741, -0.07950, 0.6508 0.2102, -0.08660, 0.5073 0.2472, -0.09640, 0.3751 0.2844, -0.10270, 0.2358 0.3225, -0.10690, 0.1221 0.3608, -0.10890, -0.0012 0.3991, -0.10830, -0.0884 0.4373, -0.10510, -0.1381 0.4757, -0.09890, -0.1204 0.5137, -0.09070, -0.0935 0.5514, -0.08120, -0.0556 0.5917, -0.06870, -0.9064 0.5917, -0.02380, -0.9334 0.5917, 0.02120, -0.9431 16 Flap element taps 1.0000, 0.00130, -0.6925 0.9365, 0.01390, -0.9421 0.8333, 0.03280, -0.9309 0.7436, 0.04930, -0.9799 0.7049, 0.05670, -2.0946 0.6667, 0.05450, -1.4424 0.6302, 0.03770, 0.3089 0.6083, 0.01980, 1.0051 0.6000, 0.00000, 0.0883 0.6076, -0.01900, -0.6988 0.6285, -0.03060, -0.6829 0.6667, -0.04090, -0.6898 0.7046, -0.04120, -0.6783 0.7429, -0.03210, -0.6851 0.8333, -0.01400, -0.6903 0.9311, -0.00120, -0.6995 --------- Run Conditions: vel=116.3 ft/s Re=0.997x10^6 AOA=30.01 Flap deflection=-45.00 Totals: Cl=0.6447 Cdp=0.5536 Cm(c/4)=-0.0557 Cs=-0.1569 Ch=-0.0188 Main component: Cl=0.5678 Cdp=0.4967 Cm=-0.1850 Flap component: Cl=0.0769 Cdp=0.0569 Cm=-0.0794 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.9882 0.5871, 0.07930, -0.9470 0.5501, 0.08690, -0.9501 0.5112, 0.09370, -0.9514 0.4731, 0.09830, -0.9646 0.4349, 0.10070, -0.9697 0.3960, 0.10120, -0.9746 0.3566, 0.10020, -0.9599 0.3172, 0.09790, -0.9513 0.2778, 0.09440, -0.9437 0.2393, 0.08960, -0.9498 0.2056, 0.08360, -0.9539 0.1633, 0.07610, -0.9322 0.1261, 0.06710, -0.9413 0.0900, 0.05640, -0.9302 0.0571, 0.04390, -0.9341 0.0283, 0.02940, -0.9354 0.0142, 0.01970, -0.9334 0.0081, 0.01410, -0.9507 0.0026, 0.00780, -0.8900 0.0000, 0.00000, -0.9540 0.0037, -0.00840, -0.0477 0.0112, -0.01420, 0.6336 0.0191, -0.01930, 0.8621 0.0397, -0.03030, 1.0029 0.0706, -0.04420, 0.9842 0.1037, -0.05710, 0.9043 0.1384, -0.06890, 0.8162 0.1741, -0.07950, 0.7036 0.2102, -0.08660, 0.5606 0.2472, -0.09640, 0.4317 0.2844, -0.10270, 0.2923 0.3225, -0.10690, 0.1757 0.3608, -0.10890, 0.0454 0.3991, -0.10830, -0.0491 0.4373, -0.10510, -0.1114 0.4757, -0.09890, -0.1039 0.5137, -0.09070, -0.0879 0.5514, -0.08120, -0.0561 0.5917, -0.06870, -0.9325 0.5917, -0.02380, -0.9610 0.5917, 0.02120, -0.9731 16 Flap element taps 1.0000, 0.00130, -0.8114 0.9365, 0.01390, -0.9932 0.8333, 0.03280, -0.9612 0.7436, 0.04930, -0.9977 0.7049, 0.05670, -2.1252 0.6667, 0.05450, -1.4723 0.6302, 0.03770, 0.2949 0.6083, 0.01980, 1.0029 0.6000, 0.00000, 0.0519 0.6076, -0.01900, -0.8154 0.6285, -0.03060, -0.7950 0.6667, -0.04090, -0.8033 0.7046, -0.04120, -0.7896 0.7429, -0.03210, -0.7966 0.8333, -0.01400, -0.8067 0.9311, -0.00120, -0.8131 --------- Run Conditions: vel=115.6 ft/s Re=0.990x10^6 AOA=35.03 Flap deflection=-45.00 Totals: Cl=0.4358 Cdp=0.6177 Cm(c/4)=-0.0016 Cs=-0.2556 Ch=-0.0360 Main component: Cl=0.5029 Cdp=0.5289 Cm=-0.1780 Flap component: Cl=-0.0670 Cdp=0.0888 Cm=-0.0015 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.9387 0.5871, 0.07930, -0.8821 0.5501, 0.08690, -0.8858 0.5112, 0.09370, -0.8840 0.4731, 0.09830, -0.8945 0.4349, 0.10070, -0.8956 0.3960, 0.10120, -0.9027 0.3566, 0.10020, -0.8920 0.3172, 0.09790, -0.8848 0.2778, 0.09440, -0.8759 0.2393, 0.08960, -0.8825 0.2056, 0.08360, -0.8884 0.1633, 0.07610, -0.8686 0.1261, 0.06710, -0.8750 0.0900, 0.05640, -0.8634 0.0571, 0.04390, -0.8679 0.0283, 0.02940, -0.8667 0.0142, 0.01970, -0.8625 0.0081, 0.01410, -0.8809 0.0026, 0.00780, -0.8223 0.0000, 0.00000, -0.8739 0.0037, -0.00840, -0.1752 0.0112, -0.01420, 0.5318 0.0191, -0.01930, 0.7909 0.0397, -0.03030, 0.9782 0.0706, -0.04420, 0.9928 0.1037, -0.05710, 0.9347 0.1384, -0.06890, 0.8603 0.1741, -0.07950, 0.7577 0.2102, -0.08660, 0.6206 0.2472, -0.09640, 0.4956 0.2844, -0.10270, 0.3510 0.3225, -0.10690, 0.2302 0.3608, -0.10890, 0.0907 0.3991, -0.10830, -0.0153 0.4373, -0.10510, -0.0942 0.4757, -0.09890, -0.0995 0.5137, -0.09070, -0.0888 0.5514, -0.08120, -0.0576 0.5917, -0.06870, -0.8818 0.5917, -0.02380, -0.9078 0.5917, 0.02120, -0.9248 16 Flap element taps 1.0000, 0.00130, -1.1063 0.9365, 0.01390, -0.9736 0.8333, 0.03280, -0.8950 0.7436, 0.04930, -0.9355 0.7049, 0.05670, -2.0349 0.6667, 0.05450, -1.3921 0.6302, 0.03770, 0.3396 0.6083, 0.01980, 1.0010 0.6000, 0.00000, -0.1278 0.6076, -0.01900, -1.1511 0.6285, -0.03060, -1.1247 0.6667, -0.04090, -1.1263 0.7046, -0.04120, -1.1133 0.7429, -0.03210, -1.1216 0.8333, -0.01400, -1.1451 0.9311, -0.00120, -1.1560 --------- Run Conditions: vel=114.5 ft/s Re=0.979x10^6 AOA=39.99 Flap deflection=-45.00 Totals: Cl=0.2837 Cdp=0.6647 Cm(c/4)=0.0371 Cs=-0.3269 Ch=-0.0457 Main component: Cl=0.4632 Cdp=0.5722 Cm=-0.1814 Flap component: Cl=-0.1795 Cdp=0.0925 Cm=0.0574 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.8940 0.5871, 0.07930, -0.8402 0.5501, 0.08690, -0.8428 0.5112, 0.09370, -0.8379 0.4731, 0.09830, -0.8460 0.4349, 0.10070, -0.8516 0.3960, 0.10120, -0.8582 0.3566, 0.10020, -0.8513 0.3172, 0.09790, -0.8434 0.2778, 0.09440, -0.8358 0.2393, 0.08960, -0.8450 0.2056, 0.08360, -0.8499 0.1633, 0.07610, -0.8338 0.1261, 0.06710, -0.8419 0.0900, 0.05640, -0.8316 0.0571, 0.04390, -0.8353 0.0283, 0.02940, -0.8348 0.0142, 0.01970, -0.8302 0.0081, 0.01410, -0.8475 0.0026, 0.00780, -0.7917 0.0000, 0.00000, -0.8368 0.0037, -0.00840, -0.3361 0.0112, -0.01420, 0.4046 0.0191, -0.01930, 0.7018 0.0397, -0.03030, 0.9473 0.0706, -0.04420, 1.0052 0.1037, -0.05710, 0.9762 0.1384, -0.06890, 0.9207 0.1741, -0.07950, 0.8321 0.2102, -0.08660, 0.7093 0.2472, -0.09640, 0.5895 0.2844, -0.10270, 0.4497 0.3225, -0.10690, 0.3249 0.3608, -0.10890, 0.1810 0.3991, -0.10830, 0.0632 0.4373, -0.10510, -0.0313 0.4757, -0.09890, -0.0501 0.5137, -0.09070, -0.0544 0.5514, -0.08120, -0.0315 0.5917, -0.06870, -0.8470 0.5917, -0.02380, -0.8674 0.5917, 0.02120, -0.8798 16 Flap element taps 1.0000, 0.00130, -1.3029 0.9365, 0.01390, -0.9230 0.8333, 0.03280, -0.8360 0.7436, 0.04930, -0.8915 0.7049, 0.05670, -1.9783 0.6667, 0.05450, -1.3393 0.6302, 0.03770, 0.3684 0.6083, 0.01980, 1.0101 0.6000, 0.00000, -0.2139 0.6076, -0.01900, -1.3976 0.6285, -0.03060, -1.3672 0.6667, -0.04090, -1.3614 0.7046, -0.04120, -1.3480 0.7429, -0.03210, -1.3495 0.8333, -0.01400, -1.3870 0.9311, -0.00120, -1.4093 --------- Run Conditions: vel=115.4 ft/s Re=0.987x10^6 AOA=44.94 Flap deflection=-45.00 Totals: Cl=0.2219 Cdp=0.7173 Cm(c/4)=0.0434 Cs=-0.3510 Ch=-0.0486 Main component: Cl=0.4398 Cdp=0.6383 Cm=-0.1962 Flap component: Cl=-0.2179 Cdp=0.0790 Cm=0.0736 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.9198 0.5871, 0.07930, -0.8620 0.5501, 0.08690, -0.8645 0.5112, 0.09370, -0.8585 0.4731, 0.09830, -0.8657 0.4349, 0.10070, -0.8687 0.3960, 0.10120, -0.8718 0.3566, 0.10020, -0.8662 0.3172, 0.09790, -0.8605 0.2778, 0.09440, -0.8527 0.2393, 0.08960, -0.8618 0.2056, 0.08360, -0.8645 0.1633, 0.07610, -0.8513 0.1261, 0.06710, -0.8567 0.0900, 0.05640, -0.8492 0.0571, 0.04390, -0.8514 0.0283, 0.02940, -0.8503 0.0142, 0.01970, -0.8445 0.0081, 0.01410, -0.8588 0.0026, 0.00780, -0.8073 0.0000, 0.00000, -0.8489 0.0037, -0.00840, -0.5274 0.0112, -0.01420, 0.2386 0.0191, -0.01930, 0.5781 0.0397, -0.03030, 0.8850 0.0706, -0.04420, 0.9949 0.1037, -0.05710, 0.9983 0.1384, -0.06890, 0.9643 0.1741, -0.07950, 0.8973 0.2102, -0.08660, 0.7922 0.2472, -0.09640, 0.6845 0.2844, -0.10270, 0.5542 0.3225, -0.10690, 0.4309 0.3608, -0.10890, 0.2879 0.3991, -0.10830, 0.1629 0.4373, -0.10510, 0.0585 0.4757, -0.09890, 0.0196 0.5137, -0.09070, -0.0061 0.5514, -0.08120, -0.0034 0.5917, -0.06870, -0.8712 0.5917, -0.02380, -0.8918 0.5917, 0.02120, -0.9059 16 Flap element taps 1.0000, 0.00130, -1.3811 0.9365, 0.01390, -0.9644 0.8333, 0.03280, -0.8645 0.7436, 0.04930, -0.9124 0.7049, 0.05670, -2.0096 0.6667, 0.05450, -1.3820 0.6302, 0.03770, 0.3402 0.6083, 0.01980, 1.0072 0.6000, 0.00000, -0.1832 0.6076, -0.01900, -1.5391 0.6285, -0.03060, -1.4843 0.6667, -0.04090, -1.4691 0.7046, -0.04120, -1.4487 0.7429, -0.03210, -1.4482 0.8333, -0.01400, -1.5008 0.9311, -0.00120, -1.5487 --------- Run Conditions: vel=117.2 ft/s Re=0.998x10^6 AOA=60.03 Flap deflection=-45.00 Totals: Cl=0.4164 Cdp=1.0709 Cm(c/4)=-0.0802 Cs=-0.1742 Ch=-0.2178 Main component: Cl=0.4236 Cdp=1.0488 Cm=-0.3169 Flap component: Cl=-0.0071 Cdp=0.0222 Cm=-0.0473 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.4657 0.5871, 0.07930, -1.3657 0.5501, 0.08690, -1.3855 0.5112, 0.09370, -1.3816 0.4731, 0.09830, -1.4106 0.4349, 0.10070, -1.4337 0.3960, 0.10120, -1.4261 0.3566, 0.10020, -1.4238 0.3172, 0.09790, -1.4231 0.2778, 0.09440, -1.4162 0.2393, 0.08960, -1.4071 0.2056, 0.08360, -1.3902 0.1633, 0.07610, -1.3809 0.1261, 0.06710, -1.3758 0.0900, 0.05640, -1.3604 0.0571, 0.04390, -1.3502 0.0283, 0.02940, -1.3341 0.0142, 0.01970, -1.3264 0.0081, 0.01410, -1.3273 0.0026, 0.00780, -1.2679 0.0000, 0.00000, -1.3249 0.0037, -0.00840, -1.4015 0.0112, -0.01420, -0.5880 0.0191, -0.01930, -0.0936 0.0397, -0.03030, 0.4678 0.0706, -0.04420, 0.7836 0.1037, -0.05710, 0.9245 0.1384, -0.06890, 0.9967 0.1741, -0.07950, 1.0095 0.2102, -0.08660, 0.9863 0.2472, -0.09640, 0.9358 0.2844, -0.10270, 0.8585 0.3225, -0.10690, 0.7574 0.3608, -0.10890, 0.6291 0.3991, -0.10830, 0.4878 0.4373, -0.10510, 0.3479 0.4757, -0.09890, 0.2278 0.5137, -0.09070, 0.1135 0.5514, -0.08120, -0.0021 0.5917, -0.06870, -1.3617 0.5917, -0.02380, -1.3938 0.5917, 0.02120, -1.4281 16 Flap element taps 1.0000, 0.00130, -1.0775 0.9365, 0.01390, -1.3894 0.8333, 0.03280, -1.3906 0.7436, 0.04930, -1.4526 0.7049, 0.05670, -2.8731 0.6667, 0.05450, -2.1172 0.6302, 0.03770, 0.0044 0.6083, 0.01980, 0.9573 0.6000, 0.00000, -0.0671 0.6076, -0.01900, -3.3444 0.6285, -0.03060, -2.6919 0.6667, -0.04090, -2.7067 0.7046, -0.04120, -2.7349 0.7429, -0.03210, -1.1622 0.8333, -0.01400, -0.6471 0.9311, -0.00120, -0.5558 --------- Run Conditions: vel=115.9 ft/s Re=0.985x10^6 AOA=70.04 Flap deflection=-45.00 Totals: Cl=0.5071 Cdp=1.4406 Cm(c/4)=-0.2115 Cs=-0.0151 Ch=-0.0737 Main component: Cl=0.2950 Cdp=1.2588 Cm=-0.3842 Flap component: Cl=0.2121 Cdp=0.1818 Cm=-0.2091 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.7562 0.5871, 0.07930, -1.6383 0.5501, 0.08690, -1.6287 0.5112, 0.09370, -1.6349 0.4731, 0.09830, -1.6321 0.4349, 0.10070, -1.6459 0.3960, 0.10120, -1.6566 0.3566, 0.10020, -1.6656 0.3172, 0.09790, -1.6745 0.2778, 0.09440, -1.6760 0.2393, 0.08960, -1.6636 0.2056, 0.08360, -1.6441 0.1633, 0.07610, -1.6181 0.1261, 0.06710, -1.5954 0.0900, 0.05640, -1.5710 0.0571, 0.04390, -1.5472 0.0283, 0.02940, -1.5213 0.0142, 0.01970, -1.5083 0.0081, 0.01410, -1.5072 0.0026, 0.00780, -1.4349 0.0000, 0.00000, -1.4924 0.0037, -0.00840, -1.6636 0.0112, -0.01420, -1.0944 0.0191, -0.01930, -0.5828 0.0397, -0.03030, 0.0725 0.0706, -0.04420, 0.4962 0.1037, -0.05710, 0.7241 0.1384, -0.06890, 0.8755 0.1741, -0.07950, 0.9569 0.2102, -0.08660, 0.9983 0.2472, -0.09640, 1.0107 0.2844, -0.10270, 0.9930 0.3225, -0.10690, 0.9479 0.3608, -0.10890, 0.8727 0.3991, -0.10830, 0.7704 0.4373, -0.10510, 0.6489 0.4757, -0.09890, 0.5194 0.5137, -0.09070, 0.3709 0.5514, -0.08120, 0.1808 0.5917, -0.06870, -1.5965 0.5917, -0.02380, -1.6379 0.5917, 0.02120, -1.6917 16 Flap element taps 1.0000, 0.00130, -1.1818 0.9365, 0.01390, -1.5768 0.8333, 0.03280, -1.6189 0.7436, 0.04930, -1.7033 0.7049, 0.05670, -3.3064 0.6667, 0.05450, -2.5559 0.6302, 0.03770, -0.3687 0.6083, 0.01980, 0.7373 0.6000, 0.00000, 0.6919 0.6076, -0.01900, -1.4358 0.6285, -0.03060, -1.4122 0.6667, -0.04090, -1.7149 0.7046, -0.04120, -1.6205 0.7429, -0.03210, -1.1288 0.8333, -0.01400, -0.4634 0.9311, -0.00120, -0.4942 --------- Run Conditions: vel=115.4 ft/s Re=0.982x10^6 AOA=80.03 Flap deflection=-45.00 Totals: Cl=0.4834 Cdp=1.7055 Cm(c/4)=-0.3168 Cs=0.1808 Ch=0.0532 Main component: Cl=0.1069 Cdp=1.3356 Cm=-0.4171 Flap component: Cl=0.3765 Cdp=0.3699 Cm=-0.3405 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.8267 0.5871, 0.07930, -1.7222 0.5501, 0.08690, -1.7376 0.5112, 0.09370, -1.7393 0.4731, 0.09830, -1.7549 0.4349, 0.10070, -1.7827 0.3960, 0.10120, -1.7744 0.3566, 0.10020, -1.7798 0.3172, 0.09790, -1.7854 0.2778, 0.09440, -1.7827 0.2393, 0.08960, -1.7774 0.2056, 0.08360, -1.7580 0.1633, 0.07610, -1.7380 0.1261, 0.06710, -1.7108 0.0900, 0.05640, -1.6711 0.0571, 0.04390, -1.6420 0.0283, 0.02940, -1.6219 0.0142, 0.01970, -1.6146 0.0081, 0.01410, -1.6069 0.0026, 0.00780, -1.5303 0.0000, 0.00000, -1.5942 0.0037, -0.00840, -1.6568 0.0112, -0.01420, -1.4651 0.0191, -0.01930, -1.0076 0.0397, -0.03030, -0.3352 0.0706, -0.04420, 0.1466 0.1037, -0.05710, 0.4296 0.1384, -0.06890, 0.6428 0.1741, -0.07950, 0.7834 0.2102, -0.08660, 0.8835 0.2472, -0.09640, 0.9543 0.2844, -0.10270, 0.9949 0.3225, -0.10690, 1.0108 0.3608, -0.10890, 0.9927 0.3991, -0.10830, 0.9450 0.4373, -0.10510, 0.8636 0.4757, -0.09890, 0.7525 0.5137, -0.09070, 0.6087 0.5514, -0.08120, 0.3809 0.5917, -0.06870, -1.6990 0.5917, -0.02380, -1.7394 0.5917, 0.02120, -1.7695 16 Flap element taps 1.0000, 0.00130, -1.1251 0.9365, 0.01390, -1.5920 0.8333, 0.03280, -1.6847 0.7436, 0.04930, -1.8189 0.7049, 0.05670, -3.5393 0.6667, 0.05450, -2.8504 0.6302, 0.03770, -0.7342 0.6083, 0.01980, 0.3473 0.6000, 0.00000, 0.9997 0.6076, -0.01900, 0.0026 0.6285, -0.03060, -0.3444 0.6667, -0.04090, -0.8145 0.7046, -0.04120, -1.0185 0.7429, -0.03210, -0.3028 0.8333, -0.01400, -0.2111 0.9311, -0.00120, -0.3295 --------- Run Conditions: vel=115.7 ft/s Re=0.984x10^6 AOA=90.05 Flap deflection=-45.00 Totals: Cl=0.3622 Cdp=1.8703 Cm(c/4)=-0.3926 Cs=0.3638 Ch=0.1603 Main component: Cl=-0.0998 Cdp=1.2993 Cm=-0.4215 Flap component: Cl=0.4620 Cdp=0.5710 Cm=-0.4386 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.9191 0.5871, 0.07930, -1.7626 0.5501, 0.08690, -1.7812 0.5112, 0.09370, -1.7763 0.4731, 0.09830, -1.7929 0.4349, 0.10070, -1.7949 0.3960, 0.10120, -1.7766 0.3566, 0.10020, -1.7805 0.3172, 0.09790, -1.7946 0.2778, 0.09440, -1.7927 0.2393, 0.08960, -1.8072 0.2056, 0.08360, -1.8045 0.1633, 0.07610, -1.7991 0.1261, 0.06710, -1.7816 0.0900, 0.05640, -1.7471 0.0571, 0.04390, -1.7140 0.0283, 0.02940, -1.6852 0.0142, 0.01970, -1.6735 0.0081, 0.01410, -1.6693 0.0026, 0.00780, -1.5836 0.0000, 0.00000, -1.6460 0.0037, -0.00840, -1.6557 0.0112, -0.01420, -1.6942 0.0191, -0.01930, -1.3427 0.0397, -0.03030, -0.7183 0.0706, -0.04420, -0.2269 0.1037, -0.05710, 0.0839 0.1384, -0.06890, 0.3332 0.1741, -0.07950, 0.5162 0.2102, -0.08660, 0.6624 0.2472, -0.09640, 0.7808 0.2844, -0.10270, 0.8771 0.3225, -0.10690, 0.9522 0.3608, -0.10890, 0.9947 0.3991, -0.10830, 1.0041 0.4373, -0.10510, 0.9796 0.4757, -0.09890, 0.9096 0.5137, -0.09070, 0.7952 0.5514, -0.08120, 0.5612 0.5917, -0.06870, -1.7639 0.5917, -0.02380, -1.8077 0.5917, 0.02120, -1.8440 16 Flap element taps 1.0000, 0.00130, -1.0301 0.9365, 0.01390, -1.5724 0.8333, 0.03280, -1.7209 0.7436, 0.04930, -1.9186 0.7049, 0.05670, -3.7207 0.6667, 0.05450, -3.1287 0.6302, 0.03770, -1.1323 0.6083, 0.01980, -0.2296 0.6000, 0.00000, 0.8382 0.6076, -0.01900, 0.8467 0.6285, -0.03060, 0.4789 0.6667, -0.04090, 0.0126 0.7046, -0.04120, -0.2921 0.7429, -0.03210, 0.0875 0.8333, -0.01400, 0.0705 0.9311, -0.00120, -0.1308 --------- Run Conditions: vel=117.0 ft/s Re=0.994x10^6 AOA=120.03 Flap deflection=-45.00 Totals: Cl=-0.0756 Cdp=1.7438 Cm(c/4)=-0.4061 Cs=0.8073 Ch=0.2872 Main component: Cl=-0.4700 Cdp=0.8199 Cm=-0.3456 Flap component: Cl=0.3945 Cdp=0.9239 Cm=-0.4474 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.7865 0.5871, 0.07930, -1.6814 0.5501, 0.08690, -1.6995 0.5112, 0.09370, -1.7191 0.4731, 0.09830, -1.7342 0.4349, 0.10070, -1.7407 0.3960, 0.10120, -1.7269 0.3566, 0.10020, -1.7328 0.3172, 0.09790, -1.7418 0.2778, 0.09440, -1.7434 0.2393, 0.08960, -1.7532 0.2056, 0.08360, -1.7471 0.1633, 0.07610, -1.7541 0.1261, 0.06710, -1.7512 0.0900, 0.05640, -1.7471 0.0571, 0.04390, -1.7159 0.0283, 0.02940, -1.6740 0.0142, 0.01970, -1.6507 0.0081, 0.01410, -1.6446 0.0026, 0.00780, -1.5724 0.0000, 0.00000, -1.6287 0.0037, -0.00840, -1.6142 0.0112, -0.01420, -1.6546 0.0191, -0.01930, -1.7227 0.0397, -0.03030, -1.5027 0.0706, -0.04420, -1.1891 0.1037, -0.05710, -0.9575 0.1384, -0.06890, -0.7311 0.1741, -0.07950, -0.5381 0.2102, -0.08660, -0.3540 0.2472, -0.09640, -0.1912 0.2844, -0.10270, -0.0007 0.3225, -0.10690, 0.1849 0.3608, -0.10890, 0.3726 0.3991, -0.10830, 0.5670 0.4373, -0.10510, 0.7504 0.4757, -0.09890, 0.9027 0.5137, -0.09070, 0.9972 0.5514, -0.08120, 0.9350 0.5917, -0.06870, -1.6834 0.5917, -0.02380, -1.7207 0.5917, 0.02120, -1.7249 16 Flap element taps 1.0000, 0.00130, -0.5543 0.9365, 0.01390, -0.9723 0.8333, 0.03280, -1.5315 0.7436, 0.04930, -1.9599 0.7049, 0.05670, -3.8399 0.6667, 0.05450, -3.5433 0.6302, 0.03770, -1.9782 0.6083, 0.01980, -2.9324 0.6000, 0.00000, -2.9734 0.6076, -0.01900, -1.1943 0.6285, -0.03060, 0.5476 0.6667, -0.04090, 0.9531 0.7046, -0.04120, 1.0029 0.7429, -0.03210, 0.9458 0.8333, -0.01400, 0.8235 0.9311, -0.00120, 0.5556 --------- Run Conditions: vel=116.9 ft/s Re=0.992x10^6 AOA=150.10 Flap deflection=-45.00 Totals: Cl=-0.1777 Cdp=0.6954 Cm(c/4)=-0.2622 Cs=0.5142 Ch=-0.0241 Main component: Cl=-0.0781 Cdp=0.1102 Cm=-0.0744 Flap component: Cl=-0.0996 Cdp=0.5852 Cm=-0.3130 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.1111 0.5871, 0.07930, -1.0771 0.5501, 0.08690, -1.0793 0.5112, 0.09370, -1.0888 0.4731, 0.09830, -1.0947 0.4349, 0.10070, -1.0959 0.3960, 0.10120, -1.0821 0.3566, 0.10020, -1.0967 0.3172, 0.09790, -1.0929 0.2778, 0.09440, -1.0968 0.2393, 0.08960, -1.0866 0.2056, 0.08360, -1.0818 0.1633, 0.07610, -1.1082 0.1261, 0.06710, -1.1208 0.0900, 0.05640, -1.1484 0.0571, 0.04390, -1.1560 0.0283, 0.02940, -1.1459 0.0142, 0.01970, -1.1259 0.0081, 0.01410, -1.1189 0.0026, 0.00780, -1.0645 0.0000, 0.00000, -1.1145 0.0037, -0.00840, -1.2154 0.0112, -0.01420, -1.5952 0.0191, -0.01930, -1.6875 0.0397, -0.03030, -1.6414 0.0706, -0.04420, -1.5359 0.1037, -0.05710, -1.4703 0.1384, -0.06890, -1.3868 0.1741, -0.07950, -1.3059 0.2102, -0.08660, -1.2106 0.2472, -0.09640, -1.1475 0.2844, -0.10270, -0.9991 0.3225, -0.10690, -0.8246 0.3608, -0.10890, -0.5848 0.3991, -0.10830, -0.2462 0.4373, -0.10510, 0.1681 0.4757, -0.09890, 0.3086 0.5137, -0.09070, -0.4079 0.5514, -0.08120, -1.0232 0.5917, -0.06870, -1.1030 0.5917, -0.02380, -1.1079 0.5917, 0.02120, -1.0973 16 Flap element taps 1.0000, 0.00130, -0.9754 0.9365, 0.01390, -1.0256 0.8333, 0.03280, -1.0558 0.7436, 0.04930, -1.0644 0.7049, 0.05670, -1.1597 0.6667, 0.05450, -1.0016 0.6302, 0.03770, -0.8388 0.6083, 0.01980, -0.9837 0.6000, 0.00000, -0.8950 0.6076, -0.01900, -0.8565 0.6285, -0.03060, -0.5171 0.6667, -0.04090, 0.0941 0.7046, -0.04120, 0.3846 0.7429, -0.03210, 0.8711 0.8333, -0.01400, 1.0035 0.9311, -0.00120, 0.8997 --------- Run Conditions: vel=122.3 ft/s Re=1.037x10^6 AOA=180.05 Flap deflection=-45.00 Totals: Cl=-0.2015 Cdp=0.2618 Cm(c/4)=-0.1418 Cs=0.2620 Ch=-0.1030 Main component: Cl=0.0279 Cdp=-0.0545 Cm=0.0121 Flap component: Cl=-0.2293 Cdp=0.3163 Cm=-0.2041 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.0137 0.5871, 0.07930, -0.9135 0.5501, 0.08690, -0.9199 0.5112, 0.09370, -0.9356 0.4731, 0.09830, -0.9421 0.4349, 0.10070, -0.9250 0.3960, 0.10120, -0.8913 0.3566, 0.10020, -0.8766 0.3172, 0.09790, -0.8517 0.2778, 0.09440, -0.8287 0.2393, 0.08960, -0.7929 0.2056, 0.08360, -0.7458 0.1633, 0.07610, -0.7199 0.1261, 0.06710, -0.6711 0.0900, 0.05640, -0.6306 0.0571, 0.04390, -0.5974 0.0283, 0.02940, -0.6380 0.0142, 0.01970, -0.7040 0.0081, 0.01410, -0.7690 0.0026, 0.00780, -0.8270 0.0000, 0.00000, -1.0012 0.0037, -0.00840, -0.8351 0.0112, -0.01420, -0.7223 0.0191, -0.01930, -0.6639 0.0397, -0.03030, -0.6133 0.0706, -0.04420, -0.6059 0.1037, -0.05710, -0.6324 0.1384, -0.06890, -0.6644 0.1741, -0.07950, -0.7100 0.2102, -0.08660, -0.7561 0.2472, -0.09640, -0.8152 0.2844, -0.10270, -0.8727 0.3225, -0.10690, -0.9487 0.3608, -0.10890, -1.0052 0.3991, -0.10830, -1.0307 0.4373, -0.10510, -1.0207 0.4757, -0.09890, -1.0050 0.5137, -0.09070, -0.9945 0.5514, -0.08120, -1.0050 0.5917, -0.06870, -1.0006 0.5917, -0.02380, -0.9600 0.5917, 0.02120, -0.9651 16 Flap element taps 1.0000, 0.00130, -0.8120 0.9365, 0.01390, -0.8282 0.8333, 0.03280, -0.8372 0.7436, 0.04930, -0.8683 0.7049, 0.05670, -0.9395 0.6667, 0.05450, -0.9805 0.6302, 0.03770, -0.9225 0.6083, 0.01980, -0.8923 0.6000, 0.00000, -0.8921 0.6076, -0.01900, -0.8724 0.6285, -0.03060, -0.9937 0.6667, -0.04090, -0.8854 0.7046, -0.04120, -0.8019 0.7429, -0.03210, 0.3333 0.8333, -0.01400, 0.7597 0.9311, -0.00120, 0.9845 --------- Run Conditions: vel=120.6 ft/s Re=1.023x10^6 AOA=210.06 Flap deflection=-45.00 Totals: Cl=0.3643 Cdp=0.3947 Cm(c/4)=0.1284 Cs=0.1591 Ch=-0.0611 Main component: Cl=0.2271 Cdp=0.3725 Cm=0.1613 Flap component: Cl=0.1372 Cdp=0.0222 Cm=0.0953 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.7133 0.5871, 0.07930, 0.8285 0.5501, 0.08690, 0.6244 0.5112, 0.09370, 0.4196 0.4731, 0.09830, 0.2108 0.4349, 0.10070, 0.0640 0.3960, 0.10120, -0.0364 0.3566, 0.10020, -0.1759 0.3172, 0.09790, -0.2760 0.2778, 0.09440, -0.4127 0.2393, 0.08960, -0.5294 0.2056, 0.08360, -0.6423 0.1633, 0.07610, -0.7828 0.1261, 0.06710, -0.8762 0.0900, 0.05640, -0.9708 0.0571, 0.04390, -0.9525 0.0283, 0.02940, -0.9003 0.0142, 0.01970, -0.9052 0.0081, 0.01410, -0.9084 0.0026, 0.00780, -0.8813 0.0000, 0.00000, -0.9395 0.0037, -0.00840, -0.9340 0.0112, -0.01420, -0.9341 0.0191, -0.01930, -0.9351 0.0397, -0.03030, -0.9447 0.0706, -0.04420, -0.9294 0.1037, -0.05710, -0.9313 0.1384, -0.06890, -0.9495 0.1741, -0.07950, -0.9587 0.2102, -0.08660, -0.9536 0.2472, -0.09640, -0.9687 0.2844, -0.10270, -0.9603 0.3225, -0.10690, -0.9599 0.3608, -0.10890, -0.9461 0.3991, -0.10830, -0.9469 0.4373, -0.10510, -0.9294 0.4757, -0.09890, -0.9273 0.5137, -0.09070, -0.9133 0.5514, -0.08120, -0.9143 0.5917, -0.06870, -0.7351 0.5917, -0.02380, 0.3169 0.5917, 0.02120, 0.5456 16 Flap element taps 1.0000, 0.00130, 0.9830 0.9365, 0.01390, 0.3394 0.8333, 0.03280, 0.4036 0.7436, 0.04930, 0.3144 0.7049, 0.05670, -0.1617 0.6667, 0.05450, -0.7221 0.6302, 0.03770, -0.6956 0.6083, 0.01980, -0.1738 0.6000, 0.00000, -0.0612 0.6076, -0.01900, -0.0898 0.6285, -0.03060, -0.7825 0.6667, -0.04090, -1.1133 0.7046, -0.04120, -1.5488 0.7429, -0.03210, -0.2948 0.8333, -0.01400, 0.1287 0.9311, -0.00120, 0.4125 --------- Run Conditions: vel=113.7 ft/s Re=0.964x10^6 AOA=240.03 Flap deflection=-45.00 Totals: Cl=0.8289 Cdp=1.0117 Cm(c/4)=0.3975 Cs=-0.2126 Ch=0.1348 Main component: Cl=0.3125 Cdp=0.7629 Cm=0.3139 Flap component: Cl=0.5164 Cdp=0.2488 Cm=0.4062 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.4995 0.5871, 0.07930, 1.0062 0.5501, 0.08690, 0.9984 0.5112, 0.09370, 0.9481 0.4731, 0.09830, 0.8617 0.4349, 0.10070, 0.7744 0.3960, 0.10120, 0.7189 0.3566, 0.10020, 0.5638 0.3172, 0.09790, 0.4522 0.2778, 0.09440, 0.3028 0.2393, 0.08960, 0.1601 0.2056, 0.08360, 0.0174 0.1633, 0.07610, -0.2280 0.1261, 0.06710, -0.4296 0.0900, 0.05640, -0.7186 0.0571, 0.04390, -1.0281 0.0283, 0.02940, -1.2240 0.0142, 0.01970, -1.1137 0.0081, 0.01410, -1.0849 0.0026, 0.00780, -1.0693 0.0000, 0.00000, -1.1276 0.0037, -0.00840, -1.1233 0.0112, -0.01420, -1.1207 0.0191, -0.01930, -1.1238 0.0397, -0.03030, -1.1326 0.0706, -0.04420, -1.1267 0.1037, -0.05710, -1.1342 0.1384, -0.06890, -1.1702 0.1741, -0.07950, -1.1727 0.2102, -0.08660, -1.1490 0.2472, -0.09640, -1.1794 0.2844, -0.10270, -1.1682 0.3225, -0.10690, -1.1964 0.3608, -0.10890, -1.1823 0.3991, -0.10830, -1.1969 0.4373, -0.10510, -1.1673 0.4757, -0.09890, -1.1574 0.5137, -0.09070, -1.1269 0.5514, -0.08120, -1.1215 0.5917, -0.06870, -0.9500 0.5917, -0.02380, -0.0316 0.5917, 0.02120, -0.5562 16 Flap element taps 1.0000, 0.00130, -1.4631 0.9365, 0.01390, 0.9655 0.8333, 0.03280, 0.7839 0.7436, 0.04930, 0.3503 0.7049, 0.05670, -0.6425 0.6667, 0.05450, -1.6505 0.6302, 0.03770, -1.5506 0.6083, 0.01980, -1.5479 0.6000, 0.00000, -1.4856 0.6076, -0.01900, -1.4528 0.6285, -0.03060, -1.4716 0.6667, -0.04090, -1.4995 0.7046, -0.04120, -1.5284 0.7429, -0.03210, -1.4951 0.8333, -0.01400, -1.4784 0.9311, -0.00120, -1.4568 --------- Run Conditions: vel=114.7 ft/s Re=0.973x10^6 AOA=269.08 Flap deflection=-45.00 Totals: Cl=0.3562 Cdp=1.5177 Cm(c/4)=0.3956 Cs=-0.3318 Ch=0.2186 Main component: Cl=0.1046 Cdp=1.0726 Cm=0.3773 Flap component: Cl=0.2516 Cdp=0.4451 Cm=0.3992 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.6401 0.5871, 0.07930, 0.7025 0.5501, 0.08690, 0.8783 0.5112, 0.09370, 0.9491 0.4731, 0.09830, 0.9799 0.4349, 0.10070, 1.0019 0.3960, 0.10120, 1.0489 0.3566, 0.10020, 0.9651 0.3172, 0.09790, 0.9242 0.2778, 0.09440, 0.8473 0.2393, 0.08960, 0.7701 0.2056, 0.08360, 0.6953 0.1633, 0.07610, 0.4770 0.1261, 0.06710, 0.2956 0.0900, 0.05640, -0.0170 0.0571, 0.04390, -0.4322 0.0283, 0.02940, -0.9948 0.0142, 0.01970, -1.3211 0.0081, 0.01410, -1.2474 0.0026, 0.00780, -1.1492 0.0000, 0.00000, -1.2004 0.0037, -0.00840, -1.1936 0.0112, -0.01420, -1.1866 0.0191, -0.01930, -1.1878 0.0397, -0.03030, -1.2003 0.0706, -0.04420, -1.1879 0.1037, -0.05710, -1.1888 0.1384, -0.06890, -1.2326 0.1741, -0.07950, -1.2272 0.2102, -0.08660, -1.1832 0.2472, -0.09640, -1.2158 0.2844, -0.10270, -1.1935 0.3225, -0.10690, -1.2284 0.3608, -0.10890, -1.2071 0.3991, -0.10830, -1.2345 0.4373, -0.10510, -1.2102 0.4757, -0.09890, -1.2151 0.5137, -0.09070, -1.2067 0.5514, -0.08120, -1.2085 0.5917, -0.06870, -0.9988 0.5917, -0.02380, -1.6508 0.5917, 0.02120, -1.6711 16 Flap element taps 1.0000, 0.00130, -1.5312 0.9365, 0.01390, 0.9136 0.8333, 0.03280, 0.9261 0.7436, 0.04930, 0.3336 0.7049, 0.05670, -1.2383 0.6667, 0.05450, -2.8248 0.6302, 0.03770, -2.5424 0.6083, 0.01980, -1.9878 0.6000, 0.00000, -1.5801 0.6076, -0.01900, -1.5629 0.6285, -0.03060, -1.5531 0.6667, -0.04090, -1.5306 0.7046, -0.04120, -1.5500 0.7429, -0.03210, -1.5420 0.8333, -0.01400, -1.5465 0.9311, -0.00120, -1.5245