S809 SPOILER FLAP, LEGR, CHORD = 18 INCHES --------- Run Conditions: vel=101.2 ft/s Re=1.000x10^6 AOA=-5.97 Flap deflection=10.00 Totals: Cl=-0.6812 Cdp=0.0280 Cm(c/4)=0.0222 Cs=0.0430 Ch=-0.0086 Main component: Cl=-0.6401 Cdp=-0.0399 Cm=0.1547 Flap component: Cl=-0.0412 Cdp=0.0679 Cm=0.0377 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.2741 0.5905, -0.01667, 0.3641 0.5709, 0.03110, 0.4321 0.5889, 0.07933, 0.3915 0.5500, 0.08689, 0.3150 0.5110, 0.09367, 0.1037 0.4731, 0.09830, -0.0298 0.4349, 0.10070, -0.1021 0.3960, 0.10120, -0.1087 0.3566, 0.10020, -0.0932 0.3172, 0.09790, -0.0590 0.2778, 0.09440, -0.0342 0.2393, 0.08960, 0.0108 0.2056, 0.08360, 0.0782 0.1633, 0.07610, 0.1600 0.1261, 0.06710, 0.2859 0.0900, 0.05640, 0.4089 0.0571, 0.04390, 0.6261 0.0283, 0.02940, 0.8634 0.0142, 0.01970, 0.9958 0.0081, 0.01410, 0.9770 0.0026, 0.00780, 0.5661 0.0000, 0.00000, -1.0182 0.0037, -0.00840, -1.9035 0.0112, -0.01420, -1.5419 0.0191, -0.01930, -1.2490 0.0397, -0.03030, -0.9434 0.0706, -0.04420, -0.9516 0.1037, -0.05710, -0.9223 0.1384, -0.06890, -0.9992 0.1741, -0.07950, -1.0302 0.2102, -0.08660, -1.0752 0.2472, -0.09640, -1.1506 0.2844, -0.10270, -1.1592 0.3225, -0.10690, -1.1440 0.3608, -0.10890, -1.1088 0.3991, -0.10830, -0.9925 0.4373, -0.10510, -0.7749 0.4757, -0.09890, -0.5209 0.5137, -0.09067, -0.3422 0.5611, -0.07859, -0.3046 16 Flap element taps 1.0000, 0.00130, -0.3425 0.9365, 0.01390, -0.3288 0.8333, 0.03280, -0.3428 0.7436, 0.04930, -0.3379 0.7049, 0.05667, -0.3277 0.6662, 0.06411, -0.3233 0.6274, 0.07172, -0.3157 0.6009, 0.07523, -0.4346 0.6069, 0.02889, 0.3704 0.6079, -0.01747, 0.4147 0.6167, -0.06381, -0.4776 0.6558, -0.05300, -0.4940 0.7045, -0.04117, -0.4981 0.7429, -0.03210, -0.4954 0.8333, -0.01400, -0.4741 0.9311, -0.00120, -0.3538 --------- Run Conditions: vel=100.9 ft/s Re=0.996x10^6 AOA=0.06 Flap deflection=10.00 Totals: Cl=-0.1282 Cdp=0.0264 Cm(c/4)=-0.0164 Cs=-0.0265 Ch=-0.0144 Main component: Cl=-0.1871 Cdp=-0.0286 Cm=0.0646 Flap component: Cl=0.0589 Cdp=0.0550 Cm=-0.0489 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.0260 0.5905, -0.01667, 0.2039 0.5709, 0.03110, 0.2203 0.5889, 0.07933, 0.1880 0.5500, 0.08689, 0.1505 0.5110, 0.09367, -0.0329 0.4731, 0.09830, -0.2060 0.4349, 0.10070, -0.3210 0.3960, 0.10120, -0.3630 0.3566, 0.10020, -0.3811 0.3172, 0.09790, -0.3742 0.2778, 0.09440, -0.3828 0.2393, 0.08960, -0.3752 0.2056, 0.08360, -0.3468 0.1633, 0.07610, -0.3063 0.1261, 0.06710, -0.2260 0.0900, 0.05640, -0.1726 0.0571, 0.04390, 0.0065 0.0283, 0.02940, 0.2210 0.0142, 0.01970, 0.4771 0.0081, 0.01410, 0.6714 0.0026, 0.00780, 0.8285 0.0000, 0.00000, 0.9611 0.0037, -0.00840, 0.3928 0.0112, -0.01420, 0.1730 0.0191, -0.01930, 0.1077 0.0397, -0.03030, 0.0441 0.0706, -0.04420, -0.1569 0.1037, -0.05710, -0.2561 0.1384, -0.06890, -0.4110 0.1741, -0.07950, -0.5131 0.2102, -0.08660, -0.6107 0.2472, -0.09640, -0.7385 0.2844, -0.10270, -0.8063 0.3225, -0.10690, -0.8566 0.3608, -0.10890, -0.8954 0.3991, -0.10830, -0.8684 0.4373, -0.10510, -0.7565 0.4757, -0.09890, -0.5882 0.5137, -0.09067, -0.3280 0.5611, -0.07859, -0.1235 16 Flap element taps 1.0000, 0.00130, -0.3763 0.9365, 0.01390, -0.3793 0.8333, 0.03280, -0.3753 0.7436, 0.04930, -0.3615 0.7049, 0.05667, -0.3541 0.6662, 0.06411, -0.3507 0.6274, 0.07172, -0.3491 0.6009, 0.07523, -0.4388 0.6069, 0.02889, 0.1728 0.6079, -0.01747, 0.2257 0.6167, -0.06381, -0.2811 0.6558, -0.05300, -0.3033 0.7045, -0.04117, -0.3103 0.7429, -0.03210, -0.2615 0.8333, -0.01400, -0.1470 0.9311, -0.00120, -0.0364 --------- Run Conditions: vel=101.2 ft/s Re=0.998x10^6 AOA=3.02 Flap deflection=10.00 Totals: Cl=0.2185 Cdp=0.0449 Cm(c/4)=-0.0502 Cs=-0.0333 Ch=0.0007 Main component: Cl=0.0767 Cdp=-0.0180 Cm=0.0099 Flap component: Cl=0.1418 Cdp=0.0629 Cm=-0.1153 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0272 0.5905, -0.01667, 0.0943 0.5709, 0.03110, 0.1094 0.5889, 0.07933, 0.0740 0.5500, 0.08689, 0.0514 0.5110, 0.09367, -0.0889 0.4731, 0.09830, -0.2834 0.4349, 0.10070, -0.4297 0.3960, 0.10120, -0.5058 0.3566, 0.10020, -0.5374 0.3172, 0.09790, -0.5500 0.2778, 0.09440, -0.5828 0.2393, 0.08960, -0.6044 0.2056, 0.08360, -0.6134 0.1633, 0.07610, -0.5947 0.1261, 0.06710, -0.5561 0.0900, 0.05640, -0.5627 0.0571, 0.04390, -0.4538 0.0283, 0.02940, -0.3393 0.0142, 0.01970, -0.1765 0.0081, 0.01410, 0.0432 0.0026, 0.00780, 0.2000 0.0000, 0.00000, 0.8328 0.0037, -0.00840, 0.9218 0.0112, -0.01420, 0.7268 0.0191, -0.01930, 0.6056 0.0397, -0.03030, 0.4307 0.0706, -0.04420, 0.1989 0.1037, -0.05710, 0.0634 0.1384, -0.06890, -0.1037 0.1741, -0.07950, -0.2304 0.2102, -0.08660, -0.3494 0.2472, -0.09640, -0.4864 0.2844, -0.10270, -0.5755 0.3225, -0.10690, -0.6386 0.3608, -0.10890, -0.7072 0.3991, -0.10830, -0.7114 0.4373, -0.10510, -0.6433 0.4757, -0.09890, -0.5251 0.5137, -0.09067, -0.3030 0.5611, -0.07859, -0.1170 16 Flap element taps 1.0000, 0.00130, -0.3711 0.9365, 0.01390, -0.4439 0.8333, 0.03280, -0.4228 0.7436, 0.04930, -0.4052 0.7049, 0.05667, -0.4017 0.6662, 0.06411, -0.4016 0.6274, 0.07172, -0.4016 0.6009, 0.07523, -0.4021 0.6069, 0.02889, 0.0693 0.6079, -0.01747, 0.1060 0.6167, -0.06381, -0.0659 0.6558, -0.05300, -0.0865 0.7045, -0.04117, -0.0618 0.7429, -0.03210, -0.0190 0.8333, -0.01400, 0.0477 0.9311, -0.00120, 0.0627 --------- Run Conditions: vel=101.2 ft/s Re=0.998x10^6 AOA=6.05 Flap deflection=10.00 Totals: Cl=0.4669 Cdp=0.0672 Cm(c/4)=-0.0690 Cs=-0.0177 Ch=0.0044 Main component: Cl=0.2725 Cdp=-0.0046 Cm=-0.0273 Flap component: Cl=0.1944 Cdp=0.0719 Cm=-0.1595 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.0057 0.5905, -0.01667, -0.0046 0.5709, 0.03110, 0.0125 0.5889, 0.07933, -0.0187 0.5500, 0.08689, -0.0244 0.5110, 0.09367, -0.0923 0.4731, 0.09830, -0.2634 0.4349, 0.10070, -0.4411 0.3960, 0.10120, -0.5660 0.3566, 0.10020, -0.6135 0.3172, 0.09790, -0.6599 0.2778, 0.09440, -0.7191 0.2393, 0.08960, -0.7700 0.2056, 0.08360, -0.8197 0.1633, 0.07610, -0.8262 0.1261, 0.06710, -0.8401 0.0900, 0.05640, -0.9095 0.0571, 0.04390, -0.8877 0.0283, 0.02940, -0.9166 0.0142, 0.01970, -0.9087 0.0081, 0.01410, -0.6651 0.0026, 0.00780, -0.5377 0.0000, 0.00000, 0.0507 0.0037, -0.00840, 0.9761 0.0112, -0.01420, 0.9643 0.0191, -0.01930, 0.8758 0.0397, -0.03030, 0.6936 0.0706, -0.04420, 0.4539 0.1037, -0.05710, 0.2992 0.1384, -0.06890, 0.1347 0.1741, -0.07950, -0.0085 0.2102, -0.08660, -0.1533 0.2472, -0.09640, -0.2949 0.2844, -0.10270, -0.4071 0.3225, -0.10690, -0.4717 0.3608, -0.10890, -0.5625 0.3991, -0.10830, -0.5853 0.4373, -0.10510, -0.5507 0.4757, -0.09890, -0.4680 0.5137, -0.09067, -0.2705 0.5611, -0.07859, -0.1225 16 Flap element taps 1.0000, 0.00130, -0.3934 0.9365, 0.01390, -0.4709 0.8333, 0.03280, -0.4511 0.7436, 0.04930, -0.4357 0.7049, 0.05667, -0.4335 0.6662, 0.06411, -0.4402 0.6274, 0.07172, -0.4378 0.6009, 0.07523, -0.4969 0.6069, 0.02889, -0.0077 0.6079, -0.01747, 0.0050 0.6167, -0.06381, 0.0175 0.6558, -0.05300, -0.0016 0.7045, -0.04117, 0.0125 0.7429, -0.03210, 0.1227 0.8333, -0.01400, 0.2591 0.9311, -0.00120, 0.1276 --------- Run Conditions: vel=101.1 ft/s Re=0.995x10^6 AOA=9.03 Flap deflection=10.00 Totals: Cl=0.7009 Cdp=0.0878 Cm(c/4)=-0.0774 Cs=0.0233 Ch=0.0112 Main component: Cl=0.4764 Cdp=0.0131 Cm=-0.0694 Flap component: Cl=0.2245 Cdp=0.0747 Cm=-0.1846 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.0241 0.5905, -0.01667, -0.1498 0.5709, 0.03110, -0.0991 0.5889, 0.07933, -0.1306 0.5500, 0.08689, -0.1315 0.5110, 0.09367, -0.1642 0.4731, 0.09830, -0.2811 0.4349, 0.10070, -0.4599 0.3960, 0.10120, -0.6285 0.3566, 0.10020, -0.6885 0.3172, 0.09790, -0.7650 0.2778, 0.09440, -0.8530 0.2393, 0.08960, -0.9356 0.2056, 0.08360, -1.0331 0.1633, 0.07610, -1.0625 0.1261, 0.06710, -1.1359 0.0900, 0.05640, -1.2727 0.0571, 0.04390, -1.3622 0.0283, 0.02940, -1.5778 0.0142, 0.01970, -1.7968 0.0081, 0.01410, -1.6908 0.0026, 0.00780, -1.6635 0.0000, 0.00000, -1.3838 0.0037, -0.00840, 0.7104 0.0112, -0.01420, 1.0025 0.0191, -0.01930, 0.9999 0.0397, -0.03030, 0.8762 0.0706, -0.04420, 0.6586 0.1037, -0.05710, 0.5002 0.1384, -0.06890, 0.3484 0.1741, -0.07950, 0.1982 0.2102, -0.08660, 0.0344 0.2472, -0.09640, -0.1035 0.2844, -0.10270, -0.2325 0.3225, -0.10690, -0.3056 0.3608, -0.10890, -0.4220 0.3991, -0.10830, -0.4596 0.4373, -0.10510, -0.4502 0.4757, -0.09890, -0.3972 0.5137, -0.09067, -0.2323 0.5611, -0.07859, -0.0787 16 Flap element taps 1.0000, 0.00130, -0.4048 0.9365, 0.01390, -0.4591 0.8333, 0.03280, -0.4512 0.7436, 0.04930, -0.4377 0.7049, 0.05667, -0.4311 0.6662, 0.06411, -0.4424 0.6274, 0.07172, -0.4421 0.6009, 0.07523, -0.4834 0.6069, 0.02889, -0.1111 0.6079, -0.01747, -0.1142 0.6167, -0.06381, -0.0384 0.6558, -0.05300, -0.0662 0.7045, -0.04117, 0.2411 0.7429, -0.03210, 0.4543 0.8333, -0.01400, 0.2926 0.9311, -0.00120, 0.1445 --------- Run Conditions: vel=100.8 ft/s Re=0.992x10^6 AOA=12.05 Flap deflection=10.00 Totals: Cl=0.9106 Cdp=0.1149 Cm(c/4)=-0.0793 Cs=0.0777 Ch=0.0167 Main component: Cl=0.6731 Cdp=0.0405 Cm=-0.1126 Flap component: Cl=0.2375 Cdp=0.0745 Cm=-0.1954 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.0210 0.5905, -0.01667, -0.3248 0.5709, 0.03110, -0.2248 0.5889, 0.07933, -0.2767 0.5500, 0.08689, -0.2743 0.5110, 0.09367, -0.2938 0.4731, 0.09830, -0.3308 0.4349, 0.10070, -0.4586 0.3960, 0.10120, -0.6514 0.3566, 0.10020, -0.7240 0.3172, 0.09790, -0.8377 0.2778, 0.09440, -0.9564 0.2393, 0.08960, -1.0726 0.2056, 0.08360, -1.2222 0.1633, 0.07610, -1.2799 0.1261, 0.06710, -1.4213 0.0900, 0.05640, -1.6246 0.0571, 0.04390, -1.8471 0.0283, 0.02940, -2.2760 0.0142, 0.01970, -2.7542 0.0081, 0.01410, -2.8400 0.0026, 0.00780, -2.9330 0.0000, 0.00000, -3.3891 0.0037, -0.00840, 0.1315 0.0112, -0.01420, 0.8745 0.0191, -0.01930, 1.0021 0.0397, -0.03030, 0.9841 0.0706, -0.04420, 0.8122 0.1037, -0.05710, 0.6659 0.1384, -0.06890, 0.5396 0.1741, -0.07950, 0.3920 0.2102, -0.08660, 0.2105 0.2472, -0.09640, 0.0791 0.2844, -0.10270, -0.0612 0.3225, -0.10690, -0.1307 0.3608, -0.10890, -0.2645 0.3991, -0.10830, -0.3107 0.4373, -0.10510, -0.3229 0.4757, -0.09890, -0.2796 0.5137, -0.09067, -0.2061 0.5611, -0.07859, -0.0247 16 Flap element taps 1.0000, 0.00130, -0.4057 0.9365, 0.01390, -0.4476 0.8333, 0.03280, -0.4424 0.7436, 0.04930, -0.4274 0.7049, 0.05667, -0.4203 0.6662, 0.06411, -0.4300 0.6274, 0.07172, -0.4239 0.6009, 0.07523, -0.4500 0.6069, 0.02889, -0.2390 0.6079, -0.01747, -0.2553 0.6167, -0.06381, -0.0990 0.6558, -0.05300, -0.0744 0.7045, -0.04117, 0.5443 0.7429, -0.03210, 0.4988 0.8333, -0.01400, 0.3077 0.9311, -0.00120, 0.1600 --------- Run Conditions: vel=102.7 ft/s Re=1.008x10^6 AOA=15.02 Flap deflection=10.00 Totals: Cl=1.0149 Cdp=0.1533 Cm(c/4)=-0.0841 Cs=0.1149 Ch=0.0204 Main component: Cl=0.7647 Cdp=0.0760 Cm=-0.1331 Flap component: Cl=0.2502 Cdp=0.0773 Cm=-0.2060 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.0257 0.5905, -0.01667, -0.5072 0.5709, 0.03110, -0.3799 0.5889, 0.07933, -0.4396 0.5500, 0.08689, -0.4364 0.5110, 0.09367, -0.4516 0.4731, 0.09830, -0.4491 0.4349, 0.10070, -0.4754 0.3960, 0.10120, -0.5264 0.3566, 0.10020, -0.6098 0.3172, 0.09790, -0.7302 0.2778, 0.09440, -0.8757 0.2393, 0.08960, -1.0300 0.2056, 0.08360, -1.2032 0.1633, 0.07610, -1.3551 0.1261, 0.06710, -1.5374 0.0900, 0.05640, -1.8271 0.0571, 0.04390, -2.1612 0.0283, 0.02940, -2.7757 0.0142, 0.01970, -3.4997 0.0081, 0.01410, -3.7204 0.0026, 0.00780, -4.0402 0.0000, 0.00000, -5.2763 0.0037, -0.00840, -0.5301 0.0112, -0.01420, 0.6331 0.0191, -0.01930, 0.9048 0.0397, -0.03030, 0.9982 0.0706, -0.04420, 0.8998 0.1037, -0.05710, 0.7741 0.1384, -0.06890, 0.6290 0.1741, -0.07950, 0.4913 0.2102, -0.08660, 0.3419 0.2472, -0.09640, 0.1982 0.2844, -0.10270, 0.0709 0.3225, -0.10690, -0.0379 0.3608, -0.10890, -0.1534 0.3991, -0.10830, -0.2270 0.4373, -0.10510, -0.2453 0.4757, -0.09890, -0.2098 0.5137, -0.09067, -0.1427 0.5611, -0.07859, -0.0868 16 Flap element taps 1.0000, 0.00130, -0.4505 0.9365, 0.01390, -0.4732 0.8333, 0.03280, -0.4657 0.7436, 0.04930, -0.4556 0.7049, 0.05667, -0.4442 0.6662, 0.06411, -0.4486 0.6274, 0.07172, -0.4521 0.6009, 0.07523, -0.4606 0.6069, 0.02889, -0.3865 0.6079, -0.01747, -0.4216 0.6167, -0.06381, -0.1716 0.6558, -0.05300, -0.0405 0.7045, -0.04117, 0.6474 0.7429, -0.03210, 0.5066 0.8333, -0.01400, 0.3092 0.9311, -0.00120, 0.1483 --------- Run Conditions: vel=101.6 ft/s Re=0.997x10^6 AOA=17.98 Flap deflection=10.00 Totals: Cl=0.8769 Cdp=0.2720 Cm(c/4)=-0.1296 Cs=0.0120 Ch=0.0264 Main component: Cl=0.5952 Cdp=0.1771 Cm=-0.1255 Flap component: Cl=0.2817 Cdp=0.0949 Cm=-0.2335 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1017 0.5905, -0.01667, -0.7397 0.5709, 0.03110, -0.5773 0.5889, 0.07933, -0.6754 0.5500, 0.08689, -0.6498 0.5110, 0.09367, -0.6361 0.4731, 0.09830, -0.6298 0.4349, 0.10070, -0.6378 0.3960, 0.10120, -0.6682 0.3566, 0.10020, -0.6684 0.3172, 0.09790, -0.6804 0.2778, 0.09440, -0.6953 0.2393, 0.08960, -0.7087 0.2056, 0.08360, -0.7537 0.1633, 0.07610, -0.7711 0.1261, 0.06710, -0.8587 0.0900, 0.05640, -1.0075 0.0571, 0.04390, -1.3417 0.0283, 0.02940, -1.9430 0.0142, 0.01970, -2.6320 0.0081, 0.01410, -2.8798 0.0026, 0.00780, -3.2163 0.0000, 0.00000, -4.3187 0.0037, -0.00840, -0.2935 0.0112, -0.01420, 0.6987 0.0191, -0.01930, 0.9282 0.0397, -0.03030, 1.0000 0.0706, -0.04420, 0.8959 0.1037, -0.05710, 0.7731 0.1384, -0.06890, 0.6384 0.1741, -0.07950, 0.4967 0.2102, -0.08660, 0.3385 0.2472, -0.09640, 0.1975 0.2844, -0.10270, 0.0619 0.3225, -0.10690, -0.0462 0.3608, -0.10890, -0.1717 0.3991, -0.10830, -0.2482 0.4373, -0.10510, -0.2786 0.4757, -0.09890, -0.2485 0.5137, -0.09067, -0.1782 0.5611, -0.07859, -0.1307 16 Flap element taps 1.0000, 0.00130, -0.5539 0.9365, 0.01390, -0.5898 0.8333, 0.03280, -0.6041 0.7436, 0.04930, -0.5958 0.7049, 0.05667, -0.5868 0.6662, 0.06411, -0.5971 0.6274, 0.07172, -0.5981 0.6009, 0.07523, -0.6049 0.6069, 0.02889, -0.5799 0.6079, -0.01747, -0.6269 0.6167, -0.06381, -0.3049 0.6558, -0.05300, -0.0606 0.7045, -0.04117, 0.6589 0.7429, -0.03210, 0.4712 0.8333, -0.01400, 0.2717 0.9311, -0.00120, 0.0958 --------- Run Conditions: vel=102.5 ft/s Re=1.004x10^6 AOA=19.99 Flap deflection=10.00 Totals: Cl=0.8705 Cdp=0.3584 Cm(c/4)=-0.1563 Cs=-0.0392 Ch=0.0321 Main component: Cl=0.5696 Cdp=0.2472 Cm=-0.1400 Flap component: Cl=0.3008 Cdp=0.1112 Cm=-0.2515 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1235 0.5905, -0.01667, -0.8315 0.5709, 0.03110, -0.6652 0.5889, 0.07933, -0.7687 0.5500, 0.08689, -0.7497 0.5110, 0.09367, -0.7259 0.4731, 0.09830, -0.7171 0.4349, 0.10070, -0.7227 0.3960, 0.10120, -0.7579 0.3566, 0.10020, -0.7498 0.3172, 0.09790, -0.7653 0.2778, 0.09440, -0.7793 0.2393, 0.08960, -0.7846 0.2056, 0.08360, -0.8332 0.1633, 0.07610, -0.8214 0.1261, 0.06710, -0.8548 0.0900, 0.05640, -0.8451 0.0571, 0.04390, -0.9391 0.0283, 0.02940, -1.2524 0.0142, 0.01970, -1.7455 0.0081, 0.01410, -2.0568 0.0026, 0.00780, -2.4371 0.0000, 0.00000, -3.5430 0.0037, -0.00840, -0.1502 0.0112, -0.01420, 0.7240 0.0191, -0.01930, 0.9303 0.0397, -0.03030, 1.0003 0.0706, -0.04420, 0.9019 0.1037, -0.05710, 0.7847 0.1384, -0.06890, 0.6633 0.1741, -0.07950, 0.5251 0.2102, -0.08660, 0.3621 0.2472, -0.09640, 0.2256 0.2844, -0.10270, 0.0871 0.3225, -0.10690, -0.0165 0.3608, -0.10890, -0.1478 0.3991, -0.10830, -0.2255 0.4373, -0.10510, -0.2647 0.4757, -0.09890, -0.2402 0.5137, -0.09067, -0.1709 0.5611, -0.07859, -0.1202 16 Flap element taps 1.0000, 0.00130, -0.6022 0.9365, 0.01390, -0.6439 0.8333, 0.03280, -0.6760 0.7436, 0.04930, -0.6794 0.7049, 0.05667, -0.6730 0.6662, 0.06411, -0.6872 0.6274, 0.07172, -0.6852 0.6009, 0.07523, -0.6866 0.6069, 0.02889, -0.6681 0.6079, -0.01747, -0.7220 0.6167, -0.06381, -0.3558 0.6558, -0.05300, -0.0425 0.7045, -0.04117, 0.6568 0.7429, -0.03210, 0.4623 0.8333, -0.01400, 0.2612 0.9311, -0.00120, 0.0783 --------- Run Conditions: vel=101.8 ft/s Re=0.996x10^6 AOA=23.98 Flap deflection=10.00 Totals: Cl=0.9479 Cdp=0.4913 Cm(c/4)=-0.1821 Cs=-0.0637 Ch=0.0388 Main component: Cl=0.6299 Cdp=0.3405 Cm=-0.1733 Flap component: Cl=0.3180 Cdp=0.1508 Cm=-0.2752 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1088 0.5905, -0.01667, -0.8825 0.5709, 0.03110, -0.6973 0.5889, 0.07933, -0.8214 0.5500, 0.08689, -0.8207 0.5110, 0.09367, -0.8388 0.4731, 0.09830, -0.8340 0.4349, 0.10070, -0.8519 0.3960, 0.10120, -0.8951 0.3566, 0.10020, -0.8816 0.3172, 0.09790, -0.8948 0.2778, 0.09440, -0.9162 0.2393, 0.08960, -0.9381 0.2056, 0.08360, -0.9913 0.1633, 0.07610, -0.9675 0.1261, 0.06710, -1.0207 0.0900, 0.05640, -1.0216 0.0571, 0.04390, -1.0541 0.0283, 0.02940, -1.1076 0.0142, 0.01970, -1.1634 0.0081, 0.01410, -1.4072 0.0026, 0.00780, -1.6982 0.0000, 0.00000, -3.1313 0.0037, -0.00840, -0.2301 0.0112, -0.01420, 0.6511 0.0191, -0.01930, 0.8868 0.0397, -0.03030, 1.0005 0.0706, -0.04420, 0.9369 0.1037, -0.05710, 0.8420 0.1384, -0.06890, 0.7415 0.1741, -0.07950, 0.6122 0.2102, -0.08660, 0.4487 0.2472, -0.09640, 0.3215 0.2844, -0.10270, 0.1806 0.3225, -0.10690, 0.0795 0.3608, -0.10890, -0.0581 0.3991, -0.10830, -0.1411 0.4373, -0.10510, -0.1978 0.4757, -0.09890, -0.1899 0.5137, -0.09067, -0.1229 0.5611, -0.07859, -0.0601 16 Flap element taps 1.0000, 0.00130, -0.7200 0.9365, 0.01390, -0.7436 0.8333, 0.03280, -0.7725 0.7436, 0.04930, -0.7733 0.7049, 0.05667, -0.7629 0.6662, 0.06411, -0.7782 0.6274, 0.07172, -0.7827 0.6009, 0.07523, -0.8032 0.6069, 0.02889, -0.7044 0.6079, -0.01747, -0.7512 0.6167, -0.06381, -0.3724 0.6558, -0.05300, 0.0096 0.7045, -0.04117, 0.6505 0.7429, -0.03210, 0.4550 0.8333, -0.01400, 0.2491 0.9311, -0.00120, 0.0470 --------- Run Conditions: vel=102.2 ft/s Re=1.001x10^6 AOA=27.00 Flap deflection=10.00 Totals: Cl=0.8708 Cdp=0.5539 Cm(c/4)=-0.1904 Cs=-0.0982 Ch=0.0384 Main component: Cl=0.5565 Cdp=0.3865 Cm=-0.1686 Flap component: Cl=0.3143 Cdp=0.1674 Cm=-0.2787 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1187 0.5905, -0.01667, -0.9463 0.5709, 0.03110, -0.7537 0.5889, 0.07933, -0.8590 0.5500, 0.08689, -0.8459 0.5110, 0.09367, -0.8395 0.4731, 0.09830, -0.8149 0.4349, 0.10070, -0.8057 0.3960, 0.10120, -0.8394 0.3566, 0.10020, -0.8074 0.3172, 0.09790, -0.8076 0.2778, 0.09440, -0.8057 0.2393, 0.08960, -0.8020 0.2056, 0.08360, -0.8478 0.1633, 0.07610, -0.8180 0.1261, 0.06710, -0.8533 0.0900, 0.05640, -0.8339 0.0571, 0.04390, -0.8486 0.0283, 0.02940, -0.8622 0.0142, 0.01970, -0.8725 0.0081, 0.01410, -0.9946 0.0026, 0.00780, -1.1637 0.0000, 0.00000, -2.4796 0.0037, -0.00840, -0.1199 0.0112, -0.01420, 0.6686 0.0191, -0.01930, 0.8886 0.0397, -0.03030, 1.0036 0.0706, -0.04420, 0.9522 0.1037, -0.05710, 0.8653 0.1384, -0.06890, 0.7757 0.1741, -0.07950, 0.6507 0.2102, -0.08660, 0.4880 0.2472, -0.09640, 0.3654 0.2844, -0.10270, 0.2229 0.3225, -0.10690, 0.1245 0.3608, -0.10890, -0.0181 0.3991, -0.10830, -0.1031 0.4373, -0.10510, -0.1686 0.4757, -0.09890, -0.1680 0.5137, -0.09067, -0.1026 0.5611, -0.07859, -0.0387 16 Flap element taps 1.0000, 0.00130, -0.7640 0.9365, 0.01390, -0.7779 0.8333, 0.03280, -0.7943 0.7436, 0.04930, -0.7897 0.7049, 0.05667, -0.7792 0.6662, 0.06411, -0.7925 0.6274, 0.07172, -0.7880 0.6009, 0.07523, -0.7817 0.6069, 0.02889, -0.7471 0.6079, -0.01747, -0.8058 0.6167, -0.06381, -0.4059 0.6558, -0.05300, 0.0182 0.7045, -0.04117, 0.6576 0.7429, -0.03210, 0.4508 0.8333, -0.01400, 0.2404 0.9311, -0.00120, 0.0275