S809 UNVENTED AILERON, LEGR, CHORD = 18 IN --------- Run Conditions: vel=205.0 ft/s Re=1.993x10^6 AOA=-6.00 Flap deflection=-10.00 Totals: Cl=-0.7486 Cdp=0.0682 Cm(c/4)=0.0530 Cs=0.0105 Ch=0.1125 Main component: Cl=-0.6258 Cdp=0.0410 Cm=0.1405 Flap component: Cl=-0.1228 Cdp=0.0272 Cm=0.1004 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3562 0.6175, -0.04610, -0.3416 0.5841, -0.02440, -0.3077 0.5775, 0.01750, -0.3070 0.5777, 0.04660, -0.3060 0.6274, 0.07170, 0.2229 0.5694, 0.08320, 0.0482 0.5112, 0.09370, -0.1607 0.4731, 0.09830, -0.2251 0.4349, 0.10070, -0.2232 0.3960, 0.10120, -0.1730 0.3566, 0.10020, -0.1249 0.3172, 0.09790, -0.0653 0.2778, 0.09440, -0.0179 0.2393, 0.08960, 0.0339 0.2056, 0.08360, 0.1061 0.1633, 0.07610, 0.2017 0.1261, 0.06710, 0.3290 0.0900, 0.05640, 0.4046 0.0571, 0.04390, 0.6760 0.0283, 0.02940, 0.9097 0.0142, 0.01970, 1.0140 0.0081, 0.01410, 0.9754 0.0026, 0.00780, 0.4833 0.0000, 0.00000, -0.1072 0.0037, -0.00840, -2.1007 0.0112, -0.01420, -1.6028 0.0191, -0.01930, -1.4682 0.0397, -0.03030, -1.1244 0.0706, -0.04420, -1.0664 0.1037, -0.05710, -0.9979 0.1384, -0.06890, -1.0690 0.1741, -0.07950, -1.0890 0.2102, -0.08660, -1.1403 0.2472, -0.09640, -1.2060 0.2844, -0.10270, -1.2077 0.3225, -0.10690, -1.1864 0.3608, -0.10890, -1.1282 0.3991, -0.10830, -0.9953 0.4373, -0.10510, -0.7685 0.4757, -0.09890, -0.4956 0.5137, -0.09070, -0.3816 0.5694, -0.07640, -0.3551 14 Flap element taps 1.0000, 0.00130, -0.3372 0.9365, 0.01390, -0.1062 0.8333, 0.03280, 0.0197 0.7436, 0.04930, 0.1121 0.7049, 0.05670, 0.1890 0.6662, 0.06410, 0.0881 0.6522, 0.01390, -0.3020 0.5969, -0.00020, -0.3221 0.6000, -0.03020, -0.3558 0.6324, -0.04540, -0.3431 0.6667, -0.04880, -0.3397 0.7046, -0.04110, -0.3536 0.7429, -0.03210, -0.3665 0.9311, -0.00120, -0.3782 --------- Run Conditions: vel=206.1 ft/s Re=1.995x10^6 AOA=0.01 Flap deflection=-10.00 Totals: Cl=-0.4471 Cdp=0.0182 Cm(c/4)=0.0584 Cs=-0.0183 Ch=0.0688 Main component: Cl=-0.3709 Cdp=0.0109 Cm=0.1091 Flap component: Cl=-0.0762 Cdp=0.0073 Cm=0.0612 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2540 0.6175, -0.04610, -0.1810 0.5841, -0.02440, -0.1523 0.5775, 0.01750, -0.1558 0.5777, 0.04660, -0.1537 0.6274, 0.07170, 0.1604 0.5694, 0.08320, -0.0144 0.5112, 0.09370, -0.2582 0.4731, 0.09830, -0.3567 0.4349, 0.10070, -0.3843 0.3960, 0.10120, -0.3579 0.3566, 0.10020, -0.3345 0.3172, 0.09790, -0.2988 0.2778, 0.09440, -0.2807 0.2393, 0.08960, -0.2594 0.2056, 0.08360, -0.2198 0.1633, 0.07610, -0.1541 0.1261, 0.06710, -0.0594 0.0900, 0.05640, -0.0674 0.0571, 0.04390, 0.2212 0.0283, 0.02940, 0.4892 0.0142, 0.01970, 0.7331 0.0081, 0.01410, 0.8843 0.0026, 0.00780, 0.9787 0.0000, 0.00000, -0.0721 0.0037, -0.00840, -0.0566 0.0112, -0.01420, -0.1653 0.0191, -0.01930, -0.2766 0.0397, -0.03030, -0.2914 0.0706, -0.04420, -0.4205 0.1037, -0.05710, -0.4699 0.1384, -0.06890, -0.6319 0.1741, -0.07950, -0.7257 0.2102, -0.08660, -0.8385 0.2472, -0.09640, -0.9712 0.2844, -0.10270, -1.0444 0.3225, -0.10690, -1.1039 0.3608, -0.10890, -1.1403 0.3991, -0.10830, -1.1214 0.4373, -0.10510, -1.0385 0.4757, -0.09890, -0.8486 0.5137, -0.09070, -0.6890 0.5694, -0.07640, -0.4202 14 Flap element taps 1.0000, 0.00130, -0.1382 0.9365, 0.01390, -0.0149 0.8333, 0.03280, 0.0474 0.7436, 0.04930, 0.1044 0.7049, 0.05670, 0.1594 0.6662, 0.06410, 0.0941 0.6522, 0.01390, -0.1513 0.5969, -0.00020, -0.1638 0.6000, -0.03020, -0.1932 0.6324, -0.04540, -0.1809 0.6667, -0.04880, -0.1785 0.7046, -0.04110, -0.1720 0.7429, -0.03210, -0.1721 0.9311, -0.00120, -0.1933 Wake drag found for this condition, Cdw=0.0320 --------- Run Conditions: vel=206.4 ft/s Re=1.989x10^6 AOA=3.03 Flap deflection=-10.00 Totals: Cl=-0.1947 Cdp=0.0113 Cm(c/4)=0.0594 Cs=-0.0216 Ch=0.0556 Main component: Cl=-0.1340 Cdp=0.0106 Cm=0.0592 Flap component: Cl=-0.0607 Cdp=0.0006 Cm=0.0486 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2409 0.6175, -0.04610, -0.1561 0.5841, -0.02440, -0.1340 0.5775, 0.01750, -0.1351 0.5777, 0.04660, -0.1330 0.6274, 0.07170, 0.0981 0.5694, 0.08320, -0.0676 0.5112, 0.09370, -0.3305 0.4731, 0.09830, -0.4463 0.4349, 0.10070, -0.4927 0.3960, 0.10120, -0.4822 0.3566, 0.10020, -0.4749 0.3172, 0.09790, -0.4546 0.2778, 0.09440, -0.4549 0.2393, 0.08960, -0.4545 0.2056, 0.08360, -0.4385 0.1633, 0.07610, -0.3992 0.1261, 0.06710, -0.3324 0.0900, 0.05640, -0.4072 0.0571, 0.04390, -0.1441 0.0283, 0.02940, 0.0755 0.0142, 0.01970, 0.3061 0.0081, 0.01410, 0.4987 0.0026, 0.00780, 0.6648 0.0000, 0.00000, -0.0409 0.0037, -0.00840, 0.6868 0.0112, -0.01420, 0.4389 0.0191, -0.01930, 0.2814 0.0397, -0.03030, 0.1345 0.0706, -0.04420, -0.0523 0.1037, -0.05710, -0.1523 0.1384, -0.06890, -0.3402 0.1741, -0.07950, -0.4587 0.2102, -0.08660, -0.5891 0.2472, -0.09640, -0.7376 0.2844, -0.10270, -0.8312 0.3225, -0.10690, -0.9133 0.3608, -0.10890, -0.9719 0.3991, -0.10830, -0.9793 0.4373, -0.10510, -0.9300 0.4757, -0.09890, -0.7733 0.5137, -0.09070, -0.6460 0.5694, -0.07640, -0.4016 14 Flap element taps 1.0000, 0.00130, -0.0790 0.9365, 0.01390, 0.0027 0.8333, 0.03280, 0.0396 0.7436, 0.04930, 0.0798 0.7049, 0.05670, 0.1214 0.6662, 0.06410, 0.0557 0.6522, 0.01390, -0.1315 0.5969, -0.00020, -0.1411 0.6000, -0.03020, -0.1659 0.6324, -0.04540, -0.1551 0.6667, -0.04880, -0.1545 0.7046, -0.04110, -0.1372 0.7429, -0.03210, -0.1353 0.9311, -0.00120, -0.1460 Wake drag found for this condition, Cdw=0.0273 --------- Run Conditions: vel=207.2 ft/s Re=1.990x10^6 AOA=6.03 Flap deflection=-10.00 Totals: Cl=0.0665 Cdp=0.0150 Cm(c/4)=0.0618 Cs=-0.0080 Ch=0.0461 Main component: Cl=0.1140 Cdp=0.0225 Cm=0.0063 Flap component: Cl=-0.0475 Cdp=-0.0074 Cm=0.0386 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2362 0.6175, -0.04610, -0.1616 0.5841, -0.02440, -0.1438 0.5775, 0.01750, -0.1461 0.5777, 0.04660, -0.1445 0.6274, 0.07170, 0.0251 0.5694, 0.08320, -0.1176 0.5112, 0.09370, -0.3914 0.4731, 0.09830, -0.5313 0.4349, 0.10070, -0.6000 0.3960, 0.10120, -0.6076 0.3566, 0.10020, -0.6192 0.3172, 0.09790, -0.6179 0.2778, 0.09440, -0.6406 0.2393, 0.08960, -0.6655 0.2056, 0.08360, -0.6773 0.1633, 0.07610, -0.6714 0.1261, 0.06710, -0.6424 0.0900, 0.05640, -0.7924 0.0571, 0.04390, -0.5917 0.0283, 0.02940, -0.4788 0.0142, 0.01970, -0.3288 0.0081, 0.01410, -0.2269 0.0026, 0.00780, 0.0619 0.0000, 0.00000, -0.0087 0.0037, -0.00840, 0.9961 0.0112, -0.01420, 0.8445 0.0191, -0.01930, 0.6949 0.0397, -0.03030, 0.4918 0.0706, -0.04420, 0.2762 0.1037, -0.05710, 0.1397 0.1384, -0.06890, -0.0605 0.1741, -0.07950, -0.1965 0.2102, -0.08660, -0.3396 0.2472, -0.09640, -0.4995 0.2844, -0.10270, -0.6097 0.3225, -0.10690, -0.7117 0.3608, -0.10890, -0.7905 0.3991, -0.10830, -0.8226 0.4373, -0.10510, -0.8024 0.4757, -0.09890, -0.6788 0.5137, -0.09070, -0.5794 0.5694, -0.07640, -0.3681 14 Flap element taps 1.0000, 0.00130, -0.0066 0.9365, 0.01390, 0.0332 0.8333, 0.03280, 0.0399 0.7436, 0.04930, 0.0573 0.7049, 0.05670, 0.0763 0.6662, 0.06410, -0.0027 0.6522, 0.01390, -0.1416 0.5969, -0.00020, -0.1501 0.6000, -0.03020, -0.1702 0.6324, -0.04540, -0.1607 0.6667, -0.04880, -0.1558 0.7046, -0.04110, -0.1160 0.7429, -0.03210, -0.1063 0.9311, -0.00120, -0.0938 Wake drag found for this condition, Cdw=0.0234 --------- Run Conditions: vel=207.7 ft/s Re=1.989x10^6 AOA=9.01 Flap deflection=-10.00 Totals: Cl=0.3095 Cdp=0.0268 Cm(c/4)=0.0642 Cs=0.0220 Ch=0.0354 Main component: Cl=0.3412 Cdp=0.0480 Cm=-0.0406 Flap component: Cl=-0.0317 Cdp=-0.0212 Cm=0.0273 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2583 0.6175, -0.04610, -0.2237 0.5841, -0.02440, -0.2064 0.5775, 0.01750, -0.2110 0.5777, 0.04660, -0.2100 0.6274, 0.07170, -0.0626 0.5694, 0.08320, -0.1562 0.5112, 0.09370, -0.4095 0.4731, 0.09830, -0.5770 0.4349, 0.10070, -0.6757 0.3960, 0.10120, -0.7086 0.3566, 0.10020, -0.7448 0.3172, 0.09790, -0.7656 0.2778, 0.09440, -0.8143 0.2393, 0.08960, -0.8678 0.2056, 0.08360, -0.9119 0.1633, 0.07610, -0.9475 0.1261, 0.06710, -0.9641 0.0900, 0.05640, -1.1918 0.0571, 0.04390, -1.0880 0.0283, 0.02940, -1.1271 0.0142, 0.01970, -1.1457 0.0081, 0.01410, -1.1408 0.0026, 0.00780, -0.8136 0.0000, 0.00000, 0.0265 0.0037, -0.00840, 0.9352 0.0112, -0.01420, 1.0036 0.0191, -0.01930, 0.9348 0.0397, -0.03030, 0.7522 0.0706, -0.04420, 0.5373 0.1037, -0.05710, 0.3828 0.1384, -0.06890, 0.1824 0.1741, -0.07950, 0.0353 0.2102, -0.08660, -0.1149 0.2472, -0.09640, -0.2824 0.2844, -0.10270, -0.4056 0.3225, -0.10690, -0.5255 0.3608, -0.10890, -0.6212 0.3991, -0.10830, -0.6767 0.4373, -0.10510, -0.6839 0.4757, -0.09890, -0.5924 0.5137, -0.09070, -0.5204 0.5694, -0.07640, -0.3470 14 Flap element taps 1.0000, 0.00130, 0.1095 0.9365, 0.01390, 0.0944 0.8333, 0.03280, 0.0588 0.7436, 0.04930, 0.0309 0.7049, 0.05670, 0.0117 0.6662, 0.06410, -0.0988 0.6522, 0.01390, -0.2071 0.5969, -0.00020, -0.2137 0.6000, -0.03020, -0.2308 0.6324, -0.04540, -0.2227 0.6667, -0.04880, -0.2088 0.7046, -0.04110, -0.1205 0.7429, -0.03210, -0.0875 0.9311, -0.00120, 0.0202 --------- Run Conditions: vel=210.5 ft/s Re=2.009x10^6 AOA=12.00 Flap deflection=-10.00 Totals: Cl=0.5559 Cdp=0.0492 Cm(c/4)=0.0520 Cs=0.0674 Ch=-0.0047 Main component: Cl=0.5430 Cdp=0.0809 Cm=-0.0800 Flap component: Cl=0.0129 Cdp=-0.0317 Cm=-0.0066 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2821 0.6175, -0.04610, -0.3149 0.5841, -0.02440, -0.3006 0.5775, 0.01750, -0.3037 0.5777, 0.04660, -0.3025 0.6274, 0.07170, -0.1979 0.5694, 0.08320, -0.2238 0.5112, 0.09370, -0.3517 0.4731, 0.09830, -0.5308 0.4349, 0.10070, -0.6761 0.3960, 0.10120, -0.7520 0.3566, 0.10020, -0.8249 0.3172, 0.09790, -0.8789 0.2778, 0.09440, -0.9596 0.2393, 0.08960, -1.0455 0.2056, 0.08360, -1.1278 0.1633, 0.07610, -1.2116 0.1261, 0.06710, -1.2825 0.0900, 0.05640, -1.5842 0.0571, 0.04390, -1.6172 0.0283, 0.02940, -1.8699 0.0142, 0.01970, -2.1374 0.0081, 0.01410, -2.3165 0.0026, 0.00780, -2.0363 0.0000, 0.00000, 0.0618 0.0037, -0.00840, 0.5400 0.0112, -0.01420, 0.9702 0.0191, -0.01930, 1.0119 0.0397, -0.03030, 0.9191 0.0706, -0.04420, 0.7371 0.1037, -0.05710, 0.5792 0.1384, -0.06890, 0.3884 0.1741, -0.07950, 0.2352 0.2102, -0.08660, 0.0808 0.2472, -0.09640, -0.0853 0.2844, -0.10270, -0.2136 0.3225, -0.10690, -0.3466 0.3608, -0.10890, -0.4569 0.3991, -0.10830, -0.5333 0.4373, -0.10510, -0.5649 0.4757, -0.09890, -0.5044 0.5137, -0.09070, -0.4587 0.5694, -0.07640, -0.3226 14 Flap element taps 1.0000, 0.00130, 0.1431 0.9365, 0.01390, 0.1021 0.8333, 0.03280, 0.0101 0.7436, 0.04930, -0.0975 0.7049, 0.05670, -0.1397 0.6662, 0.06410, -0.2303 0.6522, 0.01390, -0.2997 0.5969, -0.00020, -0.3069 0.6000, -0.03020, -0.3197 0.6324, -0.04540, -0.3129 0.6667, -0.04880, -0.2833 0.7046, -0.04110, -0.1602 0.7429, -0.03210, -0.0513 0.9311, -0.00120, 0.1787 --------- Run Conditions: vel=213.7 ft/s Re=2.002x10^6 AOA=15.01 Flap deflection=-10.00 Totals: Cl=0.6882 Cdp=0.0860 Cm(c/4)=0.0303 Cs=0.0952 Ch=-0.0727 Main component: Cl=0.6149 Cdp=0.1033 Cm=-0.0845 Flap component: Cl=0.0733 Cdp=-0.0173 Cm=-0.0570 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.2980 0.6175, -0.04610, -0.3739 0.5841, -0.02440, -0.3650 0.5775, 0.01750, -0.3656 0.5777, 0.04660, -0.3667 0.6274, 0.07170, -0.2974 0.5694, 0.08320, -0.2959 0.5112, 0.09370, -0.2937 0.4731, 0.09830, -0.3177 0.4349, 0.10070, -0.3957 0.3960, 0.10120, -0.5116 0.3566, 0.10020, -0.6478 0.3172, 0.09790, -0.7695 0.2778, 0.09440, -0.9019 0.2393, 0.08960, -1.0384 0.2056, 0.08360, -1.1715 0.1633, 0.07610, -1.3031 0.1261, 0.06710, -1.4426 0.0900, 0.05640, -1.7951 0.0571, 0.04390, -1.9700 0.0283, 0.02940, -2.4286 0.0142, 0.01970, -2.9301 0.0081, 0.01410, -3.3337 0.0026, 0.00780, -3.2443 0.0000, 0.00000, -0.1695 0.0037, -0.00840, 0.0184 0.0112, -0.01420, 0.8219 0.0191, -0.01930, 0.9842 0.0397, -0.03030, 0.9933 0.0706, -0.04420, 0.8550 0.1037, -0.05710, 0.7084 0.1384, -0.06890, 0.5358 0.1741, -0.07950, 0.3828 0.2102, -0.08660, 0.2228 0.2472, -0.09640, 0.0515 0.2844, -0.10270, -0.0853 0.3225, -0.10690, -0.2206 0.3608, -0.10890, -0.3426 0.3991, -0.10830, -0.4366 0.4373, -0.10510, -0.4864 0.4757, -0.09890, -0.4478 0.5137, -0.09070, -0.4173 0.5694, -0.07640, -0.3046 14 Flap element taps 1.0000, 0.00130, -0.0831 0.9365, 0.01390, -0.1746 0.8333, 0.03280, -0.2562 0.7436, 0.04930, -0.2975 0.7049, 0.05670, -0.3061 0.6662, 0.06410, -0.3327 0.6522, 0.01390, -0.3645 0.5969, -0.00020, -0.3670 0.6000, -0.03020, -0.3778 0.6324, -0.04540, -0.3728 0.6667, -0.04880, -0.3099 0.7046, -0.04110, -0.1994 0.7429, -0.03210, -0.0685 0.9311, -0.00120, 0.1262 --------- Run Conditions: vel=213.6 ft/s Re=1.995x10^6 AOA=18.01 Flap deflection=-10.00 Totals: Cl=0.5745 Cdp=0.1552 Cm(c/4)=-0.0038 Cs=0.0301 Ch=-0.1050 Main component: Cl=0.4677 Cdp=0.1629 Cm=-0.0685 Flap component: Cl=0.1068 Cdp=-0.0078 Cm=-0.0838 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.3899 0.6175, -0.04610, -0.5191 0.5841, -0.02440, -0.5118 0.5775, 0.01750, -0.5132 0.5777, 0.04660, -0.5142 0.6274, 0.07170, -0.4698 0.5694, 0.08320, -0.4766 0.5112, 0.09370, -0.4708 0.4731, 0.09830, -0.4774 0.4349, 0.10070, -0.4877 0.3960, 0.10120, -0.4956 0.3566, 0.10020, -0.5194 0.3172, 0.09790, -0.5496 0.2778, 0.09440, -0.5886 0.2393, 0.08960, -0.6449 0.2056, 0.08360, -0.7158 0.1633, 0.07610, -0.8052 0.1261, 0.06710, -0.9261 0.0900, 0.05640, -1.1664 0.0571, 0.04390, -1.4673 0.0283, 0.02940, -2.0268 0.0142, 0.01970, -2.5932 0.0081, 0.01410, -3.0358 0.0026, 0.00780, -3.0571 0.0000, 0.00000, -0.1575 0.0037, -0.00840, -0.0242 0.0112, -0.01420, 0.7954 0.0191, -0.01930, 0.9711 0.0397, -0.03030, 0.9989 0.0706, -0.04420, 0.8748 0.1037, -0.05710, 0.7337 0.1384, -0.06890, 0.5639 0.1741, -0.07950, 0.4105 0.2102, -0.08660, 0.2489 0.2472, -0.09640, 0.0721 0.2844, -0.10270, -0.0737 0.3225, -0.10690, -0.2220 0.3608, -0.10890, -0.3552 0.3991, -0.10830, -0.4677 0.4373, -0.10510, -0.5275 0.4757, -0.09890, -0.4981 0.5137, -0.09070, -0.4799 0.5694, -0.07640, -0.3748 14 Flap element taps 1.0000, 0.00130, -0.3029 0.9365, 0.01390, -0.3969 0.8333, 0.03280, -0.4662 0.7436, 0.04930, -0.4866 0.7049, 0.05670, -0.4869 0.6662, 0.06410, -0.4942 0.6522, 0.01390, -0.5119 0.5969, -0.00020, -0.5139 0.6000, -0.03020, -0.5191 0.6324, -0.04540, -0.5156 0.6667, -0.04880, -0.3606 0.7046, -0.04110, -0.2902 0.7429, -0.03210, -0.1506 0.9311, -0.00120, 0.0056 --------- Run Conditions: vel=213.6 ft/s Re=1.993x10^6 AOA=19.99 Flap deflection=-10.00 Totals: Cl=0.5222 Cdp=0.2013 Cm(c/4)=-0.0194 Cs=-0.0107 Ch=-0.1165 Main component: Cl=0.4076 Cdp=0.2014 Cm=-0.0681 Flap component: Cl=0.1146 Cdp=0.0000 Cm=-0.0912 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4460 0.6175, -0.04610, -0.5850 0.5841, -0.02440, -0.5799 0.5775, 0.01750, -0.5814 0.5777, 0.04660, -0.5824 0.6274, 0.07170, -0.5468 0.5694, 0.08320, -0.5584 0.5112, 0.09370, -0.5660 0.4731, 0.09830, -0.5651 0.4349, 0.10070, -0.5654 0.3960, 0.10120, -0.5622 0.3566, 0.10020, -0.5671 0.3172, 0.09790, -0.5701 0.2778, 0.09440, -0.5808 0.2393, 0.08960, -0.5969 0.2056, 0.08360, -0.6180 0.1633, 0.07610, -0.6625 0.1261, 0.06710, -0.7251 0.0900, 0.05640, -0.8575 0.0571, 0.04390, -1.1080 0.0283, 0.02940, -1.6155 0.0142, 0.01970, -2.1961 0.0081, 0.01410, -2.6381 0.0026, 0.00780, -2.7232 0.0000, 0.00000, -0.1460 0.0037, -0.00840, 0.0183 0.0112, -0.01420, 0.8001 0.0191, -0.01930, 0.9715 0.0397, -0.03030, 1.0005 0.0706, -0.04420, 0.8811 0.1037, -0.05710, 0.7425 0.1384, -0.06890, 0.5731 0.1741, -0.07950, 0.4187 0.2102, -0.08660, 0.2563 0.2472, -0.09640, 0.0751 0.2844, -0.10270, -0.0754 0.3225, -0.10690, -0.2308 0.3608, -0.10890, -0.3709 0.3991, -0.10830, -0.4933 0.4373, -0.10510, -0.5588 0.4757, -0.09890, -0.5367 0.5137, -0.09070, -0.5238 0.5694, -0.07640, -0.4207 14 Flap element taps 1.0000, 0.00130, -0.4307 0.9365, 0.01390, -0.5191 0.8333, 0.03280, -0.5776 0.7436, 0.04930, -0.5730 0.7049, 0.05670, -0.5592 0.6662, 0.06410, -0.5619 0.6522, 0.01390, -0.5781 0.5969, -0.00020, -0.5811 0.6000, -0.03020, -0.5861 0.6324, -0.04540, -0.5823 0.6667, -0.04880, -0.4321 0.7046, -0.04110, -0.3608 0.7429, -0.03210, -0.2161 0.9311, -0.00120, -0.0759 --------- Run Conditions: vel=213.4 ft/s Re=1.986x10^6 AOA=24.00 Flap deflection=-10.00 Totals: Cl=0.6093 Cdp=0.3165 Cm(c/4)=-0.0500 Cs=-0.0413 Ch=-0.1418 Main component: Cl=0.4676 Cdp=0.2997 Cm=-0.1073 Flap component: Cl=0.1417 Cdp=0.0168 Cm=-0.1141 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4703 0.6175, -0.04610, -0.6524 0.5841, -0.02440, -0.6498 0.5775, 0.01750, -0.6507 0.5777, 0.04660, -0.6513 0.6274, 0.07170, -0.6867 0.5694, 0.08320, -0.7148 0.5112, 0.09370, -0.7340 0.4731, 0.09830, -0.7365 0.4349, 0.10070, -0.7382 0.3960, 0.10120, -0.7390 0.3566, 0.10020, -0.7523 0.3172, 0.09790, -0.7672 0.2778, 0.09440, -0.7862 0.2393, 0.08960, -0.8192 0.2056, 0.08360, -0.8472 0.1633, 0.07610, -0.8885 0.1261, 0.06710, -0.9309 0.0900, 0.05640, -0.9732 0.0571, 0.04390, -1.0391 0.0283, 0.02940, -1.1761 0.0142, 0.01970, -1.4227 0.0081, 0.01410, -1.6418 0.0026, 0.00780, -1.7925 0.0000, 0.00000, -0.1330 0.0037, -0.00840, 0.0057 0.0112, -0.01420, 0.7602 0.0191, -0.01930, 0.9488 0.0397, -0.03030, 1.0123 0.0706, -0.04420, 0.9239 0.1037, -0.05710, 0.8020 0.1384, -0.06890, 0.6462 0.1741, -0.07950, 0.4984 0.2102, -0.08660, 0.3416 0.2472, -0.09640, 0.1616 0.2844, -0.10270, 0.0073 0.3225, -0.10690, -0.1606 0.3608, -0.10890, -0.3104 0.3991, -0.10830, -0.4442 0.4373, -0.10510, -0.5225 0.4757, -0.09890, -0.5159 0.5137, -0.09070, -0.5202 0.5694, -0.07640, -0.4214 14 Flap element taps 1.0000, 0.00130, -0.5706 0.9365, 0.01390, -0.6564 0.8333, 0.03280, -0.6954 0.7436, 0.04930, -0.7096 0.7049, 0.05670, -0.7019 0.6662, 0.06410, -0.6601 0.6522, 0.01390, -0.6454 0.5969, -0.00020, -0.6480 0.6000, -0.03020, -0.6500 0.6324, -0.04540, -0.6489 0.6667, -0.04880, -0.4075 0.7046, -0.04110, -0.3860 0.7429, -0.03210, -0.2427 0.9311, -0.00120, -0.1400 --------- Run Conditions: vel=214.4 ft/s Re=1.988x10^6 AOA=26.99 Flap deflection=-10.00 Totals: Cl=0.6382 Cdp=0.3870 Cm(c/4)=-0.0609 Cs=-0.0552 Ch=-0.1490 Main component: Cl=0.4907 Cdp=0.3584 Cm=-0.1265 Flap component: Cl=0.1475 Cdp=0.0286 Cm=-0.1205 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.4710 0.6175, -0.04610, -0.6717 0.5841, -0.02440, -0.6696 0.5775, 0.01750, -0.6694 0.5777, 0.04660, -0.6709 0.6274, 0.07170, -0.7437 0.5694, 0.08320, -0.7573 0.5112, 0.09370, -0.7647 0.4731, 0.09830, -0.8030 0.4349, 0.10070, -0.8146 0.3960, 0.10120, -0.8180 0.3566, 0.10020, -0.8402 0.3172, 0.09790, -0.8574 0.2778, 0.09440, -0.8727 0.2393, 0.08960, -0.8980 0.2056, 0.08360, -0.9195 0.1633, 0.07610, -0.9519 0.1261, 0.06710, -0.9786 0.0900, 0.05640, -0.9931 0.0571, 0.04390, -1.0334 0.0283, 0.02940, -1.0632 0.0142, 0.01970, -1.1729 0.0081, 0.01410, -1.3023 0.0026, 0.00780, -1.2595 0.0000, 0.00000, -0.1138 0.0037, -0.00840, -0.0067 0.0112, -0.01420, 0.7224 0.0191, -0.01930, 0.9228 0.0397, -0.03030, 1.0147 0.0706, -0.04420, 0.9528 0.1037, -0.05710, 0.8461 0.1384, -0.06890, 0.7019 0.1741, -0.07950, 0.5616 0.2102, -0.08660, 0.4118 0.2472, -0.09640, 0.2350 0.2844, -0.10270, 0.0801 0.3225, -0.10690, -0.0932 0.3608, -0.10890, -0.2482 0.3991, -0.10830, -0.3879 0.4373, -0.10510, -0.4751 0.4757, -0.09890, -0.4813 0.5137, -0.09070, -0.4967 0.5694, -0.07640, -0.4100 14 Flap element taps 1.0000, 0.00130, -0.6706 0.9365, 0.01390, -0.7261 0.8333, 0.03280, -0.7435 0.7436, 0.04930, -0.7454 0.7049, 0.05670, -0.7489 0.6662, 0.06410, -0.6922 0.6522, 0.01390, -0.6654 0.5969, -0.00020, -0.6679 0.6000, -0.03020, -0.6698 0.6324, -0.04540, -0.6680 0.6667, -0.04880, -0.3848 0.7046, -0.04110, -0.3967 0.7429, -0.03210, -0.2592 0.9311, -0.00120, -0.1868