S809 SPOILER FLAP, CLEAN, CHORD = 18 INCHES --------- Run Conditions: vel=105.7 ft/s Re=1.005x10^6 AOA=-6.01 Flap deflection=5.00 Totals: Cl=-0.3024 Cdp=-0.0247 Cm(c/4)=-0.0617 Cs=0.0563 Ch=0.0324 Main component: Cl=-0.3990 Cdp=-0.0124 Cm=0.0856 Flap component: Cl=0.0966 Cdp=-0.0123 Cm=-0.0727 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0636 0.5905, -0.01667, 0.2483 0.5709, 0.03110, 0.1482 0.5889, 0.07933, 0.1224 0.5500, 0.08689, -0.4008 0.5110, 0.09367, -0.4136 0.4731, 0.09830, -0.4683 0.4349, 0.10070, -0.4941 0.3960, 0.10120, -0.4564 0.3566, 0.10020, -0.4110 0.3172, 0.09790, -0.3434 0.2778, 0.09440, -0.3052 0.2393, 0.08960, -0.2474 0.2056, 0.08360, -0.1670 0.1633, 0.07610, -0.0740 0.1261, 0.06710, 0.0509 0.0900, 0.05640, 0.2070 0.0571, 0.04390, 0.4171 0.0283, 0.02940, 0.7056 0.0142, 0.01970, 0.9246 0.0081, 0.01410, 0.9931 0.0026, 0.00780, 0.8968 0.0000, 0.00000, 0.0252 0.0037, -0.00840, -0.9753 0.0112, -0.01420, -0.8852 0.0191, -0.01930, -0.7744 0.0397, -0.03030, -0.6575 0.0706, -0.04420, -0.6740 0.1037, -0.05710, -0.7361 0.1384, -0.06890, -0.8090 0.1741, -0.07950, -0.8754 0.2102, -0.08660, -0.9473 0.2472, -0.09640, -1.0321 0.2844, -0.10270, -1.0766 0.3225, -0.10690, -1.0876 0.3608, -0.10890, -1.0899 0.3991, -0.10830, -1.0485 0.4373, -0.10510, -0.9639 0.4757, -0.09890, -0.9571 0.5137, -0.09067, -0.3686 0.5611, -0.07859, -0.1701 16 Flap element taps 1.0000, 0.00130, 0.1728 0.9365, 0.01390, 0.0860 0.8333, 0.03280, -0.0452 0.7436, 0.04930, -0.1761 0.7049, 0.05667, -0.2199 0.6662, 0.06411, -0.3310 0.6274, 0.07172, -0.6389 0.6009, 0.07523, -1.3674 0.6069, 0.02889, 0.1197 0.6079, -0.01747, 0.2285 0.6167, -0.06381, -0.1025 0.6558, -0.05300, -0.1137 0.7045, -0.04117, -0.0269 0.7429, -0.03210, 0.0683 0.8333, -0.01400, 0.1590 0.9311, -0.00120, 0.2320 Wake drag found for this condition, Cdw=0.0202 --------- Run Conditions: vel=105.9 ft/s Re=1.005x10^6 AOA=-0.02 Flap deflection=5.00 Totals: Cl=0.3270 Cdp=-0.0252 Cm(c/4)=-0.0805 Cs=0.0251 Ch=0.0621 Main component: Cl=0.1574 Cdp=-0.0157 Cm=-0.0364 Flap component: Cl=0.1697 Cdp=-0.0094 Cm=-0.1259 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0664 0.5905, -0.01667, 0.1500 0.5709, 0.03110, 0.0721 0.5889, 0.07933, 0.0398 0.5500, 0.08689, -0.6182 0.5110, 0.09367, -0.6758 0.4731, 0.09830, -0.7143 0.4349, 0.10070, -0.7778 0.3960, 0.10120, -0.7841 0.3566, 0.10020, -0.7671 0.3172, 0.09790, -0.7331 0.2778, 0.09440, -0.7323 0.2393, 0.08960, -0.7187 0.2056, 0.08360, -0.6886 0.1633, 0.07610, -0.6435 0.1261, 0.06710, -0.5773 0.0900, 0.05640, -0.4956 0.0571, 0.04390, -0.3816 0.0283, 0.02940, -0.1955 0.0142, 0.01970, 0.0342 0.0081, 0.01410, 0.2020 0.0026, 0.00780, 0.4824 0.0000, 0.00000, 0.9461 0.0037, -0.00840, 0.8440 0.0112, -0.01420, 0.6140 0.0191, -0.01930, 0.4919 0.0397, -0.03030, 0.3060 0.0706, -0.04420, 0.1081 0.1037, -0.05710, -0.0435 0.1384, -0.06890, -0.1789 0.1741, -0.07950, -0.2973 0.2102, -0.08660, -0.4148 0.2472, -0.09640, -0.5309 0.2844, -0.10270, -0.6157 0.3225, -0.10690, -0.6656 0.3608, -0.10890, -0.7144 0.3991, -0.10830, -0.7218 0.4373, -0.10510, -0.6347 0.4757, -0.09890, -0.5886 0.5137, -0.09067, -0.3666 0.5611, -0.07859, -0.0706 16 Flap element taps 1.0000, 0.00130, 0.1467 0.9365, 0.01390, 0.0622 0.8333, 0.03280, -0.1006 0.7436, 0.04930, -0.2682 0.7049, 0.05667, -0.3458 0.6662, 0.06411, -0.5021 0.6274, 0.07172, -0.8983 0.6009, 0.07523, -1.7350 0.6069, 0.02889, 0.0438 0.6079, -0.01747, 0.1324 0.6167, -0.06381, 0.0337 0.6558, -0.05300, 0.0272 0.7045, -0.04117, 0.1050 0.7429, -0.03210, 0.1944 0.8333, -0.01400, 0.2475 0.9311, -0.00120, 0.2754 Wake drag found for this condition, Cdw=0.0216 --------- Run Conditions: vel=105.7 ft/s Re=1.004x10^6 AOA=2.98 Flap deflection=5.00 Totals: Cl=0.6270 Cdp=-0.0218 Cm(c/4)=-0.0849 Cs=0.0543 Ch=0.0836 Main component: Cl=0.4186 Cdp=-0.0297 Cm=-0.0876 Flap component: Cl=0.2084 Cdp=0.0080 Cm=-0.1535 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.1023 0.5905, -0.01667, 0.1696 0.5709, 0.03110, 0.1103 0.5889, 0.07933, 0.0889 0.5500, 0.08689, -0.2819 0.5110, 0.09367, -0.8247 0.4731, 0.09830, -0.8509 0.4349, 0.10070, -0.9175 0.3960, 0.10120, -0.9508 0.3566, 0.10020, -0.9417 0.3172, 0.09790, -0.9324 0.2778, 0.09440, -0.9585 0.2393, 0.08960, -0.9711 0.2056, 0.08360, -0.9759 0.1633, 0.07610, -0.9596 0.1261, 0.06710, -0.9420 0.0900, 0.05640, -0.9219 0.0571, 0.04390, -0.9056 0.0283, 0.02940, -0.8662 0.0142, 0.01970, -0.7756 0.0081, 0.01410, -0.7064 0.0026, 0.00780, -0.4506 0.0000, 0.00000, 0.1944 0.0037, -0.00840, 0.9897 0.0112, -0.01420, 0.9433 0.0191, -0.01930, 0.8423 0.0397, -0.03030, 0.6400 0.0706, -0.04420, 0.4142 0.1037, -0.05710, 0.2478 0.1384, -0.06890, 0.1016 0.1741, -0.07950, -0.0325 0.2102, -0.08660, -0.1675 0.2472, -0.09640, -0.2918 0.2844, -0.10270, -0.3936 0.3225, -0.10690, -0.4532 0.3608, -0.10890, -0.5249 0.3991, -0.10830, -0.5504 0.4373, -0.10510, -0.4864 0.4757, -0.09890, -0.4267 0.5137, -0.09067, -0.3984 0.5611, -0.07859, 0.0029 16 Flap element taps 1.0000, 0.00130, 0.1143 0.9365, 0.01390, 0.0378 0.8333, 0.03280, -0.1248 0.7436, 0.04930, -0.3080 0.7049, 0.05667, -0.4175 0.6662, 0.06411, -0.6205 0.6274, 0.07172, -1.2094 0.6009, 0.07523, -1.8674 0.6069, 0.02889, 0.0843 0.6079, -0.01747, 0.1533 0.6167, -0.06381, 0.0827 0.6558, -0.05300, 0.0775 0.7045, -0.04117, 0.1659 0.7429, -0.03210, 0.2446 0.8333, -0.01400, 0.2784 0.9311, -0.00120, 0.2889 Wake drag found for this condition, Cdw=0.0268 --------- Run Conditions: vel=105.5 ft/s Re=1.001x10^6 AOA=6.02 Flap deflection=5.00 Totals: Cl=0.8533 Cdp=0.0307 Cm(c/4)=-0.1102 Cs=0.0590 Ch=0.0644 Main component: Cl=0.5767 Cdp=-0.0160 Cm=-0.1096 Flap component: Cl=0.2766 Cdp=0.0467 Cm=-0.2136 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0109 0.5905, -0.01667, -0.0076 0.5709, 0.03110, -0.0154 0.5889, 0.07933, -0.0373 0.5500, 0.08689, -0.1946 0.5110, 0.09367, -0.5033 0.4731, 0.09830, -0.7169 0.4349, 0.10070, -0.8465 0.3960, 0.10120, -0.9224 0.3566, 0.10020, -0.9551 0.3172, 0.09790, -0.9997 0.2778, 0.09440, -1.0646 0.2393, 0.08960, -1.1140 0.2056, 0.08360, -1.1644 0.1633, 0.07610, -1.1804 0.1261, 0.06710, -1.2228 0.0900, 0.05640, -1.2694 0.0571, 0.04390, -1.3637 0.0283, 0.02940, -1.5008 0.0142, 0.01970, -1.5905 0.0081, 0.01410, -1.7673 0.0026, 0.00780, -1.5882 0.0000, 0.00000, -1.1136 0.0037, -0.00840, 0.7980 0.0112, -0.01420, 1.0088 0.0191, -0.01930, 0.9888 0.0397, -0.03030, 0.8396 0.0706, -0.04420, 0.6201 0.1037, -0.05710, 0.4515 0.1384, -0.06890, 0.3059 0.1741, -0.07950, 0.1668 0.2102, -0.08660, 0.0108 0.2472, -0.09640, -0.1176 0.2844, -0.10270, -0.2363 0.3225, -0.10690, -0.3056 0.3608, -0.10890, -0.4005 0.3991, -0.10830, -0.4441 0.4373, -0.10510, -0.4094 0.4757, -0.09890, -0.3451 0.5137, -0.09067, -0.2953 0.5611, -0.07859, 0.0374 16 Flap element taps 1.0000, 0.00130, -0.0813 0.9365, 0.01390, -0.1900 0.8333, 0.03280, -0.4461 0.7436, 0.04930, -0.6274 0.7049, 0.05667, -0.6424 0.6662, 0.06411, -0.6756 0.6274, 0.07172, -0.8414 0.6009, 0.07523, -1.0514 0.6069, 0.02889, -0.0288 0.6079, -0.01747, -0.0122 0.6167, -0.06381, 0.0018 0.6558, -0.05300, 0.0737 0.7045, -0.04117, 0.3925 0.7429, -0.03210, 0.3446 0.8333, -0.01400, 0.2951 0.9311, -0.00120, 0.2645 Wake drag found for this condition, Cdw=0.0337 --------- Run Conditions: vel=105.2 ft/s Re=0.997x10^6 AOA=9.05 Flap deflection=5.00 Totals: Cl=0.8450 Cdp=0.0458 Cm(c/4)=-0.0659 Cs=0.0877 Ch=0.0198 Main component: Cl=0.6397 Cdp=0.0105 Cm=-0.1129 Flap component: Cl=0.2053 Cdp=0.0353 Cm=-0.1634 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.0726 0.5905, -0.01667, -0.1534 0.5709, 0.03110, -0.1433 0.5889, 0.07933, -0.1579 0.5500, 0.08689, -0.1960 0.5110, 0.09367, -0.3535 0.4731, 0.09830, -0.5706 0.4349, 0.10070, -0.7422 0.3960, 0.10120, -0.8714 0.3566, 0.10020, -0.9040 0.3172, 0.09790, -0.9576 0.2778, 0.09440, -1.0412 0.2393, 0.08960, -1.1267 0.2056, 0.08360, -1.2239 0.1633, 0.07610, -1.2551 0.1261, 0.06710, -1.3355 0.0900, 0.05640, -1.4376 0.0571, 0.04390, -1.6519 0.0283, 0.02940, -1.9409 0.0142, 0.01970, -2.1956 0.0081, 0.01410, -2.4765 0.0026, 0.00780, -2.5343 0.0000, 0.00000, -2.3004 0.0037, -0.00840, 0.4930 0.0112, -0.01420, 0.9631 0.0191, -0.01930, 1.0145 0.0397, -0.03030, 0.9321 0.0706, -0.04420, 0.7281 0.1037, -0.05710, 0.5628 0.1384, -0.06890, 0.4319 0.1741, -0.07950, 0.2833 0.2102, -0.08660, 0.1086 0.2472, -0.09640, -0.0201 0.2844, -0.10270, -0.1576 0.3225, -0.10690, -0.2233 0.3608, -0.10890, -0.3446 0.3991, -0.10830, -0.3999 0.4373, -0.10510, -0.3925 0.4757, -0.09890, -0.3386 0.5137, -0.09067, -0.2719 0.5611, -0.07859, -0.0111 16 Flap element taps 1.0000, 0.00130, -0.2892 0.9365, 0.01390, -0.3693 0.8333, 0.03280, -0.3564 0.7436, 0.04930, -0.3386 0.7049, 0.05667, -0.3376 0.6662, 0.06411, -0.3659 0.6274, 0.07172, -0.3943 0.6009, 0.07523, -0.4726 0.6069, 0.02889, -0.1531 0.6079, -0.01747, -0.1512 0.6167, -0.06381, -0.1156 0.6558, -0.05300, 0.1452 0.7045, -0.04117, 0.4119 0.7429, -0.03210, 0.3072 0.8333, -0.01400, 0.2384 0.9311, -0.00120, 0.1698 --------- Run Conditions: vel=105.9 ft/s Re=1.004x10^6 AOA=12.02 Flap deflection=5.00 Totals: Cl=1.0018 Cdp=0.0652 Cm(c/4)=-0.0580 Cs=0.1448 Ch=0.0248 Main component: Cl=0.7905 Cdp=0.0297 Cm=-0.1389 Flap component: Cl=0.2114 Cdp=0.0355 Cm=-0.1675 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.0855 0.5905, -0.01667, -0.2750 0.5709, 0.03110, -0.2512 0.5889, 0.07933, -0.2837 0.5500, 0.08689, -0.2966 0.5110, 0.09367, -0.3447 0.4731, 0.09830, -0.4864 0.4349, 0.10070, -0.6751 0.3960, 0.10120, -0.8633 0.3566, 0.10020, -0.9154 0.3172, 0.09790, -1.0064 0.2778, 0.09440, -1.1194 0.2393, 0.08960, -1.2379 0.2056, 0.08360, -1.3853 0.1633, 0.07610, -1.4444 0.1261, 0.06710, -1.5987 0.0900, 0.05640, -1.7648 0.0571, 0.04390, -2.0582 0.0283, 0.02940, -2.5269 0.0142, 0.01970, -3.1474 0.0081, 0.01410, -3.8473 0.0026, 0.00780, -4.0554 0.0000, 0.00000, -4.3196 0.0037, -0.00840, -0.1373 0.0112, -0.01420, 0.7843 0.0191, -0.01930, 0.9808 0.0397, -0.03030, 1.0082 0.0706, -0.04420, 0.8480 0.1037, -0.05710, 0.7016 0.1384, -0.06890, 0.5950 0.1741, -0.07950, 0.4448 0.2102, -0.08660, 0.2531 0.2472, -0.09640, 0.1325 0.2844, -0.10270, -0.0174 0.3225, -0.10690, -0.0786 0.3608, -0.10890, -0.2191 0.3991, -0.10830, -0.2798 0.4373, -0.10510, -0.3001 0.4757, -0.09890, -0.2648 0.5137, -0.09067, -0.1886 0.5611, -0.07859, -0.1070 16 Flap element taps 1.0000, 0.00130, -0.3213 0.9365, 0.01390, -0.3613 0.8333, 0.03280, -0.3626 0.7436, 0.04930, -0.3420 0.7049, 0.05667, -0.3355 0.6662, 0.06411, -0.3568 0.6274, 0.07172, -0.3517 0.6009, 0.07523, -0.3585 0.6069, 0.02889, -0.2665 0.6079, -0.01747, -0.2682 0.6167, -0.06381, -0.1917 0.6558, -0.05300, 0.3442 0.7045, -0.04117, 0.4370 0.7429, -0.03210, 0.3148 0.8333, -0.01400, 0.2439 0.9311, -0.00120, 0.1661 --------- Run Conditions: vel=105.9 ft/s Re=1.004x10^6 AOA=15.01 Flap deflection=5.00 Totals: Cl=1.1059 Cdp=0.0972 Cm(c/4)=-0.0631 Cs=0.1925 Ch=0.0331 Main component: Cl=0.8705 Cdp=0.0496 Cm=-0.1498 Flap component: Cl=0.2354 Cdp=0.0476 Cm=-0.1866 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1150 0.5905, -0.01667, -0.3914 0.5709, 0.03110, -0.3547 0.5889, 0.07933, -0.3905 0.5500, 0.08689, -0.3967 0.5110, 0.09367, -0.4021 0.4731, 0.09830, -0.4213 0.4349, 0.10070, -0.4992 0.3960, 0.10120, -0.6517 0.3566, 0.10020, -0.7980 0.3172, 0.09790, -0.9300 0.2778, 0.09440, -1.0769 0.2393, 0.08960, -1.2289 0.2056, 0.08360, -1.3939 0.1633, 0.07610, -1.5403 0.1261, 0.06710, -1.7288 0.0900, 0.05640, -1.9940 0.0571, 0.04390, -2.4000 0.0283, 0.02940, -3.0788 0.0142, 0.01970, -3.7269 0.0081, 0.01410, -5.1582 0.0026, 0.00780, -5.5106 0.0000, 0.00000, -6.3391 0.0037, -0.00840, -0.8749 0.0112, -0.01420, 0.5061 0.0191, -0.01930, 0.8524 0.0397, -0.03030, 0.9952 0.0706, -0.04420, 0.9271 0.1037, -0.05710, 0.8042 0.1384, -0.06890, 0.6662 0.1741, -0.07950, 0.5361 0.2102, -0.08660, 0.3863 0.2472, -0.09640, 0.2485 0.2844, -0.10270, 0.1093 0.3225, -0.10690, -0.0015 0.3608, -0.10890, -0.1253 0.3991, -0.10830, -0.2037 0.4373, -0.10510, -0.2309 0.4757, -0.09890, -0.2012 0.5137, -0.09067, -0.1361 0.5611, -0.07859, -0.0862 16 Flap element taps 1.0000, 0.00130, -0.4083 0.9365, 0.01390, -0.4383 0.8333, 0.03280, -0.4355 0.7436, 0.04930, -0.4153 0.7049, 0.05667, -0.4079 0.6662, 0.06411, -0.4108 0.6274, 0.07172, -0.4083 0.6009, 0.07523, -0.4118 0.6069, 0.02889, -0.3690 0.6079, -0.01747, -0.3764 0.6167, -0.06381, -0.2536 0.6558, -0.05300, 0.5025 0.7045, -0.04117, 0.4237 0.7429, -0.03210, 0.3206 0.8333, -0.01400, 0.2304 0.9311, -0.00120, 0.1259 --------- Run Conditions: vel=103.8 ft/s Re=0.985x10^6 AOA=17.98 Flap deflection=5.00 Totals: Cl=0.7321 Cdp=0.3124 Cm(c/4)=-0.1429 Cs=-0.0711 Ch=0.0443 Main component: Cl=0.4382 Cdp=0.2380 Cm=-0.1060 Flap component: Cl=0.2939 Cdp=0.0743 Cm=-0.2351 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3044 0.5905, -0.01667, -0.6847 0.5709, 0.03110, -0.6361 0.5889, 0.07933, -0.7389 0.5500, 0.08689, -0.7290 0.5110, 0.09367, -0.7259 0.4731, 0.09830, -0.6970 0.4349, 0.10070, -0.7062 0.3960, 0.10120, -0.7364 0.3566, 0.10020, -0.7288 0.3172, 0.09790, -0.7362 0.2778, 0.09440, -0.7384 0.2393, 0.08960, -0.7396 0.2056, 0.08360, -0.7670 0.1633, 0.07610, -0.7510 0.1261, 0.06710, -0.7694 0.0900, 0.05640, -0.7650 0.0571, 0.04390, -0.7958 0.0283, 0.02940, -0.8226 0.0142, 0.01970, -0.8329 0.0081, 0.01410, -0.8564 0.0026, 0.00780, -0.8246 0.0000, 0.00000, -1.1454 0.0037, -0.00840, 0.5240 0.0112, -0.01420, 0.9293 0.0191, -0.01930, 0.9943 0.0397, -0.03030, 0.9517 0.0706, -0.04420, 0.8132 0.1037, -0.05710, 0.6668 0.1384, -0.06890, 0.5306 0.1741, -0.07950, 0.3917 0.2102, -0.08660, 0.2275 0.2472, -0.09640, 0.0855 0.2844, -0.10270, -0.0627 0.3225, -0.10690, -0.1759 0.3608, -0.10890, -0.3106 0.3991, -0.10830, -0.3880 0.4373, -0.10510, -0.4207 0.4757, -0.09890, -0.3831 0.5137, -0.09067, -0.3107 0.5611, -0.07859, -0.2530 16 Flap element taps 1.0000, 0.00130, -0.6553 0.9365, 0.01390, -0.7040 0.8333, 0.03280, -0.7339 0.7436, 0.04930, -0.7221 0.7049, 0.05667, -0.7120 0.6662, 0.06411, -0.7114 0.6274, 0.07172, -0.6942 0.6009, 0.07523, -0.6953 0.6069, 0.02889, -0.6578 0.6079, -0.01747, -0.6650 0.6167, -0.06381, -0.4984 0.6558, -0.05300, 0.4788 0.7045, -0.04117, 0.3327 0.7429, -0.03210, 0.2123 0.8333, -0.01400, 0.1110 0.9311, -0.00120, -0.0180 --------- Run Conditions: vel=104.0 ft/s Re=0.985x10^6 AOA=19.99 Flap deflection=5.00 Totals: Cl=0.7141 Cdp=0.3440 Cm(c/4)=-0.1415 Cs=-0.0791 Ch=0.0465 Main component: Cl=0.4265 Cdp=0.2669 Cm=-0.1085 Flap component: Cl=0.2876 Cdp=0.0771 Cm=-0.2301 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3294 0.5905, -0.01667, -0.7374 0.5709, 0.03110, -0.6861 0.5889, 0.07933, -0.7622 0.5500, 0.08689, -0.7482 0.5110, 0.09367, -0.7313 0.4731, 0.09830, -0.7151 0.4349, 0.10070, -0.7151 0.3960, 0.10120, -0.7530 0.3566, 0.10020, -0.7258 0.3172, 0.09790, -0.7279 0.2778, 0.09440, -0.7243 0.2393, 0.08960, -0.7224 0.2056, 0.08360, -0.7548 0.1633, 0.07610, -0.7200 0.1261, 0.06710, -0.7408 0.0900, 0.05640, -0.7220 0.0571, 0.04390, -0.7358 0.0283, 0.02940, -0.7536 0.0142, 0.01970, -0.7565 0.0081, 0.01410, -0.7836 0.0026, 0.00780, -0.7376 0.0000, 0.00000, -1.0326 0.0037, -0.00840, 0.5226 0.0112, -0.01420, 0.9267 0.0191, -0.01930, 0.9973 0.0397, -0.03030, 0.9628 0.0706, -0.04420, 0.8303 0.1037, -0.05710, 0.6874 0.1384, -0.06890, 0.5632 0.1741, -0.07950, 0.4242 0.2102, -0.08660, 0.2485 0.2472, -0.09640, 0.1134 0.2844, -0.10270, -0.0428 0.3225, -0.10690, -0.1496 0.3608, -0.10890, -0.2946 0.3991, -0.10830, -0.3713 0.4373, -0.10510, -0.4164 0.4757, -0.09890, -0.3826 0.5137, -0.09067, -0.3109 0.5611, -0.07859, -0.2532 16 Flap element taps 1.0000, 0.00130, -0.6576 0.9365, 0.01390, -0.6904 0.8333, 0.03280, -0.7184 0.7436, 0.04930, -0.7073 0.7049, 0.05667, -0.7009 0.6662, 0.06411, -0.7140 0.6274, 0.07172, -0.7037 0.6009, 0.07523, -0.6950 0.6069, 0.02889, -0.7013 0.6079, -0.01747, -0.7118 0.6167, -0.06381, -0.5313 0.6558, -0.05300, 0.5149 0.7045, -0.04117, 0.3255 0.7429, -0.03210, 0.2010 0.8333, -0.01400, 0.0983 0.9311, -0.00120, -0.0294 --------- Run Conditions: vel=105.7 ft/s Re=1.001x10^6 AOA=24.01 Flap deflection=5.00 Totals: Cl=0.7947 Cdp=0.4472 Cm(c/4)=-0.1628 Cs=-0.0852 Ch=0.0536 Main component: Cl=0.4864 Cdp=0.3389 Cm=-0.1375 Flap component: Cl=0.3083 Cdp=0.1083 Cm=-0.2523 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3155 0.5905, -0.01667, -0.8010 0.5709, 0.03110, -0.7394 0.5889, 0.07933, -0.8196 0.5500, 0.08689, -0.8134 0.5110, 0.09367, -0.7968 0.4731, 0.09830, -0.7778 0.4349, 0.10070, -0.7732 0.3960, 0.10120, -0.8168 0.3566, 0.10020, -0.7805 0.3172, 0.09790, -0.7820 0.2778, 0.09440, -0.7777 0.2393, 0.08960, -0.7777 0.2056, 0.08360, -0.8159 0.1633, 0.07610, -0.7707 0.1261, 0.06710, -0.7967 0.0900, 0.05640, -0.7709 0.0571, 0.04390, -0.7845 0.0283, 0.02940, -0.7938 0.0142, 0.01970, -0.7922 0.0081, 0.01410, -0.8285 0.0026, 0.00780, -0.7746 0.0000, 0.00000, -0.9838 0.0037, -0.00840, 0.3185 0.0112, -0.01420, 0.8365 0.0191, -0.01930, 0.9658 0.0397, -0.03030, 0.9961 0.0706, -0.04420, 0.9038 0.1037, -0.05710, 0.7845 0.1384, -0.06890, 0.6838 0.1741, -0.07950, 0.5512 0.2102, -0.08660, 0.3741 0.2472, -0.09640, 0.2486 0.2844, -0.10270, 0.0879 0.3225, -0.10690, -0.0158 0.3608, -0.10890, -0.1692 0.3991, -0.10830, -0.2531 0.4373, -0.10510, -0.3157 0.4757, -0.09890, -0.3027 0.5137, -0.09067, -0.2348 0.5611, -0.07859, -0.1634 16 Flap element taps 1.0000, 0.00130, -0.7431 0.9365, 0.01390, -0.7615 0.8333, 0.03280, -0.7918 0.7436, 0.04930, -0.7790 0.7049, 0.05667, -0.7678 0.6662, 0.06411, -0.7832 0.6274, 0.07172, -0.7694 0.6009, 0.07523, -0.7590 0.6069, 0.02889, -0.7554 0.6079, -0.01747, -0.7682 0.6167, -0.06381, -0.5648 0.6558, -0.05300, 0.6191 0.7045, -0.04117, 0.3416 0.7429, -0.03210, 0.2086 0.8333, -0.01400, 0.1002 0.9311, -0.00120, -0.0441 --------- Run Conditions: vel=104.6 ft/s Re=0.990x10^6 AOA=27.01 Flap deflection=5.00 Totals: Cl=0.9535 Cdp=0.5881 Cm(c/4)=-0.2035 Cs=-0.0909 Ch=0.0623 Main component: Cl=0.5978 Cdp=0.4392 Cm=-0.1846 Flap component: Cl=0.3557 Cdp=0.1488 Cm=-0.2980 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3217 0.5905, -0.01667, -0.9677 0.5709, 0.03110, -0.8992 0.5889, 0.07933, -1.0008 0.5500, 0.08689, -0.9926 0.5110, 0.09367, -0.9754 0.4731, 0.09830, -0.9571 0.4349, 0.10070, -0.9534 0.3960, 0.10120, -1.0053 0.3566, 0.10020, -0.9587 0.3172, 0.09790, -0.9597 0.2778, 0.09440, -0.9507 0.2393, 0.08960, -0.9500 0.2056, 0.08360, -0.9947 0.1633, 0.07610, -0.9390 0.1261, 0.06710, -0.9716 0.0900, 0.05640, -0.9427 0.0571, 0.04390, -0.9591 0.0283, 0.02940, -0.9615 0.0142, 0.01970, -0.9597 0.0081, 0.01410, -1.0033 0.0026, 0.00780, -0.9423 0.0000, 0.00000, -0.9887 0.0037, -0.00840, 0.0498 0.0112, -0.01420, 0.7006 0.0191, -0.01930, 0.8985 0.0397, -0.03030, 1.0007 0.0706, -0.04420, 0.9513 0.1037, -0.05710, 0.8573 0.1384, -0.06890, 0.7797 0.1741, -0.07950, 0.6587 0.2102, -0.08660, 0.4794 0.2472, -0.09640, 0.3648 0.2844, -0.10270, 0.2033 0.3225, -0.10690, 0.1067 0.3608, -0.10890, -0.0570 0.3991, -0.10830, -0.1448 0.4373, -0.10510, -0.2268 0.4757, -0.09890, -0.2309 0.5137, -0.09067, -0.1728 0.5611, -0.07859, -0.1126 16 Flap element taps 1.0000, 0.00130, -0.9362 0.9365, 0.01390, -0.9509 0.8333, 0.03280, -0.9723 0.7436, 0.04930, -0.9576 0.7049, 0.05667, -0.9477 0.6662, 0.06411, -0.9639 0.6274, 0.07172, -0.9468 0.6009, 0.07523, -0.9321 0.6069, 0.02889, -0.9202 0.6079, -0.01747, -0.9402 0.6167, -0.06381, -0.6640 0.6558, -0.05300, 0.6764 0.7045, -0.04117, 0.3391 0.7429, -0.03210, 0.2078 0.8333, -0.01400, 0.0838 0.9311, -0.00120, -0.0955