S809 VENTED AILERON MODEL, 18 IN CHORD --------- Run Conditions: vel=107.8 ft/s Re=1.007x10^6 AOA=-6.03 Flap deflection=-60.00 Totals: Cl=-0.5175 Cdp=0.4564 Cm(c/4)=0.1633 Cs=-0.3995 Ch=0.0311 Main component: Cl=-0.2352 Cdp=-0.0024 Cm=0.0298 Flap component: Cl=-0.2823 Cdp=0.4588 Cm=0.2742 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.0696 0.5871, 0.07930, 0.1344 0.5501, 0.08690, 0.0843 0.5112, 0.09370, -0.0442 0.4731, 0.09830, -0.1340 0.4349, 0.10070, -0.1498 0.3960, 0.10120, -0.0774 0.3566, 0.10020, -0.1127 0.3172, 0.09790, -0.0686 0.2778, 0.09440, -0.0511 0.2393, 0.08960, -0.0158 0.2056, 0.08360, 0.0832 0.1633, 0.07610, 0.1039 0.1261, 0.06710, 0.2401 0.0900, 0.05640, 0.3196 0.0571, 0.04390, 0.5224 0.0283, 0.02940, 0.7722 0.0142, 0.01970, 0.9512 0.0081, 0.01410, 1.0364 0.0026, 0.00780, 0.7687 0.0000, 0.00000, -0.0632 0.0037, -0.00840, -0.8271 0.0112, -0.01420, -1.0220 0.0191, -0.01930, -0.5873 0.0397, -0.03030, -0.5147 0.0706, -0.04420, -0.4871 0.1037, -0.05710, -0.4581 0.1384, -0.06890, -0.5431 0.1741, -0.07950, -0.5471 0.2102, -0.08660, -0.5182 0.2472, -0.09640, -0.5429 0.2844, -0.10270, -0.4615 0.3225, -0.10690, -0.3933 0.3608, -0.10890, -0.2116 0.3991, -0.10830, -0.0314 0.4373, -0.10510, 0.0763 0.4757, -0.09890, 0.0845 0.5137, -0.09070, 0.0801 0.5514, -0.08120, 0.0677 0.5917, -0.06870, -0.0094 0.5917, -0.02380, 0.0574 0.5917, 0.02120, 0.0598 16 Flap element taps 1.0000, 0.00130, -1.0279 0.9365, 0.01390, 0.5728 0.8333, 0.03280, 0.9885 0.7436, 0.04930, 0.5160 0.7049, 0.05670, -0.1783 0.6667, 0.05450, -0.4557 0.6302, 0.03770, -0.3594 0.6083, 0.01980, -0.8795 0.6000, 0.00000, -1.4295 0.6076, -0.01900, -1.2553 0.6285, -0.03060, -1.1475 0.6667, -0.04090, -1.1238 0.7046, -0.04120, -1.1714 0.7429, -0.03210, -1.1261 0.8333, -0.01400, -1.1009 0.9311, -0.00120, -1.0540 --------- Run Conditions: vel=108.5 ft/s Re=1.011x10^6 AOA=0.02 Flap deflection=-60.00 Totals: Cl=-0.2543 Cdp=0.4038 Cm(c/4)=0.1761 Cs=-0.4038 Ch=0.0081 Main component: Cl=0.0705 Cdp=-0.0314 Cm=-0.0276 Flap component: Cl=-0.3249 Cdp=0.4352 Cm=0.2672 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.2397 0.5871, 0.07930, 0.1859 0.5501, 0.08690, 0.0889 0.5112, 0.09370, -0.0670 0.4731, 0.09830, -0.2052 0.4349, 0.10070, -0.2624 0.3960, 0.10120, -0.2113 0.3566, 0.10020, -0.2939 0.3172, 0.09790, -0.2824 0.2778, 0.09440, -0.3019 0.2393, 0.08960, -0.2987 0.2056, 0.08360, -0.2254 0.1633, 0.07610, -0.2628 0.1261, 0.06710, -0.1620 0.0900, 0.05640, -0.1639 0.0571, 0.04390, -0.0237 0.0283, 0.02940, 0.1851 0.0142, 0.01970, 0.3901 0.0081, 0.01410, 0.5800 0.0026, 0.00780, 0.7162 0.0000, 0.00000, 0.9860 0.0037, -0.00840, 0.6463 0.0112, -0.01420, 0.3089 0.0191, -0.01930, 0.3411 0.0397, -0.03030, 0.1855 0.0706, -0.04420, 0.0637 0.1037, -0.05710, -0.0029 0.1384, -0.06890, -0.1718 0.1741, -0.07950, -0.2324 0.2102, -0.08660, -0.2400 0.2472, -0.09640, -0.3282 0.2844, -0.10270, -0.2999 0.3225, -0.10690, -0.3145 0.3608, -0.10890, -0.2028 0.3991, -0.10830, -0.0769 0.4373, -0.10510, 0.1604 0.4757, -0.09890, 0.2363 0.5137, -0.09070, 0.2359 0.5514, -0.08120, 0.2285 0.5917, -0.06870, 0.2336 0.5917, -0.02380, 0.2298 0.5917, 0.02120, 0.2281 16 Flap element taps 1.0000, 0.00130, -1.0234 0.9365, 0.01390, 0.5472 0.8333, 0.03280, 0.9856 0.7436, 0.04930, 0.3019 0.7049, 0.05670, 0.0216 0.6667, 0.05450, -0.0915 0.6302, 0.03770, -0.0077 0.6083, 0.01980, -0.6814 0.6000, 0.00000, -1.7968 0.6076, -0.01900, -1.2481 0.6285, -0.03060, -1.1034 0.6667, -0.04090, -1.0763 0.7046, -0.04120, -1.1214 0.7429, -0.03210, -1.0820 0.8333, -0.01400, -1.0659 0.9311, -0.00120, -1.0350 --------- Run Conditions: vel=109.9 ft/s Re=1.021x10^6 AOA=3.05 Flap deflection=-60.00 Totals: Cl=-0.1724 Cdp=0.3367 Cm(c/4)=0.1295 Cs=-0.3454 Ch=-0.0636 Main component: Cl=0.0691 Cdp=-0.0373 Cm=-0.0038 Flap component: Cl=-0.2415 Cdp=0.3740 Cm=0.1719 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.2599 0.5871, 0.07930, 0.2584 0.5501, 0.08690, 0.2469 0.5112, 0.09370, 0.2091 0.4731, 0.09830, 0.0454 0.4349, 0.10070, -0.0879 0.3960, 0.10120, -0.0848 0.3566, 0.10020, -0.2270 0.3172, 0.09790, -0.2557 0.2778, 0.09440, -0.3095 0.2393, 0.08960, -0.3333 0.2056, 0.08360, -0.2761 0.1633, 0.07610, -0.3596 0.1261, 0.06710, -0.2850 0.0900, 0.05640, -0.3336 0.0571, 0.04390, -0.2431 0.0283, 0.02940, -0.0915 0.0142, 0.01970, 0.0680 0.0081, 0.01410, 0.2284 0.0026, 0.00780, 0.4002 0.0000, 0.00000, 0.9048 0.0037, -0.00840, 0.8847 0.0112, -0.01420, 0.6133 0.0191, -0.01930, 0.5766 0.0397, -0.03030, 0.3783 0.0706, -0.04420, 0.2169 0.1037, -0.05710, 0.1248 0.1384, -0.06890, -0.0833 0.1741, -0.07950, -0.1681 0.2102, -0.08660, -0.1881 0.2472, -0.09640, -0.3145 0.2844, -0.10270, -0.3149 0.3225, -0.10690, -0.3809 0.3608, -0.10890, -0.3134 0.3991, -0.10830, -0.2639 0.4373, -0.10510, -0.0481 0.4757, -0.09890, 0.1601 0.5137, -0.09070, 0.2295 0.5514, -0.08120, 0.2311 0.5917, -0.06870, 0.2321 0.5917, -0.02380, 0.2420 0.5917, 0.02120, 0.2431 16 Flap element taps 1.0000, 0.00130, -0.9240 0.9365, 0.01390, 0.2454 0.8333, 0.03280, 0.3009 0.7436, 0.04930, 0.2452 0.7049, 0.05670, 0.0942 0.6667, 0.05450, 0.2307 0.6302, 0.03770, 0.8870 0.6083, 0.01980, 0.3341 0.6000, 0.00000, -1.2817 0.6076, -0.01900, -0.9777 0.6285, -0.03060, -0.9370 0.6667, -0.04090, -0.9149 0.7046, -0.04120, -0.9356 0.7429, -0.03210, -0.9277 0.8333, -0.01400, -0.9302 0.9311, -0.00120, -0.9049 --------- Run Conditions: vel=108.7 ft/s Re=1.007x10^6 AOA=6.06 Flap deflection=-60.00 Totals: Cl=-0.2274 Cdp=0.3862 Cm(c/4)=0.1555 Cs=-0.4081 Ch=-0.0835 Main component: Cl=0.0651 Cdp=-0.0399 Cm=0.0126 Flap component: Cl=-0.2925 Cdp=0.4261 Cm=0.1892 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.2658 0.5871, 0.07930, 0.2670 0.5501, 0.08690, 0.2563 0.5112, 0.09370, 0.2491 0.4731, 0.09830, 0.1360 0.4349, 0.10070, -0.0030 0.3960, 0.10120, -0.0050 0.3566, 0.10020, -0.1848 0.3172, 0.09790, -0.2334 0.2778, 0.09440, -0.3069 0.2393, 0.08960, -0.3456 0.2056, 0.08360, -0.2929 0.1633, 0.07610, -0.4157 0.1261, 0.06710, -0.3571 0.0900, 0.05640, -0.4453 0.0571, 0.04390, -0.3962 0.0283, 0.02940, -0.2989 0.0142, 0.01970, -0.1894 0.0081, 0.01410, -0.0746 0.0026, 0.00780, 0.1077 0.0000, 0.00000, 0.6872 0.0037, -0.00840, 0.9688 0.0112, -0.01420, 0.7746 0.0191, -0.01930, 0.7114 0.0397, -0.03030, 0.4967 0.0706, -0.04420, 0.3171 0.1037, -0.05710, 0.2092 0.1384, -0.06890, -0.0299 0.1741, -0.07950, -0.1330 0.2102, -0.08660, -0.1560 0.2472, -0.09640, -0.3109 0.2844, -0.10270, -0.3302 0.3225, -0.10690, -0.4363 0.3608, -0.10890, -0.3974 0.3991, -0.10830, -0.4105 0.4373, -0.10510, -0.2489 0.4757, -0.09890, -0.0668 0.5137, -0.09070, 0.1026 0.5514, -0.08120, 0.2050 0.5917, -0.06870, 0.2438 0.5917, -0.02380, 0.2580 0.5917, 0.02120, 0.2530 16 Flap element taps 1.0000, 0.00130, -1.1243 0.9365, 0.01390, 0.1641 0.8333, 0.03280, 0.3146 0.7436, 0.04930, 0.2682 0.7049, 0.05670, 0.1185 0.6667, 0.05450, 0.6715 0.6302, 0.03770, 0.9829 0.6083, 0.01980, 0.2345 0.6000, 0.00000, -1.1809 0.6076, -0.01900, -1.0072 0.6285, -0.03060, -1.0409 0.6667, -0.04090, -1.0427 0.7046, -0.04120, -1.0847 0.7429, -0.03210, -1.0890 0.8333, -0.01400, -1.1000 0.9311, -0.00120, -1.0944 --------- Run Conditions: vel=108.7 ft/s Re=1.005x10^6 AOA=9.03 Flap deflection=-60.00 Totals: Cl=-0.1563 Cdp=0.3823 Cm(c/4)=0.1657 Cs=-0.4021 Ch=-0.0918 Main component: Cl=0.1555 Cdp=-0.0290 Cm=0.0034 Flap component: Cl=-0.3118 Cdp=0.4114 Cm=0.1859 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.2082 0.5871, 0.07930, 0.2077 0.5501, 0.08690, 0.2019 0.5112, 0.09370, 0.2029 0.4731, 0.09830, 0.1428 0.4349, 0.10070, 0.0330 0.3960, 0.10120, 0.0261 0.3566, 0.10020, -0.1899 0.3172, 0.09790, -0.2649 0.2778, 0.09440, -0.3627 0.2393, 0.08960, -0.4244 0.2056, 0.08360, -0.3853 0.1633, 0.07610, -0.5527 0.1261, 0.06710, -0.5201 0.0900, 0.05640, -0.6669 0.0571, 0.04390, -0.6834 0.0283, 0.02940, -0.6888 0.0142, 0.01970, -0.6919 0.0081, 0.01410, -0.6506 0.0026, 0.00780, -0.4156 0.0000, 0.00000, 0.0311 0.0037, -0.00840, 0.9801 0.0112, -0.01420, 0.9551 0.0191, -0.01930, 0.8825 0.0397, -0.03030, 0.6765 0.0706, -0.04420, 0.4877 0.1037, -0.05710, 0.3651 0.1384, -0.06890, 0.1021 0.1741, -0.07950, -0.0135 0.2102, -0.08660, -0.0395 0.2472, -0.09640, -0.2186 0.2844, -0.10270, -0.2511 0.3225, -0.10690, -0.3916 0.3608, -0.10890, -0.3667 0.3991, -0.10830, -0.4204 0.4373, -0.10510, -0.2873 0.4757, -0.09890, -0.1439 0.5137, -0.09070, -0.0038 0.5514, -0.08120, 0.1452 0.5917, -0.06870, 0.1936 0.5917, -0.02380, 0.2068 0.5917, 0.02120, 0.2017 16 Flap element taps 1.0000, 0.00130, -1.1631 0.9365, 0.01390, 0.1009 0.8333, 0.03280, 0.2869 0.7436, 0.04930, 0.2387 0.7049, 0.05670, 0.1393 0.6667, 0.05450, 0.6960 0.6302, 0.03770, 0.9929 0.6083, 0.01980, 0.2937 0.6000, 0.00000, -1.2392 0.6076, -0.01900, -1.0288 0.6285, -0.03060, -1.0665 0.6667, -0.04090, -1.0657 0.7046, -0.04120, -1.1062 0.7429, -0.03210, -1.1097 0.8333, -0.01400, -1.1204 0.9311, -0.00120, -1.0957 --------- Run Conditions: vel=109.4 ft/s Re=1.011x10^6 AOA=12.05 Flap deflection=-60.00 Totals: Cl=0.0001 Cdp=0.3602 Cm(c/4)=0.1604 Cs=-0.3523 Ch=-0.0886 Main component: Cl=0.2980 Cdp=-0.0056 Cm=-0.0216 Flap component: Cl=-0.2979 Cdp=0.3658 Cm=0.1632 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.0961 0.5871, 0.07930, 0.1039 0.5501, 0.08690, 0.0973 0.5112, 0.09370, 0.1010 0.4731, 0.09830, 0.0661 0.4349, 0.10070, 0.0221 0.3960, 0.10120, 0.0456 0.3566, 0.10020, -0.2013 0.3172, 0.09790, -0.3099 0.2778, 0.09440, -0.4408 0.2393, 0.08960, -0.5317 0.2056, 0.08360, -0.5143 0.1633, 0.07610, -0.7349 0.1261, 0.06710, -0.7409 0.0900, 0.05640, -0.9626 0.0571, 0.04390, -1.0739 0.0283, 0.02940, -1.2341 0.0142, 0.01970, -1.4286 0.0081, 0.01410, -1.4456 0.0026, 0.00780, -1.3425 0.0000, 0.00000, -1.2887 0.0037, -0.00840, 0.7444 0.0112, -0.01420, 1.0056 0.0191, -0.01930, 0.9907 0.0397, -0.03030, 0.8416 0.0706, -0.04420, 0.6704 0.1037, -0.05710, 0.5434 0.1384, -0.06890, 0.2674 0.1741, -0.07950, 0.1465 0.2102, -0.08660, 0.1227 0.2472, -0.09640, -0.0744 0.2844, -0.10270, -0.1223 0.3225, -0.10690, -0.2919 0.3608, -0.10890, -0.2801 0.3991, -0.10830, -0.3730 0.4373, -0.10510, -0.2614 0.4757, -0.09890, -0.1487 0.5137, -0.09070, -0.0214 0.5514, -0.08120, 0.1274 0.5917, -0.06870, 0.0657 0.5917, -0.02380, 0.0845 0.5917, 0.02120, 0.0784 16 Flap element taps 1.0000, 0.00130, -1.1402 0.9365, 0.01390, 0.0235 0.8333, 0.03280, 0.1686 0.7436, 0.04930, 0.1310 0.7049, 0.05670, 0.0058 0.6667, 0.05450, 0.6157 0.6302, 0.03770, 1.0080 0.6083, 0.01980, 0.3967 0.6000, 0.00000, -1.2063 0.6076, -0.01900, -0.9752 0.6285, -0.03060, -1.0161 0.6667, -0.04090, -1.0145 0.7046, -0.04120, -1.0541 0.7429, -0.03210, -1.0627 0.8333, -0.01400, -1.0881 0.9311, -0.00120, -1.0777 --------- Run Conditions: vel=109.1 ft/s Re=1.005x10^6 AOA=15.04 Flap deflection=-60.00 Totals: Cl=0.1521 Cdp=0.3484 Cm(c/4)=0.1482 Cs=-0.2970 Ch=-0.0853 Main component: Cl=0.4272 Cdp=0.0276 Cm=-0.0482 Flap component: Cl=-0.2751 Cdp=0.3208 Cm=0.1371 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.0535 0.5871, 0.07930, -0.0600 0.5501, 0.08690, -0.0679 0.5112, 0.09370, -0.0683 0.4731, 0.09830, -0.0822 0.4349, 0.10070, -0.0799 0.3960, 0.10120, 0.0404 0.3566, 0.10020, -0.1622 0.3172, 0.09790, -0.2772 0.2778, 0.09440, -0.4449 0.2393, 0.08960, -0.5713 0.2056, 0.08360, -0.5867 0.1633, 0.07610, -0.8731 0.1261, 0.06710, -0.9257 0.0900, 0.05640, -1.2224 0.0571, 0.04390, -1.4377 0.0283, 0.02940, -1.7745 0.0142, 0.01970, -2.1868 0.0081, 0.01410, -2.3602 0.0026, 0.00780, -2.4241 0.0000, 0.00000, -2.9796 0.0037, -0.00840, 0.2743 0.0112, -0.01420, 0.9112 0.0191, -0.01930, 1.0040 0.0397, -0.03030, 0.9436 0.0706, -0.04420, 0.8093 0.1037, -0.05710, 0.6926 0.1384, -0.06890, 0.4075 0.1741, -0.07950, 0.2869 0.2102, -0.08660, 0.2737 0.2472, -0.09640, 0.0588 0.2844, -0.10270, 0.0075 0.3225, -0.10690, -0.1853 0.3608, -0.10890, -0.1852 0.3991, -0.10830, -0.3100 0.4373, -0.10510, -0.2074 0.4757, -0.09890, -0.1390 0.5137, -0.09070, -0.1149 0.5514, -0.08120, 0.1435 0.5917, -0.06870, -0.0853 0.5917, -0.02380, -0.0618 0.5917, 0.02120, -0.0696 16 Flap element taps 1.0000, 0.00130, -1.1648 0.9365, 0.01390, -0.0653 0.8333, 0.03280, 0.0011 0.7436, 0.04930, -0.0287 0.7049, 0.05670, -0.2033 0.6667, 0.05450, 0.4953 0.6302, 0.03770, 1.0206 0.6083, 0.01980, 0.4973 0.6000, 0.00000, -1.1721 0.6076, -0.01900, -0.9503 0.6285, -0.03060, -0.9974 0.6667, -0.04090, -0.9866 0.7046, -0.04120, -1.0346 0.7429, -0.03210, -1.0479 0.8333, -0.01400, -1.0715 0.9311, -0.00120, -1.0742 --------- Run Conditions: vel=109.9 ft/s Re=1.010x10^6 AOA=18.04 Flap deflection=-60.00 Totals: Cl=0.4323 Cdp=0.3246 Cm(c/4)=0.0793 Cs=-0.1747 Ch=-0.0693 Main component: Cl=0.5802 Cdp=0.1311 Cm=-0.1048 Flap component: Cl=-0.1479 Cdp=0.1934 Cm=0.0562 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.4339 0.5871, 0.07930, -0.4839 0.5501, 0.08690, -0.5205 0.5112, 0.09370, -0.4910 0.4731, 0.09830, -0.5056 0.4349, 0.10070, -0.4945 0.3960, 0.10120, -0.3603 0.3566, 0.10020, -0.5118 0.3172, 0.09790, -0.5329 0.2778, 0.09440, -0.5853 0.2393, 0.08960, -0.6135 0.2056, 0.08360, -0.5754 0.1633, 0.07610, -0.8535 0.1261, 0.06710, -0.9493 0.0900, 0.05640, -1.2883 0.0571, 0.04390, -1.6253 0.0283, 0.02940, -2.1591 0.0142, 0.01970, -2.7925 0.0081, 0.01410, -3.1882 0.0026, 0.00780, -3.4104 0.0000, 0.00000, -4.7181 0.0037, -0.00840, -0.3183 0.0112, -0.01420, 0.7160 0.0191, -0.01930, 0.9481 0.0397, -0.03030, 0.9916 0.0706, -0.04420, 0.9041 0.1037, -0.05710, 0.8052 0.1384, -0.06890, 0.5330 0.1741, -0.07950, 0.4159 0.2102, -0.08660, 0.3972 0.2472, -0.09640, 0.1812 0.2844, -0.10270, 0.1173 0.3225, -0.10690, -0.0849 0.3608, -0.10890, -0.1053 0.3991, -0.10830, -0.2570 0.4373, -0.10510, -0.1911 0.4757, -0.09890, -0.1470 0.5137, -0.09070, -0.0974 0.5514, -0.08120, -0.0583 0.5917, -0.06870, -0.4196 0.5917, -0.02380, -0.4072 0.5917, 0.02120, -0.4393 16 Flap element taps 1.0000, 0.00130, -0.8490 0.9365, 0.01390, -0.2016 0.8333, 0.03280, -0.2859 0.7436, 0.04930, -0.3800 0.7049, 0.05670, -0.7162 0.6667, 0.05450, 0.1874 0.6302, 0.03770, 1.0137 0.6083, 0.01980, 0.6949 0.6000, 0.00000, -0.8998 0.6076, -0.01900, -0.7389 0.6285, -0.03060, -0.7885 0.6667, -0.04090, -0.7676 0.7046, -0.04120, -0.8034 0.7429, -0.03210, -0.7975 0.8333, -0.01400, -0.8141 0.9311, -0.00120, -0.7794 --------- Run Conditions: vel=109.3 ft/s Re=1.002x10^6 AOA=20.01 Flap deflection=-60.00 Totals: Cl=0.5598 Cdp=0.3650 Cm(c/4)=0.0151 Cs=-0.1514 Ch=-0.0723 Main component: Cl=0.6155 Cdp=0.2414 Cm=-0.1454 Flap component: Cl=-0.0557 Cdp=0.1236 Cm=-0.0022 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.6445 0.5871, 0.07930, -0.6821 0.5501, 0.08690, -0.7452 0.5112, 0.09370, -0.7759 0.4731, 0.09830, -0.7974 0.4349, 0.10070, -0.7927 0.3960, 0.10120, -0.6728 0.3566, 0.10020, -0.7882 0.3172, 0.09790, -0.7953 0.2778, 0.09440, -0.8420 0.2393, 0.08960, -0.8572 0.2056, 0.08360, -0.7828 0.1633, 0.07610, -0.9562 0.1261, 0.06710, -0.9082 0.0900, 0.05640, -1.0138 0.0571, 0.04390, -1.0736 0.0283, 0.02940, -1.4478 0.0142, 0.01970, -2.0549 0.0081, 0.01410, -2.5006 0.0026, 0.00780, -2.9046 0.0000, 0.00000, -4.3921 0.0037, -0.00840, -0.3612 0.0112, -0.01420, 0.6768 0.0191, -0.01930, 0.9310 0.0397, -0.03030, 1.0048 0.0706, -0.04420, 0.9328 0.1037, -0.05710, 0.8459 0.1384, -0.06890, 0.5972 0.1741, -0.07950, 0.4827 0.2102, -0.08660, 0.4550 0.2472, -0.09640, 0.2472 0.2844, -0.10270, 0.1755 0.3225, -0.10690, -0.0194 0.3608, -0.10890, -0.0533 0.3991, -0.10830, -0.2139 0.4373, -0.10510, -0.1683 0.4757, -0.09890, -0.1416 0.5137, -0.09070, -0.1206 0.5514, -0.08120, -0.0813 0.5917, -0.06870, -0.6343 0.5917, -0.02380, -0.6223 0.5917, 0.02120, -0.6460 16 Flap element taps 1.0000, 0.00130, -0.7778 0.9365, 0.01390, -0.4829 0.8333, 0.03280, -0.6061 0.7436, 0.04930, -0.6077 0.7049, 0.05670, -1.0108 0.6667, 0.05450, 0.0125 0.6302, 0.03770, 0.9938 0.6083, 0.01980, 0.7720 0.6000, 0.00000, -0.7723 0.6076, -0.01900, -0.6556 0.6285, -0.03060, -0.7071 0.6667, -0.04090, -0.6876 0.7046, -0.04120, -0.7166 0.7429, -0.03210, -0.7145 0.8333, -0.01400, -0.7206 0.9311, -0.00120, -0.6986 --------- Run Conditions: vel=109.1 ft/s Re=0.999x10^6 AOA=24.01 Flap deflection=-60.00 Totals: Cl=0.6274 Cdp=0.4284 Cm(c/4)=-0.0453 Cs=-0.1360 Ch=-0.0744 Main component: Cl=0.5707 Cdp=0.3797 Cm=-0.1628 Flap component: Cl=0.0567 Cdp=0.0486 Cm=-0.0693 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.8673 0.5871, 0.07930, -0.7904 0.5501, 0.08690, -0.8347 0.5112, 0.09370, -0.8653 0.4731, 0.09830, -0.9076 0.4349, 0.10070, -0.9163 0.3960, 0.10120, -0.8065 0.3566, 0.10020, -0.9043 0.3172, 0.09790, -0.9034 0.2778, 0.09440, -0.9271 0.2393, 0.08960, -0.9031 0.2056, 0.08360, -0.7977 0.1633, 0.07610, -0.9145 0.1261, 0.06710, -0.8561 0.0900, 0.05640, -0.9292 0.0571, 0.04390, -0.9216 0.0283, 0.02940, -0.9653 0.0142, 0.01970, -1.0134 0.0081, 0.01410, -0.9561 0.0026, 0.00780, -1.0033 0.0000, 0.00000, -2.1463 0.0037, -0.00840, -0.0641 0.0112, -0.01420, 0.7082 0.0191, -0.01930, 0.9248 0.0397, -0.03030, 1.0070 0.0706, -0.04420, 0.9571 0.1037, -0.05710, 0.8909 0.1384, -0.06890, 0.6717 0.1741, -0.07950, 0.5666 0.2102, -0.08660, 0.5344 0.2472, -0.09640, 0.3380 0.2844, -0.10270, 0.2616 0.3225, -0.10690, 0.0732 0.3608, -0.10890, 0.0271 0.3991, -0.10830, -0.1449 0.4373, -0.10510, -0.1236 0.4757, -0.09890, -0.1181 0.5137, -0.09070, -0.1243 0.5514, -0.08120, -0.1071 0.5917, -0.06870, -0.8380 0.5917, -0.02380, -0.8292 0.5917, 0.02120, -0.8694 16 Flap element taps 1.0000, 0.00130, -0.6141 0.9365, 0.01390, -0.8334 0.8333, 0.03280, -0.8842 0.7436, 0.04930, -0.8414 0.7049, 0.05670, -1.3521 0.6667, 0.05450, -0.2025 0.6302, 0.03770, 0.9524 0.6083, 0.01980, 0.8550 0.6000, 0.00000, -0.5874 0.6076, -0.01900, -0.5350 0.6285, -0.03060, -0.5861 0.6667, -0.04090, -0.5645 0.7046, -0.04120, -0.5826 0.7429, -0.03210, -0.5836 0.8333, -0.01400, -0.5928 0.9311, -0.00120, -0.5626 --------- Run Conditions: vel=109.3 ft/s Re=0.998x10^6 AOA=26.98 Flap deflection=-60.00 Totals: Cl=0.6163 Cdp=0.4756 Cm(c/4)=-0.0533 Cs=-0.1442 Ch=-0.0736 Main component: Cl=0.5464 Cdp=0.4322 Cm=-0.1668 Flap component: Cl=0.0699 Cdp=0.0434 Cm=-0.0777 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.8922 0.5871, 0.07930, -0.8382 0.5501, 0.08690, -0.8550 0.5112, 0.09370, -0.8657 0.4731, 0.09830, -0.8876 0.4349, 0.10070, -0.8850 0.3960, 0.10120, -0.7858 0.3566, 0.10020, -0.8758 0.3172, 0.09790, -0.8776 0.2778, 0.09440, -0.9024 0.2393, 0.08960, -0.8860 0.2056, 0.08360, -0.7907 0.1633, 0.07610, -0.8985 0.1261, 0.06710, -0.8413 0.0900, 0.05640, -0.8918 0.0571, 0.04390, -0.8611 0.0283, 0.02940, -0.8742 0.0142, 0.01970, -0.8874 0.0081, 0.01410, -0.8241 0.0026, 0.00780, -0.7940 0.0000, 0.00000, -1.2513 0.0037, -0.00840, 0.0129 0.0112, -0.01420, 0.6972 0.0191, -0.01930, 0.9112 0.0397, -0.03030, 1.0087 0.0706, -0.04420, 0.9741 0.1037, -0.05710, 0.9203 0.1384, -0.06890, 0.7193 0.1741, -0.07950, 0.6194 0.2102, -0.08660, 0.5841 0.2472, -0.09640, 0.3968 0.2844, -0.10270, 0.3187 0.3225, -0.10690, 0.1351 0.3608, -0.10890, 0.0853 0.3991, -0.10830, -0.0937 0.4373, -0.10510, -0.0827 0.4757, -0.09890, -0.0875 0.5137, -0.09070, -0.1060 0.5514, -0.08120, -0.1008 0.5917, -0.06870, -0.8931 0.5917, -0.02380, -0.8790 0.5917, 0.02120, -0.9010 16 Flap element taps 1.0000, 0.00130, -0.5874 0.9365, 0.01390, -0.8726 0.8333, 0.03280, -0.9162 0.7436, 0.04930, -0.8765 0.7049, 0.05670, -1.4132 0.6667, 0.05450, -0.2475 0.6302, 0.03770, 0.9414 0.6083, 0.01980, 0.8742 0.6000, 0.00000, -0.5516 0.6076, -0.01900, -0.5250 0.6285, -0.03060, -0.5731 0.6667, -0.04090, -0.5526 0.7046, -0.04120, -0.5703 0.7429, -0.03210, -0.5716 0.8333, -0.01400, -0.5760 0.9311, -0.00120, -0.5488