S809 UNVENTED AILERON, LEGR, CHORD = 18 INCHES --------- Run Conditions: vel=99.6 ft/s Re=0.999x10^6 AOA=-5.98 Flap deflection=-90.00 Totals: Cl=-1.6504 Cdp=0.4951 Cm(c/4)=0.1566 Cs=-0.3205 Ch=0.5337 Main component: Cl=-1.6527 Cdp=-0.0394 Cm=0.4283 Flap component: Cl=0.0023 Cdp=0.5345 Cm=0.1516 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.9232 0.6175, -0.04610, -0.9041 0.5841, -0.02440, -0.8961 0.5775, 0.01750, -0.9030 0.5777, 0.04660, -0.9096 0.6274, 0.07170, 0.9179 0.5694, 0.08320, 0.8950 0.5112, 0.09370, 0.8914 0.4731, 0.09830, 0.9024 0.4349, 0.10070, 0.8752 0.3960, 0.10120, 0.8481 0.3566, 0.10020, 0.8337 0.3172, 0.09790, 0.8247 0.2778, 0.09440, 0.8104 0.2393, 0.08960, 0.8314 0.2056, 0.08360, 0.8490 0.1633, 0.07610, 0.8729 0.1261, 0.06710, 0.9302 0.0900, 0.05640, 0.9816 0.0571, 0.04390, 0.9930 0.0283, 0.02940, 0.7942 0.0142, 0.01970, 0.2164 0.0081, 0.01410, -0.4906 0.0026, 0.00780, -2.0947 0.0000, 0.00000, -8.1398 0.0037, -0.00840, -7.7286 0.0112, -0.01420, -5.2579 0.0191, -0.01930, -4.3616 0.0397, -0.03030, -3.3175 0.0706, -0.04420, -2.6251 0.1037, -0.05710, -2.2856 0.1384, -0.06890, -2.1527 0.1741, -0.07950, -2.0577 0.2102, -0.08660, -2.0181 0.2472, -0.09640, -2.0024 0.2844, -0.10270, -1.9236 0.3225, -0.10690, -1.8060 0.3608, -0.10890, -1.6499 0.3991, -0.10830, -1.4178 0.4373, -0.10510, -1.1536 0.4757, -0.09890, -1.0204 0.5137, -0.09070, -0.9593 0.5694, -0.07640, -0.9271 15 Flap element taps 1.0000, 0.00130, -0.8872 0.9365, 0.01390, 0.6482 0.8333, 0.03280, 0.9090 0.7436, 0.04930, 0.9090 0.7049, 0.05670, 0.9037 0.6662, 0.06410, 0.9160 0.6522, 0.01390, -0.8918 0.5969, -0.00020, -0.9049 0.6000, -0.03020, -0.9088 0.6324, -0.04540, -0.8953 0.6667, -0.04880, -0.8874 0.7046, -0.04110, -0.8823 0.7429, -0.03210, -0.8858 0.8333, -0.01400, -0.8831 0.9311, -0.00120, -0.8765 --------- Run Conditions: vel=99.9 ft/s Re=0.999x10^6 AOA=0.01 Flap deflection=-90.00 Totals: Cl=-1.6414 Cdp=0.4105 Cm(c/4)=0.1869 Cs=-0.4108 Ch=0.4993 Main component: Cl=-1.5923 Cdp=-0.0876 Cm=0.4561 Flap component: Cl=-0.0491 Cdp=0.4981 Cm=0.1412 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.8544 0.6175, -0.04610, -0.8048 0.5841, -0.02440, -0.7964 0.5775, 0.01750, -0.8004 0.5777, 0.04660, -0.8104 0.6274, 0.07170, 0.8841 0.5694, 0.08320, 0.8669 0.5112, 0.09370, 0.8715 0.4731, 0.09830, 0.8837 0.4349, 0.10070, 0.8612 0.3960, 0.10120, 0.8107 0.3566, 0.10020, 0.7583 0.3172, 0.09790, 0.7560 0.2778, 0.09440, 0.7336 0.2393, 0.08960, 0.7400 0.2056, 0.08360, 0.7472 0.1633, 0.07610, 0.7604 0.1261, 0.06710, 0.8227 0.0900, 0.05640, 0.8912 0.0571, 0.04390, 0.9688 0.0283, 0.02940, 0.9765 0.0142, 0.01970, 0.7507 0.0081, 0.01410, 0.3932 0.0026, 0.00780, -0.6669 0.0000, 0.00000, -4.4430 0.0037, -0.00840, -5.2589 0.0112, -0.01420, -3.5862 0.0191, -0.01930, -2.8358 0.0397, -0.03030, -2.1870 0.0706, -0.04420, -1.8960 0.1037, -0.05710, -1.7228 0.1384, -0.06890, -1.7927 0.1741, -0.07950, -1.8053 0.2102, -0.08660, -1.8734 0.2472, -0.09640, -1.9795 0.2844, -0.10270, -2.0173 0.3225, -0.10690, -2.0435 0.3608, -0.10890, -2.0557 0.3991, -0.10830, -1.9809 0.4373, -0.10510, -1.8001 0.4757, -0.09890, -1.5599 0.5137, -0.09070, -1.3104 0.5694, -0.07640, -0.9985 15 Flap element taps 1.0000, 0.00130, -0.8054 0.9365, 0.01390, 0.6241 0.8333, 0.03280, 0.8952 0.7436, 0.04930, 0.8798 0.7049, 0.05670, 0.8743 0.6662, 0.06410, 0.8860 0.6522, 0.01390, -0.7910 0.5969, -0.00020, -0.8054 0.6000, -0.03020, -0.8092 0.6324, -0.04540, -0.7992 0.6667, -0.04880, -0.7960 0.7046, -0.04110, -0.7933 0.7429, -0.03210, -0.7973 0.8333, -0.01400, -0.7970 0.9311, -0.00120, -0.7928 --------- Run Conditions: vel=100.0 ft/s Re=1.002x10^6 AOA=2.98 Flap deflection=-90.00 Totals: Cl=-1.6478 Cdp=0.4113 Cm(c/4)=0.2118 Cs=-0.4964 Ch=0.5228 Main component: Cl=-1.5694 Cdp=-0.1074 Cm=0.4700 Flap component: Cl=-0.0784 Cdp=0.5187 Cm=0.1479 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.9859 0.6175, -0.04610, -0.8921 0.5841, -0.02440, -0.8812 0.5775, 0.01750, -0.8883 0.5777, 0.04660, -0.8957 0.6274, 0.07170, 0.8849 0.5694, 0.08320, 0.8733 0.5112, 0.09370, 0.8758 0.4731, 0.09830, 0.8850 0.4349, 0.10070, 0.8579 0.3960, 0.10120, 0.8103 0.3566, 0.10020, 0.7163 0.3172, 0.09790, 0.7143 0.2778, 0.09440, 0.6897 0.2393, 0.08960, 0.6907 0.2056, 0.08360, 0.6930 0.1633, 0.07610, 0.7008 0.1261, 0.06710, 0.7618 0.0900, 0.05640, 0.8316 0.0571, 0.04390, 0.9279 0.0283, 0.02940, 0.9987 0.0142, 0.01970, 0.8883 0.0081, 0.01410, 0.6527 0.0026, 0.00780, -0.2019 0.0000, 0.00000, -3.1410 0.0037, -0.00840, -4.1939 0.0112, -0.01420, -2.9225 0.0191, -0.01930, -2.3060 0.0397, -0.03030, -1.8258 0.0706, -0.04420, -1.6519 0.1037, -0.05710, -1.5291 0.1384, -0.06890, -1.6542 0.1741, -0.07950, -1.7053 0.2102, -0.08660, -1.8046 0.2472, -0.09640, -1.9473 0.2844, -0.10270, -2.0165 0.3225, -0.10690, -2.0838 0.3608, -0.10890, -2.1353 0.3991, -0.10830, -2.1041 0.4373, -0.10510, -1.9649 0.4757, -0.09890, -1.7599 0.5137, -0.09070, -1.5389 0.5694, -0.07640, -1.1991 15 Flap element taps 1.0000, 0.00130, -0.8869 0.9365, 0.01390, 0.5972 0.8333, 0.03280, 0.8941 0.7436, 0.04930, 0.8786 0.7049, 0.05670, 0.8767 0.6662, 0.06410, 0.8854 0.6522, 0.01390, -0.8781 0.5969, -0.00020, -0.8938 0.6000, -0.03020, -0.8924 0.6324, -0.04540, -0.8809 0.6667, -0.04880, -0.8812 0.7046, -0.04110, -0.8772 0.7429, -0.03210, -0.8854 0.8333, -0.01400, -0.8814 0.9311, -0.00120, -0.8802 --------- Run Conditions: vel=99.9 ft/s Re=1.001x10^6 AOA=5.99 Flap deflection=-90.00 Totals: Cl=-1.5667 Cdp=0.4516 Cm(c/4)=0.2355 Cs=-0.6126 Ch=0.5629 Main component: Cl=-1.4539 Cdp=-0.1015 Cm=0.4545 Flap component: Cl=-0.1129 Cdp=0.5530 Cm=0.1587 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.1079 0.6175, -0.04610, -1.0207 0.5841, -0.02440, -1.0076 0.5775, 0.01750, -1.0121 0.5777, 0.04660, -1.0189 0.6274, 0.07170, 0.8604 0.5694, 0.08320, 0.8332 0.5112, 0.09370, 0.8438 0.4731, 0.09830, 0.8593 0.4349, 0.10070, 0.8391 0.3960, 0.10120, 0.7947 0.3566, 0.10020, 0.7158 0.3172, 0.09790, 0.6628 0.2778, 0.09440, 0.6321 0.2393, 0.08960, 0.6259 0.2056, 0.08360, 0.6205 0.1633, 0.07610, 0.6170 0.1261, 0.06710, 0.6707 0.0900, 0.05640, 0.7310 0.0571, 0.04390, 0.8387 0.0283, 0.02940, 0.9768 0.0142, 0.01970, 0.9854 0.0081, 0.01410, 0.8862 0.0026, 0.00780, 0.2553 0.0000, 0.00000, -1.6087 0.0037, -0.00840, -2.7712 0.0112, -0.01420, -2.0314 0.0191, -0.01930, -1.5966 0.0397, -0.03030, -1.3279 0.0706, -0.04420, -1.2863 0.1037, -0.05710, -1.2232 0.1384, -0.06890, -1.4001 0.1741, -0.07950, -1.4851 0.2102, -0.08660, -1.6137 0.2472, -0.09640, -1.7855 0.2844, -0.10270, -1.8832 0.3225, -0.10690, -1.9836 0.3608, -0.10890, -2.0685 0.3991, -0.10830, -2.0751 0.4373, -0.10510, -1.9747 0.4757, -0.09890, -1.8006 0.5137, -0.09070, -1.6185 0.5694, -0.07640, -1.2970 15 Flap element taps 1.0000, 0.00130, -1.0069 0.9365, 0.01390, 0.5766 0.8333, 0.03280, 0.8964 0.7436, 0.04930, 0.8519 0.7049, 0.05670, 0.8449 0.6662, 0.06410, 0.8644 0.6522, 0.01390, -1.0062 0.5969, -0.00020, -1.0229 0.6000, -0.03020, -1.0266 0.6324, -0.04540, -1.0216 0.6667, -0.04880, -1.0268 0.7046, -0.04110, -1.0230 0.7429, -0.03210, -1.0299 0.8333, -0.01400, -1.0287 0.9311, -0.00120, -1.0144 --------- Run Conditions: vel=100.2 ft/s Re=1.003x10^6 AOA=9.00 Flap deflection=-90.00 Totals: Cl=-1.4195 Cdp=0.4579 Cm(c/4)=0.2440 Cs=-0.6743 Ch=0.5648 Main component: Cl=-1.2786 Cdp=-0.0869 Cm=0.4180 Flap component: Cl=-0.1408 Cdp=0.5447 Cm=0.1585 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.1383 0.6175, -0.04610, -1.0734 0.5841, -0.02440, -1.0621 0.5775, 0.01750, -1.0694 0.5777, 0.04660, -1.0754 0.6274, 0.07170, 0.7948 0.5694, 0.08320, 0.7623 0.5112, 0.09370, 0.7742 0.4731, 0.09830, 0.7951 0.4349, 0.10070, 0.7938 0.3960, 0.10120, 0.7849 0.3566, 0.10020, 0.7074 0.3172, 0.09790, 0.6438 0.2778, 0.09440, 0.5807 0.2393, 0.08960, 0.5517 0.2056, 0.08360, 0.5325 0.1633, 0.07610, 0.5095 0.1261, 0.06710, 0.5490 0.0900, 0.05640, 0.5868 0.0571, 0.04390, 0.6913 0.0283, 0.02940, 0.8713 0.0142, 0.01970, 0.9787 0.0081, 0.01410, 0.9952 0.0026, 0.00780, 0.6602 0.0000, 0.00000, -0.2424 0.0037, -0.00840, -1.3843 0.0112, -0.01420, -1.1015 0.0191, -0.01930, -0.8646 0.0397, -0.03030, -0.7943 0.0706, -0.04420, -0.8672 0.1037, -0.05710, -0.8716 0.1384, -0.06890, -1.0868 0.1741, -0.07950, -1.2039 0.2102, -0.08660, -1.3515 0.2472, -0.09640, -1.5468 0.2844, -0.10270, -1.6677 0.3225, -0.10690, -1.7926 0.3608, -0.10890, -1.9021 0.3991, -0.10830, -1.9441 0.4373, -0.10510, -1.8733 0.4757, -0.09890, -1.7297 0.5137, -0.09070, -1.5844 0.5694, -0.07640, -1.2917 15 Flap element taps 1.0000, 0.00130, -1.0610 0.9365, 0.01390, 0.5520 0.8333, 0.03280, 0.8307 0.7436, 0.04930, 0.7633 0.7049, 0.05670, 0.7742 0.6662, 0.06410, 0.7951 0.6522, 0.01390, -1.0494 0.5969, -0.00020, -1.0744 0.6000, -0.03020, -1.0699 0.6324, -0.04540, -1.0655 0.6667, -0.04880, -1.0792 0.7046, -0.04110, -1.0699 0.7429, -0.03210, -1.0786 0.8333, -0.01400, -1.0842 0.9311, -0.00120, -1.0781 --------- Run Conditions: vel=100.3 ft/s Re=1.004x10^6 AOA=12.02 Flap deflection=-90.00 Totals: Cl=-1.2446 Cdp=0.4503 Cm(c/4)=0.2460 Cs=-0.6997 Ch=0.5521 Main component: Cl=-1.0784 Cdp=-0.0699 Cm=0.3712 Flap component: Cl=-0.1662 Cdp=0.5202 Cm=0.1557 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.1141 0.6175, -0.04610, -1.0748 0.5841, -0.02440, -1.0616 0.5775, 0.01750, -1.0728 0.5777, 0.04660, -1.0783 0.6274, 0.07170, 0.7217 0.5694, 0.08320, 0.6780 0.5112, 0.09370, 0.6919 0.4731, 0.09830, 0.7204 0.4349, 0.10070, 0.7225 0.3960, 0.10120, 0.7286 0.3566, 0.10020, 0.6818 0.3172, 0.09790, 0.6185 0.2778, 0.09440, 0.5362 0.2393, 0.08960, 0.4864 0.2056, 0.08360, 0.4448 0.1633, 0.07610, 0.3956 0.1261, 0.06710, 0.4128 0.0900, 0.05640, 0.4165 0.0571, 0.04390, 0.4954 0.0283, 0.02940, 0.6738 0.0142, 0.01970, 0.8257 0.0081, 0.01410, 0.9367 0.0026, 0.00780, 0.8401 0.0000, 0.00000, 0.6422 0.0037, -0.00840, -0.2604 0.0112, -0.01420, -0.3093 0.0191, -0.01930, -0.2228 0.0397, -0.03030, -0.3018 0.0706, -0.04420, -0.4581 0.1037, -0.05710, -0.5282 0.1384, -0.06890, -0.7640 0.1741, -0.07950, -0.9041 0.2102, -0.08660, -1.0669 0.2472, -0.09640, -1.2764 0.2844, -0.10270, -1.4148 0.3225, -0.10690, -1.5640 0.3608, -0.10890, -1.6905 0.3991, -0.10830, -1.7596 0.4373, -0.10510, -1.7208 0.4757, -0.09890, -1.6085 0.5137, -0.09070, -1.4942 0.5694, -0.07640, -1.2340 15 Flap element taps 1.0000, 0.00130, -1.0485 0.9365, 0.01390, 0.5585 0.8333, 0.03280, 0.7850 0.7436, 0.04930, 0.6847 0.7049, 0.05670, 0.7003 0.6662, 0.06410, 0.7280 0.6522, 0.01390, -1.0609 0.5969, -0.00020, -1.0821 0.6000, -0.03020, -1.0779 0.6324, -0.04540, -1.0633 0.6667, -0.04880, -1.0774 0.7046, -0.04110, -1.0773 0.7429, -0.03210, -1.0758 0.8333, -0.01400, -1.0739 0.9311, -0.00120, -1.0590 --------- Run Conditions: vel=99.9 ft/s Re=1.000x10^6 AOA=14.98 Flap deflection=-90.00 Totals: Cl=-1.0670 Cdp=0.4545 Cm(c/4)=0.2478 Cs=-0.7149 Ch=0.5451 Main component: Cl=-0.8782 Cdp=-0.0461 Cm=0.3230 Flap component: Cl=-0.1888 Cdp=0.5006 Cm=0.1532 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.0981 0.6175, -0.04610, -1.0948 0.5841, -0.02440, -1.0861 0.5775, 0.01750, -1.1056 0.5777, 0.04660, -1.0949 0.6274, 0.07170, 0.6508 0.5694, 0.08320, 0.5966 0.5112, 0.09370, 0.6092 0.4731, 0.09830, 0.6297 0.4349, 0.10070, 0.6385 0.3960, 0.10120, 0.6384 0.3566, 0.10020, 0.6242 0.3172, 0.09790, 0.5974 0.2778, 0.09440, 0.4984 0.2393, 0.08960, 0.4144 0.2056, 0.08360, 0.3425 0.1633, 0.07610, 0.2797 0.1261, 0.06710, 0.2561 0.0900, 0.05640, 0.2204 0.0571, 0.04390, 0.2474 0.0283, 0.02940, 0.3699 0.0142, 0.01970, 0.5041 0.0081, 0.01410, 0.6518 0.0026, 0.00780, 0.7573 0.0000, 0.00000, 0.9850 0.0037, -0.00840, 0.5522 0.0112, -0.01420, 0.2780 0.0191, -0.01930, 0.2874 0.0397, -0.03030, 0.1231 0.0706, -0.04420, -0.0948 0.1037, -0.05710, -0.2233 0.1384, -0.06890, -0.4544 0.1741, -0.07950, -0.6204 0.2102, -0.08660, -0.7970 0.2472, -0.09640, -1.0131 0.2844, -0.10270, -1.1746 0.3225, -0.10690, -1.3315 0.3608, -0.10890, -1.4837 0.3991, -0.10830, -1.5725 0.4373, -0.10510, -1.5681 0.4757, -0.09890, -1.4841 0.5137, -0.09070, -1.4007 0.5694, -0.07640, -1.1791 15 Flap element taps 1.0000, 0.00130, -1.0943 0.9365, 0.01390, 0.5505 0.8333, 0.03280, 0.7110 0.7436, 0.04930, 0.5978 0.7049, 0.05670, 0.6159 0.6662, 0.06410, 0.6445 0.6522, 0.01390, -1.0812 0.5969, -0.00020, -1.0966 0.6000, -0.03020, -1.0917 0.6324, -0.04540, -1.0887 0.6667, -0.04880, -1.1030 0.7046, -0.04110, -1.0949 0.7429, -0.03210, -1.0946 0.8333, -0.01400, -1.1006 0.9311, -0.00120, -1.0870 --------- Run Conditions: vel=100.2 ft/s Re=1.001x10^6 AOA=17.97 Flap deflection=-90.00 Totals: Cl=-0.8829 Cdp=0.4530 Cm(c/4)=0.2450 Cs=-0.7033 Ch=0.5321 Main component: Cl=-0.6754 Cdp=-0.0202 Cm=0.2711 Flap component: Cl=-0.2075 Cdp=0.4732 Cm=0.1490 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.0625 0.6175, -0.04610, -1.1053 0.5841, -0.02440, -1.0929 0.5775, 0.01750, -1.1105 0.5777, 0.04660, -1.1010 0.6274, 0.07170, 0.5571 0.5694, 0.08320, 0.4852 0.5112, 0.09370, 0.4928 0.4731, 0.09830, 0.5234 0.4349, 0.10070, 0.5359 0.3960, 0.10120, 0.5392 0.3566, 0.10020, 0.5312 0.3172, 0.09790, 0.5287 0.2778, 0.09440, 0.4650 0.2393, 0.08960, 0.3671 0.2056, 0.08360, 0.2630 0.1633, 0.07610, 0.1618 0.1261, 0.06710, 0.1003 0.0900, 0.05640, 0.0223 0.0571, 0.04390, -0.0323 0.0283, 0.02940, -0.0059 0.0142, 0.01970, 0.0357 0.0081, 0.01410, 0.1660 0.0026, 0.00780, 0.3265 0.0000, 0.00000, 0.8263 0.0037, -0.00840, 0.9427 0.0112, -0.01420, 0.7535 0.0191, -0.01930, 0.6584 0.0397, -0.03030, 0.4580 0.0706, -0.04420, 0.2146 0.1037, -0.05710, 0.0517 0.1384, -0.06890, -0.1787 0.1741, -0.07950, -0.3600 0.2102, -0.08660, -0.5423 0.2472, -0.09640, -0.7620 0.2844, -0.10270, -0.9325 0.3225, -0.10690, -1.1032 0.3608, -0.10890, -1.2704 0.3991, -0.10830, -1.3817 0.4373, -0.10510, -1.4052 0.4757, -0.09890, -1.3479 0.5137, -0.09070, -1.2908 0.5694, -0.07640, -1.1088 15 Flap element taps 1.0000, 0.00130, -1.1020 0.9365, 0.01390, 0.5550 0.8333, 0.03280, 0.6070 0.7436, 0.04930, 0.4836 0.7049, 0.05670, 0.5133 0.6662, 0.06410, 0.5584 0.6522, 0.01390, -1.0965 0.5969, -0.00020, -1.1124 0.6000, -0.03020, -1.1078 0.6324, -0.04540, -1.1032 0.6667, -0.04880, -1.1124 0.7046, -0.04110, -1.1075 0.7429, -0.03210, -1.1171 0.8333, -0.01400, -1.1188 0.9311, -0.00120, -1.1016 --------- Run Conditions: vel=100.6 ft/s Re=1.006x10^6 AOA=19.97 Flap deflection=-90.00 Totals: Cl=-0.7228 Cdp=0.4323 Cm(c/4)=0.2335 Cs=-0.6531 Ch=0.4988 Main component: Cl=-0.5143 Cdp=0.0028 Cm=0.2264 Flap component: Cl=-0.2085 Cdp=0.4295 Cm=0.1400 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -1.0081 0.6175, -0.04610, -1.0750 0.5841, -0.02440, -1.0633 0.5775, 0.01750, -1.0806 0.5777, 0.04660, -1.0714 0.6274, 0.07170, 0.4801 0.5694, 0.08320, 0.3727 0.5112, 0.09370, 0.3689 0.4731, 0.09830, 0.4026 0.4349, 0.10070, 0.4237 0.3960, 0.10120, 0.4325 0.3566, 0.10020, 0.4218 0.3172, 0.09790, 0.4307 0.2778, 0.09440, 0.4054 0.2393, 0.08960, 0.3443 0.2056, 0.08360, 0.2252 0.1633, 0.07610, 0.0864 0.1261, 0.06710, -0.0121 0.0900, 0.05640, -0.1301 0.0571, 0.04390, -0.2579 0.0283, 0.02940, -0.3299 0.0142, 0.01970, -0.4055 0.0081, 0.01410, -0.3211 0.0026, 0.00780, -0.1264 0.0000, 0.00000, 0.3223 0.0037, -0.00840, 0.9802 0.0112, -0.01420, 0.9384 0.0191, -0.01930, 0.8466 0.0397, -0.03030, 0.6510 0.0706, -0.04420, 0.4106 0.1037, -0.05710, 0.2415 0.1384, -0.06890, 0.0071 0.1741, -0.07950, -0.1765 0.2102, -0.08660, -0.3594 0.2472, -0.09640, -0.5842 0.2844, -0.10270, -0.7576 0.3225, -0.10690, -0.9433 0.3608, -0.10890, -1.1142 0.3991, -0.10830, -1.2425 0.4373, -0.10510, -1.2674 0.4757, -0.09890, -1.2231 0.5137, -0.09070, -1.1880 0.5694, -0.07640, -1.0291 15 Flap element taps 1.0000, 0.00130, -1.0664 0.9365, 0.01390, 0.5582 0.8333, 0.03280, 0.5117 0.7436, 0.04930, 0.3635 0.7049, 0.05670, 0.4071 0.6662, 0.06410, 0.4661 0.6522, 0.01390, -1.0657 0.5969, -0.00020, -1.0821 0.6000, -0.03020, -1.0731 0.6324, -0.04540, -1.0575 0.6667, -0.04880, -1.0671 0.7046, -0.04110, -1.0597 0.7429, -0.03210, -1.0713 0.8333, -0.01400, -1.0605 0.9311, -0.00120, -1.0557 --------- Run Conditions: vel=99.7 ft/s Re=0.997x10^6 AOA=23.97 Flap deflection=-90.00 Totals: Cl=-0.3171 Cdp=0.4491 Cm(c/4)=0.1872 Cs=-0.5392 Ch=0.4272 Main component: Cl=-0.1227 Cdp=0.1082 Cm=0.0971 Flap component: Cl=-0.1944 Cdp=0.3410 Cm=0.1169 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.9177 0.6175, -0.04610, -1.0757 0.5841, -0.02440, -1.0629 0.5775, 0.01750, -1.0795 0.5777, 0.04660, -1.0718 0.6274, 0.07170, 0.1662 0.5694, 0.08320, -0.0673 0.5112, 0.09370, -0.1720 0.4731, 0.09830, -0.1446 0.4349, 0.10070, -0.0786 0.3960, 0.10120, -0.0388 0.3566, 0.10020, -0.0281 0.3172, 0.09790, -0.0106 0.2778, 0.09440, -0.0169 0.2393, 0.08960, -0.0010 0.2056, 0.08360, 0.0092 0.1633, 0.07610, -0.0291 0.1261, 0.06710, -0.1031 0.0900, 0.05640, -0.2969 0.0571, 0.04390, -0.6184 0.0283, 0.02940, -0.9853 0.0142, 0.01970, -1.4024 0.0081, 0.01410, -1.5269 0.0026, 0.00780, -1.3834 0.0000, 0.00000, -1.7205 0.0037, -0.00840, 0.5338 0.0112, -0.01420, 0.9576 0.0191, -0.01930, 1.0015 0.0397, -0.03030, 0.9202 0.0706, -0.04420, 0.7331 0.1037, -0.05710, 0.5750 0.1384, -0.06890, 0.3570 0.1741, -0.07950, 0.1813 0.2102, -0.08660, 0.0040 0.2472, -0.09640, -0.2152 0.2844, -0.10270, -0.3969 0.3225, -0.10690, -0.5924 0.3608, -0.10890, -0.7768 0.3991, -0.10830, -0.9330 0.4373, -0.10510, -0.9947 0.4757, -0.09890, -1.0000 0.5137, -0.09070, -1.0113 0.5694, -0.07640, -0.8750 15 Flap element taps 1.0000, 0.00130, -1.0699 0.9365, 0.01390, 0.4801 0.8333, 0.03280, 0.1423 0.7436, 0.04930, -0.0572 0.7049, 0.05670, 0.0650 0.6662, 0.06410, 0.1819 0.6522, 0.01390, -1.0665 0.5969, -0.00020, -1.0859 0.6000, -0.03020, -1.0658 0.6324, -0.04540, -1.0512 0.6667, -0.04880, -1.0739 0.7046, -0.04110, -1.0758 0.7429, -0.03210, -1.0851 0.8333, -0.01400, -1.0695 0.9311, -0.00120, -1.0961 --------- Run Conditions: vel=100.5 ft/s Re=1.002x10^6 AOA=26.98 Flap deflection=-90.00 Totals: Cl=0.3499 Cdp=0.3725 Cm(c/4)=0.0532 Cs=-0.1732 Ch=0.0970 Main component: Cl=0.3902 Cdp=0.3036 Cm=-0.0904 Flap component: Cl=-0.0403 Cdp=0.0688 Cm=0.0233 Surface Pressure Data 43 Main element taps 0.6276, -0.06090, -0.6607 0.6175, -0.04610, -0.8203 0.5841, -0.02440, -0.8053 0.5775, 0.01750, -0.8181 0.5777, 0.04660, -0.8126 0.6274, 0.07170, -0.4893 0.5694, 0.08320, -0.6587 0.5112, 0.09370, -0.8172 0.4731, 0.09830, -0.8614 0.4349, 0.10070, -0.8494 0.3960, 0.10120, -0.8088 0.3566, 0.10020, -0.8039 0.3172, 0.09790, -0.7803 0.2778, 0.09440, -0.7889 0.2393, 0.08960, -0.7783 0.2056, 0.08360, -0.7751 0.1633, 0.07610, -0.8102 0.1261, 0.06710, -0.8124 0.0900, 0.05640, -0.8341 0.0571, 0.04390, -0.8806 0.0283, 0.02940, -0.9538 0.0142, 0.01970, -1.1914 0.0081, 0.01410, -1.5105 0.0026, 0.00780, -1.6902 0.0000, 0.00000, -3.0329 0.0037, -0.00840, -0.1179 0.0112, -0.01420, 0.7493 0.0191, -0.01930, 0.9284 0.0397, -0.03030, 0.9969 0.0706, -0.04420, 0.9109 0.1037, -0.05710, 0.7952 0.1384, -0.06890, 0.6177 0.1741, -0.07950, 0.4709 0.2102, -0.08660, 0.3181 0.2472, -0.09640, 0.1245 0.2844, -0.10270, -0.0421 0.3225, -0.10690, -0.2230 0.3608, -0.10890, -0.3970 0.3991, -0.10830, -0.5523 0.4373, -0.10510, -0.6267 0.4757, -0.09890, -0.6531 0.5137, -0.09070, -0.6866 0.5694, -0.07640, -0.6027 15 Flap element taps 1.0000, 0.00130, -0.8844 0.9365, 0.01390, -0.3561 0.8333, 0.03280, -0.7006 0.7436, 0.04930, -0.6720 0.7049, 0.05670, -0.5632 0.6662, 0.06410, -0.4926 0.6522, 0.01390, -0.8041 0.5969, -0.00020, -0.8241 0.6000, -0.03020, -0.8096 0.6324, -0.04540, -0.7876 0.6667, -0.04880, -0.7949 0.7046, -0.04110, -0.7975 0.7429, -0.03210, -0.8027 0.8333, -0.01400, -0.8160 0.9311, -0.00120, -0.8835