S809 UNVENTED AILERON, LEGR, CHORD = 18 INCHES --------- Run Conditions: vel=210.5 ft/s Re=1.988x10^6 AOA=-6.01 Flap deflection=-90.00 Totals: Cl=-1.7278 Cdp=0.5052 Cm(c/4)=0.1608 Cs=-0.3216 Ch=0.5414 Main component: Cl=-1.7300 Cdp=-0.0392 Cm=0.4493 Flap component: Cl=0.0022 Cdp=0.5444 Cm=0.1543 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.9465 0.6175, -0.04610, -0.9182 0.5841, -0.02440, -0.9203 0.5775, 0.01750, -0.9219 0.5777, 0.04660, -0.9171 0.6274, 0.07170, 0.9399 0.5694, 0.08320, 0.9331 0.5112, 0.09370, 0.9361 0.4731, 0.09830, 0.9335 0.4349, 0.10070, 0.9027 0.3960, 0.10120, 0.8578 0.3566, 0.10020, 0.8386 0.3172, 0.09790, 0.8285 0.2778, 0.09440, 0.8241 0.2393, 0.08960, 0.8362 0.2056, 0.08360, 0.8602 0.1633, 0.07610, 0.8932 0.1261, 0.06710, 0.9430 0.0900, 0.05640, 0.9935 0.0571, 0.04390, 1.0035 0.0283, 0.02940, 0.8089 0.0142, 0.01970, 0.2609 0.0081, 0.01410, -0.4396 0.0026, 0.00780, -1.9691 0.0000, 0.00000, -8.1888 0.0037, -0.00840, -7.8292 0.0112, -0.01420, -5.6043 0.0191, -0.01930, -4.6406 0.0397, -0.03030, -3.4435 0.0706, -0.04420, -2.7853 0.1037, -0.05710, -2.4167 0.1384, -0.06890, -2.2573 0.1741, -0.07950, -2.1478 0.2102, -0.08660, -2.1075 0.2472, -0.09640, -2.0940 0.2844, -0.10270, -2.0180 0.3225, -0.10690, -1.9181 0.3608, -0.10890, -1.7695 0.3991, -0.10830, -1.5474 0.4373, -0.10510, -1.2856 0.4757, -0.09890, -1.1003 0.5137, -0.09070, -1.0082 0.5694, -0.07640, -0.9849 15 Flap element taps 1.0000, 0.00130, -0.8920 0.9365, 0.01390, 0.6461 0.8333, 0.03280, 0.9223 0.7436, 0.04930, 0.9375 0.7049, 0.05670, 0.9351 0.6662, 0.06410, 0.9432 0.6522, 0.01390, -0.9155 0.5969, -0.00020, -0.9313 0.6000, -0.03020, -0.9271 0.6324, -0.04540, -0.9245 0.6667, -0.04880, -0.9168 0.7046, -0.04110, -0.9019 0.7429, -0.03210, -0.9005 0.8333, -0.01400, -0.8981 0.9311, -0.00120, -0.8879 --------- Run Conditions: vel=212.5 ft/s Re=2.006x10^6 AOA=-0.01 Flap deflection=-90.00 Totals: Cl=-1.6441 Cdp=0.4195 Cm(c/4)=0.1873 Cs=-0.4192 Ch=0.5073 Main component: Cl=-1.5942 Cdp=-0.0876 Cm=0.4547 Flap component: Cl=-0.0499 Cdp=0.5071 Cm=0.1437 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8605 0.6175, -0.04610, -0.8202 0.5841, -0.02440, -0.8144 0.5775, 0.01750, -0.8169 0.5777, 0.04660, -0.8130 0.6274, 0.07170, 0.9115 0.5694, 0.08320, 0.8983 0.5112, 0.09370, 0.9054 0.4731, 0.09830, 0.9074 0.4349, 0.10070, 0.8838 0.3960, 0.10120, 0.8417 0.3566, 0.10020, 0.7844 0.3172, 0.09790, 0.7615 0.2778, 0.09440, 0.7432 0.2393, 0.08960, 0.7413 0.2056, 0.08360, 0.7563 0.1633, 0.07610, 0.7796 0.1261, 0.06710, 0.8347 0.0900, 0.05640, 0.9003 0.0571, 0.04390, 0.9842 0.0283, 0.02940, 0.9940 0.0142, 0.01970, 0.7852 0.0081, 0.01410, 0.4472 0.0026, 0.00780, -0.6052 0.0000, 0.00000, -4.4247 0.0037, -0.00840, -5.2830 0.0112, -0.01420, -3.6840 0.0191, -0.01930, -2.8147 0.0397, -0.03030, -2.1791 0.0706, -0.04420, -1.9093 0.1037, -0.05710, -1.7150 0.1384, -0.06890, -1.7982 0.1741, -0.07950, -1.8143 0.2102, -0.08660, -1.8767 0.2472, -0.09640, -1.9866 0.2844, -0.10270, -2.0220 0.3225, -0.10690, -2.0516 0.3608, -0.10890, -2.0451 0.3991, -0.10830, -1.9636 0.4373, -0.10510, -1.7750 0.4757, -0.09890, -1.4906 0.5137, -0.09070, -1.2076 0.5694, -0.07640, -0.9649 15 Flap element taps 1.0000, 0.00130, -0.8132 0.9365, 0.01390, 0.6262 0.8333, 0.03280, 0.9120 0.7436, 0.04930, 0.9033 0.7049, 0.05670, 0.8992 0.6662, 0.06410, 0.9133 0.6522, 0.01390, -0.8124 0.5969, -0.00020, -0.8226 0.6000, -0.03020, -0.8190 0.6324, -0.04540, -0.8178 0.6667, -0.04880, -0.8147 0.7046, -0.04110, -0.8087 0.7429, -0.03210, -0.8099 0.8333, -0.01400, -0.8082 0.9311, -0.00120, -0.8076 --------- Run Conditions: vel=211.2 ft/s Re=1.987x10^6 AOA=3.01 Flap deflection=-90.00 Totals: Cl=-1.6926 Cdp=0.4427 Cm(c/4)=0.2211 Cs=-0.5309 Ch=0.5504 Main component: Cl=-1.6110 Cdp=-0.1031 Cm=0.4830 Flap component: Cl=-0.0815 Cdp=0.5458 Cm=0.1548 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.0541 0.6175, -0.04610, -0.9623 0.5841, -0.02440, -0.9583 0.5775, 0.01750, -0.9595 0.5777, 0.04660, -0.9550 0.6274, 0.07170, 0.8807 0.5694, 0.08320, 0.8651 0.5112, 0.09370, 0.8737 0.4731, 0.09830, 0.8784 0.4349, 0.10070, 0.8691 0.3960, 0.10120, 0.8331 0.3566, 0.10020, 0.7707 0.3172, 0.09790, 0.7344 0.2778, 0.09440, 0.7050 0.2393, 0.08960, 0.6963 0.2056, 0.08360, 0.7068 0.1633, 0.07610, 0.7220 0.1261, 0.06710, 0.7767 0.0900, 0.05640, 0.8398 0.0571, 0.04390, 0.9417 0.0283, 0.02940, 1.0082 0.0142, 0.01970, 0.8994 0.0081, 0.01410, 0.6710 0.0026, 0.00780, -0.2021 0.0000, 0.00000, -3.2296 0.0037, -0.00840, -4.2987 0.0112, -0.01420, -3.0591 0.0191, -0.01930, -2.3206 0.0397, -0.03030, -1.8553 0.0706, -0.04420, -1.6995 0.1037, -0.05710, -1.5525 0.1384, -0.06890, -1.6943 0.1741, -0.07950, -1.7492 0.2102, -0.08660, -1.8453 0.2472, -0.09640, -1.9998 0.2844, -0.10270, -2.0745 0.3225, -0.10690, -2.1520 0.3608, -0.10890, -2.2001 0.3991, -0.10830, -2.1806 0.4373, -0.10510, -2.0572 0.4757, -0.09890, -1.8357 0.5137, -0.09070, -1.5981 0.5694, -0.07640, -1.2603 15 Flap element taps 1.0000, 0.00130, -0.9638 0.9365, 0.01390, 0.5996 0.8333, 0.03280, 0.8990 0.7436, 0.04930, 0.8672 0.7049, 0.05670, 0.8654 0.6662, 0.06410, 0.8848 0.6522, 0.01390, -0.9501 0.5969, -0.00020, -0.9664 0.6000, -0.03020, -0.9617 0.6324, -0.04540, -0.9676 0.6667, -0.04880, -0.9717 0.7046, -0.04110, -0.9665 0.7429, -0.03210, -0.9700 0.8333, -0.01400, -0.9741 0.9311, -0.00120, -0.9645 --------- Run Conditions: vel=209.7 ft/s Re=1.970x10^6 AOA=6.01 Flap deflection=-90.00 Totals: Cl=-1.5782 Cdp=0.4639 Cm(c/4)=0.2379 Cs=-0.6266 Ch=0.5705 Main component: Cl=-1.4652 Cdp=-0.0943 Cm=0.4582 Flap component: Cl=-0.1131 Cdp=0.5583 Cm=0.1599 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.1313 0.6175, -0.04610, -1.0359 0.5841, -0.02440, -1.0388 0.5775, 0.01750, -1.0470 0.5777, 0.04660, -1.0395 0.6274, 0.07170, 0.8364 0.5694, 0.08320, 0.8094 0.5112, 0.09370, 0.8175 0.4731, 0.09830, 0.8268 0.4349, 0.10070, 0.8298 0.3960, 0.10120, 0.8265 0.3566, 0.10020, 0.7581 0.3172, 0.09790, 0.7056 0.2778, 0.09440, 0.6611 0.2393, 0.08960, 0.6358 0.2056, 0.08360, 0.6361 0.1633, 0.07610, 0.6355 0.1261, 0.06710, 0.6831 0.0900, 0.05640, 0.7336 0.0571, 0.04390, 0.8487 0.0283, 0.02940, 0.9862 0.0142, 0.01970, 1.0008 0.0081, 0.01410, 0.9177 0.0026, 0.00780, 0.3021 0.0000, 0.00000, -1.5455 0.0037, -0.00840, -2.7416 0.0112, -0.01420, -2.0334 0.0191, -0.01930, -1.5349 0.0397, -0.03030, -1.2978 0.0706, -0.04420, -1.2823 0.1037, -0.05710, -1.1988 0.1384, -0.06890, -1.3967 0.1741, -0.07950, -1.4908 0.2102, -0.08660, -1.6110 0.2472, -0.09640, -1.7943 0.2844, -0.10270, -1.8972 0.3225, -0.10690, -2.0077 0.3608, -0.10890, -2.0885 0.3991, -0.10830, -2.1074 0.4373, -0.10510, -2.0233 0.4757, -0.09890, -1.8403 0.5137, -0.09070, -1.6289 0.5694, -0.07640, -1.3141 15 Flap element taps 1.0000, 0.00130, -1.0469 0.9365, 0.01390, 0.5821 0.8333, 0.03280, 0.8679 0.7436, 0.04930, 0.8044 0.7049, 0.05670, 0.8139 0.6662, 0.06410, 0.8347 0.6522, 0.01390, -1.0305 0.5969, -0.00020, -1.0480 0.6000, -0.03020, -1.0441 0.6324, -0.04540, -1.0583 0.6667, -0.04880, -1.0708 0.7046, -0.04110, -1.0580 0.7429, -0.03210, -1.0582 0.8333, -0.01400, -1.0645 0.9311, -0.00120, -1.0660 --------- Run Conditions: vel=210.9 ft/s Re=1.980x10^6 AOA=9.02 Flap deflection=-90.00 Totals: Cl=-1.4228 Cdp=0.4776 Cm(c/4)=0.2477 Cs=-0.6947 Ch=0.5775 Main component: Cl=-1.2792 Cdp=-0.0800 Cm=0.4187 Flap component: Cl=-0.1436 Cdp=0.5576 Cm=0.1616 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.1389 0.6175, -0.04610, -1.0888 0.5841, -0.02440, -1.0748 0.5775, 0.01750, -1.0670 0.5777, 0.04660, -1.0612 0.6274, 0.07170, 0.7865 0.5694, 0.08320, 0.7423 0.5112, 0.09370, 0.7600 0.4731, 0.09830, 0.7758 0.4349, 0.10070, 0.7807 0.3960, 0.10120, 0.7924 0.3566, 0.10020, 0.7434 0.3172, 0.09790, 0.6773 0.2778, 0.09440, 0.6119 0.2393, 0.08960, 0.5701 0.2056, 0.08360, 0.5545 0.1633, 0.07610, 0.5322 0.1261, 0.06710, 0.5644 0.0900, 0.05640, 0.5899 0.0571, 0.04390, 0.7004 0.0283, 0.02940, 0.8778 0.0142, 0.01970, 0.9897 0.0081, 0.01410, 1.0202 0.0026, 0.00780, 0.6893 0.0000, 0.00000, -0.1551 0.0037, -0.00840, -1.2982 0.0112, -0.01420, -1.0433 0.0191, -0.01930, -0.7833 0.0397, -0.03030, -0.7433 0.0706, -0.04420, -0.8432 0.1037, -0.05710, -0.8237 0.1384, -0.06890, -1.0643 0.1741, -0.07950, -1.1891 0.2102, -0.08660, -1.3322 0.2472, -0.09640, -1.5375 0.2844, -0.10270, -1.6623 0.3225, -0.10690, -1.8002 0.3608, -0.10890, -1.9048 0.3991, -0.10830, -1.9579 0.4373, -0.10510, -1.9077 0.4757, -0.09890, -1.7612 0.5137, -0.09070, -1.5789 0.5694, -0.07640, -1.3031 15 Flap element taps 1.0000, 0.00130, -1.0788 0.9365, 0.01390, 0.5724 0.8333, 0.03280, 0.8363 0.7436, 0.04930, 0.7452 0.7049, 0.05670, 0.7627 0.6662, 0.06410, 0.7889 0.6522, 0.01390, -1.0781 0.5969, -0.00020, -1.0923 0.6000, -0.03020, -1.0951 0.6324, -0.04540, -1.1074 0.6667, -0.04880, -1.1293 0.7046, -0.04110, -1.1237 0.7429, -0.03210, -1.1251 0.8333, -0.01400, -1.1148 0.9311, -0.00120, -1.1081 --------- Run Conditions: vel=212.4 ft/s Re=1.993x10^6 AOA=12.02 Flap deflection=-90.00 Totals: Cl=-1.2482 Cdp=0.4778 Cm(c/4)=0.2516 Cs=-0.7273 Ch=0.5699 Main component: Cl=-1.0801 Cdp=-0.0594 Cm=0.3735 Flap component: Cl=-0.1681 Cdp=0.5372 Cm=0.1585 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.1461 0.6175, -0.04610, -1.0941 0.5841, -0.02440, -1.1111 0.5775, 0.01750, -1.1157 0.5777, 0.04660, -1.1094 0.6274, 0.07170, 0.7340 0.5694, 0.08320, 0.6809 0.5112, 0.09370, 0.7019 0.4731, 0.09830, 0.7070 0.4349, 0.10070, 0.7126 0.3960, 0.10120, 0.7293 0.3566, 0.10020, 0.6993 0.3172, 0.09790, 0.6426 0.2778, 0.09440, 0.5559 0.2393, 0.08960, 0.4902 0.2056, 0.08360, 0.4541 0.1633, 0.07610, 0.4069 0.1261, 0.06710, 0.4172 0.0900, 0.05640, 0.4270 0.0571, 0.04390, 0.4911 0.0283, 0.02940, 0.6659 0.0142, 0.01970, 0.8170 0.0081, 0.01410, 0.9459 0.0026, 0.00780, 0.8567 0.0000, 0.00000, 0.7137 0.0037, -0.00840, -0.1642 0.0112, -0.01420, -0.2194 0.0191, -0.01930, -0.1475 0.0397, -0.03030, -0.2537 0.0706, -0.04420, -0.4321 0.1037, -0.05710, -0.4699 0.1384, -0.06890, -0.7385 0.1741, -0.07950, -0.8864 0.2102, -0.08660, -1.0440 0.2472, -0.09640, -1.2661 0.2844, -0.10270, -1.4091 0.3225, -0.10690, -1.5700 0.3608, -0.10890, -1.6967 0.3991, -0.10830, -1.7766 0.4373, -0.10510, -1.7567 0.4757, -0.09890, -1.6429 0.5137, -0.09070, -1.5035 0.5694, -0.07640, -1.2545 15 Flap element taps 1.0000, 0.00130, -1.1253 0.9365, 0.01390, 0.5576 0.8333, 0.03280, 0.7857 0.7436, 0.04930, 0.6725 0.7049, 0.05670, 0.6908 0.6662, 0.06410, 0.7242 0.6522, 0.01390, -1.0774 0.5969, -0.00020, -1.1007 0.6000, -0.03020, -1.0883 0.6324, -0.04540, -1.1032 0.6667, -0.04880, -1.1214 0.7046, -0.04110, -1.1206 0.7429, -0.03210, -1.1183 0.8333, -0.01400, -1.1350 0.9311, -0.00120, -1.1297 --------- Run Conditions: vel=211.9 ft/s Re=2.001x10^6 AOA=14.99 Flap deflection=-90.00 Totals: Cl=-1.0599 Cdp=0.4644 Cm(c/4)=0.2493 Cs=-0.7227 Ch=0.5496 Main component: Cl=-0.8720 Cdp=-0.0407 Cm=0.3225 Flap component: Cl=-0.1879 Cdp=0.5051 Cm=0.1528 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.0977 0.6175, -0.04610, -1.0767 0.5841, -0.02440, -1.0907 0.5775, 0.01750, -1.1032 0.5777, 0.04660, -1.0970 0.6274, 0.07170, 0.6630 0.5694, 0.08320, 0.6037 0.5112, 0.09370, 0.6131 0.4731, 0.09830, 0.6209 0.4349, 0.10070, 0.6251 0.3960, 0.10120, 0.6282 0.3566, 0.10020, 0.6270 0.3172, 0.09790, 0.6003 0.2778, 0.09440, 0.5170 0.2393, 0.08960, 0.4216 0.2056, 0.08360, 0.3448 0.1633, 0.07610, 0.2869 0.1261, 0.06710, 0.2559 0.0900, 0.05640, 0.2453 0.0571, 0.04390, 0.2410 0.0283, 0.02940, 0.3659 0.0142, 0.01970, 0.4765 0.0081, 0.01410, 0.6428 0.0026, 0.00780, 0.7623 0.0000, 0.00000, 1.0054 0.0037, -0.00840, 0.5976 0.0112, -0.01420, 0.3722 0.0191, -0.01930, 0.3333 0.0397, -0.03030, 0.1558 0.0706, -0.04420, -0.0724 0.1037, -0.05710, -0.1590 0.1384, -0.06890, -0.4222 0.1741, -0.07950, -0.5893 0.2102, -0.08660, -0.7741 0.2472, -0.09640, -0.9956 0.2844, -0.10270, -1.1588 0.3225, -0.10690, -1.3239 0.3608, -0.10890, -1.4792 0.3991, -0.10830, -1.5676 0.4373, -0.10510, -1.5867 0.4757, -0.09890, -1.4999 0.5137, -0.09070, -1.4096 0.5694, -0.07640, -1.1724 15 Flap element taps 1.0000, 0.00130, -1.1229 0.9365, 0.01390, 0.5469 0.8333, 0.03280, 0.7081 0.7436, 0.04930, 0.5844 0.7049, 0.05670, 0.6060 0.6662, 0.06410, 0.6466 0.6522, 0.01390, -1.0717 0.5969, -0.00020, -1.0915 0.6000, -0.03020, -1.0787 0.6324, -0.04540, -1.0878 0.6667, -0.04880, -1.1096 0.7046, -0.04110, -1.1053 0.7429, -0.03210, -1.1046 0.8333, -0.01400, -1.1227 0.9311, -0.00120, -1.1140 --------- Run Conditions: vel=212.5 ft/s Re=2.002x10^6 AOA=17.99 Flap deflection=-90.00 Totals: Cl=-0.8639 Cdp=0.4597 Cm(c/4)=0.2447 Cs=-0.7041 Ch=0.5299 Main component: Cl=-0.6574 Cdp=-0.0128 Cm=0.2666 Flap component: Cl=-0.2065 Cdp=0.4725 Cm=0.1480 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.0496 0.6175, -0.04610, -1.0835 0.5841, -0.02440, -1.0891 0.5775, 0.01750, -1.0919 0.5777, 0.04660, -1.0874 0.6274, 0.07170, 0.5538 0.5694, 0.08320, 0.4759 0.5112, 0.09370, 0.4929 0.4731, 0.09830, 0.5118 0.4349, 0.10070, 0.5224 0.3960, 0.10120, 0.5279 0.3566, 0.10020, 0.5295 0.3172, 0.09790, 0.5261 0.2778, 0.09440, 0.4859 0.2393, 0.08960, 0.3844 0.2056, 0.08360, 0.2704 0.1633, 0.07610, 0.1715 0.1261, 0.06710, 0.0982 0.0900, 0.05640, 0.0395 0.0571, 0.04390, -0.0501 0.0283, 0.02940, -0.0254 0.0142, 0.01970, -0.0274 0.0081, 0.01410, 0.1309 0.0026, 0.00780, 0.2812 0.0000, 0.00000, 0.8023 0.0037, -0.00840, 0.9780 0.0112, -0.01420, 0.7929 0.0191, -0.01930, 0.6982 0.0397, -0.03030, 0.4978 0.0706, -0.04420, 0.2529 0.1037, -0.05710, 0.1269 0.1384, -0.06890, -0.1296 0.1741, -0.07950, -0.3072 0.2102, -0.08660, -0.4987 0.2472, -0.09640, -0.7228 0.2844, -0.10270, -0.8968 0.3225, -0.10690, -1.0755 0.3608, -0.10890, -1.2439 0.3991, -0.10830, -1.3538 0.4373, -0.10510, -1.3987 0.4757, -0.09890, -1.3420 0.5137, -0.09070, -1.2967 0.5694, -0.07640, -1.0957 15 Flap element taps 1.0000, 0.00130, -1.0898 0.9365, 0.01390, 0.5504 0.8333, 0.03280, 0.6130 0.7436, 0.04930, 0.4719 0.7049, 0.05670, 0.5013 0.6662, 0.06410, 0.5556 0.6522, 0.01390, -1.0882 0.5969, -0.00020, -1.0962 0.6000, -0.03020, -1.0928 0.6324, -0.04540, -1.1021 0.6667, -0.04880, -1.1278 0.7046, -0.04110, -1.1131 0.7429, -0.03210, -1.1131 0.8333, -0.01400, -1.1132 0.9311, -0.00120, -1.0983 --------- Run Conditions: vel=212.8 ft/s Re=2.002x10^6 AOA=19.98 Flap deflection=-90.00 Totals: Cl=-0.7129 Cdp=0.4567 Cm(c/4)=0.2365 Cs=-0.6728 Ch=0.5113 Main component: Cl=-0.5010 Cdp=0.0124 Cm=0.2234 Flap component: Cl=-0.2119 Cdp=0.4443 Cm=0.1416 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.0181 0.6175, -0.04610, -1.0893 0.5841, -0.02440, -1.0857 0.5775, 0.01750, -1.0914 0.5777, 0.04660, -1.0864 0.6274, 0.07170, 0.4940 0.5694, 0.08320, 0.3638 0.5112, 0.09370, 0.3768 0.4731, 0.09830, 0.4039 0.4349, 0.10070, 0.4152 0.3960, 0.10120, 0.4224 0.3566, 0.10020, 0.4218 0.3172, 0.09790, 0.4244 0.2778, 0.09440, 0.4135 0.2393, 0.08960, 0.3519 0.2056, 0.08360, 0.2290 0.1633, 0.07610, 0.0959 0.1261, 0.06710, -0.0138 0.0900, 0.05640, -0.1171 0.0571, 0.04390, -0.2738 0.0283, 0.02940, -0.3397 0.0142, 0.01970, -0.4641 0.0081, 0.01410, -0.3523 0.0026, 0.00780, -0.1696 0.0000, 0.00000, 0.2690 0.0037, -0.00840, 1.0001 0.0112, -0.01420, 0.9649 0.0191, -0.01930, 0.8682 0.0397, -0.03030, 0.6820 0.0706, -0.04420, 0.4436 0.1037, -0.05710, 0.2913 0.1384, -0.06890, 0.0539 0.1741, -0.07950, -0.1269 0.2102, -0.08660, -0.3178 0.2472, -0.09640, -0.5419 0.2844, -0.10270, -0.7200 0.3225, -0.10690, -0.9054 0.3608, -0.10890, -1.0793 0.3991, -0.10830, -1.2021 0.4373, -0.10510, -1.2624 0.4757, -0.09890, -1.2230 0.5137, -0.09070, -1.2193 0.5694, -0.07640, -1.0409 15 Flap element taps 1.0000, 0.00130, -1.1044 0.9365, 0.01390, 0.5298 0.8333, 0.03280, 0.5162 0.7436, 0.04930, 0.3591 0.7049, 0.05670, 0.4037 0.6662, 0.06410, 0.4694 0.6522, 0.01390, -1.0771 0.5969, -0.00020, -1.0923 0.6000, -0.03020, -1.0854 0.6324, -0.04540, -1.0966 0.6667, -0.04880, -1.1158 0.7046, -0.04110, -1.1055 0.7429, -0.03210, -1.1128 0.8333, -0.01400, -1.1156 0.9311, -0.00120, -1.1157 --------- Run Conditions: vel=212.8 ft/s Re=1.995x10^6 AOA=23.98 Flap deflection=-90.00 Totals: Cl=-0.2548 Cdp=0.4277 Cm(c/4)=0.1744 Cs=-0.4943 Ch=0.3867 Main component: Cl=-0.0801 Cdp=0.1159 Cm=0.0848 Flap component: Cl=-0.1747 Cdp=0.3117 Cm=0.1044 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8856 0.6175, -0.04610, -1.0134 0.5841, -0.02440, -1.0158 0.5775, 0.01750, -1.0186 0.5777, 0.04660, -1.0155 0.6274, 0.07170, 0.1539 0.5694, 0.08320, -0.0732 0.5112, 0.09370, -0.1495 0.4731, 0.09830, -0.1453 0.4349, 0.10070, -0.0912 0.3960, 0.10120, -0.0624 0.3566, 0.10020, -0.0529 0.3172, 0.09790, -0.0517 0.2778, 0.09440, -0.0533 0.2393, 0.08960, -0.0481 0.2056, 0.08360, -0.0471 0.1633, 0.07610, -0.0638 0.1261, 0.06710, -0.1169 0.0900, 0.05640, -0.2739 0.0571, 0.04390, -0.6013 0.0283, 0.02940, -1.0080 0.0142, 0.01970, -1.5211 0.0081, 0.01410, -1.6361 0.0026, 0.00780, -1.5040 0.0000, 0.00000, -1.9750 0.0037, -0.00840, 0.4915 0.0112, -0.01420, 0.9618 0.0191, -0.01930, 1.0104 0.0397, -0.03030, 0.9455 0.0706, -0.04420, 0.7718 0.1037, -0.05710, 0.6144 0.1384, -0.06890, 0.4156 0.1741, -0.07950, 0.2378 0.2102, -0.08660, 0.0537 0.2472, -0.09640, -0.1584 0.2844, -0.10270, -0.3343 0.3225, -0.10690, -0.5201 0.3608, -0.10890, -0.7013 0.3991, -0.10830, -0.8435 0.4373, -0.10510, -0.9269 0.4757, -0.09890, -0.9246 0.5137, -0.09070, -0.9836 0.5694, -0.07640, -0.8538 15 Flap element taps 1.0000, 0.00130, -1.0490 0.9365, 0.01390, 0.3627 0.8333, 0.03280, 0.0669 0.7436, 0.04930, -0.1027 0.7049, 0.05670, 0.0086 0.6662, 0.06410, 0.1205 0.6522, 0.01390, -1.0004 0.5969, -0.00020, -1.0143 0.6000, -0.03020, -1.0087 0.6324, -0.04540, -1.0067 0.6667, -0.04880, -1.0260 0.7046, -0.04110, -1.0237 0.7429, -0.03210, -1.0368 0.8333, -0.01400, -1.0423 0.9311, -0.00120, -1.0585 --------- Run Conditions: vel=213.4 ft/s Re=2.001x10^6 AOA=27.01 Flap deflection=-90.00 Totals: Cl=0.3673 Cdp=0.3949 Cm(c/4)=0.0569 Cs=-0.1850 Ch=0.1166 Main component: Cl=0.4142 Cdp=0.3121 Cm=-0.0968 Flap component: Cl=-0.0469 Cdp=0.0828 Cm=0.0270 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6576 0.6175, -0.04610, -0.8389 0.5841, -0.02440, -0.8280 0.5775, 0.01750, -0.8305 0.5777, 0.04660, -0.8278 0.6274, 0.07170, -0.4767 0.5694, 0.08320, -0.6774 0.5112, 0.09370, -0.8256 0.4731, 0.09830, -0.8966 0.4349, 0.10070, -0.8757 0.3960, 0.10120, -0.8349 0.3566, 0.10020, -0.8114 0.3172, 0.09790, -0.7924 0.2778, 0.09440, -0.7762 0.2393, 0.08960, -0.7759 0.2056, 0.08360, -0.7894 0.1633, 0.07610, -0.8196 0.1261, 0.06710, -0.8446 0.0900, 0.05640, -0.8748 0.0571, 0.04390, -0.9323 0.0283, 0.02940, -1.0549 0.0142, 0.01970, -1.3345 0.0081, 0.01410, -1.6231 0.0026, 0.00780, -1.6547 0.0000, 0.00000, -3.3545 0.0037, -0.00840, -0.1855 0.0112, -0.01420, 0.7450 0.0191, -0.01930, 0.9259 0.0397, -0.03030, 1.0102 0.0706, -0.04420, 0.9325 0.1037, -0.05710, 0.8175 0.1384, -0.06890, 0.6559 0.1741, -0.07950, 0.5049 0.2102, -0.08660, 0.3431 0.2472, -0.09640, 0.1534 0.2844, -0.10270, -0.0160 0.3225, -0.10690, -0.2026 0.3608, -0.10890, -0.3763 0.3991, -0.10830, -0.5299 0.4373, -0.10510, -0.6176 0.4757, -0.09890, -0.6375 0.5137, -0.09070, -0.6871 0.5694, -0.07640, -0.5956 15 Flap element taps 1.0000, 0.00130, -0.9163 0.9365, 0.01390, -0.3119 0.8333, 0.03280, -0.7155 0.7436, 0.04930, -0.7129 0.7049, 0.05670, -0.5803 0.6662, 0.06410, -0.4795 0.6522, 0.01390, -0.8373 0.5969, -0.00020, -0.8443 0.6000, -0.03020, -0.8359 0.6324, -0.04540, -0.8243 0.6667, -0.04880, -0.8394 0.7046, -0.04110, -0.8317 0.7429, -0.03210, -0.8416 0.8333, -0.01400, -0.8697 0.9311, -0.00120, -0.9507