S809 UNVENTED AILERON, CLEAN, CHORD = 18 IN --------- Run Conditions: vel=108.8 ft/s Re=1.000x10^6 AOA=-6.04 Flap deflection=0.00 Totals: Cl=-0.5687 Cdp=0.0119 Cm(c/4)=-0.0167 Cs=0.0480 Ch=-0.0086 Main component: Cl=-0.5698 Cdp=0.0300 Cm=0.1293 Flap component: Cl=0.0011 Cdp=-0.0181 Cm=-0.0043 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.2186 0.6175, -0.04610, -0.1205 0.5775, -0.01750, -0.0611 0.6274, 0.07170, -0.0668 0.5694, 0.08320, -0.2799 0.5112, 0.09090, -0.3421 0.4731, 0.09830, -0.4085 0.4349, 0.10070, -0.4052 0.3960, 0.10120, -0.3492 0.3566, 0.10020, -0.2772 0.3172, 0.09790, -0.2084 0.2778, 0.09440, -0.1552 0.2393, 0.08960, -0.0991 0.2056, 0.08360, -0.0392 0.1633, 0.07610, 0.0855 0.1261, 0.06710, 0.1967 0.0900, 0.05640, 0.3659 0.0571, 0.04390, 0.5739 0.0283, 0.02940, 0.8337 0.0142, 0.01970, 0.9908 0.0081, 0.01410, 0.9865 0.0026, 0.00780, 0.7016 0.0000, 0.00000, -0.6012 0.0037, -0.00840, -1.6444 0.0112, -0.01420, -1.3672 0.0191, -0.01930, -1.1731 0.0397, -0.03030, -0.9380 0.0706, -0.04420, -0.9024 0.1037, -0.05710, -0.9450 0.1384, -0.06890, -0.9774 0.1741, -0.07950, -1.0403 0.2102, -0.08660, -1.1345 0.2472, -0.09640, -1.2100 0.2844, -0.10270, -1.2544 0.3225, -0.10690, -1.2704 0.3608, -0.10890, -1.2762 0.3991, -0.10830, -1.2181 0.4373, -0.10510, -1.1274 0.4757, -0.09890, -1.0109 0.5137, -0.09070, -0.6652 0.5694, -0.07640, -0.3935 0.5777, -0.04660, -0.0737 15 Flap element taps 1.0000, 0.00130, 0.1906 0.9365, 0.01390, 0.1214 0.8333, 0.03280, 0.0541 0.7436, 0.04930, 0.0153 0.7049, 0.05670, 0.0268 0.6662, 0.06410, -0.0880 0.6522, 0.01390, -0.0843 0.5969, -0.00020, -0.1302 0.6000, -0.03020, -0.1189 0.6324, -0.04540, -0.1235 0.6667, -0.04880, -0.1370 0.7046, -0.04110, -0.0823 0.7429, -0.03210, -0.0141 0.8333, -0.01400, 0.0973 0.9311, -0.00120, 0.2066 Wake drag found for this condition, Cdw=0.0175 --------- Run Conditions: vel=109.6 ft/s Re=1.005x10^6 AOA=0.05 Flap deflection=0.00 Totals: Cl=0.0766 Cdp=0.0105 Cm(c/4)=-0.0313 Cs=-0.0104 Ch=-0.0583 Main component: Cl=0.0122 Cdp=0.0315 Cm=0.0021 Flap component: Cl=0.0644 Cdp=-0.0210 Cm=-0.0525 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.1303 0.6175, -0.04610, -0.0853 0.5775, -0.01750, -0.0856 0.6274, 0.07170, -0.1813 0.5694, 0.08320, -0.4315 0.5112, 0.09090, -0.6184 0.4731, 0.09830, -0.6726 0.4349, 0.10070, -0.7208 0.3960, 0.10120, -0.7182 0.3566, 0.10020, -0.6548 0.3172, 0.09790, -0.6144 0.2778, 0.09440, -0.5926 0.2393, 0.08960, -0.5780 0.2056, 0.08360, -0.5821 0.1633, 0.07610, -0.4787 0.1261, 0.06710, -0.4321 0.0900, 0.05640, -0.3187 0.0571, 0.04390, -0.1933 0.0283, 0.02940, 0.0174 0.0142, 0.01970, 0.2673 0.0081, 0.01410, 0.4135 0.0026, 0.00780, 0.7343 0.0000, 0.00000, 1.0223 0.0037, -0.00840, 0.6979 0.0112, -0.01420, 0.4447 0.0191, -0.01930, 0.3304 0.0397, -0.03030, 0.1763 0.0706, -0.04420, -0.0199 0.1037, -0.05710, -0.1734 0.1384, -0.06890, -0.2648 0.1741, -0.07950, -0.3904 0.2102, -0.08660, -0.5503 0.2472, -0.09640, -0.6533 0.2844, -0.10270, -0.7542 0.3225, -0.10690, -0.7959 0.3608, -0.10890, -0.8604 0.3991, -0.10830, -0.8418 0.4373, -0.10510, -0.7924 0.4757, -0.09890, -0.7256 0.5137, -0.09070, -0.7277 0.5694, -0.07640, -0.2389 0.5777, -0.04660, -0.0915 15 Flap element taps 1.0000, 0.00130, 0.1958 0.9365, 0.01390, 0.0977 0.8333, 0.03280, -0.0153 0.7436, 0.04930, -0.0922 0.7049, 0.05670, -0.1063 0.6662, 0.06410, -0.2454 0.6522, 0.01390, -0.0831 0.5969, -0.00020, -0.0813 0.6000, -0.03020, -0.0804 0.6324, -0.04540, -0.0894 0.6667, -0.04880, -0.0690 0.7046, -0.04110, 0.0857 0.7429, -0.03210, 0.1283 0.8333, -0.01400, 0.2141 0.9311, -0.00120, 0.2904 Wake drag found for this condition, Cdw=0.0089 --------- Run Conditions: vel=109.7 ft/s Re=1.005x10^6 AOA=3.08 Flap deflection=0.00 Totals: Cl=0.4132 Cdp=0.0074 Cm(c/4)=-0.0385 Cs=0.0148 Ch=-0.0773 Main component: Cl=0.3166 Cdp=0.0264 Cm=-0.0658 Flap component: Cl=0.0966 Cdp=-0.0190 Cm=-0.0760 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.0771 0.6175, -0.04610, -0.0771 0.5775, -0.01750, -0.0897 0.6274, 0.07170, -0.2116 0.5694, 0.08320, -0.3480 0.5112, 0.09090, -0.7794 0.4731, 0.09830, -0.8106 0.4349, 0.10070, -0.8775 0.3960, 0.10120, -0.9118 0.3566, 0.10020, -0.8554 0.3172, 0.09790, -0.8332 0.2778, 0.09440, -0.8309 0.2393, 0.08960, -0.8455 0.2056, 0.08360, -0.8929 0.1633, 0.07610, -0.8076 0.1261, 0.06710, -0.8138 0.0900, 0.05640, -0.7551 0.0571, 0.04390, -0.7253 0.0283, 0.02940, -0.6483 0.0142, 0.01970, -0.5139 0.0081, 0.01410, -0.4462 0.0026, 0.00780, -0.0994 0.0000, 0.00000, 0.5222 0.0037, -0.00840, 1.0084 0.0112, -0.01420, 0.8858 0.0191, -0.01930, 0.7660 0.0397, -0.03030, 0.5686 0.0706, -0.04420, 0.3313 0.1037, -0.05710, 0.1547 0.1384, -0.06890, 0.0567 0.1741, -0.07950, -0.0865 0.2102, -0.08660, -0.2758 0.2472, -0.09640, -0.3801 0.2844, -0.10270, -0.5023 0.3225, -0.10690, -0.5508 0.3608, -0.10890, -0.6387 0.3991, -0.10830, -0.6367 0.4373, -0.10510, -0.6224 0.4757, -0.09890, -0.5413 0.5137, -0.09070, -0.5406 0.5694, -0.07640, -0.1510 0.5777, -0.04660, -0.0928 15 Flap element taps 1.0000, 0.00130, 0.1908 0.9365, 0.01390, 0.0876 0.8333, 0.03280, -0.0491 0.7436, 0.04930, -0.1500 0.7049, 0.05670, -0.1866 0.6662, 0.06410, -0.3773 0.6522, 0.01390, -0.0869 0.5969, -0.00020, -0.0800 0.6000, -0.03020, -0.0787 0.6324, -0.04540, -0.0905 0.6667, -0.04880, 0.0882 0.7046, -0.04110, 0.1540 0.7429, -0.03210, 0.1788 0.8333, -0.01400, 0.2458 0.9311, -0.00120, 0.3164 Wake drag found for this condition, Cdw=0.0095 --------- Run Conditions: vel=110.1 ft/s Re=1.008x10^6 AOA=6.08 Flap deflection=0.00 Totals: Cl=0.7440 Cdp=0.0097 Cm(c/4)=-0.0488 Cs=0.0692 Ch=-0.0934 Main component: Cl=0.6098 Cdp=0.0204 Cm=-0.1314 Flap component: Cl=0.1342 Cdp=-0.0107 Cm=-0.1026 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.0361 0.6175, -0.04610, -0.0442 0.5775, -0.01750, -0.0715 0.6274, 0.07170, -0.2277 0.5694, 0.08320, -0.4429 0.5112, 0.09090, -0.7873 0.4731, 0.09830, -0.9621 0.4349, 0.10070, -1.0318 0.3960, 0.10120, -1.0878 0.3566, 0.10020, -1.0426 0.3172, 0.09790, -1.0442 0.2778, 0.09440, -1.0613 0.2393, 0.08960, -1.1093 0.2056, 0.08360, -1.2005 0.1633, 0.07610, -1.1455 0.1261, 0.06710, -1.2112 0.0900, 0.05640, -1.2258 0.0571, 0.04390, -1.3197 0.0283, 0.02940, -1.4437 0.0142, 0.01970, -1.5166 0.0081, 0.01410, -1.6384 0.0026, 0.00780, -1.3738 0.0000, 0.00000, -0.9507 0.0037, -0.00840, 0.8409 0.0112, -0.01420, 1.0089 0.0191, -0.01930, 0.9772 0.0397, -0.03030, 0.8318 0.0706, -0.04420, 0.6027 0.1037, -0.05710, 0.4209 0.1384, -0.06890, 0.3264 0.1741, -0.07950, 0.1733 0.2102, -0.08660, -0.0325 0.2472, -0.09640, -0.1379 0.2844, -0.10270, -0.2756 0.3225, -0.10690, -0.3296 0.3608, -0.10890, -0.4353 0.3991, -0.10830, -0.4493 0.4373, -0.10510, -0.4685 0.4757, -0.09890, -0.3894 0.5137, -0.09070, -0.3742 0.5694, -0.07640, -0.0557 0.5777, -0.04660, -0.0655 15 Flap element taps 1.0000, 0.00130, 0.1354 0.9365, 0.01390, 0.0631 0.8333, 0.03280, -0.0742 0.7436, 0.04930, -0.2010 0.7049, 0.05670, -0.2674 0.6662, 0.06410, -0.4895 0.6522, 0.01390, -0.0727 0.5969, -0.00020, -0.0639 0.6000, -0.03020, -0.0594 0.6324, -0.04540, -0.0674 0.6667, -0.04880, 0.5414 0.7046, -0.04110, 0.2000 0.7429, -0.03210, 0.2198 0.8333, -0.01400, 0.2646 0.9311, -0.00120, 0.3210 Wake drag found for this condition, Cdw=0.0086 --------- Run Conditions: vel=109.7 ft/s Re=1.004x10^6 AOA=9.05 Flap deflection=0.00 Totals: Cl=0.8514 Cdp=0.0261 Cm(c/4)=-0.0371 Cs=0.1081 Ch=-0.1259 Main component: Cl=0.7047 Cdp=0.0142 Cm=-0.1318 Flap component: Cl=0.1467 Cdp=0.0119 Cm=-0.1166 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.0318 0.6175, -0.04610, -0.0567 0.5775, -0.01750, -0.0958 0.6274, 0.07170, -0.1909 0.5694, 0.08320, -0.2140 0.5112, 0.09090, -0.4934 0.4731, 0.09830, -0.7376 0.4349, 0.10070, -0.8926 0.3960, 0.10120, -1.0163 0.3566, 0.10020, -1.0139 0.3172, 0.09790, -1.0468 0.2778, 0.09440, -1.0991 0.2393, 0.08960, -1.1883 0.2056, 0.08360, -1.3280 0.1633, 0.07610, -1.3068 0.1261, 0.06710, -1.4236 0.0900, 0.05640, -1.4963 0.0571, 0.04390, -1.7333 0.0283, 0.02940, -2.0680 0.0142, 0.01970, -2.3462 0.0081, 0.01410, -2.7244 0.0026, 0.00780, -2.6166 0.0000, 0.00000, -2.5495 0.0037, -0.00840, 0.4261 0.0112, -0.01420, 0.9435 0.0191, -0.01930, 1.0061 0.0397, -0.03030, 0.9496 0.0706, -0.04420, 0.7511 0.1037, -0.05710, 0.5785 0.1384, -0.06890, 0.4875 0.1741, -0.07950, 0.3319 0.2102, -0.08660, 0.1151 0.2472, -0.09640, 0.0092 0.2844, -0.10270, -0.1407 0.3225, -0.10690, -0.2033 0.3608, -0.10890, -0.3213 0.3991, -0.10830, -0.3489 0.4373, -0.10510, -0.3959 0.4757, -0.09890, -0.3271 0.5137, -0.09070, -0.2984 0.5694, -0.07640, -0.1239 0.5777, -0.04660, -0.0850 15 Flap element taps 1.0000, 0.00130, -0.1068 0.9365, 0.01390, -0.1756 0.8333, 0.03280, -0.2223 0.7436, 0.04930, -0.2261 0.7049, 0.05670, -0.2147 0.6662, 0.06410, -0.2188 0.6522, 0.01390, -0.0972 0.5969, -0.00020, -0.0885 0.6000, -0.03020, -0.0812 0.6324, -0.04540, -0.0903 0.6667, -0.04880, 0.5768 0.7046, -0.04110, 0.1895 0.7429, -0.03210, 0.2003 0.8333, -0.01400, 0.2202 0.9311, -0.00120, 0.2342 Wake drag found for this condition, Cdw=0.0137 --------- Run Conditions: vel=109.1 ft/s Re=0.997x10^6 AOA=12.06 Flap deflection=0.00 Totals: Cl=0.9418 Cdp=0.0493 Cm(c/4)=-0.0329 Cs=0.1485 Ch=-0.1478 Main component: Cl=0.7756 Cdp=0.0224 Cm=-0.1319 Flap component: Cl=0.1662 Cdp=0.0270 Cm=-0.1338 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.0280 0.6175, -0.04610, -0.0820 0.5775, -0.01750, -0.1297 0.6274, 0.07170, -0.2884 0.5694, 0.08320, -0.2578 0.5112, 0.09090, -0.3129 0.4731, 0.09830, -0.4399 0.4349, 0.10070, -0.6424 0.3960, 0.10120, -0.8574 0.3566, 0.10020, -0.9139 0.3172, 0.09790, -0.9951 0.2778, 0.09440, -1.0836 0.2393, 0.08960, -1.2135 0.2056, 0.08360, -1.3996 0.1633, 0.07610, -1.4190 0.1261, 0.06710, -1.5974 0.0900, 0.05640, -1.7493 0.0571, 0.04390, -2.0643 0.0283, 0.02940, -2.5284 0.0142, 0.01970, -3.1463 0.0081, 0.01410, -3.8787 0.0026, 0.00780, -3.9452 0.0000, 0.00000, -4.2926 0.0037, -0.00840, -0.1282 0.0112, -0.01420, 0.7827 0.0191, -0.01930, 0.9686 0.0397, -0.03030, 1.0098 0.0706, -0.04420, 0.8568 0.1037, -0.05710, 0.7002 0.1384, -0.06890, 0.6187 0.1741, -0.07950, 0.4651 0.2102, -0.08660, 0.2382 0.2472, -0.09640, 0.1342 0.2844, -0.10270, -0.0275 0.3225, -0.10690, -0.0937 0.3608, -0.10890, -0.2278 0.3991, -0.10830, -0.2668 0.4373, -0.10510, -0.3352 0.4757, -0.09890, -0.2827 0.5137, -0.09070, -0.2588 0.5694, -0.07640, -0.1662 0.5777, -0.04660, -0.1152 15 Flap element taps 1.0000, 0.00130, -0.2337 0.9365, 0.01390, -0.3160 0.8333, 0.03280, -0.3167 0.7436, 0.04930, -0.2990 0.7049, 0.05670, -0.2913 0.6662, 0.06410, -0.2891 0.6522, 0.01390, -0.1325 0.5969, -0.00020, -0.1242 0.6000, -0.03020, -0.1144 0.6324, -0.04540, -0.1280 0.6667, -0.04880, 0.5972 0.7046, -0.04110, 0.1787 0.7429, -0.03210, 0.1831 0.8333, -0.01400, 0.1844 0.9311, -0.00120, 0.1772 --------- Run Conditions: vel=108.7 ft/s Re=0.992x10^6 AOA=15.02 Flap deflection=0.00 Totals: Cl=1.0248 Cdp=0.0852 Cm(c/4)=-0.0406 Cs=0.1833 Ch=-0.1693 Main component: Cl=0.8337 Cdp=0.0420 Cm=-0.1384 Flap component: Cl=0.1910 Cdp=0.0432 Cm=-0.1552 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.0509 0.6175, -0.04610, -0.1216 0.5775, -0.01750, -0.1764 0.6274, 0.07170, -0.3780 0.5694, 0.08320, -0.3463 0.5112, 0.09090, -0.3786 0.4731, 0.09830, -0.3987 0.4349, 0.10070, -0.4755 0.3960, 0.10120, -0.6793 0.3566, 0.10020, -0.7654 0.3172, 0.09790, -0.8871 0.2778, 0.09440, -1.0093 0.2393, 0.08960, -1.1747 0.2056, 0.08360, -1.3996 0.1633, 0.07610, -1.4557 0.1261, 0.06710, -1.6897 0.0900, 0.05640, -1.9043 0.0571, 0.04390, -2.3235 0.0283, 0.02940, -2.9695 0.0142, 0.01970, -3.6545 0.0081, 0.01410, -4.8321 0.0026, 0.00780, -5.2609 0.0000, 0.00000, -5.9775 0.0037, -0.00840, -0.7363 0.0112, -0.01420, 0.5598 0.0191, -0.01930, 0.8778 0.0397, -0.03030, 1.0257 0.0706, -0.04420, 0.9219 0.1037, -0.05710, 0.7864 0.1384, -0.06890, 0.7171 0.1741, -0.07950, 0.5669 0.2102, -0.08660, 0.3369 0.2472, -0.09640, 0.2348 0.2844, -0.10270, 0.0657 0.3225, -0.10690, -0.0047 0.3608, -0.10890, -0.1481 0.3991, -0.10830, -0.1963 0.4373, -0.10510, -0.2837 0.4757, -0.09890, -0.2451 0.5137, -0.09070, -0.2376 0.5694, -0.07640, -0.1249 0.5777, -0.04660, -0.1551 15 Flap element taps 1.0000, 0.00130, -0.3497 0.9365, 0.01390, -0.4155 0.8333, 0.03280, -0.4195 0.7436, 0.04930, -0.3979 0.7049, 0.05670, -0.3936 0.6662, 0.06410, -0.3981 0.6522, 0.01390, -0.1801 0.5969, -0.00020, -0.1730 0.6000, -0.03020, -0.1602 0.6324, -0.04540, -0.1854 0.6667, -0.04880, 0.7022 0.7046, -0.04110, 0.1721 0.7429, -0.03210, 0.1645 0.8333, -0.01400, 0.1571 0.9311, -0.00120, 0.1353 --------- Run Conditions: vel=107.7 ft/s Re=0.982x10^6 AOA=18.02 Flap deflection=0.00 Totals: Cl=0.9222 Cdp=0.1543 Cm(c/4)=-0.0626 Cs=0.1385 Ch=-0.1941 Main component: Cl=0.7079 Cdp=0.0932 Cm=-0.1170 Flap component: Cl=0.2142 Cdp=0.0611 Cm=-0.1768 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.1204 0.6175, -0.04610, -0.2116 0.5775, -0.01750, -0.2674 0.6274, 0.07170, -0.5739 0.5694, 0.08320, -0.5118 0.5112, 0.09090, -0.5077 0.4731, 0.09830, -0.5085 0.4349, 0.10070, -0.5058 0.3960, 0.10120, -0.5859 0.3566, 0.10020, -0.5193 0.3172, 0.09790, -0.5154 0.2778, 0.09440, -0.5262 0.2393, 0.08960, -0.6421 0.2056, 0.08360, -0.9082 0.1633, 0.07610, -1.0339 0.1261, 0.06710, -1.3502 0.0900, 0.05640, -1.6184 0.0571, 0.04390, -2.0966 0.0283, 0.02940, -2.8118 0.0142, 0.01970, -3.5379 0.0081, 0.01410, -4.8523 0.0026, 0.00780, -5.3700 0.0000, 0.00000, -6.2175 0.0037, -0.00840, -0.8886 0.0112, -0.01420, 0.4894 0.0191, -0.01930, 0.8398 0.0397, -0.03030, 1.0245 0.0706, -0.04420, 0.9378 0.1037, -0.05710, 0.8110 0.1384, -0.06890, 0.7517 0.1741, -0.07950, 0.6012 0.2102, -0.08660, 0.3622 0.2472, -0.09640, 0.2607 0.2844, -0.10270, 0.0832 0.3225, -0.10690, 0.0115 0.3608, -0.10890, -0.1424 0.3991, -0.10830, -0.1979 0.4373, -0.10510, -0.3016 0.4757, -0.09890, -0.2703 0.5137, -0.09070, -0.2745 0.5694, -0.07640, -0.1535 0.5777, -0.04660, -0.2384 15 Flap element taps 1.0000, 0.00130, -0.5000 0.9365, 0.01390, -0.5500 0.8333, 0.03280, -0.5763 0.7436, 0.04930, -0.5548 0.7049, 0.05670, -0.5415 0.6662, 0.06410, -0.5354 0.6522, 0.01390, -0.2745 0.5969, -0.00020, -0.2678 0.6000, -0.03020, -0.2510 0.6324, -0.04540, -0.3800 0.6667, -0.04880, 0.7284 0.7046, -0.04110, 0.1284 0.7429, -0.03210, 0.1118 0.8333, -0.01400, 0.0931 0.9311, -0.00120, 0.0640 --------- Run Conditions: vel=108.7 ft/s Re=0.991x10^6 AOA=20.01 Flap deflection=0.00 Totals: Cl=0.6087 Cdp=0.3078 Cm(c/4)=-0.1064 Cs=-0.0810 Ch=-0.1971 Main component: Cl=0.3883 Cdp=0.2381 Cm=-0.0929 Flap component: Cl=0.2204 Cdp=0.0697 Cm=-0.1828 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.2417 0.6175, -0.04610, -0.3304 0.5775, -0.01750, -0.3974 0.6274, 0.07170, -0.7204 0.5694, 0.08320, -0.6787 0.5112, 0.09090, -0.6786 0.4731, 0.09830, -0.6724 0.4349, 0.10070, -0.6758 0.3960, 0.10120, -0.7638 0.3566, 0.10020, -0.6906 0.3172, 0.09790, -0.6739 0.2778, 0.09440, -0.6461 0.2393, 0.08960, -0.6583 0.2056, 0.08360, -0.7475 0.1633, 0.07610, -0.6300 0.1261, 0.06710, -0.6932 0.0900, 0.05640, -0.6394 0.0571, 0.04390, -0.6674 0.0283, 0.02940, -0.6913 0.0142, 0.01970, -0.6875 0.0081, 0.01410, -0.7718 0.0026, 0.00780, -0.6416 0.0000, 0.00000, -0.9323 0.0037, -0.00840, 0.5767 0.0112, -0.01420, 0.9439 0.0191, -0.01930, 1.0020 0.0397, -0.03030, 0.9850 0.0706, -0.04420, 0.8226 0.1037, -0.05710, 0.6692 0.1384, -0.06890, 0.6073 0.1741, -0.07950, 0.4502 0.2102, -0.08660, 0.1995 0.2472, -0.09640, 0.0937 0.2844, -0.10270, -0.0888 0.3225, -0.10690, -0.1602 0.3608, -0.10890, -0.3224 0.3991, -0.10830, -0.3764 0.4373, -0.10510, -0.4782 0.4757, -0.09890, -0.4371 0.5137, -0.09070, -0.4322 0.5694, -0.07640, -0.3012 0.5777, -0.04660, -0.3679 15 Flap element taps 1.0000, 0.00130, -0.6091 0.9365, 0.01390, -0.6587 0.8333, 0.03280, -0.6937 0.7436, 0.04930, -0.6726 0.7049, 0.05670, -0.6635 0.6662, 0.06410, -0.6534 0.6522, 0.01390, -0.4082 0.5969, -0.00020, -0.3977 0.6000, -0.03020, -0.3830 0.6324, -0.04540, -0.4526 0.6667, -0.04880, 0.6802 0.7046, -0.04110, 0.0234 0.7429, -0.03210, 0.0102 0.8333, -0.01400, -0.0074 0.9311, -0.00120, -0.0396 --------- Run Conditions: vel=111.6 ft/s Re=1.011x10^6 AOA=24.01 Flap deflection=0.00 Totals: Cl=0.7076 Cdp=0.4079 Cm(c/4)=-0.1278 Cs=-0.0847 Ch=-0.2201 Main component: Cl=0.4706 Cdp=0.3143 Cm=-0.1289 Flap component: Cl=0.2371 Cdp=0.0936 Cm=-0.2020 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.2351 0.6175, -0.04610, -0.3810 0.5775, -0.01750, -0.4421 0.6274, 0.07170, -0.8124 0.5694, 0.08320, -0.8057 0.5112, 0.09090, -0.8014 0.4731, 0.09830, -0.7883 0.4349, 0.10070, -0.7794 0.3960, 0.10120, -0.8072 0.3566, 0.10020, -0.7642 0.3172, 0.09790, -0.7660 0.2778, 0.09440, -0.7654 0.2393, 0.08960, -0.7624 0.2056, 0.08360, -0.7901 0.1633, 0.07610, -0.7446 0.1261, 0.06710, -0.7675 0.0900, 0.05640, -0.7475 0.0571, 0.04390, -0.7613 0.0283, 0.02940, -0.7651 0.0142, 0.01970, -0.7700 0.0081, 0.01410, -0.7976 0.0026, 0.00780, -0.7312 0.0000, 0.00000, -0.9768 0.0037, -0.00840, 0.3572 0.0112, -0.01420, 0.8603 0.0191, -0.01930, 0.9833 0.0397, -0.03030, 1.0154 0.0706, -0.04420, 0.9047 0.1037, -0.05710, 0.7828 0.1384, -0.06890, 0.6819 0.1741, -0.07950, 0.5429 0.2102, -0.08660, 0.3587 0.2472, -0.09640, 0.2183 0.2844, -0.10270, 0.0640 0.3225, -0.10690, -0.0470 0.3608, -0.10890, -0.2032 0.3991, -0.10830, -0.2927 0.4373, -0.10510, -0.3678 0.4757, -0.09890, -0.3518 0.5137, -0.09070, -0.3336 0.5694, -0.07640, -0.2317 0.5777, -0.04660, -0.3873 15 Flap element taps 1.0000, 0.00130, -0.7120 0.9365, 0.01390, -0.7554 0.8333, 0.03280, -0.7782 0.7436, 0.04930, -0.7689 0.7049, 0.05670, -0.7556 0.6662, 0.06410, -0.7361 0.6522, 0.01390, -0.4490 0.5969, -0.00020, -0.4508 0.6000, -0.03020, -0.4146 0.6324, -0.04540, -0.6198 0.6667, -0.04880, 0.6949 0.7046, -0.04110, 0.0359 0.7429, -0.03210, 0.0256 0.8333, -0.01400, 0.0046 0.9311, -0.00120, -0.0875 --------- Run Conditions: vel=110.3 ft/s Re=0.998x10^6 AOA=26.97 Flap deflection=0.00 Totals: Cl=0.8493 Cdp=0.5319 Cm(c/4)=-0.1607 Cs=-0.0889 Ch=-0.2604 Main component: Cl=0.5796 Cdp=0.4069 Cm=-0.1742 Flap component: Cl=0.2697 Cdp=0.1249 Cm=-0.2361 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.2014 0.6175, -0.04610, -0.4341 0.5775, -0.01750, -0.5086 0.6274, 0.07170, -0.9867 0.5694, 0.08320, -0.9664 0.5112, 0.09090, -0.9609 0.4731, 0.09830, -0.9454 0.4349, 0.10070, -0.9385 0.3960, 0.10120, -0.9836 0.3566, 0.10020, -0.9210 0.3172, 0.09790, -0.9234 0.2778, 0.09440, -0.9190 0.2393, 0.08960, -0.9183 0.2056, 0.08360, -0.9578 0.1633, 0.07610, -0.8951 0.1261, 0.06710, -0.9284 0.0900, 0.05640, -0.8978 0.0571, 0.04390, -0.9162 0.0283, 0.02940, -0.9137 0.0142, 0.01970, -0.9171 0.0081, 0.01410, -0.9590 0.0026, 0.00780, -0.8738 0.0000, 0.00000, -0.9422 0.0037, -0.00840, 0.1015 0.0112, -0.01420, 0.7326 0.0191, -0.01930, 0.9231 0.0397, -0.03030, 1.0270 0.0706, -0.04420, 0.9561 0.1037, -0.05710, 0.8583 0.1384, -0.06890, 0.7893 0.1741, -0.07950, 0.6585 0.2102, -0.08660, 0.4667 0.2472, -0.09640, 0.3426 0.2844, -0.10270, 0.1817 0.3225, -0.10690, 0.0838 0.3608, -0.10890, -0.0838 0.3991, -0.10830, -0.1730 0.4373, -0.10510, -0.2693 0.4757, -0.09890, -0.2676 0.5137, -0.09070, -0.2710 0.5694, -0.07640, -0.1772 0.5777, -0.04660, -0.4363 15 Flap element taps 1.0000, 0.00130, -0.8531 0.9365, 0.01390, -0.9012 0.8333, 0.03280, -0.9342 0.7436, 0.04930, -0.9262 0.7049, 0.05670, -0.9142 0.6662, 0.06410, -0.8927 0.6522, 0.01390, -0.5184 0.5969, -0.00020, -0.5160 0.6000, -0.03020, -0.4713 0.6324, -0.04540, -0.7384 0.6667, -0.04880, 0.6657 0.7046, -0.04110, 0.0548 0.7429, -0.03210, 0.0331 0.8333, -0.01400, -0.0074 0.9311, -0.00120, -0.1229 --------- Run Conditions: vel=109.1 ft/s Re=0.987x10^6 AOA=30.02 Flap deflection=0.00 Totals: Cl=0.9598 Cdp=0.6571 Cm(c/4)=-0.1925 Cs=-0.0887 Ch=-0.3007 Main component: Cl=0.6631 Cdp=0.4968 Cm=-0.2138 Flap component: Cl=0.2968 Cdp=0.1603 Cm=-0.2687 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.1463 0.6175, -0.04610, -0.4615 0.5775, -0.01750, -0.5502 0.6274, 0.07170, -1.1224 0.5694, 0.08320, -1.0951 0.5112, 0.09090, -1.0937 0.4731, 0.09830, -1.0733 0.4349, 0.10070, -1.0708 0.3960, 0.10120, -1.1330 0.3566, 0.10020, -1.0574 0.3172, 0.09790, -1.0580 0.2778, 0.09440, -1.0500 0.2393, 0.08960, -1.0493 0.2056, 0.08360, -1.1012 0.1633, 0.07610, -1.0205 0.1261, 0.06710, -1.0602 0.0900, 0.05640, -1.0220 0.0571, 0.04390, -1.0419 0.0283, 0.02940, -1.0327 0.0142, 0.01970, -1.0377 0.0081, 0.01410, -1.0904 0.0026, 0.00780, -0.9868 0.0000, 0.00000, -1.0367 0.0037, -0.00840, -0.1499 0.0112, -0.01420, 0.5870 0.0191, -0.01930, 0.8382 0.0397, -0.03030, 1.0150 0.0706, -0.04420, 0.9833 0.1037, -0.05710, 0.9118 0.1384, -0.06890, 0.8756 0.1741, -0.07950, 0.7553 0.2102, -0.08660, 0.5598 0.2472, -0.09640, 0.4505 0.2844, -0.10270, 0.2870 0.3225, -0.10690, 0.2023 0.3608, -0.10890, 0.0245 0.3991, -0.10830, -0.0630 0.4373, -0.10510, -0.1784 0.4757, -0.09890, -0.1907 0.5137, -0.09070, -0.1933 0.5694, -0.07640, -0.1113 0.5777, -0.04660, -0.4614 15 Flap element taps 1.0000, 0.00130, -1.0329 0.9365, 0.01390, -1.0771 0.8333, 0.03280, -1.0627 0.7436, 0.04930, -1.0641 0.7049, 0.05670, -1.0498 0.6662, 0.06410, -1.0366 0.6522, 0.01390, -0.5729 0.5969, -0.00020, -0.5759 0.6000, -0.03020, -0.5173 0.6324, -0.04540, -0.8403 0.6667, -0.04880, 0.6596 0.7046, -0.04110, 0.0701 0.7429, -0.03210, 0.0376 0.8333, -0.01400, -0.0226 0.9311, -0.00120, -0.1565 --------- Run Conditions: vel=109.1 ft/s Re=0.986x10^6 AOA=35.01 Flap deflection=0.00 Totals: Cl=1.0916 Cdp=0.8727 Cm(c/4)=-0.2429 Cs=-0.0885 Ch=-0.3574 Main component: Cl=0.7590 Cdp=0.6511 Cm=-0.2732 Flap component: Cl=0.3326 Cdp=0.2215 Cm=-0.3184 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.0771 0.6175, -0.04610, -0.5139 0.5775, -0.01750, -0.6072 0.6274, 0.07170, -1.3601 0.5694, 0.08320, -1.2975 0.5112, 0.09090, -1.2770 0.4731, 0.09830, -1.2747 0.4349, 0.10070, -1.2672 0.3960, 0.10120, -1.3317 0.3566, 0.10020, -1.2382 0.3172, 0.09790, -1.2339 0.2778, 0.09440, -1.2207 0.2393, 0.08960, -1.2179 0.2056, 0.08360, -1.2786 0.1633, 0.07610, -1.1809 0.1261, 0.06710, -1.2280 0.0900, 0.05640, -1.1762 0.0571, 0.04390, -1.1976 0.0283, 0.02940, -1.1872 0.0142, 0.01970, -1.1900 0.0081, 0.01410, -1.2530 0.0026, 0.00780, -1.1355 0.0000, 0.00000, -1.1782 0.0037, -0.00840, -0.5605 0.0112, -0.01420, 0.3128 0.0191, -0.01930, 0.6575 0.0397, -0.03030, 0.9524 0.0706, -0.04420, 0.9934 0.1037, -0.05710, 0.9716 0.1384, -0.06890, 0.9836 0.1741, -0.07950, 0.8868 0.2102, -0.08660, 0.7000 0.2472, -0.09640, 0.6185 0.2844, -0.10270, 0.4609 0.3225, -0.10690, 0.3937 0.3608, -0.10890, 0.2154 0.3991, -0.10830, 0.1311 0.4373, -0.10510, 0.0008 0.4757, -0.09890, -0.0312 0.5137, -0.09070, -0.0762 0.5694, -0.07640, -0.0122 0.5777, -0.04660, -0.4876 15 Flap element taps 1.0000, 0.00130, -1.1978 0.9365, 0.01390, -1.2327 0.8333, 0.03280, -1.2616 0.7436, 0.04930, -1.2566 0.7049, 0.05670, -1.2487 0.6662, 0.06410, -1.2290 0.6522, 0.01390, -0.6360 0.5969, -0.00020, -0.6273 0.6000, -0.03020, -0.5661 0.6324, -0.04540, -0.9401 0.6667, -0.04880, 0.6718 0.7046, -0.04110, 0.1320 0.7429, -0.03210, 0.0845 0.8333, -0.01400, -0.0008 0.9311, -0.00120, -0.1762 --------- Run Conditions: vel=107.5 ft/s Re=0.971x10^6 AOA=39.98 Flap deflection=0.00 Totals: Cl=1.1652 Cdp=1.0844 Cm(c/4)=-0.2876 Cs=-0.0823 Ch=-0.4078 Main component: Cl=0.8119 Cdp=0.7992 Cm=-0.3231 Flap component: Cl=0.3533 Cdp=0.2851 Cm=-0.3619 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, 0.0126 0.6175, -0.04610, -0.5208 0.5775, -0.01750, -0.6390 0.6274, 0.07170, -1.5191 0.5694, 0.08320, -1.4497 0.5112, 0.09090, -1.4368 0.4731, 0.09830, -1.4230 0.4349, 0.10070, -1.4138 0.3960, 0.10120, -1.4950 0.3566, 0.10020, -1.3869 0.3172, 0.09790, -1.3801 0.2778, 0.09440, -1.3603 0.2393, 0.08960, -1.3581 0.2056, 0.08360, -1.4252 0.1633, 0.07610, -1.3127 0.1261, 0.06710, -1.3611 0.0900, 0.05640, -1.3026 0.0571, 0.04390, -1.3245 0.0283, 0.02940, -1.3096 0.0142, 0.01970, -1.3100 0.0081, 0.01410, -1.3841 0.0026, 0.00780, -1.2517 0.0000, 0.00000, -1.2891 0.0037, -0.00840, -0.9193 0.0112, -0.01420, 0.0375 0.0191, -0.01930, 0.4596 0.0397, -0.03030, 0.8608 0.0706, -0.04420, 0.9770 0.1037, -0.05710, 1.0002 0.1384, -0.06890, 1.0595 0.1741, -0.07950, 0.9871 0.2102, -0.08660, 0.8112 0.2472, -0.09640, 0.7594 0.2844, -0.10270, 0.6091 0.3225, -0.10690, 0.5627 0.3608, -0.10890, 0.3839 0.3991, -0.10830, 0.3064 0.4373, -0.10510, 0.1617 0.4757, -0.09890, 0.1154 0.5137, -0.09070, 0.0490 0.5694, -0.07640, 0.0928 0.5777, -0.04660, -0.4955 15 Flap element taps 1.0000, 0.00130, -1.3323 0.9365, 0.01390, -1.3759 0.8333, 0.03280, -1.4051 0.7436, 0.04930, -1.4042 0.7049, 0.05670, -1.4093 0.6662, 0.06410, -1.3849 0.6522, 0.01390, -0.6705 0.5969, -0.00020, -0.6578 0.6000, -0.03020, -0.5868 0.6324, -0.04540, -0.9968 0.6667, -0.04880, 0.6992 0.7046, -0.04110, 0.1948 0.7429, -0.03210, 0.1364 0.8333, -0.01400, 0.0274 0.9311, -0.00120, -0.1758 --------- Run Conditions: vel=108.4 ft/s Re=0.978x10^6 AOA=45.03 Flap deflection=0.00 Totals: Cl=1.1987 Cdp=1.3055 Cm(c/4)=-0.3317 Cs=-0.0746 Ch=-0.4537 Main component: Cl=0.8364 Cdp=0.9542 Cm=-0.3721 Flap component: Cl=0.3622 Cdp=0.3513 Cm=-0.4023 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, 0.1064 0.6175, -0.04610, -0.5274 0.5775, -0.01750, -0.6712 0.6274, 0.07170, -1.7313 0.5694, 0.08320, -1.6055 0.5112, 0.09090, -1.6141 0.4731, 0.09830, -1.5952 0.4349, 0.10070, -1.5828 0.3960, 0.10120, -1.6653 0.3566, 0.10020, -1.5434 0.3172, 0.09790, -1.5284 0.2778, 0.09440, -1.5080 0.2393, 0.08960, -1.5017 0.2056, 0.08360, -1.5724 0.1633, 0.07610, -1.4445 0.1261, 0.06710, -1.5008 0.0900, 0.05640, -1.4335 0.0571, 0.04390, -1.4538 0.0283, 0.02940, -1.4255 0.0142, 0.01970, -1.4236 0.0081, 0.01410, -1.5023 0.0026, 0.00780, -1.3659 0.0000, 0.00000, -1.4013 0.0037, -0.00840, -1.2593 0.0112, -0.01420, -0.2678 0.0191, -0.01930, 0.2189 0.0397, -0.03030, 0.7187 0.0706, -0.04420, 0.9102 0.1037, -0.05710, 0.9835 0.1384, -0.06890, 1.0873 0.1741, -0.07950, 1.0449 0.2102, -0.08660, 0.8897 0.2472, -0.09640, 0.8649 0.2844, -0.10270, 0.7308 0.3225, -0.10690, 0.7047 0.3608, -0.10890, 0.5353 0.3991, -0.10830, 0.4648 0.4373, -0.10510, 0.3149 0.4757, -0.09890, 0.2572 0.5137, -0.09070, 0.1776 0.5694, -0.07640, 0.2010 0.5777, -0.04660, -0.4972 15 Flap element taps 1.0000, 0.00130, -1.4820 0.9365, 0.01390, -1.5144 0.8333, 0.03280, -1.5288 0.7436, 0.04930, -1.5439 0.7049, 0.05670, -1.5561 0.6662, 0.06410, -1.5462 0.6522, 0.01390, -0.7021 0.5969, -0.00020, -0.6907 0.6000, -0.03020, -0.6082 0.6324, -0.04540, -1.0464 0.6667, -0.04880, 0.7249 0.7046, -0.04110, 0.2564 0.7429, -0.03210, 0.1874 0.8333, -0.01400, 0.0551 0.9311, -0.00120, -0.1809 --------- Run Conditions: vel=111.5 ft/s Re=1.003x10^6 AOA=60.05 Flap deflection=0.00 Totals: Cl=1.0303 Cdp=1.8227 Cm(c/4)=-0.4368 Cs=-0.0173 Ch=-0.5902 Main component: Cl=0.7607 Cdp=1.2575 Cm=-0.4612 Flap component: Cl=0.2695 Cdp=0.5651 Cm=-0.4991 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, 0.4186 0.6175, -0.04610, 0.0196 0.5775, -0.01750, -0.0303 0.6274, 0.07170, -1.7635 0.5694, 0.08320, -1.8025 0.5112, 0.09090, -1.8107 0.4731, 0.09830, -1.8288 0.4349, 0.10070, -1.8392 0.3960, 0.10120, -1.8242 0.3566, 0.10020, -1.8175 0.3172, 0.09790, -1.8081 0.2778, 0.09440, -1.8059 0.2393, 0.08960, -1.7824 0.2056, 0.08360, -1.7589 0.1633, 0.07610, -1.7255 0.1261, 0.06710, -1.7092 0.0900, 0.05640, -1.6846 0.0571, 0.04390, -1.6671 0.0283, 0.02940, -1.6510 0.0142, 0.01970, -1.6445 0.0081, 0.01410, -1.6476 0.0026, 0.00780, -1.5807 0.0000, 0.00000, -1.6246 0.0037, -0.00840, -1.7990 0.0112, -0.01420, -1.0483 0.0191, -0.01930, -0.4905 0.0397, -0.03030, 0.1764 0.0706, -0.04420, 0.5720 0.1037, -0.05710, 0.7914 0.1384, -0.06890, 0.9140 0.1741, -0.07950, 0.9765 0.2102, -0.08660, 0.9968 0.2472, -0.09640, 0.9979 0.2844, -0.10270, 0.9751 0.3225, -0.10690, 0.9432 0.3608, -0.10890, 0.8693 0.3991, -0.10830, 0.7977 0.4373, -0.10510, 0.7124 0.4757, -0.09890, 0.6466 0.5137, -0.09070, 0.5695 0.5694, -0.07640, 0.5175 0.5777, -0.04660, 0.0462 15 Flap element taps 1.0000, 0.00130, -1.7276 0.9365, 0.01390, -1.7631 0.8333, 0.03280, -1.7828 0.7436, 0.04930, -1.7764 0.7049, 0.05670, -1.7768 0.6662, 0.06410, -1.7587 0.6522, 0.01390, -0.0479 0.5969, -0.00020, -0.0859 0.6000, -0.03020, -0.0365 0.6324, -0.04540, -0.2595 0.6667, -0.04880, 0.8146 0.7046, -0.04110, 0.4545 0.7429, -0.03210, 0.3966 0.8333, -0.01400, 0.2394 0.9311, -0.00120, -0.1023 --------- Run Conditions: vel=110.7 ft/s Re=0.995x10^6 AOA=70.04 Flap deflection=0.00 Totals: Cl=0.7949 Cdp=2.1295 Cm(c/4)=-0.5102 Cs=0.0202 Ch=-0.6794 Main component: Cl=0.6077 Cdp=1.4406 Cm=-0.5088 Flap component: Cl=0.1872 Cdp=0.6889 Cm=-0.5696 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, 0.6245 0.6175, -0.04610, 0.1692 0.5775, -0.01750, 0.1078 0.6274, 0.07170, -1.9170 0.5694, 0.08320, -1.9532 0.5112, 0.09090, -2.0025 0.4731, 0.09830, -2.0176 0.4349, 0.10070, -2.0104 0.3960, 0.10120, -1.9884 0.3566, 0.10020, -1.9672 0.3172, 0.09790, -1.9588 0.2778, 0.09440, -1.9562 0.2393, 0.08960, -1.9374 0.2056, 0.08360, -1.9197 0.1633, 0.07610, -1.8811 0.1261, 0.06710, -1.8545 0.0900, 0.05640, -1.8268 0.0571, 0.04390, -1.8047 0.0283, 0.02940, -1.7873 0.0142, 0.01970, -1.7791 0.0081, 0.01410, -1.7814 0.0026, 0.00780, -1.7078 0.0000, 0.00000, -1.7551 0.0037, -0.00840, -1.9207 0.0112, -0.01420, -1.4880 0.0191, -0.01930, -0.9461 0.0397, -0.03030, -0.2243 0.0706, -0.04420, 0.2521 0.1037, -0.05710, 0.5391 0.1384, -0.06890, 0.7273 0.1741, -0.07950, 0.8501 0.2102, -0.08660, 0.9244 0.2472, -0.09640, 0.9785 0.2844, -0.10270, 1.0055 0.3225, -0.10690, 1.0212 0.3608, -0.10890, 0.9922 0.3991, -0.10830, 0.9583 0.4373, -0.10510, 0.9034 0.4757, -0.09890, 0.8497 0.5137, -0.09070, 0.7785 0.5694, -0.07640, 0.7234 0.5777, -0.04660, 0.1978 15 Flap element taps 1.0000, 0.00130, -1.8324 0.9365, 0.01390, -1.9014 0.8333, 0.03280, -1.9238 0.7436, 0.04930, -1.9219 0.7049, 0.05670, -1.9195 0.6662, 0.06410, -1.8761 0.6522, 0.01390, 0.0886 0.5969, -0.00020, 0.0477 0.6000, -0.03020, 0.1063 0.6324, -0.04540, -0.1028 0.6667, -0.04880, 0.8937 0.7046, -0.04110, 0.6243 0.7429, -0.03210, 0.5611 0.8333, -0.01400, 0.3907 0.9311, -0.00120, 0.0253 --------- Run Conditions: vel=110.3 ft/s Re=0.990x10^6 AOA=80.04 Flap deflection=0.00 Totals: Cl=0.4548 Cdp=2.2205 Cm(c/4)=-0.5418 Cs=0.0639 Ch=-0.7144 Main component: Cl=0.3877 Cdp=1.4742 Cm=-0.5101 Flap component: Cl=0.0671 Cdp=0.7464 Cm=-0.5981 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, 0.7935 0.6175, -0.04610, 0.3412 0.5775, -0.01750, 0.2596 0.6274, 0.07170, -1.9240 0.5694, 0.08320, -1.9512 0.5112, 0.09090, -1.9666 0.4731, 0.09830, -1.9708 0.4349, 0.10070, -1.9902 0.3960, 0.10120, -1.9933 0.3566, 0.10020, -1.9869 0.3172, 0.09790, -1.9671 0.2778, 0.09440, -1.9677 0.2393, 0.08960, -1.9528 0.2056, 0.08360, -1.9464 0.1633, 0.07610, -1.9091 0.1261, 0.06710, -1.8907 0.0900, 0.05640, -1.8513 0.0571, 0.04390, -1.8210 0.0283, 0.02940, -1.8122 0.0142, 0.01970, -1.8027 0.0081, 0.01410, -1.7966 0.0026, 0.00780, -1.7148 0.0000, 0.00000, -1.7623 0.0037, -0.00840, -1.8000 0.0112, -0.01420, -1.7311 0.0191, -0.01930, -1.2864 0.0397, -0.03030, -0.5973 0.0706, -0.04420, -0.0986 0.1037, -0.05710, 0.2230 0.1384, -0.06890, 0.4560 0.1741, -0.07950, 0.6206 0.2102, -0.08660, 0.7382 0.2472, -0.09640, 0.8405 0.2844, -0.10270, 0.9147 0.3225, -0.10690, 0.9808 0.3608, -0.10890, 0.9989 0.3991, -0.10830, 1.0100 0.4373, -0.10510, 0.9934 0.4757, -0.09890, 0.9688 0.5137, -0.09070, 0.9162 0.5694, -0.07640, 0.8759 0.5777, -0.04660, 0.3605 15 Flap element taps 1.0000, 0.00130, -1.7590 0.9365, 0.01390, -1.8242 0.8333, 0.03280, -1.8910 0.7436, 0.04930, -1.9047 0.7049, 0.05670, -1.9038 0.6662, 0.06410, -1.8613 0.6522, 0.01390, 0.2368 0.5969, -0.00020, 0.1923 0.6000, -0.03020, 0.2613 0.6324, -0.04540, 0.0938 0.6667, -0.04880, 0.9478 0.7046, -0.04110, 0.7752 0.7429, -0.03210, 0.7141 0.8333, -0.01400, 0.5503 0.9311, -0.00120, 0.1921 --------- Run Conditions: vel=112.8 ft/s Re=1.011x10^6 AOA=90.05 Flap deflection=0.00 Totals: Cl=0.1034 Cdp=2.2338 Cm(c/4)=-0.5786 Cs=0.1053 Ch=-0.7710 Main component: Cl=0.1741 Cdp=1.4374 Cm=-0.4978 Flap component: Cl=-0.0707 Cdp=0.7964 Cm=-0.6392 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, 0.9225 0.6175, -0.04610, 0.4907 0.5775, -0.01750, 0.3963 0.6274, 0.07170, -1.9220 0.5694, 0.08320, -1.9489 0.5112, 0.09090, -1.9559 0.4731, 0.09830, -1.9683 0.4349, 0.10070, -1.9825 0.3960, 0.10120, -1.9886 0.3566, 0.10020, -1.9533 0.3172, 0.09790, -1.9418 0.2778, 0.09440, -1.9558 0.2393, 0.08960, -1.9551 0.2056, 0.08360, -1.9536 0.1633, 0.07610, -1.9286 0.1261, 0.06710, -1.9282 0.0900, 0.05640, -1.8941 0.0571, 0.04390, -1.8690 0.0283, 0.02940, -1.8548 0.0142, 0.01970, -1.8510 0.0081, 0.01410, -1.8538 0.0026, 0.00780, -1.7674 0.0000, 0.00000, -1.8137 0.0037, -0.00840, -1.8272 0.0112, -0.01420, -1.9190 0.0191, -0.01930, -1.5857 0.0397, -0.03030, -0.9588 0.0706, -0.04420, -0.4670 0.1037, -0.05710, -0.1325 0.1384, -0.06890, 0.1350 0.1741, -0.07950, 0.3295 0.2102, -0.08660, 0.4743 0.2472, -0.09640, 0.6139 0.2844, -0.10270, 0.7287 0.3225, -0.10690, 0.8445 0.3608, -0.10890, 0.9033 0.3991, -0.10830, 0.9667 0.4373, -0.10510, 0.9909 0.4757, -0.09890, 1.0033 0.5137, -0.09070, 0.9830 0.5694, -0.07640, 0.9766 0.5777, -0.04660, 0.5051 15 Flap element taps 1.0000, 0.00130, -1.8149 0.9365, 0.01390, -1.8741 0.8333, 0.03280, -1.9068 0.7436, 0.04930, -1.9223 0.7049, 0.05670, -1.9110 0.6662, 0.06410, -1.8664 0.6522, 0.01390, 0.3639 0.5969, -0.00020, 0.3194 0.6000, -0.03020, 0.3957 0.6324, -0.04540, 0.2887 0.6667, -0.04880, 0.9858 0.7046, -0.04110, 0.8926 0.7429, -0.03210, 0.8416 0.8333, -0.01400, 0.6963 0.9311, -0.00120, 0.3564 --------- Run Conditions: vel=117.2 ft/s Re=1.051x10^6 AOA=120.04 Flap deflection=0.00 Totals: Cl=-0.7495 Cdp=1.6411 Cm(c/4)=-0.5839 Cs=0.1728 Ch=-0.8140 Main component: Cl=-0.2774 Cdp=0.9683 Cm=-0.3722 Flap component: Cl=-0.4721 Cdp=0.6728 Cm=-0.6607 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, 0.9478 0.6175, -0.04610, 0.7338 0.5775, -0.01750, 0.6277 0.6274, 0.07170, -1.7895 0.5694, 0.08320, -1.8122 0.5112, 0.09090, -1.8287 0.4731, 0.09830, -1.8380 0.4349, 0.10070, -1.8370 0.3960, 0.10120, -1.8355 0.3566, 0.10020, -1.7875 0.3172, 0.09790, -1.7720 0.2778, 0.09440, -1.7677 0.2393, 0.08960, -1.7770 0.2056, 0.08360, -1.7994 0.1633, 0.07610, -1.7749 0.1261, 0.06710, -1.7870 0.0900, 0.05640, -1.7535 0.0571, 0.04390, -1.7323 0.0283, 0.02940, -1.6864 0.0142, 0.01970, -1.6661 0.0081, 0.01410, -1.6841 0.0026, 0.00780, -1.5791 0.0000, 0.00000, -1.6174 0.0037, -0.00840, -1.6158 0.0112, -0.01420, -1.6482 0.0191, -0.01930, -1.7036 0.0397, -0.03030, -1.4999 0.0706, -0.04420, -1.2292 0.1037, -0.05710, -1.0053 0.1384, -0.06890, -0.7769 0.1741, -0.07950, -0.6073 0.2102, -0.08660, -0.4764 0.2472, -0.09640, -0.3221 0.2844, -0.10270, -0.1677 0.3225, -0.10690, 0.0178 0.3608, -0.10890, 0.1472 0.3991, -0.10830, 0.3235 0.4373, -0.10510, 0.4601 0.4757, -0.09890, 0.6160 0.5137, -0.09070, 0.7177 0.5694, -0.07640, 0.8742 0.5777, -0.04660, 0.7443 15 Flap element taps 1.0000, 0.00130, -1.5946 0.9365, 0.01390, -1.6396 0.8333, 0.03280, -1.6991 0.7436, 0.04930, -1.7358 0.7049, 0.05670, -1.7532 0.6662, 0.06410, -1.6915 0.6522, 0.01390, 0.5900 0.5969, -0.00020, 0.5565 0.6000, -0.03020, 0.6303 0.6324, -0.04540, 0.6936 0.6667, -0.04880, 0.9233 0.7046, -0.04110, 0.9863 0.7429, -0.03210, 0.9971 0.8333, -0.01400, 0.9859 0.9311, -0.00120, 0.8580 --------- Run Conditions: vel=111.0 ft/s Re=1.004x10^6 AOA=150.07 Flap deflection=0.00 Totals: Cl=-0.5631 Cdp=0.4789 Cm(c/4)=-0.3512 Cs=0.1341 Ch=-0.5661 Main component: Cl=-0.0773 Cdp=0.2644 Cm=-0.1008 Flap component: Cl=-0.4858 Cdp=0.2145 Cm=-0.4321 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, 0.4496 0.6175, -0.04610, 0.6435 0.5775, -0.01750, 0.6765 0.6274, 0.07170, -0.9565 0.5694, 0.08320, -0.9575 0.5112, 0.09090, -0.9769 0.4731, 0.09830, -0.9879 0.4349, 0.10070, -0.9866 0.3960, 0.10120, -0.9996 0.3566, 0.10020, -0.9919 0.3172, 0.09790, -0.9760 0.2778, 0.09440, -0.9735 0.2393, 0.08960, -0.9677 0.2056, 0.08360, -0.9739 0.1633, 0.07610, -0.9527 0.1261, 0.06710, -0.9372 0.0900, 0.05640, -0.9194 0.0571, 0.04390, -0.9237 0.0283, 0.02940, -0.9306 0.0142, 0.01970, -0.9284 0.0081, 0.01410, -0.9413 0.0026, 0.00780, -0.8793 0.0000, 0.00000, -0.9273 0.0037, -0.00840, -0.9267 0.0112, -0.01420, -0.9298 0.0191, -0.01930, -0.9387 0.0397, -0.03030, -0.9333 0.0706, -0.04420, -0.9980 0.1037, -0.05710, -1.0385 0.1384, -0.06890, -1.0314 0.1741, -0.07950, -1.0189 0.2102, -0.08660, -1.0150 0.2472, -0.09640, -0.9915 0.2844, -0.10270, -0.9260 0.3225, -0.10690, -0.8304 0.3608, -0.10890, -0.7492 0.3991, -0.10830, -0.6021 0.4373, -0.10510, -0.4356 0.4757, -0.09890, -0.2012 0.5137, -0.09070, -0.0118 0.5694, -0.07640, 0.2743 0.5777, -0.04660, 0.7489 15 Flap element taps 1.0000, 0.00130, -0.9195 0.9365, 0.01390, -0.9275 0.8333, 0.03280, -0.9440 0.7436, 0.04930, -0.9534 0.7049, 0.05670, -0.9523 0.6662, 0.06410, -0.9097 0.6522, 0.01390, 0.6582 0.5969, -0.00020, 0.6274 0.6000, -0.03020, 0.6673 0.6324, -0.04540, 0.5679 0.6667, -0.04880, 0.5585 0.7046, -0.04110, 0.6136 0.7429, -0.03210, 0.6921 0.8333, -0.01400, 0.8316 0.9311, -0.00120, 0.9852 --------- Run Conditions: vel=115.0 ft/s Re=1.039x10^6 AOA=180.08 Flap deflection=0.00 Totals: Cl=-0.0479 Cdp=0.0185 Cm(c/4)=-0.0256 Cs=0.0185 Ch=-0.0580 Main component: Cl=0.0024 Cdp=0.0304 Cm=0.0039 Flap component: Cl=-0.0502 Cdp=-0.0119 Cm=-0.0414 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.1510 0.6175, -0.04610, 0.3749 0.5775, -0.01750, 0.3616 0.6274, 0.07170, -0.1143 0.5694, 0.08320, -0.3029 0.5112, 0.09090, -0.5432 0.4731, 0.09830, -0.6699 0.4349, 0.10070, -0.6902 0.3960, 0.10120, -0.6589 0.3566, 0.10020, -0.6119 0.3172, 0.09790, -0.5593 0.2778, 0.09440, -0.5393 0.2393, 0.08960, -0.5069 0.2056, 0.08360, -0.4860 0.1633, 0.07610, -0.3945 0.1261, 0.06710, -0.3071 0.0900, 0.05640, -0.1612 0.0571, 0.04390, -0.0386 0.0283, 0.02940, 0.0162 0.0142, 0.01970, 0.0166 0.0081, 0.01410, -0.0132 0.0026, 0.00780, 0.0204 0.0000, 0.00000, 0.0102 0.0037, -0.00840, 0.0059 0.0112, -0.01420, 0.0102 0.0191, -0.01930, 0.0094 0.0397, -0.03030, 0.0241 0.0706, -0.04420, 0.0014 0.1037, -0.05710, -0.0206 0.1384, -0.06890, -0.0991 0.1741, -0.07950, -0.2636 0.2102, -0.08660, -0.4445 0.2472, -0.09640, -0.5863 0.2844, -0.10270, -0.7021 0.3225, -0.10690, -0.7660 0.3608, -0.10890, -0.8503 0.3991, -0.10830, -0.8431 0.4373, -0.10510, -0.8097 0.4757, -0.09890, -0.6661 0.5137, -0.09070, -0.5363 0.5694, -0.07640, -0.2804 0.5777, -0.04660, 0.3684 15 Flap element taps 1.0000, 0.00130, 1.0159 0.9365, 0.01390, 0.1521 0.8333, 0.03280, 0.0041 0.7436, 0.04930, -0.0657 0.7049, 0.05670, -0.0685 0.6662, 0.06410, -0.1286 0.6522, 0.01390, 0.3533 0.5969, -0.00020, 0.3527 0.6000, -0.03020, 0.3585 0.6324, -0.04540, 0.3401 0.6667, -0.04880, 0.1296 0.7046, -0.04110, 0.0424 0.7429, -0.03210, 0.0981 0.8333, -0.01400, 0.1772 0.9311, -0.00120, 0.2975 --------- Run Conditions: vel=111.5 ft/s Re=1.007x10^6 AOA=210.06 Flap deflection=0.00 Totals: Cl=0.5255 Cdp=0.5190 Cm(c/4)=0.3640 Cs=0.1860 Ch=0.5667 Main component: Cl=0.0834 Cdp=0.1992 Cm=0.1008 Flap component: Cl=0.4421 Cdp=0.3197 Cm=0.4419 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.9670 0.6175, -0.04610, -0.9677 0.5775, -0.01750, -0.7310 0.6274, 0.07170, 0.4236 0.5694, 0.08320, 0.2532 0.5112, 0.09090, -0.0369 0.4731, 0.09830, -0.2305 0.4349, 0.10070, -0.3616 0.3960, 0.10120, -0.4861 0.3566, 0.10020, -0.5167 0.3172, 0.09790, -0.5906 0.2778, 0.09440, -0.7089 0.2393, 0.08960, -0.8345 0.2056, 0.08360, -1.0237 0.1633, 0.07610, -1.0866 0.1261, 0.06710, -1.2404 0.0900, 0.05640, -1.3526 0.0571, 0.04390, -1.5361 0.0283, 0.02940, -1.5771 0.0142, 0.01970, -1.3590 0.0081, 0.01410, -1.1743 0.0026, 0.00780, -0.8923 0.0000, 0.00000, -0.9211 0.0037, -0.00840, -0.9345 0.0112, -0.01420, -0.9410 0.0191, -0.01930, -0.9490 0.0397, -0.03030, -0.9380 0.0706, -0.04420, -0.9724 0.1037, -0.05710, -0.9776 0.1384, -0.06890, -0.9281 0.1741, -0.07950, -0.9434 0.2102, -0.08660, -1.0110 0.2472, -0.09640, -0.9858 0.2844, -0.10270, -1.0115 0.3225, -0.10690, -0.9533 0.3608, -0.10890, -1.0040 0.3991, -0.10830, -0.9759 0.4373, -0.10510, -1.0026 0.4757, -0.09890, -1.0030 0.5137, -0.09070, -1.0089 0.5694, -0.07640, -0.9666 0.5777, -0.04660, -0.7313 15 Flap element taps 1.0000, 0.00130, -0.9262 0.9365, 0.01390, 0.9873 0.8333, 0.03280, 0.7821 0.7436, 0.04930, 0.6190 0.7049, 0.05670, 0.5594 0.6662, 0.06410, 0.4064 0.6522, 0.01390, -0.7373 0.5969, -0.00020, -0.8211 0.6000, -0.03020, -1.0809 0.6324, -0.04540, -1.0084 0.6667, -0.04880, -1.0056 0.7046, -0.04110, -0.9673 0.7429, -0.03210, -0.9790 0.8333, -0.01400, -0.9686 0.9311, -0.00120, -0.9274 --------- Run Conditions: vel=100.3 ft/s Re=0.905x10^6 AOA=240.03 Flap deflection=0.00 Totals: Cl=0.7210 Cdp=1.6999 Cm(c/4)=0.5880 Cs=0.2246 Ch=0.8135 Main component: Cl=0.3754 Cdp=0.9461 Cm=0.3814 Flap component: Cl=0.3456 Cdp=0.7538 Cm=0.6647 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -1.7500 0.6175, -0.04610, -1.7168 0.5775, -0.01750, -1.4475 0.6274, 0.07170, 0.9249 0.5694, 0.08320, 0.8890 0.5112, 0.09090, 0.7140 0.4731, 0.09830, 0.5974 0.4349, 0.10070, 0.4752 0.3960, 0.10120, 0.2559 0.3566, 0.10020, 0.2705 0.3172, 0.09790, 0.1550 0.2778, 0.09440, 0.0046 0.2393, 0.08960, -0.1814 0.2056, 0.08360, -0.4972 0.1633, 0.07610, -0.5770 0.1261, 0.06710, -0.8992 0.0900, 0.05640, -1.1390 0.0571, 0.04390, -1.5468 0.0283, 0.02940, -1.7439 0.0142, 0.01970, -1.6494 0.0081, 0.01410, -1.7454 0.0026, 0.00780, -1.5653 0.0000, 0.00000, -1.6275 0.0037, -0.00840, -1.6592 0.0112, -0.01420, -1.6750 0.0191, -0.01930, -1.6863 0.0397, -0.03030, -1.6999 0.0706, -0.04420, -1.7944 0.1037, -0.05710, -1.8311 0.1384, -0.06890, -1.7232 0.1741, -0.07950, -1.7558 0.2102, -0.08660, -1.8994 0.2472, -0.09640, -1.8424 0.2844, -0.10270, -1.9010 0.3225, -0.10690, -1.7942 0.3608, -0.10890, -1.8965 0.3991, -0.10830, -1.8485 0.4373, -0.10510, -1.9209 0.4757, -0.09890, -1.9082 0.5137, -0.09070, -1.8987 0.5694, -0.07640, -1.7862 0.5777, -0.04660, -1.4178 15 Flap element taps 1.0000, 0.00130, -1.5496 0.9365, 0.01390, 0.8005 0.8333, 0.03280, 0.9841 0.7436, 0.04930, 0.9901 0.7049, 0.05670, 0.9711 0.6662, 0.06410, 0.9301 0.6522, 0.01390, -1.4767 0.5969, -0.00020, -1.6071 0.6000, -0.03020, -1.7994 0.6324, -0.04540, -1.7856 0.6667, -0.04880, -1.7944 0.7046, -0.04110, -1.7399 0.7429, -0.03210, -1.7478 0.8333, -0.01400, -1.7012 0.9311, -0.00120, -1.5857 --------- Run Conditions: vel=105.2 ft/s Re=0.947x10^6 AOA=269.09 Flap deflection=0.00 Totals: Cl=-0.1251 Cdp=2.2100 Cm(c/4)=0.5756 Cs=0.1602 Ch=0.7425 Main component: Cl=-0.0805 Cdp=1.4178 Cm=0.4954 Flap component: Cl=-0.0446 Cdp=0.7922 Cm=0.6321 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -1.9393 0.6175, -0.04610, -1.8473 0.5775, -0.01750, -1.5543 0.6274, 0.07170, 0.9601 0.5694, 0.08320, 1.0411 0.5112, 0.09090, 1.0095 0.4731, 0.09830, 1.0018 0.4349, 0.10070, 0.9731 0.3960, 0.10120, 0.7920 0.3566, 0.10020, 0.9078 0.3172, 0.09790, 0.8458 0.2778, 0.09440, 0.7660 0.2393, 0.08960, 0.6350 0.2056, 0.08360, 0.3476 0.1633, 0.07610, 0.3254 0.1261, 0.06710, -0.0125 0.0900, 0.05640, -0.2861 0.0571, 0.04390, -0.8591 0.0283, 0.02940, -1.5367 0.0142, 0.01970, -1.9398 0.0081, 0.01410, -1.9939 0.0026, 0.00780, -1.6851 0.0000, 0.00000, -1.7356 0.0037, -0.00840, -1.7689 0.0112, -0.01420, -1.7914 0.0191, -0.01930, -1.7997 0.0397, -0.03030, -1.7906 0.0706, -0.04420, -1.8823 0.1037, -0.05710, -1.9263 0.1384, -0.06890, -1.8238 0.1741, -0.07950, -1.8836 0.2102, -0.08660, -2.0522 0.2472, -0.09640, -1.9835 0.2844, -0.10270, -2.0508 0.3225, -0.10690, -1.9222 0.3608, -0.10890, -2.0106 0.3991, -0.10830, -1.9283 0.4373, -0.10510, -1.9900 0.4757, -0.09890, -1.9778 0.5137, -0.09070, -2.0073 0.5694, -0.07640, -1.9235 0.5777, -0.04660, -1.5559 15 Flap element taps 1.0000, 0.00130, -1.7628 0.9365, 0.01390, 0.1778 0.8333, 0.03280, 0.6341 0.7436, 0.04930, 0.8202 0.7049, 0.05670, 0.8726 0.6662, 0.06410, 0.8939 0.6522, 0.01390, -1.5887 0.5969, -0.00020, -1.6723 0.6000, -0.03020, -1.9217 0.6324, -0.04540, -1.9385 0.6667, -0.04880, -1.9504 0.7046, -0.04110, -1.9077 0.7429, -0.03210, -1.9440 0.8333, -0.01400, -1.9257 0.9311, -0.00120, -1.8140