S809 UNVENTED AILERON, LEGR, CHORD = 18 IN --------- Run Conditions: vel=205.0 ft/s Re=1.998x10^6 AOA=-6.00 Flap deflection=5.00 Totals: Cl=-0.2019 Cdp=0.0094 Cm(c/4)=-0.0451 Cs=0.0118 Ch=-0.0338 Main component: Cl=-0.2484 Cdp=0.0327 Cm=0.0436 Flap component: Cl=0.0465 Cdp=-0.0234 Cm=-0.0382 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.1536 0.6175, -0.04610, -0.1302 0.5841, -0.02440, -0.1297 0.5775, 0.01750, -0.1306 0.5777, 0.04660, -0.1287 0.6274, 0.07170, -0.2940 0.5694, 0.08320, -0.3872 0.5112, 0.09370, -0.5959 0.4731, 0.09830, -0.6349 0.4349, 0.10070, -0.6139 0.3960, 0.10120, -0.5498 0.3566, 0.10020, -0.4770 0.3172, 0.09790, -0.4068 0.2778, 0.09440, -0.3555 0.2393, 0.08960, -0.3080 0.2056, 0.08360, -0.2447 0.1633, 0.07610, -0.1402 0.1261, 0.06710, -0.0199 0.0900, 0.05640, 0.0098 0.0571, 0.04390, 0.3262 0.0283, 0.02940, 0.6112 0.0142, 0.01970, 0.8517 0.0081, 0.01410, 0.9586 0.0026, 0.00780, 0.8781 0.0000, 0.00000, -0.1085 0.0037, -0.00840, -0.4879 0.0112, -0.01420, -0.4718 0.0191, -0.01930, -0.5308 0.0397, -0.03030, -0.4599 0.0706, -0.04420, -0.5387 0.1037, -0.05710, -0.5474 0.1384, -0.06890, -0.6646 0.1741, -0.07950, -0.7269 0.2102, -0.08660, -0.8162 0.2472, -0.09640, -0.9052 0.2844, -0.10270, -0.9464 0.3225, -0.10690, -0.9647 0.3608, -0.10890, -0.9724 0.3991, -0.10830, -0.9141 0.4373, -0.10510, -0.8035 0.4757, -0.09890, -0.6006 0.5137, -0.09070, -0.4240 0.5694, -0.07640, -0.2216 14 Flap element taps 1.0000, 0.00130, 0.1878 0.9365, 0.01390, 0.1012 0.8333, 0.03280, -0.0258 0.7436, 0.04930, -0.1421 0.7049, 0.05670, -0.2108 0.6662, 0.06410, -0.4120 0.6522, 0.01390, -0.1322 0.5969, -0.00020, -0.1315 0.6000, -0.03020, -0.1318 0.6324, -0.04540, -0.1370 0.6667, -0.04880, -0.1203 0.7046, -0.04110, -0.0553 0.7429, -0.03210, -0.0159 0.9311, -0.00120, 0.2441 Wake drag found for this condition, Cdw=0.0224 --------- Run Conditions: vel=205.5 ft/s Re=2.001x10^6 AOA=-0.01 Flap deflection=5.00 Totals: Cl=0.4114 Cdp=-0.0108 Cm(c/4)=-0.0670 Cs=0.0108 Ch=-0.0958 Main component: Cl=0.2886 Cdp=-0.0073 Cm=-0.0742 Flap component: Cl=0.1229 Cdp=-0.0035 Cm=-0.0957 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.0062 0.6175, -0.04610, 0.0681 0.5841, -0.02440, 0.0499 0.5775, 0.01750, 0.0460 0.5777, 0.04660, 0.0560 0.6274, 0.07170, -0.4276 0.5694, 0.08320, -0.5543 0.5112, 0.09370, -0.8201 0.4731, 0.09830, -0.9013 0.4349, 0.10070, -0.9208 0.3960, 0.10120, -0.8940 0.3566, 0.10020, -0.8438 0.3172, 0.09790, -0.8061 0.2778, 0.09440, -0.7923 0.2393, 0.08960, -0.7920 0.2056, 0.08360, -0.7836 0.1633, 0.07610, -0.7239 0.1261, 0.06710, -0.6686 0.0900, 0.05640, -0.7827 0.0571, 0.04390, -0.5214 0.0283, 0.02940, -0.3496 0.0142, 0.01970, -0.1502 0.0081, 0.01410, -0.0250 0.0026, 0.00780, 0.1830 0.0000, 0.00000, -0.0972 0.0037, -0.00840, 0.9536 0.0112, -0.01420, 0.7598 0.0191, -0.01930, 0.6043 0.0397, -0.03030, 0.4177 0.0706, -0.04420, 0.2143 0.1037, -0.05710, 0.0999 0.1384, -0.06890, -0.0627 0.1741, -0.07950, -0.1775 0.2102, -0.08660, -0.3116 0.2472, -0.09640, -0.4325 0.2844, -0.10270, -0.5186 0.3225, -0.10690, -0.5763 0.3608, -0.10890, -0.6336 0.3991, -0.10830, -0.6263 0.4373, -0.10510, -0.5854 0.4757, -0.09890, -0.4506 0.5137, -0.09070, -0.3349 0.5694, -0.07640, -0.1243 14 Flap element taps 1.0000, 0.00130, 0.1170 0.9365, 0.01390, 0.0544 0.8333, 0.03280, -0.0795 0.7436, 0.04930, -0.2233 0.7049, 0.05670, -0.3121 0.6662, 0.06410, -0.4873 0.6522, 0.01390, 0.0399 0.5969, -0.00020, 0.0407 0.6000, -0.03020, 0.0465 0.6324, -0.04540, 0.0553 0.6667, -0.04880, 0.1179 0.7046, -0.04110, 0.2587 0.7429, -0.03210, 0.2497 0.9311, -0.00120, 0.2862 Wake drag found for this condition, Cdw=0.0220 --------- Run Conditions: vel=205.3 ft/s Re=1.998x10^6 AOA=3.01 Flap deflection=5.00 Totals: Cl=0.6626 Cdp=0.0036 Cm(c/4)=-0.0656 Cs=0.0312 Ch=-0.1107 Main component: Cl=0.5282 Cdp=-0.0058 Cm=-0.1256 Flap component: Cl=0.1343 Cdp=0.0094 Cm=-0.1054 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0310 0.6175, -0.04610, 0.0986 0.5841, -0.02440, 0.0789 0.5775, 0.01750, 0.0748 0.5777, 0.04660, 0.0859 0.6274, 0.07170, -0.4549 0.5694, 0.08320, -0.5972 0.5112, 0.09370, -0.8808 0.4731, 0.09830, -0.9862 0.4349, 0.10070, -1.0289 0.3960, 0.10120, -1.0242 0.3566, 0.10020, -0.9920 0.3172, 0.09790, -0.9750 0.2778, 0.09440, -0.9844 0.2393, 0.08960, -1.0114 0.2056, 0.08360, -1.0355 0.1633, 0.07610, -1.0103 0.1261, 0.06710, -0.9985 0.0900, 0.05640, -1.1897 0.0571, 0.04390, -1.0110 0.0283, 0.02940, -0.9713 0.0142, 0.01970, -0.9123 0.0081, 0.01410, -0.8750 0.0026, 0.00780, -0.5024 0.0000, 0.00000, -0.0884 0.0037, -0.00840, 0.9903 0.0112, -0.01420, 0.9782 0.0191, -0.01930, 0.8830 0.0397, -0.03030, 0.6932 0.0706, -0.04420, 0.4788 0.1037, -0.05710, 0.3396 0.1384, -0.06890, 0.1755 0.1741, -0.07950, 0.0457 0.2102, -0.08660, -0.0992 0.2472, -0.09640, -0.2276 0.2844, -0.10270, -0.3274 0.3225, -0.10690, -0.3991 0.3608, -0.10890, -0.4722 0.3991, -0.10830, -0.4834 0.4373, -0.10510, -0.4668 0.4757, -0.09890, -0.3560 0.5137, -0.09070, -0.2613 0.5694, -0.07640, -0.0726 14 Flap element taps 1.0000, 0.00130, 0.0290 0.9365, 0.01390, -0.0160 0.8333, 0.03280, -0.1079 0.7436, 0.04930, -0.2338 0.7049, 0.05670, -0.3209 0.6662, 0.06410, -0.4629 0.6522, 0.01390, 0.0685 0.5969, -0.00020, 0.0695 0.6000, -0.03020, 0.0757 0.6324, -0.04540, 0.0848 0.6667, -0.04880, 0.1569 0.7046, -0.04110, 0.2995 0.7429, -0.03210, 0.2726 0.9311, -0.00120, 0.2721 Wake drag found for this condition, Cdw=0.0267 --------- Run Conditions: vel=205.8 ft/s Re=1.998x10^6 AOA=6.01 Flap deflection=5.00 Totals: Cl=0.8713 Cdp=0.0308 Cm(c/4)=-0.0635 Cs=0.0606 Ch=-0.1391 Main component: Cl=0.7253 Cdp=0.0021 Cm=-0.1627 Flap component: Cl=0.1460 Cdp=0.0286 Cm=-0.1182 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0607 0.6175, -0.04610, 0.1211 0.5841, -0.02440, 0.1020 0.5775, 0.01750, 0.0967 0.5777, 0.04660, 0.1074 0.6274, 0.07170, -0.3982 0.5694, 0.08320, -0.5588 0.5112, 0.09370, -0.8579 0.4731, 0.09830, -0.9945 0.4349, 0.10070, -1.0704 0.3960, 0.10120, -1.0964 0.3566, 0.10020, -1.0908 0.3172, 0.09790, -1.0991 0.2778, 0.09440, -1.1363 0.2393, 0.08960, -1.1934 0.2056, 0.08360, -1.2524 0.1633, 0.07610, -1.2705 0.1261, 0.06710, -1.3060 0.0900, 0.05640, -1.5682 0.0571, 0.04390, -1.5043 0.0283, 0.02940, -1.6411 0.0142, 0.01970, -1.7729 0.0081, 0.01410, -1.8913 0.0026, 0.00780, -1.5376 0.0000, 0.00000, -0.0826 0.0037, -0.00840, 0.7333 0.0112, -0.01420, 1.0038 0.0191, -0.01930, 1.0026 0.0397, -0.03030, 0.8744 0.0706, -0.04420, 0.6780 0.1037, -0.05710, 0.5283 0.1384, -0.06890, 0.3683 0.1741, -0.07950, 0.2332 0.2102, -0.08660, 0.0827 0.2472, -0.09640, -0.0481 0.2844, -0.10270, -0.1584 0.3225, -0.10690, -0.2421 0.3608, -0.10890, -0.3282 0.3991, -0.10830, -0.3570 0.4373, -0.10510, -0.3596 0.4757, -0.09890, -0.2718 0.5137, -0.09070, -0.1958 0.5694, -0.07640, -0.0275 14 Flap element taps 1.0000, 0.00130, -0.1112 0.9365, 0.01390, -0.1770 0.8333, 0.03280, -0.2047 0.7436, 0.04930, -0.2343 0.7049, 0.05670, -0.2647 0.6662, 0.06410, -0.3409 0.6522, 0.01390, 0.0905 0.5969, -0.00020, 0.0919 0.6000, -0.03020, 0.0977 0.6324, -0.04540, 0.1065 0.6667, -0.04880, 0.1651 0.7046, -0.04110, 0.3219 0.7429, -0.03210, 0.2831 0.9311, -0.00120, 0.2354 Wake drag found for this condition, Cdw=0.0353 --------- Run Conditions: vel=205.6 ft/s Re=1.994x10^6 AOA=9.00 Flap deflection=5.00 Totals: Cl=1.0016 Cdp=0.0671 Cm(c/4)=-0.0631 Cs=0.0904 Ch=-0.1757 Main component: Cl=0.8296 Cdp=0.0151 Cm=-0.1700 Flap component: Cl=0.1720 Cdp=0.0521 Cm=-0.1430 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0730 0.6175, -0.04610, 0.1197 0.5841, -0.02440, 0.0992 0.5775, 0.01750, 0.0945 0.5777, 0.04660, 0.1059 0.6274, 0.07170, -0.3707 0.5694, 0.08320, -0.4243 0.5112, 0.09370, -0.6389 0.4731, 0.09830, -0.8166 0.4349, 0.10070, -0.9500 0.3960, 0.10120, -1.0279 0.3566, 0.10020, -1.0660 0.3172, 0.09790, -1.1133 0.2778, 0.09440, -1.1833 0.2393, 0.08960, -1.2762 0.2056, 0.08360, -1.3736 0.1633, 0.07610, -1.4378 0.1261, 0.06710, -1.5281 0.0900, 0.05640, -1.8503 0.0571, 0.04390, -1.9181 0.0283, 0.02940, -2.2515 0.0142, 0.01970, -2.6075 0.0081, 0.01410, -2.9258 0.0026, 0.00780, -2.7025 0.0000, 0.00000, -0.0858 0.0037, -0.00840, 0.2846 0.0112, -0.01420, 0.9031 0.0191, -0.01930, 1.0069 0.0397, -0.03030, 0.9696 0.0706, -0.04420, 0.8108 0.1037, -0.05710, 0.6651 0.1384, -0.06890, 0.5154 0.1741, -0.07950, 0.3745 0.2102, -0.08660, 0.2176 0.2472, -0.09640, 0.0822 0.2844, -0.10270, -0.0314 0.3225, -0.10690, -0.1228 0.3608, -0.10890, -0.2192 0.3991, -0.10830, -0.2627 0.4373, -0.10510, -0.2829 0.4757, -0.09890, -0.2137 0.5137, -0.09070, -0.1536 0.5694, -0.07640, -0.0013 14 Flap element taps 1.0000, 0.00130, -0.2603 0.9365, 0.01390, -0.3424 0.8333, 0.03280, -0.3494 0.7436, 0.04930, -0.3493 0.7049, 0.05670, -0.3453 0.6662, 0.06410, -0.3551 0.6522, 0.01390, 0.0886 0.5969, -0.00020, 0.0884 0.6000, -0.03020, 0.0944 0.6324, -0.04540, 0.1044 0.6667, -0.04880, 0.1591 0.7046, -0.04110, 0.3270 0.7429, -0.03210, 0.2778 0.9311, -0.00120, 0.1822 --------- Run Conditions: vel=207.2 ft/s Re=2.010x10^6 AOA=12.00 Flap deflection=5.00 Totals: Cl=1.0574 Cdp=0.1052 Cm(c/4)=-0.0570 Cs=0.1170 Ch=-0.1941 Main component: Cl=0.8727 Cdp=0.0354 Cm=-0.1642 Flap component: Cl=0.1848 Cdp=0.0698 Cm=-0.1568 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0819 0.6175, -0.04610, 0.1105 0.5841, -0.02440, 0.0875 0.5775, 0.01750, 0.0850 0.5777, 0.04660, 0.0983 0.6274, 0.07170, -0.4153 0.5694, 0.08320, -0.4127 0.5112, 0.09370, -0.4536 0.4731, 0.09830, -0.5426 0.4349, 0.10070, -0.6837 0.3960, 0.10120, -0.8226 0.3566, 0.10020, -0.9203 0.3172, 0.09790, -1.0181 0.2778, 0.09440, -1.1308 0.2393, 0.08960, -1.2601 0.2056, 0.08360, -1.3993 0.1633, 0.07610, -1.5120 0.1261, 0.06710, -1.6582 0.0900, 0.05640, -2.0257 0.0571, 0.04390, -2.2296 0.0283, 0.02940, -2.7518 0.0142, 0.01970, -3.3244 0.0081, 0.01410, -3.8465 0.0026, 0.00780, -3.7932 0.0000, 0.00000, -0.0834 0.0037, -0.00840, -0.2439 0.0112, -0.01420, 0.7301 0.0191, -0.01930, 0.9498 0.0397, -0.03030, 1.0090 0.0706, -0.04420, 0.8962 0.1037, -0.05710, 0.7635 0.1384, -0.06890, 0.6255 0.1741, -0.07950, 0.4863 0.2102, -0.08660, 0.3307 0.2472, -0.09640, 0.1920 0.2844, -0.10270, 0.0663 0.3225, -0.10690, -0.0336 0.3608, -0.10890, -0.1354 0.3991, -0.10830, -0.2002 0.4373, -0.10510, -0.2280 0.4757, -0.09890, -0.1745 0.5137, -0.09070, -0.1273 0.5694, -0.07640, 0.0220 14 Flap element taps 1.0000, 0.00130, -0.3646 0.9365, 0.01390, -0.4353 0.8333, 0.03280, -0.4315 0.7436, 0.04930, -0.4243 0.7049, 0.05670, -0.4181 0.6662, 0.06410, -0.4160 0.6522, 0.01390, 0.0781 0.5969, -0.00020, 0.0767 0.6000, -0.03020, 0.0841 0.6324, -0.04540, 0.0944 0.6667, -0.04880, 0.1347 0.7046, -0.04110, 0.3276 0.7429, -0.03210, 0.2724 0.9311, -0.00120, 0.1376 --------- Run Conditions: vel=207.4 ft/s Re=2.004x10^6 AOA=15.01 Flap deflection=5.00 Totals: Cl=1.0459 Cdp=0.1790 Cm(c/4)=-0.0770 Cs=0.0979 Ch=-0.2094 Main component: Cl=0.8180 Cdp=0.1020 Cm=-0.1519 Flap component: Cl=0.2279 Cdp=0.0770 Cm=-0.1893 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0237 0.6175, -0.04610, -0.0923 0.5841, -0.02440, -0.1713 0.5775, 0.01750, -0.2041 0.5777, 0.04660, -0.1348 0.6274, 0.07170, -0.5046 0.5694, 0.08320, -0.5130 0.5112, 0.09370, -0.5150 0.4731, 0.09830, -0.5372 0.4349, 0.10070, -0.5822 0.3960, 0.10120, -0.6394 0.3566, 0.10020, -0.7165 0.3172, 0.09790, -0.8015 0.2778, 0.09440, -0.9137 0.2393, 0.08960, -1.0475 0.2056, 0.08360, -1.2040 0.1633, 0.07610, -1.3695 0.1261, 0.06710, -1.5510 0.0900, 0.05640, -1.9334 0.0571, 0.04390, -2.2264 0.0283, 0.02940, -2.8421 0.0142, 0.01970, -3.5317 0.0081, 0.01410, -4.1335 0.0026, 0.00780, -4.1290 0.0000, 0.00000, -0.1614 0.0037, -0.00840, -0.5084 0.0112, -0.01420, 0.6269 0.0191, -0.01930, 0.9055 0.0397, -0.03030, 1.0113 0.0706, -0.04420, 0.9267 0.1037, -0.05710, 0.8043 0.1384, -0.06890, 0.6558 0.1741, -0.07950, 0.5179 0.2102, -0.08660, 0.3748 0.2472, -0.09640, 0.2242 0.2844, -0.10270, 0.0965 0.3225, -0.10690, -0.0260 0.3608, -0.10890, -0.1334 0.3991, -0.10830, -0.2157 0.4373, -0.10510, -0.2450 0.4757, -0.09890, -0.2019 0.5137, -0.09070, -0.1606 0.5694, -0.07640, -0.0097 14 Flap element taps 1.0000, 0.00130, -0.5074 0.9365, 0.01390, -0.5559 0.8333, 0.03280, -0.5493 0.7436, 0.04930, -0.5408 0.7049, 0.05670, -0.5337 0.6662, 0.06410, -0.5346 0.6522, 0.01390, -0.2102 0.5969, -0.00020, -0.2198 0.6000, -0.03020, -0.1810 0.6324, -0.04540, -0.1492 0.6667, -0.04880, 0.5536 0.7046, -0.04110, 0.3055 0.7429, -0.03210, 0.2464 0.9311, -0.00120, 0.0679 --------- Run Conditions: vel=209.7 ft/s Re=2.006x10^6 AOA=17.98 Flap deflection=5.00 Totals: Cl=0.8507 Cdp=0.3329 Cm(c/4)=-0.1285 Cs=-0.0539 Ch=-0.2311 Main component: Cl=0.6047 Cdp=0.2278 Cm=-0.1465 Flap component: Cl=0.2460 Cdp=0.1052 Cm=-0.2102 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.0252 0.6175, -0.04610, -0.1728 0.5841, -0.02440, -0.2678 0.5775, 0.01750, -0.3044 0.5777, 0.04660, -0.2196 0.6274, 0.07170, -0.7734 0.5694, 0.08320, -0.7481 0.5112, 0.09370, -0.7202 0.4731, 0.09830, -0.7126 0.4349, 0.10070, -0.7330 0.3960, 0.10120, -0.7454 0.3566, 0.10020, -0.7641 0.3172, 0.09790, -0.7752 0.2778, 0.09440, -0.7895 0.2393, 0.08960, -0.8084 0.2056, 0.08360, -0.8362 0.1633, 0.07610, -0.8771 0.1261, 0.06710, -0.9319 0.0900, 0.05640, -0.9581 0.0571, 0.04390, -1.0799 0.0283, 0.02940, -1.3368 0.0142, 0.01970, -1.7526 0.0081, 0.01410, -2.0766 0.0026, 0.00780, -2.2174 0.0000, 0.00000, -0.0846 0.0037, -0.00840, -0.0316 0.0112, -0.01420, 0.7605 0.0191, -0.01930, 0.9493 0.0397, -0.03030, 1.0057 0.0706, -0.04420, 0.9142 0.1037, -0.05710, 0.7939 0.1384, -0.06890, 0.6501 0.1741, -0.07950, 0.5147 0.2102, -0.08660, 0.3735 0.2472, -0.09640, 0.2213 0.2844, -0.10270, 0.0907 0.3225, -0.10690, -0.0335 0.3608, -0.10890, -0.1476 0.3991, -0.10830, -0.2351 0.4373, -0.10510, -0.2712 0.4757, -0.09890, -0.2318 0.5137, -0.09070, -0.1911 0.5694, -0.07640, -0.0492 14 Flap element taps 1.0000, 0.00130, -0.5791 0.9365, 0.01390, -0.6552 0.8333, 0.03280, -0.6892 0.7436, 0.04930, -0.6730 0.7049, 0.05670, -0.6531 0.6662, 0.06410, -0.6313 0.6522, 0.01390, -0.3017 0.5969, -0.00020, -0.3139 0.6000, -0.03020, -0.2680 0.6324, -0.04540, -0.2335 0.6667, -0.04880, 0.5774 0.7046, -0.04110, 0.2755 0.7429, -0.03210, 0.2109 0.9311, -0.00120, 0.0114 Wake drag found for this condition, Cdw=0.2803 --------- Run Conditions: vel=207.8 ft/s Re=2.005x10^6 AOA=19.99 Flap deflection=5.00 Totals: Cl=0.9396 Cdp=0.3743 Cm(c/4)=-0.1437 Cs=-0.0306 Ch=-0.2479 Main component: Cl=0.6751 Cdp=0.2587 Cm=-0.1698 Flap component: Cl=0.2645 Cdp=0.1156 Cm=-0.2266 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.0145 0.6175, -0.04610, -0.2017 0.5841, -0.02440, -0.2945 0.5775, 0.01750, -0.3452 0.5777, 0.04660, -0.2531 0.6274, 0.07170, -0.8192 0.5694, 0.08320, -0.8167 0.5112, 0.09370, -0.8048 0.4731, 0.09830, -0.8021 0.4349, 0.10070, -0.8270 0.3960, 0.10120, -0.8444 0.3566, 0.10020, -0.8650 0.3172, 0.09790, -0.8769 0.2778, 0.09440, -0.9068 0.2393, 0.08960, -0.9274 0.2056, 0.08360, -0.9670 0.1633, 0.07610, -1.0206 0.1261, 0.06710, -1.0798 0.0900, 0.05640, -1.1306 0.0571, 0.04390, -1.2027 0.0283, 0.02940, -1.3573 0.0142, 0.01970, -1.6737 0.0081, 0.01410, -1.9498 0.0026, 0.00780, -2.0771 0.0000, 0.00000, -0.1647 0.0037, -0.00840, -0.1270 0.0112, -0.01420, 0.7115 0.0191, -0.01930, 0.9283 0.0397, -0.03030, 1.0128 0.0706, -0.04420, 0.9389 0.1037, -0.05710, 0.8287 0.1384, -0.06890, 0.6914 0.1741, -0.07950, 0.5588 0.2102, -0.08660, 0.4186 0.2472, -0.09640, 0.2680 0.2844, -0.10270, 0.1360 0.3225, -0.10690, 0.0056 0.3608, -0.10890, -0.1121 0.3991, -0.10830, -0.2043 0.4373, -0.10510, -0.2466 0.4757, -0.09890, -0.2138 0.5137, -0.09070, -0.1794 0.5694, -0.07640, -0.0370 14 Flap element taps 1.0000, 0.00130, -0.6685 0.9365, 0.01390, -0.7362 0.8333, 0.03280, -0.7490 0.7436, 0.04930, -0.7497 0.7049, 0.05670, -0.7344 0.6662, 0.06410, -0.7232 0.6522, 0.01390, -0.3414 0.5969, -0.00020, -0.3561 0.6000, -0.03020, -0.3050 0.6324, -0.04540, -0.2732 0.6667, -0.04880, 0.6346 0.7046, -0.04110, 0.2724 0.7429, -0.03210, 0.2060 0.9311, -0.00120, -0.0159 --------- Run Conditions: vel=207.1 ft/s Re=1.993x10^6 AOA=23.98 Flap deflection=5.00 Totals: Cl=0.8947 Cdp=0.4742 Cm(c/4)=-0.1618 Cs=-0.0697 Ch=-0.2566 Main component: Cl=0.6272 Cdp=0.3345 Cm=-0.1778 Flap component: Cl=0.2675 Cdp=0.1397 Cm=-0.2365 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0040 0.6175, -0.04610, -0.2248 0.5841, -0.02440, -0.3246 0.5775, 0.01750, -0.3708 0.5777, 0.04660, -0.2695 0.6274, 0.07170, -0.9043 0.5694, 0.08320, -0.8830 0.5112, 0.09370, -0.8302 0.4731, 0.09830, -0.8303 0.4349, 0.10070, -0.8394 0.3960, 0.10120, -0.8358 0.3566, 0.10020, -0.8454 0.3172, 0.09790, -0.8530 0.2778, 0.09440, -0.8602 0.2393, 0.08960, -0.8728 0.2056, 0.08360, -0.8925 0.1633, 0.07610, -0.9195 0.1261, 0.06710, -0.9370 0.0900, 0.05640, -0.9530 0.0571, 0.04390, -0.9716 0.0283, 0.02940, -1.0083 0.0142, 0.01970, -1.0665 0.0081, 0.01410, -1.1309 0.0026, 0.00780, -1.0286 0.0000, 0.00000, -0.1693 0.0037, -0.00840, -0.0023 0.0112, -0.01420, 0.7023 0.0191, -0.01930, 0.9089 0.0397, -0.03030, 1.0120 0.0706, -0.04420, 0.9663 0.1037, -0.05710, 0.8742 0.1384, -0.06890, 0.7523 0.1741, -0.07950, 0.6296 0.2102, -0.08660, 0.4974 0.2472, -0.09640, 0.3519 0.2844, -0.10270, 0.2211 0.3225, -0.10690, 0.0876 0.3608, -0.10890, -0.0336 0.3991, -0.10830, -0.1318 0.4373, -0.10510, -0.1835 0.4757, -0.09890, -0.1632 0.5137, -0.09070, -0.1410 0.5694, -0.07640, -0.0368 14 Flap element taps 1.0000, 0.00130, -0.7447 0.9365, 0.01390, -0.7791 0.8333, 0.03280, -0.7941 0.7436, 0.04930, -0.7903 0.7049, 0.05670, -0.7797 0.6662, 0.06410, -0.7666 0.6522, 0.01390, -0.3741 0.5969, -0.00020, -0.3871 0.6000, -0.03020, -0.3318 0.6324, -0.04540, -0.3043 0.6667, -0.04880, 0.7072 0.7046, -0.04110, 0.2762 0.7429, -0.03210, 0.2064 0.9311, -0.00120, -0.0417 --------- Run Conditions: vel=209.7 ft/s Re=2.012x10^6 AOA=26.99 Flap deflection=5.00 Totals: Cl=0.9494 Cdp=0.5827 Cm(c/4)=-0.1929 Cs=-0.0883 Ch=-0.2904 Main component: Cl=0.6557 Cdp=0.4076 Cm=-0.2027 Flap component: Cl=0.2937 Cdp=0.1751 Cm=-0.2678 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, 0.0085 0.6175, -0.04610, -0.2761 0.5841, -0.02440, -0.3853 0.5775, 0.01750, -0.4425 0.5777, 0.04660, -0.3261 0.6274, 0.07170, -0.9837 0.5694, 0.08320, -0.9915 0.5112, 0.09370, -0.9693 0.4731, 0.09830, -0.9590 0.4349, 0.10070, -0.9499 0.3960, 0.10120, -0.9397 0.3566, 0.10020, -0.9373 0.3172, 0.09790, -0.9338 0.2778, 0.09440, -0.9351 0.2393, 0.08960, -0.9343 0.2056, 0.08360, -0.9368 0.1633, 0.07610, -0.9396 0.1261, 0.06710, -0.9390 0.0900, 0.05640, -0.9394 0.0571, 0.04390, -0.9406 0.0283, 0.02940, -0.9516 0.0142, 0.01970, -0.9712 0.0081, 0.01410, -0.9944 0.0026, 0.00780, -0.8899 0.0000, 0.00000, -0.1534 0.0037, -0.00840, -0.0431 0.0112, -0.01420, 0.6508 0.0191, -0.01930, 0.8718 0.0397, -0.03030, 1.0043 0.0706, -0.04420, 0.9836 0.1037, -0.05710, 0.9073 0.1384, -0.06890, 0.7978 0.1741, -0.07950, 0.6838 0.2102, -0.08660, 0.5583 0.2472, -0.09640, 0.4174 0.2844, -0.10270, 0.2881 0.3225, -0.10690, 0.1532 0.3608, -0.10890, 0.0292 0.3991, -0.10830, -0.0747 0.4373, -0.10510, -0.1347 0.4757, -0.09890, -0.1256 0.5137, -0.09070, -0.1152 0.5694, -0.07640, -0.0324 14 Flap element taps 1.0000, 0.00130, -0.8978 0.9365, 0.01390, -0.9267 0.8333, 0.03280, -0.9354 0.7436, 0.04930, -0.9319 0.7049, 0.05670, -0.9215 0.6662, 0.06410, -0.9111 0.6522, 0.01390, -0.4495 0.5969, -0.00020, -0.4627 0.6000, -0.03020, -0.3991 0.6324, -0.04540, -0.3747 0.6667, -0.04880, 0.7911 0.7046, -0.04110, 0.2727 0.7429, -0.03210, 0.1957 0.9311, -0.00120, -0.0923