S809 UNVENTED AILERON, CLEAN, CHORD = 18 IN --------- Run Conditions: vel=213.0 ft/s Re=1.992x10^6 AOA=-6.02 Flap deflection=-20.00 Totals: Cl=-0.9680 Cdp=0.0925 Cm(c/4)=0.0825 Cs=0.0095 Ch=0.1423 Main component: Cl=-0.8118 Cdp=0.0204 Cm=0.1934 Flap component: Cl=-0.1562 Cdp=0.0721 Cm=0.1322 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3593 0.6175, -0.04610, -0.3420 0.5841, -0.02440, -0.3452 0.5775, 0.01750, -0.3602 0.5777, 0.04660, -0.3488 0.6274, 0.07170, 0.4637 0.5694, 0.08320, 0.2923 0.5112, 0.09370, 0.0439 0.4731, 0.09830, 0.0211 0.4349, 0.10070, -0.0028 0.3960, 0.10120, 0.0084 0.3566, 0.10020, 0.0331 0.3172, 0.09790, 0.0780 0.2778, 0.09440, 0.1145 0.2393, 0.08960, 0.1657 0.2056, 0.08360, 0.2365 0.1633, 0.07610, 0.3237 0.1261, 0.06710, 0.4427 0.0900, 0.05640, 0.5839 0.0571, 0.04390, 0.7711 0.0283, 0.02940, 0.9675 0.0142, 0.01970, 1.0059 0.0081, 0.01410, 0.8972 0.0026, 0.00780, 0.2358 0.0000, 0.00000, -1.9836 0.0037, -0.00840, -3.0003 0.0112, -0.01420, -2.4773 0.0191, -0.01930, -1.6123 0.0397, -0.03030, -1.3488 0.0706, -0.04420, -1.2259 0.1037, -0.05710, -1.2313 0.1384, -0.06890, -1.2488 0.1741, -0.07950, -1.2580 0.2102, -0.08660, -1.3021 0.2472, -0.09640, -1.3713 0.2844, -0.10270, -1.3624 0.3225, -0.10690, -1.3423 0.3608, -0.10890, -1.2725 0.3991, -0.10830, -1.1247 0.4373, -0.10510, -0.8720 0.4757, -0.09890, -0.5655 0.5137, -0.09070, -0.3615 0.5694, -0.07640, -0.3885 15 Flap element taps 1.0000, 0.00130, -0.3229 0.9365, 0.01390, -0.0379 0.8333, 0.03280, 0.1268 0.7436, 0.04930, 0.2570 0.7049, 0.05670, 0.3712 0.6662, 0.06410, 0.4915 0.6522, 0.01390, -0.3316 0.5969, -0.00020, -0.2175 0.6000, -0.03020, -0.3438 0.6324, -0.04540, -0.3691 0.6667, -0.04880, -0.3852 0.7046, -0.04110, -0.3621 0.7429, -0.03210, -0.3333 0.8333, -0.01400, -0.4149 0.9311, -0.00120, -0.3457 --------- Run Conditions: vel=214.7 ft/s Re=1.996x10^6 AOA=0.03 Flap deflection=-20.00 Totals: Cl=-0.8708 Cdp=0.0580 Cm(c/4)=0.1239 Cs=-0.0584 Ch=0.1423 Main component: Cl=-0.7116 Cdp=0.0075 Cm=0.2122 Flap component: Cl=-0.1592 Cdp=0.0504 Cm=0.1295 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4520 0.6175, -0.04610, -0.2959 0.5841, -0.02440, -0.2692 0.5775, 0.01750, -0.2690 0.5777, 0.04660, -0.2655 0.6274, 0.07170, 0.4902 0.5694, 0.08320, 0.2809 0.5112, 0.09370, -0.0594 0.4731, 0.09830, -0.0839 0.4349, 0.10070, -0.1300 0.3960, 0.10120, -0.1125 0.3566, 0.10020, -0.1132 0.3172, 0.09790, -0.0888 0.2778, 0.09440, -0.0770 0.2393, 0.08960, -0.0503 0.2056, 0.08360, -0.0022 0.1633, 0.07610, 0.0537 0.1261, 0.06710, 0.1516 0.0900, 0.05640, 0.2664 0.0571, 0.04390, 0.4484 0.0283, 0.02940, 0.7013 0.0142, 0.01970, 0.9161 0.0081, 0.01410, 1.0040 0.0026, 0.00780, 0.8835 0.0000, 0.00000, 0.1627 0.0037, -0.00840, -0.8429 0.0112, -0.01420, -0.8073 0.0191, -0.01930, -0.7278 0.0397, -0.03030, -0.6587 0.0706, -0.04420, -0.7090 0.1037, -0.05710, -0.8219 0.1384, -0.06890, -0.9306 0.1741, -0.07950, -1.0338 0.2102, -0.08660, -1.1418 0.2472, -0.09640, -1.2874 0.2844, -0.10270, -1.3619 0.3225, -0.10690, -1.4515 0.3608, -0.10890, -1.4904 0.3991, -0.10830, -1.4883 0.4373, -0.10510, -1.3919 0.4757, -0.09890, -1.3152 0.5137, -0.09070, -0.9170 0.5694, -0.07640, -0.6506 15 Flap element taps 1.0000, 0.00130, -0.2850 0.9365, 0.01390, 0.0020 0.8333, 0.03280, 0.1692 0.7436, 0.04930, 0.3102 0.7049, 0.05670, 0.4210 0.6662, 0.06410, 0.5509 0.6522, 0.01390, -0.2648 0.5969, -0.00020, -0.2912 0.6000, -0.03020, -0.3419 0.6324, -0.04540, -0.3205 0.6667, -0.04880, -0.3033 0.7046, -0.04110, -0.2990 0.7429, -0.03210, -0.3001 0.8333, -0.01400, -0.3116 0.9311, -0.00120, -0.3345 --------- Run Conditions: vel=215.3 ft/s Re=1.993x10^6 AOA=3.07 Flap deflection=-20.00 Totals: Cl=-0.5836 Cdp=0.0519 Cm(c/4)=0.1242 Cs=-0.0830 Ch=0.1311 Main component: Cl=-0.4338 Cdp=0.0125 Cm=0.1493 Flap component: Cl=-0.1499 Cdp=0.0394 Cm=0.1199 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4212 0.6175, -0.04610, -0.2838 0.5841, -0.02440, -0.2608 0.5775, 0.01750, -0.2590 0.5777, 0.04660, -0.2538 0.6274, 0.07170, 0.4513 0.5694, 0.08320, 0.2215 0.5112, 0.09370, -0.1618 0.4731, 0.09830, -0.1986 0.4349, 0.10070, -0.2473 0.3960, 0.10120, -0.2402 0.3566, 0.10020, -0.2593 0.3172, 0.09790, -0.2502 0.2778, 0.09440, -0.2577 0.2393, 0.08960, -0.2504 0.2056, 0.08360, -0.2204 0.1633, 0.07610, -0.1930 0.1261, 0.06710, -0.1188 0.0900, 0.05640, -0.0402 0.0571, 0.04390, 0.1061 0.0283, 0.02940, 0.3307 0.0142, 0.01970, 0.5866 0.0081, 0.01410, 0.7625 0.0026, 0.00780, 0.9316 0.0000, 0.00000, 0.9284 0.0037, -0.00840, 0.2902 0.0112, -0.01420, 0.0733 0.0191, -0.01930, -0.0036 0.0397, -0.03030, -0.1182 0.0706, -0.04420, -0.2706 0.1037, -0.05710, -0.4309 0.1384, -0.06890, -0.5805 0.1741, -0.07950, -0.7095 0.2102, -0.08660, -0.8352 0.2472, -0.09640, -1.0006 0.2844, -0.10270, -1.0948 0.3225, -0.10690, -1.2081 0.3608, -0.10890, -1.2684 0.3991, -0.10830, -1.2952 0.4373, -0.10510, -1.2236 0.4757, -0.09890, -1.1285 0.5137, -0.09070, -0.8139 0.5694, -0.07640, -0.5876 15 Flap element taps 1.0000, 0.00130, -0.2749 0.9365, 0.01390, -0.0133 0.8333, 0.03280, 0.1408 0.7436, 0.04930, 0.2766 0.7049, 0.05670, 0.3883 0.6662, 0.06410, 0.5173 0.6522, 0.01390, -0.2534 0.5969, -0.00020, -0.2789 0.6000, -0.03020, -0.3313 0.6324, -0.04540, -0.3082 0.6667, -0.04880, -0.2920 0.7046, -0.04110, -0.2879 0.7429, -0.03210, -0.2872 0.8333, -0.01400, -0.2979 0.9311, -0.00120, -0.3248 --------- Run Conditions: vel=215.3 ft/s Re=1.988x10^6 AOA=6.05 Flap deflection=-20.00 Totals: Cl=-0.3171 Cdp=0.0471 Cm(c/4)=0.1279 Cs=-0.0803 Ch=0.1216 Main component: Cl=-0.1763 Cdp=0.0178 Cm=0.0943 Flap component: Cl=-0.1408 Cdp=0.0294 Cm=0.1113 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3859 0.6175, -0.04610, -0.2703 0.5841, -0.02440, -0.2503 0.5775, 0.01750, -0.2503 0.5777, 0.04660, -0.2438 0.6274, 0.07170, 0.4104 0.5694, 0.08320, 0.1624 0.5112, 0.09370, -0.0851 0.4731, 0.09830, -0.3218 0.4349, 0.10070, -0.3653 0.3960, 0.10120, -0.3654 0.3566, 0.10020, -0.4020 0.3172, 0.09790, -0.4096 0.2778, 0.09440, -0.4365 0.2393, 0.08960, -0.4512 0.2056, 0.08360, -0.4430 0.1633, 0.07610, -0.4513 0.1261, 0.06710, -0.4095 0.0900, 0.05640, -0.3815 0.0571, 0.04390, -0.3021 0.0283, 0.02940, -0.1628 0.0142, 0.01970, 0.0441 0.0081, 0.01410, 0.2214 0.0026, 0.00780, 0.4851 0.0000, 0.00000, 0.9412 0.0037, -0.00840, 0.8851 0.0112, -0.01420, 0.6499 0.0191, -0.01930, 0.5153 0.0397, -0.03030, 0.3092 0.0706, -0.04420, 0.1013 0.1037, -0.05710, -0.0869 0.1384, -0.06890, -0.2647 0.1741, -0.07950, -0.4116 0.2102, -0.08660, -0.5484 0.2472, -0.09640, -0.7281 0.2844, -0.10270, -0.8376 0.3225, -0.10690, -0.9708 0.3608, -0.10890, -1.0488 0.3991, -0.10830, -1.1015 0.4373, -0.10510, -1.0572 0.4757, -0.09890, -0.9586 0.5137, -0.09070, -0.8110 0.5694, -0.07640, -0.5211 15 Flap element taps 1.0000, 0.00130, -0.2498 0.9365, 0.01390, -0.0179 0.8333, 0.03280, 0.1207 0.7436, 0.04930, 0.2494 0.7049, 0.05670, 0.3608 0.6662, 0.06410, 0.4821 0.6522, 0.01390, -0.2410 0.5969, -0.00020, -0.2643 0.6000, -0.03020, -0.3142 0.6324, -0.04540, -0.2915 0.6667, -0.04880, -0.2762 0.7046, -0.04110, -0.2723 0.7429, -0.03210, -0.2700 0.8333, -0.01400, -0.2805 0.9311, -0.00120, -0.3122 --------- Run Conditions: vel=217.1 ft/s Re=2.001x10^6 AOA=9.03 Flap deflection=-20.00 Totals: Cl=-0.0428 Cdp=0.0432 Cm(c/4)=0.1300 Cs=-0.0493 Ch=0.1151 Main component: Cl=0.0876 Cdp=0.0270 Cm=0.0361 Flap component: Cl=-0.1304 Cdp=0.0162 Cm=0.1029 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3495 0.6175, -0.04610, -0.2697 0.5841, -0.02440, -0.2495 0.5775, 0.01750, -0.2539 0.5777, 0.04660, -0.2470 0.6274, 0.07170, 0.2835 0.5694, 0.08320, 0.1102 0.5112, 0.09370, -0.1745 0.4731, 0.09830, -0.3520 0.4349, 0.10070, -0.4423 0.3960, 0.10120, -0.4491 0.3566, 0.10020, -0.5324 0.3172, 0.09790, -0.5757 0.2778, 0.09440, -0.6240 0.2393, 0.08960, -0.6636 0.2056, 0.08360, -0.6824 0.1633, 0.07610, -0.7324 0.1261, 0.06710, -0.7324 0.0900, 0.05640, -0.7711 0.0571, 0.04390, -0.7912 0.0283, 0.02940, -0.7939 0.0142, 0.01970, -0.7314 0.0081, 0.01410, -0.6489 0.0026, 0.00780, -0.3603 0.0000, 0.00000, 0.1643 0.0037, -0.00840, 1.0040 0.0112, -0.01420, 0.9566 0.0191, -0.01930, 0.8516 0.0397, -0.03030, 0.6393 0.0706, -0.04420, 0.4152 0.1037, -0.05710, 0.2172 0.1384, -0.06890, 0.0220 0.1741, -0.07950, -0.1348 0.2102, -0.08660, -0.2771 0.2472, -0.09640, -0.4660 0.2844, -0.10270, -0.5876 0.3225, -0.10690, -0.7367 0.3608, -0.10890, -0.8299 0.3991, -0.10830, -0.9055 0.4373, -0.10510, -0.8889 0.4757, -0.09890, -0.7988 0.5137, -0.09070, -0.7248 0.5694, -0.07640, -0.4443 15 Flap element taps 1.0000, 0.00130, -0.2115 0.9365, 0.01390, -0.0112 0.8333, 0.03280, 0.1119 0.7436, 0.04930, 0.2373 0.7049, 0.05670, 0.3247 0.6662, 0.06410, 0.3417 0.6522, 0.01390, -0.2449 0.5969, -0.00020, -0.2609 0.6000, -0.03020, -0.3027 0.6324, -0.04540, -0.2829 0.6667, -0.04880, -0.2611 0.7046, -0.04110, -0.2518 0.7429, -0.03210, -0.2481 0.8333, -0.01400, -0.2579 0.9311, -0.00120, -0.3010 --------- Run Conditions: vel=217.4 ft/s Re=1.995x10^6 AOA=12.04 Flap deflection=-20.00 Totals: Cl=0.2202 Cdp=0.0363 Cm(c/4)=0.1265 Cs=0.0104 Ch=0.1062 Main component: Cl=0.3234 Cdp=0.0411 Cm=-0.0137 Flap component: Cl=-0.1031 Cdp=-0.0048 Cm=0.0845 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3339 0.6175, -0.04610, -0.3112 0.5841, -0.02440, -0.2968 0.5775, 0.01750, -0.3001 0.5777, 0.04660, -0.2952 0.6274, 0.07170, 0.0261 0.5694, 0.08320, 0.0024 0.5112, 0.09370, -0.1157 0.4731, 0.09830, -0.3227 0.4349, 0.10070, -0.4783 0.3960, 0.10120, -0.5289 0.3566, 0.10020, -0.6264 0.3172, 0.09790, -0.6780 0.2778, 0.09440, -0.7561 0.2393, 0.08960, -0.8353 0.2056, 0.08360, -0.8903 0.1633, 0.07610, -0.9864 0.1261, 0.06710, -1.0255 0.0900, 0.05640, -1.1621 0.0571, 0.04390, -1.3258 0.0283, 0.02940, -1.5280 0.0142, 0.01970, -1.6864 0.0081, 0.01410, -1.7887 0.0026, 0.00780, -1.7447 0.0000, 0.00000, -1.4242 0.0037, -0.00840, 0.7398 0.0112, -0.01420, 1.0070 0.0191, -0.01930, 0.9993 0.0397, -0.03030, 0.8592 0.0706, -0.04420, 0.6584 0.1037, -0.05710, 0.4683 0.1384, -0.06890, 0.2677 0.1741, -0.07950, 0.1080 0.2102, -0.08660, -0.0337 0.2472, -0.09640, -0.2280 0.2844, -0.10270, -0.3577 0.3225, -0.10690, -0.5203 0.3608, -0.10890, -0.6262 0.3991, -0.10830, -0.7227 0.4373, -0.10510, -0.7311 0.4757, -0.09890, -0.6627 0.5137, -0.09070, -0.6071 0.5694, -0.07640, -0.3759 15 Flap element taps 1.0000, 0.00130, -0.1417 0.9365, 0.01390, 0.0318 0.8333, 0.03280, 0.1342 0.7436, 0.04930, 0.1365 0.7049, 0.05670, 0.0840 0.6662, 0.06410, 0.0332 0.6522, 0.01390, -0.2912 0.5969, -0.00020, -0.3041 0.6000, -0.03020, -0.3306 0.6324, -0.04540, -0.3128 0.6667, -0.04880, -0.2541 0.7046, -0.04110, -0.2196 0.7429, -0.03210, -0.2152 0.8333, -0.01400, -0.2232 0.9311, -0.00120, -0.2635 --------- Run Conditions: vel=219.1 ft/s Re=1.993x10^6 AOA=15.02 Flap deflection=-20.00 Totals: Cl=0.4771 Cdp=0.0380 Cm(c/4)=0.1130 Cs=0.0869 Ch=0.0742 Main component: Cl=0.5355 Cdp=0.0610 Cm=-0.0569 Flap component: Cl=-0.0584 Cdp=-0.0230 Cm=0.0522 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3281 0.6175, -0.04610, -0.3855 0.5841, -0.02440, -0.3766 0.5775, 0.01750, -0.3777 0.5777, 0.04660, -0.3752 0.6274, 0.07170, -0.1446 0.5694, 0.08320, -0.1479 0.5112, 0.09370, -0.1593 0.4731, 0.09830, -0.2383 0.4349, 0.10070, -0.4161 0.3960, 0.10120, -0.5558 0.3566, 0.10020, -0.6744 0.3172, 0.09790, -0.7696 0.2778, 0.09440, -0.8798 0.2393, 0.08960, -0.9979 0.2056, 0.08360, -1.1150 0.1633, 0.07610, -1.2379 0.1261, 0.06710, -1.3591 0.0900, 0.05640, -1.5565 0.0571, 0.04390, -1.8446 0.0283, 0.02940, -2.2722 0.0142, 0.01970, -2.7106 0.0081, 0.01410, -3.2392 0.0026, 0.00780, -3.2089 0.0000, 0.00000, -3.6607 0.0037, -0.00840, 0.1089 0.0112, -0.01420, 0.8596 0.0191, -0.01930, 0.9966 0.0397, -0.03030, 0.9799 0.0706, -0.04420, 0.8287 0.1037, -0.05710, 0.6594 0.1384, -0.06890, 0.4890 0.1741, -0.07950, 0.3302 0.2102, -0.08660, 0.1692 0.2472, -0.09640, -0.0120 0.2844, -0.10270, -0.1586 0.3225, -0.10690, -0.3116 0.3608, -0.10890, -0.4411 0.3991, -0.10830, -0.5433 0.4373, -0.10510, -0.5894 0.4757, -0.09890, -0.5478 0.5137, -0.09070, -0.5221 0.5694, -0.07640, -0.3950 15 Flap element taps 1.0000, 0.00130, -0.0364 0.9365, 0.01390, 0.0919 0.8333, 0.03280, 0.0651 0.7436, 0.04930, -0.0803 0.7049, 0.05670, -0.1321 0.6662, 0.06410, -0.1484 0.6522, 0.01390, -0.3722 0.5969, -0.00020, -0.3800 0.6000, -0.03020, -0.4015 0.6324, -0.04540, -0.3886 0.6667, -0.04880, -0.3020 0.7046, -0.04110, -0.1874 0.7429, -0.03210, -0.1803 0.8333, -0.01400, -0.1813 0.9311, -0.00120, -0.1486 --------- Run Conditions: vel=221.0 ft/s Re=2.007x10^6 AOA=17.99 Flap deflection=-20.00 Totals: Cl=0.5903 Cdp=0.0527 Cm(c/4)=0.0890 Cs=0.1322 Ch=-0.0036 Main component: Cl=0.5958 Cdp=0.1032 Cm=-0.0657 Flap component: Cl=-0.0055 Cdp=-0.0505 Cm=0.0103 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4930 0.6175, -0.04610, -0.6581 0.5841, -0.02440, -0.6427 0.5775, 0.01750, -0.6448 0.5777, 0.04660, -0.6409 0.6274, 0.07170, -0.2839 0.5694, 0.08320, -0.2807 0.5112, 0.09370, -0.2709 0.4731, 0.09830, -0.2818 0.4349, 0.10070, -0.3242 0.3960, 0.10120, -0.4054 0.3566, 0.10020, -0.5284 0.3172, 0.09790, -0.6581 0.2778, 0.09440, -0.8068 0.2393, 0.08960, -0.9634 0.2056, 0.08360, -1.1225 0.1633, 0.07610, -1.2951 0.1261, 0.06710, -1.4715 0.0900, 0.05640, -1.7419 0.0571, 0.04390, -2.1416 0.0283, 0.02940, -2.7652 0.0142, 0.01970, -3.4134 0.0081, 0.01410, -4.1730 0.0026, 0.00780, -4.3692 0.0000, 0.00000, -5.4969 0.0037, -0.00840, -0.5027 0.0112, -0.01420, 0.6503 0.0191, -0.01930, 0.9212 0.0397, -0.03030, 1.0107 0.0706, -0.04420, 0.9126 0.1037, -0.05710, 0.7653 0.1384, -0.06890, 0.6007 0.1741, -0.07950, 0.4450 0.2102, -0.08660, 0.2845 0.2472, -0.09640, 0.0985 0.2844, -0.10270, -0.0568 0.3225, -0.10690, -0.2244 0.3608, -0.10890, -0.3695 0.3991, -0.10830, -0.4955 0.4373, -0.10510, -0.5672 0.4757, -0.09890, -0.5547 0.5137, -0.09070, -0.5632 0.5694, -0.07640, -0.4727 15 Flap element taps 1.0000, 0.00130, 0.1155 0.9365, 0.01390, 0.0629 0.8333, 0.03280, -0.1120 0.7436, 0.04930, -0.2449 0.7049, 0.05670, -0.2771 0.6662, 0.06410, -0.2887 0.6522, 0.01390, -0.6376 0.5969, -0.00020, -0.6536 0.6000, -0.03020, -0.6889 0.6324, -0.04540, -0.6809 0.6667, -0.04880, -0.7944 0.7046, -0.04110, -0.4187 0.7429, -0.03210, -0.2239 0.8333, -0.01400, -0.0029 0.9311, -0.00120, 0.1372 --------- Run Conditions: vel=220.7 ft/s Re=1.998x10^6 AOA=19.98 Flap deflection=-20.00 Totals: Cl=0.5139 Cdp=0.0991 Cm(c/4)=0.0613 Cs=0.0825 Ch=-0.0484 Main component: Cl=0.4883 Cdp=0.1439 Cm=-0.0515 Flap component: Cl=0.0256 Cdp=-0.0448 Cm=-0.0164 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6133 0.6175, -0.04610, -0.8066 0.5841, -0.02440, -0.7883 0.5775, 0.01750, -0.7910 0.5777, 0.04660, -0.7865 0.6274, 0.07170, -0.4392 0.5694, 0.08320, -0.4542 0.5112, 0.09370, -0.4386 0.4731, 0.09830, -0.4237 0.4349, 0.10070, -0.4099 0.3960, 0.10120, -0.3927 0.3566, 0.10020, -0.4057 0.3172, 0.09790, -0.4253 0.2778, 0.09440, -0.4846 0.2393, 0.08960, -0.5907 0.2056, 0.08360, -0.7516 0.1633, 0.07610, -0.9633 0.1261, 0.06710, -1.1789 0.0900, 0.05640, -1.4765 0.0571, 0.04390, -1.8988 0.0283, 0.02940, -2.5442 0.0142, 0.01970, -3.2096 0.0081, 0.01410, -3.9585 0.0026, 0.00780, -4.2197 0.0000, 0.00000, -5.4020 0.0037, -0.00840, -0.5139 0.0112, -0.01420, 0.6381 0.0191, -0.01930, 0.9148 0.0397, -0.03030, 1.0129 0.0706, -0.04420, 0.9219 0.1037, -0.05710, 0.7780 0.1384, -0.06890, 0.6122 0.1741, -0.07950, 0.4549 0.2102, -0.08660, 0.2929 0.2472, -0.09640, 0.1006 0.2844, -0.10270, -0.0610 0.3225, -0.10690, -0.2398 0.3608, -0.10890, -0.3955 0.3991, -0.10830, -0.5358 0.4373, -0.10510, -0.6196 0.4757, -0.09890, -0.6173 0.5137, -0.09070, -0.6362 0.5694, -0.07640, -0.5581 15 Flap element taps 1.0000, 0.00130, -0.1828 0.9365, 0.01390, -0.2767 0.8333, 0.03280, -0.3701 0.7436, 0.04930, -0.4252 0.7049, 0.05670, -0.4389 0.6662, 0.06410, -0.4444 0.6522, 0.01390, -0.7815 0.5969, -0.00020, -0.8015 0.6000, -0.03020, -0.8422 0.6324, -0.04540, -0.8442 0.6667, -0.04880, -1.0067 0.7046, -0.04110, -0.5914 0.7429, -0.03210, -0.3572 0.8333, -0.01400, -0.1139 0.9311, -0.00120, -0.0120 --------- Run Conditions: vel=219.0 ft/s Re=1.979x10^6 AOA=23.97 Flap deflection=-20.00 Totals: Cl=0.3059 Cdp=0.2671 Cm(c/4)=-0.0065 Cs=-0.1198 Ch=-0.0937 Main component: Cl=0.2387 Cdp=0.3035 Cm=-0.0545 Flap component: Cl=0.0672 Cdp=-0.0364 Cm=-0.0490 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.7793 0.6175, -0.04610, -1.0235 0.5841, -0.02440, -1.0024 0.5775, 0.01750, -1.0050 0.5777, 0.04660, -1.0005 0.6274, 0.07170, -0.7113 0.5694, 0.08320, -0.7223 0.5112, 0.09370, -0.7099 0.4731, 0.09830, -0.6909 0.4349, 0.10070, -0.6761 0.3960, 0.10120, -0.6493 0.3566, 0.10020, -0.6444 0.3172, 0.09790, -0.6293 0.2778, 0.09440, -0.6153 0.2393, 0.08960, -0.5998 0.2056, 0.08360, -0.5825 0.1633, 0.07610, -0.5867 0.1261, 0.06710, -0.5687 0.0900, 0.05640, -0.5611 0.0571, 0.04390, -0.5536 0.0283, 0.02940, -0.5581 0.0142, 0.01970, -0.5661 0.0081, 0.01410, -0.5676 0.0026, 0.00780, -0.5927 0.0000, 0.00000, -0.9113 0.0037, -0.00840, 0.4300 0.0112, -0.01420, 0.8911 0.0191, -0.01930, 0.9925 0.0397, -0.03030, 0.9910 0.0706, -0.04420, 0.8796 0.1037, -0.05710, 0.7376 0.1384, -0.06890, 0.5729 0.1741, -0.07950, 0.4173 0.2102, -0.08660, 0.2564 0.2472, -0.09640, 0.0584 0.2844, -0.10270, -0.1092 0.3225, -0.10690, -0.2995 0.3608, -0.10890, -0.4666 0.3991, -0.10830, -0.6233 0.4373, -0.10510, -0.7202 0.4757, -0.09890, -0.7279 0.5137, -0.09070, -0.7582 0.5694, -0.07640, -0.6918 15 Flap element taps 1.0000, 0.00130, -0.5679 0.9365, 0.01390, -0.6207 0.8333, 0.03280, -0.6975 0.7436, 0.04930, -0.7191 0.7049, 0.05670, -0.7207 0.6662, 0.06410, -0.7181 0.6522, 0.01390, -0.9946 0.5969, -0.00020, -1.0198 0.6000, -0.03020, -1.0572 0.6324, -0.04540, -1.0625 0.6667, -0.04880, -1.2625 0.7046, -0.04110, -0.8001 0.7429, -0.03210, -0.5252 0.8333, -0.01400, -0.2684 0.9311, -0.00120, -0.2125 --------- Run Conditions: vel=223.4 ft/s Re=2.012x10^6 AOA=27.01 Flap deflection=-20.00 Totals: Cl=0.2301 Cdp=0.2758 Cm(c/4)=0.0256 Cs=-0.1412 Ch=-0.0555 Main component: Cl=0.2070 Cdp=0.3172 Cm=-0.0440 Flap component: Cl=0.0232 Cdp=-0.0414 Cm=-0.0129 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8573 0.6175, -0.04610, -1.1170 0.5841, -0.02440, -1.0934 0.5775, 0.01750, -1.0977 0.5777, 0.04660, -1.0930 0.6274, 0.07170, -0.6238 0.5694, 0.08320, -0.6428 0.5112, 0.09370, -0.6416 0.4731, 0.09830, -0.6411 0.4349, 0.10070, -0.6349 0.3960, 0.10120, -0.6164 0.3566, 0.10020, -0.6232 0.3172, 0.09790, -0.6186 0.2778, 0.09440, -0.6187 0.2393, 0.08960, -0.6116 0.2056, 0.08360, -0.6027 0.1633, 0.07610, -0.6179 0.1261, 0.06710, -0.6093 0.0900, 0.05640, -0.6121 0.0571, 0.04390, -0.6092 0.0283, 0.02940, -0.6162 0.0142, 0.01970, -0.6289 0.0081, 0.01410, -0.6300 0.0026, 0.00780, -0.6287 0.0000, 0.00000, -0.8005 0.0037, -0.00840, 0.4661 0.0112, -0.01420, 0.8994 0.0191, -0.01930, 0.9956 0.0397, -0.03030, 0.9938 0.0706, -0.04420, 0.8852 0.1037, -0.05710, 0.7463 0.1384, -0.06890, 0.5818 0.1741, -0.07950, 0.4267 0.2102, -0.08660, 0.2662 0.2472, -0.09640, 0.0647 0.2844, -0.10270, -0.1066 0.3225, -0.10690, -0.3050 0.3608, -0.10890, -0.4799 0.3991, -0.10830, -0.6477 0.4373, -0.10510, -0.7550 0.4757, -0.09890, -0.7722 0.5137, -0.09070, -0.8109 0.5694, -0.07640, -0.7558 15 Flap element taps 1.0000, 0.00130, -0.5979 0.9365, 0.01390, -0.6362 0.8333, 0.03280, -0.6576 0.7436, 0.04930, -0.6479 0.7049, 0.05670, -0.6375 0.6662, 0.06410, -0.6244 0.6522, 0.01390, -1.0864 0.5969, -0.00020, -1.1109 0.6000, -0.03020, -1.1626 0.6324, -0.04540, -1.1651 0.6667, -0.04880, -1.4051 0.7046, -0.04110, -0.9196 0.7429, -0.03210, -0.6380 0.8333, -0.01400, -0.3678 0.9311, -0.00120, -0.3039