S809 UNVENTED AILERON, LEGR, CHORD = 18 IN --------- Run Conditions: vel=98.0 ft/s Re=0.995x10^6 AOA=-5.99 Flap deflection=-30.00 Totals: Cl=-1.2071 Cdp=0.1774 Cm(c/4)=0.1360 Cs=-0.0505 Ch=0.2255 Main component: Cl=-0.9898 Cdp=0.0378 Cm=0.2475 Flap component: Cl=-0.2173 Cdp=0.1396 Cm=0.1932 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5111 0.6175, -0.04610, -0.4573 0.5841, -0.02440, -0.4518 0.5775, 0.01750, -0.4743 0.5777, 0.04660, -0.4643 0.6274, 0.07170, 0.6661 0.5694, 0.08320, 0.5376 0.5112, 0.09370, 0.2570 0.4731, 0.09830, 0.2461 0.4349, 0.10070, 0.1946 0.3960, 0.10120, 0.1646 0.3566, 0.10020, 0.2159 0.3172, 0.09790, 0.2490 0.2778, 0.09440, 0.2816 0.2393, 0.08960, 0.3244 0.2056, 0.08360, 0.3489 0.1633, 0.07610, 0.4766 0.1261, 0.06710, 0.5628 0.0900, 0.05640, 0.6925 0.0571, 0.04390, 0.8705 0.0283, 0.02940, 1.0111 0.0142, 0.01970, 0.9413 0.0081, 0.01410, 0.6778 0.0026, 0.00780, -0.1386 0.0000, 0.00000, -0.4399 0.0037, -0.00840, -3.8077 0.0112, -0.01420, -2.7602 0.0191, -0.01930, -2.2928 0.0397, -0.03030, -1.7076 0.0706, -0.04420, -1.5280 0.1037, -0.05710, -1.3938 0.1384, -0.06890, -1.3676 0.1741, -0.07950, -1.3746 0.2102, -0.08660, -1.4462 0.2472, -0.09640, -1.4724 0.2844, -0.10270, -1.4522 0.3225, -0.10690, -1.3832 0.3608, -0.10890, -1.3192 0.3991, -0.10830, -1.1284 0.4373, -0.10510, -0.8952 0.4757, -0.09890, -0.6410 0.5137, -0.09070, -0.5581 0.5694, -0.07640, -0.5168 14 Flap element taps 1.0000, 0.00130, -0.4891 0.9365, 0.01390, 0.0088 0.8333, 0.03280, 0.2894 0.7436, 0.04930, 0.4904 0.7049, 0.05670, 0.6109 0.6662, 0.06410, 0.6916 0.6522, 0.01390, -0.4698 0.5969, -0.00020, -0.4697 0.6000, -0.03020, -0.4923 0.6324, -0.04540, -0.4921 0.6667, -0.04880, -0.5040 0.7046, -0.04110, -0.4907 0.7429, -0.03210, -0.5068 0.9311, -0.00120, -0.4948 --------- Run Conditions: vel=99.0 ft/s Re=1.003x10^6 AOA=0.01 Flap deflection=-30.00 Totals: Cl=-1.1110 Cdp=0.1162 Cm(c/4)=0.1740 Cs=-0.1164 Ch=0.2196 Main component: Cl=-0.8870 Cdp=0.0091 Cm=0.2643 Flap component: Cl=-0.2240 Cdp=0.1071 Cm=0.1874 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5714 0.6175, -0.04610, -0.4463 0.5841, -0.02440, -0.4461 0.5775, 0.01750, -0.4639 0.5777, 0.04660, -0.4582 0.6274, 0.07170, 0.5250 0.5694, 0.08320, 0.4874 0.5112, 0.09370, 0.2599 0.4731, 0.09830, 0.1403 0.4349, 0.10070, 0.0714 0.3960, 0.10120, -0.0070 0.3566, 0.10020, 0.0688 0.3172, 0.09790, 0.0832 0.2778, 0.09440, 0.1025 0.2393, 0.08960, 0.1160 0.2056, 0.08360, 0.0813 0.1633, 0.07610, 0.2385 0.1261, 0.06710, 0.2831 0.0900, 0.05640, 0.3936 0.0571, 0.04390, 0.6008 0.0283, 0.02940, 0.8498 0.0142, 0.01970, 1.0001 0.0081, 0.01410, 0.9349 0.0026, 0.00780, 0.6683 0.0000, 0.00000, -0.3812 0.0037, -0.00840, -1.6105 0.0112, -0.01420, -1.1789 0.0191, -0.01930, -1.1134 0.0397, -0.03030, -0.9096 0.0706, -0.04420, -0.9635 0.1037, -0.05710, -0.9639 0.1384, -0.06890, -1.0139 0.1741, -0.07950, -1.1111 0.2102, -0.08660, -1.3020 0.2472, -0.09640, -1.3970 0.2844, -0.10270, -1.4870 0.3225, -0.10690, -1.4960 0.3608, -0.10890, -1.5733 0.3991, -0.10830, -1.5111 0.4373, -0.10510, -1.4605 0.4757, -0.09890, -1.2390 0.5137, -0.09070, -1.0984 0.5694, -0.07640, -0.7620 14 Flap element taps 1.0000, 0.00130, -0.4673 0.9365, 0.01390, 0.0150 0.8333, 0.03280, 0.2777 0.7436, 0.04930, 0.4898 0.7049, 0.05670, 0.5707 0.6662, 0.06410, 0.5171 0.6522, 0.01390, -0.4775 0.5969, -0.00020, -0.4575 0.6000, -0.03020, -0.5024 0.6324, -0.04540, -0.5067 0.6667, -0.04880, -0.5053 0.7046, -0.04110, -0.4735 0.7429, -0.03210, -0.4999 0.9311, -0.00120, -0.4730 --------- Run Conditions: vel=99.4 ft/s Re=1.007x10^6 AOA=3.03 Flap deflection=-30.00 Totals: Cl=-0.8783 Cdp=0.0780 Cm(c/4)=0.1661 Cs=-0.1243 Ch=0.1940 Main component: Cl=-0.6766 Cdp=-0.0034 Cm=0.2194 Flap component: Cl=-0.2017 Cdp=0.0813 Cm=0.1649 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.5101 0.6175, -0.04610, -0.3844 0.5841, -0.02440, -0.3852 0.5775, 0.01750, -0.4027 0.5777, 0.04660, -0.4012 0.6274, 0.07170, 0.4322 0.5694, 0.08320, 0.4476 0.5112, 0.09370, 0.2444 0.4731, 0.09830, 0.0994 0.4349, 0.10070, 0.0092 0.3960, 0.10120, -0.1091 0.3566, 0.10020, -0.0248 0.3172, 0.09790, -0.0227 0.2778, 0.09440, -0.0106 0.2393, 0.08960, -0.0161 0.2056, 0.08360, -0.0896 0.1633, 0.07610, 0.0773 0.1261, 0.06710, 0.0878 0.0900, 0.05640, 0.1685 0.0571, 0.04390, 0.3664 0.0283, 0.02940, 0.6271 0.0142, 0.01970, 0.8448 0.0081, 0.01410, 0.8567 0.0026, 0.00780, 0.9238 0.0000, 0.00000, -0.3163 0.0037, -0.00840, -0.3896 0.0112, -0.01420, -0.3740 0.0191, -0.01930, -0.4648 0.0397, -0.03030, -0.4256 0.0706, -0.04420, -0.5735 0.1037, -0.05710, -0.6364 0.1384, -0.06890, -0.6966 0.1741, -0.07950, -0.8251 0.2102, -0.08660, -1.0577 0.2472, -0.09640, -1.1584 0.2844, -0.10270, -1.2813 0.3225, -0.10690, -1.2884 0.3608, -0.10890, -1.3945 0.3991, -0.10830, -1.3445 0.4373, -0.10510, -1.3347 0.4757, -0.09890, -1.1359 0.5137, -0.09070, -1.0313 0.5694, -0.07640, -0.7018 14 Flap element taps 1.0000, 0.00130, -0.4068 0.9365, 0.01390, 0.0205 0.8333, 0.03280, 0.2681 0.7436, 0.04930, 0.4629 0.7049, 0.05670, 0.4778 0.6662, 0.06410, 0.4059 0.6522, 0.01390, -0.4222 0.5969, -0.00020, -0.3968 0.6000, -0.03020, -0.4325 0.6324, -0.04540, -0.4441 0.6667, -0.04880, -0.4451 0.7046, -0.04110, -0.4043 0.7429, -0.03210, -0.4340 0.9311, -0.00120, -0.3967 --------- Run Conditions: vel=100.0 ft/s Re=1.010x10^6 AOA=6.02 Flap deflection=-30.00 Totals: Cl=-0.6328 Cdp=0.0656 Cm(c/4)=0.1667 Cs=-0.1316 Ch=0.1820 Main component: Cl=-0.4425 Cdp=0.0021 Cm=0.1693 Flap component: Cl=-0.1903 Cdp=0.0635 Cm=0.1530 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4938 0.6175, -0.04610, -0.3768 0.5841, -0.02440, -0.3761 0.5775, 0.01750, -0.3938 0.5777, 0.04660, -0.3956 0.6274, 0.07170, 0.3403 0.5694, 0.08320, 0.3761 0.5112, 0.09370, 0.2116 0.4731, 0.09830, 0.0493 0.4349, 0.10070, -0.0655 0.3960, 0.10120, -0.2182 0.3566, 0.10020, -0.1424 0.3172, 0.09790, -0.1550 0.2778, 0.09440, -0.1567 0.2393, 0.08960, -0.1835 0.2056, 0.08360, -0.2916 0.1633, 0.07610, -0.1311 0.1261, 0.06710, -0.1585 0.0900, 0.05640, -0.1340 0.0571, 0.04390, 0.0368 0.0283, 0.02940, 0.2644 0.0142, 0.01970, 0.4886 0.0081, 0.01410, 0.5483 0.0026, 0.00780, 0.8290 0.0000, 0.00000, -0.3158 0.0037, -0.00840, 0.5252 0.0112, -0.01420, 0.2808 0.0191, -0.01930, 0.1399 0.0397, -0.03030, 0.0288 0.0706, -0.04420, -0.1873 0.1037, -0.05710, -0.3039 0.1384, -0.06890, -0.3763 0.1741, -0.07950, -0.5291 0.2102, -0.08660, -0.7954 0.2472, -0.09640, -0.9022 0.2844, -0.10270, -1.0519 0.3225, -0.10690, -1.0716 0.3608, -0.10890, -1.2033 0.3991, -0.10830, -1.1737 0.4373, -0.10510, -1.2025 0.4757, -0.09890, -1.0329 0.5137, -0.09070, -0.9692 0.5694, -0.07640, -0.6652 14 Flap element taps 1.0000, 0.00130, -0.3916 0.9365, 0.01390, 0.0110 0.8333, 0.03280, 0.2529 0.7436, 0.04930, 0.4034 0.7049, 0.05670, 0.3735 0.6662, 0.06410, 0.3077 0.6522, 0.01390, -0.4159 0.5969, -0.00020, -0.3877 0.6000, -0.03020, -0.4223 0.6324, -0.04540, -0.4387 0.6667, -0.04880, -0.4397 0.7046, -0.04110, -0.3881 0.7429, -0.03210, -0.4222 0.9311, -0.00120, -0.3797 --------- Run Conditions: vel=100.3 ft/s Re=1.011x10^6 AOA=9.02 Flap deflection=-30.00 Totals: Cl=-0.3702 Cdp=0.0611 Cm(c/4)=0.1646 Cs=-0.1184 Ch=0.1678 Main component: Cl=-0.1968 Cdp=0.0153 Cm=0.1156 Flap component: Cl=-0.1734 Cdp=0.0458 Cm=0.1381 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4660 0.6175, -0.04610, -0.3703 0.5841, -0.02440, -0.3697 0.5775, 0.01750, -0.3876 0.5777, 0.04660, -0.3934 0.6274, 0.07170, 0.2327 0.5694, 0.08320, 0.2825 0.5112, 0.09370, 0.1720 0.4731, 0.09830, 0.0121 0.4349, 0.10070, -0.1286 0.3960, 0.10120, -0.3163 0.3566, 0.10020, -0.2605 0.3172, 0.09790, -0.2916 0.2778, 0.09440, -0.3092 0.2393, 0.08960, -0.3642 0.2056, 0.08360, -0.5061 0.1633, 0.07610, -0.3683 0.1261, 0.06710, -0.4364 0.0900, 0.05640, -0.4807 0.0571, 0.04390, -0.3686 0.0283, 0.02940, -0.2420 0.0142, 0.01970, -0.0647 0.0081, 0.01410, -0.1089 0.0026, 0.00780, 0.2300 0.0000, 0.00000, -0.3241 0.0037, -0.00840, 0.9577 0.0112, -0.01420, 0.7624 0.0191, -0.01930, 0.6040 0.0397, -0.03030, 0.4196 0.0706, -0.04420, 0.1659 0.1037, -0.05710, 0.0002 0.1384, -0.06890, -0.0754 0.1741, -0.07950, -0.2438 0.2102, -0.08660, -0.5335 0.2472, -0.09640, -0.6433 0.2844, -0.10270, -0.8125 0.3225, -0.10690, -0.8452 0.3608, -0.10890, -0.9958 0.3991, -0.10830, -0.9871 0.4373, -0.10510, -1.0524 0.4757, -0.09890, -0.9079 0.5137, -0.09070, -0.8865 0.5694, -0.07640, -0.6127 14 Flap element taps 1.0000, 0.00130, -0.3753 0.9365, 0.01390, 0.0055 0.8333, 0.03280, 0.2352 0.7436, 0.04930, 0.3018 0.7049, 0.05670, 0.2497 0.6662, 0.06410, 0.2015 0.6522, 0.01390, -0.4106 0.5969, -0.00020, -0.3805 0.6000, -0.03020, -0.4141 0.6324, -0.04540, -0.4301 0.6667, -0.04880, -0.4269 0.7046, -0.04110, -0.3683 0.7429, -0.03210, -0.4056 0.9311, -0.00120, -0.3647 --------- Run Conditions: vel=100.6 ft/s Re=1.012x10^6 AOA=12.01 Flap deflection=-30.00 Totals: Cl=-0.1063 Cdp=0.0661 Cm(c/4)=0.1581 Cs=-0.0868 Ch=0.1498 Main component: Cl=0.0432 Cdp=0.0386 Cm=0.0617 Flap component: Cl=-0.1495 Cdp=0.0275 Cm=0.1190 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4324 0.6175, -0.04610, -0.3705 0.5841, -0.02440, -0.3691 0.5775, 0.01750, -0.3841 0.5777, 0.04660, -0.3949 0.6274, 0.07170, 0.1104 0.5694, 0.08320, 0.1656 0.5112, 0.09370, 0.0985 0.4731, 0.09830, -0.0089 0.4349, 0.10070, -0.1645 0.3960, 0.10120, -0.3885 0.3566, 0.10020, -0.3619 0.3172, 0.09790, -0.4179 0.2778, 0.09440, -0.4574 0.2393, 0.08960, -0.5428 0.2056, 0.08360, -0.7212 0.1633, 0.07610, -0.6170 0.1261, 0.06710, -0.7328 0.0900, 0.05640, -0.8459 0.0571, 0.04390, -0.8320 0.0283, 0.02940, -0.8495 0.0142, 0.01970, -0.7941 0.0081, 0.01410, -1.0732 0.0026, 0.00780, -0.4704 0.0000, 0.00000, -0.3259 0.0037, -0.00840, 0.9796 0.0112, -0.01420, 0.9845 0.0191, -0.01930, 0.8903 0.0397, -0.03030, 0.7149 0.0706, -0.04420, 0.4559 0.1037, -0.05710, 0.2693 0.1384, -0.06890, 0.1980 0.1741, -0.07950, 0.0144 0.2102, -0.08660, -0.2890 0.2472, -0.09640, -0.4039 0.2844, -0.10270, -0.5848 0.3225, -0.10690, -0.6243 0.3608, -0.10890, -0.7872 0.3991, -0.10830, -0.8027 0.4373, -0.10510, -0.8939 0.4757, -0.09890, -0.7783 0.5137, -0.09070, -0.7891 0.5694, -0.07640, -0.5499 14 Flap element taps 1.0000, 0.00130, -0.3435 0.9365, 0.01390, 0.0124 0.8333, 0.03280, 0.1979 0.7436, 0.04930, 0.1639 0.7049, 0.05670, 0.1158 0.6662, 0.06410, 0.0764 0.6522, 0.01390, -0.4120 0.5969, -0.00020, -0.3796 0.6000, -0.03020, -0.4095 0.6324, -0.04540, -0.4245 0.6667, -0.04880, -0.4048 0.7046, -0.04110, -0.3426 0.7429, -0.03210, -0.3806 0.9311, -0.00120, -0.3469 --------- Run Conditions: vel=99.6 ft/s Re=0.997x10^6 AOA=15.02 Flap deflection=-30.00 Totals: Cl=0.1249 Cdp=0.0831 Cm(c/4)=0.1492 Cs=-0.0479 Ch=0.1336 Main component: Cl=0.2456 Cdp=0.0743 Cm=0.0154 Flap component: Cl=-0.1207 Cdp=0.0088 Cm=0.0983 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4401 0.6175, -0.04610, -0.4477 0.5841, -0.02440, -0.4343 0.5775, 0.01750, -0.4541 0.5777, 0.04660, -0.4505 0.6274, 0.07170, -0.0197 0.5694, 0.08320, -0.0378 0.5112, 0.09370, -0.0326 0.4731, 0.09830, -0.0490 0.4349, 0.10070, -0.1485 0.3960, 0.10120, -0.2672 0.3566, 0.10020, -0.3962 0.3172, 0.09790, -0.4883 0.2778, 0.09440, -0.5957 0.2393, 0.08960, -0.6927 0.2056, 0.08360, -0.8006 0.1633, 0.07610, -0.8956 0.1261, 0.06710, -0.9876 0.0900, 0.05640, -1.2365 0.0571, 0.04390, -1.3069 0.0283, 0.02940, -1.5311 0.0142, 0.01970, -1.7195 0.0081, 0.01410, -1.9807 0.0026, 0.00780, -1.6060 0.0000, 0.00000, -0.2318 0.0037, -0.00840, 0.6375 0.0112, -0.01420, 0.9883 0.0191, -0.01930, 1.0089 0.0397, -0.03030, 0.8955 0.0706, -0.04420, 0.6911 0.1037, -0.05710, 0.5213 0.1384, -0.06890, 0.3250 0.1741, -0.07950, 0.1614 0.2102, -0.08660, -0.0083 0.2472, -0.09640, -0.1917 0.2844, -0.10270, -0.3488 0.3225, -0.10690, -0.4903 0.3608, -0.10890, -0.6288 0.3991, -0.10830, -0.7208 0.4373, -0.10510, -0.7514 0.4757, -0.09890, -0.7015 0.5137, -0.09070, -0.6630 0.5694, -0.07640, -0.4895 14 Flap element taps 1.0000, 0.00130, -0.3202 0.9365, 0.01390, 0.0240 0.8333, 0.03280, 0.1236 0.7436, 0.04930, 0.0077 0.7049, 0.05670, -0.0234 0.6662, 0.06410, -0.0318 0.6522, 0.01390, -0.4324 0.5969, -0.00020, -0.4460 0.6000, -0.03020, -0.4601 0.6324, -0.04540, -0.4257 0.6667, -0.04880, -0.3319 0.7046, -0.04110, -0.3201 0.7429, -0.03210, -0.3254 0.9311, -0.00120, -0.3776 --------- Run Conditions: vel=100.0 ft/s Re=1.001x10^6 AOA=18.00 Flap deflection=-30.00 Totals: Cl=0.4470 Cdp=0.1070 Cm(c/4)=0.0978 Cs=0.0363 Ch=0.0498 Main component: Cl=0.4687 Cdp=0.1384 Cm=-0.0433 Flap component: Cl=-0.0217 Cdp=-0.0313 Cm=0.0265 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4608 0.6175, -0.04610, -0.5821 0.5841, -0.02440, -0.5686 0.5775, 0.01750, -0.5876 0.5777, 0.04660, -0.5870 0.6274, 0.07170, -0.2783 0.5694, 0.08320, -0.2975 0.5112, 0.09370, -0.2832 0.4731, 0.09830, -0.2729 0.4349, 0.10070, -0.2833 0.3960, 0.10120, -0.3115 0.3566, 0.10020, -0.3905 0.3172, 0.09790, -0.4921 0.2778, 0.09440, -0.6340 0.2393, 0.08960, -0.7818 0.2056, 0.08360, -0.9459 0.1633, 0.07610, -1.1029 0.1261, 0.06710, -1.2686 0.0900, 0.05640, -1.5847 0.0571, 0.04390, -1.8346 0.0283, 0.02940, -2.3294 0.0142, 0.01970, -2.8443 0.0081, 0.01410, -3.2986 0.0026, 0.00780, -3.1351 0.0000, 0.00000, -0.1191 0.0037, -0.00840, -0.0922 0.0112, -0.01420, 0.7841 0.0191, -0.01930, 0.9708 0.0397, -0.03030, 1.0021 0.0706, -0.04420, 0.8640 0.1037, -0.05710, 0.7108 0.1384, -0.06890, 0.5362 0.1741, -0.07950, 0.3792 0.2102, -0.08660, 0.2123 0.2472, -0.09640, 0.0312 0.2844, -0.10270, -0.1314 0.3225, -0.10690, -0.2813 0.3608, -0.10890, -0.4313 0.3991, -0.10830, -0.5397 0.4373, -0.10510, -0.5989 0.4757, -0.09890, -0.5762 0.5137, -0.09070, -0.5760 0.5694, -0.07640, -0.4656 14 Flap element taps 1.0000, 0.00130, -0.2452 0.9365, 0.01390, 0.0022 0.8333, 0.03280, -0.1295 0.7436, 0.04930, -0.2733 0.7049, 0.05670, -0.2936 0.6662, 0.06410, -0.2943 0.6522, 0.01390, -0.5694 0.5969, -0.00020, -0.5791 0.6000, -0.03020, -0.5918 0.6324, -0.04540, -0.4710 0.6667, -0.04880, -0.2777 0.7046, -0.04110, -0.2099 0.7429, -0.03210, -0.2126 0.9311, -0.00120, -0.2298 --------- Run Conditions: vel=99.6 ft/s Re=0.996x10^6 AOA=20.00 Flap deflection=-30.00 Totals: Cl=0.4074 Cdp=0.1498 Cm(c/4)=0.0987 Cs=-0.0014 Ch=0.0680 Main component: Cl=0.4364 Cdp=0.1939 Cm=-0.0466 Flap component: Cl=-0.0290 Cdp=-0.0441 Cm=0.0368 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6096 0.6175, -0.04610, -0.8054 0.5841, -0.02440, -0.7935 0.5775, 0.01750, -0.8095 0.5777, 0.04660, -0.8104 0.6274, 0.07170, -0.4322 0.5694, 0.08320, -0.4484 0.5112, 0.09370, -0.4435 0.4731, 0.09830, -0.4311 0.4349, 0.10070, -0.4308 0.3960, 0.10120, -0.4369 0.3566, 0.10020, -0.4751 0.3172, 0.09790, -0.5129 0.2778, 0.09440, -0.5920 0.2393, 0.08960, -0.6958 0.2056, 0.08360, -0.8375 0.1633, 0.07610, -0.9781 0.1261, 0.06710, -1.1427 0.0900, 0.05640, -1.4330 0.0571, 0.04390, -1.7170 0.0283, 0.02940, -2.2487 0.0142, 0.01970, -2.7946 0.0081, 0.01410, -3.2892 0.0026, 0.00780, -3.1732 0.0000, 0.00000, 0.0093 0.0037, -0.00840, -0.1553 0.0112, -0.01420, 0.7584 0.0191, -0.01930, 0.9593 0.0397, -0.03030, 1.0054 0.0706, -0.04420, 0.8745 0.1037, -0.05710, 0.7220 0.1384, -0.06890, 0.5462 0.1741, -0.07950, 0.3870 0.2102, -0.08660, 0.2134 0.2472, -0.09640, 0.0249 0.2844, -0.10270, -0.1477 0.3225, -0.10690, -0.3084 0.3608, -0.10890, -0.4723 0.3991, -0.10830, -0.5925 0.4373, -0.10510, -0.6684 0.4757, -0.09890, -0.6571 0.5137, -0.09070, -0.6746 0.5694, -0.07640, -0.5787 14 Flap element taps 1.0000, 0.00130, -0.2726 0.9365, 0.01390, -0.0283 0.8333, 0.03280, -0.1663 0.7436, 0.04930, -0.3988 0.7049, 0.05670, -0.4427 0.6662, 0.06410, -0.4481 0.6522, 0.01390, -0.7913 0.5969, -0.00020, -0.8038 0.6000, -0.03020, -0.8126 0.6324, -0.04540, -0.6472 0.6667, -0.04880, -0.4667 0.7046, -0.04110, -0.3030 0.7429, -0.03210, -0.3047 0.9311, -0.00120, -0.3313 --------- Run Conditions: vel=100.6 ft/s Re=1.005x10^6 AOA=24.00 Flap deflection=-30.00 Totals: Cl=0.0893 Cdp=0.2262 Cm(c/4)=0.1003 Cs=-0.1703 Ch=0.0762 Main component: Cl=0.1643 Cdp=0.2711 Cm=-0.0113 Flap component: Cl=-0.0750 Cdp=-0.0449 Cm=0.0682 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.9244 0.6175, -0.04610, -1.2174 0.5841, -0.02440, -1.2032 0.5775, 0.01750, -1.2203 0.5777, 0.04660, -1.2210 0.6274, 0.07170, -0.4576 0.5694, 0.08320, -0.5220 0.5112, 0.09370, -0.5286 0.4731, 0.09830, -0.5181 0.4349, 0.10070, -0.5060 0.3960, 0.10120, -0.4913 0.3566, 0.10020, -0.5061 0.3172, 0.09790, -0.5010 0.2778, 0.09440, -0.5001 0.2393, 0.08960, -0.4981 0.2056, 0.08360, -0.5262 0.1633, 0.07610, -0.5383 0.1261, 0.06710, -0.5597 0.0900, 0.05640, -0.5687 0.0571, 0.04390, -0.6580 0.0283, 0.02940, -0.9055 0.0142, 0.01970, -1.3199 0.0081, 0.01410, -1.7984 0.0026, 0.00780, -1.7888 0.0000, 0.00000, 0.1610 0.0037, -0.00840, 0.2225 0.0112, -0.01420, 0.8550 0.0191, -0.01930, 0.9863 0.0397, -0.03030, 0.9949 0.0706, -0.04420, 0.8598 0.1037, -0.05710, 0.7112 0.1384, -0.06890, 0.5332 0.1741, -0.07950, 0.3697 0.2102, -0.08660, 0.1877 0.2472, -0.09640, -0.0151 0.2844, -0.10270, -0.2046 0.3225, -0.10690, -0.3849 0.3608, -0.10890, -0.5738 0.3991, -0.10830, -0.7220 0.4373, -0.10510, -0.8292 0.4757, -0.09890, -0.8397 0.5137, -0.09070, -0.8921 0.5694, -0.07640, -0.8235 14 Flap element taps 1.0000, 0.00130, -0.4751 0.9365, 0.01390, -0.4164 0.8333, 0.03280, -0.4966 0.7436, 0.04930, -0.5217 0.7049, 0.05670, -0.4995 0.6662, 0.06410, -0.4709 0.6522, 0.01390, -1.2042 0.5969, -0.00020, -1.2228 0.6000, -0.03020, -1.2501 0.6324, -0.04540, -1.1900 0.6667, -0.04880, -1.0757 0.7046, -0.04110, -0.7799 0.7429, -0.03210, -0.7822 0.9311, -0.00120, -0.5531 --------- Run Conditions: vel=100.3 ft/s Re=1.001x10^6 AOA=26.97 Flap deflection=-30.00 Totals: Cl=0.0886 Cdp=0.2645 Cm(c/4)=0.1156 Cs=-0.1956 Ch=0.0918 Main component: Cl=0.1902 Cdp=0.3222 Cm=-0.0246 Flap component: Cl=-0.1016 Cdp=-0.0577 Cm=0.0905 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.0265 0.6175, -0.04610, -1.3716 0.5841, -0.02440, -1.3557 0.5775, 0.01750, -1.3718 0.5777, 0.04660, -1.3724 0.6274, 0.07170, -0.4877 0.5694, 0.08320, -0.5486 0.5112, 0.09370, -0.5680 0.4731, 0.09830, -0.5768 0.4349, 0.10070, -0.5747 0.3960, 0.10120, -0.5714 0.3566, 0.10020, -0.5880 0.3172, 0.09790, -0.5896 0.2778, 0.09440, -0.5967 0.2393, 0.08960, -0.6113 0.2056, 0.08360, -0.6306 0.1633, 0.07610, -0.6640 0.1261, 0.06710, -0.6911 0.0900, 0.05640, -0.7397 0.0571, 0.04390, -0.8443 0.0283, 0.02940, -0.9426 0.0142, 0.01970, -1.1865 0.0081, 0.01410, -1.5193 0.0026, 0.00780, -1.5313 0.0000, 0.00000, 0.2783 0.0037, -0.00840, 0.1546 0.0112, -0.01420, 0.8153 0.0191, -0.01930, 0.9669 0.0397, -0.03030, 1.0046 0.0706, -0.04420, 0.8933 0.1037, -0.05710, 0.7504 0.1384, -0.06890, 0.5778 0.1741, -0.07950, 0.4187 0.2102, -0.08660, 0.2383 0.2472, -0.09640, 0.0329 0.2844, -0.10270, -0.1618 0.3225, -0.10690, -0.3514 0.3608, -0.10890, -0.5490 0.3991, -0.10830, -0.7109 0.4373, -0.10510, -0.8350 0.4757, -0.09890, -0.8592 0.5137, -0.09070, -0.9309 0.5694, -0.07640, -0.8930 14 Flap element taps 1.0000, 0.00130, -0.4434 0.9365, 0.01390, -0.4129 0.8333, 0.03280, -0.4985 0.7436, 0.04930, -0.5326 0.7049, 0.05670, -0.5238 0.6662, 0.06410, -0.5049 0.6522, 0.01390, -1.3561 0.5969, -0.00020, -1.3821 0.6000, -0.03020, -1.4147 0.6324, -0.04540, -1.4158 0.6667, -0.04880, -1.4014 0.7046, -0.04110, -0.9547 0.7429, -0.03210, -0.9306 0.9311, -0.00120, -0.5122