S809 UNVENTED AILERON, CLEAN, CHORD = 18 INCHES --------- Run Conditions: vel=210.2 ft/s Re=1.992x10^6 AOA=-5.97 Flap deflection=-90.00 Totals: Cl=-1.4934 Cdp=0.6072 Cm(c/4)=0.1674 Cs=-0.4486 Ch=0.5234 Main component: Cl=-1.4919 Cdp=0.0800 Cm=0.4032 Flap component: Cl=-0.0014 Cdp=0.5271 Cm=0.1513 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.9329 0.6175, -0.04610, -0.8946 0.5841, -0.02440, -0.8926 0.5775, 0.01750, -0.8942 0.5777, 0.04660, -0.8851 0.6274, 0.07170, 0.9351 0.5694, 0.08320, 0.9282 0.5112, 0.09370, 0.9304 0.4731, 0.09830, 0.9280 0.4349, 0.10070, 0.8947 0.3960, 0.10120, 0.8430 0.3566, 0.10020, 0.8182 0.3172, 0.09790, 0.8050 0.2778, 0.09440, 0.7966 0.2393, 0.08960, 0.8020 0.2056, 0.08360, 0.8205 0.1633, 0.07610, 0.8537 0.1261, 0.06710, 0.9031 0.0900, 0.05640, 0.9627 0.0571, 0.04390, 1.0092 0.0283, 0.02940, 0.9429 0.0142, 0.01970, 0.6424 0.0081, 0.01410, 0.2334 0.0026, 0.00780, -0.7317 0.0000, 0.00000, -3.0244 0.0037, -0.00840, -2.5791 0.0112, -0.01420, -2.5667 0.0191, -0.01930, -2.5802 0.0397, -0.03030, -2.6265 0.0706, -0.04420, -2.6699 0.1037, -0.05710, -2.5459 0.1384, -0.06890, -2.2957 0.1741, -0.07950, -2.0322 0.2102, -0.08660, -1.8118 0.2472, -0.09640, -1.5942 0.2844, -0.10270, -1.4392 0.3225, -0.10690, -1.3321 0.3608, -0.10890, -1.2460 0.3991, -0.10830, -1.1518 0.4373, -0.10510, -1.0879 0.4757, -0.09890, -1.0428 0.5137, -0.09070, -0.9981 0.5694, -0.07640, -0.9562 15 Flap element taps 1.0000, 0.00130, -0.8312 0.9365, 0.01390, 0.6375 0.8333, 0.03280, 0.9209 0.7436, 0.04930, 0.9316 0.7049, 0.05670, 0.9289 0.6662, 0.06410, 0.9351 0.6522, 0.01390, -0.8996 0.5969, -0.00020, -0.9185 0.6000, -0.03020, -0.9083 0.6324, -0.04540, -0.9095 0.6667, -0.04880, -0.8923 0.7046, -0.04110, -0.8574 0.7429, -0.03210, -0.8508 0.8333, -0.01400, -0.8431 0.9311, -0.00120, -0.8309 --------- Run Conditions: vel=214.9 ft/s Re=2.033x10^6 AOA=-0.01 Flap deflection=-90.00 Totals: Cl=-1.6786 Cdp=0.4140 Cm(c/4)=0.1921 Cs=-0.4137 Ch=0.5068 Main component: Cl=-1.6287 Cdp=-0.0935 Cm=0.4682 Flap component: Cl=-0.0499 Cdp=0.5075 Cm=0.1436 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8701 0.6175, -0.04610, -0.8126 0.5841, -0.02440, -0.8107 0.5775, 0.01750, -0.8161 0.5777, 0.04660, -0.8102 0.6274, 0.07170, 0.9172 0.5694, 0.08320, 0.9068 0.5112, 0.09370, 0.9146 0.4731, 0.09830, 0.9125 0.4349, 0.10070, 0.8821 0.3960, 0.10120, 0.8336 0.3566, 0.10020, 0.7772 0.3172, 0.09790, 0.7622 0.2778, 0.09440, 0.7467 0.2393, 0.08960, 0.7434 0.2056, 0.08360, 0.7547 0.1633, 0.07610, 0.7858 0.1261, 0.06710, 0.8374 0.0900, 0.05640, 0.9090 0.0571, 0.04390, 0.9885 0.0283, 0.02940, 0.9911 0.0142, 0.01970, 0.7565 0.0081, 0.01410, 0.3594 0.0026, 0.00780, -0.7677 0.0000, 0.00000, -4.8930 0.0037, -0.00840, -5.5340 0.0112, -0.01420, -3.5114 0.0191, -0.01930, -2.8245 0.0397, -0.03030, -2.1436 0.0706, -0.04420, -1.8728 0.1037, -0.05710, -1.8303 0.1384, -0.06890, -1.8330 0.1741, -0.07950, -1.8445 0.2102, -0.08660, -1.9185 0.2472, -0.09640, -2.0353 0.2844, -0.10270, -2.0746 0.3225, -0.10690, -2.1092 0.3608, -0.10890, -2.1237 0.3991, -0.10830, -2.0456 0.4373, -0.10510, -1.8803 0.4757, -0.09890, -1.5994 0.5137, -0.09070, -1.3260 0.5694, -0.07640, -1.0038 15 Flap element taps 1.0000, 0.00130, -0.8117 0.9365, 0.01390, 0.6203 0.8333, 0.03280, 0.9128 0.7436, 0.04930, 0.9144 0.7049, 0.05670, 0.9085 0.6662, 0.06410, 0.9189 0.6522, 0.01390, -0.8137 0.5969, -0.00020, -0.8196 0.6000, -0.03020, -0.8163 0.6324, -0.04540, -0.8160 0.6667, -0.04880, -0.8161 0.7046, -0.04110, -0.8061 0.7429, -0.03210, -0.8082 0.8333, -0.01400, -0.8095 0.9311, -0.00120, -0.8042 --------- Run Conditions: vel=211.5 ft/s Re=2.002x10^6 AOA=2.99 Flap deflection=-90.00 Totals: Cl=-1.7270 Cdp=0.4446 Cm(c/4)=0.2260 Cs=-0.5341 Ch=0.5597 Main component: Cl=-1.6444 Cdp=-0.1124 Cm=0.4940 Flap component: Cl=-0.0825 Cdp=0.5570 Cm=0.1574 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.0882 0.6175, -0.04610, -0.9746 0.5841, -0.02440, -0.9766 0.5775, 0.01750, -0.9911 0.5777, 0.04660, -0.9823 0.6274, 0.07170, 0.9001 0.5694, 0.08320, 0.8906 0.5112, 0.09370, 0.8955 0.4731, 0.09830, 0.8929 0.4349, 0.10070, 0.8635 0.3960, 0.10120, 0.8083 0.3566, 0.10020, 0.7443 0.3172, 0.09790, 0.7237 0.2778, 0.09440, 0.7051 0.2393, 0.08960, 0.6968 0.2056, 0.08360, 0.7035 0.1633, 0.07610, 0.7313 0.1261, 0.06710, 0.7813 0.0900, 0.05640, 0.8557 0.0571, 0.04390, 0.9510 0.0283, 0.02940, 1.0040 0.0142, 0.01970, 0.8652 0.0081, 0.01410, 0.5730 0.0026, 0.00780, -0.3600 0.0000, 0.00000, -3.7652 0.0037, -0.00840, -4.5519 0.0112, -0.01420, -3.0642 0.0191, -0.01930, -2.3871 0.0397, -0.03030, -1.8776 0.0706, -0.04420, -1.6923 0.1037, -0.05710, -1.7002 0.1384, -0.06890, -1.7426 0.1741, -0.07950, -1.7889 0.2102, -0.08660, -1.8967 0.2472, -0.09640, -2.0485 0.2844, -0.10270, -2.1251 0.3225, -0.10690, -2.1997 0.3608, -0.10890, -2.2610 0.3991, -0.10830, -2.2317 0.4373, -0.10510, -2.1221 0.4757, -0.09890, -1.8927 0.5137, -0.09070, -1.6631 0.5694, -0.07640, -1.3009 15 Flap element taps 1.0000, 0.00130, -0.9962 0.9365, 0.01390, 0.5852 0.8333, 0.03280, 0.8966 0.7436, 0.04930, 0.8914 0.7049, 0.05670, 0.8869 0.6662, 0.06410, 0.8970 0.6522, 0.01390, -0.9783 0.5969, -0.00020, -0.9906 0.6000, -0.03020, -0.9881 0.6324, -0.04540, -0.9991 0.6667, -0.04880, -1.0096 0.7046, -0.04110, -0.9981 0.7429, -0.03210, -0.9949 0.8333, -0.01400, -1.0011 0.9311, -0.00120, -1.0030 --------- Run Conditions: vel=211.6 ft/s Re=1.997x10^6 AOA=6.01 Flap deflection=-90.00 Totals: Cl=-1.5977 Cdp=0.4696 Cm(c/4)=0.2424 Cs=-0.6343 Ch=0.5779 Main component: Cl=-1.4828 Cdp=-0.1021 Cm=0.4652 Flap component: Cl=-0.1149 Cdp=0.5716 Cm=0.1622 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.1348 0.6175, -0.04610, -1.0419 0.5841, -0.02440, -1.0385 0.5775, 0.01750, -1.0438 0.5777, 0.04660, -1.0353 0.6274, 0.07170, 0.8758 0.5694, 0.08320, 0.8603 0.5112, 0.09370, 0.8714 0.4731, 0.09830, 0.8735 0.4349, 0.10070, 0.8502 0.3960, 0.10120, 0.7865 0.3566, 0.10020, 0.7345 0.3172, 0.09790, 0.6670 0.2778, 0.09440, 0.6463 0.2393, 0.08960, 0.6263 0.2056, 0.08360, 0.6204 0.1633, 0.07610, 0.6363 0.1261, 0.06710, 0.6774 0.0900, 0.05640, 0.7462 0.0571, 0.04390, 0.8570 0.0283, 0.02940, 0.9866 0.0142, 0.01970, 0.9966 0.0081, 0.01410, 0.8834 0.0026, 0.00780, 0.2730 0.0000, 0.00000, -1.7654 0.0037, -0.00840, -2.7052 0.0112, -0.01420, -2.2173 0.0191, -0.01930, -1.5555 0.0397, -0.03030, -1.2844 0.0706, -0.04420, -1.2421 0.1037, -0.05710, -1.3212 0.1384, -0.06890, -1.4140 0.1741, -0.07950, -1.4980 0.2102, -0.08660, -1.6383 0.2472, -0.09640, -1.8161 0.2844, -0.10270, -1.9220 0.3225, -0.10690, -2.0277 0.3608, -0.10890, -2.1203 0.3991, -0.10830, -2.1272 0.4373, -0.10510, -2.0559 0.4757, -0.09890, -1.8638 0.5137, -0.09070, -1.6676 0.5694, -0.07640, -1.3336 15 Flap element taps 1.0000, 0.00130, -1.0446 0.9365, 0.01390, 0.5627 0.8333, 0.03280, 0.8916 0.7436, 0.04930, 0.8684 0.7049, 0.05670, 0.8631 0.6662, 0.06410, 0.8786 0.6522, 0.01390, -1.0443 0.5969, -0.00020, -1.0584 0.6000, -0.03020, -1.0562 0.6324, -0.04540, -1.0749 0.6667, -0.04880, -1.0982 0.7046, -0.04110, -1.0869 0.7429, -0.03210, -1.0883 0.8333, -0.01400, -1.0824 0.9311, -0.00120, -1.0650 --------- Run Conditions: vel=211.2 ft/s Re=1.994x10^6 AOA=9.01 Flap deflection=-90.00 Totals: Cl=-1.4776 Cdp=0.4732 Cm(c/4)=0.2547 Cs=-0.6987 Ch=0.5853 Main component: Cl=-1.3313 Cdp=-0.0964 Cm=0.4368 Flap component: Cl=-0.1463 Cdp=0.5696 Cm=0.1642 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.1457 0.6175, -0.04610, -1.0907 0.5841, -0.02440, -1.0815 0.5775, 0.01750, -1.0927 0.5777, 0.04660, -1.0832 0.6274, 0.07170, 0.8537 0.5694, 0.08320, 0.8317 0.5112, 0.09370, 0.8478 0.4731, 0.09830, 0.8492 0.4349, 0.10070, 0.8341 0.3960, 0.10120, 0.7684 0.3566, 0.10020, 0.6990 0.3172, 0.09790, 0.6304 0.2778, 0.09440, 0.5792 0.2393, 0.08960, 0.5515 0.2056, 0.08360, 0.5313 0.1633, 0.07610, 0.5300 0.1261, 0.06710, 0.5567 0.0900, 0.05640, 0.6109 0.0571, 0.04390, 0.7173 0.0283, 0.02940, 0.8828 0.0142, 0.01970, 0.9979 0.0081, 0.01410, 1.0043 0.0026, 0.00780, 0.7640 0.0000, 0.00000, -0.3233 0.0037, -0.00840, -1.2891 0.0112, -0.01420, -1.1075 0.0191, -0.01930, -0.9624 0.0397, -0.03030, -0.8187 0.0706, -0.04420, -0.8562 0.1037, -0.05710, -0.9850 0.1384, -0.06890, -1.1163 0.1741, -0.07950, -1.2522 0.2102, -0.08660, -1.4118 0.2472, -0.09640, -1.6080 0.2844, -0.10270, -1.7414 0.3225, -0.10690, -1.8887 0.3608, -0.10890, -2.0052 0.3991, -0.10830, -2.0567 0.4373, -0.10510, -1.9969 0.4757, -0.09890, -1.8597 0.5137, -0.09070, -1.6657 0.5694, -0.07640, -1.2909 15 Flap element taps 1.0000, 0.00130, -1.0857 0.9365, 0.01390, 0.5439 0.8333, 0.03280, 0.8796 0.7436, 0.04930, 0.8353 0.7049, 0.05670, 0.8344 0.6662, 0.06410, 0.8520 0.6522, 0.01390, -1.0868 0.5969, -0.00020, -1.1019 0.6000, -0.03020, -1.0946 0.6324, -0.04540, -1.1088 0.6667, -0.04880, -1.1308 0.7046, -0.04110, -1.1116 0.7429, -0.03210, -1.1169 0.8333, -0.01400, -1.1351 0.9311, -0.00120, -1.1053 --------- Run Conditions: vel=211.4 ft/s Re=1.988x10^6 AOA=12.06 Flap deflection=-90.00 Totals: Cl=-1.3041 Cdp=0.4773 Cm(c/4)=0.2613 Cs=-0.7393 Ch=0.5822 Main component: Cl=-1.1284 Cdp=-0.0794 Cm=0.3916 Flap component: Cl=-0.1757 Cdp=0.5568 Cm=0.1636 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.1301 0.6175, -0.04610, -1.1049 0.5841, -0.02440, -1.1071 0.5775, 0.01750, -1.1142 0.5777, 0.04660, -1.1042 0.6274, 0.07170, 0.8141 0.5694, 0.08320, 0.7905 0.5112, 0.09370, 0.8045 0.4731, 0.09830, 0.8109 0.4349, 0.10070, 0.8049 0.3960, 0.10120, 0.7480 0.3566, 0.10020, 0.6602 0.3172, 0.09790, 0.5996 0.2778, 0.09440, 0.4890 0.2393, 0.08960, 0.4605 0.2056, 0.08360, 0.4268 0.1633, 0.07610, 0.4047 0.1261, 0.06710, 0.4096 0.0900, 0.05640, 0.4372 0.0571, 0.04390, 0.5182 0.0283, 0.02940, 0.6765 0.0142, 0.01970, 0.8511 0.0081, 0.01410, 0.9455 0.0026, 0.00780, 0.9705 0.0000, 0.00000, 0.6397 0.0037, -0.00840, -0.1389 0.0112, -0.01420, -0.2459 0.0191, -0.01930, -0.2611 0.0397, -0.03030, -0.3086 0.0706, -0.04420, -0.4435 0.1037, -0.05710, -0.6153 0.1384, -0.06890, -0.7797 0.1741, -0.07950, -0.9400 0.2102, -0.08660, -1.1176 0.2472, -0.09640, -1.3294 0.2844, -0.10270, -1.4815 0.3225, -0.10690, -1.6496 0.3608, -0.10890, -1.7865 0.3991, -0.10830, -1.8676 0.4373, -0.10510, -1.8391 0.4757, -0.09890, -1.7276 0.5137, -0.09070, -1.5733 0.5694, -0.07640, -1.2359 15 Flap element taps 1.0000, 0.00130, -1.1133 0.9365, 0.01390, 0.5212 0.8333, 0.03280, 0.8624 0.7436, 0.04930, 0.7946 0.7049, 0.05670, 0.7933 0.6662, 0.06410, 0.8166 0.6522, 0.01390, -1.1107 0.5969, -0.00020, -1.1201 0.6000, -0.03020, -1.1149 0.6324, -0.04540, -1.1276 0.6667, -0.04880, -1.1490 0.7046, -0.04110, -1.1361 0.7429, -0.03210, -1.1312 0.8333, -0.01400, -1.1423 0.9311, -0.00120, -1.1231 --------- Run Conditions: vel=212.8 ft/s Re=1.995x10^6 AOA=14.99 Flap deflection=-90.00 Totals: Cl=-1.1303 Cdp=0.4770 Cm(c/4)=0.2651 Cs=-0.7531 Ch=0.5731 Main component: Cl=-0.9290 Cdp=-0.0583 Cm=0.3455 Flap component: Cl=-0.2013 Cdp=0.5353 Cm=0.1618 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.1154 0.6175, -0.04610, -1.1514 0.5841, -0.02440, -1.1397 0.5775, 0.01750, -1.1243 0.5777, 0.04660, -1.1204 0.6274, 0.07170, 0.7744 0.5694, 0.08320, 0.7234 0.5112, 0.09370, 0.7540 0.4731, 0.09830, 0.7688 0.4349, 0.10070, 0.7702 0.3960, 0.10120, 0.7433 0.3566, 0.10020, 0.6502 0.3172, 0.09790, 0.5603 0.2778, 0.09440, 0.4861 0.2393, 0.08960, 0.3587 0.2056, 0.08360, 0.3187 0.1633, 0.07610, 0.2736 0.1261, 0.06710, 0.2487 0.0900, 0.05640, 0.2377 0.0571, 0.04390, 0.2717 0.0283, 0.02940, 0.3768 0.0142, 0.01970, 0.5438 0.0081, 0.01410, 0.6751 0.0026, 0.00780, 0.8380 0.0000, 0.00000, 1.0034 0.0037, -0.00840, 0.6198 0.0112, -0.01420, 0.3910 0.0191, -0.01930, 0.2858 0.0397, -0.03030, 0.1215 0.0706, -0.04420, -0.0766 0.1037, -0.05710, -0.2778 0.1384, -0.06890, -0.4651 0.1741, -0.07950, -0.6449 0.2102, -0.08660, -0.8331 0.2472, -0.09640, -1.0545 0.2844, -0.10270, -1.2222 0.3225, -0.10690, -1.4044 0.3608, -0.10890, -1.5562 0.3991, -0.10830, -1.6623 0.4373, -0.10510, -1.6600 0.4757, -0.09890, -1.5757 0.5137, -0.09070, -1.4703 0.5694, -0.07640, -1.1957 15 Flap element taps 1.0000, 0.00130, -1.1010 0.9365, 0.01390, 0.5160 0.8333, 0.03280, 0.8427 0.7436, 0.04930, 0.7368 0.7049, 0.05670, 0.7397 0.6662, 0.06410, 0.7754 0.6522, 0.01390, -1.1176 0.5969, -0.00020, -1.1314 0.6000, -0.03020, -1.1256 0.6324, -0.04540, -1.1279 0.6667, -0.04880, -1.1411 0.7046, -0.04110, -1.1274 0.7429, -0.03210, -1.1328 0.8333, -0.01400, -1.1360 0.9311, -0.00120, -1.1068 --------- Run Conditions: vel=213.4 ft/s Re=1.998x10^6 AOA=17.99 Flap deflection=-90.00 Totals: Cl=-0.9350 Cdp=0.4699 Cm(c/4)=0.2631 Cs=-0.7357 Ch=0.5584 Main component: Cl=-0.7157 Cdp=-0.0351 Cm=0.2932 Flap component: Cl=-0.2193 Cdp=0.5050 Cm=0.1559 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.0826 0.6175, -0.04610, -1.1194 0.5841, -0.02440, -1.1414 0.5775, 0.01750, -1.1428 0.5777, 0.04660, -1.1381 0.6274, 0.07170, 0.7033 0.5694, 0.08320, 0.6432 0.5112, 0.09370, 0.6680 0.4731, 0.09830, 0.6722 0.4349, 0.10070, 0.6775 0.3960, 0.10120, 0.6772 0.3566, 0.10020, 0.6340 0.3172, 0.09790, 0.5314 0.2778, 0.09440, 0.4145 0.2393, 0.08960, 0.3146 0.2056, 0.08360, 0.2078 0.1633, 0.07610, 0.1161 0.1261, 0.06710, 0.0629 0.0900, 0.05640, 0.0059 0.0571, 0.04390, -0.0306 0.0283, 0.02940, -0.0193 0.0142, 0.01970, 0.0700 0.0081, 0.01410, 0.1667 0.0026, 0.00780, 0.3398 0.0000, 0.00000, 0.8183 0.0037, -0.00840, 0.9726 0.0112, -0.01420, 0.8019 0.0191, -0.01930, 0.6797 0.0397, -0.03030, 0.4705 0.0706, -0.04420, 0.2446 0.1037, -0.05710, 0.0314 0.1384, -0.06890, -0.1681 0.1741, -0.07950, -0.3568 0.2102, -0.08660, -0.5513 0.2472, -0.09640, -0.7776 0.2844, -0.10270, -0.9565 0.3225, -0.10690, -1.1509 0.3608, -0.10890, -1.3180 0.3991, -0.10830, -1.4441 0.4373, -0.10510, -1.4694 0.4757, -0.09890, -1.4110 0.5137, -0.09070, -1.3497 0.5694, -0.07640, -1.1069 15 Flap element taps 1.0000, 0.00130, -1.1348 0.9365, 0.01390, 0.5041 0.8333, 0.03280, 0.7672 0.7436, 0.04930, 0.6318 0.7049, 0.05670, 0.6421 0.6662, 0.06410, 0.6871 0.6522, 0.01390, -1.0965 0.5969, -0.00020, -1.1160 0.6000, -0.03020, -1.1030 0.6324, -0.04540, -1.1058 0.6667, -0.04880, -1.1229 0.7046, -0.04110, -1.1170 0.7429, -0.03210, -1.1191 0.8333, -0.01400, -1.1304 0.9311, -0.00120, -1.1353 --------- Run Conditions: vel=213.4 ft/s Re=1.999x10^6 AOA=19.95 Flap deflection=-90.00 Totals: Cl=-0.7988 Cdp=0.4634 Cm(c/4)=0.2571 Cs=-0.7081 Ch=0.5435 Main component: Cl=-0.5697 Cdp=-0.0146 Cm=0.2531 Flap component: Cl=-0.2291 Cdp=0.4779 Cm=0.1522 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.0382 0.6175, -0.04610, -1.1065 0.5841, -0.02440, -1.1187 0.5775, 0.01750, -1.1296 0.5777, 0.04660, -1.1242 0.6274, 0.07170, 0.6093 0.5694, 0.08320, 0.5230 0.5112, 0.09370, 0.5485 0.4731, 0.09830, 0.5699 0.4349, 0.10070, 0.5752 0.3960, 0.10120, 0.5793 0.3566, 0.10020, 0.5701 0.3172, 0.09790, 0.5389 0.2778, 0.09440, 0.4355 0.2393, 0.08960, 0.3012 0.2056, 0.08360, 0.1785 0.1633, 0.07610, 0.0725 0.1261, 0.06710, -0.0513 0.0900, 0.05640, -0.1497 0.0571, 0.04390, -0.2449 0.0283, 0.02940, -0.3240 0.0142, 0.01970, -0.3292 0.0081, 0.01410, -0.3041 0.0026, 0.00780, -0.1202 0.0000, 0.00000, 0.3341 0.0037, -0.00840, 1.0056 0.0112, -0.01420, 0.9567 0.0191, -0.01930, 0.8605 0.0397, -0.03030, 0.6596 0.0706, -0.04420, 0.4326 0.1037, -0.05710, 0.2192 0.1384, -0.06890, 0.0159 0.1741, -0.07950, -0.1746 0.2102, -0.08660, -0.3698 0.2472, -0.09640, -0.5973 0.2844, -0.10270, -0.7809 0.3225, -0.10690, -0.9812 0.3608, -0.10890, -1.1559 0.3991, -0.10830, -1.2948 0.4373, -0.10510, -1.3369 0.4757, -0.09890, -1.2955 0.5137, -0.09070, -1.2624 0.5694, -0.07640, -1.0414 15 Flap element taps 1.0000, 0.00130, -1.1185 0.9365, 0.01390, 0.5211 0.8333, 0.03280, 0.7051 0.7436, 0.04930, 0.5355 0.7049, 0.05670, 0.5504 0.6662, 0.06410, 0.6089 0.6522, 0.01390, -1.0968 0.5969, -0.00020, -1.1178 0.6000, -0.03020, -1.1027 0.6324, -0.04540, -1.1011 0.6667, -0.04880, -1.1164 0.7046, -0.04110, -1.1084 0.7429, -0.03210, -1.1102 0.8333, -0.01400, -1.1136 0.9311, -0.00120, -1.1202 --------- Run Conditions: vel=214.3 ft/s Re=2.004x10^6 AOA=23.99 Flap deflection=-90.00 Totals: Cl=-0.4118 Cdp=0.4283 Cm(c/4)=0.2125 Cs=-0.5588 Ch=0.4459 Main component: Cl=-0.2023 Cdp=0.0589 Cm=0.1399 Flap component: Cl=-0.2095 Cdp=0.3695 Cm=0.1231 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.9232 0.6175, -0.04610, -1.0752 0.5841, -0.02440, -1.0674 0.5775, 0.01750, -1.0681 0.5777, 0.04660, -1.0637 0.6274, 0.07170, 0.3129 0.5694, 0.08320, 0.1644 0.5112, 0.09370, 0.1547 0.4731, 0.09830, 0.1689 0.4349, 0.10070, 0.1969 0.3960, 0.10120, 0.2124 0.3566, 0.10020, 0.2093 0.3172, 0.09790, 0.2190 0.2778, 0.09440, 0.2238 0.2393, 0.08960, 0.2220 0.2056, 0.08360, 0.1803 0.1633, 0.07610, 0.0163 0.1261, 0.06710, -0.2032 0.0900, 0.05640, -0.4467 0.0571, 0.04390, -0.7201 0.0283, 0.02940, -1.0691 0.0142, 0.01970, -1.4332 0.0081, 0.01410, -1.7043 0.0026, 0.00780, -1.7407 0.0000, 0.00000, -1.7994 0.0037, -0.00840, 0.5633 0.0112, -0.01420, 0.9695 0.0191, -0.01930, 1.0118 0.0397, -0.03030, 0.9325 0.0706, -0.04420, 0.7552 0.1037, -0.05710, 0.5681 0.1384, -0.06890, 0.3753 0.1741, -0.07950, 0.1926 0.2102, -0.08660, 0.0043 0.2472, -0.09640, -0.2151 0.2844, -0.10270, -0.4020 0.3225, -0.10690, -0.6063 0.3608, -0.10890, -0.7913 0.3991, -0.10830, -0.9491 0.4373, -0.10510, -1.0235 0.4757, -0.09890, -1.0181 0.5137, -0.09070, -1.0308 0.5694, -0.07640, -0.8864 15 Flap element taps 1.0000, 0.00130, -1.0871 0.9365, 0.01390, 0.4005 0.8333, 0.03280, 0.2775 0.7436, 0.04930, 0.1502 0.7049, 0.05670, 0.2153 0.6662, 0.06410, 0.2927 0.6522, 0.01390, -1.0674 0.5969, -0.00020, -1.0820 0.6000, -0.03020, -1.0714 0.6324, -0.04540, -1.0721 0.6667, -0.04880, -1.0887 0.7046, -0.04110, -1.0813 0.7429, -0.03210, -1.0869 0.8333, -0.01400, -1.0935 0.9311, -0.00120, -1.0928 --------- Run Conditions: vel=220.4 ft/s Re=2.062x10^6 AOA=27.02 Flap deflection=-90.00 Totals: Cl=0.7209 Cdp=0.2741 Cm(c/4)=-0.0471 Cs=0.0833 Ch=-0.1836 Main component: Cl=0.6226 Cdp=0.4257 Cm=-0.1866 Flap component: Cl=0.0983 Cdp=-0.1516 Cm=-0.0522 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4910 0.6175, -0.04610, -0.6258 0.5841, -0.02440, -0.6186 0.5775, 0.01750, -0.6169 0.5777, 0.04660, -0.6102 0.6274, 0.07170, -0.9742 0.5694, 0.08320, -1.0628 0.5112, 0.09370, -1.2617 0.4731, 0.09830, -1.3738 0.4349, 0.10070, -1.3506 0.3960, 0.10120, -1.2664 0.3566, 0.10020, -1.1995 0.3172, 0.09790, -1.1427 0.2778, 0.09440, -1.1094 0.2393, 0.08960, -1.0877 0.2056, 0.08360, -1.0702 0.1633, 0.07610, -1.0680 0.1261, 0.06710, -1.0582 0.0900, 0.05640, -1.0529 0.0571, 0.04390, -1.0486 0.0283, 0.02940, -1.0493 0.0142, 0.01970, -1.0608 0.0081, 0.01410, -1.0654 0.0026, 0.00780, -0.9845 0.0000, 0.00000, -1.1123 0.0037, -0.00840, 0.1112 0.0112, -0.01420, 0.7513 0.0191, -0.01930, 0.9325 0.0397, -0.03030, 1.0115 0.0706, -0.04420, 0.9519 0.1037, -0.05710, 0.8403 0.1384, -0.06890, 0.6996 0.1741, -0.07950, 0.5599 0.2102, -0.08660, 0.4111 0.2472, -0.09640, 0.2346 0.2844, -0.10270, 0.0770 0.3225, -0.10690, -0.0972 0.3608, -0.10890, -0.2582 0.3991, -0.10830, -0.4022 0.4373, -0.10510, -0.4832 0.4757, -0.09890, -0.5014 0.5137, -0.09070, -0.5371 0.5694, -0.07640, -0.4542 15 Flap element taps 1.0000, 0.00130, -0.7860 0.9365, 0.01390, -1.0011 0.8333, 0.03280, -1.3424 0.7436, 0.04930, -1.0892 0.7049, 0.05670, -1.0112 0.6662, 0.06410, -0.9378 0.6522, 0.01390, -0.6208 0.5969, -0.00020, -0.6307 0.6000, -0.03020, -0.6069 0.6324, -0.04540, -0.5656 0.6667, -0.04880, -0.5504 0.7046, -0.04110, -0.5357 0.7429, -0.03210, -0.5343 0.8333, -0.01400, -0.5451 0.9311, -0.00120, -0.5667