S809 VENTED AILERON MODEL, 18 IN CHORD --------- Run Conditions: vel=113.2 ft/s Re=1.006x10^6 AOA=-6.06 Flap deflection=-90.00 Totals: Cl=-0.3332 Cdp=0.5545 Cm(c/4)=0.0283 Cs=-0.5163 Ch=0.0324 Main component: Cl=-0.3220 Cdp=-0.0663 Cm=0.0527 Flap component: Cl=-0.0112 Cdp=0.6208 Cm=0.0731 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.4523 0.5871, 0.07930, 0.4481 0.5501, 0.08690, 0.2834 0.5112, 0.09370, 0.0866 0.4731, 0.09830, 0.0762 0.4349, 0.10070, 0.0377 0.3960, 0.10120, 0.0358 0.3566, 0.10020, 0.0120 0.3172, 0.09790, 0.0227 0.2778, 0.09440, 0.0255 0.2393, 0.08960, 0.0500 0.2056, 0.08360, 0.1224 0.1633, 0.07610, 0.1559 0.1261, 0.06710, 0.2665 0.0900, 0.05640, 0.3797 0.0571, 0.04390, 0.5622 0.0283, 0.02940, 0.7991 0.0142, 0.01970, 0.9624 0.0081, 0.01410, 1.0164 0.0026, 0.00780, 0.8134 0.0000, 0.00000, -0.1007 0.0037, -0.00840, -0.9626 0.0112, -0.01420, -0.8077 0.0191, -0.01930, -0.6778 0.0397, -0.03030, -0.5312 0.0706, -0.04420, -0.5141 0.1037, -0.05710, -0.5304 0.1384, -0.06890, -0.5863 0.1741, -0.07950, -0.5960 0.2102, -0.08660, -0.6023 0.2472, -0.09640, -0.6398 0.2844, -0.10270, -0.5982 0.3225, -0.10690, -0.5592 0.3608, -0.10890, -0.4963 0.3991, -0.10830, -0.3802 0.4373, -0.10510, -0.0508 0.4757, -0.09890, 0.1795 0.5137, -0.09070, 0.3524 0.5514, -0.08120, 0.4081 0.5917, -0.06870, 0.4332 0.5917, -0.02380, 0.4424 0.5917, 0.02120, 0.4481 16 Flap element taps 1.0000, 0.00130, -1.1472 0.9365, 0.01390, 0.9278 0.8333, 0.03280, 0.8403 0.7436, 0.04930, 0.4888 0.7049, 0.05670, 0.2674 0.6667, 0.05450, -0.0270 0.6302, 0.03770, -0.6092 0.6083, 0.01980, -1.2587 0.6000, 0.00000, -1.3067 0.6076, -0.01900, -1.2721 0.6285, -0.03060, -1.2726 0.6667, -0.04090, -1.3091 0.7046, -0.04120, -1.3287 0.7429, -0.03210, -1.2547 0.8333, -0.01400, -1.2252 0.9311, -0.00120, -1.1887 --------- Run Conditions: vel=113.5 ft/s Re=1.007x10^6 AOA=0.05 Flap deflection=-90.00 Totals: Cl=-0.1038 Cdp=0.5500 Cm(c/4)=0.0502 Cs=-0.5501 Ch=0.0143 Main component: Cl=-0.0264 Cdp=-0.0842 Cm=0.0055 Flap component: Cl=-0.0774 Cdp=0.6342 Cm=0.0705 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.5760 0.5871, 0.07930, 0.5008 0.5501, 0.08690, 0.3741 0.5112, 0.09370, 0.2104 0.4731, 0.09830, -0.0558 0.4349, 0.10070, -0.0758 0.3960, 0.10120, -0.0896 0.3566, 0.10020, -0.1357 0.3172, 0.09790, -0.1584 0.2778, 0.09440, -0.1925 0.2393, 0.08960, -0.2043 0.2056, 0.08360, -0.1763 0.1633, 0.07610, -0.1803 0.1261, 0.06710, -0.1187 0.0900, 0.05640, -0.0596 0.0571, 0.04390, 0.0608 0.0283, 0.02940, 0.2529 0.0142, 0.01970, 0.4677 0.0081, 0.01410, 0.6324 0.0026, 0.00780, 0.8411 0.0000, 0.00000, 0.9945 0.0037, -0.00840, 0.6116 0.0112, -0.01420, 0.4075 0.0191, -0.01930, 0.3230 0.0397, -0.03030, 0.1988 0.0706, -0.04420, 0.0541 0.1037, -0.05710, -0.0486 0.1384, -0.06890, -0.1640 0.1741, -0.07950, -0.2286 0.2102, -0.08660, -0.2828 0.2472, -0.09640, -0.3639 0.2844, -0.10270, -0.3686 0.3225, -0.10690, -0.3685 0.3608, -0.10890, -0.3155 0.3991, -0.10830, -0.2748 0.4373, -0.10510, -0.2691 0.4757, -0.09890, 0.1925 0.5137, -0.09070, 0.3624 0.5514, -0.08120, 0.5012 0.5917, -0.06870, 0.5690 0.5917, -0.02380, 0.5710 0.5917, 0.02120, 0.5710 16 Flap element taps 1.0000, 0.00130, -1.1504 0.9365, 0.01390, 0.9130 0.8333, 0.03280, 0.7901 0.7436, 0.04930, 0.5764 0.7049, 0.05670, 0.4513 0.6667, 0.05450, 0.1804 0.6302, 0.03770, -0.4911 0.6083, 0.01980, -1.3305 0.6000, 0.00000, -1.4098 0.6076, -0.01900, -1.2755 0.6285, -0.03060, -1.2851 0.6667, -0.04090, -1.3404 0.7046, -0.04120, -1.3538 0.7429, -0.03210, -1.2552 0.8333, -0.01400, -1.2112 0.9311, -0.00120, -1.1905 --------- Run Conditions: vel=113.5 ft/s Re=1.008x10^6 AOA=3.10 Flap deflection=-90.00 Totals: Cl=-0.0211 Cdp=0.5406 Cm(c/4)=0.0605 Cs=-0.5409 Ch=0.0036 Main component: Cl=0.0870 Cdp=-0.0861 Cm=-0.0081 Flap component: Cl=-0.1081 Cdp=0.6267 Cm=0.0666 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.5677 0.5871, 0.07930, 0.5386 0.5501, 0.08690, 0.4446 0.5112, 0.09370, 0.2618 0.4731, 0.09830, 0.0919 0.4349, 0.10070, -0.1081 0.3960, 0.10120, -0.1449 0.3566, 0.10020, -0.1836 0.3172, 0.09790, -0.2248 0.2778, 0.09440, -0.2789 0.2393, 0.08960, -0.3105 0.2056, 0.08360, -0.3099 0.1633, 0.07610, -0.3334 0.1261, 0.06710, -0.3044 0.0900, 0.05640, -0.2802 0.0571, 0.04390, -0.2117 0.0283, 0.02940, -0.0876 0.0142, 0.01970, 0.0802 0.0081, 0.01410, 0.2257 0.0026, 0.00780, 0.4500 0.0000, 0.00000, 0.9105 0.0037, -0.00840, 0.9258 0.0112, -0.01420, 0.7334 0.0191, -0.01930, 0.6213 0.0397, -0.03030, 0.4446 0.0706, -0.04420, 0.2580 0.1037, -0.05710, 0.1303 0.1384, -0.06890, -0.0023 0.1741, -0.07950, -0.0866 0.2102, -0.08660, -0.1646 0.2472, -0.09640, -0.2637 0.2844, -0.10270, -0.2904 0.3225, -0.10690, -0.3095 0.3608, -0.10890, -0.2807 0.3991, -0.10830, -0.2218 0.4373, -0.10510, -0.2010 0.4757, -0.09890, 0.1695 0.5137, -0.09070, 0.3430 0.5514, -0.08120, 0.5040 0.5917, -0.06870, 0.5782 0.5917, -0.02380, 0.5754 0.5917, 0.02120, 0.5719 16 Flap element taps 1.0000, 0.00130, -1.1696 0.9365, 0.01390, 0.8989 0.8333, 0.03280, 0.6006 0.7436, 0.04930, 0.5821 0.7049, 0.05670, 0.5543 0.6667, 0.05450, 0.3402 0.6302, 0.03770, -0.3985 0.6083, 0.01980, -1.4554 0.6000, 0.00000, -1.5272 0.6076, -0.01900, -1.2839 0.6285, -0.03060, -1.2859 0.6667, -0.04090, -1.3306 0.7046, -0.04120, -1.3484 0.7429, -0.03210, -1.2845 0.8333, -0.01400, -1.2393 0.9311, -0.00120, -1.2094 --------- Run Conditions: vel=113.2 ft/s Re=1.005x10^6 AOA=6.08 Flap deflection=-90.00 Totals: Cl=-0.0423 Cdp=0.5797 Cm(c/4)=0.0539 Cs=-0.5809 Ch=-0.0615 Main component: Cl=0.0693 Cdp=-0.0768 Cm=0.0188 Flap component: Cl=-0.1117 Cdp=0.6565 Cm=0.0302 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.5046 0.5871, 0.07930, 0.4984 0.5501, 0.08690, 0.4873 0.5112, 0.09370, 0.4446 0.4731, 0.09830, 0.2831 0.4349, 0.10070, 0.1185 0.3960, 0.10120, 0.0271 0.3566, 0.10020, -0.0886 0.3172, 0.09790, -0.1966 0.2778, 0.09440, -0.2523 0.2393, 0.08960, -0.3029 0.2056, 0.08360, -0.3316 0.1633, 0.07610, -0.3787 0.1261, 0.06710, -0.3845 0.0900, 0.05640, -0.3970 0.0571, 0.04390, -0.3811 0.0283, 0.02940, -0.3293 0.0142, 0.01970, -0.2258 0.0081, 0.01410, -0.1235 0.0026, 0.00780, 0.0661 0.0000, 0.00000, 0.6373 0.0037, -0.00840, 1.0026 0.0112, -0.01420, 0.8814 0.0191, -0.01930, 0.7752 0.0397, -0.03030, 0.5840 0.0706, -0.04420, 0.3770 0.1037, -0.05710, 0.2344 0.1384, -0.06890, 0.0878 0.1741, -0.07950, -0.0124 0.2102, -0.08660, -0.1122 0.2472, -0.09640, -0.2297 0.2844, -0.10270, -0.2835 0.3225, -0.10690, -0.3279 0.3608, -0.10890, -0.3380 0.3991, -0.10830, -0.2918 0.4373, -0.10510, -0.2342 0.4757, -0.09890, -0.2370 0.5137, -0.09070, 0.1978 0.5514, -0.08120, 0.3582 0.5917, -0.06870, 0.5134 0.5917, -0.02380, 0.5035 0.5917, 0.02120, 0.5017 16 Flap element taps 1.0000, 0.00130, -1.2204 0.9365, 0.01390, 0.5332 0.8333, 0.03280, 0.5143 0.7436, 0.04930, 0.6529 0.7049, 0.05670, 0.9514 0.6667, 0.05450, 0.8430 0.6302, 0.03770, -0.0225 0.6083, 0.01980, -1.0323 0.6000, 0.00000, -1.2498 0.6076, -0.01900, -1.2623 0.6285, -0.03060, -1.2952 0.6667, -0.04090, -1.3597 0.7046, -0.04120, -1.4002 0.7429, -0.03210, -1.3275 0.8333, -0.01400, -1.2871 0.9311, -0.00120, -1.2732 --------- Run Conditions: vel=113.2 ft/s Re=1.004x10^6 AOA=9.11 Flap deflection=-90.00 Totals: Cl=0.0311 Cdp=0.5848 Cm(c/4)=0.0604 Cs=-0.5725 Ch=-0.0684 Main component: Cl=0.1711 Cdp=-0.0616 Cm=0.0050 Flap component: Cl=-0.1400 Cdp=0.6464 Cm=0.0246 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.4168 0.5871, 0.07930, 0.4043 0.5501, 0.08690, 0.4054 0.5112, 0.09370, 0.4017 0.4731, 0.09830, 0.3341 0.4349, 0.10070, 0.1807 0.3960, 0.10120, 0.0568 0.3566, 0.10020, -0.0545 0.3172, 0.09790, -0.1391 0.2778, 0.09440, -0.2790 0.2393, 0.08960, -0.3868 0.2056, 0.08360, -0.4275 0.1633, 0.07610, -0.5037 0.1261, 0.06710, -0.5442 0.0900, 0.05640, -0.6077 0.0571, 0.04390, -0.6640 0.0283, 0.02940, -0.7280 0.0142, 0.01970, -0.7419 0.0081, 0.01410, -0.7358 0.0026, 0.00780, -0.5328 0.0000, 0.00000, -0.0615 0.0037, -0.00840, 0.9731 0.0112, -0.01420, 1.0016 0.0191, -0.01930, 0.9327 0.0397, -0.03030, 0.7596 0.0706, -0.04420, 0.5471 0.1037, -0.05710, 0.3958 0.1384, -0.06890, 0.2412 0.1741, -0.07950, 0.1282 0.2102, -0.08660, 0.0171 0.2472, -0.09640, -0.1133 0.2844, -0.10270, -0.1834 0.3225, -0.10690, -0.2480 0.3608, -0.10890, -0.2821 0.3991, -0.10830, -0.2640 0.4373, -0.10510, -0.1879 0.4757, -0.09890, -0.1735 0.5137, -0.09070, 0.1565 0.5514, -0.08120, 0.2927 0.5917, -0.06870, 0.4353 0.5917, -0.02380, 0.4241 0.5917, 0.02120, 0.4202 16 Flap element taps 1.0000, 0.00130, -1.2421 0.9365, 0.01390, 0.4770 0.8333, 0.03280, 0.4651 0.7436, 0.04930, 0.7456 0.7049, 0.05670, 0.9998 0.6667, 0.05450, 0.8656 0.6302, 0.03770, 0.0637 0.6083, 0.01980, -0.9481 0.6000, 0.00000, -1.1886 0.6076, -0.01900, -1.2229 0.6285, -0.03060, -1.2611 0.6667, -0.04090, -1.3195 0.7046, -0.04120, -1.3570 0.7429, -0.03210, -1.2992 0.8333, -0.01400, -1.2739 0.9311, -0.00120, -1.2791 --------- Run Conditions: vel=113.5 ft/s Re=1.006x10^6 AOA=12.08 Flap deflection=-90.00 Totals: Cl=0.0838 Cdp=0.5822 Cm(c/4)=0.0638 Cs=-0.5518 Ch=-0.0812 Main component: Cl=0.2427 Cdp=-0.0346 Cm=-0.0017 Flap component: Cl=-0.1589 Cdp=0.6169 Cm=0.0145 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.2534 0.5871, 0.07930, 0.2723 0.5501, 0.08690, 0.2704 0.5112, 0.09370, 0.2792 0.4731, 0.09830, 0.2791 0.4349, 0.10070, 0.2454 0.3960, 0.10120, 0.1667 0.3566, 0.10020, 0.0180 0.3172, 0.09790, -0.1188 0.2778, 0.09440, -0.2610 0.2393, 0.08960, -0.3768 0.2056, 0.08360, -0.4616 0.1633, 0.07610, -0.5775 0.1261, 0.06710, -0.6746 0.0900, 0.05640, -0.8152 0.0571, 0.04390, -0.9480 0.0283, 0.02940, -1.1406 0.0142, 0.01970, -1.2975 0.0081, 0.01410, -1.4072 0.0026, 0.00780, -1.2983 0.0000, 0.00000, -1.0417 0.0037, -0.00840, 0.7833 0.0112, -0.01420, 1.0148 0.0191, -0.01930, 1.0087 0.0397, -0.03030, 0.8815 0.0706, -0.04420, 0.6809 0.1037, -0.05710, 0.5305 0.1384, -0.06890, 0.3649 0.1741, -0.07950, 0.2460 0.2102, -0.08660, 0.1279 0.2472, -0.09640, -0.0162 0.2844, -0.10270, -0.1009 0.3225, -0.10690, -0.1878 0.3608, -0.10890, -0.2412 0.3991, -0.10830, -0.2540 0.4373, -0.10510, -0.1839 0.4757, -0.09890, -0.1426 0.5137, -0.09070, -0.0975 0.5514, -0.08120, 0.2307 0.5917, -0.06870, 0.2821 0.5917, -0.02380, 0.2728 0.5917, 0.02120, 0.2639 16 Flap element taps 1.0000, 0.00130, -1.2482 0.9365, 0.01390, 0.2985 0.8333, 0.03280, 0.3757 0.7436, 0.04930, 0.7403 0.7049, 0.05670, 0.9863 0.6667, 0.05450, 0.9160 0.6302, 0.03770, 0.1720 0.6083, 0.01980, -0.8677 0.6000, 0.00000, -1.1625 0.6076, -0.01900, -1.1899 0.6285, -0.03060, -1.2213 0.6667, -0.04090, -1.2760 0.7046, -0.04120, -1.3218 0.7429, -0.03210, -1.2788 0.8333, -0.01400, -1.2674 0.9311, -0.00120, -1.2870 --------- Run Conditions: vel=113.7 ft/s Re=1.007x10^6 AOA=16.63 Flap deflection=-90.00 Totals: Cl=0.1482 Cdp=0.5837 Cm(c/4)=0.0601 Cs=-0.5169 Ch=-0.0992 Main component: Cl=0.3389 Cdp=0.0088 Cm=-0.0220 Flap component: Cl=-0.1907 Cdp=0.5749 Cm=0.0048 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.0775 0.5871, 0.07930, 0.1118 0.5501, 0.08690, 0.1021 0.5112, 0.09370, 0.1096 0.4731, 0.09830, 0.1163 0.4349, 0.10070, 0.1133 0.3960, 0.10120, 0.1335 0.3566, 0.10020, 0.0694 0.3172, 0.09790, -0.0509 0.2778, 0.09440, -0.2266 0.2393, 0.08960, -0.3841 0.2056, 0.08360, -0.5013 0.1633, 0.07610, -0.6757 0.1261, 0.06710, -0.7960 0.0900, 0.05640, -0.9810 0.0571, 0.04390, -1.1952 0.0283, 0.02940, -1.5833 0.0142, 0.01970, -1.9580 0.0081, 0.01410, -2.2519 0.0026, 0.00780, -2.2534 0.0000, 0.00000, -2.3467 0.0037, -0.00840, 0.4146 0.0112, -0.01420, 0.9380 0.0191, -0.01930, 1.0154 0.0397, -0.03030, 0.9607 0.0706, -0.04420, 0.7927 0.1037, -0.05710, 0.6530 0.1384, -0.06890, 0.4760 0.1741, -0.07950, 0.3537 0.2102, -0.08660, 0.2401 0.2472, -0.09640, 0.0834 0.2844, -0.10270, -0.0097 0.3225, -0.10690, -0.1213 0.3608, -0.10890, -0.1891 0.3991, -0.10830, -0.2318 0.4373, -0.10510, -0.1854 0.4757, -0.09890, -0.1260 0.5137, -0.09070, -0.0933 0.5514, -0.08120, 0.1662 0.5917, -0.06870, 0.1103 0.5917, -0.02380, 0.1055 0.5917, 0.02120, 0.0951 16 Flap element taps 1.0000, 0.00130, -1.2455 0.9365, 0.01390, 0.1096 0.8333, 0.03280, 0.2489 0.7436, 0.04930, 0.6754 0.7049, 0.05670, 0.9468 0.6667, 0.05450, 0.9533 0.6302, 0.03770, 0.2680 0.6083, 0.01980, -0.8098 0.6000, 0.00000, -1.1805 0.6076, -0.01900, -1.1988 0.6285, -0.03060, -1.2317 0.6667, -0.04090, -1.2873 0.7046, -0.04120, -1.3285 0.7429, -0.03210, -1.2732 0.8333, -0.01400, -1.2523 0.9311, -0.00120, -1.2661 --------- Run Conditions: vel=114.0 ft/s Re=1.008x10^6 AOA=18.07 Flap deflection=-90.00 Totals: Cl=0.2508 Cdp=0.5777 Cm(c/4)=0.0513 Cs=-0.4714 Ch=-0.1113 Main component: Cl=0.4291 Cdp=0.0497 Cm=-0.0455 Flap component: Cl=-0.1783 Cdp=0.5281 Cm=-0.0077 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1346 0.5871, 0.07930, -0.0681 0.5501, 0.08690, -0.1018 0.5112, 0.09370, -0.1022 0.4731, 0.09830, -0.0868 0.4349, 0.10070, -0.0823 0.3960, 0.10120, -0.0360 0.3566, 0.10020, -0.0735 0.3172, 0.09790, -0.0922 0.2778, 0.09440, -0.1563 0.2393, 0.08960, -0.2837 0.2056, 0.08360, -0.4330 0.1633, 0.07610, -0.6832 0.1261, 0.06710, -0.8592 0.0900, 0.05640, -1.1233 0.0571, 0.04390, -1.4455 0.0283, 0.02940, -1.9434 0.0142, 0.01970, -2.5007 0.0081, 0.01410, -3.3103 0.0026, 0.00780, -3.3637 0.0000, 0.00000, -3.8648 0.0037, -0.00840, -0.0965 0.0112, -0.01420, 0.7782 0.0191, -0.01930, 0.9711 0.0397, -0.03030, 1.0065 0.0706, -0.04420, 0.8866 0.1037, -0.05710, 0.7647 0.1384, -0.06890, 0.5828 0.1741, -0.07950, 0.4622 0.2102, -0.08660, 0.3585 0.2472, -0.09640, 0.1891 0.2844, -0.10270, 0.0902 0.3225, -0.10690, -0.0432 0.3608, -0.10890, -0.1233 0.3991, -0.10830, -0.1949 0.4373, -0.10510, -0.1694 0.4757, -0.09890, -0.1235 0.5137, -0.09070, -0.0801 0.5514, -0.08120, -0.0564 0.5917, -0.06870, -0.1007 0.5917, -0.02380, -0.1054 0.5917, 0.02120, -0.1246 16 Flap element taps 1.0000, 0.00130, -1.2054 0.9365, 0.01390, -0.0663 0.8333, 0.03280, 0.0937 0.7436, 0.04930, 0.5836 0.7049, 0.05670, 0.8903 0.6667, 0.05450, 0.9917 0.6302, 0.03770, 0.3917 0.6083, 0.01980, -0.6877 0.6000, 0.00000, -1.1263 0.6076, -0.01900, -1.1411 0.6285, -0.03060, -1.1712 0.6667, -0.04090, -1.2126 0.7046, -0.04120, -1.2673 0.7429, -0.03210, -1.2256 0.8333, -0.01400, -1.2154 0.9311, -0.00120, -1.2314 --------- Run Conditions: vel=114.3 ft/s Re=1.011x10^6 AOA=20.07 Flap deflection=-90.00 Totals: Cl=0.3319 Cdp=0.5413 Cm(c/4)=0.0373 Cs=-0.3946 Ch=-0.1186 Main component: Cl=0.4902 Cdp=0.0977 Cm=-0.0699 Flap component: Cl=-0.1583 Cdp=0.4436 Cm=-0.0172 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.3111 0.5871, 0.07930, -0.2113 0.5501, 0.08690, -0.2717 0.5112, 0.09370, -0.2883 0.4731, 0.09830, -0.2748 0.4349, 0.10070, -0.2576 0.3960, 0.10120, -0.2027 0.3566, 0.10020, -0.2376 0.3172, 0.09790, -0.2424 0.2778, 0.09440, -0.2653 0.2393, 0.08960, -0.2839 0.2056, 0.08360, -0.3278 0.1633, 0.07610, -0.5668 0.1261, 0.06710, -0.7954 0.0900, 0.05640, -1.1216 0.0571, 0.04390, -1.5183 0.0283, 0.02940, -2.1265 0.0142, 0.01970, -2.7131 0.0081, 0.01410, -4.0195 0.0026, 0.00780, -4.0384 0.0000, 0.00000, -4.8080 0.0037, -0.00840, -0.4587 0.0112, -0.01420, 0.6444 0.0191, -0.01930, 0.9169 0.0397, -0.03030, 1.0168 0.0706, -0.04420, 0.9300 0.1037, -0.05710, 0.8232 0.1384, -0.06890, 0.6445 0.1741, -0.07950, 0.5273 0.2102, -0.08660, 0.4249 0.2472, -0.09640, 0.2533 0.2844, -0.10270, 0.1511 0.3225, -0.10690, 0.0100 0.3608, -0.10890, -0.0797 0.3991, -0.10830, -0.1656 0.4373, -0.10510, -0.1577 0.4757, -0.09890, -0.1270 0.5137, -0.09070, -0.0914 0.5514, -0.08120, -0.0454 0.5917, -0.06870, -0.2630 0.5917, -0.02380, -0.2691 0.5917, 0.02120, -0.2914 16 Flap element taps 1.0000, 0.00130, -1.0753 0.9365, 0.01390, -0.2109 0.8333, 0.03280, -0.0455 0.7436, 0.04930, 0.4949 0.7049, 0.05670, 0.8256 0.6667, 0.05450, 1.0075 0.6302, 0.03770, 0.4955 0.6083, 0.01980, -0.5477 0.6000, 0.00000, -1.0087 0.6076, -0.01900, -1.0149 0.6285, -0.03060, -1.0380 0.6667, -0.04090, -1.0589 0.7046, -0.04120, -1.0759 0.7429, -0.03210, -1.0572 0.8333, -0.01400, -1.0574 0.9311, -0.00120, -1.0691 --------- Run Conditions: vel=108.7 ft/s Re=0.990x10^6 AOA=24.04 Flap deflection=-90.00 Totals: Cl=0.3455 Cdp=0.6437 Cm(c/4)=-0.0225 Cs=-0.4471 Ch=-0.1491 Main component: Cl=0.4496 Cdp=0.3439 Cm=-0.1244 Flap component: Cl=-0.1040 Cdp=0.2997 Cm=-0.0425 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.7997 0.5871, 0.07930, -0.6942 0.5501, 0.08690, -0.6907 0.5112, 0.09370, -0.7099 0.4731, 0.09830, -0.7605 0.4349, 0.10070, -0.7795 0.3960, 0.10120, -0.7715 0.3566, 0.10020, -0.7712 0.3172, 0.09790, -0.7590 0.2778, 0.09440, -0.7478 0.2393, 0.08960, -0.7430 0.2056, 0.08360, -0.7285 0.1633, 0.07610, -0.7341 0.1261, 0.06710, -0.7330 0.0900, 0.05640, -0.7238 0.0571, 0.04390, -0.7336 0.0283, 0.02940, -0.7433 0.0142, 0.01970, -0.7421 0.0081, 0.01410, -0.7471 0.0026, 0.00780, -0.7062 0.0000, 0.00000, -0.9659 0.0037, -0.00840, 0.3677 0.0112, -0.01420, 0.8554 0.0191, -0.01930, 0.9750 0.0397, -0.03030, 1.0041 0.0706, -0.04420, 0.9140 0.1037, -0.05710, 0.7984 0.1384, -0.06890, 0.6640 0.1741, -0.07950, 0.5443 0.2102, -0.08660, 0.4034 0.2472, -0.09640, 0.2573 0.2844, -0.10270, 0.1299 0.3225, -0.10690, 0.0029 0.3608, -0.10890, -0.1101 0.3991, -0.10830, -0.2027 0.4373, -0.10510, -0.2411 0.4757, -0.09890, -0.2316 0.5137, -0.09070, -0.2281 0.5514, -0.08120, -0.2002 0.5917, -0.06870, -0.7530 0.5917, -0.02380, -0.7695 0.5917, 0.02120, -0.7826 16 Flap element taps 1.0000, 0.00130, -0.9077 0.9365, 0.01390, -0.7499 0.8333, 0.03280, -0.4353 0.7436, 0.04930, 0.2300 0.7049, 0.05670, 0.6319 0.6667, 0.05450, 0.9949 0.6302, 0.03770, 0.6356 0.6083, 0.01980, -0.3560 0.6000, 0.00000, -0.8940 0.6076, -0.01900, -0.9140 0.6285, -0.03060, -0.9071 0.6667, -0.04090, -0.9041 0.7046, -0.04120, -0.9136 0.7429, -0.03210, -0.9098 0.8333, -0.01400, -0.9084 0.9311, -0.00120, -0.9120 --------- Run Conditions: vel=112.8 ft/s Re=0.994x10^6 AOA=26.99 Flap deflection=-90.00 Totals: Cl=0.4247 Cdp=0.7255 Cm(c/4)=-0.0343 Cs=-0.4537 Ch=-0.1548 Main component: Cl=0.5292 Cdp=0.4354 Cm=-0.1585 Flap component: Cl=-0.1045 Cdp=0.2901 Cm=-0.0527 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.9685 0.5871, 0.07930, -0.8697 0.5501, 0.08690, -0.8573 0.5112, 0.09370, -0.8620 0.4731, 0.09830, -0.9021 0.4349, 0.10070, -0.9301 0.3960, 0.10120, -0.9431 0.3566, 0.10020, -0.9326 0.3172, 0.09790, -0.9287 0.2778, 0.09440, -0.9177 0.2393, 0.08960, -0.9086 0.2056, 0.08360, -0.9084 0.1633, 0.07610, -0.8979 0.1261, 0.06710, -0.8981 0.0900, 0.05640, -0.8885 0.0571, 0.04390, -0.8935 0.0283, 0.02940, -0.8943 0.0142, 0.01970, -0.9044 0.0081, 0.01410, -0.9099 0.0026, 0.00780, -0.8549 0.0000, 0.00000, -0.9442 0.0037, -0.00840, 0.1444 0.0112, -0.01420, 0.7491 0.0191, -0.01930, 0.9267 0.0397, -0.03030, 1.0159 0.0706, -0.04420, 0.9554 0.1037, -0.05710, 0.8635 0.1384, -0.06890, 0.7489 0.1741, -0.07950, 0.6326 0.2102, -0.08660, 0.4846 0.2472, -0.09640, 0.3459 0.2844, -0.10270, 0.2103 0.3225, -0.10690, 0.0922 0.3608, -0.10890, -0.0433 0.3991, -0.10830, -0.1377 0.4373, -0.10510, -0.2062 0.4757, -0.09890, -0.2096 0.5137, -0.09070, -0.2337 0.5514, -0.08120, -0.2313 0.5917, -0.06870, -0.9254 0.5917, -0.02380, -0.9347 0.5917, 0.02120, -0.9553 16 Flap element taps 1.0000, 0.00130, -1.0510 0.9365, 0.01390, -0.8998 0.8333, 0.03280, -0.5699 0.7436, 0.04930, 0.1339 0.7049, 0.05670, 0.5495 0.6667, 0.05450, 0.9933 0.6302, 0.03770, 0.6974 0.6083, 0.01980, -0.3000 0.6000, 0.00000, -0.9090 0.6076, -0.01900, -0.9217 0.6285, -0.03060, -0.9196 0.6667, -0.04090, -0.9302 0.7046, -0.04120, -0.9502 0.7429, -0.03210, -0.9626 0.8333, -0.01400, -0.9790 0.9311, -0.00120, -1.0164 --------- Run Conditions: vel=113.2 ft/s Re=0.997x10^6 AOA=30.04 Flap deflection=-90.00 Totals: Cl=0.4265 Cdp=0.7807 Cm(c/4)=-0.0384 Cs=-0.4623 Ch=-0.1629 Main component: Cl=0.5474 Cdp=0.4951 Cm=-0.1745 Flap component: Cl=-0.1210 Cdp=0.2856 Cm=-0.0538 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.0299 0.5871, 0.07930, -0.9243 0.5501, 0.08690, -0.9136 0.5112, 0.09370, -0.9078 0.4731, 0.09830, -0.9422 0.4349, 0.10070, -0.9606 0.3960, 0.10120, -0.9837 0.3566, 0.10020, -0.9733 0.3172, 0.09790, -0.9691 0.2778, 0.09440, -0.9603 0.2393, 0.08960, -0.9544 0.2056, 0.08360, -0.9578 0.1633, 0.07610, -0.9433 0.1261, 0.06710, -0.9448 0.0900, 0.05640, -0.9356 0.0571, 0.04390, -0.9400 0.0283, 0.02940, -0.9385 0.0142, 0.01970, -0.9477 0.0081, 0.01410, -0.9564 0.0026, 0.00780, -0.8985 0.0000, 0.00000, -0.9651 0.0037, -0.00840, -0.0436 0.0112, -0.01420, 0.6403 0.0191, -0.01930, 0.8661 0.0397, -0.03030, 1.0111 0.0706, -0.04420, 0.9837 0.1037, -0.05710, 0.9155 0.1384, -0.06890, 0.8169 0.1741, -0.07950, 0.7084 0.2102, -0.08660, 0.5631 0.2472, -0.09640, 0.4302 0.2844, -0.10270, 0.2937 0.3225, -0.10690, 0.1774 0.3608, -0.10890, 0.0326 0.3991, -0.10830, -0.0695 0.4373, -0.10510, -0.1538 0.4757, -0.09890, -0.1711 0.5137, -0.09070, -0.2101 0.5514, -0.08120, -0.2230 0.5917, -0.06870, -0.9820 0.5917, -0.02380, -0.9932 0.5917, 0.02120, -1.0165 16 Flap element taps 1.0000, 0.00130, -1.0251 0.9365, 0.01390, -0.9379 0.8333, 0.03280, -0.6159 0.7436, 0.04930, 0.0857 0.7049, 0.05670, 0.5043 0.6667, 0.05450, 0.9778 0.6302, 0.03770, 0.7087 0.6083, 0.01980, -0.2997 0.6000, 0.00000, -0.9811 0.6076, -0.01900, -0.9932 0.6285, -0.03060, -0.9897 0.6667, -0.04090, -0.9999 0.7046, -0.04120, -1.0227 0.7429, -0.03210, -1.0073 0.8333, -0.01400, -1.0111 0.9311, -0.00120, -1.0196 --------- Run Conditions: vel=113.1 ft/s Re=0.996x10^6 AOA=35.04 Flap deflection=-90.00 Totals: Cl=0.6464 Cdp=0.8903 Cm(c/4)=-0.0688 Cs=-0.3578 Ch=-0.1581 Main component: Cl=0.6943 Cdp=0.7231 Cm=-0.2595 Flap component: Cl=-0.0479 Cdp=0.1673 Cm=-0.0694 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.4798 0.5871, 0.07930, -1.4374 0.5501, 0.08690, -1.3919 0.5112, 0.09370, -1.3701 0.4731, 0.09830, -1.3495 0.4349, 0.10070, -1.3495 0.3960, 0.10120, -1.3579 0.3566, 0.10020, -1.3408 0.3172, 0.09790, -1.3366 0.2778, 0.09440, -1.3184 0.2393, 0.08960, -1.3073 0.2056, 0.08360, -1.3047 0.1633, 0.07610, -1.2805 0.1261, 0.06710, -1.2721 0.0900, 0.05640, -1.2501 0.0571, 0.04390, -1.2459 0.0283, 0.02940, -1.2366 0.0142, 0.01970, -1.2447 0.0081, 0.01410, -1.2551 0.0026, 0.00780, -1.1863 0.0000, 0.00000, -1.2404 0.0037, -0.00840, -0.5594 0.0112, -0.01420, 0.3173 0.0191, -0.01930, 0.6588 0.0397, -0.03030, 0.9443 0.0706, -0.04420, 1.0033 0.1037, -0.05710, 0.9858 0.1384, -0.06890, 0.9275 0.1741, -0.07950, 0.8451 0.2102, -0.08660, 0.7170 0.2472, -0.09640, 0.6006 0.2844, -0.10270, 0.4707 0.3225, -0.10690, 0.3558 0.3608, -0.10890, 0.2037 0.3991, -0.10830, 0.0860 0.4373, -0.10510, -0.0282 0.4757, -0.09890, -0.0861 0.5137, -0.09070, -0.1645 0.5514, -0.08120, -0.2433 0.5917, -0.06870, -1.3771 0.5917, -0.02380, -1.3918 0.5917, 0.02120, -1.4183 16 Flap element taps 1.0000, 0.00130, -0.8623 0.9365, 0.01390, -1.0545 0.8333, 0.03280, -0.8711 0.7436, 0.04930, -0.1665 0.7049, 0.05670, 0.2367 0.6667, 0.05450, 0.8859 0.6302, 0.03770, 0.8509 0.6083, 0.01980, 0.0180 0.6000, 0.00000, -0.7504 0.6076, -0.01900, -0.7528 0.6285, -0.03060, -0.7455 0.6667, -0.04090, -0.7520 0.7046, -0.04120, -0.7635 0.7429, -0.03210, -0.7609 0.8333, -0.01400, -0.7650 0.9311, -0.00120, -0.7953 --------- Run Conditions: vel=113.1 ft/s Re=0.997x10^6 AOA=40.00 Flap deflection=-90.00 Totals: Cl=0.6491 Cdp=0.9872 Cm(c/4)=-0.0795 Cs=-0.3390 Ch=-0.1619 Main component: Cl=0.6957 Cdp=0.8355 Cm=-0.2883 Flap component: Cl=-0.0466 Cdp=0.1517 Cm=-0.0742 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.5553 0.5871, 0.07930, -1.4695 0.5501, 0.08690, -1.4636 0.5112, 0.09370, -1.4507 0.4731, 0.09830, -1.4372 0.4349, 0.10070, -1.4336 0.3960, 0.10120, -1.4466 0.3566, 0.10020, -1.4263 0.3172, 0.09790, -1.4267 0.2778, 0.09440, -1.4180 0.2393, 0.08960, -1.4057 0.2056, 0.08360, -1.4018 0.1633, 0.07610, -1.3705 0.1261, 0.06710, -1.3700 0.0900, 0.05640, -1.3458 0.0571, 0.04390, -1.3398 0.0283, 0.02940, -1.3245 0.0142, 0.01970, -1.3283 0.0081, 0.01410, -1.3403 0.0026, 0.00780, -1.2695 0.0000, 0.00000, -1.3201 0.0037, -0.00840, -0.8743 0.0112, -0.01420, 0.0713 0.0191, -0.01930, 0.4827 0.0397, -0.03030, 0.8600 0.0706, -0.04420, 0.9853 0.1037, -0.05710, 1.0115 0.1384, -0.06890, 0.9864 0.1741, -0.07950, 0.9264 0.2102, -0.08660, 0.8149 0.2472, -0.09640, 0.7172 0.2844, -0.10270, 0.5959 0.3225, -0.10690, 0.4903 0.3608, -0.10890, 0.3391 0.3991, -0.10830, 0.2161 0.4373, -0.10510, 0.0878 0.4757, -0.09890, 0.0102 0.5137, -0.09070, -0.0966 0.5514, -0.08120, -0.2069 0.5917, -0.06870, -1.4541 0.5917, -0.02380, -1.4705 0.5917, 0.02120, -1.4961 16 Flap element taps 1.0000, 0.00130, -0.8677 0.9365, 0.01390, -1.1217 0.8333, 0.03280, -0.9332 0.7436, 0.04930, -0.2296 0.7049, 0.05670, 0.1605 0.6667, 0.05450, 0.8544 0.6302, 0.03770, 0.8965 0.6083, 0.01980, 0.1075 0.6000, 0.00000, -0.7590 0.6076, -0.01900, -0.7515 0.6285, -0.03060, -0.7453 0.6667, -0.04090, -0.7504 0.7046, -0.04120, -0.7594 0.7429, -0.03210, -0.7563 0.8333, -0.01400, -0.7597 0.9311, -0.00120, -0.7923 --------- Run Conditions: vel=114.3 ft/s Re=1.006x10^6 AOA=45.08 Flap deflection=-90.00 Totals: Cl=0.5688 Cdp=1.0623 Cm(c/4)=-0.0836 Cs=-0.3474 Ch=-0.1643 Main component: Cl=0.6436 Cdp=0.9005 Cm=-0.2977 Flap component: Cl=-0.0748 Cdp=0.1618 Cm=-0.0743 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.5188 0.5871, 0.07930, -1.4015 0.5501, 0.08690, -1.4114 0.5112, 0.09370, -1.4273 0.4731, 0.09830, -1.4134 0.4349, 0.10070, -1.4073 0.3960, 0.10120, -1.4159 0.3566, 0.10020, -1.4104 0.3172, 0.09790, -1.4173 0.2778, 0.09440, -1.4151 0.2393, 0.08960, -1.4026 0.2056, 0.08360, -1.4095 0.1633, 0.07610, -1.3801 0.1261, 0.06710, -1.3823 0.0900, 0.05640, -1.3651 0.0571, 0.04390, -1.3585 0.0283, 0.02940, -1.3441 0.0142, 0.01970, -1.3497 0.0081, 0.01410, -1.3615 0.0026, 0.00780, -1.2902 0.0000, 0.00000, -1.3390 0.0037, -0.00840, -1.1058 0.0112, -0.01420, -0.1495 0.0191, -0.01930, 0.3058 0.0397, -0.03030, 0.7545 0.0706, -0.04420, 0.9401 0.1037, -0.05710, 1.0042 0.1384, -0.06890, 1.0105 0.1741, -0.07950, 0.9742 0.2102, -0.08660, 0.8834 0.2472, -0.09640, 0.8034 0.2844, -0.10270, 0.6929 0.3225, -0.10690, 0.5983 0.3608, -0.10890, 0.4513 0.3991, -0.10830, 0.3299 0.4373, -0.10510, 0.1949 0.4757, -0.09890, 0.1057 0.5137, -0.09070, -0.0183 0.5514, -0.08120, -0.1456 0.5917, -0.06870, -1.4318 0.5917, -0.02380, -1.4469 0.5917, 0.02120, -1.4740 16 Flap element taps 1.0000, 0.00130, -0.8996 0.9365, 0.01390, -1.1199 0.8333, 0.03280, -0.9364 0.7436, 0.04930, -0.2439 0.7049, 0.05670, 0.1274 0.6667, 0.05450, 0.8322 0.6302, 0.03770, 0.9111 0.6083, 0.01980, 0.1372 0.6000, 0.00000, -0.8475 0.6076, -0.01900, -0.8230 0.6285, -0.03060, -0.8130 0.6667, -0.04090, -0.8174 0.7046, -0.04120, -0.8211 0.7429, -0.03210, -0.8238 0.8333, -0.01400, -0.8276 0.9311, -0.00120, -0.8487 --------- Run Conditions: vel=113.5 ft/s Re=1.004x10^6 AOA=60.05 Flap deflection=-90.00 Totals: Cl=0.2426 Cdp=1.1609 Cm(c/4)=-0.0966 Cs=-0.3693 Ch=-0.1681 Main component: Cl=0.4001 Cdp=1.0006 Cm=-0.3051 Flap component: Cl=-0.1575 Cdp=0.1602 Cm=-0.0732 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.4112 0.5871, 0.07930, -1.2690 0.5501, 0.08690, -1.2647 0.5112, 0.09370, -1.2565 0.4731, 0.09830, -1.2538 0.4349, 0.10070, -1.2552 0.3960, 0.10120, -1.2393 0.3566, 0.10020, -1.2494 0.3172, 0.09790, -1.2529 0.2778, 0.09440, -1.2486 0.2393, 0.08960, -1.2492 0.2056, 0.08360, -1.2462 0.1633, 0.07610, -1.2526 0.1261, 0.06710, -1.2547 0.0900, 0.05640, -1.2554 0.0571, 0.04390, -1.2490 0.0283, 0.02940, -1.2442 0.0142, 0.01970, -1.2509 0.0081, 0.01410, -1.2475 0.0026, 0.00780, -1.1982 0.0000, 0.00000, -1.2520 0.0037, -0.00840, -1.3591 0.0112, -0.01420, -0.6407 0.0191, -0.01930, -0.1568 0.0397, -0.03030, 0.3969 0.0706, -0.04420, 0.7256 0.1037, -0.05710, 0.8877 0.1384, -0.06890, 0.9617 0.1741, -0.07950, 1.0004 0.2102, -0.08660, 1.0009 0.2472, -0.09640, 0.9674 0.2844, -0.10270, 0.9222 0.3225, -0.10690, 0.8492 0.3608, -0.10890, 0.7472 0.3991, -0.10830, 0.6269 0.4373, -0.10510, 0.5066 0.4757, -0.09890, 0.3903 0.5137, -0.09070, 0.2417 0.5514, -0.08120, 0.0643 0.5917, -0.06870, -1.3435 0.5917, -0.02380, -1.3570 0.5917, 0.02120, -1.3769 16 Flap element taps 1.0000, 0.00130, -0.9509 0.9365, 0.01390, -1.0960 0.8333, 0.03280, -0.8849 0.7436, 0.04930, -0.2628 0.7049, 0.05670, 0.0231 0.6667, 0.05450, 0.7436 0.6302, 0.03770, 0.9713 0.6083, 0.01980, 0.3297 0.6000, 0.00000, -1.1571 0.6076, -0.01900, -0.9542 0.6285, -0.03060, -0.9491 0.6667, -0.04090, -0.9495 0.7046, -0.04120, -0.9508 0.7429, -0.03210, -0.9591 0.8333, -0.01400, -0.9591 0.9311, -0.00120, -0.9585 --------- Run Conditions: vel=113.8 ft/s Re=1.006x10^6 AOA=70.06 Flap deflection=-90.00 Totals: Cl=-0.2179 Cdp=1.1141 Cm(c/4)=-0.0929 Cs=-0.5848 Ch=-0.1898 Main component: Cl=0.2043 Cdp=0.9085 Cm=-0.2708 Flap component: Cl=-0.4222 Cdp=0.2056 Cm=-0.0654 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.0538 0.5871, 0.07930, -0.9618 0.5501, 0.08690, -0.9570 0.5112, 0.09370, -0.9540 0.4731, 0.09830, -0.9562 0.4349, 0.10070, -0.9621 0.3960, 0.10120, -0.9461 0.3566, 0.10020, -0.9597 0.3172, 0.09790, -0.9615 0.2778, 0.09440, -0.9576 0.2393, 0.08960, -0.9569 0.2056, 0.08360, -0.9484 0.1633, 0.07610, -0.9581 0.1261, 0.06710, -0.9581 0.0900, 0.05640, -0.9565 0.0571, 0.04390, -0.9516 0.0283, 0.02940, -0.9470 0.0142, 0.01970, -0.9542 0.0081, 0.01410, -0.9468 0.0026, 0.00780, -0.9115 0.0000, 0.00000, -0.9561 0.0037, -0.00840, -1.0894 0.0112, -0.01420, -0.6448 0.0191, -0.01930, -0.2358 0.0397, -0.03030, 0.2757 0.0706, -0.04420, 0.6134 0.1037, -0.05710, 0.8019 0.1384, -0.06890, 0.8975 0.1741, -0.07950, 0.9678 0.2102, -0.08660, 1.0018 0.2472, -0.09640, 0.9952 0.2844, -0.10270, 0.9787 0.3225, -0.10690, 0.9275 0.3608, -0.10890, 0.8551 0.3991, -0.10830, 0.7506 0.4373, -0.10510, 0.6435 0.4757, -0.09890, 0.5321 0.5137, -0.09070, 0.3929 0.5514, -0.08120, 0.2225 0.5917, -0.06870, -1.0186 0.5917, -0.02380, -1.0287 0.5917, 0.02120, -1.0391 16 Flap element taps 1.0000, 0.00130, -1.5110 0.9365, 0.01390, -1.0358 0.8333, 0.03280, -0.6714 0.7436, 0.04930, -0.0981 0.7049, 0.05670, 0.1550 0.6667, 0.05450, 0.7872 0.6302, 0.03770, 0.9591 0.6083, 0.01980, 0.2187 0.6000, 0.00000, -1.7639 0.6076, -0.01900, -1.5291 0.6285, -0.03060, -1.5251 0.6667, -0.04090, -1.5263 0.7046, -0.04120, -1.5306 0.7429, -0.03210, -1.5352 0.8333, -0.01400, -1.5385 0.9311, -0.00120, -1.5294 --------- Run Conditions: vel=113.5 ft/s Re=1.006x10^6 AOA=80.05 Flap deflection=-90.00 Totals: Cl=-0.3940 Cdp=1.1215 Cm(c/4)=-0.1165 Cs=-0.5818 Ch=-0.1950 Main component: Cl=0.0594 Cdp=0.9756 Cm=-0.2965 Flap component: Cl=-0.4533 Cdp=0.1459 Cm=-0.0792 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.2104 0.5871, 0.07930, -1.0560 0.5501, 0.08690, -1.0568 0.5112, 0.09370, -1.0549 0.4731, 0.09830, -1.0542 0.4349, 0.10070, -1.0642 0.3960, 0.10120, -1.0420 0.3566, 0.10020, -1.0628 0.3172, 0.09790, -1.0592 0.2778, 0.09440, -1.0560 0.2393, 0.08960, -1.0551 0.2056, 0.08360, -1.0394 0.1633, 0.07610, -1.0527 0.1261, 0.06710, -1.0470 0.0900, 0.05640, -1.0499 0.0571, 0.04390, -1.0416 0.0283, 0.02940, -1.0341 0.0142, 0.01970, -1.0401 0.0081, 0.01410, -1.0294 0.0026, 0.00780, -0.9940 0.0000, 0.00000, -1.0436 0.0037, -0.00840, -1.1100 0.0112, -0.01420, -0.9182 0.0191, -0.01930, -0.5406 0.0397, -0.03030, -0.0087 0.0706, -0.04420, 0.3786 0.1037, -0.05710, 0.6108 0.1384, -0.06890, 0.7484 0.1741, -0.07950, 0.8658 0.2102, -0.08660, 0.9475 0.2472, -0.09640, 0.9797 0.2844, -0.10270, 1.0077 0.3225, -0.10690, 0.9914 0.3608, -0.10890, 0.9571 0.3991, -0.10830, 0.8794 0.4373, -0.10510, 0.7917 0.4757, -0.09890, 0.6807 0.5137, -0.09070, 0.5297 0.5514, -0.08120, 0.3279 0.5917, -0.06870, -1.1431 0.5917, -0.02380, -1.1529 0.5917, 0.02120, -1.1634 16 Flap element taps 1.0000, 0.00130, -1.6166 0.9365, 0.01390, -1.1404 0.8333, 0.03280, -0.7854 0.7436, 0.04930, -0.2530 0.7049, 0.05670, -0.0903 0.6667, 0.05450, 0.6162 0.6302, 0.03770, 1.0013 0.6083, 0.01980, 0.5243 0.6000, 0.00000, -1.6114 0.6076, -0.01900, -1.6442 0.6285, -0.03060, -1.6467 0.6667, -0.04090, -1.6419 0.7046, -0.04120, -1.6461 0.7429, -0.03210, -1.6547 0.8333, -0.01400, -1.6636 0.9311, -0.00120, -1.6553 --------- Run Conditions: vel=113.2 ft/s Re=1.005x10^6 AOA=90.05 Flap deflection=-90.00 Totals: Cl=-0.5509 Cdp=1.0767 Cm(c/4)=-0.1396 Cs=-0.5499 Ch=-0.1870 Main component: Cl=-0.1031 Cdp=0.9906 Cm=-0.3138 Flap component: Cl=-0.4478 Cdp=0.0861 Cm=-0.0951 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.3486 0.5871, 0.07930, -1.1379 0.5501, 0.08690, -1.1408 0.5112, 0.09370, -1.1470 0.4731, 0.09830, -1.1552 0.4349, 0.10070, -1.1590 0.3960, 0.10120, -1.1251 0.3566, 0.10020, -1.1492 0.3172, 0.09790, -1.1469 0.2778, 0.09440, -1.1427 0.2393, 0.08960, -1.1380 0.2056, 0.08360, -1.1142 0.1633, 0.07610, -1.1331 0.1261, 0.06710, -1.1263 0.0900, 0.05640, -1.1313 0.0571, 0.04390, -1.1161 0.0283, 0.02940, -1.1051 0.0142, 0.01970, -1.1073 0.0081, 0.01410, -1.0896 0.0026, 0.00780, -1.0575 0.0000, 0.00000, -1.1071 0.0037, -0.00840, -1.1184 0.0112, -0.01420, -1.1133 0.0191, -0.01930, -0.7952 0.0397, -0.03030, -0.2823 0.0706, -0.04420, 0.1257 0.1037, -0.05710, 0.3845 0.1384, -0.06890, 0.5500 0.1741, -0.07950, 0.7037 0.2102, -0.08660, 0.8298 0.2472, -0.09640, 0.8973 0.2844, -0.10270, 0.9703 0.3225, -0.10690, 0.9905 0.3608, -0.10890, 1.0000 0.3991, -0.10830, 0.9574 0.4373, -0.10510, 0.9040 0.4757, -0.09890, 0.8066 0.5137, -0.09070, 0.6609 0.5514, -0.08120, 0.4363 0.5917, -0.06870, -1.2724 0.5917, -0.02380, -1.2878 0.5917, 0.02120, -1.2933 16 Flap element taps 1.0000, 0.00130, -1.6408 0.9365, 0.01390, -1.2329 0.8333, 0.03280, -0.9092 0.7436, 0.04930, -0.4409 0.7049, 0.05670, -0.4208 0.6667, 0.05450, 0.3503 0.6302, 0.03770, 0.9774 0.6083, 0.01980, 0.8190 0.6000, 0.00000, -1.0702 0.6076, -0.01900, -1.7018 0.6285, -0.03060, -1.7086 0.6667, -0.04090, -1.6970 0.7046, -0.04120, -1.6955 0.7429, -0.03210, -1.7037 0.8333, -0.01400, -1.7375 0.9311, -0.00120, -1.7706 --------- Run Conditions: vel=112.6 ft/s Re=1.002x10^6 AOA=120.06 Flap deflection=-90.00 Totals: Cl=-0.1204 Cdp=1.0293 Cm(c/4)=-0.1069 Cs=0.4114 Ch=0.0981 Main component: Cl=-0.4942 Cdp=0.7590 Cm=-0.3181 Flap component: Cl=0.3738 Cdp=0.2703 Cm=-0.0265 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.2550 0.5871, 0.07930, -1.3372 0.5501, 0.08690, -1.3700 0.5112, 0.09370, -1.3890 0.4731, 0.09830, -1.4203 0.4349, 0.10070, -1.4520 0.3960, 0.10120, -1.4230 0.3566, 0.10020, -1.4640 0.3172, 0.09790, -1.4584 0.2778, 0.09440, -1.4540 0.2393, 0.08960, -1.4537 0.2056, 0.08360, -1.4236 0.1633, 0.07610, -1.4711 0.1261, 0.06710, -1.4722 0.0900, 0.05640, -1.4940 0.0571, 0.04390, -1.4695 0.0283, 0.02940, -1.4302 0.0142, 0.01970, -1.4070 0.0081, 0.01410, -1.3731 0.0026, 0.00780, -1.3362 0.0000, 0.00000, -1.3867 0.0037, -0.00840, -1.3661 0.0112, -0.01420, -1.4425 0.0191, -0.01930, -1.4497 0.0397, -0.03030, -1.1704 0.0706, -0.04420, -0.8288 0.1037, -0.05710, -0.5794 0.1384, -0.06890, -0.3973 0.1741, -0.07950, -0.1892 0.2102, -0.08660, 0.0162 0.2472, -0.09640, 0.1575 0.2844, -0.10270, 0.3531 0.3225, -0.10690, 0.4970 0.3608, -0.10890, 0.6685 0.3991, -0.10830, 0.7954 0.4373, -0.10510, 0.9276 0.4757, -0.09890, 0.9951 0.5137, -0.09070, 0.9835 0.5514, -0.08120, 0.8266 0.5917, -0.06870, -1.7185 0.5917, -0.02380, -1.7818 0.5917, 0.02120, -1.9557 16 Flap element taps 1.0000, 0.00130, -0.4833 0.9365, 0.01390, -0.9119 0.8333, 0.03280, -1.1724 0.7436, 0.04930, -1.1699 0.7049, 0.05670, -2.2063 0.6667, 0.05450, -1.6740 0.6302, 0.03770, -0.8670 0.6083, 0.01980, -0.6120 0.6000, 0.00000, 0.5760 0.6076, -0.01900, 0.9291 0.6285, -0.03060, 0.4682 0.6667, -0.04090, -0.0908 0.7046, -0.04120, -0.4275 0.7429, -0.03210, 0.0182 0.8333, -0.01400, 0.0604 0.9311, -0.00120, 0.0020 --------- Run Conditions: vel=112.8 ft/s Re=1.010x10^6 AOA=150.07 Flap deflection=-90.00 Totals: Cl=0.1030 Cdp=0.7191 Cm(c/4)=-0.0228 Cs=0.6746 Ch=0.1225 Main component: Cl=-0.2784 Cdp=0.1639 Cm=-0.1462 Flap component: Cl=0.3814 Cdp=0.5552 Cm=0.0560 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.1310 0.5871, 0.07930, -1.0810 0.5501, 0.08690, -1.0795 0.5112, 0.09370, -1.0843 0.4731, 0.09830, -1.0961 0.4349, 0.10070, -1.1066 0.3960, 0.10120, -1.0997 0.3566, 0.10020, -1.0907 0.3172, 0.09790, -1.0975 0.2778, 0.09440, -1.1008 0.2393, 0.08960, -1.1017 0.2056, 0.08360, -1.1066 0.1633, 0.07610, -1.1076 0.1261, 0.06710, -1.1096 0.0900, 0.05640, -1.1188 0.0571, 0.04390, -1.1194 0.0283, 0.02940, -1.1257 0.0142, 0.01970, -1.1265 0.0081, 0.01410, -1.1111 0.0026, 0.00780, -1.0575 0.0000, 0.00000, -1.1069 0.0037, -0.00840, -1.1001 0.0112, -0.01420, -1.1101 0.0191, -0.01930, -1.1137 0.0397, -0.03030, -1.1600 0.0706, -0.04420, -1.2112 0.1037, -0.05710, -1.1958 0.1384, -0.06890, -1.1573 0.1741, -0.07950, -1.0886 0.2102, -0.08660, -1.0269 0.2472, -0.09640, -0.9604 0.2844, -0.10270, -0.8290 0.3225, -0.10690, -0.6721 0.3608, -0.10890, -0.4943 0.3991, -0.10830, -0.2323 0.4373, -0.10510, 0.0777 0.4757, -0.09890, 0.4402 0.5137, -0.09070, 0.7784 0.5514, -0.08120, 0.9882 0.5917, -0.06870, -1.4391 0.5917, -0.02380, -1.5842 0.5917, 0.02120, -1.6112 16 Flap element taps 1.0000, 0.00130, -0.6775 0.9365, 0.01390, -0.9105 0.8333, 0.03280, -1.2166 0.7436, 0.04930, -1.3078 0.7049, 0.05670, -1.3085 0.6667, 0.05450, -1.2959 0.6302, 0.03770, -1.2758 0.6083, 0.01980, -1.2725 0.6000, 0.00000, -1.2724 0.6076, -0.01900, -0.8511 0.6285, -0.03060, 0.6873 0.6667, -0.04090, 0.9970 0.7046, -0.04120, 0.9594 0.7429, -0.03210, 0.8715 0.8333, -0.01400, 0.7062 0.9311, -0.00120, 0.4226 --------- Run Conditions: vel=112.5 ft/s Re=1.009x10^6 AOA=180.07 Flap deflection=-90.00 Totals: Cl=-0.0503 Cdp=0.6477 Cm(c/4)=0.0451 Cs=0.6478 Ch=0.0226 Main component: Cl=-0.1158 Cdp=-0.0337 Cm=-0.0176 Flap component: Cl=0.0655 Cdp=0.6814 Cm=0.0503 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.5170 0.5871, 0.07930, -1.3500 0.5501, 0.08690, -1.3246 0.5112, 0.09370, -1.3438 0.4731, 0.09830, -1.3598 0.4349, 0.10070, -1.3934 0.3960, 0.10120, -1.4341 0.3566, 0.10020, -1.4147 0.3172, 0.09790, -1.4564 0.2778, 0.09440, -1.4838 0.2393, 0.08960, -1.4781 0.2056, 0.08360, -1.4619 0.1633, 0.07610, -1.3616 0.1261, 0.06710, -1.2998 0.0900, 0.05640, -1.2465 0.0571, 0.04390, -1.3159 0.0283, 0.02940, -1.4376 0.0142, 0.01970, -1.5462 0.0081, 0.01410, -1.6423 0.0026, 0.00780, -1.7120 0.0000, 0.00000, -2.0821 0.0037, -0.00840, -1.6381 0.0112, -0.01420, -1.2733 0.0191, -0.01930, -1.1063 0.0397, -0.03030, -0.9217 0.0706, -0.04420, -0.8561 0.1037, -0.05710, -0.8341 0.1384, -0.06890, -0.8597 0.1741, -0.07950, -0.9224 0.2102, -0.08660, -1.0491 0.2472, -0.09640, -1.1499 0.2844, -0.10270, -1.2515 0.3225, -0.10690, -1.3053 0.3608, -0.10890, -1.4024 0.3991, -0.10830, -1.4200 0.4373, -0.10510, -1.4381 0.4757, -0.09890, -1.4261 0.5137, -0.09070, -1.3577 0.5514, -0.08120, -1.3408 0.5917, -0.06870, -1.4232 0.5917, -0.02380, -1.4231 0.5917, 0.02120, -1.4123 16 Flap element taps 1.0000, 0.00130, -1.1562 0.9365, 0.01390, -1.1835 0.8333, 0.03280, -1.2435 0.7436, 0.04930, -1.2619 0.7049, 0.05670, -1.2395 0.6667, 0.05450, -1.2111 0.6302, 0.03770, -1.1881 0.6083, 0.01980, -1.1746 0.6000, 0.00000, -1.1642 0.6076, -0.01900, -1.2379 0.6285, -0.03060, -0.2757 0.6667, -0.04090, 0.4629 0.7046, -0.04120, 0.7619 0.7429, -0.03210, 0.9867 0.8333, -0.01400, 0.9878 0.9311, -0.00120, 0.7413 --------- Run Conditions: vel=111.8 ft/s Re=1.004x10^6 AOA=210.07 Flap deflection=-90.00 Totals: Cl=0.0047 Cdp=0.5756 Cm(c/4)=0.0713 Cs=0.4957 Ch=-0.0640 Main component: Cl=0.1765 Cdp=0.1301 Cm=0.0993 Flap component: Cl=-0.1718 Cdp=0.4454 Cm=0.0451 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.0470 0.5871, 0.07930, -1.0140 0.5501, 0.08690, -0.9355 0.5112, 0.09370, -0.7524 0.4731, 0.09830, -0.3082 0.4349, 0.10070, 0.1384 0.3960, 0.10120, 0.2312 0.3566, 0.10020, 0.1717 0.3172, 0.09790, -0.0690 0.2778, 0.09440, -0.3206 0.2393, 0.08960, -0.5551 0.2056, 0.08360, -0.8264 0.1633, 0.07610, -0.9812 0.1261, 0.06710, -1.2140 0.0900, 0.05640, -1.4184 0.0571, 0.04390, -1.6819 0.0283, 0.02940, -1.8166 0.0142, 0.01970, -1.6425 0.0081, 0.01410, -1.3770 0.0026, 0.00780, -1.0014 0.0000, 0.00000, -1.0207 0.0037, -0.00840, -1.0261 0.0112, -0.01420, -1.0364 0.0191, -0.01930, -1.0378 0.0397, -0.03030, -1.0586 0.0706, -0.04420, -1.0847 0.1037, -0.05710, -1.0649 0.1384, -0.06890, -1.0166 0.1741, -0.07950, -1.0154 0.2102, -0.08660, -1.0616 0.2472, -0.09640, -1.0386 0.2844, -0.10270, -1.0557 0.3225, -0.10690, -1.0156 0.3608, -0.10890, -1.0551 0.3991, -0.10830, -1.0234 0.4373, -0.10510, -1.0411 0.4757, -0.09890, -1.0428 0.5137, -0.09070, -1.0253 0.5514, -0.08120, -1.0278 0.5917, -0.06870, -1.0547 0.5917, -0.02380, -1.0580 0.5917, 0.02120, -1.0393 16 Flap element taps 1.0000, 0.00130, -0.7549 0.9365, 0.01390, -0.8314 0.8333, 0.03280, -0.7743 0.7436, 0.04930, -1.0078 0.7049, 0.05670, -1.0750 0.6667, 0.05450, -1.0803 0.6302, 0.03770, -1.0149 0.6083, 0.01980, -0.9697 0.6000, 0.00000, -0.9559 0.6076, -0.01900, -0.9598 0.6285, -0.03060, -0.9590 0.6667, -0.04090, -0.5259 0.7046, -0.04120, -0.2686 0.7429, -0.03210, 0.6039 0.8333, -0.01400, 0.9390 0.9311, -0.00120, 1.0036 --------- Run Conditions: vel=109.0 ft/s Re=0.980x10^6 AOA=240.02 Flap deflection=-90.00 Totals: Cl=0.3274 Cdp=1.0700 Cm(c/4)=0.1749 Cs=0.2511 Ch=-0.0106 Main component: Cl=0.5056 Cdp=0.8629 Cm=0.3790 Flap component: Cl=-0.1782 Cdp=0.2071 Cm=0.0685 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.4086 0.5871, 0.07930, 0.8290 0.5501, 0.08690, 0.9930 0.5112, 0.09370, 1.0034 0.4731, 0.09830, 0.9602 0.4349, 0.10070, 0.8638 0.3960, 0.10120, 0.7063 0.3566, 0.10020, 0.6750 0.3172, 0.09790, 0.5345 0.2778, 0.09440, 0.3876 0.2393, 0.08960, 0.2131 0.2056, 0.08360, -0.0375 0.1633, 0.07610, -0.1814 0.1261, 0.06710, -0.4691 0.0900, 0.05640, -0.7440 0.0571, 0.04390, -1.1413 0.0283, 0.02940, -1.4298 0.0142, 0.01970, -1.3494 0.0081, 0.01410, -1.3705 0.0026, 0.00780, -1.2582 0.0000, 0.00000, -1.3223 0.0037, -0.00840, -1.3384 0.0112, -0.01420, -1.3508 0.0191, -0.01930, -1.3560 0.0397, -0.03030, -1.3702 0.0706, -0.04420, -1.4217 0.1037, -0.05710, -1.4304 0.1384, -0.06890, -1.3794 0.1741, -0.07950, -1.3865 0.2102, -0.08660, -1.4585 0.2472, -0.09640, -1.4510 0.2844, -0.10270, -1.4942 0.3225, -0.10690, -1.4544 0.3608, -0.10890, -1.5116 0.3991, -0.10830, -1.4712 0.4373, -0.10510, -1.4977 0.4757, -0.09890, -1.4764 0.5137, -0.09070, -1.4458 0.5514, -0.08120, -1.4293 0.5917, -0.06870, -1.4321 0.5917, -0.02380, -1.4447 0.5917, 0.02120, -1.4192 16 Flap element taps 1.0000, 0.00130, 0.5238 0.9365, 0.01390, -0.3166 0.8333, 0.03280, -0.3318 0.7436, 0.04930, -1.3281 0.7049, 0.05670, -2.5788 0.6667, 0.05450, -2.3324 0.6302, 0.03770, -1.0877 0.6083, 0.01980, -1.0992 0.6000, 0.00000, -1.0758 0.6076, -0.01900, -1.1300 0.6285, -0.03060, -1.3108 0.6667, -0.04090, -1.5476 0.7046, -0.04120, -1.7938 0.7429, -0.03210, -0.2820 0.8333, -0.01400, 0.2821 0.9311, -0.00120, 0.6171 --------- Run Conditions: vel=110.4 ft/s Re=0.995x10^6 AOA=269.08 Flap deflection=-90.00 Totals: Cl=0.5521 Cdp=1.1255 Cm(c/4)=0.1705 Cs=-0.5340 Ch=0.1493 Main component: Cl=0.0789 Cdp=1.0509 Cm=0.3592 Flap component: Cl=0.4733 Cdp=0.0746 Cm=0.0948 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.1598 0.5871, 0.07930, 0.5015 0.5501, 0.08690, 0.7441 0.5112, 0.09370, 0.8454 0.4731, 0.09830, 0.9304 0.4349, 0.10070, 0.9694 0.3960, 0.10120, 0.9244 0.3566, 0.10020, 1.0251 0.3172, 0.09790, 0.9903 0.2778, 0.09440, 0.9545 0.2393, 0.08960, 0.8810 0.2056, 0.08360, 0.7204 0.1633, 0.07610, 0.6708 0.1261, 0.06710, 0.4400 0.0900, 0.05640, 0.2124 0.0571, 0.04390, -0.2176 0.0283, 0.02940, -0.7838 0.0142, 0.01970, -1.1906 0.0081, 0.01410, -1.2733 0.0026, 0.00780, -1.0438 0.0000, 0.00000, -1.0809 0.0037, -0.00840, -1.0879 0.0112, -0.01420, -1.0940 0.0191, -0.01930, -1.0864 0.0397, -0.03030, -1.0878 0.0706, -0.04420, -1.1309 0.1037, -0.05710, -1.1329 0.1384, -0.06890, -1.0718 0.1741, -0.07950, -1.0790 0.2102, -0.08660, -1.1614 0.2472, -0.09640, -1.1299 0.2844, -0.10270, -1.1670 0.3225, -0.10690, -1.1072 0.3608, -0.10890, -1.1696 0.3991, -0.10830, -1.1330 0.4373, -0.10510, -1.1681 0.4757, -0.09890, -1.1708 0.5137, -0.09070, -1.1594 0.5514, -0.08120, -1.1564 0.5917, -0.06870, -1.1653 0.5917, -0.02380, -1.1922 0.5917, 0.02120, -1.1734 16 Flap element taps 1.0000, 0.00130, -1.6799 0.9365, 0.01390, 0.8666 0.8333, 0.03280, 0.1099 0.7436, 0.04930, -0.8226 0.7049, 0.05670, -1.4946 0.6667, 0.05450, -1.7402 0.6302, 0.03770, -1.6713 0.6083, 0.01980, -1.6817 0.6000, 0.00000, -1.6432 0.6076, -0.01900, -1.7325 0.6285, -0.03060, -1.7729 0.6667, -0.04090, -1.8343 0.7046, -0.04120, -1.8315 0.7429, -0.03210, -1.7734 0.8333, -0.01400, -1.7171 0.9311, -0.00120, -1.7076