S809 UNVENTED AILERON, CLEAN, CHORD = 18 IN --------- Run Conditions: vel=223.8 ft/s Re=1.994x10^6 AOA=-6.08 Flap deflection=0.00 Totals: Cl=-0.5364 Cdp=0.0188 Cm(c/4)=0.0048 Cs=0.0381 Ch=0.0432 Main component: Cl=-0.4908 Cdp=0.0279 Cm=0.1036 Flap component: Cl=-0.0456 Cdp=-0.0090 Cm=0.0351 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.2335 0.6175, -0.04610, -0.2015 0.5775, -0.01750, -0.1620 0.6274, 0.07170, -0.0669 0.5694, 0.08320, -0.1419 0.5112, 0.09090, -0.3800 0.4731, 0.09830, -0.4508 0.4349, 0.10070, -0.4392 0.3960, 0.10120, -0.3695 0.3566, 0.10020, -0.3052 0.3172, 0.09790, -0.2380 0.2778, 0.09440, -0.1860 0.2393, 0.08960, -0.1286 0.2056, 0.08360, -0.0552 0.1633, 0.07610, 0.0524 0.1261, 0.06710, 0.1807 0.0900, 0.05640, 0.3368 0.0571, 0.04390, 0.5471 0.0283, 0.02940, 0.8135 0.0142, 0.01970, 0.9856 0.0081, 0.01410, 1.0054 0.0026, 0.00780, 0.7345 0.0000, 0.00000, -0.4687 0.0037, -0.00840, -1.5411 0.0112, -0.01420, -1.2903 0.0191, -0.01930, -1.1081 0.0397, -0.03030, -0.8888 0.0706, -0.04420, -0.8320 0.1037, -0.05710, -0.8821 0.1384, -0.06890, -0.9281 0.1741, -0.07950, -0.9683 0.2102, -0.08660, -1.0405 0.2472, -0.09640, -1.1261 0.2844, -0.10270, -1.1484 0.3225, -0.10690, -1.1566 0.3608, -0.10890, -1.1409 0.3991, -0.10830, -1.0565 0.4373, -0.10510, -0.9203 0.4757, -0.09890, -0.6673 0.5137, -0.09070, -0.4502 0.5694, -0.07640, -0.2718 0.5777, -0.04660, -0.1600 15 Flap element taps 1.0000, 0.00130, 0.0474 0.9365, 0.01390, 0.0608 0.8333, 0.03280, 0.0179 0.7436, 0.04930, -0.0235 0.7049, 0.05670, -0.0215 0.6662, 0.06410, -0.2101 0.6522, 0.01390, -0.1600 0.5969, -0.00020, -0.1699 0.6000, -0.03020, -0.2103 0.6324, -0.04540, -0.2103 0.6667, -0.04880, -0.2098 0.7046, -0.04110, -0.2077 0.7429, -0.03210, -0.2013 0.8333, -0.01400, -0.1532 0.9311, -0.00120, -0.0239 Wake drag found for this condition, Cdw=0.0382 --------- Run Conditions: vel=225.9 ft/s Re=1.998x10^6 AOA=0.06 Flap deflection=0.00 Totals: Cl=0.0775 Cdp=0.0042 Cm(c/4)=-0.0328 Cs=-0.0041 Ch=-0.0579 Main component: Cl=0.0105 Cdp=0.0291 Cm=0.0022 Flap component: Cl=0.0670 Cdp=-0.0249 Cm=-0.0544 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.1468 0.6175, -0.04610, -0.1056 0.5775, -0.01750, -0.1083 0.6274, 0.07170, -0.1933 0.5694, 0.08320, -0.2944 0.5112, 0.09090, -0.6481 0.4731, 0.09830, -0.7125 0.4349, 0.10070, -0.7452 0.3960, 0.10120, -0.7065 0.3566, 0.10020, -0.6670 0.3172, 0.09790, -0.6299 0.2778, 0.09440, -0.6135 0.2393, 0.08960, -0.5980 0.2056, 0.08360, -0.5706 0.1633, 0.07610, -0.5071 0.1261, 0.06710, -0.4312 0.0900, 0.05640, -0.3405 0.0571, 0.04390, -0.2041 0.0283, 0.02940, 0.0105 0.0142, 0.01970, 0.2688 0.0081, 0.01410, 0.4501 0.0026, 0.00780, 0.7365 0.0000, 0.00000, 1.0139 0.0037, -0.00840, 0.6934 0.0112, -0.01420, 0.4408 0.0191, -0.01930, 0.3230 0.0397, -0.03030, 0.1600 0.0706, -0.04420, -0.0180 0.1037, -0.05710, -0.1800 0.1384, -0.06890, -0.3051 0.1741, -0.07950, -0.4263 0.2102, -0.08660, -0.5530 0.2472, -0.09640, -0.6816 0.2844, -0.10270, -0.7666 0.3225, -0.10690, -0.8395 0.3608, -0.10890, -0.8895 0.3991, -0.10830, -0.8906 0.4373, -0.10510, -0.8364 0.4757, -0.09890, -0.7590 0.5137, -0.09070, -0.4572 0.5694, -0.07640, -0.2732 0.5777, -0.04660, -0.1079 15 Flap element taps 1.0000, 0.00130, 0.1947 0.9365, 0.01390, 0.0981 0.8333, 0.03280, -0.0107 0.7436, 0.04930, -0.0952 0.7049, 0.05670, -0.1095 0.6662, 0.06410, -0.3277 0.6522, 0.01390, -0.1060 0.5969, -0.00020, -0.1043 0.6000, -0.03020, -0.1056 0.6324, -0.04540, -0.1070 0.6667, -0.04880, -0.0883 0.7046, -0.04110, 0.0891 0.7429, -0.03210, 0.1330 0.8333, -0.01400, 0.2243 0.9311, -0.00120, 0.2856 Wake drag found for this condition, Cdw=0.0075 --------- Run Conditions: vel=226.2 ft/s Re=1.996x10^6 AOA=3.10 Flap deflection=0.00 Totals: Cl=0.4297 Cdp=0.0079 Cm(c/4)=-0.0405 Cs=0.0154 Ch=-0.0767 Main component: Cl=0.3348 Cdp=0.0278 Cm=-0.0730 Flap component: Cl=0.0950 Cdp=-0.0199 Cm=-0.0748 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.0863 0.6175, -0.04610, -0.0808 0.5775, -0.01750, -0.0851 0.6274, 0.07170, -0.2716 0.5694, 0.08320, -0.4019 0.5112, 0.09090, -0.8232 0.4731, 0.09830, -0.8708 0.4349, 0.10070, -0.9223 0.3960, 0.10120, -0.9022 0.3566, 0.10020, -0.8796 0.3172, 0.09790, -0.8611 0.2778, 0.09440, -0.8677 0.2393, 0.08960, -0.8797 0.2056, 0.08360, -0.8844 0.1633, 0.07610, -0.8574 0.1261, 0.06710, -0.8258 0.0900, 0.05640, -0.7980 0.0571, 0.04390, -0.7580 0.0283, 0.02940, -0.6768 0.0142, 0.01970, -0.5337 0.0081, 0.01410, -0.4208 0.0026, 0.00780, -0.1097 0.0000, 0.00000, 0.4990 0.0037, -0.00840, 1.0120 0.0112, -0.01420, 0.8923 0.0191, -0.01930, 0.7710 0.0397, -0.03030, 0.5628 0.0706, -0.04420, 0.3466 0.1037, -0.05710, 0.1633 0.1384, -0.06890, 0.0189 0.1741, -0.07950, -0.1189 0.2102, -0.08660, -0.2603 0.2472, -0.09640, -0.3987 0.2844, -0.10270, -0.5000 0.3225, -0.10690, -0.5879 0.3608, -0.10890, -0.6559 0.3991, -0.10830, -0.6777 0.4373, -0.10510, -0.6510 0.4757, -0.09890, -0.5689 0.5137, -0.09070, -0.3790 0.5694, -0.07640, -0.1835 0.5777, -0.04660, -0.0850 15 Flap element taps 1.0000, 0.00130, 0.1939 0.9365, 0.01390, 0.0859 0.8333, 0.03280, -0.0423 0.7436, 0.04930, -0.1442 0.7049, 0.05670, -0.1684 0.6662, 0.06410, -0.3958 0.6522, 0.01390, -0.0837 0.5969, -0.00020, -0.0827 0.6000, -0.03020, -0.0830 0.6324, -0.04540, -0.0842 0.6667, -0.04880, 0.0412 0.7046, -0.04110, 0.1532 0.7429, -0.03210, 0.1848 0.8333, -0.01400, 0.2593 0.9311, -0.00120, 0.3087 Wake drag found for this condition, Cdw=0.0088 --------- Run Conditions: vel=227.6 ft/s Re=2.003x10^6 AOA=6.10 Flap deflection=0.00 Totals: Cl=0.7266 Cdp=0.0155 Cm(c/4)=-0.0421 Cs=0.0618 Ch=-0.0887 Main component: Cl=0.6076 Cdp=0.0249 Cm=-0.1312 Flap component: Cl=0.1190 Cdp=-0.0094 Cm=-0.0919 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.0386 0.6175, -0.04610, -0.0460 0.5775, -0.01750, -0.0538 0.6274, 0.07170, -0.3415 0.5694, 0.08320, -0.5164 0.5112, 0.09090, -0.8017 0.4731, 0.09830, -0.9791 0.4349, 0.10070, -1.0414 0.3960, 0.10120, -1.0319 0.3566, 0.10020, -1.0245 0.3172, 0.09790, -1.0305 0.2778, 0.09440, -1.0719 0.2393, 0.08960, -1.1296 0.2056, 0.08360, -1.1736 0.1633, 0.07610, -1.1919 0.1261, 0.06710, -1.2134 0.0900, 0.05640, -1.2638 0.0571, 0.04390, -1.3489 0.0283, 0.02940, -1.4555 0.0142, 0.01970, -1.5280 0.0081, 0.01410, -1.5779 0.0026, 0.00780, -1.4237 0.0000, 0.00000, -0.9498 0.0037, -0.00840, 0.8496 0.0112, -0.01420, 1.0096 0.0191, -0.01930, 0.9751 0.0397, -0.03030, 0.8174 0.0706, -0.04420, 0.6109 0.1037, -0.05710, 0.4280 0.1384, -0.06890, 0.2757 0.1741, -0.07950, 0.1319 0.2102, -0.08660, -0.0155 0.2472, -0.09640, -0.1595 0.2844, -0.10270, -0.2718 0.3225, -0.10690, -0.3717 0.3608, -0.10890, -0.4527 0.3991, -0.10830, -0.4929 0.4373, -0.10510, -0.4908 0.4757, -0.09890, -0.4132 0.5137, -0.09070, -0.3589 0.5694, -0.07640, -0.1062 0.5777, -0.04660, -0.0499 15 Flap element taps 1.0000, 0.00130, 0.1629 0.9365, 0.01390, 0.0784 0.8333, 0.03280, -0.0616 0.7436, 0.04930, -0.1821 0.7049, 0.05670, -0.2260 0.6662, 0.06410, -0.3681 0.6522, 0.01390, -0.0506 0.5969, -0.00020, -0.0539 0.6000, -0.03020, -0.0513 0.6324, -0.04540, -0.0514 0.6667, -0.04880, 0.3475 0.7046, -0.04110, 0.1952 0.7429, -0.03210, 0.2226 0.8333, -0.01400, 0.2804 0.9311, -0.00120, 0.3130 Wake drag found for this condition, Cdw=0.0107 --------- Run Conditions: vel=227.6 ft/s Re=1.991x10^6 AOA=9.06 Flap deflection=0.00 Totals: Cl=0.9386 Cdp=0.0295 Cm(c/4)=-0.0393 Cs=0.1186 Ch=-0.1009 Main component: Cl=0.8063 Cdp=0.0254 Cm=-0.1694 Flap component: Cl=0.1323 Cdp=0.0042 Cm=-0.1027 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.0146 0.6175, -0.04610, -0.0286 0.5775, -0.01750, -0.0399 0.6274, 0.07170, -0.3485 0.5694, 0.08320, -0.5036 0.5112, 0.09090, -0.7865 0.4731, 0.09830, -0.9839 0.4349, 0.10070, -1.0820 0.3960, 0.10120, -1.1069 0.3566, 0.10020, -1.1331 0.3172, 0.09790, -1.1585 0.2778, 0.09440, -1.2136 0.2393, 0.08960, -1.2954 0.2056, 0.08360, -1.3738 0.1633, 0.07610, -1.4354 0.1261, 0.06710, -1.5053 0.0900, 0.05640, -1.6416 0.0571, 0.04390, -1.8449 0.0283, 0.02940, -2.1518 0.0142, 0.01970, -2.5066 0.0081, 0.01410, -2.7865 0.0026, 0.00780, -2.8942 0.0000, 0.00000, -2.8326 0.0037, -0.00840, 0.3802 0.0112, -0.01420, 0.9368 0.0191, -0.01930, 1.0088 0.0397, -0.03030, 0.9495 0.0706, -0.04420, 0.7806 0.1037, -0.05710, 0.6111 0.1384, -0.06890, 0.4589 0.1741, -0.07950, 0.3147 0.2102, -0.08660, 0.1654 0.2472, -0.09640, 0.0175 0.2844, -0.10270, -0.1026 0.3225, -0.10690, -0.2139 0.3608, -0.10890, -0.3058 0.3991, -0.10830, -0.3619 0.4373, -0.10510, -0.3796 0.4757, -0.09890, -0.3146 0.5137, -0.09070, -0.2637 0.5694, -0.07640, -0.0549 0.5777, -0.04660, -0.0330 15 Flap element taps 1.0000, 0.00130, 0.0359 0.9365, 0.01390, -0.0104 0.8333, 0.03280, -0.0950 0.7436, 0.04930, -0.1889 0.7049, 0.05670, -0.2361 0.6662, 0.06410, -0.3096 0.6522, 0.01390, -0.0363 0.5969, -0.00020, -0.0422 0.6000, -0.03020, -0.0382 0.6324, -0.04540, -0.0363 0.6667, -0.04880, 0.5471 0.7046, -0.04110, 0.2077 0.7429, -0.03210, 0.2315 0.8333, -0.01400, 0.2725 0.9311, -0.00120, 0.2768 Wake drag found for this condition, Cdw=0.0218 --------- Run Conditions: vel=230.7 ft/s Re=2.015x10^6 AOA=12.09 Flap deflection=0.00 Totals: Cl=1.0624 Cdp=0.0585 Cm(c/4)=-0.0468 Cs=0.1653 Ch=-0.1532 Main component: Cl=0.8895 Cdp=0.0272 Cm=-0.1702 Flap component: Cl=0.1729 Cdp=0.0314 Cm=-0.1394 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.0173 0.6175, -0.04610, -0.0441 0.5775, -0.01750, -0.0578 0.6274, 0.07170, -0.3497 0.5694, 0.08320, -0.3835 0.5112, 0.09090, -0.5446 0.4731, 0.09830, -0.7566 0.4349, 0.10070, -0.9161 0.3960, 0.10120, -0.9978 0.3566, 0.10020, -1.0710 0.3172, 0.09790, -1.1345 0.2778, 0.09440, -1.2250 0.2393, 0.08960, -1.3411 0.2056, 0.08360, -1.4576 0.1633, 0.07610, -1.5690 0.1261, 0.06710, -1.6956 0.0900, 0.05640, -1.9103 0.0571, 0.04390, -2.2379 0.0283, 0.02940, -2.7435 0.0142, 0.01970, -3.2583 0.0081, 0.01410, -3.9835 0.0026, 0.00780, -4.2305 0.0000, 0.00000, -4.7577 0.0037, -0.00840, -0.2189 0.0112, -0.01420, 0.7540 0.0191, -0.01930, 0.9600 0.0397, -0.03030, 1.0039 0.0706, -0.04420, 0.8857 0.1037, -0.05710, 0.7362 0.1384, -0.06890, 0.5883 0.1741, -0.07950, 0.4463 0.2102, -0.08660, 0.2984 0.2472, -0.09640, 0.1469 0.2844, -0.10270, 0.0206 0.3225, -0.10690, -0.1015 0.3608, -0.10890, -0.2037 0.3991, -0.10830, -0.2753 0.4373, -0.10510, -0.3091 0.4757, -0.09890, -0.2593 0.5137, -0.09070, -0.2168 0.5694, -0.07640, -0.0379 0.5777, -0.04660, -0.0475 15 Flap element taps 1.0000, 0.00130, -0.1754 0.9365, 0.01390, -0.2795 0.8333, 0.03280, -0.3001 0.7436, 0.04930, -0.3187 0.7049, 0.05670, -0.3278 0.6662, 0.06410, -0.3276 0.6522, 0.01390, -0.0546 0.5969, -0.00020, -0.0621 0.6000, -0.03020, -0.0566 0.6324, -0.04540, -0.0548 0.6667, -0.04880, 0.6141 0.7046, -0.04110, 0.1931 0.7429, -0.03210, 0.2109 0.8333, -0.01400, 0.2319 0.9311, -0.00120, 0.1977 --------- Run Conditions: vel=229.8 ft/s Re=1.998x10^6 AOA=15.08 Flap deflection=0.00 Totals: Cl=1.0885 Cdp=0.0917 Cm(c/4)=-0.0473 Cs=0.1947 Ch=-0.1808 Main component: Cl=0.8936 Cdp=0.0379 Cm=-0.1552 Flap component: Cl=0.1949 Cdp=0.0538 Cm=-0.1608 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.0296 0.6175, -0.04610, -0.0663 0.5775, -0.01750, -0.0826 0.6274, 0.07170, -0.4217 0.5694, 0.08320, -0.4182 0.5112, 0.09090, -0.4216 0.4731, 0.09830, -0.4651 0.4349, 0.10070, -0.5761 0.3960, 0.10120, -0.7049 0.3566, 0.10020, -0.8414 0.3172, 0.09790, -0.9591 0.2778, 0.09440, -1.0931 0.2393, 0.08960, -1.2485 0.2056, 0.08360, -1.4057 0.1633, 0.07610, -1.5705 0.1261, 0.06710, -1.7529 0.0900, 0.05640, -2.0374 0.0571, 0.04390, -2.4706 0.0283, 0.02940, -3.1564 0.0142, 0.01970, -3.8877 0.0081, 0.01410, -4.7557 0.0026, 0.00780, -5.3499 0.0000, 0.00000, -6.4921 0.0037, -0.00840, -0.8129 0.0112, -0.01420, 0.5321 0.0191, -0.01930, 0.8643 0.0397, -0.03030, 1.0113 0.0706, -0.04420, 0.9448 0.1037, -0.05710, 0.8174 0.1384, -0.06890, 0.6762 0.1741, -0.07950, 0.5386 0.2102, -0.08660, 0.3948 0.2472, -0.09640, 0.2415 0.2844, -0.10270, 0.1111 0.3225, -0.10690, -0.0200 0.3608, -0.10890, -0.1298 0.3991, -0.10830, -0.2149 0.4373, -0.10510, -0.2617 0.4757, -0.09890, -0.2255 0.5137, -0.09070, -0.1968 0.5694, -0.07640, -0.0732 0.5777, -0.04660, -0.0719 15 Flap element taps 1.0000, 0.00130, -0.3564 0.9365, 0.01390, -0.4460 0.8333, 0.03280, -0.4374 0.7436, 0.04930, -0.4358 0.7049, 0.05670, -0.4280 0.6662, 0.06410, -0.4080 0.6522, 0.01390, -0.0776 0.5969, -0.00020, -0.0874 0.6000, -0.03020, -0.0807 0.6324, -0.04540, -0.0799 0.6667, -0.04880, 0.6332 0.7046, -0.04110, 0.1691 0.7429, -0.03210, 0.1815 0.8333, -0.01400, 0.1832 0.9311, -0.00120, 0.1132 --------- Run Conditions: vel=230.4 ft/s Re=1.994x10^6 AOA=18.07 Flap deflection=0.00 Totals: Cl=0.9476 Cdp=0.1612 Cm(c/4)=-0.0676 Cs=0.1407 Ch=-0.2012 Main component: Cl=0.7321 Cdp=0.0870 Cm=-0.1247 Flap component: Cl=0.2155 Cdp=0.0742 Cm=-0.1807 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.0888 0.6175, -0.04610, -0.1382 0.5775, -0.01750, -0.1566 0.6274, 0.07170, -0.5608 0.5694, 0.08320, -0.5555 0.5112, 0.09090, -0.5532 0.4731, 0.09830, -0.5445 0.4349, 0.10070, -0.5472 0.3960, 0.10120, -0.5451 0.3566, 0.10020, -0.5618 0.3172, 0.09790, -0.5718 0.2778, 0.09440, -0.6062 0.2393, 0.08960, -0.6898 0.2056, 0.08360, -0.8447 0.1633, 0.07610, -1.0741 0.1261, 0.06710, -1.3391 0.0900, 0.05640, -1.6856 0.0571, 0.04390, -2.1702 0.0283, 0.02940, -2.9091 0.0142, 0.01970, -3.6857 0.0081, 0.01410, -4.5307 0.0026, 0.00780, -5.2587 0.0000, 0.00000, -6.5309 0.0037, -0.00840, -0.8905 0.0112, -0.01420, 0.4899 0.0191, -0.01930, 0.8405 0.0397, -0.03030, 1.0087 0.0706, -0.04420, 0.9554 0.1037, -0.05710, 0.8349 0.1384, -0.06890, 0.6926 0.1741, -0.07950, 0.5554 0.2102, -0.08660, 0.4117 0.2472, -0.09640, 0.2528 0.2844, -0.10270, 0.1168 0.3225, -0.10690, -0.0241 0.3608, -0.10890, -0.1417 0.3991, -0.10830, -0.2384 0.4373, -0.10510, -0.2942 0.4757, -0.09890, -0.2642 0.5137, -0.09070, -0.2418 0.5694, -0.07640, -0.1420 0.5777, -0.04660, -0.1412 15 Flap element taps 1.0000, 0.00130, -0.5372 0.9365, 0.01390, -0.5811 0.8333, 0.03280, -0.5908 0.7436, 0.04930, -0.5899 0.7049, 0.05670, -0.5828 0.6662, 0.06410, -0.5548 0.6522, 0.01390, -0.1539 0.5969, -0.00020, -0.1661 0.6000, -0.03020, -0.1568 0.6324, -0.04540, -0.1636 0.6667, -0.04880, 0.6523 0.7046, -0.04110, 0.1117 0.7429, -0.03210, 0.1221 0.8333, -0.01400, 0.1111 0.9311, -0.00120, 0.0155 --------- Run Conditions: vel=231.6 ft/s Re=1.998x10^6 AOA=20.06 Flap deflection=0.00 Totals: Cl=0.6531 Cdp=0.3235 Cm(c/4)=-0.1172 Cs=-0.0799 Ch=-0.2118 Main component: Cl=0.4251 Cdp=0.2384 Cm=-0.1058 Flap component: Cl=0.2279 Cdp=0.0852 Cm=-0.1926 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.2015 0.6175, -0.04610, -0.2567 0.5775, -0.01750, -0.2775 0.6274, 0.07170, -0.7229 0.5694, 0.08320, -0.7269 0.5112, 0.09090, -0.7264 0.4731, 0.09830, -0.7225 0.4349, 0.10070, -0.7164 0.3960, 0.10120, -0.7069 0.3566, 0.10020, -0.7166 0.3172, 0.09790, -0.7073 0.2778, 0.09440, -0.7004 0.2393, 0.08960, -0.7007 0.2056, 0.08360, -0.6949 0.1633, 0.07610, -0.7011 0.1261, 0.06710, -0.6944 0.0900, 0.05640, -0.6959 0.0571, 0.04390, -0.6971 0.0283, 0.02940, -0.6965 0.0142, 0.01970, -0.7019 0.0081, 0.01410, -0.7096 0.0026, 0.00780, -0.7172 0.0000, 0.00000, -1.0907 0.0037, -0.00840, 0.4481 0.0112, -0.01420, 0.9055 0.0191, -0.01930, 0.9956 0.0397, -0.03030, 0.9867 0.0706, -0.04420, 0.8708 0.1037, -0.05710, 0.7291 0.1384, -0.06890, 0.5767 0.1741, -0.07950, 0.4345 0.2102, -0.08660, 0.2880 0.2472, -0.09640, 0.1215 0.2844, -0.10270, -0.0169 0.3225, -0.10690, -0.1646 0.3608, -0.10890, -0.2862 0.3991, -0.10830, -0.3863 0.4373, -0.10510, -0.4397 0.4757, -0.09890, -0.4013 0.5137, -0.09070, -0.3710 0.5694, -0.07640, -0.2530 0.5777, -0.04660, -0.2605 15 Flap element taps 1.0000, 0.00130, -0.6332 0.9365, 0.01390, -0.6863 0.8333, 0.03280, -0.7284 0.7436, 0.04930, -0.7343 0.7049, 0.05670, -0.7314 0.6662, 0.06410, -0.6961 0.6522, 0.01390, -0.2755 0.5969, -0.00020, -0.2884 0.6000, -0.03020, -0.2788 0.6324, -0.04540, -0.2872 0.6667, -0.04880, 0.6126 0.7046, -0.04110, 0.0231 0.7429, -0.03210, 0.0338 0.8333, -0.01400, 0.0238 0.9311, -0.00120, -0.0740 --------- Run Conditions: vel=230.3 ft/s Re=1.979x10^6 AOA=24.06 Flap deflection=0.00 Totals: Cl=0.7397 Cdp=0.4245 Cm(c/4)=-0.1347 Cs=-0.0861 Ch=-0.2332 Main component: Cl=0.4984 Cdp=0.3110 Cm=-0.1359 Flap component: Cl=0.2413 Cdp=0.1136 Cm=-0.2110 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.1964 0.6175, -0.04610, -0.2709 0.5775, -0.01750, -0.2992 0.6274, 0.07170, -0.8211 0.5694, 0.08320, -0.8296 0.5112, 0.09090, -0.8286 0.4731, 0.09830, -0.8273 0.4349, 0.10070, -0.8223 0.3960, 0.10120, -0.8112 0.3566, 0.10020, -0.8225 0.3172, 0.09790, -0.8155 0.2778, 0.09440, -0.8101 0.2393, 0.08960, -0.8088 0.2056, 0.08360, -0.8036 0.1633, 0.07610, -0.8129 0.1261, 0.06710, -0.8063 0.0900, 0.05640, -0.8060 0.0571, 0.04390, -0.8084 0.0283, 0.02940, -0.8155 0.0142, 0.01970, -0.8257 0.0081, 0.01410, -0.8323 0.0026, 0.00780, -0.8205 0.0000, 0.00000, -0.9230 0.0037, -0.00840, 0.3350 0.0112, -0.01420, 0.8476 0.0191, -0.01930, 0.9725 0.0397, -0.03030, 1.0048 0.0706, -0.04420, 0.9216 0.1037, -0.05710, 0.7996 0.1384, -0.06890, 0.6576 0.1741, -0.07950, 0.5236 0.2102, -0.08660, 0.3838 0.2472, -0.09640, 0.2194 0.2844, -0.10270, 0.0799 0.3225, -0.10690, -0.0731 0.3608, -0.10890, -0.1995 0.3991, -0.10830, -0.3107 0.4373, -0.10510, -0.3765 0.4757, -0.09890, -0.3524 0.5137, -0.09070, -0.3349 0.5694, -0.07640, -0.2436 0.5777, -0.04660, -0.2773 15 Flap element taps 1.0000, 0.00130, -0.7745 0.9365, 0.01390, -0.8033 0.8333, 0.03280, -0.8209 0.7436, 0.04930, -0.8263 0.7049, 0.05670, -0.8225 0.6662, 0.06410, -0.7839 0.6522, 0.01390, -0.2954 0.5969, -0.00020, -0.3122 0.6000, -0.03020, -0.2977 0.6324, -0.04540, -0.3237 0.6667, -0.04880, 0.6612 0.7046, -0.04110, 0.0142 0.7429, -0.03210, 0.0226 0.8333, -0.01400, -0.0043 0.9311, -0.00120, -0.1279 --------- Run Conditions: vel=232.3 ft/s Re=1.986x10^6 AOA=27.00 Flap deflection=0.00 Totals: Cl=0.9106 Cdp=0.5642 Cm(c/4)=-0.1761 Cs=-0.0893 Ch=-0.2864 Main component: Cl=0.6290 Cdp=0.4089 Cm=-0.1881 Flap component: Cl=0.2816 Cdp=0.1553 Cm=-0.2549 Surface Pressure Data 42 Main element taps 0.6276, -0.06090, -0.1806 0.6175, -0.04610, -0.2968 0.5775, -0.01750, -0.3250 0.6274, 0.07170, -1.0172 0.5694, 0.08320, -1.0276 0.5112, 0.09090, -1.0288 0.4731, 0.09830, -1.0261 0.4349, 0.10070, -1.0206 0.3960, 0.10120, -1.0053 0.3566, 0.10020, -1.0181 0.3172, 0.09790, -1.0093 0.2778, 0.09440, -1.0035 0.2393, 0.08960, -1.0019 0.2056, 0.08360, -0.9918 0.1633, 0.07610, -1.0017 0.1261, 0.06710, -0.9931 0.0900, 0.05640, -0.9970 0.0571, 0.04390, -0.9966 0.0283, 0.02940, -1.0003 0.0142, 0.01970, -1.0060 0.0081, 0.01410, -1.0057 0.0026, 0.00780, -0.9870 0.0000, 0.00000, -1.0316 0.0037, -0.00840, 0.0477 0.0112, -0.01420, 0.7046 0.0191, -0.01930, 0.9002 0.0397, -0.03030, 1.0066 0.0706, -0.04420, 0.9719 0.1037, -0.05710, 0.8794 0.1384, -0.06890, 0.7523 0.1741, -0.07950, 0.6304 0.2102, -0.08660, 0.5024 0.2472, -0.09640, 0.3445 0.2844, -0.10270, 0.2076 0.3225, -0.10690, 0.0532 0.3608, -0.10890, -0.0754 0.3991, -0.10830, -0.1940 0.4373, -0.10510, -0.2705 0.4757, -0.09890, -0.2639 0.5137, -0.09070, -0.2658 0.5694, -0.07640, -0.1898 0.5777, -0.04660, -0.2946 15 Flap element taps 1.0000, 0.00130, -0.9953 0.9365, 0.01390, -1.0058 0.8333, 0.03280, -1.0156 0.7436, 0.04930, -1.0229 0.7049, 0.05670, -1.0224 0.6662, 0.06410, -0.9649 0.6522, 0.01390, -0.3254 0.5969, -0.00020, -0.3449 0.6000, -0.03020, -0.3285 0.6324, -0.04540, -0.4334 0.6667, -0.04880, 0.7202 0.7046, -0.04110, 0.0246 0.7429, -0.03210, 0.0252 0.8333, -0.01400, -0.0175 0.9311, -0.00120, -0.1834 Wake drag found for this condition, Cdw=0.6302