S809 SPOILER FLAP, LEGR, CHORD = 18 INCHES --------- Run Conditions: vel=102.1 ft/s Re=1.002x10^6 AOA=-6.04 Flap deflection=60.00 Totals: Cl=0.0149 Cdp=0.4711 Cm(c/4)=-0.1042 Cs=-0.4700 Ch=0.0626 Main component: Cl=-0.2226 Cdp=-0.0028 Cm=0.0386 Flap component: Cl=0.2375 Cdp=0.4738 Cm=-0.1341 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0623 0.5905, -0.01667, 0.0943 0.5709, 0.03110, 0.1057 0.5889, 0.07933, 0.1045 0.5500, 0.08689, 0.2101 0.5110, 0.09367, 0.0809 0.4731, 0.09830, 0.0048 0.4349, 0.10070, -0.0573 0.3960, 0.10120, -0.0858 0.3566, 0.10020, -0.0963 0.3172, 0.09790, -0.0811 0.2778, 0.09440, -0.0790 0.2393, 0.08960, -0.0635 0.2056, 0.08360, -0.0242 0.1633, 0.07610, 0.0335 0.1261, 0.06710, 0.1364 0.0900, 0.05640, 0.2308 0.0571, 0.04390, 0.4335 0.0283, 0.02940, 0.6701 0.0142, 0.01970, 0.8779 0.0081, 0.01410, 0.9627 0.0026, 0.00780, 0.8735 0.0000, 0.00000, 0.3092 0.0037, -0.00840, -0.4986 0.0112, -0.01420, -0.5008 0.0191, -0.01930, -0.4214 0.0397, -0.03030, -0.2940 0.0706, -0.04420, -0.3766 0.1037, -0.05710, -0.3851 0.1384, -0.06890, -0.4572 0.1741, -0.07950, -0.4870 0.2102, -0.08660, -0.5136 0.2472, -0.09640, -0.5418 0.2844, -0.10270, -0.5194 0.3225, -0.10690, -0.4668 0.3608, -0.10890, -0.3749 0.3991, -0.10830, -0.2100 0.4373, -0.10510, 0.0006 0.4757, -0.09890, 0.0689 0.5137, -0.09067, 0.0965 0.5611, -0.07859, 0.0902 16 Flap element taps 1.0000, 0.00130, -1.1825 0.9365, 0.01390, -1.1520 0.8333, 0.03280, -1.1486 0.7436, 0.04930, -1.1370 0.7049, 0.05667, -1.1322 0.6662, 0.06411, -1.1200 0.6274, 0.07172, -1.0999 0.6009, 0.07523, -1.1392 0.6069, 0.02889, 0.2482 0.6079, -0.01747, 0.4459 0.6167, -0.06381, 0.6686 0.6558, -0.05300, 0.4094 0.7045, -0.04117, 0.2671 0.7429, -0.03210, 0.1922 0.8333, -0.01400, 0.3114 0.9311, -0.00120, 0.2529 --------- Run Conditions: vel=101.6 ft/s Re=0.998x10^6 AOA=0.02 Flap deflection=60.00 Totals: Cl=0.3117 Cdp=0.5138 Cm(c/4)=-0.1045 Cs=-0.5136 Ch=0.0687 Main component: Cl=0.0829 Cdp=-0.0390 Cm=-0.0157 Flap component: Cl=0.2288 Cdp=0.5528 Cm=-0.1667 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.2428 0.5905, -0.01667, 0.2622 0.5709, 0.03110, 0.2739 0.5889, 0.07933, 0.2699 0.5500, 0.08689, 0.2359 0.5110, 0.09367, 0.1219 0.4731, 0.09830, -0.0091 0.4349, 0.10070, -0.1249 0.3960, 0.10120, -0.1992 0.3566, 0.10020, -0.2513 0.3172, 0.09790, -0.2774 0.2778, 0.09440, -0.3120 0.2393, 0.08960, -0.3386 0.2056, 0.08360, -0.3401 0.1633, 0.07610, -0.3293 0.1261, 0.06710, -0.2770 0.0900, 0.05640, -0.2640 0.0571, 0.04390, -0.1291 0.0283, 0.02940, 0.0189 0.0142, 0.01970, 0.2114 0.0081, 0.01410, 0.4090 0.0026, 0.00780, 0.5561 0.0000, 0.00000, 0.9782 0.0037, -0.00840, 0.7775 0.0112, -0.01420, 0.5657 0.0191, -0.01930, 0.4763 0.0397, -0.03030, 0.3524 0.0706, -0.04420, 0.1672 0.1037, -0.05710, 0.0759 0.1384, -0.06890, -0.0493 0.1741, -0.07950, -0.1318 0.2102, -0.08660, -0.2000 0.2472, -0.09640, -0.2690 0.2844, -0.10270, -0.2955 0.3225, -0.10690, -0.2947 0.3608, -0.10890, -0.2671 0.3991, -0.10830, -0.1736 0.4373, -0.10510, 0.0082 0.4757, -0.09890, 0.1823 0.5137, -0.09067, 0.2588 0.5611, -0.07859, 0.2650 16 Flap element taps 1.0000, 0.00130, -1.2543 0.9365, 0.01390, -1.2506 0.8333, 0.03280, -1.2419 0.7436, 0.04930, -1.2173 0.7049, 0.05667, -1.2037 0.6662, 0.06411, -1.1904 0.6274, 0.07172, -1.1580 0.6009, 0.07523, -1.1968 0.6069, 0.02889, 0.1421 0.6079, -0.01747, 0.2930 0.6167, -0.06381, 0.9348 0.6558, -0.05300, 0.4981 0.7045, -0.04117, 0.3683 0.7429, -0.03210, 0.3176 0.8333, -0.01400, 0.4293 0.9311, -0.00120, 0.3418 --------- Run Conditions: vel=102.7 ft/s Re=1.006x10^6 AOA=3.02 Flap deflection=60.00 Totals: Cl=0.2912 Cdp=0.4920 Cm(c/4)=-0.0892 Cs=-0.4760 Ch=0.0499 Main component: Cl=0.0982 Cdp=-0.0404 Cm=-0.0049 Flap component: Cl=0.1930 Cdp=0.5324 Cm=-0.1635 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.2602 0.5905, -0.01667, 0.2680 0.5709, 0.03110, 0.2781 0.5889, 0.07933, 0.2620 0.5500, 0.08689, 0.2641 0.5110, 0.09367, 0.2430 0.4731, 0.09830, 0.1689 0.4349, 0.10070, 0.0232 0.3960, 0.10120, -0.1060 0.3566, 0.10020, -0.1842 0.3172, 0.09790, -0.2418 0.2778, 0.09440, -0.3023 0.2393, 0.08960, -0.3518 0.2056, 0.08360, -0.3839 0.1633, 0.07610, -0.3891 0.1261, 0.06710, -0.3701 0.0900, 0.05640, -0.3871 0.0571, 0.04390, -0.2971 0.0283, 0.02940, -0.2056 0.0142, 0.01970, -0.0661 0.0081, 0.01410, 0.1229 0.0026, 0.00780, 0.2498 0.0000, 0.00000, 0.8491 0.0037, -0.00840, 0.9263 0.0112, -0.01420, 0.7452 0.0191, -0.01930, 0.6435 0.0397, -0.03030, 0.4874 0.0706, -0.04420, 0.2799 0.1037, -0.05710, 0.1685 0.1384, -0.06890, 0.0338 0.1741, -0.07950, -0.0661 0.2102, -0.08660, -0.1571 0.2472, -0.09640, -0.2410 0.2844, -0.10270, -0.2887 0.3225, -0.10690, -0.3046 0.3608, -0.10890, -0.3063 0.3991, -0.10830, -0.2400 0.4373, -0.10510, -0.0905 0.4757, -0.09890, 0.0956 0.5137, -0.09067, 0.2488 0.5611, -0.07859, 0.2707 16 Flap element taps 1.0000, 0.00130, -1.1812 0.9365, 0.01390, -1.1969 0.8333, 0.03280, -1.2088 0.7436, 0.04930, -1.1932 0.7049, 0.05667, -1.1814 0.6662, 0.06411, -1.1764 0.6274, 0.07172, -1.1408 0.6009, 0.07523, -1.1731 0.6069, 0.02889, 0.0886 0.6079, -0.01747, 0.2204 0.6167, -0.06381, 0.6832 0.6558, -0.05300, 0.3096 0.7045, -0.04117, 0.3059 0.7429, -0.03210, 0.2752 0.8333, -0.01400, 0.3474 0.9311, -0.00120, 0.4387 --------- Run Conditions: vel=104.1 ft/s Re=1.020x10^6 AOA=6.04 Flap deflection=60.00 Totals: Cl=0.3737 Cdp=0.4670 Cm(c/4)=-0.1568 Cs=-0.4251 Ch=-0.0092 Main component: Cl=0.0551 Cdp=-0.0212 Cm=0.0295 Flap component: Cl=0.3187 Cdp=0.4882 Cm=-0.2916 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.1553 0.5905, -0.01667, 0.1521 0.5709, 0.03110, 0.1588 0.5889, 0.07933, 0.1469 0.5500, 0.08689, 0.2657 0.5110, 0.09367, 0.2548 0.4731, 0.09830, 0.2635 0.4349, 0.10070, 0.2511 0.3960, 0.10120, 0.1700 0.3566, 0.10020, 0.0467 0.3172, 0.09790, -0.0799 0.2778, 0.09440, -0.1951 0.2393, 0.08960, -0.2904 0.2056, 0.08360, -0.3710 0.1633, 0.07610, -0.4128 0.1261, 0.06710, -0.4406 0.0900, 0.05640, -0.5082 0.0571, 0.04390, -0.4831 0.0283, 0.02940, -0.4844 0.0142, 0.01970, -0.4381 0.0081, 0.01410, -0.2245 0.0026, 0.00780, -0.1192 0.0000, 0.00000, 0.4814 0.0037, -0.00840, 0.9859 0.0112, -0.01420, 0.9019 0.0191, -0.01930, 0.8064 0.0397, -0.03030, 0.6385 0.0706, -0.04420, 0.4167 0.1037, -0.05710, 0.2827 0.1384, -0.06890, 0.1342 0.1741, -0.07950, 0.0130 0.2102, -0.08660, -0.1056 0.2472, -0.09640, -0.2171 0.2844, -0.10270, -0.2957 0.3225, -0.10690, -0.3443 0.3608, -0.10890, -0.3939 0.3991, -0.10830, -0.3857 0.4373, -0.10510, -0.3161 0.4757, -0.09890, -0.2144 0.5137, -0.09067, -0.0297 0.5611, -0.07859, 0.1055 16 Flap element taps 1.0000, 0.00130, -1.0551 0.9365, 0.01390, -1.0545 0.8333, 0.03280, -1.0851 0.7436, 0.04930, -1.0879 0.7049, 0.05667, -1.0846 0.6662, 0.06411, -1.0914 0.6274, 0.07172, -1.0687 0.6009, 0.07523, -1.1173 0.6069, 0.02889, -0.6667 0.6079, -0.01747, -1.5680 0.6167, -0.06381, -0.6079 0.6558, -0.05300, 0.1201 0.7045, -0.04117, 0.3547 0.7429, -0.03210, 0.5764 0.8333, -0.01400, 0.9877 0.9311, -0.00120, 0.7104 --------- Run Conditions: vel=102.8 ft/s Re=1.006x10^6 AOA=9.03 Flap deflection=60.00 Totals: Cl=0.5354 Cdp=0.4639 Cm(c/4)=-0.1778 Cs=-0.3741 Ch=-0.0331 Main component: Cl=0.1900 Cdp=0.0157 Cm=0.0024 Flap component: Cl=0.3454 Cdp=0.4482 Cm=-0.3305 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.0654 0.5905, -0.01667, -0.0898 0.5709, 0.03110, -0.0864 0.5889, 0.07933, -0.0608 0.5500, 0.08689, 0.1572 0.5110, 0.09367, 0.1486 0.4731, 0.09830, 0.1531 0.4349, 0.10070, 0.1485 0.3960, 0.10120, 0.1191 0.3566, 0.10020, 0.0727 0.3172, 0.09790, -0.0556 0.2778, 0.09440, -0.2069 0.2393, 0.08960, -0.3425 0.2056, 0.08360, -0.4643 0.1633, 0.07610, -0.5520 0.1261, 0.06710, -0.6287 0.0900, 0.05640, -0.7641 0.0571, 0.04390, -0.8272 0.0283, 0.02940, -0.9747 0.0142, 0.01970, -1.0943 0.0081, 0.01410, -0.9411 0.0026, 0.00780, -0.9217 0.0000, 0.00000, -0.4807 0.0037, -0.00840, 0.8801 0.0112, -0.01420, 0.9946 0.0191, -0.01930, 0.9554 0.0397, -0.03030, 0.8110 0.0706, -0.04420, 0.6024 0.1037, -0.05710, 0.4605 0.1384, -0.06890, 0.3050 0.1741, -0.07950, 0.1774 0.2102, -0.08660, 0.0460 0.2472, -0.09640, -0.0730 0.2844, -0.10270, -0.1709 0.3225, -0.10690, -0.2393 0.3608, -0.10890, -0.3077 0.3991, -0.10830, -0.3237 0.4373, -0.10510, -0.2769 0.4757, -0.09890, -0.2019 0.5137, -0.09067, -0.0336 0.5611, -0.07859, 0.0650 16 Flap element taps 1.0000, 0.00130, -0.9937 0.9365, 0.01390, -0.9935 0.8333, 0.03280, -1.0244 0.7436, 0.04930, -1.0325 0.7049, 0.05667, -1.0232 0.6662, 0.06411, -1.0307 0.6274, 0.07172, -1.0072 0.6009, 0.07523, -1.1945 0.6069, 0.02889, -1.5332 0.6079, -0.01747, -1.9472 0.6167, -0.06381, -0.9482 0.6558, -0.05300, -0.0580 0.7045, -0.04117, 0.3561 0.7429, -0.03210, 0.6584 0.8333, -0.01400, 0.9878 0.9311, -0.00120, 0.7382 --------- Run Conditions: vel=102.7 ft/s Re=1.004x10^6 AOA=12.03 Flap deflection=60.00 Totals: Cl=0.6149 Cdp=0.4901 Cm(c/4)=-0.1779 Cs=-0.3512 Ch=-0.0412 Main component: Cl=0.2900 Cdp=0.0404 Cm=-0.0218 Flap component: Cl=0.3250 Cdp=0.4497 Cm=-0.3321 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1548 0.5905, -0.01667, -0.1890 0.5709, 0.03110, -0.1798 0.5889, 0.07933, -0.1440 0.5500, 0.08689, 0.0569 0.5110, 0.09367, 0.0413 0.4731, 0.09830, 0.0276 0.4349, 0.10070, 0.0307 0.3960, 0.10120, 0.0096 0.3566, 0.10020, 0.0173 0.3172, 0.09790, -0.0184 0.2778, 0.09440, -0.1170 0.2393, 0.08960, -0.2697 0.2056, 0.08360, -0.4414 0.1633, 0.07610, -0.5721 0.1261, 0.06710, -0.7068 0.0900, 0.05640, -0.8971 0.0571, 0.04390, -1.0556 0.0283, 0.02940, -1.3448 0.0142, 0.01970, -1.6316 0.0081, 0.01410, -1.6027 0.0026, 0.00780, -1.6772 0.0000, 0.00000, -1.5565 0.0037, -0.00840, 0.6177 0.0112, -0.01420, 0.9781 0.0191, -0.01930, 1.0052 0.0397, -0.03030, 0.9186 0.0706, -0.04420, 0.7346 0.1037, -0.05710, 0.5951 0.1384, -0.06890, 0.4500 0.1741, -0.07950, 0.3176 0.2102, -0.08660, 0.1774 0.2472, -0.09640, 0.0577 0.2844, -0.10270, -0.0514 0.3225, -0.10690, -0.1295 0.3608, -0.10890, -0.2128 0.3991, -0.10830, -0.2425 0.4373, -0.10510, -0.2140 0.4757, -0.09890, -0.1645 0.5137, -0.09067, -0.0629 0.5611, -0.07859, 0.0988 16 Flap element taps 1.0000, 0.00130, -0.9518 0.9365, 0.01390, -0.9508 0.8333, 0.03280, -0.9837 0.7436, 0.04930, -0.9859 0.7049, 0.05667, -0.9799 0.6662, 0.06411, -0.9989 0.6274, 0.07172, -0.9927 0.6009, 0.07523, -1.3749 0.6069, 0.02889, -1.7892 0.6079, -0.01747, -1.7059 0.6167, -0.06381, -1.0246 0.6558, -0.05300, -0.1311 0.7045, -0.04117, 0.3552 0.7429, -0.03210, 0.6634 0.8333, -0.01400, 0.9905 0.9311, -0.00120, 0.7621 --------- Run Conditions: vel=101.9 ft/s Re=0.996x10^6 AOA=15.01 Flap deflection=60.00 Totals: Cl=0.5651 Cdp=0.5719 Cm(c/4)=-0.1660 Cs=-0.4060 Ch=-0.0382 Main component: Cl=0.3024 Cdp=0.0819 Cm=-0.0330 Flap component: Cl=0.2627 Cdp=0.4900 Cm=-0.3065 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.2696 0.5905, -0.01667, -0.3286 0.5709, 0.03110, -0.3164 0.5889, 0.07933, -0.2835 0.5500, 0.08689, -0.0744 0.5110, 0.09367, -0.0495 0.4731, 0.09830, -0.0664 0.4349, 0.10070, -0.0786 0.3960, 0.10120, -0.0941 0.3566, 0.10020, -0.0711 0.3172, 0.09790, -0.0803 0.2778, 0.09440, -0.0944 0.2393, 0.08960, -0.1078 0.2056, 0.08360, -0.2091 0.1633, 0.07610, -0.3541 0.1261, 0.06710, -0.5494 0.0900, 0.05640, -0.7907 0.0571, 0.04390, -1.0414 0.0283, 0.02940, -1.4203 0.0142, 0.01970, -1.8143 0.0081, 0.01410, -1.8667 0.0026, 0.00780, -2.0333 0.0000, 0.00000, -2.2086 0.0037, -0.00840, 0.4029 0.0112, -0.01420, 0.9258 0.0191, -0.01930, 1.0049 0.0397, -0.03030, 0.9584 0.0706, -0.04420, 0.8028 0.1037, -0.05710, 0.6628 0.1384, -0.06890, 0.5270 0.1741, -0.07950, 0.3920 0.2102, -0.08660, 0.2447 0.2472, -0.09640, 0.1216 0.2844, -0.10270, 0.0059 0.3225, -0.10690, -0.0744 0.3608, -0.10890, -0.1747 0.3991, -0.10830, -0.2094 0.4373, -0.10510, -0.2006 0.4757, -0.09890, -0.1479 0.5137, -0.09067, -0.0902 0.5611, -0.07859, 0.0849 16 Flap element taps 1.0000, 0.00130, -0.9784 0.9365, 0.01390, -0.9870 0.8333, 0.03280, -1.0057 0.7436, 0.04930, -1.0195 0.7049, 0.05667, -1.0165 0.6662, 0.06411, -1.0395 0.6274, 0.07172, -1.0608 0.6009, 0.07523, -1.4260 0.6069, 0.02889, -1.3481 0.6079, -0.01747, -1.3040 0.6167, -0.06381, -0.9405 0.6558, -0.05300, -0.2019 0.7045, -0.04117, 0.3115 0.7429, -0.03210, 0.6471 0.8333, -0.01400, 0.9918 0.9311, -0.00120, 0.7706 --------- Run Conditions: vel=103.5 ft/s Re=1.009x10^6 AOA=17.99 Flap deflection=60.00 Totals: Cl=0.5104 Cdp=0.6549 Cm(c/4)=-0.1686 Cs=-0.4652 Ch=-0.0536 Main component: Cl=0.2893 Cdp=0.1666 Cm=-0.0471 Flap component: Cl=0.2211 Cdp=0.4883 Cm=-0.2935 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.5449 0.5905, -0.01667, -0.7479 0.5709, 0.03110, -0.6846 0.5889, 0.07933, -0.3940 0.5500, 0.08689, -0.2062 0.5110, 0.09367, -0.1748 0.4731, 0.09830, -0.1554 0.4349, 0.10070, -0.2138 0.3960, 0.10120, -0.2625 0.3566, 0.10020, -0.2170 0.3172, 0.09790, -0.2174 0.2778, 0.09440, -0.2163 0.2393, 0.08960, -0.2119 0.2056, 0.08360, -0.2571 0.1633, 0.07610, -0.2500 0.1261, 0.06710, -0.3237 0.0900, 0.05640, -0.4594 0.0571, 0.04390, -0.7588 0.0283, 0.02940, -1.2006 0.0142, 0.01970, -1.6562 0.0081, 0.01410, -1.7807 0.0026, 0.00780, -2.0132 0.0000, 0.00000, -2.3741 0.0037, -0.00840, 0.3071 0.0112, -0.01420, 0.8893 0.0191, -0.01930, 0.9972 0.0397, -0.03030, 0.9769 0.0706, -0.04420, 0.8351 0.1037, -0.05710, 0.7027 0.1384, -0.06890, 0.5835 0.1741, -0.07950, 0.4449 0.2102, -0.08660, 0.2849 0.2472, -0.09640, 0.1637 0.2844, -0.10270, 0.0368 0.3225, -0.10690, -0.0413 0.3608, -0.10890, -0.1619 0.3991, -0.10830, -0.2059 0.4373, -0.10510, -0.2212 0.4757, -0.09890, -0.1844 0.5137, -0.09067, -0.1245 0.5611, -0.07859, -0.0692 16 Flap element taps 1.0000, 0.00130, -0.9837 0.9365, 0.01390, -0.9887 0.8333, 0.03280, -1.0096 0.7436, 0.04930, -1.0283 0.7049, 0.05667, -1.0223 0.6662, 0.06411, -1.0537 0.6274, 0.07172, -1.0699 0.6009, 0.07523, -1.3130 0.6069, 0.02889, -1.2884 0.6079, -0.01747, -1.2269 0.6167, -0.06381, -1.0148 0.6558, -0.05300, -0.3881 0.7045, -0.04117, 0.1871 0.7429, -0.03210, 0.5647 0.8333, -0.01400, 0.9858 0.9311, -0.00120, 0.7955 --------- Run Conditions: vel=103.0 ft/s Re=1.004x10^6 AOA=19.99 Flap deflection=60.00 Totals: Cl=0.4768 Cdp=0.6756 Cm(c/4)=-0.1611 Cs=-0.4719 Ch=-0.0609 Main component: Cl=0.2927 Cdp=0.2132 Cm=-0.0600 Flap component: Cl=0.1841 Cdp=0.4624 Cm=-0.2709 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.6433 0.5905, -0.01667, -0.8969 0.5709, 0.03110, -0.8370 0.5889, 0.07933, -0.4233 0.5500, 0.08689, -0.2345 0.5110, 0.09367, -0.2457 0.4731, 0.09830, -0.1954 0.4349, 0.10070, -0.2275 0.3960, 0.10120, -0.3334 0.3566, 0.10020, -0.2965 0.3172, 0.09790, -0.3003 0.2778, 0.09440, -0.2954 0.2393, 0.08960, -0.2843 0.2056, 0.08360, -0.3373 0.1633, 0.07610, -0.3008 0.1261, 0.06710, -0.3449 0.0900, 0.05640, -0.3317 0.0571, 0.04390, -0.4897 0.0283, 0.02940, -0.9068 0.0142, 0.01970, -1.4039 0.0081, 0.01410, -1.6100 0.0026, 0.00780, -1.8912 0.0000, 0.00000, -2.3596 0.0037, -0.00840, 0.2607 0.0112, -0.01420, 0.8667 0.0191, -0.01930, 0.9896 0.0397, -0.03030, 0.9894 0.0706, -0.04420, 0.8560 0.1037, -0.05710, 0.7292 0.1384, -0.06890, 0.6342 0.1741, -0.07950, 0.4956 0.2102, -0.08660, 0.3188 0.2472, -0.09640, 0.2096 0.2844, -0.10270, 0.0733 0.3225, -0.10690, 0.0074 0.3608, -0.10890, -0.1258 0.3991, -0.10830, -0.1673 0.4373, -0.10510, -0.1999 0.4757, -0.09890, -0.1749 0.5137, -0.09067, -0.1127 0.5611, -0.07859, -0.0619 16 Flap element taps 1.0000, 0.00130, -0.8985 0.9365, 0.01390, -0.8979 0.8333, 0.03280, -0.9206 0.7436, 0.04930, -0.9260 0.7049, 0.05667, -0.9192 0.6662, 0.06411, -0.9541 0.6274, 0.07172, -0.9630 0.6009, 0.07523, -1.1031 0.6069, 0.02889, -1.1313 0.6079, -0.01747, -1.0844 0.6167, -0.06381, -0.9403 0.6558, -0.05300, -0.4272 0.7045, -0.04117, 0.1555 0.7429, -0.03210, 0.5355 0.8333, -0.01400, 0.9831 0.9311, -0.00120, 0.8185 --------- Run Conditions: vel=103.3 ft/s Re=1.006x10^6 AOA=23.99 Flap deflection=60.00 Totals: Cl=0.5129 Cdp=0.8245 Cm(c/4)=-0.1799 Cs=-0.5448 Ch=-0.0748 Main component: Cl=0.3594 Cdp=0.3359 Cm=-0.1017 Flap component: Cl=0.1535 Cdp=0.4886 Cm=-0.2792 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.8666 0.5905, -0.01667, -1.2636 0.5709, 0.03110, -1.2002 0.5889, 0.07933, -0.5285 0.5500, 0.08689, -0.4408 0.5110, 0.09367, -0.4424 0.4731, 0.09830, -0.4096 0.4349, 0.10070, -0.4184 0.3960, 0.10120, -0.5087 0.3566, 0.10020, -0.4695 0.3172, 0.09790, -0.5062 0.2778, 0.09440, -0.5168 0.2393, 0.08960, -0.5099 0.2056, 0.08360, -0.5778 0.1633, 0.07610, -0.5128 0.1261, 0.06710, -0.5608 0.0900, 0.05640, -0.5357 0.0571, 0.04390, -0.5619 0.0283, 0.02940, -0.6032 0.0142, 0.01970, -0.7282 0.0081, 0.01410, -0.9801 0.0026, 0.00780, -1.3084 0.0000, 0.00000, -2.0958 0.0037, -0.00840, 0.1812 0.0112, -0.01420, 0.8127 0.0191, -0.01930, 0.9685 0.0397, -0.03030, 1.0096 0.0706, -0.04420, 0.9067 0.1037, -0.05710, 0.7962 0.1384, -0.06890, 0.7278 0.1741, -0.07950, 0.5938 0.2102, -0.08660, 0.4046 0.2472, -0.09640, 0.3020 0.2844, -0.10270, 0.1541 0.3225, -0.10690, 0.0924 0.3608, -0.10890, -0.0609 0.3991, -0.10830, -0.1119 0.4373, -0.10510, -0.1719 0.4757, -0.09890, -0.1702 0.5137, -0.09067, -0.1139 0.5611, -0.07859, -0.1016 16 Flap element taps 1.0000, 0.00130, -0.9932 0.9365, 0.01390, -0.9934 0.8333, 0.03280, -1.0216 0.7436, 0.04930, -1.0251 0.7049, 0.05667, -1.0127 0.6662, 0.06411, -1.0565 0.6274, 0.07172, -1.0641 0.6009, 0.07523, -1.1766 0.6069, 0.02889, -1.2118 0.6079, -0.01747, -1.1790 0.6167, -0.06381, -1.0756 0.6558, -0.05300, -0.6119 0.7045, -0.04117, 0.0370 0.7429, -0.03210, 0.4508 0.8333, -0.01400, 0.9802 0.9311, -0.00120, 0.8439 --------- Run Conditions: vel=103.0 ft/s Re=1.004x10^6 AOA=27.02 Flap deflection=60.00 Totals: Cl=0.5379 Cdp=0.9448 Cm(c/4)=-0.1975 Cs=-0.5973 Ch=-0.0824 Main component: Cl=0.4067 Cdp=0.4239 Cm=-0.1328 Flap component: Cl=0.1312 Cdp=0.5209 Cm=-0.2919 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.9943 0.5905, -0.01667, -1.4685 0.5709, 0.03110, -1.4445 0.5889, 0.07933, -0.6902 0.5500, 0.08689, -0.6195 0.5110, 0.09367, -0.6191 0.4731, 0.09830, -0.6019 0.4349, 0.10070, -0.6004 0.3960, 0.10120, -0.6689 0.3566, 0.10020, -0.5814 0.3172, 0.09790, -0.6090 0.2778, 0.09440, -0.6212 0.2393, 0.08960, -0.6190 0.2056, 0.08360, -0.6975 0.1633, 0.07610, -0.6108 0.1261, 0.06710, -0.6564 0.0900, 0.05640, -0.6148 0.0571, 0.04390, -0.6436 0.0283, 0.02940, -0.6694 0.0142, 0.01970, -0.6698 0.0081, 0.01410, -0.8095 0.0026, 0.00780, -1.0499 0.0000, 0.00000, -2.0700 0.0037, -0.00840, 0.0693 0.0112, -0.01420, 0.7472 0.0191, -0.01930, 0.9348 0.0397, -0.03030, 1.0144 0.0706, -0.04420, 0.9342 0.1037, -0.05710, 0.8357 0.1384, -0.06890, 0.7927 0.1741, -0.07950, 0.6606 0.2102, -0.08660, 0.4626 0.2472, -0.09640, 0.3684 0.2844, -0.10270, 0.2127 0.3225, -0.10690, 0.1592 0.3608, -0.10890, -0.0097 0.3991, -0.10830, -0.0633 0.4373, -0.10510, -0.1462 0.4757, -0.09890, -0.1579 0.5137, -0.09067, -0.1072 0.5611, -0.07859, -0.1235 16 Flap element taps 1.0000, 0.00130, -1.0962 0.9365, 0.01390, -1.1004 0.8333, 0.03280, -1.1391 0.7436, 0.04930, -1.1431 0.7049, 0.05667, -1.1328 0.6662, 0.06411, -1.1808 0.6274, 0.07172, -1.1836 0.6009, 0.07523, -1.2760 0.6069, 0.02889, -1.3213 0.6079, -0.01747, -1.2809 0.6167, -0.06381, -1.1980 0.6558, -0.05300, -0.7431 0.7045, -0.04117, -0.0452 0.7429, -0.03210, 0.3910 0.8333, -0.01400, 0.9718 0.9311, -0.00120, 0.8544