S809 SPOILER FLAP, CLEAN, CHORD = 18 INCHES --------- Run Conditions: vel=106.3 ft/s Re=1.008x10^6 AOA=-6.01 Flap deflection=10.00 Totals: Cl=-0.3434 Cdp=0.0189 Cm(c/4)=-0.0905 Cs=0.0171 Ch=0.0471 Main component: Cl=-0.5207 Cdp=-0.0257 Cm=0.1246 Flap component: Cl=0.1774 Cdp=0.0447 Cm=-0.1292 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.1072 0.5905, -0.01667, 0.2618 0.5709, 0.03110, 0.3115 0.5889, 0.07933, 0.2441 0.5500, 0.08689, 0.0454 0.5110, 0.09367, -0.1930 0.4731, 0.09830, -0.1822 0.4349, 0.10070, -0.2367 0.3960, 0.10120, -0.2493 0.3566, 0.10020, -0.2554 0.3172, 0.09790, -0.2164 0.2778, 0.09440, -0.1885 0.2393, 0.08960, -0.1351 0.2056, 0.08360, -0.0568 0.1633, 0.07610, 0.0110 0.1261, 0.06710, 0.1426 0.0900, 0.05640, 0.2832 0.0571, 0.04390, 0.4913 0.0283, 0.02940, 0.7619 0.0142, 0.01970, 0.9544 0.0081, 0.01410, 1.0056 0.0026, 0.00780, 0.7710 0.0000, 0.00000, -0.2470 0.0037, -0.00840, -1.2587 0.0112, -0.01420, -1.0839 0.0191, -0.01930, -0.9321 0.0397, -0.03030, -0.7795 0.0706, -0.04420, -0.7581 0.1037, -0.05710, -0.8052 0.1384, -0.06890, -0.8891 0.1741, -0.07950, -0.9450 0.2102, -0.08660, -0.9923 0.2472, -0.09640, -1.0838 0.2844, -0.10270, -1.1048 0.3225, -0.10690, -1.1441 0.3608, -0.10890, -1.1237 0.3991, -0.10830, -1.0697 0.4373, -0.10510, -0.9970 0.4757, -0.09890, -0.9605 0.5137, -0.09067, -0.3518 0.5611, -0.07859, -0.1411 16 Flap element taps 1.0000, 0.00130, -0.0718 0.9365, 0.01390, -0.1682 0.8333, 0.03280, -0.3376 0.7436, 0.04930, -0.5400 0.7049, 0.05667, -0.6577 0.6662, 0.06411, -0.7528 0.6274, 0.07172, -0.8280 0.6009, 0.07523, -1.0780 0.6069, 0.02889, 0.2699 0.6079, -0.01747, 0.2888 0.6167, -0.06381, -0.1307 0.6558, -0.05300, -0.1532 0.7045, -0.04117, -0.1463 0.7429, -0.03210, -0.0416 0.8333, -0.01400, 0.1103 0.9311, -0.00120, 0.1493 --------- Run Conditions: vel=106.5 ft/s Re=1.008x10^6 AOA=-0.01 Flap deflection=10.00 Totals: Cl=-0.0354 Cdp=0.0233 Cm(c/4)=-0.0518 Cs=-0.0233 Ch=-0.0062 Main component: Cl=-0.1682 Cdp=-0.0616 Cm=0.0634 Flap component: Cl=0.1328 Cdp=0.0849 Cm=-0.1064 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.1501 0.5905, -0.01667, 0.3807 0.5709, 0.03110, 0.4879 0.5889, 0.07933, 0.4205 0.5500, 0.08689, 0.2762 0.5110, 0.09367, -0.1211 0.4731, 0.09830, -0.2906 0.4349, 0.10070, -0.3189 0.3960, 0.10120, -0.3471 0.3566, 0.10020, -0.4084 0.3172, 0.09790, -0.4083 0.2778, 0.09440, -0.4249 0.2393, 0.08960, -0.4141 0.2056, 0.08360, -0.3695 0.1633, 0.07610, -0.3655 0.1261, 0.06710, -0.2771 0.0900, 0.05640, -0.2054 0.0571, 0.04390, -0.0629 0.0283, 0.02940, 0.1571 0.0142, 0.01970, 0.4174 0.0081, 0.01410, 0.6080 0.0026, 0.00780, 0.8148 0.0000, 0.00000, 0.9747 0.0037, -0.00840, 0.5179 0.0112, -0.01420, 0.2870 0.0191, -0.01930, 0.1939 0.0397, -0.03030, 0.0484 0.0706, -0.04420, -0.1012 0.1037, -0.05710, -0.2364 0.1384, -0.06890, -0.3962 0.1741, -0.07950, -0.5015 0.2102, -0.08660, -0.5804 0.2472, -0.09640, -0.7158 0.2844, -0.10270, -0.7729 0.3225, -0.10690, -0.8639 0.3608, -0.10890, -0.8837 0.3991, -0.10830, -0.8789 0.4373, -0.10510, -0.7772 0.4757, -0.09890, -0.7416 0.5137, -0.09067, -0.3068 0.5611, -0.07859, -0.0905 16 Flap element taps 1.0000, 0.00130, -0.3651 0.9365, 0.01390, -0.4497 0.8333, 0.03280, -0.4348 0.7436, 0.04930, -0.4259 0.7049, 0.05667, -0.4227 0.6662, 0.06411, -0.4254 0.6274, 0.07172, -0.4307 0.6009, 0.07523, -0.5816 0.6069, 0.02889, 0.4469 0.6079, -0.01747, 0.4402 0.6167, -0.06381, -0.1951 0.6558, -0.05300, -0.2163 0.7045, -0.04117, -0.2086 0.7429, -0.03210, -0.0780 0.8333, -0.01400, 0.0848 0.9311, -0.00120, 0.0419 --------- Run Conditions: vel=106.6 ft/s Re=1.010x10^6 AOA=2.99 Flap deflection=10.00 Totals: Cl=0.1999 Cdp=0.0294 Cm(c/4)=-0.0492 Cs=-0.0190 Ch=-0.0015 Main component: Cl=0.0505 Cdp=-0.0636 Cm=0.0231 Flap component: Cl=0.1494 Cdp=0.0930 Cm=-0.1226 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.1619 0.5905, -0.01667, 0.3641 0.5709, 0.03110, 0.4697 0.5889, 0.07933, 0.4100 0.5500, 0.08689, 0.2604 0.5110, 0.09367, -0.0243 0.4731, 0.09830, -0.3979 0.4349, 0.10070, -0.4341 0.3960, 0.10120, -0.4475 0.3566, 0.10020, -0.5320 0.3172, 0.09790, -0.5510 0.2778, 0.09440, -0.5908 0.2393, 0.08960, -0.6027 0.2056, 0.08360, -0.5773 0.1633, 0.07610, -0.6148 0.1261, 0.06710, -0.5600 0.0900, 0.05640, -0.5432 0.0571, 0.04390, -0.4703 0.0283, 0.02940, -0.3526 0.0142, 0.01970, -0.1643 0.0081, 0.01410, 0.0070 0.0026, 0.00780, 0.2146 0.0000, 0.00000, 0.7901 0.0037, -0.00840, 0.9347 0.0112, -0.01420, 0.7482 0.0191, -0.01930, 0.6216 0.0397, -0.03030, 0.4094 0.0706, -0.04420, 0.2162 0.1037, -0.05710, 0.0580 0.1384, -0.06890, -0.1347 0.1741, -0.07950, -0.2558 0.2102, -0.08660, -0.3403 0.2472, -0.09640, -0.4934 0.2844, -0.10270, -0.5632 0.3225, -0.10690, -0.6789 0.3608, -0.10890, -0.7135 0.3991, -0.10830, -0.7387 0.4373, -0.10510, -0.6427 0.4757, -0.09890, -0.5898 0.5137, -0.09067, -0.5362 0.5611, -0.07859, -0.0452 16 Flap element taps 1.0000, 0.00130, -0.3867 0.9365, 0.01390, -0.4716 0.8333, 0.03280, -0.4488 0.7436, 0.04930, -0.4354 0.7049, 0.05667, -0.4394 0.6662, 0.06411, -0.4355 0.6274, 0.07172, -0.4413 0.6009, 0.07523, -0.5892 0.6069, 0.02889, 0.4199 0.6079, -0.01747, 0.4142 0.6167, -0.06381, -0.1423 0.6558, -0.05300, -0.1626 0.7045, -0.04117, -0.1434 0.7429, -0.03210, -0.0033 0.8333, -0.01400, 0.1241 0.9311, -0.00120, 0.0530 --------- Run Conditions: vel=106.5 ft/s Re=1.008x10^6 AOA=6.00 Flap deflection=10.00 Totals: Cl=0.4881 Cdp=0.0400 Cm(c/4)=-0.0566 Cs=0.0113 Ch=0.0069 Main component: Cl=0.3100 Cdp=-0.0527 Cm=-0.0314 Flap component: Cl=0.1781 Cdp=0.0927 Cm=-0.1476 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.1421 0.5905, -0.01667, 0.2812 0.5709, 0.03110, 0.2909 0.5889, 0.07933, 0.2587 0.5500, 0.08689, 0.1865 0.5110, 0.09367, -0.0917 0.4731, 0.09830, -0.3328 0.4349, 0.10070, -0.4972 0.3960, 0.10120, -0.5833 0.3566, 0.10020, -0.6977 0.3172, 0.09790, -0.7331 0.2778, 0.09440, -0.7929 0.2393, 0.08960, -0.8295 0.2056, 0.08360, -0.8302 0.1633, 0.07610, -0.9143 0.1261, 0.06710, -0.9022 0.0900, 0.05640, -0.9561 0.0571, 0.04390, -0.9866 0.0283, 0.02940, -1.0321 0.0142, 0.01970, -1.0090 0.0081, 0.01410, -0.9631 0.0026, 0.00780, -0.8096 0.0000, 0.00000, -0.2222 0.0037, -0.00840, 0.9429 0.0112, -0.01420, 0.9786 0.0191, -0.01930, 0.9026 0.0397, -0.03030, 0.7021 0.0706, -0.04420, 0.5009 0.1037, -0.05710, 0.3349 0.1384, -0.06890, 0.1213 0.1741, -0.07950, -0.0101 0.2102, -0.08660, -0.0966 0.2472, -0.09640, -0.2629 0.2844, -0.10270, -0.3424 0.3225, -0.10690, -0.4785 0.3608, -0.10890, -0.5272 0.3991, -0.10830, -0.5796 0.4373, -0.10510, -0.5050 0.4757, -0.09890, -0.4364 0.5137, -0.09067, -0.4081 0.5611, -0.07859, 0.0115 16 Flap element taps 1.0000, 0.00130, -0.4090 0.9365, 0.01390, -0.4906 0.8333, 0.03280, -0.4610 0.7436, 0.04930, -0.4476 0.7049, 0.05667, -0.4473 0.6662, 0.06411, -0.4379 0.6274, 0.07172, -0.4458 0.6009, 0.07523, -0.6468 0.6069, 0.02889, 0.2556 0.6079, -0.01747, 0.2834 0.6167, -0.06381, -0.0310 0.6558, -0.05300, -0.0478 0.7045, -0.04117, -0.0209 0.7429, -0.03210, 0.0990 0.8333, -0.01400, 0.1810 0.9311, -0.00120, 0.0766 --------- Run Conditions: vel=106.5 ft/s Re=1.008x10^6 AOA=9.00 Flap deflection=10.00 Totals: Cl=0.7244 Cdp=0.0749 Cm(c/4)=-0.0755 Cs=0.0394 Ch=0.0153 Main component: Cl=0.4973 Cdp=-0.0107 Cm=-0.0701 Flap component: Cl=0.2270 Cdp=0.0856 Cm=-0.1872 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.0134 0.5905, -0.01667, -0.0402 0.5709, 0.03110, -0.0170 0.5889, 0.07933, -0.0400 0.5500, 0.08689, -0.0352 0.5110, 0.09367, -0.0955 0.4731, 0.09830, -0.2861 0.4349, 0.10070, -0.4893 0.3960, 0.10120, -0.5764 0.3566, 0.10020, -0.7337 0.3172, 0.09790, -0.7971 0.2778, 0.09440, -0.8920 0.2393, 0.08960, -0.9692 0.2056, 0.08360, -0.9994 0.1633, 0.07610, -1.1229 0.1261, 0.06710, -1.1689 0.0900, 0.05640, -1.3198 0.0571, 0.04390, -1.4603 0.0283, 0.02940, -1.6998 0.0142, 0.01970, -1.8777 0.0081, 0.01410, -2.0311 0.0026, 0.00780, -2.0462 0.0000, 0.00000, -1.7591 0.0037, -0.00840, 0.6285 0.0112, -0.01420, 0.9843 0.0191, -0.01930, 0.9988 0.0397, -0.03030, 0.8731 0.0706, -0.04420, 0.6915 0.1037, -0.05710, 0.5310 0.1384, -0.06890, 0.3118 0.1741, -0.07950, 0.1790 0.2102, -0.08660, 0.0859 0.2472, -0.09640, -0.0879 0.2844, -0.10270, -0.1798 0.3225, -0.10690, -0.3303 0.3608, -0.10890, -0.3964 0.3991, -0.10830, -0.4728 0.4373, -0.10510, -0.4268 0.4757, -0.09890, -0.3586 0.5137, -0.09067, -0.3073 0.5611, -0.07859, 0.0253 16 Flap element taps 1.0000, 0.00130, -0.4186 0.9365, 0.01390, -0.4867 0.8333, 0.03280, -0.4592 0.7436, 0.04930, -0.4550 0.7049, 0.05667, -0.4581 0.6662, 0.06411, -0.4526 0.6274, 0.07172, -0.4650 0.6009, 0.07523, -0.5115 0.6069, 0.02889, -0.0233 0.6079, -0.01747, -0.0337 0.6167, -0.06381, 0.0079 0.6558, -0.05300, -0.0164 0.7045, -0.04117, 0.2097 0.7429, -0.03210, 0.4334 0.8333, -0.01400, 0.2879 0.9311, -0.00120, 0.1265 --------- Run Conditions: vel=106.5 ft/s Re=1.008x10^6 AOA=12.01 Flap deflection=10.00 Totals: Cl=0.9482 Cdp=0.0981 Cm(c/4)=-0.0782 Cs=0.1014 Ch=0.0200 Main component: Cl=0.7057 Cdp=0.0160 Cm=-0.1152 Flap component: Cl=0.2425 Cdp=0.0821 Cm=-0.1999 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.0169 0.5905, -0.01667, -0.2501 0.5709, 0.03110, -0.1850 0.5889, 0.07933, -0.2203 0.5500, 0.08689, -0.2138 0.5110, 0.09367, -0.2386 0.4731, 0.09830, -0.3130 0.4349, 0.10070, -0.4861 0.3960, 0.10120, -0.6073 0.3566, 0.10020, -0.7892 0.3172, 0.09790, -0.8894 0.2778, 0.09440, -1.0168 0.2393, 0.08960, -1.1260 0.2056, 0.08360, -1.2057 0.1633, 0.07610, -1.3719 0.1261, 0.06710, -1.4671 0.0900, 0.05640, -1.6780 0.0571, 0.04390, -1.9395 0.0283, 0.02940, -2.3843 0.0142, 0.01970, -2.9889 0.0081, 0.01410, -3.4946 0.0026, 0.00780, -3.7185 0.0000, 0.00000, -3.9596 0.0037, -0.00840, -0.0362 0.0112, -0.01420, 0.8090 0.0191, -0.01930, 0.9766 0.0397, -0.03030, 0.9724 0.0706, -0.04420, 0.8416 0.1037, -0.05710, 0.7016 0.1384, -0.06890, 0.4983 0.1741, -0.07950, 0.3657 0.2102, -0.08660, 0.2669 0.2472, -0.09640, 0.0970 0.2844, -0.10270, -0.0043 0.3225, -0.10690, -0.1516 0.3608, -0.10890, -0.2363 0.3991, -0.10830, -0.3232 0.4373, -0.10510, -0.3043 0.4757, -0.09890, -0.2565 0.5137, -0.09067, -0.1914 0.5611, -0.07859, -0.0143 16 Flap element taps 1.0000, 0.00130, -0.4227 0.9365, 0.01390, -0.4713 0.8333, 0.03280, -0.4480 0.7436, 0.04930, -0.4446 0.7049, 0.05667, -0.4494 0.6662, 0.06411, -0.4456 0.6274, 0.07172, -0.4553 0.6009, 0.07523, -0.4773 0.6069, 0.02889, -0.1882 0.6079, -0.01747, -0.2158 0.6167, -0.06381, -0.0687 0.6558, -0.05300, -0.0430 0.7045, -0.04117, 0.5006 0.7429, -0.03210, 0.5176 0.8333, -0.01400, 0.3065 0.9311, -0.00120, 0.1505 --------- Run Conditions: vel=106.5 ft/s Re=1.007x10^6 AOA=15.01 Flap deflection=10.00 Totals: Cl=1.1230 Cdp=0.1316 Cm(c/4)=-0.0809 Cs=0.1637 Ch=0.0225 Main component: Cl=0.8689 Cdp=0.0481 Cm=-0.1506 Flap component: Cl=0.2541 Cdp=0.0836 Cm=-0.2100 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0072 0.5905, -0.01667, -0.4568 0.5709, 0.03110, -0.3372 0.5889, 0.07933, -0.3952 0.5500, 0.08689, -0.3813 0.5110, 0.09367, -0.4014 0.4731, 0.09830, -0.4000 0.4349, 0.10070, -0.4553 0.3960, 0.10120, -0.5915 0.3566, 0.10020, -0.7368 0.3172, 0.09790, -0.8750 0.2778, 0.09440, -1.0454 0.2393, 0.08960, -1.1943 0.2056, 0.08360, -1.3623 0.1633, 0.07610, -1.5228 0.1261, 0.06710, -1.7033 0.0900, 0.05640, -1.9793 0.0571, 0.04390, -2.3864 0.0283, 0.02940, -3.0751 0.0142, 0.01970, -3.7332 0.0081, 0.01410, -5.1804 0.0026, 0.00780, -5.5120 0.0000, 0.00000, -6.3740 0.0037, -0.00840, -0.8897 0.0112, -0.01420, 0.4976 0.0191, -0.01930, 0.8518 0.0397, -0.03030, 1.0064 0.0706, -0.04420, 0.9327 0.1037, -0.05710, 0.8125 0.1384, -0.06890, 0.6797 0.1741, -0.07950, 0.5425 0.2102, -0.08660, 0.3955 0.2472, -0.09640, 0.2644 0.2844, -0.10270, 0.1217 0.3225, -0.10690, 0.0180 0.3608, -0.10890, -0.1018 0.3991, -0.10830, -0.1768 0.4373, -0.10510, -0.1999 0.4757, -0.09890, -0.1685 0.5137, -0.09067, -0.0996 0.5611, -0.07859, -0.0484 16 Flap element taps 1.0000, 0.00130, -0.4478 0.9365, 0.01390, -0.4703 0.8333, 0.03280, -0.4629 0.7436, 0.04930, -0.4590 0.7049, 0.05667, -0.4540 0.6662, 0.06411, -0.4524 0.6274, 0.07172, -0.4507 0.6009, 0.07523, -0.4586 0.6069, 0.02889, -0.3420 0.6079, -0.01747, -0.3783 0.6167, -0.06381, -0.1287 0.6558, -0.05300, -0.0159 0.7045, -0.04117, 0.6572 0.7429, -0.03210, 0.5160 0.8333, -0.01400, 0.3213 0.9311, -0.00120, 0.1654 --------- Run Conditions: vel=104.6 ft/s Re=0.987x10^6 AOA=17.97 Flap deflection=10.00 Totals: Cl=0.7631 Cdp=0.3514 Cm(c/4)=-0.1570 Cs=-0.0989 Ch=0.0273 Main component: Cl=0.4640 Cdp=0.2466 Cm=-0.1165 Flap component: Cl=0.2991 Cdp=0.1048 Cm=-0.2490 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1588 0.5905, -0.01667, -0.8015 0.5709, 0.03110, -0.6336 0.5889, 0.07933, -0.7549 0.5500, 0.08689, -0.7330 0.5110, 0.09367, -0.7267 0.4731, 0.09830, -0.7069 0.4349, 0.10070, -0.7162 0.3960, 0.10120, -0.7559 0.3566, 0.10020, -0.7342 0.3172, 0.09790, -0.7409 0.2778, 0.09440, -0.7705 0.2393, 0.08960, -0.7690 0.2056, 0.08360, -0.7980 0.1633, 0.07610, -0.7804 0.1261, 0.06710, -0.7843 0.0900, 0.05640, -0.7741 0.0571, 0.04390, -0.7805 0.0283, 0.02940, -0.8193 0.0142, 0.01970, -0.8357 0.0081, 0.01410, -0.8489 0.0026, 0.00780, -0.8202 0.0000, 0.00000, -1.1347 0.0037, -0.00840, 0.5307 0.0112, -0.01420, 0.9350 0.0191, -0.01930, 1.0051 0.0397, -0.03030, 0.9703 0.0706, -0.04420, 0.8220 0.1037, -0.05710, 0.6767 0.1384, -0.06890, 0.5478 0.1741, -0.07950, 0.4023 0.2102, -0.08660, 0.2384 0.2472, -0.09640, 0.1038 0.2844, -0.10270, -0.0480 0.3225, -0.10690, -0.1492 0.3608, -0.10890, -0.2790 0.3991, -0.10830, -0.3543 0.4373, -0.10510, -0.3801 0.4757, -0.09890, -0.3411 0.5137, -0.09067, -0.2641 0.5611, -0.07859, -0.1893 16 Flap element taps 1.0000, 0.00130, -0.6627 0.9365, 0.01390, -0.6924 0.8333, 0.03280, -0.7092 0.7436, 0.04930, -0.7038 0.7049, 0.05667, -0.6976 0.6662, 0.06411, -0.6996 0.6274, 0.07172, -0.6895 0.6009, 0.07523, -0.6996 0.6069, 0.02889, -0.6536 0.6079, -0.01747, -0.7017 0.6167, -0.06381, -0.3557 0.6558, -0.05300, -0.1483 0.7045, -0.04117, 0.6300 0.7429, -0.03210, 0.4399 0.8333, -0.01400, 0.2251 0.9311, -0.00120, 0.0454 --------- Run Conditions: vel=105.2 ft/s Re=0.994x10^6 AOA=19.95 Flap deflection=10.00 Totals: Cl=0.7674 Cdp=0.3965 Cm(c/4)=-0.1633 Cs=-0.1108 Ch=0.0294 Main component: Cl=0.4658 Cdp=0.2819 Cm=-0.1241 Flap component: Cl=0.3016 Cdp=0.1146 Cm=-0.2534 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1694 0.5905, -0.01667, -0.8825 0.5709, 0.03110, -0.6959 0.5889, 0.07933, -0.7914 0.5500, 0.08689, -0.7855 0.5110, 0.09367, -0.7762 0.4731, 0.09830, -0.7391 0.4349, 0.10070, -0.7366 0.3960, 0.10120, -0.7791 0.3566, 0.10020, -0.7430 0.3172, 0.09790, -0.7437 0.2778, 0.09440, -0.7604 0.2393, 0.08960, -0.7499 0.2056, 0.08360, -0.7816 0.1633, 0.07610, -0.7444 0.1261, 0.06710, -0.7591 0.0900, 0.05640, -0.7436 0.0571, 0.04390, -0.7586 0.0283, 0.02940, -0.7759 0.0142, 0.01970, -0.7864 0.0081, 0.01410, -0.8100 0.0026, 0.00780, -0.7652 0.0000, 0.00000, -1.0467 0.0037, -0.00840, 0.5024 0.0112, -0.01420, 0.9187 0.0191, -0.01930, 1.0005 0.0397, -0.03030, 0.9825 0.0706, -0.04420, 0.8430 0.1037, -0.05710, 0.7041 0.1384, -0.06890, 0.5925 0.1741, -0.07950, 0.4487 0.2102, -0.08660, 0.2733 0.2472, -0.09640, 0.1458 0.2844, -0.10270, -0.0123 0.3225, -0.10690, -0.1059 0.3608, -0.10890, -0.2467 0.3991, -0.10830, -0.3202 0.4373, -0.10510, -0.3571 0.4757, -0.09890, -0.3271 0.5137, -0.09067, -0.2505 0.5611, -0.07859, -0.1928 16 Flap element taps 1.0000, 0.00130, -0.6807 0.9365, 0.01390, -0.7037 0.8333, 0.03280, -0.7303 0.7436, 0.04930, -0.7315 0.7049, 0.05667, -0.7229 0.6662, 0.06411, -0.7315 0.6274, 0.07172, -0.7204 0.6009, 0.07523, -0.7131 0.6069, 0.02889, -0.6995 0.6079, -0.01747, -0.7583 0.6167, -0.06381, -0.3803 0.6558, -0.05300, -0.1414 0.7045, -0.04117, 0.6262 0.7429, -0.03210, 0.4312 0.8333, -0.01400, 0.2181 0.9311, -0.00120, 0.0370 --------- Run Conditions: vel=105.3 ft/s Re=0.995x10^6 AOA=23.98 Flap deflection=10.00 Totals: Cl=0.8696 Cdp=0.5226 Cm(c/4)=-0.1917 Cs=-0.1241 Ch=0.0375 Main component: Cl=0.5418 Cdp=0.3675 Cm=-0.1595 Flap component: Cl=0.3278 Cdp=0.1550 Cm=-0.2839 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1810 0.5905, -0.01667, -0.9828 0.5709, 0.03110, -0.7788 0.5889, 0.07933, -0.8787 0.5500, 0.08689, -0.8731 0.5110, 0.09367, -0.8803 0.4731, 0.09830, -0.8466 0.4349, 0.10070, -0.8440 0.3960, 0.10120, -0.8901 0.3566, 0.10020, -0.8362 0.3172, 0.09790, -0.8320 0.2778, 0.09440, -0.8415 0.2393, 0.08960, -0.8325 0.2056, 0.08360, -0.8741 0.1633, 0.07610, -0.8272 0.1261, 0.06710, -0.8460 0.0900, 0.05640, -0.8247 0.0571, 0.04390, -0.8364 0.0283, 0.02940, -0.8447 0.0142, 0.01970, -0.8504 0.0081, 0.01410, -0.8844 0.0026, 0.00780, -0.8334 0.0000, 0.00000, -0.9305 0.0037, -0.00840, 0.2666 0.0112, -0.01420, 0.8105 0.0191, -0.01930, 0.9585 0.0397, -0.03030, 1.0107 0.0706, -0.04420, 0.9142 0.1037, -0.05710, 0.8024 0.1384, -0.06890, 0.7171 0.1741, -0.07950, 0.5817 0.2102, -0.08660, 0.4027 0.2472, -0.09640, 0.2863 0.2844, -0.10270, 0.1229 0.3225, -0.10690, 0.0347 0.3608, -0.10890, -0.1189 0.3991, -0.10830, -0.1979 0.4373, -0.10510, -0.2579 0.4757, -0.09890, -0.2474 0.5137, -0.09067, -0.1775 0.5611, -0.07859, -0.1150 16 Flap element taps 1.0000, 0.00130, -0.8077 0.9365, 0.01390, -0.8200 0.8333, 0.03280, -0.8459 0.7436, 0.04930, -0.8441 0.7049, 0.05667, -0.8332 0.6662, 0.06411, -0.8421 0.6274, 0.07172, -0.8246 0.6009, 0.07523, -0.8158 0.6069, 0.02889, -0.7804 0.6079, -0.01747, -0.8437 0.6167, -0.06381, -0.4376 0.6558, -0.05300, -0.0472 0.7045, -0.04117, 0.6451 0.7429, -0.03210, 0.4224 0.8333, -0.01400, 0.2098 0.9311, -0.00120, 0.0085 --------- Run Conditions: vel=105.0 ft/s Re=0.992x10^6 AOA=27.01 Flap deflection=10.00 Totals: Cl=1.0262 Cdp=0.6727 Cm(c/4)=-0.2333 Cs=-0.1332 Ch=0.0493 Main component: Cl=0.6536 Cdp=0.4718 Cm=-0.2076 Flap component: Cl=0.3726 Cdp=0.2009 Cm=-0.3306 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1823 0.5905, -0.01667, -1.1755 0.5709, 0.03110, -0.9445 0.5889, 0.07933, -1.0662 0.5500, 0.08689, -1.0547 0.5110, 0.09367, -1.0589 0.4731, 0.09830, -1.0285 0.4349, 0.10070, -1.0255 0.3960, 0.10120, -1.0802 0.3566, 0.10020, -1.0166 0.3172, 0.09790, -1.0131 0.2778, 0.09440, -1.0203 0.2393, 0.08960, -1.0099 0.2056, 0.08360, -1.0593 0.1633, 0.07610, -1.0031 0.1261, 0.06710, -1.0276 0.0900, 0.05640, -1.0011 0.0571, 0.04390, -1.0138 0.0283, 0.02940, -1.0192 0.0142, 0.01970, -1.0226 0.0081, 0.01410, -1.0642 0.0026, 0.00780, -1.0029 0.0000, 0.00000, -1.0347 0.0037, -0.00840, -0.0138 0.0112, -0.01420, 0.6655 0.0191, -0.01930, 0.8850 0.0397, -0.03030, 1.0124 0.0706, -0.04420, 0.9586 0.1037, -0.05710, 0.8733 0.1384, -0.06890, 0.8110 0.1741, -0.07950, 0.6843 0.2102, -0.08660, 0.5068 0.2472, -0.09640, 0.4012 0.2844, -0.10270, 0.2355 0.3225, -0.10690, 0.1532 0.3608, -0.10890, -0.0090 0.3991, -0.10830, -0.0918 0.4373, -0.10510, -0.1698 0.4757, -0.09890, -0.1768 0.5137, -0.09067, -0.1106 0.5611, -0.07859, -0.0508 16 Flap element taps 1.0000, 0.00130, -0.9941 0.9365, 0.01390, -0.9921 0.8333, 0.03280, -1.0131 0.7436, 0.04930, -1.0152 0.7049, 0.05667, -1.0034 0.6662, 0.06411, -1.0177 0.6274, 0.07172, -1.0010 0.6009, 0.07523, -0.9918 0.6069, 0.02889, -0.9432 0.6079, -0.01747, -1.0250 0.6167, -0.06381, -0.5108 0.6558, -0.05300, 0.0835 0.7045, -0.04117, 0.6356 0.7429, -0.03210, 0.4166 0.8333, -0.01400, 0.2028 0.9311, -0.00120, -0.0273