S809 SPOILER FLAP, CLEAN, CHORD = 18 INCHES --------- Run Conditions: vel=104.6 ft/s Re=1.005x10^6 AOA=-6.06 Flap deflection=60.00 Totals: Cl=-0.0253 Cdp=0.4749 Cm(c/4)=-0.1320 Cs=-0.4695 Ch=0.0865 Main component: Cl=-0.3392 Cdp=-0.0660 Cm=0.0715 Flap component: Cl=0.3140 Cdp=0.5409 Cm=-0.1846 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.4983 0.5905, -0.01667, 0.4973 0.5709, 0.03110, 0.5099 0.5889, 0.07933, 0.4969 0.5500, 0.08689, 0.4436 0.5110, 0.09367, 0.1941 0.4731, 0.09830, 0.0771 0.4349, 0.10070, 0.0543 0.3960, 0.10120, -0.0013 0.3566, 0.10020, -0.0203 0.3172, 0.09790, -0.0185 0.2778, 0.09440, -0.0259 0.2393, 0.08960, -0.0014 0.2056, 0.08360, 0.0170 0.1633, 0.07610, 0.0927 0.1261, 0.06710, 0.1782 0.0900, 0.05640, 0.3028 0.0571, 0.04390, 0.4735 0.0283, 0.02940, 0.7187 0.0142, 0.01970, 0.9136 0.0081, 0.01410, 0.9770 0.0026, 0.00780, 0.8903 0.0000, 0.00000, 0.2013 0.0037, -0.00840, -0.6684 0.0112, -0.01420, -0.6118 0.0191, -0.01930, -0.5196 0.0397, -0.03030, -0.4332 0.0706, -0.04420, -0.4479 0.1037, -0.05710, -0.4937 0.1384, -0.06890, -0.5338 0.1741, -0.07950, -0.5752 0.2102, -0.08660, -0.6208 0.2472, -0.09640, -0.6583 0.2844, -0.10270, -0.6537 0.3225, -0.10690, -0.6154 0.3608, -0.10890, -0.5712 0.3991, -0.10830, -0.5238 0.4373, -0.10510, -0.4724 0.4757, -0.09890, -0.0194 0.5137, -0.09067, 0.2008 0.5611, -0.07859, 0.4016 16 Flap element taps 1.0000, 0.00130, -1.1414 0.9365, 0.01390, -1.1426 0.8333, 0.03280, -1.1564 0.7436, 0.04930, -1.1540 0.7049, 0.05667, -1.1424 0.6662, 0.06411, -1.1434 0.6274, 0.07172, -1.1159 0.6009, 0.07523, -1.1575 0.6069, 0.02889, 0.1695 0.6079, -0.01747, 0.2880 0.6167, -0.06381, 1.0112 0.6558, -0.05300, 0.7163 0.7045, -0.04117, 0.5973 0.7429, -0.03210, 0.5541 0.8333, -0.01400, 0.5834 0.9311, -0.00120, 0.3985 --------- Run Conditions: vel=103.5 ft/s Re=0.994x10^6 AOA=0.03 Flap deflection=60.00 Totals: Cl=0.2873 Cdp=0.5139 Cm(c/4)=-0.1223 Cs=-0.5137 Ch=0.0820 Main component: Cl=0.0072 Cdp=-0.0863 Cm=0.0111 Flap component: Cl=0.2802 Cdp=0.6002 Cm=-0.2053 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.5592 0.5905, -0.01667, 0.5533 0.5709, 0.03110, 0.5636 0.5889, 0.07933, 0.5481 0.5500, 0.08689, 0.4593 0.5110, 0.09367, 0.2747 0.4731, 0.09830, 0.1332 0.4349, 0.10070, -0.1260 0.3960, 0.10120, -0.1765 0.3566, 0.10020, -0.1931 0.3172, 0.09790, -0.2302 0.2778, 0.09440, -0.2781 0.2393, 0.08960, -0.2921 0.2056, 0.08360, -0.3298 0.1633, 0.07610, -0.2881 0.1261, 0.06710, -0.2616 0.0900, 0.05640, -0.1955 0.0571, 0.04390, -0.1100 0.0283, 0.02940, 0.0578 0.0142, 0.01970, 0.2673 0.0081, 0.01410, 0.4046 0.0026, 0.00780, 0.6779 0.0000, 0.00000, 0.9841 0.0037, -0.00840, 0.7808 0.0112, -0.01420, 0.5641 0.0191, -0.01930, 0.4652 0.0397, -0.03030, 0.3062 0.0706, -0.04420, 0.1403 0.1037, -0.05710, 0.0152 0.1384, -0.06890, -0.0728 0.1741, -0.07950, -0.1621 0.2102, -0.08660, -0.2601 0.2472, -0.09640, -0.3309 0.2844, -0.10270, -0.3720 0.3225, -0.10690, -0.3652 0.3608, -0.10890, -0.3669 0.3991, -0.10830, -0.2959 0.4373, -0.10510, -0.2730 0.4757, -0.09890, -0.0360 0.5137, -0.09067, 0.2523 0.5611, -0.07859, 0.4274 16 Flap element taps 1.0000, 0.00130, -1.2269 0.9365, 0.01390, -1.2383 0.8333, 0.03280, -1.2378 0.7436, 0.04930, -1.2300 0.7049, 0.05667, -1.2185 0.6662, 0.06411, -1.2173 0.6274, 0.07172, -1.1771 0.6009, 0.07523, -1.2066 0.6069, 0.02889, 0.0674 0.6079, -0.01747, 0.1495 0.6167, -0.06381, 1.0139 0.6558, -0.05300, 0.7074 0.7045, -0.04117, 0.6092 0.7429, -0.03210, 0.5692 0.8333, -0.01400, 0.6151 0.9311, -0.00120, 0.4695 --------- Run Conditions: vel=103.8 ft/s Re=0.997x10^6 AOA=3.03 Flap deflection=60.00 Totals: Cl=0.2969 Cdp=0.5126 Cm(c/4)=-0.1121 Cs=-0.4962 Ch=0.0580 Main component: Cl=0.0419 Cdp=-0.0827 Cm=0.0209 Flap component: Cl=0.2550 Cdp=0.5953 Cm=-0.2138 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.5289 0.5905, -0.01667, 0.5189 0.5709, 0.03110, 0.5295 0.5889, 0.07933, 0.4928 0.5500, 0.08689, 0.4916 0.5110, 0.09367, 0.4385 0.4731, 0.09830, 0.2708 0.4349, 0.10070, 0.0914 0.3960, 0.10120, -0.0704 0.3566, 0.10020, -0.1907 0.3172, 0.09790, -0.2305 0.2778, 0.09440, -0.2907 0.2393, 0.08960, -0.3274 0.2056, 0.08360, -0.3987 0.1633, 0.07610, -0.3722 0.1261, 0.06710, -0.3812 0.0900, 0.05640, -0.3475 0.0571, 0.04390, -0.3118 0.0283, 0.02940, -0.2104 0.0142, 0.01970, -0.0525 0.0081, 0.01410, 0.0538 0.0026, 0.00780, 0.3072 0.0000, 0.00000, 0.8283 0.0037, -0.00840, 0.9558 0.0112, -0.01420, 0.7799 0.0191, -0.01930, 0.6715 0.0397, -0.03030, 0.4836 0.0706, -0.04420, 0.2857 0.1037, -0.05710, 0.1418 0.1384, -0.06890, 0.0452 0.1741, -0.07950, -0.0641 0.2102, -0.08660, -0.1866 0.2472, -0.09640, -0.2713 0.2844, -0.10270, -0.3357 0.3225, -0.10690, -0.3424 0.3608, -0.10890, -0.3743 0.3991, -0.10830, -0.3118 0.4373, -0.10510, -0.2677 0.4757, -0.09890, -0.2755 0.5137, -0.09067, 0.2005 0.5611, -0.07859, 0.3665 16 Flap element taps 1.0000, 0.00130, -1.1991 0.9365, 0.01390, -1.2123 0.8333, 0.03280, -1.2564 0.7436, 0.04930, -1.2401 0.7049, 0.05667, -1.2255 0.6662, 0.06411, -1.2334 0.6274, 0.07172, -1.1890 0.6009, 0.07523, -1.2021 0.6069, 0.02889, -0.0487 0.6079, -0.01747, 0.0280 0.6167, -0.06381, 0.6532 0.6558, -0.05300, 0.5240 0.7045, -0.04117, 0.5356 0.7429, -0.03210, 0.5267 0.8333, -0.01400, 0.5852 0.9311, -0.00120, 0.6031 --------- Run Conditions: vel=104.4 ft/s Re=1.003x10^6 AOA=6.02 Flap deflection=60.00 Totals: Cl=0.4142 Cdp=0.4989 Cm(c/4)=-0.1307 Cs=-0.4527 Ch=0.0141 Main component: Cl=0.1388 Cdp=-0.0646 Cm=0.0120 Flap component: Cl=0.2754 Cdp=0.5635 Cm=-0.2588 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.3838 0.5905, -0.01667, 0.3705 0.5709, 0.03110, 0.3863 0.5889, 0.07933, 0.3949 0.5500, 0.08689, 0.4369 0.5110, 0.09367, 0.4382 0.4731, 0.09830, 0.3875 0.4349, 0.10070, 0.1912 0.3960, 0.10120, -0.0092 0.3566, 0.10020, -0.0858 0.3172, 0.09790, -0.2012 0.2778, 0.09440, -0.3607 0.2393, 0.08960, -0.4025 0.2056, 0.08360, -0.5036 0.1633, 0.07610, -0.5046 0.1261, 0.06710, -0.5582 0.0900, 0.05640, -0.5735 0.0571, 0.04390, -0.6173 0.0283, 0.02940, -0.6296 0.0142, 0.01970, -0.5844 0.0081, 0.01410, -0.5647 0.0026, 0.00780, -0.3021 0.0000, 0.00000, 0.2246 0.0037, -0.00840, 0.9895 0.0112, -0.01420, 0.9558 0.0191, -0.01930, 0.8730 0.0397, -0.03030, 0.6867 0.0706, -0.04420, 0.4722 0.1037, -0.05710, 0.3166 0.1384, -0.06890, 0.2121 0.1741, -0.07950, 0.0901 0.2102, -0.08660, -0.0527 0.2472, -0.09640, -0.1498 0.2844, -0.10270, -0.2363 0.3225, -0.10690, -0.2619 0.3608, -0.10890, -0.3242 0.3991, -0.10830, -0.2923 0.4373, -0.10510, -0.2316 0.4757, -0.09890, -0.2158 0.5137, -0.09067, 0.1230 0.5611, -0.07859, 0.2639 16 Flap element taps 1.0000, 0.00130, -1.1217 0.9365, 0.01390, -1.1398 0.8333, 0.03280, -1.1661 0.7436, 0.04930, -1.1521 0.7049, 0.05667, -1.1412 0.6662, 0.06411, -1.1655 0.6274, 0.07172, -1.1298 0.6009, 0.07523, -1.1739 0.6069, 0.02889, -0.2627 0.6079, -0.01747, -0.6961 0.6167, -0.06381, -0.1005 0.6558, -0.05300, 0.3483 0.7045, -0.04117, 0.4429 0.7429, -0.03210, 0.4597 0.8333, -0.01400, 0.9854 0.9311, -0.00120, 0.7189 --------- Run Conditions: vel=104.9 ft/s Re=1.005x10^6 AOA=9.05 Flap deflection=60.00 Totals: Cl=0.5793 Cdp=0.4609 Cm(c/4)=-0.1627 Cs=-0.3640 Ch=-0.0175 Main component: Cl=0.2503 Cdp=-0.0209 Cm=-0.0048 Flap component: Cl=0.3289 Cdp=0.4818 Cm=-0.3191 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.1055 0.5905, -0.01667, 0.0904 0.5709, 0.03110, 0.1008 0.5889, 0.07933, 0.0985 0.5500, 0.08689, 0.2588 0.5110, 0.09367, 0.2517 0.4731, 0.09830, 0.2673 0.4349, 0.10070, 0.2307 0.3960, 0.10120, 0.1159 0.3566, 0.10020, -0.0071 0.3172, 0.09790, -0.1592 0.2778, 0.09440, -0.3141 0.2393, 0.08960, -0.4319 0.2056, 0.08360, -0.5755 0.1633, 0.07610, -0.6424 0.1261, 0.06710, -0.7620 0.0900, 0.05640, -0.8480 0.0571, 0.04390, -0.9867 0.0283, 0.02940, -1.1565 0.0142, 0.01970, -1.2768 0.0081, 0.01410, -1.3992 0.0026, 0.00780, -1.2119 0.0000, 0.00000, -0.9208 0.0037, -0.00840, 0.8087 0.0112, -0.01420, 1.0024 0.0191, -0.01930, 0.9905 0.0397, -0.03030, 0.8507 0.0706, -0.04420, 0.6478 0.1037, -0.05710, 0.4892 0.1384, -0.06890, 0.3731 0.1741, -0.07950, 0.2440 0.2102, -0.08660, 0.0939 0.2472, -0.09640, -0.0182 0.2844, -0.10270, -0.1189 0.3225, -0.10690, -0.1700 0.3608, -0.10890, -0.2515 0.3991, -0.10830, -0.2527 0.4373, -0.10510, -0.2091 0.4757, -0.09890, -0.1598 0.5137, -0.09067, -0.1312 0.5611, -0.07859, 0.1834 16 Flap element taps 1.0000, 0.00130, -1.0084 0.9365, 0.01390, -1.0206 0.8333, 0.03280, -1.0494 0.7436, 0.04930, -1.0601 0.7049, 0.05667, -1.0527 0.6662, 0.06411, -1.0709 0.6274, 0.07172, -1.0418 0.6009, 0.07523, -1.1279 0.6069, 0.02889, -1.1503 0.6079, -0.01747, -1.8481 0.6167, -0.06381, -0.7468 0.6558, -0.05300, 0.0790 0.7045, -0.04117, 0.4074 0.7429, -0.03210, 0.6580 0.8333, -0.01400, 0.9882 0.9311, -0.00120, 0.7501 --------- Run Conditions: vel=105.2 ft/s Re=1.007x10^6 AOA=12.06 Flap deflection=60.00 Totals: Cl=0.6871 Cdp=0.4731 Cm(c/4)=-0.1777 Cs=-0.3191 Ch=-0.0384 Main component: Cl=0.3517 Cdp=0.0159 Cm=-0.0293 Flap component: Cl=0.3353 Cdp=0.4572 Cm=-0.3411 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.0862 0.5905, -0.01667, -0.1220 0.5709, 0.03110, -0.1059 0.5889, 0.07933, -0.0812 0.5500, 0.08689, 0.1074 0.5110, 0.09367, 0.1006 0.4731, 0.09830, 0.1076 0.4349, 0.10070, 0.1038 0.3960, 0.10120, 0.0762 0.3566, 0.10020, 0.0652 0.3172, 0.09790, -0.0499 0.2778, 0.09440, -0.2386 0.2393, 0.08960, -0.4040 0.2056, 0.08360, -0.5898 0.1633, 0.07610, -0.7028 0.1261, 0.06710, -0.8488 0.0900, 0.05640, -1.0081 0.0571, 0.04390, -1.2131 0.0283, 0.02940, -1.6146 0.0142, 0.01970, -1.9012 0.0081, 0.01410, -2.2214 0.0026, 0.00780, -2.1396 0.0000, 0.00000, -2.1995 0.0037, -0.00840, 0.4617 0.0112, -0.01420, 0.9418 0.0191, -0.01930, 1.0091 0.0397, -0.03030, 0.9418 0.0706, -0.04420, 0.7695 0.1037, -0.05710, 0.6218 0.1384, -0.06890, 0.4945 0.1741, -0.07950, 0.3646 0.2102, -0.08660, 0.2211 0.2472, -0.09640, 0.0988 0.2844, -0.10270, -0.0100 0.3225, -0.10690, -0.0779 0.3608, -0.10890, -0.1698 0.3991, -0.10830, -0.1980 0.4373, -0.10510, -0.1730 0.4757, -0.09890, -0.1163 0.5137, -0.09067, -0.0641 0.5611, -0.07859, 0.1727 16 Flap element taps 1.0000, 0.00130, -0.9688 0.9365, 0.01390, -0.9726 0.8333, 0.03280, -0.9971 0.7436, 0.04930, -1.0103 0.7049, 0.05667, -1.0109 0.6662, 0.06411, -1.0315 0.6274, 0.07172, -1.0196 0.6009, 0.07523, -1.3705 0.6069, 0.02889, -1.8588 0.6079, -0.01747, -1.8389 0.6167, -0.06381, -1.0021 0.6558, -0.05300, -0.0946 0.7045, -0.04117, 0.3645 0.7429, -0.03210, 0.6613 0.8333, -0.01400, 0.9878 0.9311, -0.00120, 0.7753 --------- Run Conditions: vel=104.6 ft/s Re=1.001x10^6 AOA=15.04 Flap deflection=60.00 Totals: Cl=0.6505 Cdp=0.5380 Cm(c/4)=-0.1606 Cs=-0.3508 Ch=-0.0365 Main component: Cl=0.3792 Cdp=0.0510 Cm=-0.0401 Flap component: Cl=0.2713 Cdp=0.4870 Cm=-0.3125 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1880 0.5905, -0.01667, -0.2467 0.5709, 0.03110, -0.2302 0.5889, 0.07933, -0.2045 0.5500, 0.08689, 0.0010 0.5110, 0.09367, 0.0126 0.4731, 0.09830, 0.0070 0.4349, 0.10070, -0.0001 0.3960, 0.10120, -0.0256 0.3566, 0.10020, 0.0015 0.3172, 0.09790, -0.0090 0.2778, 0.09440, -0.0530 0.2393, 0.08960, -0.1624 0.2056, 0.08360, -0.3995 0.1633, 0.07610, -0.5694 0.1261, 0.06710, -0.7783 0.0900, 0.05640, -0.9937 0.0571, 0.04390, -1.2934 0.0283, 0.02940, -1.7210 0.0142, 0.01970, -2.2821 0.0081, 0.01410, -2.7923 0.0026, 0.00780, -2.7654 0.0000, 0.00000, -3.1080 0.0037, -0.00840, 0.1560 0.0112, -0.01420, 0.8527 0.0191, -0.01930, 0.9932 0.0397, -0.03030, 0.9862 0.0706, -0.04420, 0.8403 0.1037, -0.05710, 0.7049 0.1384, -0.06890, 0.5859 0.1741, -0.07950, 0.4564 0.2102, -0.08660, 0.3061 0.2472, -0.09640, 0.1839 0.2844, -0.10270, 0.0680 0.3225, -0.10690, -0.0041 0.3608, -0.10890, -0.1117 0.3991, -0.10830, -0.1475 0.4373, -0.10510, -0.1384 0.4757, -0.09890, -0.0918 0.5137, -0.09067, -0.0342 0.5611, -0.07859, 0.1194 16 Flap element taps 1.0000, 0.00130, -0.9591 0.9365, 0.01390, -0.9684 0.8333, 0.03280, -0.9911 0.7436, 0.04930, -0.9967 0.7049, 0.05667, -0.9958 0.6662, 0.06411, -1.0269 0.6274, 0.07172, -1.0365 0.6009, 0.07523, -1.4461 0.6069, 0.02889, -1.4165 0.6079, -0.01747, -1.3830 0.6167, -0.06381, -0.9179 0.6558, -0.05300, -0.1485 0.7045, -0.04117, 0.3452 0.7429, -0.03210, 0.6545 0.8333, -0.01400, 0.9899 0.9311, -0.00120, 0.7892 --------- Run Conditions: vel=103.1 ft/s Re=0.988x10^6 AOA=18.00 Flap deflection=60.00 Totals: Cl=0.6219 Cdp=0.6051 Cm(c/4)=-0.1580 Cs=-0.3833 Ch=-0.0425 Main component: Cl=0.3967 Cdp=0.0990 Cm=-0.0534 Flap component: Cl=0.2252 Cdp=0.5061 Cm=-0.2991 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3186 0.5905, -0.01667, -0.4157 0.5709, 0.03110, -0.3989 0.5889, 0.07933, -0.3505 0.5500, 0.08689, -0.1247 0.5110, 0.09367, -0.0944 0.4731, 0.09830, -0.0854 0.4349, 0.10070, -0.1148 0.3960, 0.10120, -0.1532 0.3566, 0.10020, -0.1032 0.3172, 0.09790, -0.1062 0.2778, 0.09440, -0.1211 0.2393, 0.08960, -0.1147 0.2056, 0.08360, -0.2076 0.1633, 0.07610, -0.3274 0.1261, 0.06710, -0.6034 0.0900, 0.05640, -0.8807 0.0571, 0.04390, -1.2635 0.0283, 0.02940, -1.8044 0.0142, 0.01970, -2.3514 0.0081, 0.01410, -3.3100 0.0026, 0.00780, -3.2863 0.0000, 0.00000, -3.8912 0.0037, -0.00840, -0.1499 0.0112, -0.01420, 0.7444 0.0191, -0.01930, 0.9565 0.0397, -0.03030, 1.0074 0.0706, -0.04420, 0.8881 0.1037, -0.05710, 0.7669 0.1384, -0.06890, 0.6639 0.1741, -0.07950, 0.5328 0.2102, -0.08660, 0.3723 0.2472, -0.09640, 0.2521 0.2844, -0.10270, 0.1280 0.3225, -0.10690, 0.0569 0.3608, -0.10890, -0.0655 0.3991, -0.10830, -0.1089 0.4373, -0.10510, -0.1212 0.4757, -0.09890, -0.0899 0.5137, -0.09067, -0.0276 0.5611, -0.07859, 0.0195 16 Flap element taps 1.0000, 0.00130, -0.9878 0.9365, 0.01390, -0.9943 0.8333, 0.03280, -1.0148 0.7436, 0.04930, -1.0237 0.7049, 0.05667, -1.0228 0.6662, 0.06411, -1.0481 0.6274, 0.07172, -1.0536 0.6009, 0.07523, -1.3044 0.6069, 0.02889, -1.2665 0.6079, -0.01747, -1.2150 0.6167, -0.06381, -0.9237 0.6558, -0.05300, -0.2371 0.7045, -0.04117, 0.2972 0.7429, -0.03210, 0.6252 0.8333, -0.01400, 0.9883 0.9311, -0.00120, 0.8018 --------- Run Conditions: vel=104.1 ft/s Re=0.996x10^6 AOA=19.98 Flap deflection=60.00 Totals: Cl=0.4778 Cdp=0.7664 Cm(c/4)=-0.1817 Cs=-0.5570 Ch=-0.0718 Main component: Cl=0.2847 Cdp=0.2851 Cm=-0.0751 Flap component: Cl=0.1931 Cdp=0.4813 Cm=-0.2843 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.8054 0.5905, -0.01667, -1.1036 0.5709, 0.03110, -1.0555 0.5889, 0.07933, -0.5347 0.5500, 0.08689, -0.3873 0.5110, 0.09367, -0.4121 0.4731, 0.09830, -0.3769 0.4349, 0.10070, -0.3788 0.3960, 0.10120, -0.4566 0.3566, 0.10020, -0.4370 0.3172, 0.09790, -0.4615 0.2778, 0.09440, -0.4747 0.2393, 0.08960, -0.4543 0.2056, 0.08360, -0.5041 0.1633, 0.07610, -0.4305 0.1261, 0.06710, -0.4527 0.0900, 0.05640, -0.4174 0.0571, 0.04390, -0.4421 0.0283, 0.02940, -0.4587 0.0142, 0.01970, -0.4695 0.0081, 0.01410, -0.5073 0.0026, 0.00780, -0.4306 0.0000, 0.00000, -0.6979 0.0037, -0.00840, 0.6641 0.0112, -0.01420, 0.9697 0.0191, -0.01930, 1.0207 0.0397, -0.03030, 0.9672 0.0706, -0.04420, 0.8087 0.1037, -0.05710, 0.6761 0.1384, -0.06890, 0.5829 0.1741, -0.07950, 0.4481 0.2102, -0.08660, 0.2726 0.2472, -0.09640, 0.1532 0.2844, -0.10270, 0.0192 0.3225, -0.10690, -0.0466 0.3608, -0.10890, -0.1874 0.3991, -0.10830, -0.2341 0.4373, -0.10510, -0.2609 0.4757, -0.09890, -0.2403 0.5137, -0.09067, -0.1723 0.5611, -0.07859, -0.1276 16 Flap element taps 1.0000, 0.00130, -0.9975 0.9365, 0.01390, -1.0012 0.8333, 0.03280, -1.0232 0.7436, 0.04930, -1.0292 0.7049, 0.05667, -1.0298 0.6662, 0.06411, -1.0605 0.6274, 0.07172, -1.0667 0.6009, 0.07523, -1.2309 0.6069, 0.02889, -1.2566 0.6079, -0.01747, -1.2043 0.6167, -0.06381, -1.0787 0.6558, -0.05300, -0.5760 0.7045, -0.04117, 0.0613 0.7429, -0.03210, 0.4691 0.8333, -0.01400, 0.9814 0.9311, -0.00120, 0.8380 --------- Run Conditions: vel=105.0 ft/s Re=1.000x10^6 AOA=24.02 Flap deflection=60.00 Totals: Cl=0.5273 Cdp=0.9228 Cm(c/4)=-0.2017 Cs=-0.6283 Ch=-0.0817 Main component: Cl=0.3607 Cdp=0.3924 Cm=-0.1128 Flap component: Cl=0.1665 Cdp=0.5304 Cm=-0.3033 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -1.0615 0.5905, -0.01667, -1.4699 0.5709, 0.03110, -1.4266 0.5889, 0.07933, -0.7116 0.5500, 0.08689, -0.5907 0.5110, 0.09367, -0.6114 0.4731, 0.09830, -0.6038 0.4349, 0.10070, -0.5794 0.3960, 0.10120, -0.5783 0.3566, 0.10020, -0.5853 0.3172, 0.09790, -0.6082 0.2778, 0.09440, -0.6267 0.2393, 0.08960, -0.6099 0.2056, 0.08360, -0.6182 0.1633, 0.07610, -0.6068 0.1261, 0.06710, -0.6022 0.0900, 0.05640, -0.5961 0.0571, 0.04390, -0.5907 0.0283, 0.02940, -0.6052 0.0142, 0.01970, -0.6118 0.0081, 0.01410, -0.6139 0.0026, 0.00780, -0.5692 0.0000, 0.00000, -0.8231 0.0037, -0.00840, 0.4260 0.0112, -0.01420, 0.8720 0.0191, -0.01930, 0.9773 0.0397, -0.03030, 0.9921 0.0706, -0.04420, 0.8859 0.1037, -0.05710, 0.7749 0.1384, -0.06890, 0.6564 0.1741, -0.07950, 0.5234 0.2102, -0.08660, 0.3884 0.2472, -0.09640, 0.2439 0.2844, -0.10270, 0.1231 0.3225, -0.10690, 0.0112 0.3608, -0.10890, -0.1089 0.3991, -0.10830, -0.1949 0.4373, -0.10510, -0.2331 0.4757, -0.09890, -0.2357 0.5137, -0.09067, -0.1807 0.5611, -0.07859, -0.1762 16 Flap element taps 1.0000, 0.00130, -1.1540 0.9365, 0.01390, -1.1762 0.8333, 0.03280, -1.1982 0.7436, 0.04930, -1.2150 0.7049, 0.05667, -1.2108 0.6662, 0.06411, -1.2419 0.6274, 0.07172, -1.2628 0.6009, 0.07523, -1.3932 0.6069, 0.02889, -1.4134 0.6079, -0.01747, -1.3719 0.6167, -0.06381, -1.2737 0.6558, -0.05300, -0.7642 0.7045, -0.04117, -0.0703 0.7429, -0.03210, 0.3851 0.8333, -0.01400, 0.9645 0.9311, -0.00120, 0.8294 --------- Run Conditions: vel=106.3 ft/s Re=1.014x10^6 AOA=27.02 Flap deflection=60.00 Totals: Cl=0.5620 Cdp=1.0035 Cm(c/4)=-0.2111 Cs=-0.6387 Ch=-0.0884 Main component: Cl=0.4191 Cdp=0.4642 Cm=-0.1425 Flap component: Cl=0.1429 Cdp=0.5393 Cm=-0.3077 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -1.1139 0.5905, -0.01667, -1.5933 0.5709, 0.03110, -1.5475 0.5889, 0.07933, -0.7953 0.5500, 0.08689, -0.6992 0.5110, 0.09367, -0.7186 0.4731, 0.09830, -0.7037 0.4349, 0.10070, -0.6959 0.3960, 0.10120, -0.6975 0.3566, 0.10020, -0.6885 0.3172, 0.09790, -0.6902 0.2778, 0.09440, -0.7100 0.2393, 0.08960, -0.7030 0.2056, 0.08360, -0.7175 0.1633, 0.07610, -0.7012 0.1261, 0.06710, -0.6993 0.0900, 0.05640, -0.6905 0.0571, 0.04390, -0.6837 0.0283, 0.02940, -0.6938 0.0142, 0.01970, -0.7010 0.0081, 0.01410, -0.7056 0.0026, 0.00780, -0.6528 0.0000, 0.00000, -0.7419 0.0037, -0.00840, 0.2474 0.0112, -0.01420, 0.7871 0.0191, -0.01930, 0.9408 0.0397, -0.03030, 1.0077 0.0706, -0.04420, 0.9359 0.1037, -0.05710, 0.8446 0.1384, -0.06890, 0.7390 0.1741, -0.07950, 0.6124 0.2102, -0.08660, 0.4804 0.2472, -0.09640, 0.3414 0.2844, -0.10270, 0.2192 0.3225, -0.10690, 0.1063 0.3608, -0.10890, -0.0205 0.3991, -0.10830, -0.1136 0.4373, -0.10510, -0.1655 0.4757, -0.09890, -0.1833 0.5137, -0.09067, -0.1362 0.5611, -0.07859, -0.1570 16 Flap element taps 1.0000, 0.00130, -1.1620 0.9365, 0.01390, -1.1890 0.8333, 0.03280, -1.2284 0.7436, 0.04930, -1.2283 0.7049, 0.05667, -1.2245 0.6662, 0.06411, -1.2479 0.6274, 0.07172, -1.2748 0.6009, 0.07523, -1.4529 0.6069, 0.02889, -1.4617 0.6079, -0.01747, -1.4189 0.6167, -0.06381, -1.3259 0.6558, -0.05300, -0.8243 0.7045, -0.04117, -0.1047 0.7429, -0.03210, 0.3579 0.8333, -0.01400, 0.9670 0.9311, -0.00120, 0.8514 --------- Run Conditions: vel=105.3 ft/s Re=1.003x10^6 AOA=29.99 Flap deflection=60.00 Totals: Cl=0.5937 Cdp=1.0729 Cm(c/4)=-0.2175 Cs=-0.6325 Ch=-0.0921 Main component: Cl=0.4765 Cdp=0.5344 Cm=-0.1730 Flap component: Cl=0.1172 Cdp=0.5385 Cm=-0.3071 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -1.1443 0.5905, -0.01667, -1.6610 0.5709, 0.03110, -1.6119 0.5889, 0.07933, -0.8752 0.5500, 0.08689, -0.8030 0.5110, 0.09367, -0.8149 0.4731, 0.09830, -0.8294 0.4349, 0.10070, -0.8258 0.3960, 0.10120, -0.8312 0.3566, 0.10020, -0.8023 0.3172, 0.09790, -0.7990 0.2778, 0.09440, -0.8130 0.2393, 0.08960, -0.8018 0.2056, 0.08360, -0.8176 0.1633, 0.07610, -0.8012 0.1261, 0.06710, -0.8010 0.0900, 0.05640, -0.7898 0.0571, 0.04390, -0.7823 0.0283, 0.02940, -0.7919 0.0142, 0.01970, -0.7935 0.0081, 0.01410, -0.8018 0.0026, 0.00780, -0.7388 0.0000, 0.00000, -0.8122 0.0037, -0.00840, 0.0405 0.0112, -0.01420, 0.6706 0.0191, -0.01930, 0.8754 0.0397, -0.03030, 1.0007 0.0706, -0.04420, 0.9653 0.1037, -0.05710, 0.8946 0.1384, -0.06890, 0.8071 0.1741, -0.07950, 0.6904 0.2102, -0.08660, 0.5633 0.2472, -0.09640, 0.4317 0.2844, -0.10270, 0.3092 0.3225, -0.10690, 0.1997 0.3608, -0.10890, 0.0666 0.3991, -0.10830, -0.0299 0.4373, -0.10510, -0.0934 0.4757, -0.09890, -0.1243 0.5137, -0.09067, -0.0871 0.5611, -0.07859, -0.1309 16 Flap element taps 1.0000, 0.00130, -1.1752 0.9365, 0.01390, -1.1921 0.8333, 0.03280, -1.2084 0.7436, 0.04930, -1.2202 0.7049, 0.05667, -1.2229 0.6662, 0.06411, -1.2470 0.6274, 0.07172, -1.2691 0.6009, 0.07523, -1.4670 0.6069, 0.02889, -1.4925 0.6079, -0.01747, -1.4400 0.6167, -0.06381, -1.3503 0.6558, -0.05300, -0.8598 0.7045, -0.04117, -0.1296 0.7429, -0.03210, 0.3358 0.8333, -0.01400, 0.9580 0.9311, -0.00120, 0.8581 --------- Run Conditions: vel=105.3 ft/s Re=1.003x10^6 AOA=34.97 Flap deflection=60.00 Totals: Cl=0.6188 Cdp=1.2193 Cm(c/4)=-0.2332 Cs=-0.6445 Ch=-0.0929 Main component: Cl=0.5503 Cdp=0.6547 Cm=-0.2204 Flap component: Cl=0.0685 Cdp=0.5646 Cm=-0.3144 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -1.1658 0.5905, -0.01667, -1.7235 0.5709, 0.03110, -1.6915 0.5889, 0.07933, -1.0367 0.5500, 0.08689, -0.9605 0.5110, 0.09367, -0.9620 0.4731, 0.09830, -0.9870 0.4349, 0.10070, -0.9960 0.3960, 0.10120, -1.0059 0.3566, 0.10020, -0.9759 0.3172, 0.09790, -0.9606 0.2778, 0.09440, -0.9613 0.2393, 0.08960, -0.9504 0.2056, 0.08360, -0.9768 0.1633, 0.07610, -0.9598 0.1261, 0.06710, -0.9612 0.0900, 0.05640, -0.9509 0.0571, 0.04390, -0.9417 0.0283, 0.02940, -0.9472 0.0142, 0.01970, -0.9495 0.0081, 0.01410, -0.9576 0.0026, 0.00780, -0.8825 0.0000, 0.00000, -0.9534 0.0037, -0.00840, -0.3201 0.0112, -0.01420, 0.4423 0.0191, -0.01930, 0.7313 0.0397, -0.03030, 0.9590 0.0706, -0.04420, 0.9882 0.1037, -0.05710, 0.9620 0.1384, -0.06890, 0.9041 0.1741, -0.07950, 0.8083 0.2102, -0.08660, 0.6941 0.2472, -0.09640, 0.5777 0.2844, -0.10270, 0.4614 0.3225, -0.10690, 0.3550 0.3608, -0.10890, 0.2214 0.3991, -0.10830, 0.1163 0.4373, -0.10510, 0.0365 0.4757, -0.09890, -0.0128 0.5137, -0.09067, 0.0053 0.5611, -0.07859, -0.0717 16 Flap element taps 1.0000, 0.00130, -1.2222 0.9365, 0.01390, -1.2456 0.8333, 0.03280, -1.2708 0.7436, 0.04930, -1.2781 0.7049, 0.05667, -1.2880 0.6662, 0.06411, -1.3185 0.6274, 0.07172, -1.3467 0.6009, 0.07523, -1.5262 0.6069, 0.02889, -1.5290 0.6079, -0.01747, -1.4772 0.6167, -0.06381, -1.3938 0.6558, -0.05300, -0.8969 0.7045, -0.04117, -0.1500 0.7429, -0.03210, 0.3146 0.8333, -0.01400, 0.9510 0.9311, -0.00120, 0.8750 --------- Run Conditions: vel=106.3 ft/s Re=1.012x10^6 AOA=39.98 Flap deflection=60.00 Totals: Cl=0.6223 Cdp=1.3963 Cm(c/4)=-0.2589 Cs=-0.6701 Ch=-0.0937 Main component: Cl=0.6056 Cdp=0.7879 Cm=-0.2690 Flap component: Cl=0.0167 Cdp=0.6085 Cm=-0.3334 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -1.1693 0.5905, -0.01667, -1.7989 0.5709, 0.03110, -1.7563 0.5889, 0.07933, -1.2221 0.5500, 0.08689, -1.1675 0.5110, 0.09367, -1.1627 0.4731, 0.09830, -1.1563 0.4349, 0.10070, -1.1682 0.3960, 0.10120, -1.1867 0.3566, 0.10020, -1.1542 0.3172, 0.09790, -1.1336 0.2778, 0.09440, -1.1308 0.2393, 0.08960, -1.1171 0.2056, 0.08360, -1.1388 0.1633, 0.07610, -1.1223 0.1261, 0.06710, -1.1259 0.0900, 0.05640, -1.1181 0.0571, 0.04390, -1.1066 0.0283, 0.02940, -1.1113 0.0142, 0.01970, -1.1093 0.0081, 0.01410, -1.1192 0.0026, 0.00780, -1.0352 0.0000, 0.00000, -1.1094 0.0037, -0.00840, -0.6899 0.0112, -0.01420, 0.1775 0.0191, -0.01930, 0.5480 0.0397, -0.03030, 0.8785 0.0706, -0.04420, 0.9797 0.1037, -0.05710, 0.9950 0.1384, -0.06890, 0.9702 0.1741, -0.07950, 0.8969 0.2102, -0.08660, 0.8022 0.2472, -0.09640, 0.7027 0.2844, -0.10270, 0.5936 0.3225, -0.10690, 0.4946 0.3608, -0.10890, 0.3618 0.3991, -0.10830, 0.2530 0.4373, -0.10510, 0.1591 0.4757, -0.09890, 0.0940 0.5137, -0.09067, 0.0920 0.5611, -0.07859, -0.0136 16 Flap element taps 1.0000, 0.00130, -1.3240 0.9365, 0.01390, -1.3592 0.8333, 0.03280, -1.4042 0.7436, 0.04930, -1.4181 0.7049, 0.05667, -1.4196 0.6662, 0.06411, -1.4483 0.6274, 0.07172, -1.4737 0.6009, 0.07523, -1.6756 0.6069, 0.02889, -1.6373 0.6079, -0.01747, -1.5846 0.6167, -0.06381, -1.4931 0.6558, -0.05300, -0.9487 0.7045, -0.04117, -0.1724 0.7429, -0.03210, 0.2973 0.8333, -0.01400, 0.9453 0.9311, -0.00120, 0.8898 --------- Run Conditions: vel=104.0 ft/s Re=0.988x10^6 AOA=44.98 Flap deflection=60.00 Totals: Cl=0.5851 Cdp=1.5525 Cm(c/4)=-0.2802 Cs=-0.6846 Ch=-0.0880 Main component: Cl=0.6287 Cdp=0.9138 Cm=-0.3124 Flap component: Cl=-0.0437 Cdp=0.6387 Cm=-0.3456 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -1.1450 0.5905, -0.01667, -1.8045 0.5709, 0.03110, -1.7668 0.5889, 0.07933, -1.4079 0.5500, 0.08689, -1.3399 0.5110, 0.09367, -1.3400 0.4731, 0.09830, -1.3283 0.4349, 0.10070, -1.3409 0.3960, 0.10120, -1.3561 0.3566, 0.10020, -1.3285 0.3172, 0.09790, -1.3069 0.2778, 0.09440, -1.2954 0.2393, 0.08960, -1.2598 0.2056, 0.08360, -1.2651 0.1633, 0.07610, -1.2454 0.1261, 0.06710, -1.2513 0.0900, 0.05640, -1.2407 0.0571, 0.04390, -1.2307 0.0283, 0.02940, -1.2322 0.0142, 0.01970, -1.2296 0.0081, 0.01410, -1.2398 0.0026, 0.00780, -1.1494 0.0000, 0.00000, -1.2282 0.0037, -0.00840, -1.0179 0.0112, -0.01420, -0.0954 0.0191, -0.01930, 0.3391 0.0397, -0.03030, 0.7628 0.0706, -0.04420, 0.9324 0.1037, -0.05710, 0.9930 0.1384, -0.06890, 1.0006 0.1741, -0.07950, 0.9540 0.2102, -0.08660, 0.8812 0.2472, -0.09640, 0.8006 0.2844, -0.10270, 0.7051 0.3225, -0.10690, 0.6139 0.3608, -0.10890, 0.4888 0.3991, -0.10830, 0.3800 0.4373, -0.10510, 0.2776 0.4757, -0.09890, 0.2002 0.5137, -0.09067, 0.1796 0.5611, -0.07859, 0.0523 16 Flap element taps 1.0000, 0.00130, -1.3977 0.9365, 0.01390, -1.4339 0.8333, 0.03280, -1.4849 0.7436, 0.04930, -1.5289 0.7049, 0.05667, -1.5359 0.6662, 0.06411, -1.5746 0.6274, 0.07172, -1.6080 0.6009, 0.07523, -1.8117 0.6069, 0.02889, -1.6908 0.6079, -0.01747, -1.6392 0.6167, -0.06381, -1.5376 0.6558, -0.05300, -0.9681 0.7045, -0.04117, -0.1837 0.7429, -0.03210, 0.2851 0.8333, -0.01400, 0.9330 0.9311, -0.00120, 0.8969 --------- Run Conditions: vel=105.3 ft/s Re=1.001x10^6 AOA=59.98 Flap deflection=60.00 Totals: Cl=0.3226 Cdp=1.8541 Cm(c/4)=-0.3221 Cs=-0.6483 Ch=-0.0814 Main component: Cl=0.5536 Cdp=1.2086 Cm=-0.4014 Flap component: Cl=-0.2310 Cdp=0.6455 Cm=-0.3624 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.9049 0.5905, -0.01667, -1.5649 0.5709, 0.03110, -1.6360 0.5889, 0.07933, -1.6870 0.5500, 0.08689, -1.6192 0.5110, 0.09367, -1.6248 0.4731, 0.09830, -1.6199 0.4349, 0.10070, -1.6305 0.3960, 0.10120, -1.6352 0.3566, 0.10020, -1.6393 0.3172, 0.09790, -1.6322 0.2778, 0.09440, -1.6321 0.2393, 0.08960, -1.5997 0.2056, 0.08360, -1.5890 0.1633, 0.07610, -1.5765 0.1261, 0.06710, -1.5503 0.0900, 0.05640, -1.5524 0.0571, 0.04390, -1.5330 0.0283, 0.02940, -1.5281 0.0142, 0.01970, -1.5213 0.0081, 0.01410, -1.5182 0.0026, 0.00780, -1.4283 0.0000, 0.00000, -1.5183 0.0037, -0.00840, -1.6609 0.0112, -0.01420, -0.8626 0.0191, -0.01930, -0.3251 0.0397, -0.03030, 0.2955 0.0706, -0.04420, 0.6605 0.1037, -0.05710, 0.8427 0.1384, -0.06890, 0.9273 0.1741, -0.07950, 0.9776 0.2102, -0.08660, 0.9948 0.2472, -0.09640, 0.9773 0.2844, -0.10270, 0.9367 0.3225, -0.10690, 0.8796 0.3608, -0.10890, 0.8016 0.3991, -0.10830, 0.7029 0.4373, -0.10510, 0.6192 0.4757, -0.09890, 0.5205 0.5137, -0.09067, 0.4697 0.5611, -0.07859, 0.3063 16 Flap element taps 1.0000, 0.00130, -1.5057 0.9365, 0.01390, -1.5453 0.8333, 0.03280, -1.5851 0.7436, 0.04930, -1.6310 0.7049, 0.05667, -1.6482 0.6662, 0.06411, -1.6760 0.6274, 0.07172, -1.7380 0.6009, 0.07523, -1.9456 0.6069, 0.02889, -1.7202 0.6079, -0.01747, -1.6666 0.6167, -0.06381, -1.5611 0.6558, -0.05300, -0.9084 0.7045, -0.04117, -0.1289 0.7429, -0.03210, 0.3019 0.8333, -0.01400, 0.9179 0.9311, -0.00120, 0.9360 --------- Run Conditions: vel=104.6 ft/s Re=0.992x10^6 AOA=70.01 Flap deflection=60.00 Totals: Cl=0.0598 Cdp=1.9100 Cm(c/4)=-0.3398 Cs=-0.5967 Ch=-0.0790 Main component: Cl=0.4018 Cdp=1.3095 Cm=-0.4284 Flap component: Cl=-0.3420 Cdp=0.6005 Cm=-0.3652 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.6849 0.5905, -0.01667, -1.3425 0.5709, 0.03110, -1.4248 0.5889, 0.07933, -1.7765 0.5500, 0.08689, -1.6773 0.5110, 0.09367, -1.6767 0.4731, 0.09830, -1.6774 0.4349, 0.10070, -1.6882 0.3960, 0.10120, -1.6979 0.3566, 0.10020, -1.7170 0.3172, 0.09790, -1.7157 0.2778, 0.09440, -1.7231 0.2393, 0.08960, -1.6925 0.2056, 0.08360, -1.6704 0.1633, 0.07610, -1.6566 0.1261, 0.06710, -1.6249 0.0900, 0.05640, -1.6145 0.0571, 0.04390, -1.5949 0.0283, 0.02940, -1.5844 0.0142, 0.01970, -1.5784 0.0081, 0.01410, -1.5753 0.0026, 0.00780, -1.4853 0.0000, 0.00000, -1.5782 0.0037, -0.00840, -1.7615 0.0112, -0.01420, -1.2284 0.0191, -0.01930, -0.7047 0.0397, -0.03030, -0.0364 0.0706, -0.04420, 0.4036 0.1037, -0.05710, 0.6488 0.1384, -0.06890, 0.7877 0.1741, -0.07950, 0.8916 0.2102, -0.08660, 0.9604 0.2472, -0.09640, 0.9857 0.2844, -0.10270, 0.9900 0.3225, -0.10690, 0.9716 0.3608, -0.10890, 0.9308 0.3991, -0.10830, 0.8618 0.4373, -0.10510, 0.7960 0.4757, -0.09890, 0.7069 0.5137, -0.09067, 0.6432 0.5611, -0.07859, 0.4787 16 Flap element taps 1.0000, 0.00130, -1.5235 0.9365, 0.01390, -1.5513 0.8333, 0.03280, -1.5809 0.7436, 0.04930, -1.6162 0.7049, 0.05667, -1.6208 0.6662, 0.06411, -1.6427 0.6274, 0.07172, -1.7049 0.6009, 0.07523, -1.8910 0.6069, 0.02889, -1.7141 0.6079, -0.01747, -1.6755 0.6167, -0.06381, -1.5487 0.6558, -0.05300, -0.8110 0.7045, -0.04117, -0.0574 0.7429, -0.03210, 0.3362 0.8333, -0.01400, 0.9015 0.9311, -0.00120, 0.9582 --------- Run Conditions: vel=105.9 ft/s Re=1.005x10^6 AOA=79.98 Flap deflection=60.00 Totals: Cl=-0.1992 Cdp=1.8212 Cm(c/4)=-0.3380 Cs=-0.5131 Ch=-0.0733 Main component: Cl=0.2289 Cdp=1.3110 Cm=-0.4288 Flap component: Cl=-0.4281 Cdp=0.5102 Cm=-0.3489 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3828 0.5905, -0.01667, -0.9946 0.5709, 0.03110, -1.1045 0.5889, 0.07933, -1.7154 0.5500, 0.08689, -1.6090 0.5110, 0.09367, -1.6232 0.4731, 0.09830, -1.6365 0.4349, 0.10070, -1.6454 0.3960, 0.10120, -1.6505 0.3566, 0.10020, -1.6800 0.3172, 0.09790, -1.6909 0.2778, 0.09440, -1.7036 0.2393, 0.08960, -1.6844 0.2056, 0.08360, -1.6637 0.1633, 0.07610, -1.6561 0.1261, 0.06710, -1.6185 0.0900, 0.05640, -1.6072 0.0571, 0.04390, -1.5862 0.0283, 0.02940, -1.5728 0.0142, 0.01970, -1.5632 0.0081, 0.01410, -1.5550 0.0026, 0.00780, -1.4725 0.0000, 0.00000, -1.5659 0.0037, -0.00840, -1.6207 0.0112, -0.01420, -1.4587 0.0191, -0.01930, -1.0057 0.0397, -0.03030, -0.3509 0.0706, -0.04420, 0.1229 0.1037, -0.05710, 0.4042 0.1384, -0.06890, 0.5818 0.1741, -0.07950, 0.7303 0.2102, -0.08660, 0.8485 0.2472, -0.09640, 0.9145 0.2844, -0.10270, 0.9653 0.3225, -0.10690, 0.9842 0.3608, -0.10890, 0.9908 0.3991, -0.10830, 0.9558 0.4373, -0.10510, 0.9237 0.4757, -0.09890, 0.8570 0.5137, -0.09067, 0.8007 0.5611, -0.07859, 0.6531 16 Flap element taps 1.0000, 0.00130, -1.4381 0.9365, 0.01390, -1.4514 0.8333, 0.03280, -1.4671 0.7436, 0.04930, -1.4906 0.7049, 0.05667, -1.4978 0.6662, 0.06411, -1.5043 0.6274, 0.07172, -1.5349 0.6009, 0.07523, -1.6477 0.6069, 0.02889, -1.5639 0.6079, -0.01747, -1.5311 0.6167, -0.06381, -1.4130 0.6558, -0.05300, -0.6369 0.7045, -0.04117, 0.0571 0.7429, -0.03210, 0.3970 0.8333, -0.01400, 0.8893 0.9311, -0.00120, 0.9771 --------- Run Conditions: vel=105.6 ft/s Re=1.001x10^6 AOA=89.99 Flap deflection=60.00 Totals: Cl=-0.4437 Cdp=1.6633 Cm(c/4)=-0.3354 Cs=-0.4440 Ch=-0.0632 Main component: Cl=0.0600 Cdp=1.2495 Cm=-0.4152 Flap component: Cl=-0.5037 Cdp=0.4138 Cm=-0.3360 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.0853 0.5905, -0.01667, -0.6595 0.5709, 0.03110, -0.7401 0.5889, 0.07933, -1.6232 0.5500, 0.08689, -1.5495 0.5110, 0.09367, -1.5509 0.4731, 0.09830, -1.5528 0.4349, 0.10070, -1.5648 0.3960, 0.10120, -1.5646 0.3566, 0.10020, -1.6062 0.3172, 0.09790, -1.6179 0.2778, 0.09440, -1.6412 0.2393, 0.08960, -1.6304 0.2056, 0.08360, -1.6109 0.1633, 0.07610, -1.6185 0.1261, 0.06710, -1.5608 0.0900, 0.05640, -1.5434 0.0571, 0.04390, -1.5103 0.0283, 0.02940, -1.4951 0.0142, 0.01970, -1.4860 0.0081, 0.01410, -1.4709 0.0026, 0.00780, -1.3975 0.0000, 0.00000, -1.4881 0.0037, -0.00840, -1.5004 0.0112, -0.01420, -1.5363 0.0191, -0.01930, -1.1969 0.0397, -0.03030, -0.6108 0.0706, -0.04420, -0.1442 0.1037, -0.05710, 0.1492 0.1384, -0.06890, 0.3436 0.1741, -0.07950, 0.5234 0.2102, -0.08660, 0.6832 0.2472, -0.09640, 0.7774 0.2844, -0.10270, 0.8716 0.3225, -0.10690, 0.9247 0.3608, -0.10890, 0.9796 0.3991, -0.10830, 0.9839 0.4373, -0.10510, 0.9932 0.4757, -0.09890, 0.9587 0.5137, -0.09067, 0.9213 0.5611, -0.07859, 0.8033 16 Flap element taps 1.0000, 0.00130, -1.3581 0.9365, 0.01390, -1.3668 0.8333, 0.03280, -1.3733 0.7436, 0.04930, -1.3990 0.7049, 0.05667, -1.4031 0.6662, 0.06411, -1.3982 0.6274, 0.07172, -1.4180 0.6009, 0.07523, -1.4718 0.6069, 0.02889, -1.4058 0.6079, -0.01747, -1.3960 0.6167, -0.06381, -1.2649 0.6558, -0.05300, -0.4530 0.7045, -0.04117, 0.1718 0.7429, -0.03210, 0.4624 0.8333, -0.01400, 0.8788 0.9311, -0.00120, 0.9925 --------- Run Conditions: vel=106.3 ft/s Re=1.011x10^6 AOA=120.00 Flap deflection=60.00 Totals: Cl=-0.9441 Cdp=0.7418 Cm(c/4)=-0.3281 Cs=-0.4467 Ch=-0.0072 Main component: Cl=-0.1869 Cdp=0.6495 Cm=-0.2448 Flap component: Cl=-0.7572 Cdp=0.0923 Cm=-0.3619 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.6505 0.5905, -0.01667, 0.2587 0.5709, 0.03110, 0.2648 0.5889, 0.07933, -0.8529 0.5500, 0.08689, -0.8050 0.5110, 0.09367, -0.8169 0.4731, 0.09830, -0.8225 0.4349, 0.10070, -0.8238 0.3960, 0.10120, -0.7986 0.3566, 0.10020, -0.8525 0.3172, 0.09790, -0.8455 0.2778, 0.09440, -0.8563 0.2393, 0.08960, -0.8354 0.2056, 0.08360, -0.8098 0.1633, 0.07610, -0.8571 0.1261, 0.06710, -0.8225 0.0900, 0.05640, -0.8446 0.0571, 0.04390, -0.8265 0.0283, 0.02940, -0.8227 0.0142, 0.01970, -0.8180 0.0081, 0.01410, -0.7932 0.0026, 0.00780, -0.7735 0.0000, 0.00000, -0.8393 0.0037, -0.00840, -0.8356 0.0112, -0.01420, -0.8570 0.0191, -0.01930, -0.9085 0.0397, -0.03030, -0.7462 0.0706, -0.04420, -0.5071 0.1037, -0.05710, -0.3283 0.1384, -0.06890, -0.2094 0.1741, -0.07950, -0.0514 0.2102, -0.08660, 0.1256 0.2472, -0.09640, 0.2259 0.2844, -0.10270, 0.3735 0.3225, -0.10690, 0.4707 0.3608, -0.10890, 0.6160 0.3991, -0.10830, 0.7107 0.4373, -0.10510, 0.8386 0.4757, -0.09890, 0.9190 0.5137, -0.09067, 0.9842 0.5611, -0.07859, 0.9975 16 Flap element taps 1.0000, 0.00130, -1.5105 0.9365, 0.01390, -1.5223 0.8333, 0.03280, -1.5426 0.7436, 0.04930, -1.6011 0.7049, 0.05667, -1.6107 0.6662, 0.06411, -1.5677 0.6274, 0.07172, -1.6237 0.6009, 0.07523, -1.7382 0.6069, 0.02889, -1.2856 0.6079, -0.01747, -1.2729 0.6167, -0.06381, -0.9330 0.6558, -0.05300, 0.0539 0.7045, -0.04117, 0.4847 0.7429, -0.03210, 0.6390 0.8333, -0.01400, 0.8323 0.9311, -0.00120, 0.9485 --------- Run Conditions: vel=105.5 ft/s Re=1.004x10^6 AOA=150.00 Flap deflection=60.00 Totals: Cl=0.0082 Cdp=0.5158 Cm(c/4)=-0.0291 Cs=0.4507 Ch=0.0721 Main component: Cl=-0.2081 Cdp=0.2489 Cm=-0.1430 Flap component: Cl=0.2163 Cdp=0.2669 Cm=0.0512 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.5476 0.5905, -0.01667, -0.7097 0.5709, 0.03110, -0.6619 0.5889, 0.07933, -0.9238 0.5500, 0.08689, -0.8730 0.5110, 0.09367, -0.8848 0.4731, 0.09830, -0.8700 0.4349, 0.10070, -0.8816 0.3960, 0.10120, -0.8653 0.3566, 0.10020, -0.8986 0.3172, 0.09790, -0.9024 0.2778, 0.09440, -0.9124 0.2393, 0.08960, -0.9026 0.2056, 0.08360, -0.8807 0.1633, 0.07610, -0.9150 0.1261, 0.06710, -0.8865 0.0900, 0.05640, -0.8836 0.0571, 0.04390, -0.8609 0.0283, 0.02940, -0.8553 0.0142, 0.01970, -0.8407 0.0081, 0.01410, -0.8242 0.0026, 0.00780, -0.7880 0.0000, 0.00000, -0.8641 0.0037, -0.00840, -0.8678 0.0112, -0.01420, -0.8413 0.0191, -0.01930, -0.8404 0.0397, -0.03030, -0.8555 0.0706, -0.04420, -0.9256 0.1037, -0.05710, -0.9570 0.1384, -0.06890, -0.9618 0.1741, -0.07950, -0.9199 0.2102, -0.08660, -0.8481 0.2472, -0.09640, -0.8108 0.2844, -0.10270, -0.6907 0.3225, -0.10690, -0.5844 0.3608, -0.10890, -0.4230 0.3991, -0.10830, -0.2323 0.4373, -0.10510, 0.0283 0.4757, -0.09890, 0.2995 0.5137, -0.09067, 0.6053 0.5611, -0.07859, 0.8838 16 Flap element taps 1.0000, 0.00130, -0.5625 0.9365, 0.01390, 0.8471 0.8333, 0.03280, 0.5443 0.7436, 0.04930, 0.2617 0.7049, 0.05667, 0.1669 0.6662, 0.06411, -0.0321 0.6274, 0.07172, -0.3350 0.6009, 0.07523, -1.0256 0.6069, 0.02889, -1.0282 0.6079, -0.01747, -1.0547 0.6167, -0.06381, -0.6663 0.6558, -0.05300, -0.1620 0.7045, -0.04117, -0.4387 0.7429, -0.03210, -0.5792 0.8333, -0.01400, -0.6220 0.9311, -0.00120, -0.5852 --------- Run Conditions: vel=103.8 ft/s Re=0.988x10^6 AOA=180.01 Flap deflection=60.00 Totals: Cl=0.1995 Cdp=0.6815 Cm(c/4)=0.1281 Cs=0.6814 Ch=-0.0140 Main component: Cl=-0.0370 Cdp=0.0250 Cm=-0.0025 Flap component: Cl=0.2365 Cdp=0.6564 Cm=0.1805 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -1.2614 0.5905, -0.01667, -1.2884 0.5709, 0.03110, -1.2552 0.5889, 0.07933, -1.3130 0.5500, 0.08689, -1.1739 0.5110, 0.09367, -1.1756 0.4731, 0.09830, -1.1672 0.4349, 0.10070, -1.1791 0.3960, 0.10120, -1.1729 0.3566, 0.10020, -1.2010 0.3172, 0.09790, -1.2150 0.2778, 0.09440, -1.2424 0.2393, 0.08960, -1.2683 0.2056, 0.08360, -1.2902 0.1633, 0.07610, -1.3457 0.1261, 0.06710, -1.3568 0.0900, 0.05640, -1.3966 0.0571, 0.04390, -1.4429 0.0283, 0.02940, -1.5262 0.0142, 0.01970, -1.6180 0.0081, 0.01410, -1.7137 0.0026, 0.00780, -1.7855 0.0000, 0.00000, -2.1796 0.0037, -0.00840, -1.6484 0.0112, -0.01420, -1.3385 0.0191, -0.01930, -1.2338 0.0397, -0.03030, -1.1598 0.0706, -0.04420, -1.1433 0.1037, -0.05710, -1.1827 0.1384, -0.06890, -1.2268 0.1741, -0.07950, -1.2366 0.2102, -0.08660, -1.2410 0.2472, -0.09640, -1.2570 0.2844, -0.10270, -1.2435 0.3225, -0.10690, -1.2327 0.3608, -0.10890, -1.2259 0.3991, -0.10830, -1.2179 0.4373, -0.10510, -1.1967 0.4757, -0.09890, -1.1973 0.5137, -0.09067, -1.1857 0.5611, -0.07859, -1.1941 16 Flap element taps 1.0000, 0.00130, -1.1072 0.9365, 0.01390, 0.9539 0.8333, 0.03280, 0.9685 0.7436, 0.04930, 0.7854 0.7049, 0.05667, 0.6787 0.6662, 0.06411, 0.4800 0.6274, 0.07172, 0.1243 0.6009, 0.07523, -1.0947 0.6069, 0.02889, -1.0948 0.6079, -0.01747, -1.1160 0.6167, -0.06381, -1.3070 0.6558, -0.05300, -1.2127 0.7045, -0.04117, -1.1919 0.7429, -0.03210, -1.1583 0.8333, -0.01400, -1.1506 0.9311, -0.00120, -1.1287 --------- Run Conditions: vel=104.3 ft/s Re=0.992x10^6 AOA=210.01 Flap deflection=60.00 Totals: Cl=-0.0343 Cdp=0.7876 Cm(c/4)=0.1168 Cs=0.6991 Ch=-0.0706 Main component: Cl=0.1001 Cdp=0.0819 Cm=0.0366 Flap component: Cl=-0.1344 Cdp=0.7057 Cm=0.1712 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -1.1960 0.5905, -0.01667, -1.1945 0.5709, 0.03110, -1.1926 0.5889, 0.07933, -1.2359 0.5500, 0.08689, -1.2470 0.5110, 0.09367, -1.2889 0.4731, 0.09830, -1.2749 0.4349, 0.10070, -1.2321 0.3960, 0.10120, -1.0612 0.3566, 0.10020, -0.7905 0.3172, 0.09790, -0.6062 0.2778, 0.09440, -0.5514 0.2393, 0.08960, -0.5958 0.2056, 0.08360, -0.7218 0.1633, 0.07610, -0.8937 0.1261, 0.06710, -1.0883 0.0900, 0.05640, -1.3160 0.0571, 0.04390, -1.5901 0.0283, 0.02940, -1.7895 0.0142, 0.01970, -1.7827 0.0081, 0.01410, -1.6431 0.0026, 0.00780, -1.2764 0.0000, 0.00000, -1.3145 0.0037, -0.00840, -1.3308 0.0112, -0.01420, -1.3390 0.0191, -0.01930, -1.3845 0.0397, -0.03030, -1.4650 0.0706, -0.04420, -1.4582 0.1037, -0.05710, -1.3869 0.1384, -0.06890, -1.3198 0.1741, -0.07950, -1.2761 0.2102, -0.08660, -1.2547 0.2472, -0.09640, -1.2564 0.2844, -0.10270, -1.2662 0.3225, -0.10690, -1.2477 0.3608, -0.10890, -1.2627 0.3991, -0.10830, -1.2488 0.4373, -0.10510, -1.2391 0.4757, -0.09890, -1.2312 0.5137, -0.09067, -1.2039 0.5611, -0.07859, -1.1974 16 Flap element taps 1.0000, 0.00130, -1.1228 0.9365, 0.01390, 0.6168 0.8333, 0.03280, 0.9461 0.7436, 0.04930, 0.9953 0.7049, 0.05667, 0.9745 0.6662, 0.06411, 0.8814 0.6274, 0.07172, 0.6196 0.6009, 0.07523, -1.1654 0.6069, 0.02889, -1.1675 0.6079, -0.01747, -1.1876 0.6167, -0.06381, -1.1473 0.6558, -0.05300, -1.1501 0.7045, -0.04117, -1.1729 0.7429, -0.03210, -1.1519 0.8333, -0.01400, -1.1503 0.9311, -0.00120, -1.1348 --------- Run Conditions: vel=103.8 ft/s Re=0.988x10^6 AOA=240.01 Flap deflection=60.00 Totals: Cl=0.1793 Cdp=1.5047 Cm(c/4)=0.3357 Cs=0.5968 Ch=-0.1648 Main component: Cl=0.4812 Cdp=0.7904 Cm=0.3421 Flap component: Cl=-0.3019 Cdp=0.7143 Cm=0.3418 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -1.6433 0.5905, -0.01667, -1.6304 0.5709, 0.03110, -1.6021 0.5889, 0.07933, -1.6692 0.5500, 0.08689, 0.9737 0.5110, 0.09367, 0.9811 0.4731, 0.09830, 0.8789 0.4349, 0.10070, 0.7399 0.3960, 0.10120, 0.5930 0.3566, 0.10020, 0.4667 0.3172, 0.09790, 0.3151 0.2778, 0.09440, 0.1354 0.2393, 0.08960, -0.0468 0.2056, 0.08360, -0.2699 0.1633, 0.07610, -0.4968 0.1261, 0.06710, -0.7542 0.0900, 0.05640, -1.0658 0.0571, 0.04390, -1.4460 0.0283, 0.02940, -1.6424 0.0142, 0.01970, -1.5291 0.0081, 0.01410, -1.5349 0.0026, 0.00780, -1.4340 0.0000, 0.00000, -1.5411 0.0037, -0.00840, -1.5608 0.0112, -0.01420, -1.5453 0.0191, -0.01930, -1.5554 0.0397, -0.03030, -1.5731 0.0706, -0.04420, -1.6119 0.1037, -0.05710, -1.6354 0.1384, -0.06890, -1.6403 0.1741, -0.07950, -1.6348 0.2102, -0.08660, -1.6515 0.2472, -0.09640, -1.6555 0.2844, -0.10270, -1.6601 0.3225, -0.10690, -1.6510 0.3608, -0.10890, -1.6822 0.3991, -0.10830, -1.6890 0.4373, -0.10510, -1.6891 0.4757, -0.09890, -1.6856 0.5137, -0.09067, -1.6297 0.5611, -0.07859, -1.6217 16 Flap element taps 1.0000, 0.00130, -1.0008 0.9365, 0.01390, -0.0120 0.8333, 0.03280, 0.4030 0.7436, 0.04930, 0.6413 0.7049, 0.05667, 0.7635 0.6662, 0.06411, 0.8579 0.6274, 0.07172, 0.9584 0.6009, 0.07523, 0.4670 0.6069, 0.02889, 0.6008 0.6079, -0.01747, 0.2584 0.6167, -0.06381, -1.7372 0.6558, -0.05300, -1.7805 0.7045, -0.04117, -1.8013 0.7429, -0.03210, -1.8455 0.8333, -0.01400, -1.7667 0.9311, -0.00120, -1.3074 --------- Run Conditions: vel=104.6 ft/s Re=0.996x10^6 AOA=269.01 Flap deflection=60.00 Totals: Cl=0.2588 Cdp=1.3840 Cm(c/4)=0.1848 Cs=-0.2349 Ch=-0.0224 Main component: Cl=0.1199 Cdp=1.2214 Cm=0.4021 Flap component: Cl=0.1390 Cdp=0.1626 Cm=0.1298 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -1.6712 0.5905, -0.01667, -1.6658 0.5709, 0.03110, -1.6287 0.5889, 0.07933, -1.7168 0.5500, 0.08689, 0.6176 0.5110, 0.09367, 0.8309 0.4731, 0.09830, 0.9487 0.4349, 0.10070, 0.9864 0.3960, 0.10120, 0.9824 0.3566, 0.10020, 0.9969 0.3172, 0.09790, 0.9547 0.2778, 0.09440, 0.8866 0.2393, 0.08960, 0.8042 0.2056, 0.08360, 0.6674 0.1633, 0.07610, 0.5179 0.1261, 0.06710, 0.2929 0.0900, 0.05640, -0.0099 0.0571, 0.04390, -0.5034 0.0283, 0.02940, -1.1457 0.0142, 0.01970, -1.5835 0.0081, 0.01410, -1.6168 0.0026, 0.00780, -1.3861 0.0000, 0.00000, -1.4797 0.0037, -0.00840, -1.5027 0.0112, -0.01420, -1.4954 0.0191, -0.01930, -1.5012 0.0397, -0.03030, -1.5220 0.0706, -0.04420, -1.5701 0.1037, -0.05710, -1.6048 0.1384, -0.06890, -1.6157 0.1741, -0.07950, -1.6438 0.2102, -0.08660, -1.6703 0.2472, -0.09640, -1.6786 0.2844, -0.10270, -1.6863 0.3225, -0.10690, -1.6467 0.3608, -0.10890, -1.6718 0.3991, -0.10830, -1.6536 0.4373, -0.10510, -1.6672 0.4757, -0.09890, -1.6704 0.5137, -0.09067, -1.6513 0.5611, -0.07859, -1.6436 16 Flap element taps 1.0000, 0.00130, -0.9986 0.9365, 0.01390, -1.0146 0.8333, 0.03280, -1.6305 0.7436, 0.04930, -1.6936 0.7049, 0.05667, -1.6663 0.6662, 0.06411, -1.6540 0.6274, 0.07172, -1.6376 0.6009, 0.07523, -1.6347 0.6069, 0.02889, 0.9556 0.6079, -0.01747, 0.9750 0.6167, -0.06381, -2.2023 0.6558, -0.05300, -2.3076 0.7045, -0.04117, -1.9468 0.7429, -0.03210, -1.1450 0.8333, -0.01400, -1.1881 0.9311, -0.00120, -1.1399