S809 VENTED AILERON MODEL, 18 IN CHORD --------- Run Conditions: vel=100.8 ft/s Re=0.995x10^6 AOA=-5.97 Flap deflection=0.00 Totals: Cl=-0.5043 Cdp=0.0240 Cm(c/4)=-0.0085 Cs=0.0285 Ch=-0.0241 Main component: Cl=-0.4871 Cdp=0.0425 Cm=0.1093 Flap component: Cl=-0.0172 Cdp=-0.0184 Cm=0.0082 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.2904 0.5871, 0.07930, -0.1380 0.5501, 0.08690, -0.3985 0.5112, 0.09370, -0.4187 0.4731, 0.09830, -0.4502 0.4349, 0.10070, -0.4420 0.3960, 0.10120, -0.4321 0.3566, 0.10020, -0.3228 0.3172, 0.09790, -0.2557 0.2778, 0.09440, -0.2143 0.2393, 0.08960, -0.1620 0.2056, 0.08360, -0.1213 0.1633, 0.07610, 0.0289 0.1261, 0.06710, 0.1279 0.0900, 0.05640, 0.3034 0.0571, 0.04390, 0.5011 0.0283, 0.02940, 0.7783 0.0142, 0.01970, 0.9660 0.0081, 0.01410, 0.9736 0.0026, 0.00780, 0.7889 0.0000, 0.00000, -0.2693 0.0037, -0.00840, -1.2753 0.0112, -0.01420, -1.1054 0.0191, -0.01930, -0.9518 0.0397, -0.03030, -0.7828 0.0706, -0.04420, -0.7898 0.1037, -0.05710, -0.8512 0.1384, -0.06890, -0.8782 0.1741, -0.07950, -0.9460 0.2102, -0.08660, -1.0645 0.2472, -0.09640, -1.1432 0.2844, -0.10270, -1.1980 0.3225, -0.10690, -1.1920 0.3608, -0.10890, -1.2240 0.3991, -0.10830, -1.1398 0.4373, -0.10510, -1.0779 0.4757, -0.09890, -1.0640 0.5137, -0.09070, -0.5293 0.5514, -0.08120, -0.3580 0.5917, -0.06870, -0.1381 0.5917, -0.02380, -0.1928 0.5917, 0.02120, -0.1142 16 Flap element taps 1.0000, 0.00130, 0.1809 0.9365, 0.01390, 0.1143 0.8333, 0.03280, 0.0710 0.7436, 0.04930, 0.0257 0.7049, 0.05670, -0.0580 0.6667, 0.05450, 0.4667 0.6302, 0.03770, -0.2618 0.6083, 0.01980, -0.1678 0.6000, 0.00000, -0.2196 0.6076, -0.01900, -0.1934 0.6285, -0.03060, -0.1821 0.6667, -0.04090, -0.1384 0.7046, -0.04120, -0.1211 0.7429, -0.03210, -0.0285 0.8333, -0.01400, 0.1132 0.9311, -0.00120, 0.1974 --------- Run Conditions: vel=101.3 ft/s Re=0.997x10^6 AOA=-0.02 Flap deflection=0.00 Totals: Cl=0.1077 Cdp=0.0096 Cm(c/4)=-0.0294 Cs=-0.0096 Ch=0.0030 Main component: Cl=0.0423 Cdp=0.0321 Cm=-0.0040 Flap component: Cl=0.0654 Cdp=-0.0226 Cm=-0.0524 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1704 0.5871, 0.07930, -0.1776 0.5501, 0.08690, -0.6215 0.5112, 0.09370, -0.6235 0.4731, 0.09830, -0.6688 0.4349, 0.10070, -0.7071 0.3960, 0.10120, -0.7460 0.3566, 0.10020, -0.6566 0.3172, 0.09790, -0.6232 0.2778, 0.09440, -0.6179 0.2393, 0.08960, -0.6094 0.2056, 0.08360, -0.6222 0.1633, 0.07610, -0.5071 0.1261, 0.06710, -0.4675 0.0900, 0.05640, -0.3588 0.0571, 0.04390, -0.2481 0.0283, 0.02940, -0.0402 0.0142, 0.01970, 0.1996 0.0081, 0.01410, 0.3316 0.0026, 0.00780, 0.6669 0.0000, 0.00000, 1.0197 0.0037, -0.00840, 0.7628 0.0112, -0.01420, 0.5108 0.0191, -0.01930, 0.3928 0.0397, -0.03030, 0.2259 0.0706, -0.04420, 0.0204 0.1037, -0.05710, -0.1390 0.1384, -0.06890, -0.2268 0.1741, -0.07950, -0.3494 0.2102, -0.08660, -0.5231 0.2472, -0.09640, -0.6328 0.2844, -0.10270, -0.7365 0.3225, -0.10690, -0.7652 0.3608, -0.10890, -0.8523 0.3991, -0.10830, -0.8248 0.4373, -0.10510, -0.7713 0.4757, -0.09890, -0.7084 0.5137, -0.09070, -0.6734 0.5514, -0.08120, -0.2610 0.5917, -0.06870, -0.1401 0.5917, -0.02380, -0.1371 0.5917, 0.02120, -0.1632 16 Flap element taps 1.0000, 0.00130, 0.1819 0.9365, 0.01390, 0.0995 0.8333, 0.03280, 0.0067 0.7436, 0.04930, -0.0905 0.7049, 0.05670, -0.1684 0.6667, 0.05450, -0.1267 0.6302, 0.03770, -0.1643 0.6083, 0.01980, -0.1505 0.6000, 0.00000, -0.1678 0.6076, -0.01900, -0.1825 0.6285, -0.03060, -0.2283 0.6667, -0.04090, 0.2403 0.7046, -0.04120, -0.0086 0.7429, -0.03210, 0.0975 0.8333, -0.01400, 0.2213 0.9311, -0.00120, 0.2771 Wake drag found for this condition, Cdw=0.0124 --------- Run Conditions: vel=101.6 ft/s Re=0.997x10^6 AOA=3.00 Flap deflection=0.00 Totals: Cl=0.4269 Cdp=0.0081 Cm(c/4)=-0.0383 Cs=0.0143 Ch=0.0129 Main component: Cl=0.3301 Cdp=0.0250 Cm=-0.0697 Flap component: Cl=0.0968 Cdp=-0.0169 Cm=-0.0753 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1938 0.5871, 0.07930, -0.2216 0.5501, 0.08690, -0.7568 0.5112, 0.09370, -0.7474 0.4731, 0.09830, -0.7860 0.4349, 0.10070, -0.8414 0.3960, 0.10120, -0.9097 0.3566, 0.10020, -0.8328 0.3172, 0.09790, -0.8210 0.2778, 0.09440, -0.8360 0.2393, 0.08960, -0.8544 0.2056, 0.08360, -0.9053 0.1633, 0.07610, -0.8161 0.1261, 0.06710, -0.8237 0.0900, 0.05640, -0.7708 0.0571, 0.04390, -0.7528 0.0283, 0.02940, -0.6789 0.0142, 0.01970, -0.5562 0.0081, 0.01410, -0.5044 0.0026, 0.00780, -0.1437 0.0000, 0.00000, 0.4738 0.0037, -0.00840, 1.0204 0.0112, -0.01420, 0.9087 0.0191, -0.01930, 0.7943 0.0397, -0.03030, 0.5910 0.0706, -0.04420, 0.3474 0.1037, -0.05710, 0.1637 0.1384, -0.06890, 0.0693 0.1741, -0.07950, -0.0699 0.2102, -0.08660, -0.2640 0.2472, -0.09640, -0.3795 0.2844, -0.10270, -0.5030 0.3225, -0.10690, -0.5413 0.3608, -0.10890, -0.6507 0.3991, -0.10830, -0.6417 0.4373, -0.10510, -0.6210 0.4757, -0.09890, -0.5465 0.5137, -0.09070, -0.5013 0.5514, -0.08120, -0.1737 0.5917, -0.06870, -0.1200 0.5917, -0.02380, -0.0600 0.5917, 0.02120, -0.1677 16 Flap element taps 1.0000, 0.00130, 0.1649 0.9365, 0.01390, 0.0856 0.8333, 0.03280, -0.0249 0.7436, 0.04930, -0.1565 0.7049, 0.05670, -0.2734 0.6667, 0.05450, -0.1516 0.6302, 0.03770, -0.1615 0.6083, 0.01980, -0.1588 0.6000, 0.00000, -0.1990 0.6076, -0.01900, -0.2062 0.6285, -0.03060, -0.2329 0.6667, -0.04090, 0.4898 0.7046, -0.04120, -0.0061 0.7429, -0.03210, 0.1435 0.8333, -0.01400, 0.2568 0.9311, -0.00120, 0.2959 Wake drag found for this condition, Cdw=0.0141 --------- Run Conditions: vel=101.8 ft/s Re=0.995x10^6 AOA=6.02 Flap deflection=0.00 Totals: Cl=0.6951 Cdp=0.0098 Cm(c/4)=-0.0369 Cs=0.0631 Ch=0.0168 Main component: Cl=0.5747 Cdp=0.0181 Cm=-0.1167 Flap component: Cl=0.1204 Cdp=-0.0083 Cm=-0.0933 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1958 0.5871, 0.07930, -0.3265 0.5501, 0.08690, -0.4748 0.5112, 0.09370, -0.7472 0.4731, 0.09830, -0.8916 0.4349, 0.10070, -0.9605 0.3960, 0.10120, -1.0510 0.3566, 0.10020, -0.9907 0.3172, 0.09790, -1.0040 0.2778, 0.09440, -1.0407 0.2393, 0.08960, -1.0899 0.2056, 0.08360, -1.1797 0.1633, 0.07610, -1.1227 0.1261, 0.06710, -1.1857 0.0900, 0.05640, -1.2073 0.0571, 0.04390, -1.3053 0.0283, 0.02940, -1.4229 0.0142, 0.01970, -1.5024 0.0081, 0.01410, -1.6338 0.0026, 0.00780, -1.3289 0.0000, 0.00000, -0.9321 0.0037, -0.00840, 0.8527 0.0112, -0.01420, 1.0207 0.0191, -0.01930, 0.9912 0.0397, -0.03030, 0.8385 0.0706, -0.04420, 0.6024 0.1037, -0.05710, 0.4182 0.1384, -0.06890, 0.3206 0.1741, -0.07950, 0.1715 0.2102, -0.08660, -0.0351 0.2472, -0.09640, -0.1524 0.2844, -0.10270, -0.2903 0.3225, -0.10690, -0.3379 0.3608, -0.10890, -0.4651 0.3991, -0.10830, -0.4722 0.4373, -0.10510, -0.4827 0.4757, -0.09890, -0.4169 0.5137, -0.09070, -0.3559 0.5514, -0.08120, -0.2799 0.5917, -0.06870, -0.1057 0.5917, -0.02380, 0.0027 0.5917, 0.02120, -0.1800 16 Flap element taps 1.0000, 0.00130, 0.0841 0.9365, 0.01390, 0.0264 0.8333, 0.03280, -0.0745 0.7436, 0.04930, -0.1958 0.7049, 0.05670, -0.3047 0.6667, 0.05450, -0.1820 0.6302, 0.03770, -0.1649 0.6083, 0.01980, -0.1764 0.6000, 0.00000, -0.2594 0.6076, -0.01900, -0.2341 0.6285, -0.03060, -0.2150 0.6667, -0.04090, 0.6366 0.7046, -0.04120, -0.0141 0.7429, -0.03210, 0.1751 0.8333, -0.01400, 0.2737 0.9311, -0.00120, 0.2880 Wake drag found for this condition, Cdw=0.0146 --------- Run Conditions: vel=101.3 ft/s Re=0.991x10^6 AOA=9.01 Flap deflection=0.00 Totals: Cl=0.8092 Cdp=0.0213 Cm(c/4)=-0.0208 Cs=0.1057 Ch=0.0068 Main component: Cl=0.6937 Cdp=0.0182 Cm=-0.1301 Flap component: Cl=0.1155 Cdp=0.0031 Cm=-0.0914 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.1858 0.5871, 0.07930, -0.2499 0.5501, 0.08690, -0.3782 0.5112, 0.09370, -0.6029 0.4731, 0.09830, -0.7932 0.4349, 0.10070, -0.9026 0.3960, 0.10120, -1.0275 0.3566, 0.10020, -0.9938 0.3172, 0.09790, -1.0271 0.2778, 0.09440, -1.0922 0.2393, 0.08960, -1.1766 0.2056, 0.08360, -1.3066 0.1633, 0.07610, -1.2846 0.1261, 0.06710, -1.3913 0.0900, 0.05640, -1.4685 0.0571, 0.04390, -1.7142 0.0283, 0.02940, -2.0291 0.0142, 0.01970, -2.3074 0.0081, 0.01410, -2.6790 0.0026, 0.00780, -2.5201 0.0000, 0.00000, -2.4711 0.0037, -0.00840, 0.4616 0.0112, -0.01420, 0.9623 0.0191, -0.01930, 1.0239 0.0397, -0.03030, 0.9560 0.0706, -0.04420, 0.7492 0.1037, -0.05710, 0.5716 0.1384, -0.06890, 0.4757 0.1741, -0.07950, 0.3246 0.2102, -0.08660, 0.1092 0.2472, -0.09640, -0.0120 0.2844, -0.10270, -0.1608 0.3225, -0.10690, -0.2165 0.3608, -0.10890, -0.3590 0.3991, -0.10830, -0.3813 0.4373, -0.10510, -0.4146 0.4757, -0.09890, -0.3629 0.5137, -0.09070, -0.2976 0.5514, -0.08120, -0.2877 0.5917, -0.06870, -0.1186 0.5917, -0.02380, -0.0179 0.5917, 0.02120, -0.1722 16 Flap element taps 1.0000, 0.00130, -0.0985 0.9365, 0.01390, -0.1310 0.8333, 0.03280, -0.1223 0.7436, 0.04930, -0.1469 0.7049, 0.05670, -0.1843 0.6667, 0.05450, -0.1671 0.6302, 0.03770, -0.1558 0.6083, 0.01980, -0.1721 0.6000, 0.00000, -0.2550 0.6076, -0.01900, -0.2534 0.6285, -0.03060, -0.1995 0.6667, -0.04090, 0.6401 0.7046, -0.04120, -0.0494 0.7429, -0.03210, 0.1522 0.8333, -0.01400, 0.2328 0.9311, -0.00120, 0.2098 Wake drag found for this condition, Cdw=0.0265 --------- Run Conditions: vel=101.5 ft/s Re=0.990x10^6 AOA=12.00 Flap deflection=0.00 Totals: Cl=1.0524 Cdp=0.0294 Cm(c/4)=-0.0226 Cs=0.1901 Ch=0.0328 Main component: Cl=0.8992 Cdp=0.0470 Cm=-0.1686 Flap component: Cl=0.1531 Cdp=-0.0176 Cm=-0.1129 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.3594 0.5871, 0.07930, -0.3905 0.5501, 0.08690, -0.4524 0.5112, 0.09370, -0.5979 0.4731, 0.09830, -0.7942 0.4349, 0.10070, -0.9384 0.3960, 0.10120, -1.1040 0.3566, 0.10020, -1.0981 0.3172, 0.09790, -1.1600 0.2778, 0.09440, -1.2559 0.2393, 0.08960, -1.3742 0.2056, 0.08360, -1.5451 0.1633, 0.07610, -1.5691 0.1261, 0.06710, -1.7432 0.0900, 0.05640, -1.9185 0.0571, 0.04390, -2.2679 0.0283, 0.02940, -2.7918 0.0142, 0.01970, -3.4099 0.0081, 0.01410, -4.4085 0.0026, 0.00780, -4.4592 0.0000, 0.00000, -5.0152 0.0037, -0.00840, -0.3598 0.0112, -0.01420, 0.7117 0.0191, -0.01930, 0.9537 0.0397, -0.03030, 1.0272 0.0706, -0.04420, 0.8868 0.1037, -0.05710, 0.7365 0.1384, -0.06890, 0.6535 0.1741, -0.07950, 0.5049 0.2102, -0.08660, 0.2896 0.2472, -0.09640, 0.1704 0.2844, -0.10270, 0.0136 0.3225, -0.10690, -0.0498 0.3608, -0.10890, -0.2061 0.3991, -0.10830, -0.2431 0.4373, -0.10510, -0.3060 0.4757, -0.09890, -0.2854 0.5137, -0.09070, -0.2518 0.5514, -0.08120, -0.2006 0.5917, -0.06870, -0.4968 0.5917, -0.02380, -0.1368 0.5917, 0.02120, -0.3653 16 Flap element taps 1.0000, 0.00130, -0.0634 0.9365, 0.01390, -0.0719 0.8333, 0.03280, -0.0942 0.7436, 0.04930, -0.1909 0.7049, 0.05670, -0.3240 0.6667, 0.05450, -0.2937 0.6302, 0.03770, -0.2445 0.6083, 0.01980, -0.4134 0.6000, 0.00000, -1.1991 0.6076, -0.01900, -1.2342 0.6285, -0.03060, 0.6751 0.6667, -0.04090, 0.5442 0.7046, -0.04120, -0.0208 0.7429, -0.03210, 0.1964 0.8333, -0.01400, 0.2795 0.9311, -0.00120, 0.2462 --------- Run Conditions: vel=101.2 ft/s Re=0.985x10^6 AOA=14.97 Flap deflection=0.00 Totals: Cl=1.1670 Cdp=0.0653 Cm(c/4)=-0.0303 Cs=0.2384 Ch=0.0422 Main component: Cl=0.9771 Cdp=0.0698 Cm=-0.1758 Flap component: Cl=0.1898 Cdp=-0.0045 Cm=-0.1406 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.4838 0.5871, 0.07930, -0.4976 0.5501, 0.08690, -0.5057 0.5112, 0.09370, -0.5300 0.4731, 0.09830, -0.6191 0.4349, 0.10070, -0.7607 0.3960, 0.10120, -0.9700 0.3566, 0.10020, -1.0094 0.3172, 0.09790, -1.1144 0.2778, 0.09440, -1.2414 0.2393, 0.08960, -1.3914 0.2056, 0.08360, -1.6000 0.1633, 0.07610, -1.6679 0.1261, 0.06710, -1.8977 0.0900, 0.05640, -2.1440 0.0571, 0.04390, -2.6061 0.0283, 0.02940, -3.3434 0.0142, 0.01970, -4.1253 0.0081, 0.01410, -5.5303 0.0026, 0.00780, -6.0357 0.0000, 0.00000, -7.0899 0.0037, -0.00840, -1.1304 0.0112, -0.01420, 0.4156 0.0191, -0.01930, 0.8248 0.0397, -0.03030, 1.0317 0.0706, -0.04420, 0.9522 0.1037, -0.05710, 0.8294 0.1384, -0.06890, 0.7574 0.1741, -0.07950, 0.6193 0.2102, -0.08660, 0.4029 0.2472, -0.09640, 0.2844 0.2844, -0.10270, 0.1231 0.3225, -0.10690, 0.0554 0.3608, -0.10890, -0.1079 0.3991, -0.10830, -0.1585 0.4373, -0.10510, -0.2370 0.4757, -0.09890, -0.2300 0.5137, -0.09070, -0.2107 0.5514, -0.08120, -0.1674 0.5917, -0.06870, -0.5356 0.5917, -0.02380, -0.1889 0.5917, 0.02120, -0.5365 16 Flap element taps 1.0000, 0.00130, -0.1821 0.9365, 0.01390, -0.1939 0.8333, 0.03280, -0.2107 0.7436, 0.04930, -0.2858 0.7049, 0.05670, -0.4053 0.6667, 0.05450, -0.4394 0.6302, 0.03770, -0.3677 0.6083, 0.01980, -0.6016 0.6000, 0.00000, -1.3870 0.6076, -0.01900, -1.3221 0.6285, -0.03060, 0.7362 0.6667, -0.04090, 0.5443 0.7046, -0.04120, -0.0220 0.7429, -0.03210, 0.1886 0.8333, -0.01400, 0.2561 0.9311, -0.00120, 0.1986 --------- Run Conditions: vel=98.1 ft/s Re=0.953x10^6 AOA=17.96 Flap deflection=0.00 Totals: Cl=0.6178 Cdp=0.2569 Cm(c/4)=-0.0927 Cs=-0.0539 Ch=0.0449 Main component: Cl=0.3860 Cdp=0.2396 Cm=-0.0841 Flap component: Cl=0.2318 Cdp=0.0172 Cm=-0.1753 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.7339 0.5871, 0.07930, -0.6884 0.5501, 0.08690, -0.6910 0.5112, 0.09370, -0.6891 0.4731, 0.09830, -0.7183 0.4349, 0.10070, -0.7264 0.3960, 0.10120, -0.8015 0.3566, 0.10020, -0.7192 0.3172, 0.09790, -0.7178 0.2778, 0.09440, -0.7209 0.2393, 0.08960, -0.7293 0.2056, 0.08360, -0.8033 0.1633, 0.07610, -0.7137 0.1261, 0.06710, -0.7634 0.0900, 0.05640, -0.7190 0.0571, 0.04390, -0.7412 0.0283, 0.02940, -0.7590 0.0142, 0.01970, -0.7574 0.0081, 0.01410, -0.8250 0.0026, 0.00780, -0.7064 0.0000, 0.00000, -1.0169 0.0037, -0.00840, 0.6063 0.0112, -0.01420, 0.9651 0.0191, -0.01930, 1.0218 0.0397, -0.03030, 0.9810 0.0706, -0.04420, 0.8085 0.1037, -0.05710, 0.6479 0.1384, -0.06890, 0.5669 0.1741, -0.07950, 0.4132 0.2102, -0.08660, 0.1840 0.2472, -0.09640, 0.0529 0.2844, -0.10270, -0.1188 0.3225, -0.10690, -0.1974 0.3608, -0.10890, -0.3728 0.3991, -0.10830, -0.4281 0.4373, -0.10510, -0.5082 0.4757, -0.09890, -0.4938 0.5137, -0.09070, -0.4673 0.5514, -0.08120, -0.4149 0.5917, -0.06870, -0.8461 0.5917, -0.02380, -0.3403 0.5917, 0.02120, -0.7631 16 Flap element taps 1.0000, 0.00130, -0.5105 0.9365, 0.01390, -0.5310 0.8333, 0.03280, -0.5286 0.7436, 0.04930, -0.5916 0.7049, 0.05670, -0.7362 0.6667, 0.05450, -0.7422 0.6302, 0.03770, -0.5948 0.6083, 0.01980, -0.8422 0.6000, 0.00000, -1.7983 0.6076, -0.01900, -1.7650 0.6285, -0.03060, 0.6495 0.6667, -0.04090, 0.4431 0.7046, -0.04120, -0.2563 0.7429, -0.03210, 0.0036 0.8333, -0.01400, 0.0732 0.9311, -0.00120, -0.0119 --------- Run Conditions: vel=97.4 ft/s Re=0.943x10^6 AOA=19.97 Flap deflection=0.00 Totals: Cl=0.6212 Cdp=0.2991 Cm(c/4)=-0.1042 Cs=-0.0689 Ch=0.0474 Main component: Cl=0.3734 Cdp=0.2626 Cm=-0.0851 Flap component: Cl=0.2479 Cdp=0.0364 Cm=-0.1906 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.7159 0.5871, 0.07930, -0.6826 0.5501, 0.08690, -0.6853 0.5112, 0.09370, -0.6935 0.4731, 0.09830, -0.6975 0.4349, 0.10070, -0.7028 0.3960, 0.10120, -0.7860 0.3566, 0.10020, -0.6977 0.3172, 0.09790, -0.6975 0.2778, 0.09440, -0.6969 0.2393, 0.08960, -0.7033 0.2056, 0.08360, -0.7714 0.1633, 0.07610, -0.6684 0.1261, 0.06710, -0.7142 0.0900, 0.05640, -0.6671 0.0571, 0.04390, -0.6937 0.0283, 0.02940, -0.7107 0.0142, 0.01970, -0.7142 0.0081, 0.01410, -0.7811 0.0026, 0.00780, -0.6653 0.0000, 0.00000, -0.9640 0.0037, -0.00840, 0.5601 0.0112, -0.01420, 0.9473 0.0191, -0.01930, 1.0185 0.0397, -0.03030, 0.9980 0.0706, -0.04420, 0.8355 0.1037, -0.05710, 0.6818 0.1384, -0.06890, 0.6084 0.1741, -0.07950, 0.4560 0.2102, -0.08660, 0.2250 0.2472, -0.09640, 0.0964 0.2844, -0.10270, -0.0802 0.3225, -0.10690, -0.1555 0.3608, -0.10890, -0.3382 0.3991, -0.10830, -0.3979 0.4373, -0.10510, -0.4860 0.4757, -0.09890, -0.4775 0.5137, -0.09070, -0.4597 0.5514, -0.08120, -0.4095 0.5917, -0.06870, -0.8448 0.5917, -0.02380, -0.4411 0.5917, 0.02120, -0.7633 16 Flap element taps 1.0000, 0.00130, -0.5664 0.9365, 0.01390, -0.5777 0.8333, 0.03280, -0.6101 0.7436, 0.04930, -0.7153 0.7049, 0.05670, -0.8664 0.6667, 0.05450, -0.7636 0.6302, 0.03770, -0.5810 0.6083, 0.01980, -0.8417 0.6000, 0.00000, -1.8126 0.6076, -0.01900, -1.7741 0.6285, -0.03060, 0.6481 0.6667, -0.04090, 0.4375 0.7046, -0.04120, -0.2667 0.7429, -0.03210, -0.0096 0.8333, -0.01400, 0.0559 0.9311, -0.00120, -0.0376 --------- Run Conditions: vel=105.3 ft/s Re=1.008x10^6 AOA=23.97 Flap deflection=0.00 Totals: Cl=0.6639 Cdp=0.3786 Cm(c/4)=-0.1212 Cs=-0.0763 Ch=0.0428 Main component: Cl=0.3997 Cdp=0.3106 Cm=-0.1009 Flap component: Cl=0.2642 Cdp=0.0681 Cm=-0.2104 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.7372 0.5871, 0.07930, -0.7220 0.5501, 0.08690, -0.7229 0.5112, 0.09370, -0.7248 0.4731, 0.09830, -0.7341 0.4349, 0.10070, -0.7281 0.3960, 0.10120, -0.7123 0.3566, 0.10020, -0.7256 0.3172, 0.09790, -0.7232 0.2778, 0.09440, -0.7232 0.2393, 0.08960, -0.7242 0.2056, 0.08360, -0.7139 0.1633, 0.07610, -0.7224 0.1261, 0.06710, -0.7186 0.0900, 0.05640, -0.7214 0.0571, 0.04390, -0.7230 0.0283, 0.02940, -0.7324 0.0142, 0.01970, -0.7336 0.0081, 0.01410, -0.7351 0.0026, 0.00780, -0.7013 0.0000, 0.00000, -0.9587 0.0037, -0.00840, 0.3645 0.0112, -0.01420, 0.8575 0.0191, -0.01930, 0.9733 0.0397, -0.03030, 1.0029 0.0706, -0.04420, 0.9116 0.1037, -0.05710, 0.7861 0.1384, -0.06890, 0.6445 0.1741, -0.07950, 0.5162 0.2102, -0.08660, 0.3757 0.2472, -0.09640, 0.2051 0.2844, -0.10270, 0.0658 0.3225, -0.10690, -0.0883 0.3608, -0.10890, -0.2244 0.3991, -0.10830, -0.3418 0.4373, -0.10510, -0.4006 0.4757, -0.09890, -0.4062 0.5137, -0.09070, -0.4099 0.5514, -0.08120, -0.3649 0.5917, -0.06870, -0.8579 0.5917, -0.02380, -0.3816 0.5917, 0.02120, -0.8130 16 Flap element taps 1.0000, 0.00130, -0.7227 0.9365, 0.01390, -0.7509 0.8333, 0.03280, -0.7417 0.7436, 0.04930, -0.7446 0.7049, 0.05670, -0.8811 0.6667, 0.05450, -0.7846 0.6302, 0.03770, -0.6098 0.6083, 0.01980, -0.8970 0.6000, 0.00000, -1.8623 0.6076, -0.01900, -1.7778 0.6285, -0.03060, 0.6696 0.6667, -0.04090, 0.4444 0.7046, -0.04120, -0.2751 0.7429, -0.03210, -0.0159 0.8333, -0.01400, 0.0182 0.9311, -0.00120, -0.0915 --------- Run Conditions: vel=103.7 ft/s Re=0.993x10^6 AOA=26.99 Flap deflection=0.00 Totals: Cl=0.7695 Cdp=0.4850 Cm(c/4)=-0.1493 Cs=-0.0830 Ch=0.0510 Main component: Cl=0.4731 Cdp=0.3835 Cm=-0.1336 Flap component: Cl=0.2964 Cdp=0.1015 Cm=-0.2421 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.8438 0.5871, 0.07930, -0.8247 0.5501, 0.08690, -0.8233 0.5112, 0.09370, -0.8259 0.4731, 0.09830, -0.8399 0.4349, 0.10070, -0.8327 0.3960, 0.10120, -0.8138 0.3566, 0.10020, -0.8268 0.3172, 0.09790, -0.8233 0.2778, 0.09440, -0.8242 0.2393, 0.08960, -0.8240 0.2056, 0.08360, -0.8139 0.1633, 0.07610, -0.8217 0.1261, 0.06710, -0.8183 0.0900, 0.05640, -0.8200 0.0571, 0.04390, -0.8197 0.0283, 0.02940, -0.8268 0.0142, 0.01970, -0.8277 0.0081, 0.01410, -0.8297 0.0026, 0.00780, -0.7950 0.0000, 0.00000, -0.8786 0.0037, -0.00840, 0.1464 0.0112, -0.01420, 0.7462 0.0191, -0.01930, 0.9173 0.0397, -0.03030, 1.0107 0.0706, -0.04420, 0.9601 0.1037, -0.05710, 0.8588 0.1384, -0.06890, 0.7344 0.1741, -0.07950, 0.6147 0.2102, -0.08660, 0.4831 0.2472, -0.09640, 0.3194 0.2844, -0.10270, 0.1831 0.3225, -0.10690, 0.0299 0.3608, -0.10890, -0.1102 0.3991, -0.10830, -0.2333 0.4373, -0.10510, -0.3037 0.4757, -0.09890, -0.3209 0.5137, -0.09070, -0.3460 0.5514, -0.08120, -0.3144 0.5917, -0.06870, -0.8448 0.5917, -0.02380, -0.4219 0.5917, 0.02120, -0.9375 16 Flap element taps 1.0000, 0.00130, -0.8460 0.9365, 0.01390, -0.8738 0.8333, 0.03280, -0.8643 0.7436, 0.04930, -0.8600 0.7049, 0.05670, -0.9952 0.6667, 0.05450, -0.8901 0.6302, 0.03770, -0.7119 0.6083, 0.01980, -1.0287 0.6000, 0.00000, -1.9286 0.6076, -0.01900, -1.7612 0.6285, -0.03060, 0.6999 0.6667, -0.04090, 0.4518 0.7046, -0.04120, -0.2559 0.7429, -0.03210, -0.0081 0.8333, -0.01400, 0.0062 0.9311, -0.00120, -0.1264 --------- Run Conditions: vel=100.8 ft/s Re=0.963x10^6 AOA=29.99 Flap deflection=0.00 Totals: Cl=0.9355 Cdp=0.6266 Cm(c/4)=-0.1928 Cs=-0.0751 Ch=0.0688 Main component: Cl=0.5875 Cdp=0.4795 Cm=-0.1822 Flap component: Cl=0.3480 Cdp=0.1471 Cm=-0.2915 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.0440 0.5871, 0.07930, -1.0171 0.5501, 0.08690, -1.0119 0.5112, 0.09370, -1.0147 0.4731, 0.09830, -1.0235 0.4349, 0.10070, -1.0160 0.3960, 0.10120, -0.9969 0.3566, 0.10020, -1.0091 0.3172, 0.09790, -1.0076 0.2778, 0.09440, -1.0066 0.2393, 0.08960, -1.0057 0.2056, 0.08360, -0.9928 0.1633, 0.07610, -1.0020 0.1261, 0.06710, -0.9971 0.0900, 0.05640, -0.9971 0.0571, 0.04390, -0.9976 0.0283, 0.02940, -0.9991 0.0142, 0.01970, -1.0005 0.0081, 0.01410, -0.9995 0.0026, 0.00780, -0.9612 0.0000, 0.00000, -1.0278 0.0037, -0.00840, -0.1443 0.0112, -0.01420, 0.5843 0.0191, -0.01930, 0.8254 0.0397, -0.03030, 0.9947 0.0706, -0.04420, 0.9946 0.1037, -0.05710, 0.9226 0.1384, -0.06890, 0.8152 0.1741, -0.07950, 0.7109 0.2102, -0.08660, 0.5909 0.2472, -0.09640, 0.4364 0.2844, -0.10270, 0.3041 0.3225, -0.10690, 0.1521 0.3608, -0.10890, 0.0121 0.3991, -0.10830, -0.1173 0.4373, -0.10510, -0.2000 0.4757, -0.09890, -0.2304 0.5137, -0.09070, -0.2642 0.5514, -0.08120, -0.2469 0.5917, -0.06870, -0.8117 0.5917, -0.02380, -0.3141 0.5917, 0.02120, -1.1220 16 Flap element taps 1.0000, 0.00130, -0.9887 0.9365, 0.01390, -1.0142 0.8333, 0.03280, -1.0227 0.7436, 0.04930, -1.0417 0.7049, 0.05670, -1.2048 0.6667, 0.05450, -1.0816 0.6302, 0.03770, -0.8963 0.6083, 0.01980, -1.2592 0.6000, 0.00000, -2.0605 0.6076, -0.01900, -1.7498 0.6285, -0.03060, 0.7476 0.6667, -0.04090, 0.4748 0.7046, -0.04120, -0.2211 0.7429, -0.03210, 0.0106 0.8333, -0.01400, 0.0049 0.9311, -0.00120, -0.1562 --------- Run Conditions: vel=106.0 ft/s Re=1.004x10^6 AOA=34.98 Flap deflection=0.00 Totals: Cl=1.1019 Cdp=0.8513 Cm(c/4)=-0.2503 Cs=-0.0658 Ch=0.0914 Main component: Cl=0.6987 Cdp=0.6281 Cm=-0.2429 Flap component: Cl=0.4032 Cdp=0.2232 Cm=-0.3550 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.3048 0.5871, 0.07930, -1.2322 0.5501, 0.08690, -1.2287 0.5112, 0.09370, -1.2299 0.4731, 0.09830, -1.2285 0.4349, 0.10070, -1.2283 0.3960, 0.10120, -1.2057 0.3566, 0.10020, -1.2219 0.3172, 0.09790, -1.2134 0.2778, 0.09440, -1.2179 0.2393, 0.08960, -1.2149 0.2056, 0.08360, -1.1950 0.1633, 0.07610, -1.2070 0.1261, 0.06710, -1.1990 0.0900, 0.05640, -1.2015 0.0571, 0.04390, -1.1981 0.0283, 0.02940, -1.1951 0.0142, 0.01970, -1.1974 0.0081, 0.01410, -1.1881 0.0026, 0.00780, -1.1494 0.0000, 0.00000, -1.2113 0.0037, -0.00840, -0.5822 0.0112, -0.01420, 0.3004 0.0191, -0.01930, 0.6401 0.0397, -0.03030, 0.9210 0.0706, -0.04420, 0.9988 0.1037, -0.05710, 0.9873 0.1384, -0.06890, 0.9112 0.1741, -0.07950, 0.8290 0.2102, -0.08660, 0.7350 0.2472, -0.09640, 0.5972 0.2844, -0.10270, 0.4759 0.3225, -0.10690, 0.3307 0.3608, -0.10890, 0.1965 0.3991, -0.10830, 0.0608 0.4373, -0.10510, -0.0311 0.4757, -0.09890, -0.0830 0.5137, -0.09070, -0.1295 0.5514, -0.08120, -0.1338 0.5917, -0.06870, -0.7431 0.5917, -0.02380, -0.2001 0.5917, 0.02120, -1.3785 16 Flap element taps 1.0000, 0.00130, -1.1772 0.9365, 0.01390, -1.1985 0.8333, 0.03280, -1.2081 0.7436, 0.04930, -1.2555 0.7049, 0.05670, -1.4473 0.6667, 0.05450, -1.3135 0.6302, 0.03770, -1.1461 0.6083, 0.01980, -1.5291 0.6000, 0.00000, -2.1705 0.6076, -0.01900, -1.6652 0.6285, -0.03060, 0.7959 0.6667, -0.04090, 0.5081 0.7046, -0.04120, -0.1519 0.7429, -0.03210, 0.0507 0.8333, -0.01400, 0.0178 0.9311, -0.00120, -0.1896 --------- Run Conditions: vel=102.7 ft/s Re=0.970x10^6 AOA=39.95 Flap deflection=0.00 Totals: Cl=1.1808 Cdp=1.0604 Cm(c/4)=-0.2966 Cs=-0.0547 Ch=0.1078 Main component: Cl=0.7502 Cdp=0.7638 Cm=-0.2906 Flap component: Cl=0.4306 Cdp=0.2966 Cm=-0.4025 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.4970 0.5871, 0.07930, -1.3918 0.5501, 0.08690, -1.3757 0.5112, 0.09370, -1.3722 0.4731, 0.09830, -1.3678 0.4349, 0.10070, -1.3709 0.3960, 0.10120, -1.3432 0.3566, 0.10020, -1.3601 0.3172, 0.09790, -1.3494 0.2778, 0.09440, -1.3548 0.2393, 0.08960, -1.3471 0.2056, 0.08360, -1.3225 0.1633, 0.07610, -1.3339 0.1261, 0.06710, -1.3215 0.0900, 0.05640, -1.3248 0.0571, 0.04390, -1.3157 0.0283, 0.02940, -1.3114 0.0142, 0.01970, -1.3103 0.0081, 0.01410, -1.2989 0.0026, 0.00780, -1.2608 0.0000, 0.00000, -1.3217 0.0037, -0.00840, -0.9418 0.0112, -0.01420, 0.0168 0.0191, -0.01930, 0.4317 0.0397, -0.03030, 0.8169 0.0706, -0.04420, 0.9742 0.1037, -0.05710, 1.0097 0.1384, -0.06890, 0.9683 0.1741, -0.07950, 0.9167 0.2102, -0.08660, 0.8481 0.2472, -0.09640, 0.7325 0.2844, -0.10270, 0.6271 0.3225, -0.10690, 0.4928 0.3608, -0.10890, 0.3673 0.3991, -0.10830, 0.2320 0.4373, -0.10510, 0.1355 0.4757, -0.09890, 0.0691 0.5137, -0.09070, 0.0098 0.5514, -0.08120, -0.0142 0.5917, -0.06870, -0.6348 0.5917, -0.02380, -0.1312 0.5917, 0.02120, -1.5076 16 Flap element taps 1.0000, 0.00130, -1.2880 0.9365, 0.01390, -1.3219 0.8333, 0.03280, -1.3209 0.7436, 0.04930, -1.3678 0.7049, 0.05670, -1.5677 0.6667, 0.05450, -1.4747 0.6302, 0.03770, -1.3566 0.6083, 0.01980, -1.6912 0.6000, 0.00000, -2.1851 0.6076, -0.01900, -1.5153 0.6285, -0.03060, 0.8341 0.6667, -0.04090, 0.5501 0.7046, -0.04120, -0.0704 0.7429, -0.03210, 0.1070 0.8333, -0.01400, 0.0512 0.9311, -0.00120, -0.1875 --------- Run Conditions: vel=99.3 ft/s Re=0.938x10^6 AOA=44.97 Flap deflection=0.00 Totals: Cl=1.2099 Cdp=1.2675 Cm(c/4)=-0.3411 Cs=-0.0416 Ch=0.1202 Main component: Cl=0.7667 Cdp=0.8923 Cm=-0.3317 Flap component: Cl=0.4432 Cdp=0.3752 Cm=-0.4474 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.6218 0.5871, 0.07930, -1.5351 0.5501, 0.08690, -1.5121 0.5112, 0.09370, -1.5014 0.4731, 0.09830, -1.4912 0.4349, 0.10070, -1.4886 0.3960, 0.10120, -1.4559 0.3566, 0.10020, -1.4773 0.3172, 0.09790, -1.4654 0.2778, 0.09440, -1.4675 0.2393, 0.08960, -1.4578 0.2056, 0.08360, -1.4237 0.1633, 0.07610, -1.4394 0.1261, 0.06710, -1.4214 0.0900, 0.05640, -1.4217 0.0571, 0.04390, -1.4081 0.0283, 0.02940, -1.4007 0.0142, 0.01970, -1.4002 0.0081, 0.01410, -1.3854 0.0026, 0.00780, -1.3481 0.0000, 0.00000, -1.4103 0.0037, -0.00840, -1.2492 0.0112, -0.01420, -0.2662 0.0191, -0.01930, 0.2065 0.0397, -0.03030, 0.6810 0.0706, -0.04420, 0.9115 0.1037, -0.05710, 0.9972 0.1384, -0.06890, 0.9888 0.1741, -0.07950, 0.9681 0.2102, -0.08660, 0.9295 0.2472, -0.09640, 0.8352 0.2844, -0.10270, 0.7507 0.3225, -0.10690, 0.6290 0.3608, -0.10890, 0.5185 0.3991, -0.10830, 0.3857 0.4373, -0.10510, 0.2892 0.4757, -0.09890, 0.2133 0.5137, -0.09070, 0.1413 0.5514, -0.08120, 0.1000 0.5917, -0.06870, -0.5302 0.5917, -0.02380, -0.0406 0.5917, 0.02120, -1.6123 16 Flap element taps 1.0000, 0.00130, -1.3871 0.9365, 0.01390, -1.4324 0.8333, 0.03280, -1.4470 0.7436, 0.04930, -1.4599 0.7049, 0.05670, -1.6570 0.6667, 0.05450, -1.5935 0.6302, 0.03770, -1.5492 0.6083, 0.01980, -1.7808 0.6000, 0.00000, -2.1777 0.6076, -0.01900, -1.3485 0.6285, -0.03060, 0.8626 0.6667, -0.04090, 0.5922 0.7046, -0.04120, 0.0161 0.7429, -0.03210, 0.1659 0.8333, -0.01400, 0.0874 0.9311, -0.00120, -0.1762 --------- Run Conditions: vel=111.0 ft/s Re=1.007x10^6 AOA=60.02 Flap deflection=0.00 Totals: Cl=1.1080 Cdp=1.8813 Cm(c/4)=-0.4743 Cs=0.0197 Ch=0.1538 Main component: Cl=0.6905 Cdp=1.2502 Cm=-0.4359 Flap component: Cl=0.4175 Cdp=0.6311 Cm=-0.5842 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.9482 0.5871, 0.07930, -1.8324 0.5501, 0.08690, -1.8133 0.5112, 0.09370, -1.8035 0.4731, 0.09830, -1.8130 0.4349, 0.10070, -1.8206 0.3960, 0.10120, -1.8265 0.3566, 0.10020, -1.8069 0.3172, 0.09790, -1.7980 0.2778, 0.09440, -1.7860 0.2393, 0.08960, -1.7708 0.2056, 0.08360, -1.7663 0.1633, 0.07610, -1.7385 0.1261, 0.06710, -1.7214 0.0900, 0.05640, -1.6973 0.0571, 0.04390, -1.6792 0.0283, 0.02940, -1.6637 0.0142, 0.01970, -1.6553 0.0081, 0.01410, -1.6613 0.0026, 0.00780, -1.5814 0.0000, 0.00000, -1.6434 0.0037, -0.00840, -1.8095 0.0112, -0.01420, -1.0663 0.0191, -0.01930, -0.5076 0.0397, -0.03030, 0.1571 0.0706, -0.04420, 0.5601 0.1037, -0.05710, 0.7735 0.1384, -0.06890, 0.9064 0.1741, -0.07950, 0.9720 0.2102, -0.08660, 0.9883 0.2472, -0.09640, 0.9984 0.2844, -0.10270, 0.9681 0.3225, -0.10690, 0.9383 0.3608, -0.10890, 0.8564 0.3991, -0.10830, 0.7860 0.4373, -0.10510, 0.6980 0.4757, -0.09890, 0.6171 0.5137, -0.09070, 0.5414 0.5514, -0.08120, 0.4681 0.5917, -0.06870, -0.1548 0.5917, -0.02380, 0.2461 0.5917, 0.02120, -1.8414 16 Flap element taps 1.0000, 0.00130, -1.6486 0.9365, 0.01390, -1.7203 0.8333, 0.03280, -1.7314 0.7436, 0.04930, -1.7613 0.7049, 0.05670, -1.9853 0.6667, 0.05450, -1.8795 0.6302, 0.03770, -1.9721 0.6083, 0.01980, -1.9927 0.6000, 0.00000, -2.2963 0.6076, -0.01900, -0.7925 0.6285, -0.03060, 0.9206 0.6667, -0.04090, 0.7384 0.7046, -0.04120, 0.3312 0.7429, -0.03210, 0.3930 0.8333, -0.01400, 0.2678 0.9311, -0.00120, -0.0700 --------- Run Conditions: vel=107.7 ft/s Re=0.974x10^6 AOA=70.02 Flap deflection=0.00 Totals: Cl=0.8686 Cdp=2.1945 Cm(c/4)=-0.5519 Cs=0.0665 Ch=0.1708 Main component: Cl=0.5301 Cdp=1.4017 Cm=-0.4752 Flap component: Cl=0.3386 Cdp=0.7928 Cm=-0.6665 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -2.0319 0.5871, 0.07930, -1.9322 0.5501, 0.08690, -1.9280 0.5112, 0.09370, -1.9242 0.4731, 0.09830, -1.9233 0.4349, 0.10070, -1.9335 0.3960, 0.10120, -1.9522 0.3566, 0.10020, -1.9400 0.3172, 0.09790, -1.9492 0.2778, 0.09440, -1.9442 0.2393, 0.08960, -1.9171 0.2056, 0.08360, -1.9036 0.1633, 0.07610, -1.8612 0.1261, 0.06710, -1.8398 0.0900, 0.05640, -1.8059 0.0571, 0.04390, -1.7857 0.0283, 0.02940, -1.7706 0.0142, 0.01970, -1.7552 0.0081, 0.01410, -1.7592 0.0026, 0.00780, -1.6687 0.0000, 0.00000, -1.7333 0.0037, -0.00840, -1.8886 0.0112, -0.01420, -1.4745 0.0191, -0.01930, -0.9428 0.0397, -0.03030, -0.2345 0.0706, -0.04420, 0.2394 0.1037, -0.05710, 0.5159 0.1384, -0.06890, 0.7139 0.1741, -0.07950, 0.8360 0.2102, -0.08660, 0.9050 0.2472, -0.09640, 0.9696 0.2844, -0.10270, 0.9897 0.3225, -0.10690, 1.0110 0.3608, -0.10890, 0.9741 0.3991, -0.10830, 0.9454 0.4373, -0.10510, 0.8885 0.4757, -0.09890, 0.8231 0.5137, -0.09070, 0.7640 0.5514, -0.08120, 0.6868 0.5917, -0.06870, 0.1144 0.5917, -0.02380, 0.3687 0.5917, 0.02120, -1.9162 16 Flap element taps 1.0000, 0.00130, -1.6923 0.9365, 0.01390, -1.8185 0.8333, 0.03280, -1.8799 0.7436, 0.04930, -1.9108 0.7049, 0.05670, -2.1899 0.6667, 0.05450, -1.9972 0.6302, 0.03770, -2.1221 0.6083, 0.01980, -2.0889 0.6000, 0.00000, -2.4037 0.6076, -0.01900, -0.4162 0.6285, -0.03060, 0.9439 0.6667, -0.04090, 0.8424 0.7046, -0.04120, 0.5564 0.7429, -0.03210, 0.5648 0.8333, -0.01400, 0.4236 0.9311, -0.00120, 0.0626 --------- Run Conditions: vel=105.3 ft/s Re=0.953x10^6 AOA=80.02 Flap deflection=0.00 Totals: Cl=0.5326 Cdp=2.3636 Cm(c/4)=-0.6052 Cs=0.1149 Ch=0.1778 Main component: Cl=0.3234 Cdp=1.4537 Cm=-0.4872 Flap component: Cl=0.2091 Cdp=0.9099 Cm=-0.7230 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -2.0291 0.5871, 0.07930, -1.9350 0.5501, 0.08690, -1.9384 0.5112, 0.09370, -1.9521 0.4731, 0.09830, -1.9677 0.4349, 0.10070, -1.9689 0.3960, 0.10120, -1.9866 0.3566, 0.10020, -1.9809 0.3172, 0.09790, -1.9836 0.2778, 0.09440, -1.9922 0.2393, 0.08960, -1.9735 0.2056, 0.08360, -1.9664 0.1633, 0.07610, -1.9278 0.1261, 0.06710, -1.9038 0.0900, 0.05640, -1.8737 0.0571, 0.04390, -1.8501 0.0283, 0.02940, -1.8474 0.0142, 0.01970, -1.8319 0.0081, 0.01410, -1.8311 0.0026, 0.00780, -1.7377 0.0000, 0.00000, -1.8086 0.0037, -0.00840, -1.8445 0.0112, -0.01420, -1.7711 0.0191, -0.01930, -1.3194 0.0397, -0.03030, -0.6233 0.0706, -0.04420, -0.1128 0.1037, -0.05710, 0.2080 0.1384, -0.06890, 0.4520 0.1741, -0.07950, 0.6202 0.2102, -0.08660, 0.7379 0.2472, -0.09640, 0.8472 0.2844, -0.10270, 0.9173 0.3225, -0.10690, 0.9860 0.3608, -0.10890, 0.9989 0.3991, -0.10830, 1.0152 0.4373, -0.10510, 0.9989 0.4757, -0.09890, 0.9635 0.5137, -0.09070, 0.9280 0.5514, -0.08120, 0.8662 0.5917, -0.06870, 0.3812 0.5917, -0.02380, 0.4109 0.5917, 0.02120, -1.8987 16 Flap element taps 1.0000, 0.00130, -1.6827 0.9365, 0.01390, -1.8468 0.8333, 0.03280, -1.9167 0.7436, 0.04930, -1.9717 0.7049, 0.05670, -2.2778 0.6667, 0.05450, -2.0106 0.6302, 0.03770, -2.1643 0.6083, 0.01980, -2.1005 0.6000, 0.00000, -2.4292 0.6076, -0.01900, -0.0951 0.6285, -0.03060, 0.9622 0.6667, -0.04090, 0.9364 0.7046, -0.04120, 0.7583 0.7429, -0.03210, 0.7327 0.8333, -0.01400, 0.5896 0.9311, -0.00120, 0.2261 --------- Run Conditions: vel=104.7 ft/s Re=0.946x10^6 AOA=90.02 Flap deflection=0.00 Totals: Cl=0.1485 Cdp=2.4851 Cm(c/4)=-0.6616 Cs=0.1494 Ch=0.1841 Main component: Cl=0.0933 Cdp=1.4795 Cm=-0.5018 Flap component: Cl=0.0552 Cdp=1.0056 Cm=-0.7811 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -2.1472 0.5871, 0.07930, -2.0762 0.5501, 0.08690, -2.0888 0.5112, 0.09370, -2.1117 0.4731, 0.09830, -2.1317 0.4349, 0.10070, -2.1458 0.3960, 0.10120, -2.1502 0.3566, 0.10020, -2.1240 0.3172, 0.09790, -2.1232 0.2778, 0.09440, -2.1193 0.2393, 0.08960, -2.1047 0.2056, 0.08360, -2.0923 0.1633, 0.07610, -2.0490 0.1261, 0.06710, -2.0025 0.0900, 0.05640, -1.9493 0.0571, 0.04390, -1.8976 0.0283, 0.02940, -1.8735 0.0142, 0.01970, -1.8647 0.0081, 0.01410, -1.8652 0.0026, 0.00780, -1.7651 0.0000, 0.00000, -1.8326 0.0037, -0.00840, -1.8400 0.0112, -0.01420, -1.9282 0.0191, -0.01930, -1.5947 0.0397, -0.03030, -0.9715 0.0706, -0.04420, -0.4706 0.1037, -0.05710, -0.1400 0.1384, -0.06890, 0.1264 0.1741, -0.07950, 0.3237 0.2102, -0.08660, 0.4765 0.2472, -0.09640, 0.6197 0.2844, -0.10270, 0.7329 0.3225, -0.10690, 0.8408 0.3608, -0.10890, 0.9034 0.3991, -0.10830, 0.9680 0.4373, -0.10510, 0.9974 0.4757, -0.09890, 1.0009 0.5137, -0.09070, 1.0021 0.5514, -0.08120, 0.9682 0.5917, -0.06870, 0.5955 0.5917, -0.02380, 0.3028 0.5917, 0.02120, -1.9874 16 Flap element taps 1.0000, 0.00130, -1.6432 0.9365, 0.01390, -1.8685 0.8333, 0.03280, -2.0081 0.7436, 0.04930, -2.0499 0.7049, 0.05670, -2.3884 0.6667, 0.05450, -2.0731 0.6302, 0.03770, -2.3000 0.6083, 0.01980, -2.1984 0.6000, 0.00000, -2.5326 0.6076, -0.01900, 0.0613 0.6285, -0.03060, 0.9508 0.6667, -0.04090, 0.9903 0.7046, -0.04120, 0.9050 0.7429, -0.03210, 0.8611 0.8333, -0.01400, 0.7341 0.9311, -0.00120, 0.3940 --------- Run Conditions: vel=113.2 ft/s Re=1.023x10^6 AOA=119.99 Flap deflection=0.00 Totals: Cl=-0.7125 Cdp=1.7465 Cm(c/4)=-0.6197 Cs=0.2558 Ch=0.1571 Main component: Cl=-0.3213 Cdp=0.8697 Cm=-0.3418 Flap component: Cl=-0.3913 Cdp=0.8769 Cm=-0.7451 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -1.8835 0.5871, 0.07930, -1.7628 0.5501, 0.08690, -1.7696 0.5112, 0.09370, -1.7937 0.4731, 0.09830, -1.7756 0.4349, 0.10070, -1.7627 0.3960, 0.10120, -1.7419 0.3566, 0.10020, -1.7198 0.3172, 0.09790, -1.7130 0.2778, 0.09440, -1.7153 0.2393, 0.08960, -1.7059 0.2056, 0.08360, -1.7094 0.1633, 0.07610, -1.7117 0.1261, 0.06710, -1.7225 0.0900, 0.05640, -1.7309 0.0571, 0.04390, -1.7006 0.0283, 0.02940, -1.6603 0.0142, 0.01970, -1.6378 0.0081, 0.01410, -1.6354 0.0026, 0.00780, -1.5539 0.0000, 0.00000, -1.6087 0.0037, -0.00840, -1.6011 0.0112, -0.01420, -1.6254 0.0191, -0.01930, -1.6902 0.0397, -0.03030, -1.5074 0.0706, -0.04420, -1.2291 0.1037, -0.05710, -1.0097 0.1384, -0.06890, -0.8096 0.1741, -0.07950, -0.6356 0.2102, -0.08660, -0.4778 0.2472, -0.09640, -0.3329 0.2844, -0.10270, -0.1697 0.3225, -0.10690, -0.0115 0.3608, -0.10890, 0.1359 0.3991, -0.10830, 0.3048 0.4373, -0.10510, 0.4704 0.4757, -0.09890, 0.6235 0.5137, -0.09070, 0.7520 0.5514, -0.08120, 0.8512 0.5917, -0.06870, 0.9949 0.5917, -0.02380, 0.2366 0.5917, 0.02120, -1.8156 16 Flap element taps 1.0000, 0.00130, -1.4260 0.9365, 0.01390, -1.4943 0.8333, 0.03280, -1.6092 0.7436, 0.04930, -1.7145 0.7049, 0.05670, -1.9333 0.6667, 0.05450, -1.8146 0.6302, 0.03770, -2.2443 0.6083, 0.01980, -2.6317 0.6000, 0.00000, -2.9119 0.6076, -0.01900, 0.0215 0.6285, -0.03060, 0.8047 0.6667, -0.04090, 0.8808 0.7046, -0.04120, 0.9106 0.7429, -0.03210, 0.9761 0.8333, -0.01400, 0.9938 0.9311, -0.00120, 0.8640 --------- Run Conditions: vel=109.6 ft/s Re=0.989x10^6 AOA=150.04 Flap deflection=0.00 Totals: Cl=-0.4376 Cdp=0.4989 Cm(c/4)=-0.3468 Cs=0.2137 Ch=0.0520 Main component: Cl=0.0192 Cdp=0.1831 Cm=-0.0660 Flap component: Cl=-0.4567 Cdp=0.3158 Cm=-0.4379 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.9795 0.5871, 0.07930, -0.9207 0.5501, 0.08690, -0.9186 0.5112, 0.09370, -0.9239 0.4731, 0.09830, -0.9309 0.4349, 0.10070, -0.9339 0.3960, 0.10120, -0.8964 0.3566, 0.10020, -0.9266 0.3172, 0.09790, -0.9263 0.2778, 0.09440, -0.9242 0.2393, 0.08960, -0.9217 0.2056, 0.08360, -0.8945 0.1633, 0.07610, -0.9249 0.1261, 0.06710, -0.9127 0.0900, 0.05640, -0.9164 0.0571, 0.04390, -0.9005 0.0283, 0.02940, -0.9021 0.0142, 0.01970, -0.8933 0.0081, 0.01410, -0.8716 0.0026, 0.00780, -0.8483 0.0000, 0.00000, -0.8947 0.0037, -0.00840, -0.9581 0.0112, -0.01420, -1.2562 0.0191, -0.01930, -1.3705 0.0397, -0.03030, -1.3959 0.0706, -0.04420, -1.3198 0.1037, -0.05710, -1.2838 0.1384, -0.06890, -1.2638 0.1741, -0.07950, -1.2084 0.2102, -0.08660, -1.1310 0.2472, -0.09640, -1.1251 0.2844, -0.10270, -1.0268 0.3225, -0.10690, -0.9568 0.3608, -0.10890, -0.8380 0.3991, -0.10830, -0.6972 0.4373, -0.10510, -0.4799 0.4757, -0.09890, -0.2351 0.5137, -0.09070, -0.0158 0.5514, -0.08120, 0.2161 0.5917, -0.06870, 0.7094 0.5917, -0.02380, 0.4968 0.5917, 0.02120, -0.8854 16 Flap element taps 1.0000, 0.00130, -0.5831 0.9365, 0.01390, -0.6498 0.8333, 0.03280, -0.8588 0.7436, 0.04930, -0.9045 0.7049, 0.05670, -1.0906 0.6667, 0.05450, -0.9385 0.6302, 0.03770, -1.0575 0.6083, 0.01980, -1.0532 0.6000, 0.00000, -1.4297 0.6076, -0.01900, 0.3544 0.6285, -0.03060, 0.6024 0.6667, -0.04090, 0.3823 0.7046, -0.04120, 0.2197 0.7429, -0.03210, 0.5905 0.8333, -0.01400, 0.7696 0.9311, -0.00120, 0.9536 --------- Run Conditions: vel=118.8 ft/s Re=1.072x10^6 AOA=180.05 Flap deflection=0.00 Totals: Cl=0.0698 Cdp=0.0215 Cm(c/4)=0.0224 Cs=0.0214 Ch=-0.0044 Main component: Cl=0.0270 Cdp=0.0092 Cm=0.0062 Flap component: Cl=0.0428 Cdp=0.0123 Cm=0.0337 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, -0.5374 0.5871, 0.07930, -0.4748 0.5501, 0.08690, -0.4405 0.5112, 0.09370, -0.5393 0.4731, 0.09830, -0.6274 0.4349, 0.10070, -0.6346 0.3960, 0.10120, -0.5690 0.3566, 0.10020, -0.5721 0.3172, 0.09790, -0.5325 0.2778, 0.09440, -0.5023 0.2393, 0.08960, -0.4599 0.2056, 0.08360, -0.3782 0.1633, 0.07610, -0.3343 0.1261, 0.06710, -0.2193 0.0900, 0.05640, -0.1139 0.0571, 0.04390, -0.0138 0.0283, 0.02940, 0.0097 0.0142, 0.01970, 0.0129 0.0081, 0.01410, 0.0323 0.0026, 0.00780, 0.0191 0.0000, 0.00000, 0.0105 0.0037, -0.00840, 0.0101 0.0112, -0.01420, 0.0158 0.0191, -0.01930, 0.0165 0.0397, -0.03030, -0.0006 0.0706, -0.04420, -0.0038 0.1037, -0.05710, -0.0596 0.1384, -0.06890, -0.2073 0.1741, -0.07950, -0.3489 0.2102, -0.08660, -0.4623 0.2472, -0.09640, -0.6280 0.2844, -0.10270, -0.7177 0.3225, -0.10690, -0.8292 0.3608, -0.10890, -0.8792 0.3991, -0.10830, -0.8984 0.4373, -0.10510, -0.8186 0.4757, -0.09890, -0.6738 0.5137, -0.09070, -0.5348 0.5514, -0.08120, -0.3653 0.5917, -0.06870, 0.3598 0.5917, -0.02380, 0.2194 0.5917, 0.02120, 0.0155 16 Flap element taps 1.0000, 0.00130, 0.9958 0.9365, 0.01390, 0.2486 0.8333, 0.03280, 0.1199 0.7436, 0.04930, 0.0861 0.7049, 0.05670, 0.1284 0.6667, 0.05450, 0.1127 0.6302, 0.03770, 0.0303 0.6083, 0.01980, -0.0191 0.6000, 0.00000, -0.2468 0.6076, -0.01900, 0.2380 0.6285, -0.03060, 0.1395 0.6667, -0.04090, 0.0439 0.7046, -0.04120, -0.5075 0.7429, -0.03210, -0.0447 0.8333, -0.01400, 0.0912 0.9311, -0.00120, 0.0770 --------- Run Conditions: vel=110.0 ft/s Re=0.992x10^6 AOA=210.06 Flap deflection=0.00 Totals: Cl=0.4890 Cdp=0.5209 Cm(c/4)=0.3651 Cs=0.2059 Ch=-0.0209 Main component: Cl=0.0106 Cdp=0.2061 Cm=0.0792 Flap component: Cl=0.4785 Cdp=0.3148 Cm=0.4569 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.9927 0.5871, 0.07930, 0.3684 0.5501, 0.08690, 0.1907 0.5112, 0.09370, -0.0185 0.4731, 0.09830, -0.2192 0.4349, 0.10070, -0.3436 0.3960, 0.10120, -0.3945 0.3566, 0.10020, -0.5326 0.3172, 0.09790, -0.6208 0.2778, 0.09440, -0.7500 0.2393, 0.08960, -0.8722 0.2056, 0.08360, -0.9816 0.1633, 0.07610, -1.1545 0.1261, 0.06710, -1.2720 0.0900, 0.05640, -1.4379 0.0571, 0.04390, -1.5704 0.0283, 0.02940, -1.5422 0.0142, 0.01970, -1.2044 0.0081, 0.01410, -0.9349 0.0026, 0.00780, -0.8065 0.0000, 0.00000, -0.8493 0.0037, -0.00840, -0.8479 0.0112, -0.01420, -0.8396 0.0191, -0.01930, -0.8394 0.0397, -0.03030, -0.8601 0.0706, -0.04420, -0.8464 0.1037, -0.05710, -0.8526 0.1384, -0.06890, -0.8971 0.1741, -0.07950, -0.8990 0.2102, -0.08660, -0.8758 0.2472, -0.09640, -0.9132 0.2844, -0.10270, -0.8982 0.3225, -0.10690, -0.9163 0.3608, -0.10890, -0.9054 0.3991, -0.10830, -0.9175 0.4373, -0.10510, -0.8916 0.4757, -0.09890, -0.8869 0.5137, -0.09070, -0.8797 0.5514, -0.08120, -0.8681 0.5917, -0.06870, -0.9278 0.5917, -0.02380, -0.9575 0.5917, 0.02120, 0.5722 16 Flap element taps 1.0000, 0.00130, -0.8922 0.9365, 0.01390, 0.9579 0.8333, 0.03280, 0.7569 0.7436, 0.04930, 0.5641 0.7049, 0.05670, 0.3729 0.6667, 0.05450, 0.2867 0.6302, 0.03770, 0.4828 0.6083, 0.01980, 0.2413 0.6000, 0.00000, -1.3492 0.6076, -0.01900, -0.9888 0.6285, -0.03060, -0.9568 0.6667, -0.04090, -0.9762 0.7046, -0.04120, -0.9988 0.7429, -0.03210, -0.9305 0.8333, -0.01400, -0.9129 0.9311, -0.00120, -0.8954 --------- Run Conditions: vel=113.5 ft/s Re=1.017x10^6 AOA=240.01 Flap deflection=0.00 Totals: Cl=0.7752 Cdp=1.7719 Cm(c/4)=0.6333 Cs=0.2142 Ch=-0.1085 Main component: Cl=0.3246 Cdp=0.9202 Cm=0.3559 Flap component: Cl=0.4507 Cdp=0.8518 Cm=0.7580 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.8618 0.5871, 0.07930, 0.9271 0.5501, 0.08690, 0.8528 0.5112, 0.09370, 0.7551 0.4731, 0.09830, 0.6384 0.4349, 0.10070, 0.5301 0.3960, 0.10120, 0.4242 0.3566, 0.10020, 0.3065 0.3172, 0.09790, 0.1777 0.2778, 0.09440, 0.0219 0.2393, 0.08960, -0.1537 0.2056, 0.08360, -0.3574 0.1633, 0.07610, -0.5819 0.1261, 0.06710, -0.8254 0.0900, 0.05640, -1.1416 0.0571, 0.04390, -1.5166 0.0283, 0.02940, -1.7276 0.0142, 0.01970, -1.6269 0.0081, 0.01410, -1.6201 0.0026, 0.00780, -1.5520 0.0000, 0.00000, -1.6344 0.0037, -0.00840, -1.6395 0.0112, -0.01420, -1.6518 0.0191, -0.01930, -1.6625 0.0397, -0.03030, -1.7075 0.0706, -0.04420, -1.7589 0.1037, -0.05710, -1.7891 0.1384, -0.06890, -1.7874 0.1741, -0.07950, -1.7604 0.2102, -0.08660, -1.7406 0.2472, -0.09640, -1.7130 0.2844, -0.10270, -1.6951 0.3225, -0.10690, -1.6830 0.3608, -0.10890, -1.6938 0.3991, -0.10830, -1.7089 0.4373, -0.10510, -1.7279 0.4757, -0.09890, -1.7242 0.5137, -0.09070, -1.7251 0.5514, -0.08120, -1.6758 0.5917, -0.06870, -1.7093 0.5917, -0.02380, -1.7861 0.5917, 0.02120, 0.4749 16 Flap element taps 1.0000, 0.00130, -1.6294 0.9365, 0.01390, 0.7690 0.8333, 0.03280, 0.9866 0.7436, 0.04930, 0.9848 0.7049, 0.05670, 0.9329 0.6667, 0.05450, 0.8489 0.6302, 0.03770, 0.5730 0.6083, 0.01980, 0.0961 0.6000, 0.00000, -2.0591 0.6076, -0.01900, -1.8310 0.6285, -0.03060, -1.8250 0.6667, -0.04090, -1.8644 0.7046, -0.04120, -1.9071 0.7429, -0.03210, -1.8541 0.8333, -0.01400, -1.7868 0.9311, -0.00120, -1.6796 --------- Run Conditions: vel=106.2 ft/s Re=0.948x10^6 AOA=269.02 Flap deflection=0.00 Totals: Cl=-0.0964 Cdp=2.3240 Cm(c/4)=0.6193 Cs=0.1362 Ch=-0.1523 Main component: Cl=-0.0732 Cdp=1.4030 Cm=0.4831 Flap component: Cl=-0.0232 Cdp=0.9210 Cm=0.7167 Surface Pressure Data 42 Main element taps 0.6220, 0.06610, 0.1049 0.5871, 0.07930, 0.9264 0.5501, 0.08690, 0.9754 0.5112, 0.09370, 0.9959 0.4731, 0.09830, 0.9949 0.4349, 0.10070, 0.9822 0.3960, 0.10120, 0.9531 0.3566, 0.10020, 0.9115 0.3172, 0.09790, 0.8427 0.2778, 0.09440, 0.7547 0.2393, 0.08960, 0.6390 0.2056, 0.08360, 0.4851 0.1633, 0.07610, 0.2891 0.1261, 0.06710, 0.0439 0.0900, 0.05640, -0.3119 0.0571, 0.04390, -0.8417 0.0283, 0.02940, -1.5274 0.0142, 0.01970, -1.9362 0.0081, 0.01410, -1.8747 0.0026, 0.00780, -1.6958 0.0000, 0.00000, -1.7790 0.0037, -0.00840, -1.7822 0.0112, -0.01420, -1.7929 0.0191, -0.01930, -1.7980 0.0397, -0.03030, -1.8089 0.0706, -0.04420, -1.8375 0.1037, -0.05710, -1.8680 0.1384, -0.06890, -1.9013 0.1741, -0.07950, -1.9319 0.2102, -0.08660, -1.9556 0.2472, -0.09640, -1.9693 0.2844, -0.10270, -1.9768 0.3225, -0.10690, -1.9646 0.3608, -0.10890, -1.9525 0.3991, -0.10830, -1.9410 0.4373, -0.10510, -1.9202 0.4757, -0.09890, -1.9215 0.5137, -0.09070, -1.9726 0.5514, -0.08120, -2.0143 0.5917, -0.06870, -1.9819 0.5917, -0.02380, -2.0165 0.5917, 0.02120, 0.3544 16 Flap element taps 1.0000, 0.00130, -1.7719 0.9365, 0.01390, 0.1638 0.8333, 0.03280, 0.6562 0.7436, 0.04930, 0.8512 0.7049, 0.05670, 0.9242 0.6667, 0.05450, 0.9975 0.6302, 0.03770, 0.2473 0.6083, 0.01980, -0.3162 0.6000, 0.00000, -2.3701 0.6076, -0.01900, -2.1175 0.6285, -0.03060, -2.0955 0.6667, -0.04090, -2.1293 0.7046, -0.04120, -2.1090 0.7429, -0.03210, -1.9776 0.8333, -0.01400, -1.8836 0.9311, -0.00120, -1.8203