S809 SPOILER FLAP, LEGR, CHORD = 18 INCHES --------- Run Conditions: vel=105.0 ft/s Re=0.997x10^6 AOA=-5.98 Flap deflection=-5.00 Totals: Cl=-0.5475 Cdp=0.0356 Cm(c/4)=0.0297 Cs=0.0216 Ch=-0.0019 Main component: Cl=-0.4492 Cdp=0.0321 Cm=0.0886 Flap component: Cl=-0.0983 Cdp=0.0035 Cm=0.0781 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.2387 0.5905, -0.01667, -0.2238 0.5709, 0.03110, -0.2178 0.5889, 0.07933, -0.2066 0.5500, 0.08689, -0.2577 0.5110, 0.09367, -0.4125 0.4731, 0.09830, -0.4148 0.4349, 0.10070, -0.4081 0.3960, 0.10120, -0.3671 0.3566, 0.10020, -0.3068 0.3172, 0.09790, -0.2322 0.2778, 0.09440, -0.1964 0.2393, 0.08960, -0.1301 0.2056, 0.08360, -0.0548 0.1633, 0.07610, 0.0453 0.1261, 0.06710, 0.1834 0.0900, 0.05640, 0.3170 0.0571, 0.04390, 0.5455 0.0283, 0.02940, 0.8016 0.0142, 0.01970, 0.9731 0.0081, 0.01410, 0.9880 0.0026, 0.00780, 0.6791 0.0000, 0.00000, -0.5992 0.0037, -0.00840, -1.5289 0.0112, -0.01420, -1.2970 0.0191, -0.01930, -1.0597 0.0397, -0.03030, -0.8081 0.0706, -0.04420, -0.8494 0.1037, -0.05710, -0.8367 0.1384, -0.06890, -0.9204 0.1741, -0.07950, -0.9552 0.2102, -0.08660, -1.0112 0.2472, -0.09640, -1.0849 0.2844, -0.10270, -1.0962 0.3225, -0.10690, -1.0821 0.3608, -0.10890, -1.0582 0.3991, -0.10830, -0.9591 0.4373, -0.10510, -0.7649 0.4757, -0.09890, -0.5162 0.5137, -0.09067, -0.3191 0.5611, -0.07859, -0.2549 16 Flap element taps 1.0000, 0.00130, -0.1770 0.9365, 0.01390, -0.0397 0.8333, 0.03280, 0.0345 0.7436, 0.04930, 0.1526 0.7049, 0.05667, 0.1690 0.6662, 0.06411, -0.1302 0.6274, 0.07172, -0.2483 0.6009, 0.07523, -0.2265 0.6069, 0.02889, -0.2200 0.6079, -0.01747, -0.2269 0.6167, -0.06381, -0.3134 0.6558, -0.05300, -0.2586 0.7045, -0.04117, -0.2523 0.7429, -0.03210, -0.2460 0.8333, -0.01400, -0.2701 0.9311, -0.00120, -0.2734 --------- Run Conditions: vel=105.0 ft/s Re=0.996x10^6 AOA=0.01 Flap deflection=-5.00 Totals: Cl=-0.2789 Cdp=-0.0037 Cm(c/4)=0.0369 Cs=0.0036 Ch=-0.0603 Main component: Cl=-0.2074 Cdp=0.0100 Cm=0.0592 Flap component: Cl=-0.0714 Cdp=-0.0137 Cm=0.0474 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1307 0.5905, -0.01667, -0.0885 0.5709, 0.03110, -0.0380 0.5889, 0.07933, -0.0667 0.5500, 0.08689, -0.1996 0.5110, 0.09367, -0.3952 0.4731, 0.09830, -0.4523 0.4349, 0.10070, -0.4918 0.3960, 0.10120, -0.4910 0.3566, 0.10020, -0.4647 0.3172, 0.09790, -0.4225 0.2778, 0.09440, -0.4190 0.2393, 0.08960, -0.3898 0.2056, 0.08360, -0.3516 0.1633, 0.07610, -0.2904 0.1261, 0.06710, -0.1944 0.0900, 0.05640, -0.1222 0.0571, 0.04390, 0.0689 0.0283, 0.02940, 0.2990 0.0142, 0.01970, 0.5579 0.0081, 0.01410, 0.7385 0.0026, 0.00780, 0.8884 0.0000, 0.00000, 0.8940 0.0037, -0.00840, 0.2147 0.0112, -0.01420, 0.0068 0.0191, -0.01930, -0.0322 0.0397, -0.03030, -0.0690 0.0706, -0.04420, -0.2690 0.1037, -0.05710, -0.3607 0.1384, -0.06890, -0.5161 0.1741, -0.07950, -0.6147 0.2102, -0.08660, -0.7248 0.2472, -0.09640, -0.8524 0.2844, -0.10270, -0.9235 0.3225, -0.10690, -0.9751 0.3608, -0.10890, -1.0258 0.3991, -0.10830, -1.0125 0.4373, -0.10510, -0.9131 0.4757, -0.09890, -0.7457 0.5137, -0.09067, -0.4867 0.5611, -0.07859, -0.2506 16 Flap element taps 1.0000, 0.00130, 0.1349 0.9365, 0.01390, 0.1000 0.8333, 0.03280, 0.0189 0.7436, 0.04930, -0.0484 0.7049, 0.05667, -0.0589 0.6662, 0.06411, -0.0709 0.6274, 0.07172, -0.0940 0.6009, 0.07523, -0.1147 0.6069, 0.02889, -0.0604 0.6079, -0.01747, -0.1511 0.6167, -0.06381, -1.1036 0.6558, -0.05300, -0.6787 0.7045, -0.04117, -0.3735 0.7429, -0.03210, -0.1968 0.8333, -0.01400, 0.0174 0.9311, -0.00120, 0.1433 Wake drag found for this condition, Cdw=0.0296 --------- Run Conditions: vel=105.2 ft/s Re=0.998x10^6 AOA=3.00 Flap deflection=-5.00 Totals: Cl=-0.0642 Cdp=-0.0156 Cm(c/4)=0.0386 Cs=0.0122 Ch=-0.0582 Main component: Cl=-0.0146 Cdp=0.0027 Cm=0.0238 Flap component: Cl=-0.0496 Cdp=-0.0182 Cm=0.0310 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1797 0.5905, -0.01667, -0.0635 0.5709, 0.03110, 0.1086 0.5889, 0.07933, -0.0304 0.5500, 0.08689, -0.1770 0.5110, 0.09367, -0.3918 0.4731, 0.09830, -0.4837 0.4349, 0.10070, -0.5491 0.3960, 0.10120, -0.5687 0.3566, 0.10020, -0.5687 0.3172, 0.09790, -0.5454 0.2778, 0.09440, -0.5648 0.2393, 0.08960, -0.5580 0.2056, 0.08360, -0.5419 0.1633, 0.07610, -0.5117 0.1261, 0.06710, -0.4463 0.0900, 0.05640, -0.4279 0.0571, 0.04390, -0.2879 0.0283, 0.02940, -0.1320 0.0142, 0.01970, 0.0723 0.0081, 0.01410, 0.2991 0.0026, 0.00780, 0.4712 0.0000, 0.00000, 0.9635 0.0037, -0.00840, 0.7802 0.0112, -0.01420, 0.5433 0.0191, -0.01930, 0.4298 0.0397, -0.03030, 0.2783 0.0706, -0.04420, 0.0444 0.1037, -0.05710, -0.0859 0.1384, -0.06890, -0.2629 0.1741, -0.07950, -0.3864 0.2102, -0.08660, -0.5083 0.2472, -0.09640, -0.6510 0.2844, -0.10270, -0.7426 0.3225, -0.10690, -0.8178 0.3608, -0.10890, -0.8901 0.3991, -0.10830, -0.9047 0.4373, -0.10510, -0.8337 0.4757, -0.09890, -0.6986 0.5137, -0.09067, -0.4620 0.5611, -0.07859, -0.2368 16 Flap element taps 1.0000, 0.00130, 0.0919 0.9365, 0.01390, 0.0559 0.8333, 0.03280, -0.0050 0.7436, 0.04930, -0.0507 0.7049, 0.05667, -0.0668 0.6662, 0.06411, -0.1117 0.6274, 0.07172, -0.2357 0.6009, 0.07523, -0.2641 0.6069, 0.02889, 0.0467 0.6079, -0.01747, -0.3279 0.6167, -0.06381, -0.9047 0.6558, -0.05300, -0.8436 0.7045, -0.04117, -0.3847 0.7429, -0.03210, -0.1213 0.8333, -0.01400, 0.0628 0.9311, -0.00120, 0.1582 Wake drag found for this condition, Cdw=0.0329 --------- Run Conditions: vel=105.3 ft/s Re=0.997x10^6 AOA=6.03 Flap deflection=-5.00 Totals: Cl=0.1999 Cdp=-0.0111 Cm(c/4)=0.0384 Cs=0.0321 Ch=-0.0485 Main component: Cl=0.2289 Cdp=0.0022 Cm=-0.0273 Flap component: Cl=-0.0290 Cdp=-0.0133 Cm=0.0164 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1406 0.5905, -0.01667, -0.0306 0.5709, 0.03110, 0.1499 0.5889, 0.07933, -0.0687 0.5500, 0.08689, -0.1903 0.5110, 0.09367, -0.4080 0.4731, 0.09830, -0.5360 0.4349, 0.10070, -0.6296 0.3960, 0.10120, -0.6691 0.3566, 0.10020, -0.6968 0.3172, 0.09790, -0.6965 0.2778, 0.09440, -0.7421 0.2393, 0.08960, -0.7624 0.2056, 0.08360, -0.7726 0.1633, 0.07610, -0.7822 0.1261, 0.06710, -0.7549 0.0900, 0.05640, -0.8097 0.0571, 0.04390, -0.7465 0.0283, 0.02940, -0.7265 0.0142, 0.01970, -0.6627 0.0081, 0.01410, -0.4038 0.0026, 0.00780, -0.2392 0.0000, 0.00000, 0.3942 0.0037, -0.00840, 0.9838 0.0112, -0.01420, 0.8944 0.0191, -0.01930, 0.7846 0.0397, -0.03030, 0.5971 0.0706, -0.04420, 0.3489 0.1037, -0.05710, 0.1942 0.1384, -0.06890, 0.0029 0.1741, -0.07950, -0.1372 0.2102, -0.08660, -0.2653 0.2472, -0.09640, -0.4251 0.2844, -0.10270, -0.5225 0.3225, -0.10690, -0.6109 0.3608, -0.10890, -0.6947 0.3991, -0.10830, -0.7310 0.4373, -0.10510, -0.6805 0.4757, -0.09890, -0.5732 0.5137, -0.09067, -0.3593 0.5611, -0.07859, -0.1466 16 Flap element taps 1.0000, 0.00130, 0.0445 0.9365, 0.01390, 0.0087 0.8333, 0.03280, -0.0474 0.7436, 0.04930, -0.1034 0.7049, 0.05667, -0.1351 0.6662, 0.06411, -0.2072 0.6274, 0.07172, -0.3332 0.6009, 0.07523, -0.3606 0.6069, 0.02889, 0.0763 0.6079, -0.01747, -0.3399 0.6167, -0.06381, -0.7363 0.6558, -0.05300, -0.7790 0.7045, -0.04117, -0.4818 0.7429, -0.03210, -0.1788 0.8333, -0.01400, 0.0632 0.9311, -0.00120, 0.1455 Wake drag found for this condition, Cdw=0.0379 --------- Run Conditions: vel=105.0 ft/s Re=0.996x10^6 AOA=9.03 Flap deflection=-5.00 Totals: Cl=0.4285 Cdp=-0.0015 Cm(c/4)=0.0378 Cs=0.0688 Ch=-0.0456 Main component: Cl=0.4375 Cdp=0.0011 Cm=-0.0681 Flap component: Cl=-0.0090 Cdp=-0.0026 Cm=0.0002 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.0960 0.5905, -0.01667, 0.0333 0.5709, 0.03110, 0.1961 0.5889, 0.07933, -0.1316 0.5500, 0.08689, -0.1975 0.5110, 0.09367, -0.3727 0.4731, 0.09830, -0.5302 0.4349, 0.10070, -0.6569 0.3960, 0.10120, -0.7213 0.3566, 0.10020, -0.7854 0.3172, 0.09790, -0.8117 0.2778, 0.09440, -0.8853 0.2393, 0.08960, -0.9327 0.2056, 0.08360, -0.9715 0.1633, 0.07610, -1.0285 0.1261, 0.06710, -1.0464 0.0900, 0.05640, -1.1768 0.0571, 0.04390, -1.2147 0.0283, 0.02940, -1.3705 0.0142, 0.01970, -1.5123 0.0081, 0.01410, -1.3095 0.0026, 0.00780, -1.2622 0.0000, 0.00000, -0.8509 0.0037, -0.00840, 0.8316 0.0112, -0.01420, 0.9976 0.0191, -0.01930, 0.9629 0.0397, -0.03030, 0.8100 0.0706, -0.04420, 0.5826 0.1037, -0.05710, 0.4213 0.1384, -0.06890, 0.2216 0.1741, -0.07950, 0.0761 0.2102, -0.08660, -0.0573 0.2472, -0.09640, -0.2192 0.2844, -0.10270, -0.3328 0.3225, -0.10690, -0.4408 0.3608, -0.10890, -0.5346 0.3991, -0.10830, -0.5915 0.4373, -0.10510, -0.5504 0.4757, -0.09890, -0.4647 0.5137, -0.09067, -0.2636 0.5611, -0.07859, -0.0532 16 Flap element taps 1.0000, 0.00130, -0.0268 0.9365, 0.01390, -0.0686 0.8333, 0.03280, -0.1087 0.7436, 0.04930, -0.1657 0.7049, 0.05667, -0.2101 0.6662, 0.06411, -0.2674 0.6274, 0.07172, -0.3639 0.6009, 0.07523, -0.3896 0.6069, 0.02889, 0.1166 0.6079, -0.01747, -0.2797 0.6167, -0.06381, -0.6644 0.6558, -0.05300, -0.7257 0.7045, -0.04117, -0.5397 0.7429, -0.03210, -0.2269 0.8333, -0.01400, 0.0618 0.9311, -0.00120, 0.1284 Wake drag found for this condition, Cdw=0.0456 --------- Run Conditions: vel=106.2 ft/s Re=1.007x10^6 AOA=12.03 Flap deflection=-5.00 Totals: Cl=0.6186 Cdp=0.0079 Cm(c/4)=0.0314 Cs=0.1212 Ch=-0.0454 Main component: Cl=0.5928 Cdp=0.0084 Cm=-0.0929 Flap component: Cl=0.0258 Cdp=-0.0005 Cm=-0.0274 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1341 0.5905, -0.01667, 0.0414 0.5709, 0.03110, 0.2114 0.5889, 0.07933, -0.2086 0.5500, 0.08689, -0.2340 0.5110, 0.09367, -0.3125 0.4731, 0.09830, -0.4450 0.4349, 0.10070, -0.5995 0.3960, 0.10120, -0.6987 0.3566, 0.10020, -0.8065 0.3172, 0.09790, -0.8677 0.2778, 0.09440, -0.9742 0.2393, 0.08960, -1.0508 0.2056, 0.08360, -1.1224 0.1633, 0.07610, -1.2296 0.1261, 0.06710, -1.2987 0.0900, 0.05640, -1.5045 0.0571, 0.04390, -1.6580 0.0283, 0.02940, -2.0097 0.0142, 0.01970, -2.3781 0.0081, 0.01410, -2.3433 0.0026, 0.00780, -2.3952 0.0000, 0.00000, -2.5467 0.0037, -0.00840, 0.3923 0.0112, -0.01420, 0.9374 0.0191, -0.01930, 1.0026 0.0397, -0.03030, 0.9340 0.0706, -0.04420, 0.7492 0.1037, -0.05710, 0.5952 0.1384, -0.06890, 0.3947 0.1741, -0.07950, 0.2519 0.2102, -0.08660, 0.1193 0.2472, -0.09640, -0.0497 0.2844, -0.10270, -0.1698 0.3225, -0.10690, -0.2982 0.3608, -0.10890, -0.4024 0.3991, -0.10830, -0.4835 0.4373, -0.10510, -0.4574 0.4757, -0.09890, -0.3916 0.5137, -0.09067, -0.3066 0.5611, -0.07859, 0.0126 16 Flap element taps 1.0000, 0.00130, -0.1220 0.9365, 0.01390, -0.1700 0.8333, 0.03280, -0.1881 0.7436, 0.04930, -0.2329 0.7049, 0.05667, -0.2640 0.6662, 0.06411, -0.3051 0.6274, 0.07172, -0.3489 0.6009, 0.07523, -0.3868 0.6069, 0.02889, 0.1382 0.6079, -0.01747, -0.3130 0.6167, -0.06381, -0.8212 0.6558, -0.05300, -0.8139 0.7045, -0.04117, -0.3175 0.7429, -0.03210, -0.0482 0.8333, -0.01400, 0.0691 0.9311, -0.00120, 0.0968 Wake drag found for this condition, Cdw=0.0566 --------- Run Conditions: vel=105.7 ft/s Re=1.001x10^6 AOA=15.00 Flap deflection=-5.00 Totals: Cl=0.7032 Cdp=0.0271 Cm(c/4)=0.0336 Cs=0.1558 Ch=-0.0516 Main component: Cl=0.6686 Cdp=0.0172 Cm=-0.1009 Flap component: Cl=0.0346 Cdp=0.0099 Cm=-0.0370 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1574 0.5905, -0.01667, 0.0319 0.5709, 0.03110, 0.2520 0.5889, 0.07933, -0.2889 0.5500, 0.08689, -0.3124 0.5110, 0.09367, -0.3152 0.4731, 0.09830, -0.3306 0.4349, 0.10070, -0.4008 0.3960, 0.10120, -0.5058 0.3566, 0.10020, -0.6442 0.3172, 0.09790, -0.7638 0.2778, 0.09440, -0.8997 0.2393, 0.08960, -1.0251 0.2056, 0.08360, -1.1537 0.1633, 0.07610, -1.2949 0.1261, 0.06710, -1.4317 0.0900, 0.05640, -1.6946 0.0571, 0.04390, -1.9663 0.0283, 0.02940, -2.4788 0.0142, 0.01970, -3.0732 0.0081, 0.01410, -3.1941 0.0026, 0.00780, -3.4242 0.0000, 0.00000, -4.2515 0.0037, -0.00840, -0.1504 0.0112, -0.01420, 0.7731 0.0191, -0.01930, 0.9587 0.0397, -0.03030, 0.9860 0.0706, -0.04420, 0.8481 0.1037, -0.05710, 0.7075 0.1384, -0.06890, 0.5356 0.1741, -0.07950, 0.3904 0.2102, -0.08660, 0.2424 0.2472, -0.09640, 0.0824 0.2844, -0.10270, -0.0569 0.3225, -0.10690, -0.1826 0.3608, -0.10890, -0.2982 0.3991, -0.10830, -0.3845 0.4373, -0.10510, -0.3816 0.4757, -0.09890, -0.3245 0.5137, -0.09067, -0.2574 0.5611, -0.07859, 0.0574 16 Flap element taps 1.0000, 0.00130, -0.2379 0.9365, 0.01390, -0.2758 0.8333, 0.03280, -0.2826 0.7436, 0.04930, -0.2966 0.7049, 0.05667, -0.2873 0.6662, 0.06411, -0.2864 0.6274, 0.07172, -0.2829 0.6009, 0.07523, -0.3365 0.6069, 0.02889, 0.1476 0.6079, -0.01747, -0.3433 0.6167, -0.06381, -0.7577 0.6558, -0.05300, -0.7919 0.7045, -0.04117, -0.3797 0.7429, -0.03210, -0.0780 0.8333, -0.01400, 0.0477 0.9311, -0.00120, 0.0410 Wake drag found for this condition, Cdw=0.0754 --------- Run Conditions: vel=106.6 ft/s Re=1.009x10^6 AOA=18.00 Flap deflection=-5.00 Totals: Cl=0.7007 Cdp=0.0915 Cm(c/4)=0.0067 Cs=0.1295 Ch=-0.0505 Main component: Cl=0.6380 Cdp=0.0670 Cm=-0.1052 Flap component: Cl=0.0627 Cdp=0.0245 Cm=-0.0618 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.2069 0.5905, -0.01667, -0.0105 0.5709, 0.03110, 0.1884 0.5889, 0.07933, -0.4965 0.5500, 0.08689, -0.5089 0.5110, 0.09367, -0.5350 0.4731, 0.09830, -0.5376 0.4349, 0.10070, -0.5508 0.3960, 0.10120, -0.5503 0.3566, 0.10020, -0.5814 0.3172, 0.09790, -0.6131 0.2778, 0.09440, -0.6681 0.2393, 0.08960, -0.7372 0.2056, 0.08360, -0.8435 0.1633, 0.07610, -0.9939 0.1261, 0.06710, -1.1671 0.0900, 0.05640, -1.4635 0.0571, 0.04390, -1.8359 0.0283, 0.02940, -2.4540 0.0142, 0.01970, -3.1668 0.0081, 0.01410, -3.3870 0.0026, 0.00780, -3.7223 0.0000, 0.00000, -4.9350 0.0037, -0.00840, -0.4367 0.0112, -0.01420, 0.6636 0.0191, -0.01930, 0.9147 0.0397, -0.03030, 0.9976 0.0706, -0.04420, 0.8903 0.1037, -0.05710, 0.7631 0.1384, -0.06890, 0.5951 0.1741, -0.07950, 0.4509 0.2102, -0.08660, 0.3073 0.2472, -0.09640, 0.1415 0.2844, -0.10270, -0.0009 0.3225, -0.10690, -0.1374 0.3608, -0.10890, -0.2600 0.3991, -0.10830, -0.3594 0.4373, -0.10510, -0.3678 0.4757, -0.09890, -0.3243 0.5137, -0.09067, -0.2507 0.5611, -0.07859, 0.0135 16 Flap element taps 1.0000, 0.00130, -0.3866 0.9365, 0.01390, -0.4421 0.8333, 0.03280, -0.4437 0.7436, 0.04930, -0.4361 0.7049, 0.05667, -0.4198 0.6662, 0.06411, -0.4155 0.6274, 0.07172, -0.4156 0.6009, 0.07523, -0.4705 0.6069, 0.02889, 0.0889 0.6079, -0.01747, -0.4115 0.6167, -0.06381, -0.7657 0.6558, -0.05300, -0.8191 0.7045, -0.04117, -0.5022 0.7429, -0.03210, -0.1566 0.8333, -0.01400, 0.0019 0.9311, -0.00120, -0.0352 --------- Run Conditions: vel=105.3 ft/s Re=0.996x10^6 AOA=20.00 Flap deflection=-5.00 Totals: Cl=0.6244 Cdp=0.1689 Cm(c/4)=-0.0224 Cs=0.0548 Ch=-0.0497 Main component: Cl=0.5504 Cdp=0.1361 Cm=-0.1110 Flap component: Cl=0.0740 Cdp=0.0328 Cm=-0.0725 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.2528 0.5905, -0.01667, -0.0444 0.5709, 0.03110, 0.1562 0.5889, 0.07933, -0.6619 0.5500, 0.08689, -0.6823 0.5110, 0.09367, -0.6540 0.4731, 0.09830, -0.6432 0.4349, 0.10070, -0.6934 0.3960, 0.10120, -0.7009 0.3566, 0.10020, -0.7241 0.3172, 0.09790, -0.7273 0.2778, 0.09440, -0.7367 0.2393, 0.08960, -0.7278 0.2056, 0.08360, -0.7443 0.1633, 0.07610, -0.7861 0.1261, 0.06710, -0.8182 0.0900, 0.05640, -0.8961 0.0571, 0.04390, -1.1006 0.0283, 0.02940, -1.5942 0.0142, 0.01970, -2.2372 0.0081, 0.01410, -2.4989 0.0026, 0.00780, -2.8751 0.0000, 0.00000, -3.9659 0.0037, -0.00840, -0.2097 0.0112, -0.01420, 0.7233 0.0191, -0.01930, 0.9334 0.0397, -0.03030, 0.9971 0.0706, -0.04420, 0.8900 0.1037, -0.05710, 0.7649 0.1384, -0.06890, 0.5979 0.1741, -0.07950, 0.4555 0.2102, -0.08660, 0.3137 0.2472, -0.09640, 0.1462 0.2844, -0.10270, 0.0025 0.3225, -0.10690, -0.1370 0.3608, -0.10890, -0.2647 0.3991, -0.10830, -0.3696 0.4373, -0.10510, -0.3830 0.4757, -0.09890, -0.3427 0.5137, -0.09067, -0.2650 0.5611, -0.07859, -0.0306 16 Flap element taps 1.0000, 0.00130, -0.4671 0.9365, 0.01390, -0.5230 0.8333, 0.03280, -0.5327 0.7436, 0.04930, -0.5280 0.7049, 0.05667, -0.5076 0.6662, 0.06411, -0.4937 0.6274, 0.07172, -0.4914 0.6009, 0.07523, -0.5476 0.6069, 0.02889, 0.0549 0.6079, -0.01747, -0.4584 0.6167, -0.06381, -0.8127 0.6558, -0.05300, -0.8692 0.7045, -0.04117, -0.5631 0.7429, -0.03210, -0.1997 0.8333, -0.01400, -0.0422 0.9311, -0.00120, -0.0837 --------- Run Conditions: vel=105.2 ft/s Re=0.994x10^6 AOA=24.01 Flap deflection=-5.00 Totals: Cl=0.6464 Cdp=0.2967 Cm(c/4)=-0.0550 Cs=-0.0080 Ch=-0.0449 Main component: Cl=0.5500 Cdp=0.2450 Cm=-0.1385 Flap component: Cl=0.0964 Cdp=0.0516 Cm=-0.0943 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.2618 0.5905, -0.01667, -0.0548 0.5709, 0.03110, 0.1217 0.5889, 0.07933, -0.8439 0.5500, 0.08689, -0.8626 0.5110, 0.09367, -0.8537 0.4731, 0.09830, -0.8052 0.4349, 0.10070, -0.7943 0.3960, 0.10120, -0.7971 0.3566, 0.10020, -0.8318 0.3172, 0.09790, -0.8456 0.2778, 0.09440, -0.8625 0.2393, 0.08960, -0.8504 0.2056, 0.08360, -0.8428 0.1633, 0.07610, -0.8575 0.1261, 0.06710, -0.8462 0.0900, 0.05640, -0.8484 0.0571, 0.04390, -0.8572 0.0283, 0.02940, -0.9013 0.0142, 0.01970, -1.0256 0.0081, 0.01410, -1.2415 0.0026, 0.00780, -1.6016 0.0000, 0.00000, -2.7561 0.0037, -0.00840, -0.0419 0.0112, -0.01420, 0.7369 0.0191, -0.01930, 0.9290 0.0397, -0.03030, 1.0014 0.0706, -0.04420, 0.9191 0.1037, -0.05710, 0.8133 0.1384, -0.06890, 0.6618 0.1741, -0.07950, 0.5285 0.2102, -0.08660, 0.3940 0.2472, -0.09640, 0.2317 0.2844, -0.10270, 0.0883 0.3225, -0.10690, -0.0529 0.3608, -0.10890, -0.1865 0.3991, -0.10830, -0.3000 0.4373, -0.10510, -0.3257 0.4757, -0.09890, -0.3017 0.5137, -0.09067, -0.2226 0.5611, -0.07859, -0.0773 16 Flap element taps 1.0000, 0.00130, -0.5820 0.9365, 0.01390, -0.6325 0.8333, 0.03280, -0.6389 0.7436, 0.04930, -0.6345 0.7049, 0.05667, -0.6143 0.6662, 0.06411, -0.5994 0.6274, 0.07172, -0.5950 0.6009, 0.07523, -0.6451 0.6069, 0.02889, 0.0204 0.6079, -0.01747, -0.4901 0.6167, -0.06381, -0.7944 0.6558, -0.05300, -0.8525 0.7045, -0.04117, -0.6284 0.7429, -0.03210, -0.2480 0.8333, -0.01400, -0.0604 0.9311, -0.00120, -0.1293 --------- Run Conditions: vel=105.2 ft/s Re=0.996x10^6 AOA=27.00 Flap deflection=-5.00 Totals: Cl=0.7093 Cdp=0.3588 Cm(c/4)=-0.0641 Cs=0.0023 Ch=-0.0395 Main component: Cl=0.5990 Cdp=0.2929 Cm=-0.1541 Flap component: Cl=0.1103 Cdp=0.0659 Cm=-0.1087 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.2681 0.5905, -0.01667, -0.0639 0.5709, 0.03110, 0.0911 0.5889, 0.07933, -0.8686 0.5500, 0.08689, -0.8824 0.5110, 0.09367, -0.8930 0.4731, 0.09830, -0.8636 0.4349, 0.10070, -0.8589 0.3960, 0.10120, -0.8381 0.3566, 0.10020, -0.8405 0.3172, 0.09790, -0.8338 0.2778, 0.09440, -0.8516 0.2393, 0.08960, -0.8572 0.2056, 0.08360, -0.8907 0.1633, 0.07610, -0.9521 0.1261, 0.06710, -1.0259 0.0900, 0.05640, -1.0746 0.0571, 0.04390, -1.0558 0.0283, 0.02940, -1.0868 0.0142, 0.01970, -1.1705 0.0081, 0.01410, -1.3168 0.0026, 0.00780, -1.5874 0.0000, 0.00000, -3.1228 0.0037, -0.00840, -0.2863 0.0112, -0.01420, 0.6254 0.0191, -0.01930, 0.8742 0.0397, -0.03030, 1.0018 0.0706, -0.04420, 0.9506 0.1037, -0.05710, 0.8620 0.1384, -0.06890, 0.7221 0.1741, -0.07950, 0.5934 0.2102, -0.08660, 0.4642 0.2472, -0.09640, 0.3042 0.2844, -0.10270, 0.1608 0.3225, -0.10690, 0.0160 0.3608, -0.10890, -0.1198 0.3991, -0.10830, -0.2427 0.4373, -0.10510, -0.2754 0.4757, -0.09890, -0.2632 0.5137, -0.09067, -0.1877 0.5611, -0.07859, -0.0797 16 Flap element taps 1.0000, 0.00130, -0.6482 0.9365, 0.01390, -0.6864 0.8333, 0.03280, -0.6959 0.7436, 0.04930, -0.6922 0.7049, 0.05667, -0.6781 0.6662, 0.06411, -0.6644 0.6274, 0.07172, -0.6667 0.6009, 0.07523, -0.7155 0.6069, 0.02889, 0.0062 0.6079, -0.01747, -0.4983 0.6167, -0.06381, -0.7832 0.6558, -0.05300, -0.8423 0.7045, -0.04117, -0.6347 0.7429, -0.03210, -0.2525 0.8333, -0.01400, -0.0662 0.9311, -0.00120, -0.1550