S809 SPOILER FLAP, CLEAN, CHORD = 18 INCHES --------- Run Conditions: vel=104.9 ft/s Re=0.995x10^6 AOA=-6.04 Flap deflection=-5.00 Totals: Cl=-0.6955 Cdp=0.0213 Cm(c/4)=0.0445 Cs=0.0520 Ch=-0.0473 Main component: Cl=-0.5687 Cdp=0.0339 Cm=0.1260 Flap component: Cl=-0.1268 Cdp=-0.0126 Cm=0.0920 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.2556 0.5905, -0.01667, -0.2138 0.5709, 0.03110, -0.1419 0.5889, 0.07933, -0.1472 0.5500, 0.08689, -0.3036 0.5110, 0.09367, -0.3508 0.4731, 0.09830, -0.3606 0.4349, 0.10070, -0.3562 0.3960, 0.10120, -0.3272 0.3566, 0.10020, -0.2622 0.3172, 0.09790, -0.1948 0.2778, 0.09440, -0.1537 0.2393, 0.08960, -0.0947 0.2056, 0.08360, -0.0259 0.1633, 0.07610, 0.0866 0.1261, 0.06710, 0.2099 0.0900, 0.05640, 0.3685 0.0571, 0.04390, 0.5815 0.0283, 0.02940, 0.8453 0.0142, 0.01970, 0.9886 0.0081, 0.01410, 0.9759 0.0026, 0.00780, 0.7009 0.0000, 0.00000, -0.7415 0.0037, -0.00840, -1.7774 0.0112, -0.01420, -1.4561 0.0191, -0.01930, -1.2468 0.0397, -0.03030, -1.0095 0.0706, -0.04420, -0.9348 0.1037, -0.05710, -0.9703 0.1384, -0.06890, -1.0084 0.1741, -0.07950, -1.0557 0.2102, -0.08660, -1.1335 0.2472, -0.09640, -1.2126 0.2844, -0.10270, -1.2510 0.3225, -0.10690, -1.2499 0.3608, -0.10890, -1.2582 0.3991, -0.10830, -1.1908 0.4373, -0.10510, -1.0509 0.4757, -0.09890, -0.8421 0.5137, -0.09067, -0.5224 0.5611, -0.07859, -0.3244 16 Flap element taps 1.0000, 0.00130, 0.0688 0.9365, 0.01390, 0.0928 0.8333, 0.03280, 0.0966 0.7436, 0.04930, 0.1339 0.7049, 0.05667, 0.1833 0.6662, 0.06411, 0.0884 0.6274, 0.07172, -0.1514 0.6009, 0.07523, -0.1574 0.6069, 0.02889, -0.1781 0.6079, -0.01747, -0.2832 0.6167, -0.06381, -1.0985 0.6558, -0.05300, -0.4300 0.7045, -0.04117, -0.2907 0.7429, -0.03210, -0.2545 0.8333, -0.01400, -0.1774 0.9311, -0.00120, 0.0042 --------- Run Conditions: vel=105.2 ft/s Re=0.997x10^6 AOA=0.01 Flap deflection=-5.00 Totals: Cl=-0.2309 Cdp=-0.0263 Cm(c/4)=0.0231 Cs=0.0263 Ch=-0.0462 Main component: Cl=-0.1939 Cdp=0.0033 Cm=0.0589 Flap component: Cl=-0.0370 Cdp=-0.0296 Cm=0.0219 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.2776 0.5905, -0.01667, -0.0030 0.5709, 0.03110, 0.1795 0.5889, 0.07933, -0.0274 0.5500, 0.08689, -0.4138 0.5110, 0.09367, -0.4208 0.4731, 0.09830, -0.4698 0.4349, 0.10070, -0.5162 0.3960, 0.10120, -0.5367 0.3566, 0.10020, -0.4934 0.3172, 0.09790, -0.4609 0.2778, 0.09440, -0.4560 0.2393, 0.08960, -0.4352 0.2056, 0.08360, -0.4151 0.1633, 0.07610, -0.3299 0.1261, 0.06710, -0.2570 0.0900, 0.05640, -0.1459 0.0571, 0.04390, 0.0122 0.0283, 0.02940, 0.2603 0.0142, 0.01970, 0.5157 0.0081, 0.01410, 0.6671 0.0026, 0.00780, 0.9186 0.0000, 0.00000, 0.9499 0.0037, -0.00840, 0.3452 0.0112, -0.01420, 0.1299 0.0191, -0.01930, 0.0518 0.0397, -0.03030, -0.0686 0.0706, -0.04420, -0.2250 0.1037, -0.05710, -0.3666 0.1384, -0.06890, -0.4725 0.1741, -0.07950, -0.5892 0.2102, -0.08660, -0.7279 0.2472, -0.09640, -0.8471 0.2844, -0.10270, -0.9427 0.3225, -0.10690, -0.9902 0.3608, -0.10890, -1.0612 0.3991, -0.10830, -1.0503 0.4373, -0.10510, -0.9610 0.4757, -0.09890, -0.9126 0.5137, -0.09067, -0.5855 0.5611, -0.07859, -0.2741 16 Flap element taps 1.0000, 0.00130, 0.1478 0.9365, 0.01390, 0.1083 0.8333, 0.03280, 0.0472 0.7436, 0.04930, -0.0005 0.7049, 0.05667, -0.0124 0.6662, 0.06411, -0.0497 0.6274, 0.07172, -0.1624 0.6009, 0.07523, -0.2985 0.6069, 0.02889, 0.1100 0.6079, -0.01747, -0.2206 0.6167, -0.06381, -1.2779 0.6558, -0.05300, -0.4863 0.7045, -0.04117, -0.1055 0.7429, -0.03210, -0.0270 0.8333, -0.01400, 0.1063 0.9311, -0.00120, 0.2053 --------- Run Conditions: vel=105.3 ft/s Re=0.997x10^6 AOA=3.04 Flap deflection=-5.00 Totals: Cl=0.0812 Cdp=-0.0296 Cm(c/4)=0.0170 Cs=0.0338 Ch=-0.0302 Main component: Cl=0.0823 Cdp=0.0086 Cm=-0.0002 Flap component: Cl=-0.0011 Cdp=-0.0382 Cm=-0.0027 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3332 0.5905, -0.01667, -0.0260 0.5709, 0.03110, 0.1772 0.5889, 0.07933, -0.0501 0.5500, 0.08689, -0.4820 0.5110, 0.09367, -0.5548 0.4731, 0.09830, -0.5872 0.4349, 0.10070, -0.6435 0.3960, 0.10120, -0.6934 0.3566, 0.10020, -0.6618 0.3172, 0.09790, -0.6473 0.2778, 0.09440, -0.6652 0.2393, 0.08960, -0.6675 0.2056, 0.08360, -0.6826 0.1633, 0.07610, -0.6200 0.1261, 0.06710, -0.5880 0.0900, 0.05640, -0.5264 0.0571, 0.04390, -0.4426 0.0283, 0.02940, -0.2939 0.0142, 0.01970, -0.1014 0.0081, 0.01410, 0.0314 0.0026, 0.00780, 0.3352 0.0000, 0.00000, 0.8767 0.0037, -0.00840, 0.9141 0.0112, -0.01420, 0.7020 0.0191, -0.01930, 0.5735 0.0397, -0.03030, 0.3620 0.0706, -0.04420, 0.1447 0.1037, -0.05710, -0.0281 0.1384, -0.06890, -0.1522 0.1741, -0.07950, -0.2896 0.2102, -0.08660, -0.4509 0.2472, -0.09640, -0.5794 0.2844, -0.10270, -0.6948 0.3225, -0.10690, -0.7544 0.3608, -0.10890, -0.8501 0.3991, -0.10830, -0.8591 0.4373, -0.10510, -0.7976 0.4757, -0.09890, -0.7304 0.5137, -0.09067, -0.6883 0.5611, -0.07859, -0.1963 16 Flap element taps 1.0000, 0.00130, 0.1368 0.9365, 0.01390, 0.0931 0.8333, 0.03280, 0.0154 0.7436, 0.04930, -0.0433 0.7049, 0.05667, -0.0613 0.6662, 0.06411, -0.1160 0.6274, 0.07172, -0.2841 0.6009, 0.07523, -0.4384 0.6069, 0.02889, 0.0981 0.6079, -0.01747, -0.3010 0.6167, -0.06381, -1.1610 0.6558, -0.05300, -0.3822 0.7045, -0.04117, -0.0340 0.7429, -0.03210, 0.0180 0.8333, -0.01400, 0.1372 0.9311, -0.00120, 0.2252 --------- Run Conditions: vel=105.5 ft/s Re=1.000x10^6 AOA=6.05 Flap deflection=-5.00 Totals: Cl=0.3999 Cdp=-0.0321 Cm(c/4)=0.0101 Cs=0.0741 Ch=-0.0143 Main component: Cl=0.3648 Cdp=0.0092 Cm=-0.0613 Flap component: Cl=0.0351 Cdp=-0.0413 Cm=-0.0272 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3553 0.5905, -0.01667, -0.0489 0.5709, 0.03110, 0.1592 0.5889, 0.07933, -0.0754 0.5500, 0.08689, -0.2677 0.5110, 0.09367, -0.6750 0.4731, 0.09830, -0.7428 0.4349, 0.10070, -0.7941 0.3960, 0.10120, -0.8616 0.3566, 0.10020, -0.8381 0.3172, 0.09790, -0.8460 0.2778, 0.09440, -0.8865 0.2393, 0.08960, -0.9167 0.2056, 0.08360, -0.9668 0.1633, 0.07610, -0.9346 0.1261, 0.06710, -0.9543 0.0900, 0.05640, -0.9574 0.0571, 0.04390, -0.9783 0.0283, 0.02940, -0.9931 0.0142, 0.01970, -0.9642 0.0081, 0.01410, -0.9585 0.0026, 0.00780, -0.7027 0.0000, 0.00000, -0.0748 0.0037, -0.00840, 0.9752 0.0112, -0.01420, 0.9792 0.0191, -0.01930, 0.8909 0.0397, -0.03030, 0.6846 0.0706, -0.04420, 0.4509 0.1037, -0.05710, 0.2653 0.1384, -0.06890, 0.1348 0.1741, -0.07950, -0.0151 0.2102, -0.08660, -0.1908 0.2472, -0.09640, -0.3259 0.2844, -0.10270, -0.4558 0.3225, -0.10690, -0.5236 0.3608, -0.10890, -0.6375 0.3991, -0.10830, -0.6651 0.4373, -0.10510, -0.6349 0.4757, -0.09890, -0.5624 0.5137, -0.09067, -0.5067 0.5611, -0.07859, -0.0954 16 Flap element taps 1.0000, 0.00130, 0.1245 0.9365, 0.01390, 0.0767 0.8333, 0.03280, -0.0141 0.7436, 0.04930, -0.0872 0.7049, 0.05667, -0.1144 0.6662, 0.06411, -0.1892 0.6274, 0.07172, -0.4073 0.6009, 0.07523, -0.5969 0.6069, 0.02889, 0.0771 0.6079, -0.01747, -0.3567 0.6167, -0.06381, -1.0002 0.6558, -0.05300, -0.3080 0.7045, -0.04117, 0.0276 0.7429, -0.03210, 0.0651 0.8333, -0.01400, 0.1673 0.9311, -0.00120, 0.2413 --------- Run Conditions: vel=105.3 ft/s Re=0.999x10^6 AOA=9.05 Flap deflection=-5.00 Totals: Cl=0.6194 Cdp=-0.0189 Cm(c/4)=0.0071 Cs=0.1161 Ch=-0.0105 Main component: Cl=0.5544 Cdp=0.0063 Cm=-0.0948 Flap component: Cl=0.0650 Cdp=-0.0252 Cm=-0.0502 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3146 0.5905, -0.01667, -0.0244 0.5709, 0.03110, 0.1757 0.5889, 0.07933, -0.1233 0.5500, 0.08689, -0.2588 0.5110, 0.09367, -0.5055 0.4731, 0.09830, -0.6744 0.4349, 0.10070, -0.7929 0.3960, 0.10120, -0.8950 0.3566, 0.10020, -0.8940 0.3172, 0.09790, -0.9217 0.2778, 0.09440, -0.9868 0.2393, 0.08960, -1.0566 0.2056, 0.08360, -1.1474 0.1633, 0.07610, -1.1637 0.1261, 0.06710, -1.2492 0.0900, 0.05640, -1.3248 0.0571, 0.04390, -1.4600 0.0283, 0.02940, -1.6636 0.0142, 0.01970, -1.8357 0.0081, 0.01410, -2.0642 0.0026, 0.00780, -1.9398 0.0000, 0.00000, -1.5809 0.0037, -0.00840, 0.6916 0.0112, -0.01420, 1.0049 0.0191, -0.01930, 1.0081 0.0397, -0.03030, 0.8738 0.0706, -0.04420, 0.6560 0.1037, -0.05710, 0.4766 0.1384, -0.06890, 0.3457 0.1741, -0.07950, 0.1913 0.2102, -0.08660, 0.0050 0.2472, -0.09640, -0.1321 0.2844, -0.10270, -0.2740 0.3225, -0.10690, -0.3490 0.3608, -0.10890, -0.4793 0.3991, -0.10830, -0.5243 0.4373, -0.10510, -0.5179 0.4757, -0.09890, -0.4515 0.5137, -0.09067, -0.3824 0.5611, -0.07859, -0.0300 16 Flap element taps 1.0000, 0.00130, 0.0043 0.9365, 0.01390, -0.0362 0.8333, 0.03280, -0.1009 0.7436, 0.04930, -0.1574 0.7049, 0.05667, -0.2010 0.6662, 0.06411, -0.3023 0.6274, 0.07172, -0.4654 0.6009, 0.07523, -0.5372 0.6069, 0.02889, 0.0924 0.6079, -0.01747, -0.3331 0.6167, -0.06381, -0.9068 0.6558, -0.05300, -0.3541 0.7045, -0.04117, 0.0491 0.7429, -0.03210, 0.0751 0.8333, -0.01400, 0.1572 0.9311, -0.00120, 0.2020 Wake drag found for this condition, Cdw=0.0302 --------- Run Conditions: vel=105.0 ft/s Re=0.996x10^6 AOA=12.07 Flap deflection=-5.00 Totals: Cl=0.7456 Cdp=0.0027 Cm(c/4)=0.0105 Cs=0.1533 Ch=-0.0221 Main component: Cl=0.6684 Cdp=0.0023 Cm=-0.1077 Flap component: Cl=0.0772 Cdp=0.0004 Cm=-0.0641 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.2421 0.5905, -0.01667, 0.0464 0.5709, 0.03110, 0.2229 0.5889, 0.07933, -0.1908 0.5500, 0.08689, -0.2249 0.5110, 0.09367, -0.3265 0.4731, 0.09830, -0.5041 0.4349, 0.10070, -0.6694 0.3960, 0.10120, -0.8245 0.3566, 0.10020, -0.8652 0.3172, 0.09790, -0.9328 0.2778, 0.09440, -1.0305 0.2393, 0.08960, -1.1359 0.2056, 0.08360, -1.2644 0.1633, 0.07610, -1.3053 0.1261, 0.06710, -1.4287 0.0900, 0.05640, -1.5785 0.0571, 0.04390, -1.7972 0.0283, 0.02940, -2.2142 0.0142, 0.01970, -2.6831 0.0081, 0.01410, -3.1095 0.0026, 0.00780, -3.2176 0.0000, 0.00000, -3.2504 0.0037, -0.00840, 0.2098 0.0112, -0.01420, 0.8925 0.0191, -0.01930, 1.0064 0.0397, -0.03030, 0.9636 0.0706, -0.04420, 0.7852 0.1037, -0.05710, 0.6196 0.1384, -0.06890, 0.4951 0.1741, -0.07950, 0.3424 0.2102, -0.08660, 0.1494 0.2472, -0.09640, 0.0120 0.2844, -0.10270, -0.1386 0.3225, -0.10690, -0.2210 0.3608, -0.10890, -0.3636 0.3991, -0.10830, -0.4214 0.4373, -0.10510, -0.4350 0.4757, -0.09890, -0.3828 0.5137, -0.09067, -0.3037 0.5611, -0.07859, -0.0196 16 Flap element taps 1.0000, 0.00130, -0.1455 0.9365, 0.01390, -0.1896 0.8333, 0.03280, -0.2127 0.7436, 0.04930, -0.2489 0.7049, 0.05667, -0.2771 0.6662, 0.06411, -0.3349 0.6274, 0.07172, -0.3476 0.6009, 0.07523, -0.3856 0.6069, 0.02889, 0.1474 0.6079, -0.01747, -0.2430 0.6167, -0.06381, -0.8481 0.6558, -0.05300, -0.4662 0.7045, -0.04117, 0.0291 0.7429, -0.03210, 0.0551 0.8333, -0.01400, 0.1174 0.9311, -0.00120, 0.1361 Wake drag found for this condition, Cdw=0.0441 --------- Run Conditions: vel=105.3 ft/s Re=0.998x10^6 AOA=15.01 Flap deflection=-5.00 Totals: Cl=0.8350 Cdp=0.0196 Cm(c/4)=0.0163 Cs=0.1974 Ch=-0.0295 Main component: Cl=0.7521 Cdp=0.0021 Cm=-0.1142 Flap component: Cl=0.0829 Cdp=0.0174 Cm=-0.0724 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1867 0.5905, -0.01667, 0.0833 0.5709, 0.03110, 0.2408 0.5889, 0.07933, -0.2596 0.5500, 0.08689, -0.2812 0.5110, 0.09367, -0.2989 0.4731, 0.09830, -0.3414 0.4349, 0.10070, -0.4672 0.3960, 0.10120, -0.6180 0.3566, 0.10020, -0.7667 0.3172, 0.09790, -0.8763 0.2778, 0.09440, -1.0200 0.2393, 0.08960, -1.1458 0.2056, 0.08360, -1.2866 0.1633, 0.07610, -1.4283 0.1261, 0.06710, -1.5766 0.0900, 0.05640, -1.8045 0.0571, 0.04390, -2.1527 0.0283, 0.02940, -2.7150 0.0142, 0.01970, -3.3175 0.0081, 0.01410, -4.3301 0.0026, 0.00780, -4.6198 0.0000, 0.00000, -5.1249 0.0037, -0.00840, -0.4292 0.0112, -0.01420, 0.6754 0.0191, -0.01930, 0.9257 0.0397, -0.03030, 0.9956 0.0706, -0.04420, 0.8807 0.1037, -0.05710, 0.7442 0.1384, -0.06890, 0.5845 0.1741, -0.07950, 0.4421 0.2102, -0.08660, 0.2903 0.2472, -0.09640, 0.1383 0.2844, -0.10270, -0.0123 0.3225, -0.10690, -0.1300 0.3608, -0.10890, -0.2507 0.3991, -0.10830, -0.3392 0.4373, -0.10510, -0.3565 0.4757, -0.09890, -0.3199 0.5137, -0.09067, -0.2408 0.5611, -0.07859, -0.0559 16 Flap element taps 1.0000, 0.00130, -0.2526 0.9365, 0.01390, -0.2982 0.8333, 0.03280, -0.2961 0.7436, 0.04930, -0.3030 0.7049, 0.05667, -0.3091 0.6662, 0.06411, -0.3130 0.6274, 0.07172, -0.3073 0.6009, 0.07523, -0.3625 0.6069, 0.02889, 0.1754 0.6079, -0.01747, -0.1978 0.6167, -0.06381, -0.7796 0.6558, -0.05300, -0.5513 0.7045, -0.04117, 0.0049 0.7429, -0.03210, 0.0497 0.8333, -0.01400, 0.0908 0.9311, -0.00120, 0.0713 Wake drag found for this condition, Cdw=0.0655 --------- Run Conditions: vel=105.2 ft/s Re=0.995x10^6 AOA=17.99 Flap deflection=-5.00 Totals: Cl=0.9023 Cdp=0.0628 Cm(c/4)=0.0027 Cs=0.2190 Ch=-0.0272 Main component: Cl=0.7947 Cdp=0.0281 Cm=-0.1219 Flap component: Cl=0.1077 Cdp=0.0347 Cm=-0.0948 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.1927 0.5905, -0.01667, 0.0718 0.5709, 0.03110, 0.2027 0.5889, 0.07933, -0.4230 0.5500, 0.08689, -0.4415 0.5110, 0.09367, -0.4516 0.4731, 0.09830, -0.4435 0.4349, 0.10070, -0.4578 0.3960, 0.10120, -0.4932 0.3566, 0.10020, -0.5699 0.3172, 0.09790, -0.6723 0.2778, 0.09440, -0.8384 0.2393, 0.08960, -1.0016 0.2056, 0.08360, -1.1965 0.1633, 0.07610, -1.3883 0.1261, 0.06710, -1.5939 0.0900, 0.05640, -1.8863 0.0571, 0.04390, -2.3311 0.0283, 0.02940, -3.0600 0.0142, 0.01970, -3.7722 0.0081, 0.01410, -5.3301 0.0026, 0.00780, -5.7169 0.0000, 0.00000, -6.7145 0.0037, -0.00840, -1.0363 0.0112, -0.01420, 0.4395 0.0191, -0.01930, 0.8210 0.0397, -0.03030, 0.9990 0.0706, -0.04420, 0.9354 0.1037, -0.05710, 0.8215 0.1384, -0.06890, 0.6739 0.1741, -0.07950, 0.5372 0.2102, -0.08660, 0.3847 0.2472, -0.09640, 0.2329 0.2844, -0.10270, 0.0803 0.3225, -0.10690, -0.0436 0.3608, -0.10890, -0.1724 0.3991, -0.10830, -0.2699 0.4373, -0.10510, -0.3020 0.4757, -0.09890, -0.2812 0.5137, -0.09067, -0.2008 0.5611, -0.07859, -0.0833 16 Flap element taps 1.0000, 0.00130, -0.3836 0.9365, 0.01390, -0.4246 0.8333, 0.03280, -0.4169 0.7436, 0.04930, -0.4059 0.7049, 0.05667, -0.4006 0.6662, 0.06411, -0.4043 0.6274, 0.07172, -0.4085 0.6009, 0.07523, -0.4676 0.6069, 0.02889, 0.1433 0.6079, -0.01747, -0.2206 0.6167, -0.06381, -0.7131 0.6558, -0.05300, -0.6195 0.7045, -0.04117, -0.0332 0.7429, -0.03210, 0.0380 0.8333, -0.01400, 0.0581 0.9311, -0.00120, 0.0140 Wake drag found for this condition, Cdw=0.0641 --------- Run Conditions: vel=104.6 ft/s Re=0.993x10^6 AOA=20.02 Flap deflection=-5.00 Totals: Cl=0.5137 Cdp=0.2220 Cm(c/4)=-0.0493 Cs=-0.0327 Ch=-0.0325 Main component: Cl=0.4012 Cdp=0.1829 Cm=-0.0885 Flap component: Cl=0.1125 Cdp=0.0391 Cm=-0.1005 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3856 0.5905, -0.01667, -0.0718 0.5709, 0.03110, 0.0966 0.5889, 0.07933, -0.7311 0.5500, 0.08689, -0.7714 0.5110, 0.09367, -0.7505 0.4731, 0.09830, -0.6692 0.4349, 0.10070, -0.6750 0.3960, 0.10120, -0.7114 0.3566, 0.10020, -0.7315 0.3172, 0.09790, -0.7276 0.2778, 0.09440, -0.7408 0.2393, 0.08960, -0.7252 0.2056, 0.08360, -0.7364 0.1633, 0.07610, -0.7332 0.1261, 0.06710, -0.7291 0.0900, 0.05640, -0.7191 0.0571, 0.04390, -0.7304 0.0283, 0.02940, -0.7487 0.0142, 0.01970, -0.7595 0.0081, 0.01410, -0.7674 0.0026, 0.00780, -0.7513 0.0000, 0.00000, -1.0421 0.0037, -0.00840, 0.5644 0.0112, -0.01420, 0.9443 0.0191, -0.01930, 1.0006 0.0397, -0.03030, 0.9523 0.0706, -0.04420, 0.8037 0.1037, -0.05710, 0.6590 0.1384, -0.06890, 0.5016 0.1741, -0.07950, 0.3559 0.2102, -0.08660, 0.1949 0.2472, -0.09640, 0.0337 0.2844, -0.10270, -0.1263 0.3225, -0.10690, -0.2547 0.3608, -0.10890, -0.3906 0.3991, -0.10830, -0.4892 0.4373, -0.10510, -0.5174 0.4757, -0.09890, -0.4834 0.5137, -0.09067, -0.3956 0.5611, -0.07859, -0.1910 16 Flap element taps 1.0000, 0.00130, -0.5623 0.9365, 0.01390, -0.5979 0.8333, 0.03280, -0.6040 0.7436, 0.04930, -0.5934 0.7049, 0.05667, -0.5805 0.6662, 0.06411, -0.5745 0.6274, 0.07172, -0.5658 0.6009, 0.07523, -0.6290 0.6069, 0.02889, 0.0187 0.6079, -0.01747, -0.4090 0.6167, -0.06381, -1.0118 0.6558, -0.05300, -0.8376 0.7045, -0.04117, -0.1626 0.7429, -0.03210, -0.1099 0.8333, -0.01400, -0.0812 0.9311, -0.00120, -0.1294 --------- Run Conditions: vel=105.6 ft/s Re=1.001x10^6 AOA=24.03 Flap deflection=-5.00 Totals: Cl=0.5658 Cdp=0.3006 Cm(c/4)=-0.0657 Cs=-0.0441 Ch=-0.0268 Main component: Cl=0.4373 Cdp=0.2420 Cm=-0.1083 Flap component: Cl=0.1285 Cdp=0.0585 Cm=-0.1172 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3686 0.5905, -0.01667, -0.0658 0.5709, 0.03110, 0.0793 0.5889, 0.07933, -0.7813 0.5500, 0.08689, -0.8149 0.5110, 0.09367, -0.8376 0.4731, 0.09830, -0.7770 0.4349, 0.10070, -0.7301 0.3960, 0.10120, -0.7275 0.3566, 0.10020, -0.7293 0.3172, 0.09790, -0.7322 0.2778, 0.09440, -0.7441 0.2393, 0.08960, -0.7295 0.2056, 0.08360, -0.7440 0.1633, 0.07610, -0.7303 0.1261, 0.06710, -0.7312 0.0900, 0.05640, -0.7125 0.0571, 0.04390, -0.7214 0.0283, 0.02940, -0.7267 0.0142, 0.01970, -0.7389 0.0081, 0.01410, -0.7481 0.0026, 0.00780, -0.7248 0.0000, 0.00000, -0.9794 0.0037, -0.00840, 0.4116 0.0112, -0.01420, 0.8784 0.0191, -0.01930, 0.9826 0.0397, -0.03030, 0.9882 0.0706, -0.04420, 0.8726 0.1037, -0.05710, 0.7488 0.1384, -0.06890, 0.6102 0.1741, -0.07950, 0.4710 0.2102, -0.08660, 0.3088 0.2472, -0.09640, 0.1555 0.2844, -0.10270, -0.0088 0.3225, -0.10690, -0.1354 0.3608, -0.10890, -0.2808 0.3991, -0.10830, -0.3880 0.4373, -0.10510, -0.4327 0.4757, -0.09890, -0.4170 0.5137, -0.09067, -0.3297 0.5611, -0.07859, -0.1965 16 Flap element taps 1.0000, 0.00130, -0.6404 0.9365, 0.01390, -0.6595 0.8333, 0.03280, -0.6701 0.7436, 0.04930, -0.6582 0.7049, 0.05667, -0.6529 0.6662, 0.06411, -0.6514 0.6274, 0.07172, -0.6475 0.6009, 0.07523, -0.7072 0.6069, 0.02889, 0.0050 0.6079, -0.01747, -0.4132 0.6167, -0.06381, -0.9284 0.6558, -0.05300, -0.8563 0.7045, -0.04117, -0.1915 0.7429, -0.03210, -0.1056 0.8333, -0.01400, -0.0904 0.9311, -0.00120, -0.1564 --------- Run Conditions: vel=104.7 ft/s Re=0.992x10^6 AOA=27.01 Flap deflection=-5.00 Totals: Cl=0.6354 Cdp=0.3756 Cm(c/4)=-0.0834 Cs=-0.0461 Ch=-0.0198 Main component: Cl=0.4875 Cdp=0.2978 Cm=-0.1307 Flap component: Cl=0.1479 Cdp=0.0779 Cm=-0.1369 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3584 0.5905, -0.01667, -0.0642 0.5709, 0.03110, 0.0622 0.5889, 0.07933, -0.8294 0.5500, 0.08689, -0.8483 0.5110, 0.09367, -0.8793 0.4731, 0.09830, -0.8463 0.4349, 0.10070, -0.8057 0.3960, 0.10120, -0.7904 0.3566, 0.10020, -0.7734 0.3172, 0.09790, -0.7750 0.2778, 0.09440, -0.7907 0.2393, 0.08960, -0.7777 0.2056, 0.08360, -0.7995 0.1633, 0.07610, -0.7809 0.1261, 0.06710, -0.7837 0.0900, 0.05640, -0.7635 0.0571, 0.04390, -0.7716 0.0283, 0.02940, -0.7719 0.0142, 0.01970, -0.7829 0.0081, 0.01410, -0.7986 0.0026, 0.00780, -0.7739 0.0000, 0.00000, -0.8353 0.0037, -0.00840, 0.2432 0.0112, -0.01420, 0.7955 0.0191, -0.01930, 0.9450 0.0397, -0.03030, 0.9993 0.0706, -0.04420, 0.9187 0.1037, -0.05710, 0.8163 0.1384, -0.06890, 0.6957 0.1741, -0.07950, 0.5651 0.2102, -0.08660, 0.4053 0.2472, -0.09640, 0.2594 0.2844, -0.10270, 0.0950 0.3225, -0.10690, -0.0266 0.3608, -0.10890, -0.1769 0.3991, -0.10830, -0.2881 0.4373, -0.10510, -0.3479 0.4757, -0.09890, -0.3443 0.5137, -0.09067, -0.2618 0.5611, -0.07859, -0.1717 16 Flap element taps 1.0000, 0.00130, -0.7020 0.9365, 0.01390, -0.7184 0.8333, 0.03280, -0.7260 0.7436, 0.04930, -0.7170 0.7049, 0.05667, -0.7123 0.6662, 0.06411, -0.7109 0.6274, 0.07172, -0.7036 0.6009, 0.07523, -0.7623 0.6069, 0.02889, -0.0031 0.6079, -0.01747, -0.4109 0.6167, -0.06381, -0.8514 0.6558, -0.05300, -0.8116 0.7045, -0.04117, -0.1740 0.7429, -0.03210, -0.0901 0.8333, -0.01400, -0.0871 0.9311, -0.00120, -0.1678