S809 SPOILER FLAP, CLEAN, CHORD = 18 INCHES --------- Run Conditions: vel=104.0 ft/s Re=1.000x10^6 AOA=-5.98 Flap deflection=0.00 Totals: Cl=-0.5301 Cdp=0.0179 Cm(c/4)=-0.0257 Cs=0.0374 Ch=-0.0145 Main component: Cl=-0.5464 Cdp=0.0523 Cm=0.1250 Flap component: Cl=0.0163 Cdp=-0.0343 Cm=-0.0185 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.2966 0.5905, -0.01667, -0.2535 0.5709, 0.03110, -0.2555 0.5889, 0.07933, -0.2810 0.5500, 0.08689, -0.3632 0.5110, 0.09367, -0.4298 0.4731, 0.09830, -0.4294 0.4349, 0.10070, -0.4269 0.3960, 0.10120, -0.3853 0.3566, 0.10020, -0.3271 0.3172, 0.09790, -0.2573 0.2778, 0.09440, -0.2110 0.2393, 0.08960, -0.1451 0.2056, 0.08360, -0.0768 0.1633, 0.07610, 0.0287 0.1261, 0.06710, 0.1539 0.0900, 0.05640, 0.3165 0.0571, 0.04390, 0.5254 0.0283, 0.02940, 0.7994 0.0142, 0.01970, 0.9771 0.0081, 0.01410, 0.9880 0.0026, 0.00780, 0.7661 0.0000, 0.00000, -0.5183 0.0037, -0.00840, -1.5545 0.0112, -0.01420, -1.3141 0.0191, -0.01930, -1.1299 0.0397, -0.03030, -0.9204 0.0706, -0.04420, -0.8855 0.1037, -0.05710, -0.9311 0.1384, -0.06890, -0.9922 0.1741, -0.07950, -1.0557 0.2102, -0.08660, -1.1278 0.2472, -0.09640, -1.2162 0.2844, -0.10270, -1.2558 0.3225, -0.10690, -1.2861 0.3608, -0.10890, -1.2944 0.3991, -0.10830, -1.2484 0.4373, -0.10510, -1.1506 0.4757, -0.09890, -1.0793 0.5137, -0.09067, -0.5839 0.5611, -0.07859, -0.3937 16 Flap element taps 1.0000, 0.00130, 0.1798 0.9365, 0.01390, 0.1086 0.8333, 0.03280, 0.0293 0.7436, 0.04930, -0.0410 0.7049, 0.05667, -0.0146 0.6662, 0.06411, -0.0555 0.6274, 0.07172, -0.0862 0.6009, 0.07523, 0.0975 0.6069, 0.02889, -0.2597 0.6079, -0.01747, -0.2551 0.6167, -0.06381, -0.2685 0.6558, -0.05300, -0.0914 0.7045, -0.04117, 0.0115 0.7429, -0.03210, 0.0516 0.8333, -0.01400, 0.1462 0.9311, -0.00120, 0.2283 Wake drag found for this condition, Cdw=0.0115 --------- Run Conditions: vel=104.7 ft/s Re=1.007x10^6 AOA=-0.02 Flap deflection=0.00 Totals: Cl=0.1207 Cdp=0.0142 Cm(c/4)=-0.0448 Cs=-0.0142 Ch=0.0167 Main component: Cl=0.0291 Cdp=0.0486 Cm=-0.0040 Flap component: Cl=0.0916 Cdp=-0.0345 Cm=-0.0710 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3293 0.5905, -0.01667, -0.2693 0.5709, 0.03110, -0.2773 0.5889, 0.07933, -0.3205 0.5500, 0.08689, -0.6290 0.5110, 0.09367, -0.6699 0.4731, 0.09830, -0.7020 0.4349, 0.10070, -0.7349 0.3960, 0.10120, -0.7285 0.3566, 0.10020, -0.6983 0.3172, 0.09790, -0.6537 0.2778, 0.09440, -0.6445 0.2393, 0.08960, -0.6183 0.2056, 0.08360, -0.5928 0.1633, 0.07610, -0.5301 0.1261, 0.06710, -0.4589 0.0900, 0.05640, -0.3630 0.0571, 0.04390, -0.2308 0.0283, 0.02940, -0.0135 0.0142, 0.01970, 0.2451 0.0081, 0.01410, 0.4146 0.0026, 0.00780, 0.7032 0.0000, 0.00000, 0.9870 0.0037, -0.00840, 0.6807 0.0112, -0.01420, 0.4277 0.0191, -0.01930, 0.3147 0.0397, -0.03030, 0.1506 0.0706, -0.04420, -0.0294 0.1037, -0.05710, -0.1786 0.1384, -0.06890, -0.3114 0.1741, -0.07950, -0.4272 0.2102, -0.08660, -0.5472 0.2472, -0.09640, -0.6718 0.2844, -0.10270, -0.7537 0.3225, -0.10690, -0.8220 0.3608, -0.10890, -0.8763 0.3991, -0.10830, -0.8802 0.4373, -0.10510, -0.8036 0.4757, -0.09890, -0.7321 0.5137, -0.09067, -0.5221 0.5611, -0.07859, -0.2446 16 Flap element taps 1.0000, 0.00130, 0.1667 0.9365, 0.01390, 0.0801 0.8333, 0.03280, -0.0375 0.7436, 0.04930, -0.1402 0.7049, 0.05667, -0.1397 0.6662, 0.06411, -0.2021 0.6274, 0.07172, -0.2689 0.6009, 0.07523, -0.2573 0.6069, 0.02889, -0.2913 0.6079, -0.01747, -0.2880 0.6167, -0.06381, 0.1749 0.6558, -0.05300, 0.0455 0.7045, -0.04117, 0.1249 0.7429, -0.03210, 0.1383 0.8333, -0.01400, 0.2126 0.9311, -0.00120, 0.2701 Wake drag found for this condition, Cdw=0.0098 --------- Run Conditions: vel=105.2 ft/s Re=1.010x10^6 AOA=2.99 Flap deflection=0.00 Totals: Cl=0.4578 Cdp=0.0219 Cm(c/4)=-0.0543 Cs=0.0021 Ch=0.0334 Main component: Cl=0.3282 Cdp=0.0493 Cm=-0.0715 Flap component: Cl=0.1296 Cdp=-0.0274 Cm=-0.0974 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3336 0.5905, -0.01667, -0.3141 0.5709, 0.03110, -0.2967 0.5889, 0.07933, -0.3366 0.5500, 0.08689, -0.7507 0.5110, 0.09367, -0.7962 0.4731, 0.09830, -0.8463 0.4349, 0.10070, -0.8963 0.3960, 0.10120, -0.9092 0.3566, 0.10020, -0.8982 0.3172, 0.09790, -0.8729 0.2778, 0.09440, -0.8831 0.2393, 0.08960, -0.8850 0.2056, 0.08360, -0.8922 0.1633, 0.07610, -0.8596 0.1261, 0.06710, -0.8343 0.0900, 0.05640, -0.7990 0.0571, 0.04390, -0.7590 0.0283, 0.02940, -0.6738 0.0142, 0.01970, -0.5312 0.0081, 0.01410, -0.4279 0.0026, 0.00780, -0.1501 0.0000, 0.00000, 0.4886 0.0037, -0.00840, 0.9892 0.0112, -0.01420, 0.8689 0.0191, -0.01930, 0.7474 0.0397, -0.03030, 0.5388 0.0706, -0.04420, 0.3196 0.1037, -0.05710, 0.1457 0.1384, -0.06890, -0.0049 0.1741, -0.07950, -0.1374 0.2102, -0.08660, -0.2737 0.2472, -0.09640, -0.4051 0.2844, -0.10270, -0.5038 0.3225, -0.10690, -0.5853 0.3608, -0.10890, -0.6586 0.3991, -0.10830, -0.6833 0.4373, -0.10510, -0.6342 0.4757, -0.09890, -0.5522 0.5137, -0.09067, -0.5175 0.5611, -0.07859, -0.1511 16 Flap element taps 1.0000, 0.00130, 0.1624 0.9365, 0.01390, 0.0693 0.8333, 0.03280, -0.0698 0.7436, 0.04930, -0.1895 0.7049, 0.05667, -0.1989 0.6662, 0.06411, -0.2741 0.6274, 0.07172, -0.3626 0.6009, 0.07523, -0.4182 0.6069, 0.02889, -0.3017 0.6079, -0.01747, -0.3062 0.6167, -0.06381, 0.4462 0.6558, -0.05300, 0.1101 0.7045, -0.04117, 0.1807 0.7429, -0.03210, 0.1837 0.8333, -0.01400, 0.2461 0.9311, -0.00120, 0.2897 Wake drag found for this condition, Cdw=0.0100 --------- Run Conditions: vel=105.3 ft/s Re=1.010x10^6 AOA=6.01 Flap deflection=0.00 Totals: Cl=0.7577 Cdp=0.0236 Cm(c/4)=-0.0576 Cs=0.0558 Ch=0.0478 Main component: Cl=0.5975 Cdp=0.0441 Cm=-0.1281 Flap component: Cl=0.1602 Cdp=-0.0205 Cm=-0.1185 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3549 0.5905, -0.01667, -0.3307 0.5709, 0.03110, -0.3034 0.5889, 0.07933, -0.3371 0.5500, 0.08689, -0.5523 0.5110, 0.09367, -0.8592 0.4731, 0.09830, -0.9573 0.4349, 0.10070, -1.0247 0.3960, 0.10120, -1.0617 0.3566, 0.10020, -1.0701 0.3172, 0.09790, -1.0694 0.2778, 0.09440, -1.1039 0.2393, 0.08960, -1.1358 0.2056, 0.08360, -1.1808 0.1633, 0.07610, -1.1870 0.1261, 0.06710, -1.2150 0.0900, 0.05640, -1.2531 0.0571, 0.04390, -1.3346 0.0283, 0.02940, -1.4443 0.0142, 0.01970, -1.5004 0.0081, 0.01410, -1.6259 0.0026, 0.00780, -1.4430 0.0000, 0.00000, -0.9354 0.0037, -0.00840, 0.8342 0.0112, -0.01420, 0.9946 0.0191, -0.01930, 0.9608 0.0397, -0.03030, 0.7997 0.0706, -0.04420, 0.5861 0.1037, -0.05710, 0.4100 0.1384, -0.06890, 0.2536 0.1741, -0.07950, 0.1113 0.2102, -0.08660, -0.0344 0.2472, -0.09640, -0.1703 0.2844, -0.10270, -0.2833 0.3225, -0.10690, -0.3753 0.3608, -0.10890, -0.4629 0.3991, -0.10830, -0.5046 0.4373, -0.10510, -0.4791 0.4757, -0.09890, -0.4010 0.5137, -0.09067, -0.3586 0.5611, -0.07859, -0.0369 16 Flap element taps 1.0000, 0.00130, 0.0969 0.9365, 0.01390, 0.0357 0.8333, 0.03280, -0.0952 0.7436, 0.04930, -0.2240 0.7049, 0.05667, -0.2594 0.6662, 0.06411, -0.3515 0.6274, 0.07172, -0.4622 0.6009, 0.07523, -0.6249 0.6069, 0.02889, -0.3187 0.6079, -0.01747, -0.3475 0.6167, -0.06381, 0.5865 0.6558, -0.05300, 0.1710 0.7045, -0.04117, 0.2258 0.7429, -0.03210, 0.2176 0.8333, -0.01400, 0.2636 0.9311, -0.00120, 0.2857 Wake drag found for this condition, Cdw=0.0112 --------- Run Conditions: vel=105.2 ft/s Re=1.009x10^6 AOA=9.00 Flap deflection=0.00 Totals: Cl=0.8369 Cdp=0.0422 Cm(c/4)=-0.0419 Cs=0.0893 Ch=0.0216 Main component: Cl=0.6848 Cdp=0.0347 Cm=-0.1324 Flap component: Cl=0.1521 Cdp=0.0074 Cm=-0.1178 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.2850 0.5905, -0.01667, -0.2524 0.5709, 0.03110, -0.2402 0.5889, 0.07933, -0.2625 0.5500, 0.08689, -0.3976 0.5110, 0.09367, -0.6387 0.4731, 0.09830, -0.7999 0.4349, 0.10070, -0.9173 0.3960, 0.10120, -0.9910 0.3566, 0.10020, -1.0373 0.3172, 0.09790, -1.0583 0.2778, 0.09440, -1.1184 0.2393, 0.08960, -1.1882 0.2056, 0.08360, -1.2712 0.1633, 0.07610, -1.3133 0.1261, 0.06710, -1.3746 0.0900, 0.05640, -1.4952 0.0571, 0.04390, -1.6983 0.0283, 0.02940, -1.9804 0.0142, 0.01970, -2.2205 0.0081, 0.01410, -2.4923 0.0026, 0.00780, -2.5531 0.0000, 0.00000, -2.3201 0.0037, -0.00840, 0.4917 0.0112, -0.01420, 0.9535 0.0191, -0.01930, 0.9959 0.0397, -0.03030, 0.9105 0.0706, -0.04420, 0.7224 0.1037, -0.05710, 0.5507 0.1384, -0.06890, 0.3931 0.1741, -0.07950, 0.2512 0.2102, -0.08660, 0.0960 0.2472, -0.09640, -0.0469 0.2844, -0.10270, -0.1683 0.3225, -0.10690, -0.2738 0.3608, -0.10890, -0.3728 0.3991, -0.10830, -0.4328 0.4373, -0.10510, -0.4262 0.4757, -0.09890, -0.3584 0.5137, -0.09067, -0.3030 0.5611, -0.07859, -0.0460 16 Flap element taps 1.0000, 0.00130, -0.1522 0.9365, 0.01390, -0.1989 0.8333, 0.03280, -0.2095 0.7436, 0.04930, -0.2257 0.7049, 0.05667, -0.2237 0.6662, 0.06411, -0.2472 0.6274, 0.07172, -0.2707 0.6009, 0.07523, -0.3113 0.6069, 0.02889, -0.2549 0.6079, -0.01747, -0.2619 0.6167, -0.06381, 0.5081 0.6558, -0.05300, 0.1432 0.7045, -0.04117, 0.1914 0.7429, -0.03210, 0.1760 0.8333, -0.01400, 0.2035 0.9311, -0.00120, 0.1818 --------- Run Conditions: vel=105.0 ft/s Re=1.007x10^6 AOA=12.00 Flap deflection=0.00 Totals: Cl=0.9568 Cdp=0.0659 Cm(c/4)=-0.0395 Cs=0.1345 Ch=0.0232 Main component: Cl=0.7812 Cdp=0.0396 Cm=-0.1387 Flap component: Cl=0.1756 Cdp=0.0262 Cm=-0.1382 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3053 0.5905, -0.01667, -0.2909 0.5709, 0.03110, -0.2661 0.5889, 0.07933, -0.3014 0.5500, 0.08689, -0.3195 0.5110, 0.09367, -0.4258 0.4731, 0.09830, -0.6037 0.4349, 0.10070, -0.7734 0.3960, 0.10120, -0.9038 0.3566, 0.10020, -0.9957 0.3172, 0.09790, -1.0584 0.2778, 0.09440, -1.1532 0.2393, 0.08960, -1.2570 0.2056, 0.08360, -1.3778 0.1633, 0.07610, -1.4666 0.1261, 0.06710, -1.5915 0.0900, 0.05640, -1.7731 0.0571, 0.04390, -2.0519 0.0283, 0.02940, -2.4967 0.0142, 0.01970, -3.1120 0.0081, 0.01410, -3.6996 0.0026, 0.00780, -3.9243 0.0000, 0.00000, -4.1573 0.0037, -0.00840, -0.0842 0.0112, -0.01420, 0.7893 0.0191, -0.01930, 0.9615 0.0397, -0.03030, 0.9773 0.0706, -0.04420, 0.8358 0.1037, -0.05710, 0.6824 0.1384, -0.06890, 0.5295 0.1741, -0.07950, 0.3865 0.2102, -0.08660, 0.2327 0.2472, -0.09640, 0.0871 0.2844, -0.10270, -0.0415 0.3225, -0.10690, -0.1549 0.3608, -0.10890, -0.2658 0.3991, -0.10830, -0.3380 0.4373, -0.10510, -0.3516 0.4757, -0.09890, -0.3003 0.5137, -0.09067, -0.2379 0.5611, -0.07859, -0.1394 16 Flap element taps 1.0000, 0.00130, -0.2724 0.9365, 0.01390, -0.3217 0.8333, 0.03280, -0.3142 0.7436, 0.04930, -0.3109 0.7049, 0.05667, -0.2976 0.6662, 0.06411, -0.3053 0.6274, 0.07172, -0.3027 0.6009, 0.07523, -0.2991 0.6069, 0.02889, -0.2825 0.6079, -0.01747, -0.3046 0.6167, -0.06381, 0.5614 0.6558, -0.05300, 0.1520 0.7045, -0.04117, 0.1932 0.7429, -0.03210, 0.1685 0.8333, -0.01400, 0.1788 0.9311, -0.00120, 0.1307 --------- Run Conditions: vel=104.7 ft/s Re=1.003x10^6 AOA=15.00 Flap deflection=0.00 Totals: Cl=1.0392 Cdp=0.0998 Cm(c/4)=-0.0433 Cs=0.1726 Ch=0.0303 Main component: Cl=0.8383 Cdp=0.0571 Cm=-0.1413 Flap component: Cl=0.2009 Cdp=0.0427 Cm=-0.1594 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3600 0.5905, -0.01667, -0.3741 0.5709, 0.03110, -0.3333 0.5889, 0.07933, -0.3844 0.5500, 0.08689, -0.3804 0.5110, 0.09367, -0.3979 0.4731, 0.09830, -0.4351 0.4349, 0.10070, -0.5477 0.3960, 0.10120, -0.7048 0.3566, 0.10020, -0.8452 0.3172, 0.09790, -0.9565 0.2778, 0.09440, -1.0891 0.2393, 0.08960, -1.2313 0.2056, 0.08360, -1.3928 0.1633, 0.07610, -1.5264 0.1261, 0.06710, -1.7073 0.0900, 0.05640, -1.9559 0.0571, 0.04390, -2.3473 0.0283, 0.02940, -2.9892 0.0142, 0.01970, -3.6337 0.0081, 0.01410, -4.8385 0.0026, 0.00780, -5.3025 0.0000, 0.00000, -5.9973 0.0037, -0.00840, -0.7368 0.0112, -0.01420, 0.5546 0.0191, -0.01930, 0.8688 0.0397, -0.03030, 0.9959 0.0706, -0.04420, 0.9095 0.1037, -0.05710, 0.7793 0.1384, -0.06890, 0.6363 0.1741, -0.07950, 0.4982 0.2102, -0.08660, 0.3438 0.2472, -0.09640, 0.1990 0.2844, -0.10270, 0.0646 0.3225, -0.10690, -0.0549 0.3608, -0.10890, -0.1732 0.3991, -0.10830, -0.2600 0.4373, -0.10510, -0.2885 0.4757, -0.09890, -0.2540 0.5137, -0.09067, -0.1922 0.5611, -0.07859, -0.1392 16 Flap element taps 1.0000, 0.00130, -0.3769 0.9365, 0.01390, -0.4136 0.8333, 0.03280, -0.4073 0.7436, 0.04930, -0.3969 0.7049, 0.05667, -0.3827 0.6662, 0.06411, -0.3892 0.6274, 0.07172, -0.3862 0.6009, 0.07523, -0.3828 0.6069, 0.02889, -0.3503 0.6079, -0.01747, -0.3900 0.6167, -0.06381, 0.6560 0.6558, -0.05300, 0.1575 0.7045, -0.04117, 0.1925 0.7429, -0.03210, 0.1616 0.8333, -0.01400, 0.1586 0.9311, -0.00120, 0.0871 --------- Run Conditions: vel=103.4 ft/s Re=0.990x10^6 AOA=17.95 Flap deflection=0.00 Totals: Cl=0.9554 Cdp=0.1676 Cm(c/4)=-0.0672 Cs=0.1350 Ch=0.0389 Main component: Cl=0.7200 Cdp=0.1022 Cm=-0.1181 Flap component: Cl=0.2355 Cdp=0.0654 Cm=-0.1892 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.4500 0.5905, -0.01667, -0.5078 0.5709, 0.03110, -0.4532 0.5889, 0.07933, -0.5472 0.5500, 0.08689, -0.5256 0.5110, 0.09367, -0.5150 0.4731, 0.09830, -0.5049 0.4349, 0.10070, -0.5048 0.3960, 0.10120, -0.5264 0.3566, 0.10020, -0.5328 0.3172, 0.09790, -0.5454 0.2778, 0.09440, -0.6046 0.2393, 0.08960, -0.7427 0.2056, 0.08360, -0.9683 0.1633, 0.07610, -1.1749 0.1261, 0.06710, -1.4281 0.0900, 0.05640, -1.7276 0.0571, 0.04390, -2.1796 0.0283, 0.02940, -2.8970 0.0142, 0.01970, -3.5946 0.0081, 0.01410, -4.9933 0.0026, 0.00780, -5.5277 0.0000, 0.00000, -6.4034 0.0037, -0.00840, -0.9461 0.0112, -0.01420, 0.4626 0.0191, -0.01930, 0.8231 0.0397, -0.03030, 0.9950 0.0706, -0.04420, 0.9306 0.1037, -0.05710, 0.8108 0.1384, -0.06890, 0.6727 0.1741, -0.07950, 0.5336 0.2102, -0.08660, 0.3792 0.2472, -0.09640, 0.2322 0.2844, -0.10270, 0.0921 0.3225, -0.10690, -0.0342 0.3608, -0.10890, -0.1627 0.3991, -0.10830, -0.2583 0.4373, -0.10510, -0.2987 0.4757, -0.09890, -0.2759 0.5137, -0.09067, -0.2149 0.5611, -0.07859, -0.1473 16 Flap element taps 1.0000, 0.00130, -0.5363 0.9365, 0.01390, -0.5630 0.8333, 0.03280, -0.5703 0.7436, 0.04930, -0.5602 0.7049, 0.05667, -0.5372 0.6662, 0.06411, -0.5420 0.6274, 0.07172, -0.5338 0.6009, 0.07523, -0.5245 0.6069, 0.02889, -0.4765 0.6079, -0.01747, -0.5323 0.6167, -0.06381, 0.7367 0.6558, -0.05300, 0.1213 0.7045, -0.04117, 0.1521 0.7429, -0.03210, 0.1135 0.8333, -0.01400, 0.1027 0.9311, -0.00120, 0.0100 --------- Run Conditions: vel=106.8 ft/s Re=1.021x10^6 AOA=19.97 Flap deflection=0.00 Totals: Cl=0.6168 Cdp=0.3254 Cm(c/4)=-0.1122 Cs=-0.0951 Ch=0.0418 Main component: Cl=0.3750 Cdp=0.2521 Cm=-0.0896 Flap component: Cl=0.2418 Cdp=0.0732 Cm=-0.1953 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.6223 0.5905, -0.01667, -0.6635 0.5709, 0.03110, -0.6070 0.5889, 0.07933, -0.7440 0.5500, 0.08689, -0.6993 0.5110, 0.09367, -0.6900 0.4731, 0.09830, -0.6753 0.4349, 0.10070, -0.6812 0.3960, 0.10120, -0.7014 0.3566, 0.10020, -0.7011 0.3172, 0.09790, -0.6938 0.2778, 0.09440, -0.6926 0.2393, 0.08960, -0.6899 0.2056, 0.08360, -0.7138 0.1633, 0.07610, -0.6947 0.1261, 0.06710, -0.7058 0.0900, 0.05640, -0.6863 0.0571, 0.04390, -0.7001 0.0283, 0.02940, -0.7203 0.0142, 0.01970, -0.7209 0.0081, 0.01410, -0.7387 0.0026, 0.00780, -0.7193 0.0000, 0.00000, -1.0020 0.0037, -0.00840, 0.5579 0.0112, -0.01420, 0.9324 0.0191, -0.01930, 0.9907 0.0397, -0.03030, 0.9542 0.0706, -0.04420, 0.8128 0.1037, -0.05710, 0.6670 0.1384, -0.06890, 0.5211 0.1741, -0.07950, 0.3776 0.2102, -0.08660, 0.2132 0.2472, -0.09640, 0.0609 0.2844, -0.10270, -0.0839 0.3225, -0.10690, -0.2140 0.3608, -0.10890, -0.3461 0.3991, -0.10830, -0.4428 0.4373, -0.10510, -0.4801 0.4757, -0.09890, -0.4437 0.5137, -0.09067, -0.3762 0.5611, -0.07859, -0.3138 16 Flap element taps 1.0000, 0.00130, -0.6341 0.9365, 0.01390, -0.6708 0.8333, 0.03280, -0.6921 0.7436, 0.04930, -0.6910 0.7049, 0.05667, -0.6728 0.6662, 0.06411, -0.6783 0.6274, 0.07172, -0.6682 0.6009, 0.07523, -0.6484 0.6069, 0.02889, -0.6261 0.6079, -0.01747, -0.6874 0.6167, -0.06381, 0.6507 0.6558, -0.05300, 0.0163 0.7045, -0.04117, 0.0530 0.7429, -0.03210, 0.0099 0.8333, -0.01400, 0.0012 0.9311, -0.00120, -0.0915 --------- Run Conditions: vel=105.5 ft/s Re=1.004x10^6 AOA=23.99 Flap deflection=0.00 Totals: Cl=0.7052 Cdp=0.4271 Cm(c/4)=-0.1349 Cs=-0.1035 Ch=0.0499 Main component: Cl=0.4403 Cdp=0.3251 Cm=-0.1204 Flap component: Cl=0.2649 Cdp=0.1019 Cm=-0.2190 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.6238 0.5905, -0.01667, -0.7527 0.5709, 0.03110, -0.6734 0.5889, 0.07933, -0.8155 0.5500, 0.08689, -0.7876 0.5110, 0.09367, -0.7797 0.4731, 0.09830, -0.7625 0.4349, 0.10070, -0.7566 0.3960, 0.10120, -0.7625 0.3566, 0.10020, -0.7618 0.3172, 0.09790, -0.7575 0.2778, 0.09440, -0.7620 0.2393, 0.08960, -0.7605 0.2056, 0.08360, -0.7594 0.1633, 0.07610, -0.7627 0.1261, 0.06710, -0.7647 0.0900, 0.05640, -0.7571 0.0571, 0.04390, -0.7537 0.0283, 0.02940, -0.7659 0.0142, 0.01970, -0.7677 0.0081, 0.01410, -0.7739 0.0026, 0.00780, -0.7674 0.0000, 0.00000, -1.0072 0.0037, -0.00840, 0.3604 0.0112, -0.01420, 0.8533 0.0191, -0.01930, 0.9775 0.0397, -0.03030, 0.9953 0.0706, -0.04420, 0.8936 0.1037, -0.05710, 0.7740 0.1384, -0.06890, 0.6273 0.1741, -0.07950, 0.4908 0.2102, -0.08660, 0.3522 0.2472, -0.09640, 0.1933 0.2844, -0.10270, 0.0516 0.3225, -0.10690, -0.0872 0.3608, -0.10890, -0.2265 0.3991, -0.10830, -0.3394 0.4373, -0.10510, -0.3809 0.4757, -0.09890, -0.3756 0.5137, -0.09067, -0.3029 0.5611, -0.07859, -0.2289 16 Flap element taps 1.0000, 0.00130, -0.7137 0.9365, 0.01390, -0.7453 0.8333, 0.03280, -0.7678 0.7436, 0.04930, -0.7660 0.7049, 0.05667, -0.7609 0.6662, 0.06411, -0.7632 0.6274, 0.07172, -0.7483 0.6009, 0.07523, -0.7397 0.6069, 0.02889, -0.6919 0.6079, -0.01747, -0.7719 0.6167, -0.06381, 0.7925 0.6558, -0.05300, 0.0386 0.7045, -0.04117, 0.0644 0.7429, -0.03210, 0.0053 0.8333, -0.01400, -0.0019 0.9311, -0.00120, -0.1011 --------- Run Conditions: vel=104.4 ft/s Re=0.993x10^6 AOA=26.98 Flap deflection=0.00 Totals: Cl=0.8483 Cdp=0.5523 Cm(c/4)=-0.1716 Cs=-0.1073 Ch=0.0604 Main component: Cl=0.5399 Cdp=0.4142 Cm=-0.1627 Flap component: Cl=0.3084 Cdp=0.1381 Cm=-0.2605 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.6648 0.5905, -0.01667, -0.8675 0.5709, 0.03110, -0.7847 0.5889, 0.07933, -0.9590 0.5500, 0.08689, -0.9473 0.5110, 0.09367, -0.9365 0.4731, 0.09830, -0.9167 0.4349, 0.10070, -0.9056 0.3960, 0.10120, -0.9086 0.3566, 0.10020, -0.9101 0.3172, 0.09790, -0.9067 0.2778, 0.09440, -0.9117 0.2393, 0.08960, -0.9090 0.2056, 0.08360, -0.9054 0.1633, 0.07610, -0.9097 0.1261, 0.06710, -0.9098 0.0900, 0.05640, -0.9040 0.0571, 0.04390, -0.9011 0.0283, 0.02940, -0.9093 0.0142, 0.01970, -0.9113 0.0081, 0.01410, -0.9190 0.0026, 0.00780, -0.9128 0.0000, 0.00000, -0.9642 0.0037, -0.00840, 0.1055 0.0112, -0.01420, 0.7282 0.0191, -0.01930, 0.9162 0.0397, -0.03030, 1.0020 0.0706, -0.04420, 0.9457 0.1037, -0.05710, 0.8523 0.1384, -0.06890, 0.7201 0.1741, -0.07950, 0.5936 0.2102, -0.08660, 0.4659 0.2472, -0.09640, 0.3110 0.2844, -0.10270, 0.1719 0.3225, -0.10690, 0.0334 0.3608, -0.10890, -0.1088 0.3991, -0.10830, -0.2311 0.4373, -0.10510, -0.2859 0.4757, -0.09890, -0.2978 0.5137, -0.09067, -0.2352 0.5611, -0.07859, -0.1725 16 Flap element taps 1.0000, 0.00130, -0.8826 0.9365, 0.01390, -0.9066 0.8333, 0.03280, -0.9210 0.7436, 0.04930, -0.9238 0.7049, 0.05667, -0.9172 0.6662, 0.06411, -0.9176 0.6274, 0.07172, -0.9027 0.6009, 0.07523, -0.8964 0.6069, 0.02889, -0.8056 0.6079, -0.01747, -0.9045 0.6167, -0.06381, 0.8439 0.6558, -0.05300, 0.0674 0.7045, -0.04117, 0.0782 0.7429, -0.03210, 0.0114 0.8333, -0.01400, -0.0164 0.9311, -0.00120, -0.1449 --------- Run Conditions: vel=103.4 ft/s Re=0.985x10^6 AOA=29.96 Flap deflection=0.00 Totals: Cl=0.9858 Cdp=0.6936 Cm(c/4)=-0.2096 Cs=-0.1087 Ch=0.0715 Main component: Cl=0.6361 Cdp=0.5156 Cm=-0.2075 Flap component: Cl=0.3497 Cdp=0.1780 Cm=-0.3023 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.6982 0.5905, -0.01667, -0.9991 0.5709, 0.03110, -0.9072 0.5889, 0.07933, -1.1447 0.5500, 0.08689, -1.1177 0.5110, 0.09367, -1.1069 0.4731, 0.09830, -1.0846 0.4349, 0.10070, -1.0734 0.3960, 0.10120, -1.0773 0.3566, 0.10020, -1.0738 0.3172, 0.09790, -1.0699 0.2778, 0.09440, -1.0754 0.2393, 0.08960, -1.0708 0.2056, 0.08360, -1.0648 0.1633, 0.07610, -1.0675 0.1261, 0.06710, -1.0685 0.0900, 0.05640, -1.0604 0.0571, 0.04390, -1.0560 0.0283, 0.02940, -1.0603 0.0142, 0.01970, -1.0606 0.0081, 0.01410, -1.0685 0.0026, 0.00780, -1.0610 0.0000, 0.00000, -1.0938 0.0037, -0.00840, -0.1684 0.0112, -0.01420, 0.5779 0.0191, -0.01930, 0.8321 0.0397, -0.03030, 0.9921 0.0706, -0.04420, 0.9824 0.1037, -0.05710, 0.9173 0.1384, -0.06890, 0.8019 0.1741, -0.07950, 0.6876 0.2102, -0.08660, 0.5696 0.2472, -0.09640, 0.4235 0.2844, -0.10270, 0.2884 0.3225, -0.10690, 0.1490 0.3608, -0.10890, 0.0044 0.3991, -0.10830, -0.1214 0.4373, -0.10510, -0.1892 0.4757, -0.09890, -0.2156 0.5137, -0.09067, -0.1591 0.5611, -0.07859, -0.1203 16 Flap element taps 1.0000, 0.00130, -1.0449 0.9365, 0.01390, -1.0534 0.8333, 0.03280, -1.0680 0.7436, 0.04930, -1.0743 0.7049, 0.05667, -1.0738 0.6662, 0.06411, -1.0754 0.6274, 0.07172, -1.0597 0.6009, 0.07523, -1.0578 0.6069, 0.02889, -0.9225 0.6079, -0.01747, -1.0306 0.6167, -0.06381, 0.8730 0.6558, -0.05300, 0.1006 0.7045, -0.04117, 0.1018 0.7429, -0.03210, 0.0262 0.8333, -0.01400, -0.0199 0.9311, -0.00120, -0.1812 --------- Run Conditions: vel=105.5 ft/s Re=1.002x10^6 AOA=34.95 Flap deflection=0.00 Totals: Cl=1.1274 Cdp=0.9182 Cm(c/4)=-0.2667 Cs=-0.1067 Ch=0.0834 Main component: Cl=0.7283 Cdp=0.6663 Cm=-0.2651 Flap component: Cl=0.3991 Cdp=0.2519 Cm=-0.3641 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.6855 0.5905, -0.01667, -1.1148 0.5709, 0.03110, -1.0302 0.5889, 0.07933, -1.3830 0.5500, 0.08689, -1.3285 0.5110, 0.09367, -1.3102 0.4731, 0.09830, -1.2781 0.4349, 0.10070, -1.2645 0.3960, 0.10120, -1.2633 0.3566, 0.10020, -1.2651 0.3172, 0.09790, -1.2567 0.2778, 0.09440, -1.2537 0.2393, 0.08960, -1.2497 0.2056, 0.08360, -1.2369 0.1633, 0.07610, -1.2376 0.1261, 0.06710, -1.2366 0.0900, 0.05640, -1.2276 0.0571, 0.04390, -1.2204 0.0283, 0.02940, -1.2208 0.0142, 0.01970, -1.2206 0.0081, 0.01410, -1.2257 0.0026, 0.00780, -1.2221 0.0000, 0.00000, -1.2416 0.0037, -0.00840, -0.5765 0.0112, -0.01420, 0.3084 0.0191, -0.01930, 0.6565 0.0397, -0.03030, 0.9312 0.0706, -0.04420, 0.9974 0.1037, -0.05710, 0.9803 0.1384, -0.06890, 0.8990 0.1741, -0.07950, 0.8094 0.2102, -0.08660, 0.7130 0.2472, -0.09640, 0.5850 0.2844, -0.10270, 0.4603 0.3225, -0.10690, 0.3268 0.3608, -0.10890, 0.1850 0.3991, -0.10830, 0.0541 0.4373, -0.10510, -0.0241 0.4757, -0.09890, -0.0717 0.5137, -0.09067, -0.0307 0.5611, -0.07859, -0.0240 16 Flap element taps 1.0000, 0.00130, -1.2464 0.9365, 0.01390, -1.2630 0.8333, 0.03280, -1.2787 0.7436, 0.04930, -1.2706 0.7049, 0.05667, -1.2638 0.6662, 0.06411, -1.2683 0.6274, 0.07172, -1.2525 0.6009, 0.07523, -1.2500 0.6069, 0.02889, -1.0419 0.6079, -0.01747, -1.1538 0.6167, -0.06381, 0.9061 0.6558, -0.05300, 0.1653 0.7045, -0.04117, 0.1503 0.7429, -0.03210, 0.0673 0.8333, -0.01400, -0.0041 0.9311, -0.00120, -0.2077 --------- Run Conditions: vel=104.4 ft/s Re=0.992x10^6 AOA=39.93 Flap deflection=0.00 Totals: Cl=1.1976 Cdp=1.1341 Cm(c/4)=-0.3145 Cs=-0.1009 Ch=0.0960 Main component: Cl=0.7721 Cdp=0.8082 Cm=-0.3127 Flap component: Cl=0.4256 Cdp=0.3259 Cm=-0.4133 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.6529 0.5905, -0.01667, -1.1827 0.5709, 0.03110, -1.1077 0.5889, 0.07933, -1.5857 0.5500, 0.08689, -1.5091 0.5110, 0.09367, -1.4620 0.4731, 0.09830, -1.4355 0.4349, 0.10070, -1.4184 0.3960, 0.10120, -1.4124 0.3566, 0.10020, -1.4094 0.3172, 0.09790, -1.3955 0.2778, 0.09440, -1.3935 0.2393, 0.08960, -1.3788 0.2056, 0.08360, -1.3657 0.1633, 0.07610, -1.3668 0.1261, 0.06710, -1.3613 0.0900, 0.05640, -1.3450 0.0571, 0.04390, -1.3330 0.0283, 0.02940, -1.3318 0.0142, 0.01970, -1.3279 0.0081, 0.01410, -1.3340 0.0026, 0.00780, -1.3294 0.0000, 0.00000, -1.3443 0.0037, -0.00840, -0.9378 0.0112, -0.01420, 0.0268 0.0191, -0.01930, 0.4522 0.0397, -0.03030, 0.8299 0.0706, -0.04420, 0.9727 0.1037, -0.05710, 1.0037 0.1384, -0.06890, 0.9564 0.1741, -0.07950, 0.8954 0.2102, -0.08660, 0.8237 0.2472, -0.09640, 0.7168 0.2844, -0.10270, 0.6064 0.3225, -0.10690, 0.4836 0.3608, -0.10890, 0.3499 0.3991, -0.10830, 0.2191 0.4373, -0.10510, 0.1317 0.4757, -0.09890, 0.0698 0.5137, -0.09067, 0.0933 0.5611, -0.07859, 0.0728 16 Flap element taps 1.0000, 0.00130, -1.3911 0.9365, 0.01390, -1.4086 0.8333, 0.03280, -1.4221 0.7436, 0.04930, -1.4227 0.7049, 0.05667, -1.4225 0.6662, 0.06411, -1.4299 0.6274, 0.07172, -1.4134 0.6009, 0.07523, -1.4013 0.6069, 0.02889, -1.1212 0.6079, -0.01747, -1.2265 0.6167, -0.06381, 0.9300 0.6558, -0.05300, 0.2351 0.7045, -0.04117, 0.2007 0.7429, -0.03210, 0.1156 0.8333, -0.01400, 0.0195 0.9311, -0.00120, -0.2195 --------- Run Conditions: vel=103.3 ft/s Re=0.980x10^6 AOA=44.95 Flap deflection=0.00 Totals: Cl=1.1971 Cdp=1.3175 Cm(c/4)=-0.3484 Cs=-0.0867 Ch=0.1014 Main component: Cl=0.7730 Cdp=0.9270 Cm=-0.3479 Flap component: Cl=0.4242 Cdp=0.3906 Cm=-0.4450 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.5788 0.5905, -0.01667, -1.1881 0.5709, 0.03110, -1.1149 0.5889, 0.07933, -1.6949 0.5500, 0.08689, -1.5885 0.5110, 0.09367, -1.5610 0.4731, 0.09830, -1.5345 0.4349, 0.10070, -1.5176 0.3960, 0.10120, -1.5078 0.3566, 0.10020, -1.5021 0.3172, 0.09790, -1.4908 0.2778, 0.09440, -1.4840 0.2393, 0.08960, -1.4705 0.2056, 0.08360, -1.4486 0.1633, 0.07610, -1.4476 0.1261, 0.06710, -1.4370 0.0900, 0.05640, -1.4253 0.0571, 0.04390, -1.4109 0.0283, 0.02940, -1.4028 0.0142, 0.01970, -1.3982 0.0081, 0.01410, -1.4015 0.0026, 0.00780, -1.3987 0.0000, 0.00000, -1.4147 0.0037, -0.00840, -1.2319 0.0112, -0.01420, -0.2438 0.0191, -0.01930, 0.2383 0.0397, -0.03030, 0.7028 0.0706, -0.04420, 0.9143 0.1037, -0.05710, 0.9907 0.1384, -0.06890, 0.9774 0.1741, -0.07950, 0.9461 0.2102, -0.08660, 0.9037 0.2472, -0.09640, 0.8183 0.2844, -0.10270, 0.7269 0.3225, -0.10690, 0.6171 0.3608, -0.10890, 0.4958 0.3991, -0.10830, 0.3701 0.4373, -0.10510, 0.2813 0.4757, -0.09890, 0.2098 0.5137, -0.09067, 0.2172 0.5611, -0.07859, 0.1764 16 Flap element taps 1.0000, 0.00130, -1.4697 0.9365, 0.01390, -1.4967 0.8333, 0.03280, -1.4884 0.7436, 0.04930, -1.4744 0.7049, 0.05667, -1.4812 0.6662, 0.06411, -1.4912 0.6274, 0.07172, -1.4803 0.6009, 0.07523, -1.4831 0.6069, 0.02889, -1.1270 0.6079, -0.01747, -1.2305 0.6167, -0.06381, 0.9503 0.6558, -0.05300, 0.3104 0.7045, -0.04117, 0.2643 0.7429, -0.03210, 0.1786 0.8333, -0.01400, 0.0626 0.9311, -0.00120, -0.2016 --------- Run Conditions: vel=105.5 ft/s Re=0.999x10^6 AOA=59.95 Flap deflection=0.00 Totals: Cl=1.0622 Cdp=1.8928 Cm(c/4)=-0.4670 Cs=-0.0284 Ch=0.1261 Main component: Cl=0.6761 Cdp=1.2719 Cm=-0.4447 Flap component: Cl=0.3861 Cdp=0.6209 Cm=-0.5648 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.3424 0.5905, -0.01667, -1.1920 0.5709, 0.03110, -1.1140 0.5889, 0.07933, -2.0215 0.5500, 0.08689, -1.8865 0.5110, 0.09367, -1.8511 0.4731, 0.09830, -1.8192 0.4349, 0.10070, -1.8112 0.3960, 0.10120, -1.7961 0.3566, 0.10020, -1.8041 0.3172, 0.09790, -1.7805 0.2778, 0.09440, -1.7835 0.2393, 0.08960, -1.7610 0.2056, 0.08360, -1.7540 0.1633, 0.07610, -1.7427 0.1261, 0.06710, -1.7129 0.0900, 0.05640, -1.7066 0.0571, 0.04390, -1.6803 0.0283, 0.02940, -1.6582 0.0142, 0.01970, -1.6530 0.0081, 0.01410, -1.6439 0.0026, 0.00780, -1.6469 0.0000, 0.00000, -1.6551 0.0037, -0.00840, -1.8238 0.0112, -0.01420, -1.0364 0.0191, -0.01930, -0.4748 0.0397, -0.03030, 0.1912 0.0706, -0.04420, 0.5913 0.1037, -0.05710, 0.7973 0.1384, -0.06890, 0.8971 0.1741, -0.07950, 0.9604 0.2102, -0.08660, 0.9902 0.2472, -0.09640, 0.9905 0.2844, -0.10270, 0.9686 0.3225, -0.10690, 0.9123 0.3608, -0.10890, 0.8476 0.3991, -0.10830, 0.7540 0.4373, -0.10510, 0.6856 0.4757, -0.09890, 0.6041 0.5137, -0.09067, 0.5745 0.5611, -0.07859, 0.4983 16 Flap element taps 1.0000, 0.00130, -1.6989 0.9365, 0.01390, -1.7394 0.8333, 0.03280, -1.7435 0.7436, 0.04930, -1.7347 0.7049, 0.05667, -1.7298 0.6662, 0.06411, -1.7415 0.6274, 0.07172, -1.7743 0.6009, 0.07523, -1.7883 0.6069, 0.02889, -1.1201 0.6079, -0.01747, -1.2653 0.6167, -0.06381, 1.0077 0.6558, -0.05300, 0.5614 0.7045, -0.04117, 0.4859 0.7429, -0.03210, 0.4018 0.8333, -0.01400, 0.2431 0.9311, -0.00120, -0.1001 --------- Run Conditions: vel=104.3 ft/s Re=0.985x10^6 AOA=70.01 Flap deflection=0.00 Totals: Cl=0.8067 Cdp=2.1816 Cm(c/4)=-0.5416 Cs=0.0123 Ch=0.1426 Main component: Cl=0.5181 Cdp=1.3953 Cm=-0.4757 Flap component: Cl=0.2886 Cdp=0.7863 Cm=-0.6474 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.4150 0.5905, -0.01667, -0.9870 0.5709, 0.03110, -0.7439 0.5889, 0.07933, -2.0785 0.5500, 0.08689, -2.0278 0.5110, 0.09367, -1.9727 0.4731, 0.09830, -1.9341 0.4349, 0.10070, -1.9129 0.3960, 0.10120, -1.8994 0.3566, 0.10020, -1.9200 0.3172, 0.09790, -1.9043 0.2778, 0.09440, -1.9088 0.2393, 0.08960, -1.8764 0.2056, 0.08360, -1.8502 0.1633, 0.07610, -1.8494 0.1261, 0.06710, -1.8213 0.0900, 0.05640, -1.8072 0.0571, 0.04390, -1.7749 0.0283, 0.02940, -1.7669 0.0142, 0.01970, -1.7488 0.0081, 0.01410, -1.7287 0.0026, 0.00780, -1.7362 0.0000, 0.00000, -1.7469 0.0037, -0.00840, -1.9103 0.0112, -0.01420, -1.4518 0.0191, -0.01930, -0.9144 0.0397, -0.03030, -0.2036 0.0706, -0.04420, 0.2739 0.1037, -0.05710, 0.5448 0.1384, -0.06890, 0.6993 0.1741, -0.07950, 0.8221 0.2102, -0.08660, 0.9144 0.2472, -0.09640, 0.9629 0.2844, -0.10270, 0.9934 0.3225, -0.10690, 0.9773 0.3608, -0.10890, 0.9632 0.3991, -0.10830, 0.9052 0.4373, -0.10510, 0.8682 0.4757, -0.09890, 0.8022 0.5137, -0.09067, 0.7623 0.5611, -0.07859, 0.6769 16 Flap element taps 1.0000, 0.00130, -1.7875 0.9365, 0.01390, -1.8590 0.8333, 0.03280, -1.8981 0.7436, 0.04930, -1.8866 0.7049, 0.05667, -1.8857 0.6662, 0.06411, -1.9029 0.6274, 0.07172, -1.9578 0.6009, 0.07523, -2.0250 0.6069, 0.02889, -0.8350 0.6079, -0.01747, -1.0180 0.6167, -0.06381, 1.0028 0.6558, -0.05300, 0.7346 0.7045, -0.04117, 0.6429 0.7429, -0.03210, 0.5704 0.8333, -0.01400, 0.3922 0.9311, -0.00120, 0.0223 --------- Run Conditions: vel=105.9 ft/s Re=1.000x10^6 AOA=79.96 Flap deflection=0.00 Totals: Cl=0.4852 Cdp=2.3273 Cm(c/4)=-0.5867 Cs=0.0720 Ch=0.1499 Main component: Cl=0.3158 Cdp=1.4481 Cm=-0.4882 Flap component: Cl=0.1695 Cdp=0.8793 Cm=-0.6925 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.0153 0.5905, -0.01667, -0.9893 0.5709, 0.03110, -0.7890 0.5889, 0.07933, -2.0458 0.5500, 0.08689, -2.0088 0.5110, 0.09367, -1.9706 0.4731, 0.09830, -1.9618 0.4349, 0.10070, -1.9441 0.3960, 0.10120, -1.9294 0.3566, 0.10020, -1.9728 0.3172, 0.09790, -1.9619 0.2778, 0.09440, -1.9699 0.2393, 0.08960, -1.9485 0.2056, 0.08360, -1.9192 0.1633, 0.07610, -1.9323 0.1261, 0.06710, -1.8897 0.0900, 0.05640, -1.8822 0.0571, 0.04390, -1.8336 0.0283, 0.02940, -1.8181 0.0142, 0.01970, -1.8049 0.0081, 0.01410, -1.7747 0.0026, 0.00780, -1.7900 0.0000, 0.00000, -1.8029 0.0037, -0.00840, -1.8384 0.0112, -0.01420, -1.7418 0.0191, -0.01930, -1.2827 0.0397, -0.03030, -0.5856 0.0706, -0.04420, -0.0685 0.1037, -0.05710, 0.2451 0.1384, -0.06890, 0.4357 0.1741, -0.07950, 0.6069 0.2102, -0.08660, 0.7569 0.2472, -0.09640, 0.8461 0.2844, -0.10270, 0.9312 0.3225, -0.10690, 0.9526 0.3608, -0.10890, 0.9926 0.3991, -0.10830, 0.9728 0.4373, -0.10510, 0.9790 0.4757, -0.09890, 0.9440 0.5137, -0.09067, 0.9157 0.5611, -0.07859, 0.8483 16 Flap element taps 1.0000, 0.00130, -1.8087 0.9365, 0.01390, -1.8518 0.8333, 0.03280, -1.9017 0.7436, 0.04930, -1.9138 0.7049, 0.05667, -1.9380 0.6662, 0.06411, -1.9604 0.6274, 0.07172, -2.0404 0.6009, 0.07523, -2.1059 0.6069, 0.02889, -0.8743 0.6079, -0.01747, -1.0304 0.6167, -0.06381, 0.9932 0.6558, -0.05300, 0.8632 0.7045, -0.04117, 0.7810 0.7429, -0.03210, 0.7271 0.8333, -0.01400, 0.5492 0.9311, -0.00120, 0.1720 --------- Run Conditions: vel=105.6 ft/s Re=0.996x10^6 AOA=89.99 Flap deflection=0.00 Totals: Cl=0.1266 Cdp=2.3281 Cm(c/4)=-0.6169 Cs=0.1262 Ch=0.1473 Main component: Cl=0.0966 Cdp=1.3918 Cm=-0.4730 Flap component: Cl=0.0299 Cdp=0.9363 Cm=-0.7259 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.3855 0.5905, -0.01667, -1.0447 0.5709, 0.03110, -0.8688 0.5889, 0.07933, -1.9572 0.5500, 0.08689, -1.9679 0.5110, 0.09367, -1.9121 0.4731, 0.09830, -1.9019 0.4349, 0.10070, -1.9032 0.3960, 0.10120, -1.8680 0.3566, 0.10020, -1.9319 0.3172, 0.09790, -1.9333 0.2778, 0.09440, -1.9513 0.2393, 0.08960, -1.9463 0.2056, 0.08360, -1.9099 0.1633, 0.07610, -1.9539 0.1261, 0.06710, -1.9174 0.0900, 0.05640, -1.9055 0.0571, 0.04390, -1.8519 0.0283, 0.02940, -1.8184 0.0142, 0.01970, -1.8003 0.0081, 0.01410, -1.7555 0.0026, 0.00780, -1.7706 0.0000, 0.00000, -1.7835 0.0037, -0.00840, -1.7887 0.0112, -0.01420, -1.8675 0.0191, -0.01930, -1.5382 0.0397, -0.03030, -0.9225 0.0706, -0.04420, -0.4175 0.1037, -0.05710, -0.0947 0.1384, -0.06890, 0.1084 0.1741, -0.07950, 0.3101 0.2102, -0.08660, 0.5043 0.2472, -0.09640, 0.6201 0.2844, -0.10270, 0.7521 0.3225, -0.10690, 0.8073 0.3608, -0.10890, 0.9021 0.3991, -0.10830, 0.9259 0.4373, -0.10510, 0.9811 0.4757, -0.09890, 0.9863 0.5137, -0.09067, 0.9821 0.5611, -0.07859, 0.9482 16 Flap element taps 1.0000, 0.00130, -1.7887 0.9365, 0.01390, -1.8416 0.8333, 0.03280, -1.8876 0.7436, 0.04930, -1.9076 0.7049, 0.05667, -1.9480 0.6662, 0.06411, -1.9737 0.6274, 0.07172, -2.0745 0.6009, 0.07523, -2.1713 0.6069, 0.02889, -0.9601 0.6079, -0.01747, -1.0830 0.6167, -0.06381, 0.9367 0.6558, -0.05300, 0.9450 0.7045, -0.04117, 0.8808 0.7429, -0.03210, 0.8520 0.8333, -0.01400, 0.6912 0.9311, -0.00120, 0.3328 --------- Run Conditions: vel=110.0 ft/s Re=1.039x10^6 AOA=119.96 Flap deflection=0.00 Totals: Cl=-0.7589 Cdp=1.7725 Cm(c/4)=-0.6274 Cs=0.2277 Ch=0.1118 Main component: Cl=-0.3425 Cdp=0.9116 Cm=-0.3601 Flap component: Cl=-0.4165 Cdp=0.8609 Cm=-0.7460 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.9727 0.5905, -0.01667, -1.0947 0.5709, 0.03110, -1.0214 0.5889, 0.07933, -1.7345 0.5500, 0.08689, -1.8026 0.5110, 0.09367, -1.8549 0.4731, 0.09830, -1.8311 0.4349, 0.10070, -1.8067 0.3960, 0.10120, -1.7394 0.3566, 0.10020, -1.7934 0.3172, 0.09790, -1.7771 0.2778, 0.09440, -1.7841 0.2393, 0.08960, -1.7847 0.2056, 0.08360, -1.7437 0.1633, 0.07610, -1.8077 0.1261, 0.06710, -1.7641 0.0900, 0.05640, -1.7826 0.0571, 0.04390, -1.7497 0.0283, 0.02940, -1.6997 0.0142, 0.01970, -1.6618 0.0081, 0.01410, -1.6116 0.0026, 0.00780, -1.6347 0.0000, 0.00000, -1.6402 0.0037, -0.00840, -1.6274 0.0112, -0.01420, -1.6537 0.0191, -0.01930, -1.7095 0.0397, -0.03030, -1.4996 0.0706, -0.04420, -1.1925 0.1037, -0.05710, -0.9680 0.1384, -0.06890, -0.8187 0.1741, -0.07950, -0.6350 0.2102, -0.08660, -0.4238 0.2472, -0.09640, -0.3036 0.2844, -0.10270, -0.1152 0.3225, -0.10690, -0.0091 0.3608, -0.10890, 0.1769 0.3991, -0.10830, 0.3012 0.4373, -0.10510, 0.4926 0.4757, -0.09890, 0.6335 0.5137, -0.09067, 0.7733 0.5611, -0.07859, 0.8762 16 Flap element taps 1.0000, 0.00130, -1.6008 0.9365, 0.01390, -1.6615 0.8333, 0.03280, -1.6933 0.7436, 0.04930, -1.7622 0.7049, 0.05667, -1.8139 0.6662, 0.06411, -1.8527 0.6274, 0.07172, -1.9796 0.6009, 0.07523, -2.1962 0.6069, 0.02889, -1.0952 0.6079, -0.01747, -1.1662 0.6167, -0.06381, 0.6186 0.6558, -0.05300, 0.9417 0.7045, -0.04117, 0.9705 0.7429, -0.03210, 1.0107 0.8333, -0.01400, 0.9790 0.9311, -0.00120, 0.8161 --------- Run Conditions: vel=106.3 ft/s Re=1.003x10^6 AOA=150.01 Flap deflection=0.00 Totals: Cl=-0.6347 Cdp=0.5710 Cm(c/4)=-0.3882 Cs=0.1773 Ch=0.0191 Main component: Cl=-0.1283 Cdp=0.2099 Cm=-0.1041 Flap component: Cl=-0.5064 Cdp=0.3611 Cm=-0.4928 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, 0.6535 0.5905, -0.01667, -0.7324 0.5709, 0.03110, -0.7067 0.5889, 0.07933, -1.0068 0.5500, 0.08689, -1.0057 0.5110, 0.09367, -1.0334 0.4731, 0.09830, -1.0337 0.4349, 0.10070, -1.0374 0.3960, 0.10120, -1.0240 0.3566, 0.10020, -1.0370 0.3172, 0.09790, -1.0383 0.2778, 0.09440, -1.0376 0.2393, 0.08960, -1.0318 0.2056, 0.08360, -1.0088 0.1633, 0.07610, -1.0137 0.1261, 0.06710, -0.9973 0.0900, 0.05640, -0.9960 0.0571, 0.04390, -0.9973 0.0283, 0.02940, -1.0017 0.0142, 0.01970, -1.0007 0.0081, 0.01410, -0.9834 0.0026, 0.00780, -0.9811 0.0000, 0.00000, -1.0020 0.0037, -0.00840, -0.9897 0.0112, -0.01420, -0.9778 0.0191, -0.01930, -0.9821 0.0397, -0.03030, -1.0019 0.0706, -0.04420, -1.0627 0.1037, -0.05710, -1.0853 0.1384, -0.06890, -1.0918 0.1741, -0.07950, -1.0652 0.2102, -0.08660, -1.0176 0.2472, -0.09640, -0.9968 0.2844, -0.10270, -0.9197 0.3225, -0.10690, -0.8444 0.3608, -0.10890, -0.7448 0.3991, -0.10830, -0.5986 0.4373, -0.10510, -0.3980 0.4757, -0.09890, -0.1943 0.5137, -0.09067, 0.0936 0.5611, -0.07859, 0.3041 16 Flap element taps 1.0000, 0.00130, -0.9747 0.9365, 0.01390, -0.9883 0.8333, 0.03280, -0.9940 0.7436, 0.04930, -1.0222 0.7049, 0.05667, -1.0427 0.6662, 0.06411, -1.0377 0.6274, 0.07172, -1.0473 0.6009, 0.07523, -1.0916 0.6069, 0.02889, -0.7368 0.6079, -0.01747, -0.7765 0.6167, -0.06381, 0.1243 0.6558, -0.05300, 0.5117 0.7045, -0.04117, 0.6528 0.7429, -0.03210, 0.7021 0.8333, -0.01400, 0.8241 0.9311, -0.00120, 0.9794 --------- Run Conditions: vel=107.9 ft/s Re=1.019x10^6 AOA=180.00 Flap deflection=0.00 Totals: Cl=-0.0130 Cdp=-0.0077 Cm(c/4)=-0.0301 Cs=-0.0077 Ch=0.0008 Main component: Cl=0.0470 Cdp=-0.0333 Cm=0.0148 Flap component: Cl=-0.0600 Cdp=0.0256 Cm=-0.0481 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.4993 0.5905, -0.01667, -0.1018 0.5709, 0.03110, -0.0822 0.5889, 0.07933, -0.6886 0.5500, 0.08689, -0.4648 0.5110, 0.09367, -0.6075 0.4731, 0.09830, -0.6611 0.4349, 0.10070, -0.6707 0.3960, 0.10120, -0.6291 0.3566, 0.10020, -0.6042 0.3172, 0.09790, -0.5582 0.2778, 0.09440, -0.5324 0.2393, 0.08960, -0.4824 0.2056, 0.08360, -0.4125 0.1633, 0.07610, -0.3299 0.1261, 0.06710, -0.2021 0.0900, 0.05640, -0.0706 0.0571, 0.04390, 0.0072 0.0283, 0.02940, 0.0204 0.0142, 0.01970, 0.0139 0.0081, 0.01410, 0.0196 0.0026, 0.00780, 0.0163 0.0000, 0.00000, 0.0071 0.0037, -0.00840, 0.0079 0.0112, -0.01420, 0.0167 0.0191, -0.01930, 0.0171 0.0397, -0.03030, 0.0155 0.0706, -0.04420, -0.0147 0.1037, -0.05710, -0.0884 0.1384, -0.06890, -0.2402 0.1741, -0.07950, -0.3899 0.2102, -0.08660, -0.5182 0.2472, -0.09640, -0.6575 0.2844, -0.10270, -0.7528 0.3225, -0.10690, -0.8341 0.3608, -0.10890, -0.8988 0.3991, -0.10830, -0.8979 0.4373, -0.10510, -0.8206 0.4757, -0.09890, -0.7049 0.5137, -0.09067, -0.4438 0.5611, -0.07859, -0.2713 16 Flap element taps 1.0000, 0.00130, 1.0110 0.9365, 0.01390, 0.1287 0.8333, 0.03280, -0.0075 0.7436, 0.04930, -0.0996 0.7049, 0.05667, -0.0840 0.6662, 0.06411, -0.1435 0.6274, 0.07172, -0.1848 0.6009, 0.07523, -0.0791 0.6069, 0.02889, -0.0816 0.6079, -0.01747, -0.1032 0.6167, -0.06381, -0.1547 0.6558, -0.05300, -0.0299 0.7045, -0.04117, 0.1070 0.7429, -0.03210, 0.1025 0.8333, -0.01400, 0.1696 0.9311, -0.00120, 0.2859 --------- Run Conditions: vel=105.3 ft/s Re=0.994x10^6 AOA=210.00 Flap deflection=0.00 Totals: Cl=0.6093 Cdp=0.5605 Cm(c/4)=0.3661 Cs=0.1807 Ch=-0.0057 Main component: Cl=0.1352 Cdp=0.2166 Cm=0.1036 Flap component: Cl=0.4741 Cdp=0.3439 Cm=0.4645 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -0.9381 0.5905, -0.01667, -0.3593 0.5709, 0.03110, -0.5014 0.5889, 0.07933, 0.9910 0.5500, 0.08689, 0.1892 0.5110, 0.09367, -0.0425 0.4731, 0.09830, -0.2050 0.4349, 0.10070, -0.3286 0.3960, 0.10120, -0.4133 0.3566, 0.10020, -0.5065 0.3172, 0.09790, -0.5867 0.2778, 0.09440, -0.7012 0.2393, 0.08960, -0.8027 0.2056, 0.08360, -0.9102 0.1633, 0.07610, -0.9965 0.1261, 0.06710, -1.0551 0.0900, 0.05640, -1.0632 0.0571, 0.04390, -0.9725 0.0283, 0.02940, -0.9676 0.0142, 0.01970, -0.9776 0.0081, 0.01410, -0.9615 0.0026, 0.00780, -0.9489 0.0000, 0.00000, -0.9752 0.0037, -0.00840, -0.9593 0.0112, -0.01420, -0.9396 0.0191, -0.01930, -0.9328 0.0397, -0.03030, -0.9190 0.0706, -0.04420, -0.9291 0.1037, -0.05710, -0.9284 0.1384, -0.06890, -0.9402 0.1741, -0.07950, -0.9566 0.2102, -0.08660, -0.9621 0.2472, -0.09640, -0.9676 0.2844, -0.10270, -0.9779 0.3225, -0.10690, -0.9683 0.3608, -0.10890, -0.9842 0.3991, -0.10830, -0.9740 0.4373, -0.10510, -0.9677 0.4757, -0.09890, -0.9747 0.5137, -0.09067, -0.9572 0.5611, -0.07859, -0.9409 16 Flap element taps 1.0000, 0.00130, -0.9238 0.9365, 0.01390, 0.9685 0.8333, 0.03280, 0.7736 0.7436, 0.04930, 0.5816 0.7049, 0.05667, 0.5223 0.6662, 0.06411, 0.4178 0.6274, 0.07172, 0.2747 0.6009, 0.07523, -0.6848 0.6069, 0.02889, -0.7673 0.6079, -0.01747, -0.2900 0.6167, -0.06381, -0.9717 0.6558, -0.05300, -0.9882 0.7045, -0.04117, -1.0050 0.7429, -0.03210, -1.0027 0.8333, -0.01400, -0.9804 0.9311, -0.00120, -0.9319 --------- Run Conditions: vel=97.8 ft/s Re=0.921x10^6 AOA=239.97 Flap deflection=0.00 Totals: Cl=0.7436 Cdp=1.7779 Cm(c/4)=0.6271 Cs=0.2459 Ch=-0.1003 Main component: Cl=0.2917 Cdp=0.9363 Cm=0.3574 Flap component: Cl=0.4520 Cdp=0.8416 Cm=0.7476 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -1.6714 0.5905, -0.01667, -0.2385 0.5709, 0.03110, 0.0439 0.5889, 0.07933, 0.9064 0.5500, 0.08689, 0.8362 0.5110, 0.09367, 0.7059 0.4731, 0.09830, 0.5996 0.4349, 0.10070, 0.4814 0.3960, 0.10120, 0.3660 0.3566, 0.10020, 0.2485 0.3172, 0.09790, 0.1143 0.2778, 0.09440, -0.0566 0.2393, 0.08960, -0.2274 0.2056, 0.08360, -0.4332 0.1633, 0.07610, -0.6491 0.1261, 0.06710, -0.8980 0.0900, 0.05640, -1.1970 0.0571, 0.04390, -1.5707 0.0283, 0.02940, -1.7360 0.0142, 0.01970, -1.6437 0.0081, 0.01410, -1.6325 0.0026, 0.00780, -1.6213 0.0000, 0.00000, -1.6559 0.0037, -0.00840, -1.6649 0.0112, -0.01420, -1.6663 0.0191, -0.01930, -1.6786 0.0397, -0.03030, -1.7233 0.0706, -0.04420, -1.7852 0.1037, -0.05710, -1.8008 0.1384, -0.06890, -1.8019 0.1741, -0.07950, -1.7957 0.2102, -0.08660, -1.7995 0.2472, -0.09640, -1.7890 0.2844, -0.10270, -1.8016 0.3225, -0.10690, -1.7852 0.3608, -0.10890, -1.8205 0.3991, -0.10830, -1.8229 0.4373, -0.10510, -1.8270 0.4757, -0.09890, -1.8224 0.5137, -0.09067, -1.7729 0.5611, -0.07859, -1.7361 16 Flap element taps 1.0000, 0.00130, -1.6150 0.9365, 0.01390, 0.7817 0.8333, 0.03280, 0.9964 0.7436, 0.04930, 0.9816 0.7049, 0.05667, 0.9561 0.6662, 0.06411, 0.9271 0.6274, 0.07172, 0.8494 0.6009, 0.07523, -0.6423 0.6069, 0.02889, -0.7154 0.6079, -0.01747, -0.1660 0.6167, -0.06381, -1.8171 0.6558, -0.05300, -1.8635 0.7045, -0.04117, -1.8552 0.7429, -0.03210, -1.8088 0.8333, -0.01400, -1.7754 0.9311, -0.00120, -1.6691 --------- Run Conditions: vel=101.6 ft/s Re=0.958x10^6 AOA=269.01 Flap deflection=0.00 Totals: Cl=-0.0602 Cdp=2.3193 Cm(c/4)=0.6212 Cs=0.1002 Ch=-0.1567 Main component: Cl=-0.0888 Cdp=1.3885 Cm=0.4805 Flap component: Cl=0.0287 Cdp=0.9309 Cm=0.7201 Surface Pressure Data 41 Main element taps 0.6083, -0.06444, -1.9435 0.5905, -0.01667, -0.1253 0.5709, 0.03110, -0.7478 0.5889, 0.07933, -0.0502 0.5500, 0.08689, 0.9952 0.5110, 0.09367, 1.0024 0.4731, 0.09830, 1.0102 0.4349, 0.10070, 0.9875 0.3960, 0.10120, 0.9417 0.3566, 0.10020, 0.9043 0.3172, 0.09790, 0.8270 0.2778, 0.09440, 0.7201 0.2393, 0.08960, 0.6047 0.2056, 0.08360, 0.4356 0.1633, 0.07610, 0.2504 0.1261, 0.06710, -0.0138 0.0900, 0.05640, -0.3613 0.0571, 0.04390, -0.9163 0.0283, 0.02940, -1.5821 0.0142, 0.01970, -1.9652 0.0081, 0.01410, -1.8713 0.0026, 0.00780, -1.7637 0.0000, 0.00000, -1.7929 0.0037, -0.00840, -1.8003 0.0112, -0.01420, -1.8051 0.0191, -0.01930, -1.8136 0.0397, -0.03030, -1.8250 0.0706, -0.04420, -1.8815 0.1037, -0.05710, -1.9035 0.1384, -0.06890, -1.9201 0.1741, -0.07950, -1.9503 0.2102, -0.08660, -1.9764 0.2472, -0.09640, -1.9885 0.2844, -0.10270, -2.0002 0.3225, -0.10690, -1.9835 0.3608, -0.10890, -2.0025 0.3991, -0.10830, -1.9907 0.4373, -0.10510, -1.9851 0.4757, -0.09890, -1.9939 0.5137, -0.09067, -1.9381 0.5611, -0.07859, -1.9942 16 Flap element taps 1.0000, 0.00130, -1.7757 0.9365, 0.01390, 0.1828 0.8333, 0.03280, 0.6710 0.7436, 0.04930, 0.8431 0.7049, 0.05667, 0.9068 0.6662, 0.06411, 0.9572 0.6274, 0.07172, 0.9916 0.6009, 0.07523, -0.1837 0.6069, 0.02889, -0.4019 0.6079, -0.01747, -0.2640 0.6167, -0.06381, -2.0627 0.6558, -0.05300, -2.1184 0.7045, -0.04117, -2.0096 0.7429, -0.03210, -1.9535 0.8333, -0.01400, -1.9013 0.9311, -0.00120, -1.8277